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Application-Permit
I Garfield County Building & Planning Department 108 8th Street, Suite #401 Glenwood Springs, Co. 81601 Office:970·945·8212 Fax: 970·384-3470 Inspection Line: 970·384-5003 Building Permit No. Parcel No: 2139-163-00-014 Locality: Job Address: ___ 270Q_~Jear Creek Rd. DeBeque Use of Building: compr~~sor building __ Owner: Chevron Inc. Contractor: Elkhorn Construction Inc. ------~------- Fees: Plan Check: $ 1,468.58 Septic: Bldg Permit: $ ___ 2,259.35_ Other Fees: Total Fees: $ 3!727.93 --~,-- Clerk: ~-Jtcr~CT Date: Id;-ti:\J~ I I 2 3 4 5 6 7 8 9 lO II 12 GARFIELD COUNTY BUILDING PERMIT APPLICATION 108 s• Street, Suite401, Glenwood Springs, Co 81601 Phone: 970-945-82121 Fax: 970-384-3470 i Inspection Line: 970-384-5003 ~~v.narfis:ld-countv~~ Parcel No: (this infonnation is available at the-assessors office 970-945-9134} 2139-163-00-014 Job Address: (if an address has not been assigned. please provide Cr. Hwy or Street Name & City) or and legal de-scription 2700 Clear Creek Road, p .0. De Beaue CO 81630-CPF located 2.5 miles north-northeast of end of CR 211 ·about 19.5 north-northeast of De Beaue Lot No: NA Block No: Subd./ Exemption; Owner: (property owner) Mailing Address: 11111 S. Wilcrest Drive Ph: Alt Ph: Chevron U.SA Inc. Houston. TX 77099 (281) 561-4991 (970) 257-6042 Contractor: Mailing Address::?181 45 1/2 Road Ph: AltPh: Elkhorn Construction, Inc.* D~l B~que. CO 81f330 (970) 283-1009 (970) 625-4180 Architect J Engineer: Rodney Burrows Mailing Address: 12567 W. Cedar Drive. Ph: A It Ph: ZAP Enor & Cons! Services. Inc. Suite 210. Lakewood. CO 80228 (720) 529-4430 (971) 533-6665 ~-Ft. o(Building: Sq. Ft, or Acres of lot: Height: No. ofFioors: 8,160 fl' (53ft X 154ft) 140,600 sq. ft. (CPF primary pad) 40 fl Single story _Use ofBui,ldin@: Comp·ressor uilding.-::compresses natural gas far insertion into a pipeline and transfer oft'site for sales Describe Work: - Foundation installation. placement of modular unit. and utility hookups Class of Work: ~New o Alteration o Addition Garage: Septic: To be perrni\1erJ wl:h CP~ NA o Attached c Detached (& ISDS restroom bldg oCommunity Driveway Permit: NA (,II:. .d' Owners valuation of Work: s 1.179.900 NOTICE Box 296, Authorin·. This applicaticm for a Building Permit must be signed by the Owner of the prop~:rty, described above. or an authorize<! agent. If the signature below is not that of the Owner. a scp;uatc letter Qfauthority, ~ig.ocd by the Owner. must be pr(n•id.:d with this Application. Legal Access. A Building Pcnnh cmmot bo! issued without proof oflo.:gal and adequate access to the properly for purposes of inspections by the Building Department. Oth\'r Perinits. Multiple separate pcnni1s may be required: (I) Sunc Electrical Pemtit, (2} County ISDS Permit, (3) 1\notbcr permit required for usc on the property identified abo\'C, e.g. State or Co1,1nty Highway/ Road Access or a State Wastewater Discharge Permit. Void Permit. A Building Permit becomes null and void if the work amhoriz~>d i~ not commenced within 180 days of the date of issuance and if work is ~uspcndcd or abandoned fer 11 period of 1 SO days after commencement. CERTIFICATIO:'II l hereby certify that I have read this Application and that the infonnation contained abc.wc is true and correct, I understand that the Building Department accepts the Application, ·along with the plans and specifications and other data submined by me or on my behalf (submittals), bMcd upon my ccnifkaticm as to accuracy. As'sull'ling completeness of the submittals and appro\'al of this ApplkatWn, a Buildin!! Penn it will be issued granting permission t<> me. a$ Owner. to tonstructthe structurc(s) and facilities detailed on the submitfais. reviewed by the Building DCpartmcnt. ln consideration nf the issuance of the Building Penn it. I agn:e thnt t and my agents will comply with provision~ of any fcd~ral. state or local law rcg\lloting the work ~nd the Garfield County Building Code, ISDS rcgo~lations and applicable land use rcgul;ttion~ (County RegulmimllS)). 1 a~know!ctlg•~ that th"' Building !'cnuit may be su~p>.~tlded or rcvok..:d, upon notkc from th(' County. if\bc location, comtructionorusccfthestruct\!rc(s) and faeility{ics). dc~-.ribOO aboH•. ate not in ~omp!i;.mcc with Ccunty Rcgulatilm(s) or tmy other applicubh: bw. 1 hereby gf.mt permissiOn 10 the Building Dcpatlmcmto enter the propcny, described above, to in~pcct the work. I further acknowledge that the issuance of the Building Pcm1it docs not pr.;owntthe Building Official fN:lm: ( l) requiring the correction of errors in the submittals, if tally, discovered af\:cr iss Wince: or (2) stopping construction or use of the structure(s) or faci!ity(les) if su~h i~ in \·iolation of County Rcgu!ation(s) or M}' other npplicabk: law. Review oftl1is Applkalion, including submina!s, nnd inspco;thms of !h.; work by the Building Department do not constitute an acceptance of responsibility or \!ability by the County <)f errors, omi$Si0lls or discrepancies. As the Owner, l acknowledge that responsibility for wmpliancc wi!h federal. state and local laws and County Regulations rest whh me and my uuthorizcd agcnl~. including without limiWtlon my !lrthito:ct do:si£1lcr, ..::nginccr :~m!t nr hui!dcr. l HERCBY ACKNOWLEDGE THAT J HAVE READ AND UNDERSTAND TUE !'\!OTIC F. & CERTIFICATIO:\' ABOVE: i2:(_ 1 /i i1 -·" -· 12/;jJ,OC".Q_ ";;/ ~c.ii c l. ,··~~/!..( .. 7.· lA, 1-'t· mvNER siGNA''iuiiE ---··· --·· DATE ,• Elkhorn Constructton, Inc wtll mstall foundatron and place Ul•ll URS Washington Division assembled permit application !Contact. Sally Cu!finl)URS Washill.,.Q!on Division. 1800 E Union Ave .. Suite 100 Denver, CO 80237 Office 303-843-2219 Cell 303-526-65141 . STAFF SE ONLY Special Conditions: 2lkit/i X, ¥ o/1, 2:6 Adjusted Valuation: Plan Check Fee: Pennit Fcc: Manu home Fcc: Mise Fees: 02~4Q0,90 1446,5'6 2::29'1,05 ISDS Fee: Total Fees: Fees Paid: ~~t~l/ flCq"'' Uatc: ISDS No & Issued Date: '31 z. 7-/'1/!J L){)\l\ ~d-'L\ }0 Setbacks: OCC Group: Const Type: v Zoning: B'§DEPT: . • l'I.NG DEPT: v 12-LHL~ 1~·~~~~. k2-LHL<r2 ~\~~ APPROVAL--· '"""''\: DATE-~ APPROVAI. DATE GARFIELD COUNTY BUILDING AND PLANNING 970-945-8212 MINIMUM APPLICATION REQUIREMENTS FOR CONSTRUCTION OF COMMERCIAL OR MULTI-FAMILY RESIDENTIAL BUILDINGS Including NEW CONSTRUCTION ADDITIONS ALTERATIONS And MOVED BUILDINGS In order to understand the scope of the work intended under a permit application and expedite the issuance of a permit it is important that complete information be provided. When reviewing a plan and it's discovered that required information has not been provided by the applicant, this will result in the delay of the permit issuance and in proceeding with building construction. The owner or contractor shall be required to provide this information before the plan review can proceed. Other plans that are in line for review may be given attention before the new information may be reviewed after it has been provided to the Building Department. Please review this document to determine if you have enough information to design your project and provide adequate information to facilitate a plan review. Also, please consider using a design professional for assistance in your design and a construction professional for construction of your project. Any project with more than ten (10) occupants requires the plans to be sealed by a Colorado Registered Design Professional. To provide for a more understandable plan and in order to determine compliance with the building, plumbing and mechanical codes, applicants are requested to review the following checklist prior to and during design. Plans to be included for a Building Permit must be on draft paper at least 18"x 24'"' and drawn to scale. 1 Plans must include a floor plan, a concrete footing and foundation plan, elevations all sides with decks, balcony steps, hand rails and guard rails, windows and doors, including the finish grade and original grade line. A section showing in detail, from the bottom of the footing to the top of the roof, including re-bar, anchor bolts, pressure treated plates, floor joists, wall studs and spacing, insulation, sheeting, house-rap, (which is required), siding or any approved building material. Engineered foundations may be required. Check with the Building Department. A window schedule. A door schedule. A floor framing plan, a roofing framing plan, roof must be designed to withstand a 40 pound per square foot up to 7,000 feet in elevation, a 90 M.P.H. windspeed, wind exposure B or C, and a 36 inch frost depth. All sheets need to be identified by number and indexed. All of the above requirements must be met or your plans will be returned. All plans submitted must be incompliance with the 2003 IBC, IPC, IMC and IFGC. Applicants are required to indicate appropriately and to submit completed checklist at time of application for a permit: 1. Is a site plan included that identifies the location of the proposed structure, additions or other buildings, setback easements, and utility easements showing distances to the property lines from each comer of the proposed structure prepared by a licensed surveyor and has the surveyors signature and professional stamp on the drawing? Slopes of 30% or more on properties must be show on site plan. (NOTE: Section 106.2) Any site plan for the placement of any portion of a structure within 50 ft. of a property line and not within a previously surveyed building envelope on a subdivision final plat shall be prepared by a licensed surveyor and have the surveyors signature and professional stamp on the drawing. Any structure to be built within a building envelope of a lot shown on a recorded subdivision plat, shall include a copy of the building envelope as it is shown on the final plat with the proposed structure located within the envelope. Yes x 2. Does the site plan when applicable include the location of the I.S.D.S. (Individual Sewage Disposal System) and distances to the property lines, wells (on subject property and adjacent properties), streams or water courses? This information must be certified by a licensed surveyor with their signature and professional stamp on the design. Yes No X Not necessary for this project ___ ISDS will be permitted ~ith permanent restroom butldmg 3. Does the site plan indicate the location and direction of the State, County or private road accessing the property? Yes x 4. Is the l.S.D.S. (Individual Sewage Disposal System) designed, stamped and signed by a Colorado Registered Engineer? 2 Yes __ _ No Not necessary for this project X ISDS will be permitted wlth permanent restroom building 5. Are the plans submitted for application review construction drawings and not drawings that are stamped or marked identifYing them as "Not for construction, for permit issuance only", "Approval drawings only", "For permit issuance only" or similar language? Yes x No__ Not necessary for this project __ _ 6. Do the plans include a foundation plan indicating the size, location and spacing of all reinforcing steel in accordance with the uniform building code or per stamped engineered design? Yes_x_ No Not necessary for this project __ 7. If the building is a pre-engineered structure, is there a stamped, signed engineered foundation plan for this building? Yes_x_ No__ Not necessary for this project __ 8. Do the plans indicate the location and size of ventilation openings for under floor crawl spaces and the clearances required between wood and earth? Yes__ No__ Not necessary for project_x_ 9. Do the plans indicate the size and location of the ventilation openings for the attic, roof joist spaces and soffits? Yes__ No__ Not necessary for this project_x_ 10. Do the plans include design loads as required under the IBC or IRC for roof snowloads, (a minimum of 40 .pounds per square foot in Garfield County)? Yes_x_ No__ Not necessary for this project __ 11. Do the plans include design loads as required for floor loads under the IBC or IRC? Yes_x_ No__ Not necessary for this project __ 12. Does the plan include a building section drawing indicating foundation, wall, floor, and roof construction? Yes_x_ No__ Not necessary for this project __ 13. Is the wind speed and exposure design included in the plan? Yes_x_ No__ Not necessary for this project __ 14. Does the building section drawing include size and spacing of floor joists, wall studs, ceiling joists, roof rafters or joists or trusses? Yes_x_ No__ Not necessary for this project __ 15. Does the building section drawing or other detail include the method of positive connection of all columns and beams? Yes_x_ No__ Not necessary for this project __ 3 16. Does the elevation plan indicate the height of the building or proposed addition from the undisturbed grade to the midpoint between the ridge and eave of a gable or shed roof or the top of a flat roof? (Check applicable zone district for building height maximum) Yes_X_ No__ Not necessary for this project __ 17. Does the plan include any stove or zero clearance fireplace planned for installation including make and model and Colorado Phase II certifications or Phase II EPA certification? Yes No Not necessary for this project_x_ 18. Does the plan include a masonry fireplace including a fireplace section indicating design to comply with the IBC or IRC? Yes__ No Not necessary for this project_x_ 19. Does the plan include a window schedule or other verification that egress/rescue windows from sleeping rooms and/or basements comply with the requirements of the IBC oriRC? 20. 21. 22. 23. 24. 25. Yes No Not necessary for this project_x_ Does the plan include a window schedule or other verification that windows provide natural light and ventilation for all habitable rooms? Yes No Not necessary for this project x ------ Do the plans indicate the location of glazing subject to human impact such as glass doors, glazing immediately adjacent to such doors; glazing adjacent to any surface normally used as a walking surface; sliding glass doors; fixed glass panels; shower doors and tub enclosures and specify safety glazing for these areas? Yes__ No Not necessary for this project_x_ Do the plans include a complete design for all mechanical systems planned for installation in this building? Yes x No · Not necessary for this project __ _ Have all areas in the building been accurately identified for the intended use? (Occupancy as identified in the IBC Chapter 3) Yes_x_ No Not necessary for this project __ _ Does the plan indicate the quantity, form, use and storage of any hazardous materials that may be in use in this building? Yes_x_ No__ Not necessary for this project __ Is the location of all natural and liquid petroleum gas furnaces, boilers and water heaters indicated on the plan? Yes__ No __ . . X The building will not be heated or Not necessary for this proJeCt __ air conditioned 4 26. 27. 28. 29. 30. 31. 32. 33. 34. 35. Do the plans indicate the location and dimension of restroom facilities and if more than four employees and both sexes are employed, facilities for both sexes? Yes__ No__ Not necessary for this gr~li)Gt X Restrooms located at separate facility ut! tng Do the plans indicate that restrooms and access to the building are handicapped accessible? Yes __ No __ Not necessary for this ~rO;j@Gt X urlarng Restrooms located at separate facility Have two (2) complete sets of construction drawings been submitted with the application? Yes x No Have you designed or had this plan designed while considering building and other construction code requirements? Yes_x_ No__ Not necessary for this project __ Does the plan accurately indicate what you intend to construct and what will receive a final inspection by the Garfield County Building Department? Yes_x_ No __ Do your plans comply with all zoning rules and regulations in the County related to your zone district? For corner lots see supplemental section 5.05.03 in the Garfield County Zoning Resolution for setbacks. Yes X No __ _ Do you understand that approval for design and/or construction changes are required prior to the implementation of these changes? Yes_x_ No __ Do you understand that the Building Department will collect a "Plan Review" fee from you at the time of application and that you will be required to pay the "Permit" fee as well as any "Septic System" or "Road Impact" fees required, at the time you pick up your building permit? Yes_x_ No __ Are you aware that you are required to call for all inspections required under the IBC including approval on a final inspection prior to receiving a Certificate of Occupancy and occupancy of the building? Yes_X_ No __ Are you aware that the Permit Application must be signed by the Owner or a written authority be given for an Agent and that the party responsible for the project must comply with the Uniform Codes? Yes_x_ No __ 5 36. Are you aware that you must call iu for an inspection by 3:30 the business day before the requested inspection in order to receive it the following business day? Inspections will be made between 7:30a.m. and 3:30p.m. Monday through Friday. Inspections are to be called in to 384-5003. 3 7. Are you aware that requesting inspections on work that is not ready or not accessible will result in a $50.00 re-inspection fee? Yes x No ___ _ 38. Are you aware that prior to issuance of a building permit you are required to show proof of a driveway access permit or obtain a statement from the Garfield County Road & Bridge Department stating one is not necessary? You can contact the Road & Bridge Department at 625-8601. Yes x No ____ _ 39. Do you understand that you will be required to hire a State of Colorado Licensed Electrician and Plumber to perform installations and hookups? The license number will be required at time of inspection. Yes X No ____ _ 40. Are you aware, that on the front of the building permit application you will need to fill in the Parcel/ Schedule Number for the lot you are applying for this permit on prior to submittal of the building permit application? Your attention in this is appreciated. Yes X No. ___ _ 41. Do you know that the local fire district may require you to submit plans for their review of fire safety issues? Yes X No (Please check with the building department about this requirement) 42. Do you understand that if you are planning on doing any excavating or grading to the property prior to issuance of a building permit that you will be required to obtain a grading permit? Yes x 43. Did an Architect seal the plans for your commercial project? State Law requires any commercial project with occupancy of more than 10 persons as per Section 1004 of the IBC to prepare the plans and specifications for the project. Yes No Not Necessary for this project __ x __ _ I hereby acknowledge that I have read, understand, and answered these questions to the best of my ability. 6 Signature ffi;j,u.fA/ C:, · ~/ /{/1--tJ~ Date 1; /0 /zoo'fj Phone: '2?/1-:)2 9 -7/'S:l(days); -z_'i!' I-4J¥71b--IZ Cf ::L (evenings) Project Address: '2700 C.Ll::AR CREFK f:lo. PC. t3ox 2% De-i:St=ctuf CO 'iiib30 I I i Note: If you answered "No" on any of these questions you may be required to provide this information at the request of the Building Official prior to beginning the plan review process. Delays in issuing the permit are to be expected. Work may not proceed without the issuance of the permit. *If you have answered "Not necessary for this project" on any of the questions and it is determined by the Building Official that the information is necessary to review the application and plans to determine minimum compliance with the adopted codes, please expect the following: A The application may be placed behind more recent applications for building permits in the review process and not reviewed until required information has been provided and the application rotates again to first position for review. R Delay in issuance of the permit. C. Delay in proceeding with construction. *If you answered "No" to this question the circumstances described in the question could result in a "Stop Work Order" being issued or a "Certificate of Occupancy" not being issued. Bpcomm October 2006 7 UIL lNG GARFIELD COUNTY, COLORADO INSPECTION WILL NOT BE MADE UNLESS THIS CARD IS POSIED ON THE JOB . Date Issued _____co} (}r,__,J-'--\-0----""~---Permit No.J-t-1-1\cts~--- AGREEMENT In consideration of the issuance of the permit, the applicant hereby agrees to comply with all laws and regulations related to the zoning, location; construction and erection of the proposed structured for which this permit is granted, and further agrees that if the above said regulations are not fully complied with in the zoning, location, erection and construction of the above described st~ucture, the permit may then be revoked by notice from the County Building department and IMMEDIATELY BECOME NULL AND VOID. useCDMpl'I'S:sn:_pv.i(~q....---------- Address or Legal Description~ fu.,e_k \<d_ u~"-"'f_.,e_,_..,_ ___ _ Owner _tb.,ev""-Lron-""''-'------------Contractor Elldlor-n Building Permi!Type tt>M~oifA[ This Card Must Be Posted So It Is Plainly Visible From The Street Until Final Inspection INSPECTION RECORD Footing Driveway Foundation I Grouting Insulation '}_-3~D'{ )(j1ll[ Underground Plumbing Drywall Rough Plumbing EJedrk final (by State inspector) (Prior to Final) J..~$-/0 LA/ Rough Mechanical Septic Final v Gas Piping FINAL i}tvL-1---11~rv Eiectrk !Rough {by State 1nspe{:tor) (You Must Ca!! For Finollns!3e<:tion) (P>ior to Framing) Notes Framing (to in dude Roof in place & Windows & Doors installed & Firestopping in pia<: e) THIS PERMIT IS NOT TRANSFERABLE For ~nspe'l:"tion Cat! 970~384~5003 Offi1.:e 970~945~8212 108 8th Street, Suite 401 G1enwood Springs, Co!orado 81601 ~::eR_ov_ED_ldd~A~_o.::_t:'C.----D-0 ::T£~T;;;'-JAni--D~l'-'~"'-\}-l-l-} or:___ __ _ PROTECT PERM~WEATHEto;;AGE t (DO NOT LAMINATE) ~ 'J ~ ......... ~ ~ ~ ~ ....... I ~ ~· ·ct "'t: '<J"' 1:)0 t IJ'.-~ i ~ ~ I rl\ ~ <::10 l I '-b ~ c() ' -f{J t J ~ ~ ( -"' \~ ~ ()--.... ~ ....._ 'W-~ 0 ::i -I ~ ':') 0 ~ ~ I j <.\ ~ ~ ~ N '\Ill """ \1 '~.( ~ \b ~ fi ~ \N I '.) - l ~ ~ ~ '-.) I ~ 1 - Cl ~ ~ ~ ~ "' ~ ~ V1 ~ 0 w ~ -} I "-t ·~ 1--~ ~ ~ ~ ~ '-.) ~ \ ~ 1 ~ ~ "'( ~' ~ ~ 'No. _____ 1_,_1,_,1"'9,_5 -'---Assessor's Parcel No. 2139-163-00-014 Date __ ..:.1=2/..:.11c:./::.20:.:0:.::8_ BUILDINGPI!RMIT CARD Job Address __ 2""7'-'0"'0~C~Ie~a,_._r-"C:JCre~e'-"k'-'-r"-d,L.!D~e'-!:B""e.,.q~ue~-------------------- Owner ____ ..::C:.::h"'e"'"vr:.::o"'n..::U:.::S:.:.A:__ _____ Address 11111 S.wilcrestdr, TX Phone #970-257-6042 Contractor Elkhorn Construction Address 12567 45 1/2rd, DeBeque Phone # 970-283-1009 Setbacks: Front _____ . Rear _____ RH _____ LH _____ Zoning ____ _ compressor bldg f natural gas !/insert into pipeline (A·2) Soils Test=-..,--,;--------- Footing hAd!~ Foundati~J11/ tft...IJ.. Grout ___________ _ Underground Plumbing _____ _ Rough Plumbing-------- Framing ___________ _ Insulation-----------Roofing ___________ _ Drywall ------------ Gas Piping----------- INSPECTIONS Weatherproofing __________ _ Mechanical ____________ _ Electrical Rough (State)--------- Electrical Final (State) _________ _ Final /Checklist Completed? ___ _ Certificate Occupancy # ---------Date ___________ _ Septic System#~--------- Date------------Final ___________ _ Other--------------- NOTES (continue on back) COUNTY OF GARFIELD-BUILDING DEPARTMENT CORRECTION NOTICE 108 8th St., Suite 401 Glenwood Springs, 'Colorado Phone (970) 945-8212 Job located at ot 7&6 ~Ad--~&!: Permit No. !1195 I have this day inspected this structure and these premises and found the following corrections needed: aa:£a11 for Re-lnspection 0 $50.00 Re-lnspection Fee must be paid prior to Re-lnspection You are hereby notified that the above correction must be inspected before covering. When correction(s) have been made, call for inspection at 970-384-5003. Date /-qv.-.(!) 9 20 ~,_,.----c::::::--- Building Inspector ~dZ~ ------ Phone (970) 945-8212 AUG 3 1 2009 THUNDER MOUNTAIN TESTING ••• 2973 F. Road • Gnmd Jundioa, CO 81504 (970) 256-9965/ CeU (970) 210..7008/ FAX (970) 314-7067 Elkhorn Construction 218145 Y, Road DeBeque, CO 81630 ATIN: Mr.JohnDick RE: Chevron Compressor Building 2700 Clear Creek Road DeBeque,CO Dear Mr. Dick, August 25, 2009 Pernrit # 11195 As requested, struetw:al steel special inspection was conducted per the ffiC 2003 Edition • Chapter 17: Structural Tests aod Speciallnspeetion aod Garfield County requirements. I arrived on site at 9:00 AM. I met with Mr. Rob Ziegler with Elkhorn Construction to review areas ready for inspection. Visualre-inspection was conducted at the Roof Framing Plan level on the repairs to theW' & o/.'' ASTM A32S High Strength beam to beam, beam to column and crane rai1 bolted connections. Project bolt tension requiremenls indicate "Snug Tiglrt" as referenced on the approved jobsite drawings provided by VP Buildings, Inc. in Memphis, TN: Job 07-27053 dated 1/16/07: General Notes-A32S & A490 Bolt Tightening Requirements. As a minimum, 10"/0 of all eonnectioDs, but llOt less 1hao two bolts per connection were inspected for proper bolt tension requiremenls as 1oquiled for Periodic Inspection per Table 1704.3 -Item 2.a per Chapler 17 of the me. Inspection was conducted at grid line A-D & I • 10. Bolted COJII!eCiicoJs inspected wen: obsened to be adequately tensioned per project requirements. During my iospectiotiS on site I spoke with Mr. Rob Jooes fur the review of two eacb compressor buildings on site for Chevron at 25-4 Rood: Booster Compressor Pads. Afterreviewiog the appRI'Wed project drawiogs from the building manufur:hlnlr, no column or beam stua:tmal steel oor high slralgdJ bolted c:oouection were listed or observed to be installed at time of illspection. Struelmal Steel aod Bolting Special Inspection is not roquiied fur either building reviewed. Cc: George Lux -Chevron Inspection Report COLORADO STATE ELECTRICAL BOARD INSPECTION REPORT I CORRECTION NOTICE Date Received: 08-FEB-10 Perm~ Number: 671618 Contractor/HomeOwner: SPECIALIZED AUTOMATION SERVICES LLC Address: Type of Inspection: Action: 2700 CLEAR CREEK RD Complete Final Accepted Comments or Corrections: 1) 314.25 Cover, faceplate, luminaires or canopy required for boxes (gutter cover in control room) 2) 35 kv switchgear clerances must be maintained 3) 110.3(B) Listed and labeled equipment shall be installed and used per listing and labeling (em light not working) 4) 210.8 (B)(5) GFI required (Non residential) Sinks 1, where receptacles are installed within 1.8 m (6 ft) of the outside edge of the sink. 5) battery cover required 480.9(8) Batteries, Live Parts. Guarding of live parts shall comply with 110.27 6) Installer on site making corrections Inspectors Name: Cyrus Tuchscher Phone Number: 970-625-5085 Date: 08-FEB-1 0 COLORADO STATE ELECTRICAL BOARD DEPARTMENT OF REGULATORY AGENCIES 1580 logan St. Suite 550 Denver, Colorado 80203-1941 Phone: (303) 894-2985 https://www.dora.state.co.us/plslreal!Ep_ Web_Inspection_GUI.Process_Page Page 1 of 1 2/912010 From: To: CC: Subject: Date: Attachments: Jake Mall Cuffin, Sally; RE: Driveway permit exemption Thursday, November 06, 2008 1:25:38 PM Sally: you are exempt from the dtiveway access permit requirement for this project. Jake -----Original Message----- From: Cuffin, Sally <Sally.Cuffin@wgint.com> Sent: Thursday, November 06, 2008 12:48 PM To: jmall@garfie1d-county.com <jmall@garfie1d-county.com> Subject: Driveway permit exemption Jake, I just realized that I never got an official driveway exemption email from you for buildings at Chevron's Central Production Facility. The facility is located about 2.5 miles north of the end of CR 211 (near the confluence of Tom Creek and Clear Creek). Let me know if you have questions. Thanks! Sally Cuffin (303) 843-2219 (303) 526-6514 (cell) August 29, 2007 Mr. Fred Jarman, Director Garfield County Building & Planning Department 108 81h Street, Suite 401 Glenwood Splings, CO 81601 Re: Autholization to. Represent Chevron - James S. Talbot Senior Counsel Sally Cuffin, Washington Group International Inc. Dear Mr. Beai1: Law Department North America Exploration and Production .Company 1llll s. Wilcrest #N2006 Houston, Texas 77099·4397 Tel 281·561·3536 Fax 281·561·3515 jtalbot@chevron.com Chevron U.S.A. Incc (Chevron) has retained the services of Sally Cuffin of the Washington Group International Inc.. Ms. Cuffin will represent Chevron in facility permitting for our Piceance Project in Garfield County, a role in which she will prepare and submit Special Use Permit Applications, ISDS, building, grading, pipeline, road crossing and other routine construction related applications and information on behalf of Chevron. Ms. Cuffin is als.o authorized to participate in discussions Pflfore appointed and elected boards regarding the various applications, however at such meetings, her authority to legally bind Chevron is limited to the tem1s set forth in the Permit Applications or other written docnments filed on our behalf. Sincerely, cc: Nicole Johnson Timothy Barrett Sally Cuffin CHEVRON PRODUCTION FACILITY PICEAf\JCE BASIN DEVELOPA1EIVJ GARFIELD COUNTY, COLORADO COMPRESSOR BUILDING -FACILITY ZZZ-4003 2 COMPRESSOR BUILDING MANUFACTURED BY ALTA CONSTRUCTION 3 4 5 6 7 RIO BLANCO COUNTY GARFIELD COUNTY ____r----I ---Project Site' New gll Township 55 Range 9BW s~~\ Rifle Silt Cosfle I~ \J lw Parachute !-z3 -----DeBeq·-:-:-:ue:-+-~MES-A-- ---- ---- ---__ _j ~ Exit 62 COUNTY PITKIN COUNTY 2 BUILDING ELEVATIONS NTS FOR 8Ull01NG DETAILS SEE VENDOR DRAWINGS r'Y\IPRC !MASS 11-19-08 CHEVRON PICEANCE CENTRAL PRODUCTION FACILITY COMPP..ESSOR BUILDING GARFIELD COUNTY, COLORADO HVAC CALCULATIONS Summary The proposed compressor building for the Chevron Piceance Central Processing facility will be an unconditioned insulated metal building that will house three (initially) engine-driven compressors with expansion capability for a fourth unit in the future. The compressors are designed to compressed pipeline-quality natural gas in large volumes prior to insertion of the gas stream into a natural gas pipeline. All natural gas process streams within the facility are contained in pressure-rated vessels and pressure-rated process piping. The engines are powered by fuel gas, which is natural gas conditioned within the plant for use within in-plant power and heating equipment. The building is designed to comply with the International Building Code, International Fire Code and International Mechanical Code (2003 edition of each), 2005 National Electrical Code, and API RP 500. Heating Requirements Because of the large volume of air flow required in the building for safety-related ventilation purposes, the building will be unconditioned and unheated (except for heat recovered from the actual process gases and heat given off by the engines and compressors.) Since the building is unconditioned, the requirements of the International Energy Efficiency Code do not apply. Cooling Requirements The building has no air conditioning or cooling equipment. Heat from the compressors will be removed from the building by utilizing large volumes of fresh air exhaust. Ventilation Requirements Because of the presence of large volumes of flammable natural gas within the building, the building will be classified as an H-2 occupancy per the IMC and IBC. For this reason, and to comply with API RP 500, the building is designed for a minimum of 6 air changes per hour of fresh air ventilation, as required per code. For additional safety and redundancy, the building is designed for natural ventilation at a rate of 12 air changes per hour, as well as forced air ventilation at a rate of at least 12 air changes per hour. Summer Operating Conditions In the summer, both natural and forced fresh air ventilation will be utilized to the maximum extent possible to keep heat buildup within the building manageable. Temperatures within the building near the floor area will be very 11ear ambient conditions. Due to the volume of air flow, heat gain through the building skin will make minimal contributions to the overall temperature rise. As the fresh moves through the building, it will be heated by the compressors and engines and will rise vertically above the equipment to exit from the ceiling. Although the temperature rise will be substantial due to this effect, the hot air will be closer to the ceiling where workers will be unlikely to be working. (This building is primarily unmanned, but is designed for occasional maintenance and monitoring by the operating staff.) Winter Operating Conditions In the winter, forced air ventilation can be reduced or eliminated when the temperature drops below the level of personnel comfort within the building. Fresh air ventilation, supplemented by the pull of the engines from the fresh air intake of the engines, will be adequate to maintain 12 air changes per hour natural ventilation. In extreme cold emergencies, the engines will produce enough heat to keep the building functional down to the extreme design temperature of -30 degrees F. In emergency situations below that temperature, if the engines are turned off, the building will cool over a period of 24 to 72 hours, and ventilation can be further reduced by closing some of the louvers to prevent damage to the engines and piping. In between Summer and Winter The forced air ventilation fans can be manually controlled in the seasons between summer and winter to balance heat loss and gain to keep indoor temperatures at the working level reasonably temperate. That is, the staff can keep the fans on when it gets too warm, and turn the fans off when it gets too cool. Summary Calculations are attached that describe the details of our design demonstrating compliance with the IMC. Rodney D. Burrows, PE Page 1 of8 11-1-08 CHJ!;VRON PICEANCE CENTRAL PRODUCTION FACILITY COMPRESSOR BUILDING GARFIELD COUNTY, COLORADO HVAC CALCULATIONS Prepared by J. Stewart, PE, & Rod Burrows, PE Project Associates, Inc. VENTILATION CALCULATIONS (SUMMER): Building Elevation: 61 00' Normal Barometric Pressure: 11.709 psia Calculated Building Volume= L x W x H + 2 (bx2h) where: L = 154'; W =53'; H = 32'; b = 26.5'; h = 8' :.Building Volume= (154) (53) (32) + 2 ( 26.; X 8) = 261,396 ft3 Ventilation Volume@ 12 ACH = (12)(261,396) I 60 = 52,279 ACFM Exhaust Fan Capacity= 27,780 ACFM/fan = 53.1% for each fan Air Cp = 0.24 (Keenan & Kaye Gas Tables) Air Specific Volume= [379.79 x 14.696 x (T +460)] I (23.963 x 11.709 x 520) = 17.53 ft 3/#@ 94°F Caterpillar Heat Rejection @Full Load= 6285 Btu/min (See Cat Gas Engine Tech Data@ 1200 rpm)= 377,100 Btu/hr/unit Ariel Frame Heat Rejection@ Design= 83,500 Btu/ft/unit (From Ariel Compressor Co. through P AI= Houston) Summer Solar Heat Load= 45,789 Btu/hr (R. ButTows' estimate per ASHRAE Fundamentals Sol-Air method, July afternoon) :. Total Summer Heat Gain @ 94°F = = (4ea) (377,100 Btu!hr) + (4ea) (83,500 Btu/br) + 45,789 Btulbr = 1 ,888,189 Btu/hr Air Mass Flow Required for desired 1 oop Temperature Rise Q=mCpL'.T M = Q I (CpL'.T) = 1,888,189 I [(0.24) (10)] = 786,745 #/hr = 13,112 #/min Total Air Volume Flow Requirement (Summer) TVR = (13,112) (17.53) = 229,853 ACFM Combustion Air Flow (CAF) = 3369 ACFM :. Total Combustion Air (TCA) = (4) (3369) = 13,476 ACFM Ventilation Air Requirement (Summer) for l0°F Rise V AR (Summer)= 229,853-13,476 = 216,377 ACFM Page 2 of8 Page 3 ofS :. Supplemental Ventilation (Summer) SV (SurrL'ller): 216,377-52,279 ACFM = 164,098 ACFM This supplemental air requirement to limit heat rise in the building to 1 O"F is equivalent to 3.14 times the 12 ACH requirement. The actual air changes per hour required to meet the Summer IO"F temperature rise is 49.7. There must be an air change every 1.2 minutes to meet the Summer 1 O"F temperature rise, which is impractical. Current Design Louver Area= 4 (9.24) + 10 (18.94) = 226.36 ft 2 Air Velocity@ 12 ACH = 52,279 I 226.36 =231ft/min = 3.85 ft/sec Air velocity@ 49.7 ACH = 229,853/ 226.36 = 1015 ft/min = 46.9 ft/sec = 11.5 rnlhr Page 3 of8 Building Ventilation Assuming 12 ACH via Natural Ventilation (Summer): Ventilation Flow: 52,279 ACFM Engine Combustion Air: 13,476 ACFM Total Building Air Flow: 25,755 ACFM 65,755117.53 3751 #/min 225,060 #lhr :. Temperature Rise= Q/mCp = 1,888,1891 co.24) (225,o6o) =36°F Maximum internal building temperature with only natural ventilation will be approximately 141°F on a 105°F day. (This temperature would be seen at the interior of the ridge vents.) The use of emergency fans or fans of similar capacity will increase building air flow by (2)(27,780 ACFM) or 55,560 ACFM. Total Building Air Flow= 65,755 + 55,560 ACFM = 121,315 ACFM =6920 #/min = 415,225 #/hr Temperature rise= 1,888,189 I (415,225 #/hr) (0.24) = 19°F :.Maximum inside building temperature on 105°F day will be approximately 124°F. Again, the maximum temperature will be seen at the interior of the ridge vents. Temperatures seen near the floor level will be similar to ambient air since the volume of fresh air intake is so high. Page 5 of8 VENTILATION CALCULATIONS (WINTER): Estimated Supplemental Heat Requirement without Compressors Minimum Winter Interior Temperature: 45°F Minimum Winter Ambient Design Temperature: -30°F Minimum ACH without Engines: 12 Air Specific Heat: 0.24 Btu/sq ft •p Air Specific Volume: 13.61 fe/sq ft@ -3o·F Ventilation@ 12 ACH: 52,279 ACFM Heat Requirement: Q = mCpL'.T (60) = (52,279 ACFM) (0.24) (45--30°F) (60) (13.61) = 4.148.517 Btu!hr Estimated Supplemental Heat with Compressors Combustion Air@ 45°F = 13,476 ACFM . . . 13.61 CombustiOn A1r Eqmva1ent@ -3o•F = (13,476 ACFM) (15 _98 ) =11,477 ACFM :. m = (52,279 + 11,4112113.61 = 63,7561 13.61 = 4684 #/min Heat with compressors= (4684) (60 (0.24) (75)-4ea 377,100)-4ea (83,500) = 3.216.32Q Btulhr VENTILATION CALCULATIONS (WINTER): Engines Operating-No Supplemental Heat Minimum Ambient Temperature: -30°F Normal Ventilation without Engines: 12 ACH 52,279 ACFM Combustion Air: 13,476 ACFM Air Specific Heat: 0.24 btu/#/degreeF Air Specific Volume: 13.61 fe/# Total Building Air Flow: 52,279 + 13,476 ACFM 65,755 ACFM 4831 #/min 289,882 #!hr Page 6 of8 Heat from Engines/Compressors: (4ea) (377,100 Btu/br) + (4ea) (83,500 Btu/hr) 1,842,400 Btu!hr :. Winter Temperature Rise without Supplemental Heat and with Compressors Operating: L\T=QjmCp = 1,842,400 Btu!hr / (259,552 #!hr) (0.24 btu/#/degreeF) =26°F :.Building Temperature= -4°F on a -30°F day VENTILATION CALCULATION (WINTER): Vent Air Flov,r Based on Equipment ·Heat Release Combustion air@ 45°F: Design Building Temperature: Design Ambient Temperature: Total Engine Heat Release: Total Compressor Heat Release: Total Equipment Heat Release: 13,476 ACFM 843 #/min 50,598 #!hr 45°F -30°F 4(377,100) = 1,508,400 Btu!hr 4(83,500) = 334,000 Btu!hr I, 84 2, 400 Btu/hr :.Air flow to balance equipment heat release at a building temperature of 45°F is: QT = mCpt.T Is+ mCpflT Is :.1,842,4oo = (50,598) (0.24) (75) 15 + (m) (0.24) (75) 15 (m) (0.24) (75) I 5 = 1,842,400-910,764 so ml 5 = 51.758 #!hr Supplemental Air :. Supplemental Air@ -30°F = (51,758) (13.61) I 60 =l1.740ACFM :. Total Ventilation Intake@ -30°F = (50,598 + 51,758) (13.60) 60 = 23.218 ACFM@ -30°F Page 7 of8 Winter Operation with Single Compressor Unit Combustion Air Flow: -3369 ACFM Air Specific Volume@ 45"F: :. C.A. = 12,650 #lhr Building Design Temperature: 45"F Ambient Temperature: -30°F Total Engine Heat Release: 377,100 Btu/hr Total Compressor Heat Release: 460,600 Btu/hr Air flow to balance equipment heat release is: QT = mCpll T /1 + mCpll TIs 460,600 = (12,650) (0.24) (75) I? ( m) (0.24) (75) Is = 1460,600-(12,650) (0.24) (75)] l (0.24) (75) = 12,939 #/hr of Supplemental Air* Supplemental Air@ -30"F = (12,939) (13.61) I 60 =2935 ACFM :. Total Ventilation Intake= (12,650 + 12,939) = 25,589 #/hr = (25,589) cu.61) 1 6o = 5804 ACFM@ -30"F 22 Pages Attached Page 8 of8 TEMP Ill~ I T liN~~~~;:;' IT~~~~~~o I":~~~::,~~~:;:;" TEMP ·F 'F "F To: To5'F -+ToC 10( +90 We + We ..• 11C 4( ....., -:-w rF -:-w 1349 --:w'F :-w 134.8 BUILDING ENVELOPE CALCULATIONS Bldg Volume= area= r.oof area Wa!!area= 261,396 8162 8470 10971 -,.. -~ -""''"" ~ 41 3f 156 7ci'F 0 60"F ,276 5( -., ,103 1-. cubicft Hl OFF ON ON I PIPING I btiiliU "' lh,- • H::~~:,, biUihi b1t ihi b 126bOC ! I OF 22 COMP TOTAL , •• ,., "'n FORCED TOTAL !CALC'! GAIN GAIN OPEN ~FM FAN 1 F~~ 2 . CFM V~;~· ~ l~~=l ~-t :.. ·~, 261~~>F~F~O~FF~~4-~W~140~~ OFF OFF W140 TOTAL NATURAL ""•••I• ••In• GA .IN OPEN CFM lfi:: h ,... H;-Hii 473 ,316 I 56260 9, 156 YES I ;..-;..- ,552 ;..-2: 28 •.189 I H•l;:;;;;..; 151 I 28140 0 FORCED ! FAN 1 FAN 2 CFM I I 1125~ ON OFF 56280 56280 OFF OFF OFF ~~:~~ CFM otm Rl64( 125 1256( 71. 71. "' T 'F 0. 1--. 1--. 0. ~ 2 4 34. I' · tOOf area 19441 12 R' all r-va!ue Con,,...voent u-value Bldg u-value= 0.083333333 btufhr/degreeF/sqft 1620.083333 btulhr/degreeF Heating capacity of Catco Model CGA 12362G catalytic heater x six heaters x seven heaters HEAT RETENTION CAPACITY CALCULATIONS wt of compressor 21,000 lb wtof engine 40,000 lb wtofframe 10,000 lb wtof mise piping 10,000 lb wtof lube oil 500 lb wt of concrete 3375000 lb hours to cool down from 200F to 45F Heat lost due to Infiltration: Bldg Volume= 1 air change per hour- AirCp Air specific volume O=m Cp deltaT 261,396 4,690 0.24 17.53 mass=4690 cfm/17.53 cftllb= 26.51b/minute 0= 287.51blmin * .24 btullb * 70 Q= 4494.7 btu/min Q= 269682 btu/hr specific ht 0.1220 0.1220 0.1220 0.1220 0.5100 0.2000 cltilb 18000 108000 126000 delta T 155 155 155 155 155 25 Total heat loss case 2 = heat conduction loss + heat infiltration loss btulhr btu/hr btufhr heat retention {btu) 397110 756400 189100 189100 39525 16,875,000 18,446,235 ''" 163.59165 6.816319 I heat loss case 2= 213,303 (32.55% of this is conduction loss or 113rd) How many catalytic heaters will it take to keep warm at45F continuously after engines coo! down? 22.18272 Case 3: S air changes per hour Conduction heat loss stays the same at Fresh air heating requirement increases by six X Total heat loss requirement= 129,607 289,682 1,747,899 btu/hr x6= brulhr 1,618,092 btu/hr of which 7.4% is related to conduction loss through building envelope Chevron rae ~ 'v> >ii' ii. i .i .. · ... WM!WMoM·WW•+·M·W&M•d 3.3 Input Information XXX Title: S. G. COMPRESSOR BUJLDING HEATING & VENTILATION CALCULATIONS Customer: CHEVRON MCBU Project: PICEANCE BASIN/SKINNER RIDGE FIELD Project Spec No: 2033-201-60-SW-0001-01 REV: 0 II Date: 29 JUNE 2007 _____.!. Table 1-Meteorological Data a. Barometric Pressure Pressure 11.143 PSIA b. Ambient Temperature Maximum -Design 105 op Minimum Design -Valley -30 op Minimum Design -Mesa -30 op AJr Cooler-Design Max. 105 op c. Wind Design Code ASCE 7-95 Design Velocity 90 MPH Exposure Factor c Category m Importance Factor 1.15 Prevailing Direction TBD d. Relative Humidity Design 75.0% e. Ice/Frost Line, Below Surface Design 42 Inches f. Seismic Zone Design 0 g. Soil Bearing Capacity Design See Soil Report PSF h. Site Elevation Design-Valley 6200 Feet Above MSL Design -Mesa 8200 Feet Above MSL i. Rainfall Annual Average 20 Inches Monthly -Max. 25 Inches 24 Hour -25 Y r Max. 1.0 Inches I Hour-25 YrMax 1.0 Inches j. Snowfall Annual Average 78.0 Inches Monthly -Max. 15.4 Inches 24 Hour -25 Y r Max. Inches I Hour-25 Yr Max Inches Snow Load Design -Valley 5 Feet Snow Load Design Mesa 20 Feet Snow Load Design 40 PSF k. )Building Interior Temperatures Minimum 45 op Chevron - Title: S. G. COMPRESSOR BUILDING HEATING & VENTILATION CALCULATIONS Customer: CHEVRON MCBU Project: PICEANCE BASIN/SKINNER RIDGE FIELD Project Spec No: 2033-201-60-SW-0001-01 REV: 0 Date: 29 JUNE 2007 Table 2 -General Data Air Changes for Adequately Ventilated Spaces 6 per hour Safety Factor for Air Changes for Natural Ventilation for 2 Adequately Ventilated Spaces Reciprocating Engines Caterpillar G3520B LE Reciprocating Compressors Ariel JGT/4 Building Supplier Alta Construction, Inc. Building Designer VP Buildings, Inc. Building Installed Location Piceance Basin, Skinner Ridge Field -Valley Chevron - Component Helium Hydrogen Oxygen I Argon Nitrogen Methane C02 Ethane Propane Iso-Butane N-Butane !so-Pentane N-Pentane Hexanes+ Total Title: S. G. COMPRESSOR BUILDING HEATING & VENTILATION CALCULATIONS Customer: CHEVRON MCBU Project: PICEANCE BASIN/SKINNER RIDGE FIELD Project Spec No: 2033-201-60-SW-0001-01 REV: 0 Date: 29 JUNE 2007 Table 3 -Gas Composition Normalized Mole % Mass% 0.005 0.001 0.000 0.000 0.012 0.021 0.122 0.184 88.916 76.747 2.428 5.749 5.679 9.188 1.686 4.000 0.337 1.053 0.350 1.095 0.141 0.544 0.105 0.409 0.219 1.009 100.000 100.000 ii ..... . G3520B LE GAS ENGINE TECHNICAL DATA CATERPILLAR® ENGINE SPEED: 1400 FUEL: NAT GAS EFFECTIVE COMPRESSION RATIO: 8:1 FUEL SYSTEM: CAT WlDE RANGE AFTERCOOLER-STAGE 1 MM. INLET (°F): 202 WITH AIR FUEL RA T!O CONTROL AFTERCOOLER-STAGE 2 MM. INLET (0 F): 130 FUEL PRESS. RANGE (PSIG): 15.0 ~ 60.0 JACKET WATER-MAX. OUTLET (°F): 201 MIN. METHANE NUMBER: BO COOLING SYSTEM: JW+OC+1AC, 2AC RATED ALTITUDE (Fl): 5000 IGNITION SYSTEM: ADEM3 AT AIR TO TURBO. TEMP. ("F): 77 EXHAUST MANIFOLD: DRY NOx Emission Level 1 .0 g/bhp-hr COMBUSTION: LOW EMISSION FUEL LHV (BTU/SCF): 905 APPLICATION: INDUSTRIAUPETROLEUM ~G AND EFFICIENCY NOTES LOAD 100% 75% 50% ENGINE POWER {WITHOUT FAN) (1) BHP 1725 1293 862 ENGINE EFFICIENCY (ISO 3046/1) (2) % 37.0 34.9 32.1 ENGINE EFFICIENCY (NOMINAL) (2) % 36.1 34.0 31.3 THERMAL EFFICIENCY (NOMINAL) (3} % 45.8 48.3 52.1 TOTAL EFFICIENCY (NOMINAL) _141 % 81.9 82.4 83.4 ENGINE DATA FUEL CONSUMPTION {ISO 3046/1) (5) BTU/bhp-hr 6877 7302 7941 FUEL CONSUMPTION (NOMINAL) (5) BTU/bhp-hr 7044 7480 8135 AIR FLOW (77 °F, 14.7 psi) (6) SCFM 3525 2692 1851 AIRFLOW (6) lb/hr 15629 11933 8206 COMPRESSOR OUT PRESSURE in. HG (abs) 90.4 80.2 59.2 COMPRESSOR OUT TEMPERATURE OF 336 310 240 AFTERCOOLER AIR OUT TEMPERATURE OF 133 131 131 INLET MAN. PRESSURE (7) in. HG (abs) 79.3 65.3 46.5 INLET MAN. TEMPERATURE (MEASURED IN PLENUM (8) OF 142 142 141 TIMING (9) 0 BTDC 25 22 19 EXHAUST STACK TEMPERATURE (10) OF 1002 1017 1062 EXHAUST GAS FLOW(@ stack temp.) (11) CFM 10383 8029 5712 EXHAUST MASS FLOW (11) lb/hr 16240 12419 8558 EMISSIONS DATA NOx (as N02) (12) g/bhp-hr 1 1 1 co (13) g/bhp-hr 2.42 2.44 2.56 THC (molecular weight of 15.84) (13) g/bhp-hr 3.34 2.73 2.38 NMHC (molecular weight of 15.84) (13) g/bhp-hr 0.51 0.41 0.36 NMNEHC (molecular weight of 15.84) (13) g/bhp-hr 0.34 0.28 0.24 HCHO (Formaldehydes) (13) g/bhp-hr 0.48 0.45 0.41 C02 (13) g/bhp-hr 482 492 508 EXHAUST02 (14) %DRY 8.7 8.3 7.9 LAMBDA (14) 1.60 1.53 1.45 HEAT BALANCE OAT~ LHVINPUT (15) BTU/min 202459 161231 116900 HEAT REJECTION TO JACKET (JW) (16) (23) BTU/min 31025 29186 26299 HEAT REJECTION TO ATMOSPHERE (17) BTU/min 6911 5760 4609 HEAT REJECTION TO LUBE OIL (OC) (18)(23) BTU/min 7013 6387 5608 HEAT REJECTION TO EXHAUST (LHV to 77"F) (19) BTU/min 70347 54283 39161 HEAT REJECTION TO EXHAUST (LHV to 350°F) (19) BTU/min 47799 37515 27789 HEAT REJECTION TO STAGE 1 NC (1AC) (20)(23) BTU/min 6893 4847 1222 HEAT REJECTION TO STAGE 2 NC (2AC) (21)(24) BTU/min 7136 5917 3435 CONDITIONS AND DEFINI]JONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH lSD 3046/1. DATA REPRESENTS CONDITIONS OF 77°F, 29.6 IN HG BAROMETRIC PRESSURE, 30% RELATIVE HUMIDITY, 10 IN H20 AIR FILTER RESTRICTION, AND 20 IN H20 EXHAUST STACK PRESSURE. ENGINE EFFICIENCY AND FUEL CONSUMPTION SPECIFICALLY NOTED AS ISO 3046/1 EMISSION LEVELS ARE BASED ON THE ENGINE OPERATING AT STEADY STATE CONDITIONS AND ADJUSTED TO THE SPECIFIED NOx LEVEL AT 100% LOAD. EMISSION TOLERANCES SPECIFIED ARE DEPENDANT UPON FUEL QUALITY. METHANE NUMBER CANNOT VARY MORE THAN± 3. PUBLISHED PART LOAD DATA IS WITH AIR FUEL RATIO CONTROL. ENGINE RATING IS WITH 2 ENGINE DRIVEN WATER PUMPS. FOR NOTES INFORMATION CONSULT PAGE THREE. DM8645 (02) PAGE1 OF3 08-Sep..OS G3520B GAS ENGINE TECHNICAL DA 'fA CiTERPillAR® FUEL USAGE GUIDE CAT METHANE NUMBER! "' 35 ,, 4!i 50 ;, 60 r 25 8 ... !GNi110U11MING 22 Z2 24 24 25 25 25 25 25 25 DERATION FACTOR 0.90 0.90 0.90 1.00 100 1.00 1.00 1.00 1.0 1.00 1.00 1.00 ALTITUDE DERATION FACTORS AT RATED SPEED 130 120 AIR 110 TO 100 TURBO 90 80 ("F) 70 so 60 AFTERCOOLER HEA REJECTION FACTORS ACHRF 130 "' AIR 110 TO 100 TURBO 90 80 ("F) 70 so 50 AL TllUDE (FEET ABOVE SEA LEVEL) Ml 130 120 AIR 110 TO 100 TURBO 90 80 ("F) 70 so so ALlTIUDE (FEET ABOVE SEA LEVEL) FUEL USAGE GUIDE; This IBblo shows the derate fat;tor rnqu\red fur a plvon fuel. Note that dernUon occurs as the m~>lhanc numbl!rdec:roases. Me!hana numbar Is a scale to mansore do!anntion characlerii>lics ol various fuel!;. The mathane rmmoor of a fool is delerll'ined by usln~ the Caterpillar Methane Number Calculation prot~ram. ALTIWOE OERAJJON FACTORS• This tabla shows lila dcrallon required far various a1r Inlet tampem\Uics and aH)tudes. Usn this informaHon olo!lll with lha fuel usage guide chart lo help da!ermine actual engine puwer for your sHe. INLET ANO EXHAUST RESTRICTION CORRECTIONS FOR ALTITUDE CAPABIUTY: To determine the appropriate altltllde derate factor to bo appfoed to this eogine forlnlcl or e~h~us\ r~s\rictions din"Mcrtng frllm tho star>dard Cll!ldltions ~sled on PIIIJ111, a oorr11ction to tho sl!e all!lude can be made to ad)U~t for \his diHor~rwc. Add 139 leo\ lnlhe site alllludc fpr each additional Inch of H20 of exhaust slack pl~$ure greal11r than spnc sheet condillnns. Add 122 feel In the sl!e altitude fw eadl ndditionallncll of H20 of Inlet r11strlc1io~ gmnter than sp;-x: sheet conditions. If site inlet restriction or exhaust stack pressura am less than spnc shent cond<tinns, lba same trends appty to lowerllw sltc allll.ude. ACDJAL ENGINE RATING· !I ls !mport~nt to note that the All!tuderfempcrntorc dera!Jon ~nd the Fuel Usage Guide derntinn nrc not cumulative. They are not to be added together. The same Is true for the Low Enermr Fuel derntion (rnference the Caterpl!l~r Methane Number Progrnm} and the Fuel Us6ge Guido de mUon. Hownver.lhe Allitudnrrempemturo derntiDn end Low EnellJY Fuol deration are cumulative; arn:lthey mwt be added IO[Jelhet In the roothod shown billow. To dclarmlnn the actual pownr IJVal!able, lake the towns! !111111{1 between 1) and 2). 1) (Al\~uderrampnrature Deration)+ (Low Energy Fuel Duration) 2) Fuel Usage Guida Derntion Note: For NA's alwnys add thn Low EnefiiY Fuel dem~on to the Altltude/TemJ>IIraluro domlion. For TA engines only add the Low En!>ll]Y Fuel damUon to !he Allilude/Tempernturo deration whenevorthe Affitudorrempnrature dcra!Jon Is less \han 1.0 {100%). This will give the actual r;~ting for \he engine at the conditions Spl!"dfilld. ~l,.F.R HEAT REJECUON fACTORS !ACHRFl: Allercno\ot heal rcjecllon Is olven for standard conditions o! 77'F and 500 II aiUlude. ro m~lntain a constant uir Inlet rmnlfrlld temperature, n51hn alrto lurtx> temperature goes up, ~o must \he haet rejccli>:>n. /<..<; altltude Increases, the turbocharger must work hntder to overcomr. the lower a\mosphnrtc pressure. This Increases tho amoum. of heal that must be romoved from the Inlet sir by tho annrcooler. Usc U1e allercO<l!cr hoot rcje~~inn r~r.tor {ACHRF) lo ad)ttsl for amb!ent and am tude contiitlons. Mu~p!y this factor by U1e ~1andatd anercontor haat mjuctioo. Fallufll lo property accpunt for !hes~ f,,,..,m rould rusun in delonaUon nnd cause tho Nl(Jlne lu shutdown or fall. For2 Stago Anercuob~ with separnlo drr;ults, the 1st s\age win collod 74% of the addition'<! 1\c~t. MINIMUM ~.J::O CAPABILITY AT MAX SIT!'!~ Th!& \able ~hovr.; U\c minimum al!owablo engine turndown Sp!<lld wMere the Blll!lne wi!lm:llnlaln the Rated Speed"s To""IJC for U\e given ambiont cond!Uons. At 6SOO It and obovo, the engine Is not capablo of being loadlld bclPW 1300 rpm. A tn"n\m!Jm ~!"(line load of 50%, 56%, and Q!l% must ho malntalnlld at6500 11,7000 II, and 60(){) It resp~ctive!y when below 1300 rpm OMSG45{0:Z) PAGE :Z Of l S..Sep..OB >2or:: ze.- r-~'--------------------------------------------------------~ G3520B GAS ENGINE TECHNICAL DATA CATERPILLAR® 1 ENGINE RATING IS WITH 2 ENGINE DRIVEN WATER PUMPS. TOLERANCE IS± 3% OF FULL LOAD. 2 ISO 3046/1 ENGINE EFFICIENCY TOLERANCE IS (+)0, (-)5% OF FULL LOAD% EFFICIENCY VALUE. NOMINAL ENGINE EFFICIENCY TOLERANCE IS± 2.5% OF FULL LOAD% EFFICIENCY VALUE. 3 THERMAL EFFICIENCY: JACKET HEAT+ LUBE OIL HEAT+ STAGE 1 AIC HEAT+ EXH. HEAT TO 35DT 4 TOTAL EFFICIENCY= ENGINE EFF. +THERMAL EFF. TOLERANCE IS± 10% OF FULL LOAD DATA. 5 ISO 3046/1 FUEL CONSUMPTION TOLERANCE IS (+)5, (-)0% OF FULL LOAD DATA. NOMINAL FUEL CONSUMPTION TOLERANCE IS± 2.5% OF FULL LOAD DATA. 6 UNDRIED AIR. FLOW TOLERANCE IS± 5 % 7 INLET MANIFOLD PRESSURE TOLERANCE IS± 5% B INLET MANIFOLD TEMPERATURE TOLERANCE IS± 9"F. 9 TIMING INDICATED IS FOR USE WITH THE MINIMUM FUEL METHANE NUMBER SPECIFIED. CONSULT THE APPROPRIATE FUEL USAGE GUIDE FOR TIMING AT OTHER METHANE NUMBERS. 10 EXHAUST STACK TEMPERATURE TOLERANCE IS (+)63"F, (-)54"F. 11 WET EXHAUST. FLOW TOLERANCE IS± 6 % 12 NOX TOLERANCES ARE± 18% OF SPECIFIED VALUE. 13 CO, C02, THC, and NMHC VALUES ARE "NOT TO EXCEED". THC, NMHC, AND NMNEHC DO NOT INCLUDE ALDEHYDES. ENGINE SHOULD BE SETUP TO THE NOMINAL PUBLISHED NOX LEVEL. AN OXIDATION CATALYST MAY BE REQUIRED TO MEET FEDERAL, STATE OR LOCAL CO OR HC REQUIREMENTS. 14 02% TOLERANCE IS± 0.5; LAMBDA TOLERANCE IS± 0.05. LAMBDA AND 02 LEVEL ARE THE RESULT OF ADJUSTING THE ENGINE TO OPERATEATTHE SPECIFIED NOX LEVEL 15 LHV INPUT TOLERANCE IS± 2.5%. 16 HEAT REJECTION TO JACKET TOLERANCE IS± 10% OF FULL LOAD DATA, BASED ON TREATED WATER. 17 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS± 50% OF FULL LOAD DATA, BASED ON TREATED WATER. 18 HEAT REJECTION OF LUBE OIL TOLERANCE IS± 20% OF FULL LOAD DATA, BASED ON TREATED WATER. 19 HEAT REJECTION TO EXHAUST TOLERANCE IS± 10% OF FULL LOAD DATA, BASED ON TREATED WATER. 20 HEAT REJECTION TOAIC·STAGE 1 TOLERANCE IS± 5% OF FULL LOAD DATA, BASED ON TREATED WATER. 21 HEAT REJECTION TO STAGE 2 A/C TOLERANCE IS± 5% OF FULL LOAD DATA, BASED ON TREATED WATER. ZZ SPECIAL RATING REQUEST REQUIRED FORA RATING AT THESE AMBIENT CONDITIONS. SITE SPECIFIC COOLING SYSTEM SIZING EQUATIONS (WITH TOLERANCES) 23 TOTAL JACKET CIRCUIT (JW+OC+1AC) = (JW x 1.1) + (OC x 1.2) + (1AC x 1.05) + [0.74 x (1AC +ZAG) x (ACHRF-1) x 1.05]. 24 TOTAL AFTERCOOLER CIRCUIT (2AC) =(ZAG X 1.05) + [(1AC + 2AC) x 0.26 x (ACHRF-1) x 1.05]. DM8645 (02) PAGE30F3 I 4444 BRITTMOORE ROAD HOUSTON, TX 77041 USA TELEPHONE: 713-335-7000 FAX: 713-335-7527 E01005 ldenaticaaon CHEVRON N. AMERICA E&P Compressor Package I EQ111PMENT II NllME & MODEL [ SERWNO. I (OMPRESSOR II ARIELJGT/4 I F-24403 I THROW1 II 9.125 I C-78722 UUNDERS I THROW2 II 5.875 I C-78723 I THROW3 II 9.125 I C-78724 I THROW4 II 5.875 I C-78725 I MOTOR/ENGINE II CATERPILLAR G3520 ~~~u GLF00111· I COOLER II AIR X-CHANGER 156-EH II 061329X I fiLTER II PECO II 227890-13 i r FoR MODELS: JGE, JGH, JGK AND JGT SECTION 1 -DESIGN SPECIFICATIONS & DATA Tab!e 1-5: JGT FRt..ME SPECIFICATIONSa MODEL JGT/2 JGT/4 ' .JGT/6 Stroke, inches (mm) 4-1/2 (114) 4-1/2 (114) 4-1/2 (114) Speed, RPMb 750 To 1500 750 To 1500 750 To 1500 Piston Speed, FPM (m/s) To 1125 To 1125 (5.72) To 1125 (5.72) (5.72) Number of Throws 2 4 6 Horsepower (kW) To 1300 (969) To 2600 To 3900 (2908) (1939) Height-Bottom to Crankshaft Centerline, 17 (432) 17 (432) 17 (432) in. (mm) Connecting Rod Centerline to Centerline, 13.75 (349) 13.75 (349) 13.75 (349) in. (mm) Maximum Width, in. (m) 157 (3.99) 157 (3.99) 157 (3.99) Maximum Length, in. (m) 57 (1.45) 101 (2.57) 140.5 (3.57) Approximate Weight with Cylinders, lb. (kg) 10,000 (4540) 21,000 (9530) 31,000 (14 075) Oil Pump Flow Rate @ Max. Rated 17(1.1) 32 (2.0) 58 (3.7) Speed & 180'F (82'C), GPM (Lis) 9il Heat Rejectiqn, STU/hr. (kW) ';., ··. '' 34,000 (1 0.0) 68,000 (19.9) 102,000 (29.9) Sump Capacity, US gallons (L) 15 (57) 37 (140) 56 (212) Piston Rod Diameter, in. (mm) 2.000 (51) 2.000 (51) 2.000 (51) Internal Rod Load-Double Acting: Compression +Tension, lbf. (kN) 74,000 (329) 74,000 (329) 74,000 (329) Tension, lbf. (kN) 37,000 (165) 37,000 (165) 37,000 (165) Compression, lbf. (kN) 40,000 (178) 40,000 (178) 40,000 (178) Internal Rod Load -Single Acting: Tension, lbf. (kN) 37,000 (165) 37,000 (165) 37,000 (165) a. For more information, see the Electronic Datebook available in the Ariel Performance Program. b. Rated speeds for non-lube and lubricated process applications may vary. 1/06 PAGE 1 -7 DRAWING TRANSMITTAL J.C. £fd.£dge Sa/eJ Lo., Ync. 9800 Richmond Avenue Suite 325 Houston, TX 77042 Phone: (713) 780-7200 Fax: (713) 780-9324 /lor~ Date: January 15, 2008 Your Order No.: 0728-0093 To: Alta Construction, Inc. Attn: Larry Reeves 17 Smiths Fork Way Lyman, WY 82937 Project: Chevron Piceance Basin Project No: --~r Eldridga Sa~9433 SubmiJted By: Fred S. Mott 2 Copies of the following drawings or bulletins are submitted: For your x Approval __ Distribution Equipment is Released for fabrication Manufacturer Eldridge Hartzell Hartzell AWV AWV AWV AWV Western Canweil Western Canwell x Held for your approval before release Description Compressor Bldg. Ventilation Exhaust Assembly Spec Sheet Fan Performance Fan Curve Spec Sheet Louver Size Schedule LE-31 Stationary Louver Standard Installation Methods Spec Sheet Ridgepac General Arrangement Model A02SH-483-L-STFQL5 A02S H-483-L-STF Q L5 A02SH-483-L-STFQL5 LE-31 LE-31 LE-31 LE-31 RP-12 RP-12 Drawing H-29433-1 01 LE-31 900 r---- , ' ' _ APPROVED AS 1S _ APPROVED AS NOTED _ REVISE and RESUBMIT I Dote: ____ ~ By : le=:==== ALTA CONSTRUCTION, INC. PROJECT: CHEVRON PICEANCE BASIN PO# 0728-0093 LCE H-29433 Emergency Ventilation Exhaust Fans Per EEG Drawing (2) Hartzell series 02SH Direct Drive Standard Air Flow "H" Heavy (Industrial) Panel Fans model 02SH-483-L- STFQL5. Hartzell type "L" 3-blades, cast aluminum, fixed pitch, precision balanced, airfoil propeller is directly driven by a Reliance/Balder 841XL 5 HP 870 RPM 450/60/3 motor with a performance of 27,780 CFM at 0.374" wgsp. 2.00 1.75 1.50 Ol ~ ~~SP ~~ 3: 1.25 ' c = ~ - ;:J ~ Hartzell Fan, Inc.® ESP-Version 1.17.144-March. 2007 ~ I--- = - - -- - ---- = ~ - 1.00 if) <f) <!> ~ 0.. ~ ~wr = --t.l 0.75 "" 2 (f) 0.50 0.25 ~ - r-r--r-- ~ X /""' - - - " _.. - 0.00 ~ ~ ---~= r -, I ~ I I ISC I ~J L ~ I J l I I I I I I I I I 0 5000 10000 15000 20000 25000 Volume Flow Rate (cfm) Hartzell Fan, Inc. certifies that the model shown is licensed to bear the AMCA Seal. The ratings shown are based on tests and procedures performed in accordance with AMCA Publication 211 and comply with ihe requirements of the AMCA Certified Ratings Program. · The AMCA Certified Ratings Seal applies to air performance railngs onfy. Performance certified is for Installation Type 8: Free lniet, Ducted Outlet. Speed {RPM} shown is nominal. PerfDrmance is based on actual speed of test. Performance RaHngs do no! inctude the effects of appurtenance$ (Accessorfes). Sound ratings are based on sound power level data obtained in accordance with N/JCA Standard 300- 30000 The sound power level ratings shown are in declbels, referred to 10"-12 wans. calculated per AMCA Standard 301. Fan Outlet Sound Testlng._Values sho\lfY'I are 1or outlet Lwo sound po~Ner levels for: Installation Type B; free 1nle1, ducted outlet. Ratings include the effects of duel end correction. 8 7 6 5 4 3 2 1 0 '1J 0 ~ <1> ~ S' '0 ~ r~~;:~~ -----8/;~~00;~--~- Job Ret Alta Chevron Piceance Tag#: Proposal#: Rep. Name: Phone#: Fax#: Basin Compressor Bldg Emergency Ventilation Exhaust Fan 07H-16650-PROJ L.C. Eldridge Sales Co., Inc. FSM 713-760-7200 713-760-9324 Fan Selected: A02SH-483-L---STFQL5 02S-Direct Drive Panel Fan, Standard Flow Vol Flow Rate 27780. Static Pressure 0.37 4 Density . 07 5 Operating Temp 70 F Fan RPM 870 Max Safe RPM 1193 ' Operating Power 4.209 1 Standard Power 4.209 1 Static Efficiency 0.388 j Outlet Velocity 2193 '-----------~··~·- Discharge Sound Power Levels~2-J referred to 10'-12 watts 1 2 3 4 5 6 7 96 94 89 87 84 84 80 L..__ . ------- See page 2 for sound information, including dBA and LwA. PAGE 1 Hartzell Fan, Inc.® ESP-Version 1.17.144-March, 2007 Print Date: 8/1012007 A02SH-483-L---STFQL5 Discharge Sound Pressure= 79 dBA@ 5.0 ft Radiated Sound Pressure = 79 ctBA @ 5.0 ft Discharge Sound Power= 91 LwA Radiated Sound Power= 91 LwA VFR: 27780. cfm SP: 0.374 in wg Fan RPM: 870 The A-weighted sound pressure level (dBA) is based on Hartzell Laboratory sound power tests, and is calculated in accordance with AMCA standard 301. The dBA, LwA and radiated values are not AMCA International Licensed The calculation assumes a free field condition with a directivity factor for hemi-spherical radiation (0 = 2). The installed sound pressure levels are influenced by the installation and acoustic environment, and cannot be guaranteed. Use of this estimated level alone for field acceptability tests is not recommended. Although the calculation can be done for any stated distance, the free field does not start until 20 to 50 feet from the equipment in most instaflations. Contact Hartzell Fan for more information concerning dBA values. PAGE2 ALTA CONSTRUCTION, INC. PROJECT: CHEVRON PICEANCE BASIN PO# 0728-0093 LCE H-29433 LE-31 Extruded Aluminum Fixed Drainable Louvers (12) 8" wide x 4' high American Warming & Ventilating model LE-31 aluminum fixed drainable louvers, .051 Alum expanded screen, AWV standard clip angles ( mill finish) with fasteners which are mounted to the louver only, AWV standard Amerflur finish to match building. LOUVER SCHEDULE ~ ~ j 4:-' ..::-fi'""" &----fr~ N ~#j!WJflj' 12' f ~&: S!.§. p ~ > < ·:{ • '-. k + t COMMENTS 0 o-. ..-,():} -~ 01<, ~~ 0 '<) :;f~ i< . ~ ~ \0:: < !LE-31 <4 [48 ! 48 fx1 X I LE-31 110 96 l•a 1x1 ,x I . i . 'OPI'"rlol FINISH , • I ll'l_ TO MR' <-rf THE f>HII nn"r:: NOTE , UNLESS uo NOTED, ALL :>r-t:.~ 1r I ARE STANDARD. ~UATOR: awv.amerlcan warming ~TE : ~.14.2008 ,. and ventilating A MESTEK COMPANY l!W\1. PROIJIICTION No. : 7JO'.'(~~g) DRJVE "'l'f;.;iJ· OHIO I PROJECT : '-r oBASIN Phooa Fax 865 1:>75 • CUO.IUMC" I ORDER No. : ALTA'-v"v'~"~"vn,INC.u;Lo~• '" -LOUVER SIZE SCHEDULE,. . ARCH. I ENGR. : ! CKD.BY f\PPD.BY l"'"l£ l~'<l AGf:NT / No. : / / DRN. DY • D'.tG. NO, CU_S1 UMt:.>-< SIGN OFF:' RF'Vr~rnN '"""-..-/ CK -:;;;;; nan • ,.H·29433 ~ Model LE-31 EXTRUDED ALUMINUM, 6" FIXED DRAINABLE TYPE DEEP, BLADE 1 " \yp 4 A = WIDTH 8 = HEIGHT SECTION VIEW STANDARD HORIZONTAL MULLION ( ( I I I I ..,. r STANDARD VERTICAL MULLION --: FRAME: BLADES: FINISH: SCREEN: MODEL LE-31 STANDARD SPECIFICATIONS 6" DEEP CHANNEL, .081" THICK 6063-T5 EXTRUDED ALUMINUM ALLOY • . 081" THICK 6063-T5 EXTRUDED ALUMINUM ALLOY. MILL. 1 /2" REMOVABLE EXPANDED ALUMINUM BIRD SCREEN, LOCATED ON INTERIOR. MAXIMUM PANEL SIZE: 96" x 96". MINIMUM PANEL SIZE: 1 2" x 12". DIMENSIONS: "A" (WIDTH) AND "8" (HEIGHT) ARE OPENING SIZES. LOUVERS ARE MADE 1/2" UNDERSIZE. * PANELS OVER 48" WIDE WILL BE 7-1 /2" DEEP DUE TO A VERTICAL INTERIOR BLADE SUPPORT ANGLE. -+ +-, . -1--J I I I : I I I I L_ _ __j ) -11-i EXTENDED SILL OPTIONAL ARCHITECTURAL VERTICAL MULLION OPTIONAL 1" '2 J- -C" FLANGED FRAME OPTIONAL (JAMB SHOWN) ) AVN certif1u that tile model L£-31 louver ahown herein !a !icenacd to ~or tho AMCA Se<ll. The ratings shown or¢ ba~ed on teat!! and proe<Kiurce performed in occordonce with AMCA Pub!i<;:OOon 511 and oomply with the requirements of tho AMCA Certffiad Rot!ngs Program. The ~CA Certified Ratings Seal applies to alr pertorrnonc-e rcUngs and water penelratlon rallnge.. aw '-1' american warming y 0 and ventilating A MESTEK COMPANY 7301 INTERNATIONAL DRIVE HOUAND, OHIO Phon• (419) 865-5000 Fox (419) 865-1375 LE-31 STATIONARY LOUVER JlRN, BY ESS DATE t2-~-oo :0\./G, NO, R£V, LE-31 Water Penetration Pressure Drop Free Area : 0.01 oz (3.0 g) at 1250 fpm (6.35 m/s) recommended free area velocity : 0.21 in wg (52 Pa.) at 1250 fpm (S.35 m/s) and 11550 scfm (5.45 semis) : 9.24 sq ft (0.858 sq m) = 57.8% for 48" x 48" (1.22m x 1.22m) test size ~ ~ .E INTAKE PRESSURE DROP (248} (174) 0.7 {124) 0.5 /74.4) 0.3 (49.6) 0.2 j 1/ 1-;,: C> {24.8) 0.1 ili J: {17.4) 0.07 (12 4) 0.05 /7.4) 0.03 {5.0) 0.02 v (25) {),01 200 400 1000 2000 10000 (1.0) (2.0) (5.1) (10.2) (50.8) VELOCITY THROUGH FREE AREA fpm (mls) standard air~ .075 !bs per cu ft Ratings do not include the efiect of a wire bird screen Test based on a 48" x 48" test size per AMCA Standard 511 lllmc:ll.l CERTIFIED RP.TIOGS AWV certifies that ihe model LE~31 louver shown herem is licensed to bear the AMCA SeaL The ratings shown are based on tests and procedures performed in accordance with AMCA Publication 511 and oomply with the requirements of the AMCA CertifiOO Ratings Program. The AMCA Certified Ratings Seal applies to air performance and water penetration r<rtir>gs LE-31 Balow Is an 9Xplane~tion of how to use tho AMCA Performance FREE AREA IN SQUARE FEET (sq meters) in. 12 24 mm 305 610 12 0.18 0.43 305 0.017 0.040 24 0.69 1.70 610 0.064 0.158 36 1.21 2.96 914 0.112 0.275 46 1.72 4.23 1219 0.160 0.393 60 2.24 5.49 1524 0.208 0.510 72 2.76 6.76 1829 0.255 0.628 84 3.27 8.02 2134 0.304 0.745 96 3,78 9.29 2438 0.351 0.863 ' ' _, (91.5} 0.3 O' o' -:z: % E: --.ij : E ~:: : ~ ·e : St.n: " ~ ' -· g-.a:: -L1l ' ¢1 tt: : 0. < . N ' 0 IJJ: W< 0:' u.: (16.0) O.Z5 (61.0) 0.2 {45.7) 0.15 (JO.S) 0.1 {i5.3) 0.05 0 WIDTH 36 48 60 72 84 914 1219 1524 1829 2134 0.69 0.94 1.16 1.42 1.67 0.064 0.087 0.108 0.132 0.155 2.70 3.71 4.59 5.59 6.60 0.251 0.345 0.426 0.519 0.613 4.72 6.47 8.01 9.76 11.52 0.439 0.601 0.744 0.907 1.070 6.73 9.24 11.43 13.93 16.44 0.625 0.858 1.062 1.295 1.527 6.75 12.00 14.85 18.11 21.36 0.813 1.115 1.380 1,682 1.984 10.76 14.77 18.27 22.28 26.28 1.000 1.372 1.697 2.070 2.441 12.76 17.53 21.69 26.4<5 31.20 1.187 1.629 2.015 2.457 2.899 14.79 20.30 25.12 30.62 36.13 1.374 1.886 2.334 2.845 3.357 WATER PENETRATION Less than .01 oz: /sqf1 AMCA Standards Are base<:l. on maximum of 1250 fpm frl* area velocity and a min of .01 ozlsqlt 96 2438 1.93 0.179 7.60 0,706 13.27 1.233 18.94 1.760 24.62 2.287 30.29 2.814 36.96 3.341 41.63 3.868 free area of water penetration. The AMCA test was una,ble to determine the beg\nnmg water penetration due to the fact that ls lies above 1250 fpm through free area ' 500 BOO 700 800 900 1000 1100 1200 1300 : (i5T: ~(i.OI: : (i. 5T: ; (i.OT:: (4~5j: ,' (5.0): : (5..5T: : (6.0j; ,' 16.5): !..-~~-' '·---~' !..----' '--~--•!.. •••• • '-----' '-~---' L----' L----' -------' VELOCITY THROUGH FREE AREA fpm (mls) Both maximum recommended free area velocity and beginning ot water penetration are 1250 fpm at standard a1r -.075 !bs per cu ft. The above water penetration data is based on mill fimsh, 48" :< 48" test siz:e per AMCA Standard 511. data forth& recommended free area velocity of 1250 fpm (6.35 m/s). Openings that require mul1iple louver panels in both width and height will require internal structural supports. It Is recommended that large openings be divided with structural members so that the louvers will span either width or height with a single panel. Unusually high wind loading may require structural supports on non~multiple wide and multiple high assemblies. Structural supports and mounting accessories are-not supplied as a standard. To determine minimum free area required !or louver: Ste-p #1: Divide the required CFM llow by the maximum recommended free area velod\y. Stop #2; Select the most desirable louver ske, from the free area table, that meets !he minimum free area requirement. Stap #3: Compare specified performance to the certified water penetration and pres.sure drop ratings. Fonn No. 0·561 Deoember 2000 Example: Given: 15000 CFM design flow Step #1: min. free area = Design CFM Max. Recommended Veloc1ty 15000 12sqft 1250 Stop #2: · From the free area (able above !he approximate louver size is 48" x 60" = ( 12 sq ft) HEA])S SE:ALANT BY OTt-ERS JAMBS SEALAI'{T BY 01HERS SEALANT Bl nTHERS SILLS SlLL E:XTENSIDH OPTIONAL MtlJNTlNG ANGLE CSEE NOT( 2) TYP!CAL :Sf:ALANT BY OfHERS MIJJNTING ANGLE. <SEE NOT£ Cl TYPICAL S(ALANf BY OTHERS SE'LANT IiY OTHERS Mfil.JNTING ANGLE <SEE NOTE 2) TYPICAL SJLL E:XTENS[QN OPTIONAL MOUNTNG PLAT£ <SE:£ NOTE 3) Sf:AL.\tH Bl OTHERS SEALANT Bl' OTHERS SCALANT BY UTHERS TYPICAL ' SILL E:XH:NSION OPTIONAL MOONllNG ANEiLE <SEE NOTE 2) TYPICAL SE.ALAN1 BY OTHERS HOON.TING ANGLE <SEE NOTE 21 TYPICAL SEALANT li:Y DTH£RS: SEALANT BY OTHERS MWNTlNG ANGLE <S(£: NOT£ 2> TYPJCAL StLL EXTf:NSlCN OPTIIlNAL. HOUNfNG PLATE (S(:~ N!JTC 3) TYPiCAL TYF!CAL DEEP CURTAIN YALL OPENING TYPICAL NARRD'W CURTAIN Y ALL OPENING TYPICAL MASONRY VALL OPE:N!NG TYPICAL YODD FRAME \JALL OPENJNG INSTILLATION NOTES: 1. ALL HOUNTJNG FAS1£NERS TO OPENINGS, SEALANT, SHIHS. HASDNR'f ANCHORS, EfC. ARE NOT Sl.P?LIED 00 INSTALLED BY LOUVER 1-FGR. 2. CUP ANGL£S, HOLNTING PLATES, fASTE~RS TO LOUVERS, AND :STRUCTURAL 3UPPQ£TS J:AN ONLY BE PRDVInE:D AT AN l'lliDITIDNAL CD!)T, PL-t::~SE CD.!'-GUL T f"A.CTORY FOR PRlC!NG. 3. RECOMMENDED KCli.J'.ITlNG fOR DEEP 'VALL lJP£NltliS1 AS It HlNlHUH: USE 1-1,r,e. X l-1rE; x l/8 CONTlNUOUS PLATE: OR CLIP ANGL£!0: IJN IN:SIDE PER1MET£R !F LOUV£R-FRN1E W'ITH l/-4 .. DIAHE:TER FASTLHERS [N MAX. lS-CENTERS. THE LOC.AT!DH Of l/-4 .. DIAMETER JofJUNTING ANCHOR BOLTS SHDULD BE SUCH AS TO GlVE A f'iNIHUK OF 2 llllL TS tl< A Slll£ 3. RE:COHHEN.llf::P M~TrNO fOR NA~Q"'W ._.,~L Cf'Ef!iiNGS• I>S A HI!U~M US£ l/8 x l-1/2 x 3 HOUNTtt>IG PLATES !Ji! CONTfNUOUS PLAT£ ON lNSIDE PERIHETER !Jf LOUVER FR.A~ \liTH 1/<4' DIAHETER FASTENERS ON XAX, 18~ CENT£RS. THE LOCATION Ot 1/.~t• D1AI1£TER KOUNTIHG Btl.. TS SHOULD :8! SUCH AS TO Gtv!: A HINIHUH Of !:' BDL TS [l>.l A SIDE; !5. 'WIDTH AND H£IGHT DIHE:NSlONS A.R£ IJPLN!NG S.[ZES. LOUVERS ARE MADE UNDERSiZED. TYPICAL 1/-4' AKtlllND PLRIMETER OF LOUVER FRAME.. LOUVERS IJ!TH LARGER UNDERSJZING Ci<i OC SUPPLIED UP!lN REQUEST. 6. THESE ARE: GENERAL H[).INTING hRRANGEMENTS rDR LUOV£R ~1\.LL OPENINGS. VIE'WS SHOYN SHOULD COVER MOST KIJ.JNTING SITUATIONS ENCDUNTE:RED. LARGE "'-JLTIPLE VIDE AND/OR HIGH LOUVER PANEL ASSEMBLIES RE:QUtR£ STRUCTURAL SUPPORT ON INTERIOR Of UJUV[R P'ANEL.:S, 'riHlCH CAN BE PROVILED AT AN ADDITIONAL COST. 7. R£FtRENC£ DRA'WlNG No, 22,.6.5 AND 22,.66 f"Ol( LOOVER MULUON INSTALLATION INSTRUCTIONS AS REOI,JIRED, s. B£CAUSE LOCAL BUILDING CODES. AND tMSTALt..ATION STANDARDS HAY VARY FROH OJR RECOHMENDED HINIMJHS, \1( RECOtt1END THAT TH(Y BE USED CV(R OJRS 'WHEN AND \IHEr;E REQUIRED. OW'l ~;r.-~ii!Jr.;;"• A Wf:SnK OOioiPAJIT '>JI0'1 ,.._10«, IIIIJO/C tCu..tl. Q!!s;> ,.,.. .. {tlfl ~ F<t .. [•lt) .-..1nl S ANDARD INSfALlATION METHODS , • ., 8 l'bl,l'l' :a.s..-~"" -ev.c ..,n;; 900 A"" L----------------------------------------------------------------------------------------------------------------------L---=an~·--~--------~--~u ALTA CONSTRUCTION, INC. PROJECT: CHEVRON PICEANCE BASIN PO# 0728-0093 LCE H-29433 RP-12 Ridgepac Gravity Ventilator A 140ft. long run of Western Canwell model RP-12 Ridgepac Gravity Ventilator, galvanized steel painted external outside only to match building with bird screen, Dampers and two manual chain operators with 100' chain drops and idler pulleys for side wall are included. I = = = ~ j~ I 165/8" 1 I liS" GAl' B!!TWEEN UNITS END OPERATOR UNrT 11---11~ 11-:J- SIDE. VfE'N • CONTINUOUS RUN l.Nbr.AlL\ TION TOP PLATE DAMPER ·WINDBANIJ 1,718" >.------· 12" -----~ ZJ" 28l/8" ------------ II:- END ADDED UNIT __ ] QESCB IPTION· 140' LONG RUN OF RP-12 GALVANIZED PAINTED EXTERNAL WITH BIRDSCREEN, DAMPERS AND TWO MANUAL CHAIN OPERA TORS WITH PULLEYS FOR SIDE WALL J:ROJECI:. CHEVRON PICEANCE BASIN LQCATION· CUSTOMER· ALTA CONSTRUCTION, INC. GENERAL ARRANGEMENT-RIDGEPAC ><=A<.Jt• M T 5. ...rrn.cvr~:~ av llJi. Tli ].!7-97 WESTERN-CANWELL : ;-· :-:-, .. Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 TABLE OF CONTENTS REV:O Page 2 of 14 1.0 EXECUTIVE SUMMARY ............................................................................................................ 3 2.0 PURPOSE ....................................................................................................................................... 4 3.0 SCOPE •....•.••.••.•.••.••.•.•..•.••••.•••...•••.•••.••..•••••.••.•..••.•.••.••..•••.••••.•....•..•.•••.•.••.•••.•••.••..•.•••••••••....••.••••••• 4 4.0 CONCLUSIONS ............................................................................................................................. 4 5.0 RECOMMENDATIONS ••.•....••.••••••...••.••.•..•.•••.••••.•....••.••.•.•....••.•••••...••.••••••.•...•.•••.••••••...•••.••••.•••. 4 6.0 REFERENCE DOCUMENTS .•••.•..••.••••.•..•.••.••.•....••.••••..•....••••.••.•.••.••.••••••....••.•••.•.....••.••.••.••.•..•• 4 7.0 FACILITY DESIGN PARAMETERS ......................................................................................... 5 8.0 FLAMMABLE HYDROCARBON INVENTORY •••••...•.•••••.•..•.••.••.•..•...•.•••.•..•...•.•••.•••••......••.•• 5 9.0 FACILITY AND ENCLOSURE DESIGN PARAMETERS •.••.••.••.•..•...•.••.•••••.•...••.•••••..•.•..••.••• 6 10.0 CONSTRUCTION ......................................................................................................................... 7 11.0 FIRE AND GAS DETECTION ••.••.•.•..••.••...••..•.••.•...•.••••.••...••••.••.•..•.••.••.•••.•...•.•••.••.•••...••.••.•••••..• 8 12.0 FIRE SUPPRESSION .................................................................................................................... 9 13.0 CODE DISCUSSION ...••.••.•.....•.•••.•....•.•••.•.....•.••.•••.....••.••••....•.••.•••••..•••.•.••••.......••••••.••....••.••.••••• 10 Tables Table I: Liquid Inventories .......................................................................................................................... 6 Appendix Appendix A ................................................................................................................................................. 13 Appendix B ................................................................................................................................................. 14 Page2/14 1.0 EXECUTIVE SUMMARY Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page3 of14 The Chevron Mid-Continent & Alaska Business Unit (Chevron) is currently developing facilities in the Piceance Basin of Western Colorado for the purposes of natural gas production, treatment, transmission, and delivery to sales pipelines. These facilities include modular facilities close to the gas wellheads, as well as a number of modular unit process facilities at a Central Production Facility (CPF) to be located north of the town of De Beque, Colorado. Because of the unique nature of fire and explosion hazards at natural gas facilities, Chevron has planned and designed these facilities to incorporate fire prevention and protection systems and procedures in accordance with industry standards, relevant building and fire protection codes, and Chevron's Safety in Design program. The purpose of this document is to present the design and operational philosophy Chevron proposes for the development of these facilities within the CPF. The key design parameter in the design of the fire protection system for the CPF is the ability to quickly and automatically depressure most of the facility, shut down the flow of hydrocarbons to the facility, and remove all electrical power, except essential power, upon automatic detection of a fire anywhere in the facility. As is typical in the petroleum industry, Chevron has designed the production and treatment facilities at the CPF as a series of modular unit processes. Each module is designed to accomplish some function or functions related to natural gas processing, such as removal of water and solids flowing within the gas stream, removal of heavier hydrocarbons from the gas stream, compression of the gas prior to release to a pipeline, metering the gas prior to delivery of the gas to a customer's pipeline, etc. Because of the harsh weather conditions at the site, many of these unit processes are enclosed to protect certain equipment and instrumentation from the elements. Some of the process skids wiJI be mostly enclosed; other process modules will have an enclosure around the instrumentation and control equipment only. Most of the process enclosures wiJI be factory built, and Chevron has been working with the Colorado Division of Housing to secure plan reviews and permits for these prefabricated facilities. Several of the facilities wiJI be site- built enclosures, including a large facility housing the main compression equipment at the CPF. Additionally, some of the prefabricated facilities will house support and utility processes, but wiJI not house any significant hydrocarbon materials. Because of the nature of the fire hazard associated with the enclosures housing process gases and associated equipment, the primary focus of this narrative wiJI be on the process buildings. The process equipment enclosures are classified by the International Building Code (IBC) as buildings with an Occupancy Classification of H-2. This rating is based on the amount of flammable gas and liquids carried in the equipment and piping within the enclosures. Although buildings with an H-2 occupancy rating are normally required to have an automatic sprinkler system, Chevron is proposing to protect these facilities with a non-water-based emergency system in accordance with the exemptions allowed in IBC Section 903.3.1.1.1. The design and construction of the process building enclosures have been conducted after identifying and taking into account the hazards associated with the types of equipment and materials contained within the enclosure. The design and construction standards utilized are more stringent than required by current industry codes and standards. The enclosures are constructed of noncombustible materials and have fire and gas detection systems specifically designed for the gas processing industry. The egress requirements of IBC Chapter I 0 and the NFP A Life Safety Code requirements are also incorporated into the design. Page 3/14 2.0 PURPOSE Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page 4of14 This philosophy identifies the design parameters utilized to engineer equipment enclosures that meet the requirements of the IBC for buildings with an H-2 rating but without an automatic sprinkler system. 3.0 SCOPE This document only analyzes those equipment enclosures located at the Central Processing Facility in Chevron's Piceance Basin Development. It focuses on those enclosures with an H-2 rating by identifying the hazards within the enclosure and the design measures used to mitigate those hazards to personnel who may be present at the time of an incident. 4.0 CONCLUSIONS The parameters utilized in the design and construction of the equipment enclosures covered by this philosophy adequately protect personnel from the hazards due to the presence of hydrocarbons in the enclosure, without employing automatic sprinkler systems. 5.0 RECOMMENDATIONS All enclosures covered by this philosophy should be built and installed as designed. Additionally, operational and maintenance procedures should be implemented to ensure that all safety systems are tested and maintained in accordance with IBC and International Fire Code (!FC) requirements. 6.0 REFERENCE DOCUMENTS Reference Document IBC 2003 IFC 2003 IMC 2003 APIRP14C APIRP14G APIRP500 Document Title International Code Council - International Building Code· 2003 International Fire Code · 2003 International Mechanical Code -2003 American Petroleum Institute - Recommended Practice for Analysis, Design, Installation, and Testing of Basic Surface Safety Systems for Offshore Production Platforms Recommended Practice for Fire Prevention and Control on Open Type Offshore Production Platforms Recommended Practice for Classification of Locations for Electrical Installations at Petroleum Facilities Classified as Class I, Division 1 and Division 2 Page4/14 APIRP752 APIRP2030 API Publication 251 OA COGCC 30 CFR Chapter II Title: PICEANCE FIRE PROTECTION PIDLOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV: 0 Page 5 of 14 Management of Hazards Associated with Location of Process Plant Buildings Application of Fixed Water Spray for Fire Protection in the Petroleum and Petrochemical Industries Fire Protection Considerations for the Design and Operation of Liquid Petroleum Gas (LPG) Storage Facilities Colorado Oil and Gas Conservation Commission - Rules for Oil and Gas Development in Colorado -Section 606A "Fire Prevention and Protection" Code of Federal Regulations - Title 30 (Mineral Resources) -Chapter II Part 250.800 "Production Safety Systems" 7.0 FACILITY DESIGN PARAMETERS The CPF is designed to be an unmanned facility. The control system is specifically designed to ensure that in the case of a significant event, all instrumentation fails safe, the main electrical feed to the affected area is shut off, incoming hydrocarbon flow to the facility is blocked at the battery limit (boundary) of the facility, and the bulk of the hydrocarbon inventory in the facility is depressured to the facility's flare system. Although some limited portion of the piping and some vessels within the plant may have a residual gas pressure after the shutdown, virtually all fuel sources within the facility will be immediately shut off. The CPF does not have water available for fire suppression activities. Additionally, no local fire water system exists to provide for tie-in for CPF fire suppression systems. 8.0 FLAMMABLE HYDROCARBON INVENTORY 8.1 Liquid Inventory The primary fire hazard within the enclosures listed in Table 1 is related to hydrocarbons processed within the facility. In addition to various volumes of natural gas, these buildings will contain various quantities of hydrocarbon condensates (condensates are flammable hydrocarbon liquids that condense out of the gas stream when the gas is exposed to typical ambient temperature and pressure). The hydrocarbon condensate liquid contained in most of the process buildings in Table I is a Class !A flammable liquid (its flash point is less than 73"F and its boiling point is less than !OO"F). The exempt quantity of Class !A liquids, per the IBC, is 30 gallons. The exempt quantity for flammable gases in the IBC is 1000 standard cubic feet, which is exceeded in each of the building enclosures. Due to the inventory of flammable materials located in each enclosure, a rating of H-2 for each of the enclosures and compressor building is warranted. Fire protection methods based on this occupancy classification are further discussed below. Page 5/14 Enclosure ·.· Chevron Title: PICEANCE FIRE PROTECTION PIDLOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST -0001 Date: 19 November 2008 Table 1: Liquid Inventories Liquid Volmne. ·•. Liquiq . }?lash Point @ 0 REV:O Page6 of14 Boiling Point@ .... · . . . . . . (gallons) · . PSIG ("F) OPSIG("F) .. ··.•· Gas Separator 604 Condensate -16 37 128 Water Liquid 426 Condensate -2 78 Separator 1013 Water Gas Filter --Condensate N/A N/A Separator 34 Water Sales Gas 253 Condensate -20 34 Compressors 42 Water 1000 Lubricating oil 262 >300 Condensate 55 Condensate -2 78 Loading --Water Produced 20 Condensate -2 78 Water and 51 Water Condensate Pumps Flare Scrubber 257 Condensate -2 78 --Water Vapor 14 Condensate -4 75 Recovery Unit --Water Fuel Gas 35 Condensate -15 37 --Water 9.0 FACILITY AND ENCLOSURE DESIGN PARAMETERS 9.1 General Almost all of the process building enclosures will contain some amount of hydrocarbon condensate liquid, which is produced from the wellhead along with the lighter natural gas components. Some of the individual unit processes are specifically designed to remove Page6/14 Title: PICEANCE FIRE PROTECTION PIDLOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page 7 of14 these flammable liquids and transfer them to holding tanks elsewhere within the plant. The volumes of flammable liquids in many of tbese enclosures exceed the IBC thresholds at which a building is classified as H-2. These volumes may increase the fire hazard witbin each enclosure to some degree, but do not change the overall philosophy of our proposed fire protection program. 9.2 All flammable liquids and gases within the enclosures are totally contained within the process piping and ASME-rated pressure vessels. An automatic fire and gas detection system is provided to detect any leaks or fires. 9.3 In the event of a fire anywhere within the CPF, the facility is depressured to the flare to remove the bulk of the flammable gas sources from the fire. Any remaining hydrocarbon liquid would initially be protected and contained within the process piping and/or vessel(s) in which it resides within the enclosure. The rate at which the hydrocarbon liquid would contribute to the ongoing fire would depend upon the amount of damage in the containing piping/vessel(s). If the containment is damaged or breached, the materials would burn in place along with the remaining gaseous components. The relative volumes of gas and liquids being burned, and access to the fire of an oxidizing airflow, would determine the extent to which the liquid boils in place as it contributes to the fire. 9.4 Although a combination liquid-and-gas fire might burn hotter and longer than a pure gas fire, the fundamental principle behind our proposed fire protection system is unchanged. The system is designed to contain the fire and allow it to burn out in place. There is no need to attempt to suppress the fire with a water-based sprinkler system. It would likely cause a more substantial hazard by allowing the remaining flammable gases to form a combustible cloud capable of re-ignition until allowed to dissipate. 9.5 It would also be undesirable for the fire department to attempt to put out the fire within an enclosure prior to the consumption of the fuel exposed to the fire. As mentioned above, the remaining gaseous components, along with liquid components that are vaporized due to the heat of the fire, would be dangerous and subject to re-ignition. (See sections 13.3.4 and 13.3.5 for details of this hazard.) 9.6 A closed drain system is provided that removes all liquid from the enclosure's coaming area to a remote underground sump tank. The drain system incorporates P-traps to prevent flammable gases from venting into the enclosure. Liquids collected in the underground sump are subsequently pumped into the facility's above-ground storage tanks. 10.0 CONSTRUCTION Each enclosure has the following construction attributes: 10.1 All hazardous gases and liquids within each enclosure are housed in self-contained process piping and/or pressure-rated vessels. Piping is designed and constructed in accordance with ANSI B31.3 requirements for gas facilities of this type. All pressure vessels are designed in accordance with applicable ASME Section VIII requirements for these vessels. 10.2 Process piping and vessels are designed to contain all materials with no significant leakage. A fire and gas detection system is specifically designed for each enclosure to Page7/14 10.3 1o.4 10.5 10.6 10.7 10.8 10.9 10.10 Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page 8 of14 detect the presence of hydrocarbons in the air or a fire event, and will initiate emergency shutdown systems within the plant upon detection of a significant amount of hydrocarbons. (Details of this system are described in the following sections.) Each enclosure is constructed entirely of noncombustible materials. Additionally, all equipment, piping, instrumentation, junction boxes, panel boards and cable within the enclosure are also noncombustible or flame-retardant. Adequate access/egress is provided to allow safe evacuation from the enclosure in the event of a fire or gas release in compliance with IBC and NFP A Life Safety Code requirements. These criteria include the provision of at least two means of egress from any building with travel distance to an exit greater than 25 feet. No dead-end corridors are allowed in any of the buildings greater than 20 feet. Ventilation is provided to the enclosure in compliance with IMC requirements. Panic door hardware and emergency exit lighting are provided in compliance with IBC. To prevent electrical ignition of hydrocarbon vapors, all electrical components on the process skids are explosion-proof and rated for service in Class I, Group D, Division I atmospheres as rated by API RP 500, and each component is certified as such by a Nationally Recognized Testing Laboratory (NRTL). All 208VAC and 120VAC wiring and equipment within each process skid are wired to an on-skid explosion-proof panelboard. All equipment in the compressor building is rated for Class I, Division 2. (The distinction is a result of the presence of the combustion engines driving the compressors.) Although the enclosures are designed to be safe when continuously occupied, the facilities in practice will be normally unoccupied. Personnel only occupy an enclosure with the doors open when conducting equipment monitoring and observance activities. The operational activities typically require personnel in the enclosure for less than 15 minutes on any given day. Any maintenance activities within the facility will be conducted under stringent safety protocols, including additional fire suppression equipment and personnel being present. 10.11 Operational procedures at the plant prohibit the accumulation of any combustible materials within the enclosure. 10.12 The design of the site surrounding each enclosure incorporates a significant barrier zone covered with noncombustible gravel and no vegetation. Additionally, the site has significant security measures in place, and no admittance to the general public is allowed. 10.13 All enclosures and the process control and safety systems that interface with them were designed using Chevron's "Offshore Gulf of Mexico" standards and design criteria. Chevron considers these standards to be more stringent than most onshore standards, leading to a more conservative design. 11.0 FIRE AND GAS DETECTION Each enclosure is equipped with the following fire and gas detection technology, in strict compliance with the JFC and API RP 500: Page 8./ 14 Title: PICEANCE FIRE PROTECTION PHILOSOPHY Cnstomer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page 9 of14 11.1 Infrared point gas detectors which are tied to a central monitoring system will initiate shutdown of electrical service and hydrocarbon flow to and from the enclosure when gas is detected. These detectors are set to alarm when flammable gas at a concentration of 20% of the lower explosive limit (LEL) is detected. A complete shutdown of power and hydrocarbon flow to the enclosure is initiated when flammable gas at 40% of LEL is detected. All detection and monitoring equipment used at the site is listed by a Nationally Recognized Testing Laboratory (NRTL). See Appendix B. 11.2 A pneumatic fusible loop system consisting of stainless steel tubing pressurized with 40 psig instrument air, and including elements which will melt at 180"F, is provided on all hydrocarbon processing equipment per API RP 500. This system is equipped with a pressure sensor that is tied to a central monitoring system. A loss of pressure in the loop will indicate the affected enclosure and will shut down hydrocarbon flow to and from the enclosure and throughout the CPF and will initiate depressurization of the affected facilities to a dedicated flare. See Appendix A. 11.3 "Triple-infrared" fire detectors have been installed in each enclosure, and when a fire is detected, a programmable logic controller (PLC) will shut down the flow of hydrocarbons to and from the enclosure, as well as throughout the CPF. The bulk of the hydrocarbon inventories throughout the CPF will be depressured to a dedicated flare. (Some minor residual amounts of gas under pressure will still be present in some vessels and piping sections outside of the building enclosures.) Triple-infrared photo-electric flame detectors (known as 'fire eyes' in the gas processing industry) will be installed in all H-2 occupancy buildings and will be tied to the fire alarm systems described above. 11.4 The triple-infrared open-path fire detector system is independent from and redundant with the pneumatic fusible loop system, and both of these systems are independent from the gas detection system. 11.5 Note that the types of detectors described above in Sections 11.1 through 11.3 are provided in lieu of the smoke detector system outlined in IBC Section 903.3.1.1.1. The primary reason for this is that there are no commercially available weatherproof smoke detectors that are rated for Class I, Division I service. 12.0 FIRE SUPPRESSION For these process enclosures, the flammable content hazard located within these enclosures is primarily pressurized natural gas. The experience within the petroleum industry is that a typical water-based sprinkler system cannot extinguish a pressurized gas fire, and in fact can create more of a hazard than it mitigates. The standard of the natural gas industry, as codified in API RP 500, is that suppression of a pressurized natural gas fire is best accomplished by immediately shutting off all incoming sources of fuel and venting all other inventories of fuel to a flare system. The remaining non-pressurized gas, along with any associated hydrocarbon liquid, is allowed to bum itself out. For manual suppression of small fires on a limited basis, each enclosure is equipped with hand- held 30-lb Class ABC fire extinguishers located at each door. Page 9/14 13.0 CODE DISCUSSION 13.1 IBC Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page 10of14 13.1.1 IBC 2003 normally requires an automatic fire sprinkler system for all H-2 occupancies. 13.1.2 All of the process buildings in this project are classified as H-2 due to the large volume of hazardous materials. 13.1. 3 However, these buildings qualify as exempt from this requirement per IBC 903.3.1.1.1 Exempt Locations. Comments applicable to the facility under discussion are listed parenthetically following the code citation. IBC 903.3.1.1.1. Exempt Locations ..... Automatic sprinklers shall not be required in the following rooms or areas where such rooms or areas are protected with an approved automatic fire detection system in accordance with Section 907.2 that will respond to visible or invisible particles of combustion. (In these facilities, an APT-compliant gas detection system is installed and designed to respond to concentrations of flammable gas before any combustion takes place.) Sprinklers shall not be omitted from any room merely because it is damp, offire- resistance-rated construction or contains electrical equipment 1. Any room where the application of water, or flame and water, constitutes a serious life or fire hazard. (This is true for these facilities. Water sprayed on a pressurized gas fire is unlikely to stop the fire, and could add an explosive hazard due to an unburned gas cloud if it did put out the fire momentarily.) 2. Any room or space where sprinklers are considered undesirable because of the nature of the contents, when approved by the building official. (This is true for these facilities. Because of the nature of the contents - pressurized natural gas -the petroleum industry standard for safety is to mitigate the risk with an API-RP500 compliant gas detection & emergency shutdown system.) 3. Generator or transformer room ... Not Applicable 4. In rooms or areas that are of noncombustible construction with wholly noncombustible contents. (This exemption is partially true of the operating buildings in discussion. The buildings are of noncombustible construction, although the hydrocarbon contents within the process piping and vessels are combustible. However, upon detection of fire, the process equipment is depressured and all flammable gases are vented to the flare except for trace amounts remaining in the pipes at atmospheric pressure.) Page 10/14 Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Cbevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page 11 of14 13.1.4 IBC Discussion 13.2 IMC In summary, it is believed the buildings proposed for the Chevron CPF are exactly the type of facility envisioned by the code writers when developing this exemption. There is no ·question that these facilities contain hazardous flammable materials, but application of a water-based sprinkler system would be counterproductive, and would create more safety hazards than it would solve. A far more desirable solution is the substitution of a fire and gas-hazard detection and emergency shutdown system specifically developed for this industry by the API. With the concurrence of the Building Official and Fire Marshall of Garfield County regarding this exemption, the proposed facilities will be in total compliance with the intent and with the specific language incorporated into the IBC, IFC and related International codes. Each of the process equipment enclosures includes either fixed or manually operable louvers which make the use of non-water sprinkler (gaseous, dry chemical, carbon dioxide, foam, etc.) fire suppression systems problematic. Louvers are provided in compliance with the IMC, which mandates adequate ventilation for rooms containing hazardous materials. Additionally, standard practice in the gas processing industry is to provide such ventilation to allow flammable gases to disperse, ideally before hazardous accumulations of the gases accumulate within the building. The reasoning within our industry, as codified in API documents, is that ventilating the gas is much safer than trying to contain it within the building and suppress any fires with a non-water based suppression system. 13.3 API The Chevron CPF is designed in its entirety to be in total compliance with applicable standards of the American Petroleum Institute. 13.3 .I API RP 500, as detailed above, provides the design standards and details for a gas detection system specifically designed to prevent the accumulation of hazardous levels of flammable and explosive gases as applicable to our industry. 13.3.2 API RP 14G Section 5.7.d "Automatic Fire Control Systems -Enclosed Machinery Areas" indicates "Gas compressors, hydrocarbon pumps, and generators in adequately ventilated enclosed areas are normally not protected by automatic fire control systems." 13.3.3 API RP14G Section 5.6.c "Manual Fire Control Systems-Enclosed Machinery Areas" recommends dry chemical fire extinguishers and these are provided in each enclosure. 13.3.4 API RP2030 specifically discusses the hazards of attempting to suppress a flammable liquid or gas fire with water in two sections: 6.4 EXTINGUISHMENT .... Extinguishment by water spray is generally most effective where the fuel is a combustible solid, water-soluble liquid or high flash point liquid. However, the risks associated with extinguishing certain fires should be carefully evaluated. If significant quantities of flammable gases or vapors are Page 11/14 Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 REV:O Page 12 of14 released a more hazardous condition with potential for explosive re-ignition can be created by extinguishing such fires instead of allowing them to burn at a controlled rate with appropriate surveillance and protection of surrounding equipment. 7 .2.3 Extinguishment. Extinguishment is seldom the primary purpose of water spray system installations in the petroleum industry ... It should be noted that extinguishment of low flash point hydrocarbon liquids with water spray is seldom possible and not necessarily desirable. A key question during hazard analysis is "If the material is extinguished while still generating vapor, is there a risk of vapor cloud re-ignition?" (The answer is yes at this facility.) 13.3.5 API Publication 25!0A is primarily geared towards the liquefied Petroleum gas industry, but has relevant information for fighting pressurized gas fires. Per Table 5 ·Water -Application Methods: .. One disadvantage of water deluge and water sprays is that they ... may not be effective for jet (torch) fires. Also Section 5.5 Detection Systems gives general guidance on hydrocarbon vapor detectors, heat detectors and flame detectors. This facility includes all three systems, and complies with the guidance of this document. 13.3.6 Fire fighting and suppression standards in the oil and gas industry vary from standard industrial, high rise, and low rise practices. The engineering standards employed in the design of hydrocarbon equipment are conservative and attempt to contain hydrocarbon inventories within the equipment. However, in the event of a leak, the design of the external areas surrounding the equipment are designed to quickly isolate the leak, depressure the equipment, prevent the spread of the hydrocarbon leak, minimize the propagation of any fire event, maintain mechanical integrity through inventory liquidation without catastrophic failure, and minimize exposure to personnel and environment. Chevron SOPs require facility personnel to not engage in fire fighting beyond the incipient stage. The facility and the enclosures have been designed within these parameters. Page 12/14 t i z;; Title: PICEANCE FIRE PROTECTION PHILOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 Appendix A 1.0 GAS DETECTION SYSTEM OPERATING DETAILS REV:O Page 13 of14 1.1 Each equipment enclosure is provided with a combustible gas detection system listed by a Nationally Recognized Testing Laboratory (NRTL) which exceeds the requirements of API Recommended Practice RPI4C. The gas detection sensor is wired to the facility Emergency Shutdown System (ESS). 1.2 When the gas detector in an equipment enclosure detects the presence of gas at 20% Lower Explosive Limit (LEL), it performs the following functions: • Indicates on the Human-Machine Interface (HMI) video screens in the Control Room • Indicates on the HMI on the nine (9) outdoor Local Control Panels • Activates a dedicated alarm on the audible alarm system • The 24VDC control system on the skid remains energized, and the skid remains in operation. 1.3 When the gas detector in an enclosure detects the presence of gas at 40% LEL, it performs the following functions: • Indicates on the HMI video screens in the Control Room • Indicates on the HMI on the nine (9) outdoor Local Control Panels • Activates a dedicated alarm on the audible alarm system • Trips off the AC power feed to that enclosure's explosion-proof panel board at its source in the Electrical Building. • Shuts off all hydrocarbon flow to the enclosure from the source outside of the enclosure • Shutdown valves which shut off hydrocarbon flow are fail-safe, pneumatically operated, and will also close upon safety system failure or loss of air pressure to the fusible loop system. • The 24VDC control system on the skid remains energized, but the skid remains shut off from hydrocarbon flow until the shutdown is manually reset by the Control Room operator. 1.4 The gas detection system shall be tested and recalibrated every 3 months in accordance with 30 CPR Chapter II Part 250.804 "Production safety-system testing and records." The gas detection system that is proposed will be certified by an NRTL to fully comply with this standard and with the system design details contained within API RP 500. Page 13/14 Title: PICEANCE FIRE PROTECTION PffiLOSOPHY Customer: Chevron Project: Piceance Basin Project Spec No: 2033-201-00-ST-0001 Date: 19 November 2008 AppendixB REV:O Page 14 of 14 1.0 EQUIPMENT ENCLOSURE FIRE DETECTION SYSTEM OPERATING DETAILS 1.1 Each equipment enclosure is provided with a pneumatic fusible plug loop fire detection system which exceeds the requirements of API Recommended Practice RP14C. A pressure transmitter, wired to the facility Emergency Shutdown System (ESS), monitors the fusible loop's pneumatic pressure. 1.2 When a fusible plug inside of the equipment enclosure melts in the presence of a fire, the pressure transmitter detects the loss of air pressure in the fusible loop system and signals the ESS which performs the following functions: • Indicates on the HMI video screens iu the Control Room • Indicates on the HMI on the nine (9) outdoor Local Control Panels • Activates a dedicated alarm on the audible alarm system • Trips off the AC power feed to that enclosure's explosion-proof panelboard at its source in the Electrical Building. • Shuts off all hydrocarbon flow to the entire facility • Shutdown valves which shut off hydrocarbon flow are fail-safe, pneumatically operated, and will also close upon safety system failure or loss of air pressure to the fusible loop system. • The 24VDC control system on the skid remains energized, but the skid remains shut off from hydrocarbon flow until the shutdown is manually reset by the Control Room operator. • Depressures the bulk of the natural gas process lines and vessels within the facility to the flare. (Some sections of piping and vessels outside of the building enclosures, such as the glycol reboiler, may have minor amounts of residual gas under pressure.) 1.3 Each of the enclosures rated for H-2 occupancy will also be equipped with triple infrared flame detectors ("fire eyes") per section 8.3 and pneumatic fusible loop system per section 8.2. 1.4 Because the enclosures are exposed to ambient weather and Class I, Division 1 conditions, and because there are no commercially available weatherproof smoke detectors rated for Class I, Division 1 service, smoke detection systems will not be installed in this facility. Instead, our design philosophy is to use gas detection to detect the presence of a potentially dangerous atmospheric hazard and, in parallel, to use two different technologies (triple infrared flame detection and pneumatic fusible heat detection.) We propose the API-RP500 methodology of detecting the gases and shutting down the plant upon detection of dangerous levels of flammable gas. Page 14/14 Date: 1 o I 20 I 2008 07-27053 Calculations Hazardous Materials Occupancy Time: 1:57:43 PM Page: 1 of 175 VP Buildings 3200 Players Club Circle Memphis, TN 38125-8843 STRUCTURAL DESIGN DATA Project: Chevron Name: 7079 Chevron R1_Stress Check 10_2008 with 08_2008 Loading Builder PO #: Jobsite: near DeBeque CO City, State: Rifle, Colorado 81650 County: Garfield Country: United States TABLE OF CONTENTS Letter of Certification ............................................................................................................................................ 2 Building Loading-Expanded Report ......................... , .......................................................................................... 4 Reactions -Expanded Report .............................................................................................................................. 22 Bracing -Summary Report ........................... ~ ...................................................................................................... 57 Secondary-Summary Report .............................................................................................................................. 67 Framing -Summary Report ................................................................................................................................. 83 Covering -Summary Report ....... : ................................................. , ................................................. : .................. 173 File: 7079 Chevron R1_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Name: Alta Construction, Inc. Address: 17 Smith Fork Way City, State: Lyman, Wyoming 82937 Country: United States Builder PO#: Jobsite: near DeBeque CO City, State: Rifle, Colorado 81650 County, Country: Garfield, United States This is to certify that the above referenced VP BUILDINGS project has been designed for the applicable portions of the following Building Code and in accordance with the order documents which have stipulated the following applied environmental loads and conditions: Overall Building Description Shape Overall Overall Floor Area Wall Area Roof Area Max. Eave Min. Eave Max. Roof Min. Roof Peak Width Length (sq. ft.) (sq. ft.) (sq. ft.) Height Height2 Pitch Pitch Height base 53/0/0 154/0/0 8162 13716 8604 32/0/0 Loads and Codes -Shape: base City: Rifle County: Garfield State: Colorado 89AJSC 04AISJ Building Code: 2003 International Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind Loa~ WindSpeed~~ Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: . Wind Enclosure: Enclosed Wind Importance Factor: 1.1 SO Topographic Factor: 1.0000 NOT Windbome Debris Regiori Base Elevation: 0/0/0 Primary Zone Strip Width: I 017/3 Parts I Portions Zone Strip Width: 5/3/10 Basic Wind Pressure: 20.74 psf c rane c e u e norma on Shdll~ ti Name Type 5 ton UH Underhung __ Crane Built Up: Cold Form: Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf SnowLoad ~ Roof Snow Load: 5.00 psf Design Snow (Slope ): . 0 psf Snow Exposure Category (Factor): 2 Partially Exposed (1.00) Snow Importance: 1.100 Thennal Category (Factor): Heated ( 1. 00) Ground I Roof Conversion: 0.70 % Snow Used in Seismic: 20.00 Seismic SnOw Load: 15.00 psf Unobstructed, Slippery Roof Service Classification Method of Operation C{Moderate Service)_ Pendant Qperated 32/0/0 4.000:12 4.000:12 40/10/0 Country: United States Rainfall: 4.00 inches per hour Live Load Live Load: 20.00 psf Not Reducible Seismic Load Mapped Spectral Response * Ss:43.60 %g Mapped Spectral Response~ 81:9.10 %g Seismic Hazard I Use Group: Group 2 Seismic Importance: 1.250 Seismic Performance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Bracing Seisrilic Period: 0.2691 Framing R-Factor: 3.0000 Bracing R-Factor: 3.0000 Soil Profile Type: Stiff soil (0, 4) Frame Redundancy Factor: 1.0000 Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W _ Capacity (Ton). Bridge Bridge Construction Span 5.00 42/0/0 Single Girder Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain all code and loading infonnation for this specific building site. The steel design is in accordance with VP BUILDINGS standard design practices, which have been established based upon pertinent procedures and recommendations of the following organizations: American Institute of Steel ConstruCtion (AISC) American Iron and Steel Institute (AISI) American Welding Society (A WS) American Society for Testing and Materials (ASTM) Canadian Standards Association CSA W59-Welded Steel Construction Limit State Design of Steel Structures Metal Building ManufacturerS Association (MBMA) VP Buildings is certified by: • CSA A660 Certified (Design and Manufacturing) File: 7079 Chevron R\_Stress Check 10_2008with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy -IAS Approved Fabricator -Canadian Welding Bureau Div. I Certified Date: 1 o I 20 I zoos Time: I :57:43 PM Page: 3 of 175 VP Buildings has designed the structural steel components of this building in accordance with the Building Code, Steel Specifications, and Standards indicated above. Steel components are designed utilizing the following steel grades unless noted otherwise: 3 Plate members fabricated from plate, bar, strip steel or sheets ASTM A529, A572, A lOll -All Grade 55 ksi Hot Rolled Shapes 011, S, C, Angles, etc) ASTM A36, or ASTM A36Mod50, A529, A572, A588, A709, A992-Al! Grade 50 ksi Tube and Pipe Sections ASTM ASOO, Grade B (Fy • 42 ksi pipe, Fy-46 kSi tube) Light Gage Sections ASTM A I Oll SS Grade 55 ksi, A653 SS Grade 55 ksi Round Rod Bracing ASTM AS72 Grade 65 ksi This certification DOES NOT apply to the design of the foundation or other on-site structures or components not supplied by VP BUILDINGS, nor does it apply to unauthorized modifications to framing systems provided by VP BUlLDINGS. Furthermore, it is understood that certification is based upon the premise that all components furnished by VP BUILDINGS will be erected or constructed in strict compliance with pertinent documents furnished by VP BUILDINGS. Prepru-ed by: tv\~ :.: ,, File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Shape: base Loads and Codes ~Shape: base City: Rifle County: Garfield Building Code: 2003 International Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Side Type A D A D B D B D Live Load Mag 3.390 l.l20 3.390 l.l20 Units psf psf psf psf Shape Entire Entire Entire Entire Live Load: 20.00 psf Not Reducible Wind Load Wind Speed: 90.00 mph Wind Enclosure: Enclosed Height Used: 36/5/0 (Type: Mean) Base Elevation: 0/0/0 Primary Zone Strip Width: 1017/3 Velocity Pressure: (qz) 23.85 psf Topographic Factor: 1.0000 Directionality Factor: 0.8500 Wind-Exposure (Factor): C (1.023) Basic Wind Pressure: 20.74 psf Snow Load Roof Snow Load: 75.00 psf Design Snow (Sloped): 75.00 psf Snow Accumulation Factor:: 1.000 Snow Importance: 1.109 Ground I Roof Conversion: 0. 70 Seismic Load Mapped Spectral Response w Ss:4J.60 %g Mapped Spectral Response-Sl:9.!.0 %g Seismic Hazard I Use Group: Group 2 Seismic Perfonnance I Design Category: C System NOT detailed for Seismic Seismic Importance: 1.250 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W Framing R-Factor: 3.0000 Bracing R-Factor: 3.0000 Side Type Mag Units Shape I E 0.310 psf Entire E 0.403 psf Entire E 0.008 kif Cranes E 0.011 kif Cranes 2 E 0.291 psf Entire 2 E 0.378 psf Entire 2 E 0.008 kif Cranes 2 E 0.0! I kif Cranes Applied to Fnn Pur Fnn Pur Applied to Frm Bro Fnn Bee Frm Bee Fm> Bee State: Built Up: Colorado 89AISC 04AISI Cold Fonn: Country: United States Rainfall: 4.00 inches per hour Frame Weight (assumed for seismic):8.00 psf Description Covering Weight w 24 Panel Rib+ Secondary Weight 2.27 ; Roof: A Covering Weight w 24 Panel Rib: Roof: A Covering Weight-24 Panel Rib+ Secondary Weight 2.27 :Roof: B Covering Weight w 24 Panel Rib: Roof: B Gust Factor: 1.0000 Wind Importance Factor: 1.150 Least Horiz. Dimension: 53/0/0 NOT Windborne Debris Region Parts /Portions Zone Strip Width: 5/3/10 qz=Q.00256' (!.IS)' (90.00)A2 '(!.00) The 'Low Rise' Method is Used Snow Exposure Category (Factor): 2 Partially ExpOsed (1.00) Thennal Category (Factor): Heated (1.00) Unobstructed, Slippery Roof Rain Surcharge: 0.00 Slope Reduction: 0.79 Slope Used: 18.435 ( 4.000:12) %Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Frame Redundancy Factor: 1.0000 BraCe Redundancy Factor: 1.0000 Soil Profile Type: Stiff soil (D, 4) Framing Seismic Period: 0.4480 Bracing Seismic Period: 0.2691 Seismic Period Height Used: 32/0/0 Design Spectral Response-Sds: 0.4218 Design Spectral Response-Sdl: 0.1456 Description Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 1.17: Wall: Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 1.17 : Wall: I Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Wall: I Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Wall: I Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 1.03 :Wall: 2 Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 1.03 : Wall: 2 Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Wal\:2 Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Wall: 2 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Verslon: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 5 of !75 3 E 0.) 10 psf Entire Fnn 3 E 0.403 psf Entire Brc 3 E 0.008 k1f Cranes Fnn 3 E 0.011 k1f Cranes Brc 4 E 0.325 psf Entire Fnn 4 E 0.422 psf Entire Brc 4 E 0.008 k1f Cranes Fnn 4 E 0.011 k1f Cranes Brc A E 6.282 psf Entire Fnn A E 8.153 psf Entire BrC A E 0.008 k1f Cranes Fnn A E 0.011 k1f Cranes Brc B E 6.282 psf Entire Fnn B E 8.153 psf Entire Brc B E 0.008 k1f Cranes Fnn B E O.Oll k1f Cranes Brc Deflection Conditions Frames are vertically. supporting: Metal RoofPurlins and Panels Deflection Limit Ovenide V /240 Frames are laterally supporting:Underhung Crane Deflection Limit Override W400 Purlins are supporting:Meta1 Roof Panels Deflection Limit Override V/240 Girts are supporting:Metal Wall Panels Deflection Limit Override Hl240 Seismic: Covering Weight N 24 Panel Rib+ Secondary Weight 1.17 : Wall: 3 Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 1.!7: Wall: 3 Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Wall:3 Seismic Effect From Au~ei!iary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Wa11:3 Seismic: Covering Weight-24 Panel Rib+ Secondary Weight !.28 : Wall: 4 Seismic: Covering Weight N 24 Panel Rib+ Secondary Weight L28: Wall: 4 Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt : Wa11:4 Seismic Effect From Auxilia1y Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Wa!l:4 Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 2.27 + 15.000 Snow+ (Includes 20.000 Collateral 8.000 Frame Weight) :Roof: A Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 2.27 + 15.000 Snow+ (Includes 20.000 Collateral 8.000 Frame Weight): Roof: A Seismic EffectFromAuxilimy Dead Load, 5 ton UH and Bridge Wt and Trolley /Hoist Wt: Roof: A Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Troliey I Hoist Wt: Roof: A Seismic: Covering Weight M 24 Panel Rib+ Secondary Weight 2.27 + 15.000 Snow+ (Includes 20.000 Collateral 8.000 Frame Weight): Roof: B Seismic: Covering Weight-24 Panel Rib+ Secondary Weight 2.27 + 15.000 Snow+ (Includes 20.000 Collateral 8.000 Frame Weight) :Roof: B Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Roof: B Seismic Effect From Auxiliary Dead Load, 5 ton UH and Bridge Wt and Trolley I Hoist Wt: Roof: B c rane c e u e norma on Shd111 t1 I Name Type Service Classification Method of Operation Capacity Bridge Bridge Construction IT on) Soan I 5 ton UH Underhung Crane C (Moderate Service) Pendant Operated 5.00 421010 Single Girder I Name I Bridge Wt I : Trolley I ) ll Wheel Wheel No. of Horz. Vert. Headroom Crane Note lk) Hoist Wt lkl Soacin Load (k) Wheels Clear Clear Soacing I 5 ton UH I 7.15 I l.lO I 61010 7.34 2 11310 01010 4/810 0/ll/0 Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain all code and loading infonnation for this specific building site. Desien Load Combinations-Framin No. Origin Factor Aoolication Description 1 System 1.000 1.0 D+ 1.0 AD+ l.OCG + 1.0 S D+AD+CG+S 2 System 1.000 1.0 D +LOAD+ 1.0 CG + 1.0 US\"' D+AD+CG+USl~ 3 System 1.000 1.0 D + 1.0 AD+ !.0 CG + 1.0 *USl D+AD+CG+*USJ 4 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WI> D+AD+CG+Wl> 5 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <Wl D +AD+ CG +<WI 6 System 1.000 1.0 D + l.O AD + 1.0 CO + 1.0 W2> D+AD+CG+W2> 7 System 1.000 !.0 D + 1.0 AD + 1.0 CG + 1.0 <W2 D+AD+CG+<W2 8 System 1.000 1.0 D+ J.O AD+ 1.0 CG + 0.750 S +0.750 WI> D+AD+CG+S+Wl> 9 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <Wl D+AD+CG+S+<W! lO System 1.000 1.0 D + 1.0 AD+ !.0 CG + 0.750 S + 0.750 W2> D + AD+CG + S + W2> 11 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <W2 D+ AD+CG +S+<W2 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: I :57:43 PM Page: 6 of 175 12 System 1.000 LO D + 1.0 AD+ 1.0 CO+ 1.0 *AL> D+AD+CG+*AL> 13 System 1.000 !.0 D + 1.0 AD + 1.0 CG + 1.0 AL *> D+AD+CG+AL*> 14 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + LO <*AL D +AD+ CG+<*AL 15 System 1.000 l.OD + 1.0 AD+ LOCO+ l.O<AL* D+ AD+CG+<AL* 16 System 1.000 .600 D + 0.600 AD+ 0.600 CU + 1.0 WI> D+AD+CU+Wl> 17 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<Wl 18 System 1.000 0.600 D + Q.600 AD+ 0:600 CU + 1.0 W2> D+AD+CU+W2> 19 System 1.000 0.600 D + Q.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 *AL> D +AD+ CG + S+*AL> 21 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL *> D+AD+CG+S+AL*> 22 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 <*AL D+AD+CG+S+<*AL 23 System 1.000 1.0 D +LOAD+ 1.0 CG + 0.563 S +0.750 <AL* D+AD+CG+S+<AL* 24 System 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WI>+ 0.750 *AL> D+AD+CG+Wl>+*AL> 25 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WI>+ 0.750 AL*> +AD+ CG + Wl>+AL *> 26 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 <WI+ 0.750 <*AL D+AD+CG +<Wl+<*AL 27 System 1.000 1.0 D + 1.0 AD+ 1.0 CG+ 0.375 <WI +0.750 <AL* D+AD+CG+<Wl+<AL* 28 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 W2>+ 0.750 *AL> D+AD+CG +W2>+*AL> 29 System 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 W2> +0.750 AL*> D + AD+ CG + W2>+AL *> 30 System 1.000 1.0 D+ 1.0 AD+ l.O CG +0.375 <W2 -i-0.750 <*AL + AD+ CG + <W2+<* AL 31 System 1.000 1.0 D + 1.0 AD+ l.O CG + 0.375 <W2 + 0.750 <AL* + AD+ CG + <W2+<AL * 32 System 1.000 1.0 D + 1.0 AD+ l.OCG+O.J50 S + 0.750 E> +0.100 EG+ AD+CG+S+E>+EG+ 33. System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.150 S +0.750<E+0.700 EG+ AD+CG+S+<E+EG+ 34 System 1.000 .600 D + o.600 AD+ 0.600 CU + 0.700 E> + 0.700 EG-+AD+CU+E>+EG- 35 System 1.000 Q.600 D + o.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-+AD+CU+<E+EG- 36 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 0.150 S +0.750 EB>+0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 .600 D + 0.600 AD+ o.600 CU + 0.700 EB> + 0.700 EG-D+AD+CU+EB>+EG- 38 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.150 S +0.750 <EB +0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived 1.000 .600 D + 0.600 AD+ 0.600 CU + 0.700 <EB + 0.700 EG-+AD+CU+<EB+EG- 40 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 1.0 WPAI +AD+CG+WPAl 41 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPAI +AD+CG+S+WPAI 42 System Derived 1.000 .600 D +o.600 AD +0.600CU + 1.0 WPAJ D+AD+CU+WPAl 43 System Derived · 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPAJ +0.750 *AL+0.750 ALB> D+AD+CG+WPAl+*AL+ALB> 44 System Derived 1.000 1.0 D + l.O AD+ 1.0 CG +0.375 WPAI +0.750 AL* + 0.750 ALB> +AD+CG+WPAl+AL*+ALB> 45 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPDI +AD+CG+WPDI 46 System Derived 1.000 1.0 D.+ 1.0 AD+ 1.0 CG +0.750 S +0.750 WPDI +AD+CG+S+WPDI 47 System Derived 1.000 .600 D +0.600 AD +0.600CU + 1.0 WPDI D+AD+CU+WPDI 48 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG+ 0.375 WPDJ +0.750 *AL + 0.750 <ALB D+AD+CG+WPDJ+*AL+<ALB 49 System Derived 1.000 l.O D-!-1.0 AD+ 1.0 CG+0.375 WPDl +0.750 AL* + 0.750 <ALB +AD+CG+WPDl+AL*+<ALB 50 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA2 +AD+CG+WPA2 51 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 WPA2 +AD+CG+S+WPA2 52 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPA2 D+AD+CU+WPA2 53 System Derived 1.000 l.O D+ 1.0 AD+ l.O CG + 0.375 WPA2 +0.750 *AL + 0.750 ALB> +AD+CG+WPA2+*AL+ALB> 54 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.375 WPA2 +0.750 AL* + 0.750 ALB> +AD+CG+WPA2+AL*+ALB> 55 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPD2 D+AD+CG+WPD2 56 System DeriVed 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPD2 +AD+CG+S+WPD2 57 System Derived 1..000 .600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 WPD2 +0.750 *AL + 0.750 <ALB D+AD+CG+WPD2+*AL+<ALB 59 System Derived 1.000 l.O D+ 1.0 AD+ 1.0 CG +0.375 WPD2 +0.750 AL* + 0.750 <ALB D+AD+CG+WPD2+AL *+<ALB 60 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPBI D+AD+CG+WPBI 61 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPBJ D+AD+CG+S+WPBl 62 System Derived 1.000 .600 D +0.600 AD+ 0.600CU + 1.0 WPBJ D+AD+CU+WPBI 63 System Derived 1.000 1.0 D + l.O AD+ 1.0 CG + 0.375 WPBI + 0.750 *AL + 0.750 ALB> D+AD+CG+WPBI+*AL +ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPBI +0.750 AL* +0.750 ALB> D+AD+CG+WPBl+AL *+ALB> 65 System Derived 1.000 J.OD+ LOAD+ l.OCG+ J.OWPCJ D+AD+CG+WPCI 66 System Derived 1.000 1.0 D+ 1.0 AD+ J.OCG +0.7508 +0.750 WPCJ D+AD+CG+S+WPCl 67 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPCJ D+AD+CU+WPCI 68 System Derived 1.000 l.O D+ 1.0 AD+ 1.0 CG +0.375 WPCl + 0.750 *AL + 0.750 <ALB +AD+CG+WPC I+* AL +<ALB 69 System Derived 1.000 1.0 D + I .0 AD+ 1.0 CG + 0.375 WPCI + 0.750 AL * + 0.750 <ALB +AD+CG+W:PC I+AL *+<ALB 70 System Derived 1.000 \.0 D + 1.0 AD+ 1.0 CG + !.0 WPB2 D+AD+CG+WPB2 71 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG + 0.750 S + 0.750 WPB2 +AD+CG +S+ WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 Q+AD+CU+WPB2 73 System Derived 1.000 1.0 D+ LOAD+ 1.0 CG + 0.375 WPB2 + 0.750 *AL + 0.750 ALB> D+AD+CG+WPB2+*AL+ALB> 74 SyStem Derived 1.000 1.0 D + 1.0 AD+ I .0 CG + 0.375 WPB2 + 0. 750 AL * + 0.750 ALB> D+AD+CG+WPB2+AL *+ALB> 75 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPC2 D+ AD+CG + WPC2 76 System Derived !.000 !.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC2 D + AD+CG + S+ WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 D+AD+CU+WPC2 78 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPC2 +0.750 *AL + 0.750 <ALB D+/\D+CG+WPC2+* AL +<ALB File: 7079 Chevron Rl_Stress Check 10_2008 wilh 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 7 of 175 79 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPC2 + 0.750 AL* + 0.750 <ALB D+AD+CG+WPC2+AL *+<ALB 80 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 S + 1.0 ALB> D+AD+CG+S+ALB> 81 System Derived 1.000 1.0 D + t.O AD+ 1.0 CG + 1.0 *AL + 1.0 ALB> D +AD+ CG+*AL+ALB> 82 System Derived 1.000 1.0 D + t.O AD + 1.0 CG + 1.0 AL * + 1.0 ALB> D +AD+ CG+AL *+ALB> 83 System Derived 1.000 1.0 D +LOAD+ 1.0 CO+ 0.563 S + 0.750 *AL + 0.750 ALB> D+AD+CG+S+*AL+ALB> 84 System Deriveq 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.563 S + 0.750 AL* + 0.750 ALB> D+AD+CG+S+AL *+ALB> 85 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 S + 1.0 <ALB D+ AD+CG +S+<ALB 86 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 *AL + LO <ALB D+ AD+CG+*AL+<ALB 87 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 AL * + 1.0 <ALB D +AD+ CG+AL *+<ALB 88 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 *AL + 0.750 <ALB D+AD+CG+S+*AL+<ALB 89 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 AL* +0.750 <ALB D+AD+CG+S+AL *+<ALB Desi_gn Load Combinations~ BracinJ,! No. Origin Factor Application Description 1 System 1.000 0.700 E> E> 2 SYstem 1.000 .700 <E (E 3 System 1.000 l.OWPA1 WPA1 4 System 1.000 1.0 WPD1 WPD1 5 System 1.000 1.0 WPA2 WPA2 6 System 1.000 l.OWPD2 WPDZ 7 System 1.000 1.0 WPB1 WPB1 8 System 1.000 1.0 WPC1 WPC1 9 System 1.000 1.0 WPB2 WPB2 10 System 1.000 1.0 WPC2 WPC2 11 System 1.000 0.375 WPA1 +0.750 AL' WPAl+AL* 12 System 1.000 .375 WPD1 +0.750 'AL WPDl+*AL 13 System 1.000 ~.375 WPA2 +0.750 AL' WPA2+AL* 14 System 1.000 .375 WPD2 +0.750 'AL :~2+*AL 15 System 1.000 0.375WPB1 +0.750AL' Bl+AL* 16 System 1.000 0.375 WPC1 +0.750 'AL WPCI+*AL 17 System 1.000 .375 WPB2 +0.750 AL' WPB2+AL* 18 System 1.000 0.375 WPC2 +0.750 *AL WPC2+*AL 19 System 1.000 1.0 AL* . AL* 20 Svstem 1.000 1.0 *AL 'AL . D esign L C 11 oad ombmations ~Pur n No. Origin Factor Application Descriotion 1 System 1.000 l.OD+l.OCG+l.OS D+CG+S 2 System 1.000 l.OD+ l.OCG+ l.OUS1' D+CG+USl* 3 System 1.000 1.0 D+ 1.0 CG+ 1.0 'US1 D+CG+'US1 4 System 1.000 1.0 D + 1.0 CG + 1.0 PF1 D+CG+PF1(Span 1) 5 System 1.000 l.OD+l.OCG+l.OPF1 D +CG + PF1(Span 9) 6 System 1.000 1.0 D + 1.0 CG + 1.0 PH1 D+CG+PH1(Span 1) 7 System 1.000 1.0 D + 1.0 CG + 1.0 PH1 D + CG + PHJ (Span 9) 8 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 D + CG + PF2(Spans 1 and 2) 9 System 1.000 l.OD+ LOCG+ LOPF2 D +CO+ PF2{Spans 2 and 3) 10 System 1.000 LOD+l.OCG+LOPF2 D +CO+ PF2(Spans 3 and 4) 11 System 1.000 1.0 D+ l.OCG + 1.0 PF2 D + CG + PF2(Spans 4 and 5) 12 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 D + CG + PF2(Spans 5 and 6) 13 s'ystem 1.000 LOD+ 1.0 CG + 1.0 PF2 D + CG + PF2(Spans 6 and 7) 14 System 1.000 1.0 D+ LOCO+ 1.0 PF2 D + CG + PF2(Spans 7 and 8) 15 System 1.000 1.00+ l.OCG + l.OPF2 D + CG + PFZ(Spans 8 and 9) 16 System 1.000 1.0 D + 1.0 CG + J.O Wl> D+CG+Wl> 17 System 1.000 l.OD+ l.OCG+ l.O<W2 D+CG+<W2 18 System 1.000 o.600 D + 0.600 CU + 1.0 W1> D+CU+W1> 19 System 1.000 0.600 D + o.600 CU + 1.0 <W2 D+CU+<W2 20 System 1.000 1.0 D + i.O CG + 0.750 S +0.750 WI> D+CG+S+W1> 21 System 1.000 LOD+ LOCO +0.750S+0.750<W2 D+CG+S+<W2 22 System Derived 1.000 1.0 D + 1.0 CG + 0.150 S + 0.750 EB> + 0.700 EG+ D+CG+S+EB>+EG+ 23 System Derived 1.200 1.200 D + 1.200 CG +0.200 S + 1.0 EB> + 0.700 EG+ D+CG+S+EB>+EG+ 24 System Derived 1.200 0.900 D + 0.900 CG + 1.0 EB> + 0.700 EG-D+CG+EB>+EG~ 25 System Derived !.000 Q.600 D + 0.600 CU + 0.700 EB> +0.700 EG-D+CU+EB>+EO" 26 System Derived 1.000 1.0 D + 1.0 CG + 0.150 S + 0.750 <EB + 0.700 EG+ D+CG+S+<EB+EG+ 27 System Derived 1.200 \.200D + 1.200 CG +0.200S + 1.0 <EB+0.700 EG+ D+CG+S+<EB+EG+ 28 System Derived 1.200 0.900 D + 0.900 CG + !,0 <EB + 0.700 EG~ D+CG+<EB+EG~ 29 System Derived 1.000 0.600 D + 0.600 CU + 0.700 <EB + 0.700 EO~ D+CU+<EB+EG- File: 7079 Chevron R !_Stress Check I 0_2008 with 08 _2008 Loading Version: 7.la . 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 8 of 175 30 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPAI D+CG+WPAI 31 System Derived 1.000 ~.600 D + 0.600 CU + 1.0 WPAI D+CU +WPAI 32 System Derived 1.000 1.0 D + 1.0 CO+ 0.750 S + 0.750 WPAI D+CG+S+WPAI 33 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPDI D+CG+WPDl 34 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPDJ D+CU+WPDI 35 System Derived 1.000 1.0 D + 1.0 CG +0.750 S + 0.750 WPDI D+CG+S+WPDJ 36 System Derived 1.000 1.0 D + 1.0 CO+ 1.0 WPA2 D+CG+WPA2 37 System Derived 1.000 p.600 D + 0.600 CU + 1.0 WPA2 D+CU+WPA2 38 System Derived 1.000 1.0 D + 1.0 CG + 0.750 S + 0.750 WPA2 D+CG+S+WPA2 39 System Derived 1.000 1.0 D + 1.0 CO+ 1.0 WPD2 D+CG+WPD2 40 System Derived 1.000 p.600 D + 0.600 CU + 1.0 WPD2 D+CU+WPD2 41 System Derived 1.000 1.0 D + 1.0 CO +0.750 S + 0.750 WPD2 D+CG+S+WPD2 42 System Derived 1.000 1.0 D+ 1.0 CO+ I.OWPBJ D+CO+WPBJ 43 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPB I . D+CU+WPBI 44 System Derived 1.000 1.0 D + 1.0 CO+ 0.750 S + 0.750 WPB I D+CG+S+WPBl 45 System Derived 1.000 1.0 D + 1.0 CO+ J·.O WPCI D+CO+WPCI 46 System Derived 1.000 0.600 D+ 0.600 CU + 1.0 WPCJ D+CU+WPCI 47 System Derived 1.000 1.0 D + 1.0 CO +0.750 S + 0.750 WPCJ D+CO+S+WPCJ 48 System Derived 1.000 1.0 D + 1.0 CO + 1.0 WPB2 D+CO+WPB2 49 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPB2 l)+CU+WPB2 so System Derived 1.000 1.0 D + 1.0 CG +0.750 S + 0.750 WPB2 D+CG+S+WPB2 51 System Derived 1.000 1.0 D + 1.0 CO + 1.0 WPC2 D+CG+WPC2 52 System Derived 1.000 p.600 D + 0.600 CU + 1.0 WPC2 D+CU+WPC2 53 System Derived 1.000 1.0 D + 1.0 CO +0.750 S + 0.750 WPC2 D+CG+S+WPC2 Desien Load Combinations ~ Girt No. Or_ig_in Factor A,ppjication Desc~jption 1 System 1.000 LOW!> WI> 2 System 1.000 1:o<w2 <W2 3 System Derived 1.000 ~.700EB> EB> 4 System Derived 1.000 J.OWPAI WPAI 5 System Derived 1.000 1.0 WPA2 WPA2 6 System Derived 1.000 1.0 WPBI WPBI 7 System Derived 1.000 1.0 WPB2 WPB2 8 System Derived 1.000 0.700<EB EB 9 System Derived 1.000 1.0 WPDI WPDI 10 System Derived 1.000 l.OWPD2 WPD2 II System Derived 1.000 l.OWPCJ WPCJ 12 §ystem Derived 1.000 1.0 WPC2 WPC2 D I L dC b es n oa om inat ons ~ R f P 00 • ane No. Origin Factor Application Description I System 1.000 J.OD+J.OS D+S 2 System 1.000 l.OD+ l.OUSI* D+USI* 3 System 1.000 1.0 D + 1.0 *USI D+*USt 4 System 1.000 1.0 D + 1.0 WI> D+WJ> 5 System 1.000 l.O D + l.O <W2 D+<W2 6 System 1.000 .600 D+ 1.0 WI> D+Wt> 7 System 1.000 .600 D+ I.O<W2 D+<W2 Desi n Load Combinations~ Wall~ Panel No. Orj_gjn Factor A~;~p_lication Descr)ption I System 1.000 1.0 WI> WI> 2 ~y§tem 1.000 l.O<W2 W2 D fl I L d C b" F e ect on oa om mataons ~ ramm No. Origin Factor DefH DefY Application Description I System 1.000 0 240 1.0 s . s 2 System 1.000 0 240 !.0 US\* US!* 3 System 1.000 0 240 1.0 *US I *US! 4 System 1.000 0 240 0.700 Wl> WJ> 5 System 1.000 0 240 0.700 <WI <WI 6 System 1.000 0 240 0.700 W2> W2> 7 System 1.000 0 240 0.700 <W2 <W2 8 System Derived 1.000 0 240 0.700 WPAI WPAI 9 System Derived 1.000 0 240 ~.700 WPDJ WPDl File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 9 of 175 10 System DeriVed 1.000 0 240 0.700 WPA2 WPA2 II System Derived LOOO 0 240 0.700 WPD2 Wl)D2 12 System Derived LOOO 0 240 0.700 WPBI WPBI 13 System Derived LOOO 0 240 0.700 WPCI WPC1 14 System Derived 1.000 0 240 0.700 WPB2 WPB2 15 System Derived LOOO 0 240 0.700 WPC2 WPC2 16 System 1.000 400 0 0.700 WI> WI> 17 System LOOO 400 0 0.700<Wl WI \8 System 1.000 400 0 0.700 W2> W2> 19 System 1.000 400 0 0.700<W2 <W2 20 System Derived LOOO 400 0 0.700 WPAI WPAI 21 System Derived 1.000 400 0 0.700 WPDI WPDI 22 System Derived LOOO 400 0 0.700 WPA2 WPA2 23 System Derived LOOO 400 0 0.700WPD2 WPD2 24 System Derived 1.000 400 0 0.700 WPBI WPBI 25 System Derived LOOO 400 0 0.700WPCI WPCI 26 System Derived LOOO 400 0 0.700 WPB2 WPB2 27 System Derived LOGO 400 0 0.700 WPC2 WPC2 28 System LOGO 100 0 0.600 E> + 0. 700 EG-E>+EG· 29 System LOOO 100 0 .600 <E + 0. 700 EG-E+EG- 30 System Derived LOOO \00 0 0.600 EB> EB> 31 System Derived 1.000 \00 0 0.600 <EB l<EB 32 System LOOO 400 0 l.O<AL"' AL* 33 Svstem LOOO 400 0 1.0 *AL> *AL> Deflection Load Combinations Purlin - No. Origin Factor Deflection Application Description I System LOOO 240 LOs s 2 System LOOO 240 1.0 USI"' US\* 3 System LOOO 240 1.0 *USl *USl Dfltl LdC b'tl G'rt e cc on oa om ma ons-' No. Ori~rin Factor Deflection Aoolication Descriotion I System \.000 240 .700WI> WI> 2 Svstem \.000 240 .700<W2 W2 Deflectio Lo d Combinatlo Roof Panel n a ns-- NO. Origin Factor DefH DefY Application Description I System \.000 !50 !50 LOS s 2 System \.000 !50 ISO I.OUSl* USI* 3 Svstem \.000 !50 ISO \.0 *US\ *USl Load Type Descriptions D Material Dead Weight c Collateral Load CG Collateral Load for Gravity Cases cu Collateral Load for Wind Cases L Live Load ASL" Alternate Span Live Load, Shifted Right "ASL Alternate Span Live Load, Shifted Left PL2 Partial Live, Full, 2 Spans L> Live~ Notional Right <L Live ~Notional Left s Snow Load US!* Unbalanced Snow Load l, Shifted Right *US! Unbalanced Snow Load 1, Shifted Left US2* Unbalanced Snow-Load 2, Shifted Right *US2 Unbalanced Snow Load 2, Shifted Left SD Snow Drift Load ss Sliding Snow Load RS Rain Surcharge Load PFI Partial Load, Full, I Span PHI Partial Load, Half, I Span PF2 Partial Load, Full, 2 Spans PH2 Partial Load, Half, 2 Spans S> Snow· Notional Right <S Snow ·Notional Left MRS Minimum Roof Snow MRS> Minimum Roof Snow-Notional Right <MRS Minimum Roof Snow -Notional Left w Wind Load WI> Wind Load, Case I, Right <WI Wind Load, Case I, Left W2> Wind Load, Case 2, Right <W2 Wind Load, Case 2, Left W3> Wind Load, Case 3, Right <W3 Wind Load, Case 3, Left W4> Wind Load, Case 4, Right <W4 Wind Load, Case 4, Left WS> Wind Load, Case 5, Right <WS Wind Load, Case S, Left W6> Wind Load, Case 6, Right <W6 Wind Load, Case 6, Left WP Wind Load, Parallel to Ridge WPR Wind Load, Jl Ridge, Right WPL Wind Load, II Ridge, Left WPAI Wind Parallel-Ref A, Case I WPA2 Wind Parallel -Ref A, Case 2 WP81 Wind Parallel-RefB, Case ! File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 10 of 175 WPB2 Wind Parallel· RefB, Case 2 WPCJ Wind Parallel· RefC, Case 1 WPC2 Wind Parallel -Ref C, Case 2 WPDI Wind Parallel-RefD, Case I WPD2 Wind Parallel-RefD, Case 2 WBI> Wind Brace Reaction, Case I, Right <WBI Wind Brace Reaction, Case 1, Left WB2> Wind Brace Reaction, Case 2, Right <WB2 Wind Brace Reaction, Case 2, Left WB3> Wind Brace Reaction, Case 3, Right <WB3 Wind Brace Reaction, Case 3, Left WB4> Wind Brace Reaction, Case 4, Right <WB4 Wind Brace Reaction, Case 4, Left WBS> Wind Brace Reaction, Case 5, Right <WBS Wind Brace Reaction, Case 5, Left WB6> Wind Brace Reaction, Case 6, Right <WB6 Wind Brace Reaction, Case 6, Left MW Minimum Wind Load MWB Minimum Wind Bracing Reaction E Seismic Lolld E> Seismic Load, Right <E Seismic Load, Left EG Vertical Seismic Effect EG+ Vertical Seismic Effect, Additive EG-Vertical Seismic Effect, Subtractive EB> Seismic Brace Reaction, Right <EB Seismic Brace Reaction, Left FL Floor Live Load FL' Alternate Span Floor Live Load, Shifted Right *FL Alternate Span Floor Live Load, Shifted Left FD Floor Dead Load AL Auxiliary Live Load AL*> Auxiliary Live Load, Right, Right *AL> Auxiliary Live Load, Right, Left <AL* Auxiliary Live Load, Left, Right <*AL Auxiliary Live Load, Left, Left AL' Aux Live, Right 'AL Aux Live, Left AL'>(I) Auxiliary Live Load, Right, Right, Aisle l 'AL>(J) Auxiliary Live Load, Right, Left, Aisle l <AL'(l) Auxiliary Live Load, Left, Right, Aisle 1 <*AL(l) Auxiliary Live Load, Left, Left, Aisle l AL'(I) Aux Live, Right, Aisle I *AL(l) Aux Live, Left, Aisle 1 AL*>(2) Auxiliary Live Load, Right, Right, Aisle 2 *AL>(2) Auxiliary Live Load, Right, Left, Aisle 2 <AL*(2) Auxiliary Live Load, Left, Right, Aisle 2 <*AL(2) Auxiliary Live Load, Left, Left, Aisle 2 AL'(2) Aux Live, Right, Aisle 2 *AL(2) Aux Live, Left, Aisle 2 AL'>(3) Auxiliary Live Load, Right, Right, Aisle 3 'AL>(3) Auxiliary Live Load, Right, Left, Aisle 3 <AL*(3) Auxiliary Live Load, Left, Right, Aisle 3 <*AL(3) Auxiliary Llve Load, Left, Left, Aisle 3 AL*(3) Aux Live, Right, Aisle 3 *AL(3) Aux Live, Left, Aisle 3 AL*>(4) Auxiliary Live Load, Right, Right, Aisle 4 *AL>(4) Auxiliary Live Load, Right, Left, Aisle 4 <AL*(4) Auxiliary Live Load, Left, Right, Aisle 4 <'AL(4) Auxiliary Live Load, Left, Left, Aisle_ 4 AL'(4) Aux Live, Right, Aisle 4 'AL(4) Aux Live, Left, Aisle 4 AL'>(S) Auxiliary Live Load, Right, Right, Aisle 5 'AL>(S) Auxiliary Live Load, Right, Left, Aisle 5 <AL'(S) Auxiliary Live Load, Left, Right, Aisle 5 <*AL(S) Auxiliary Live Load, Left, Left, Aisle 5 AL'(5) Aux Live, Right, Aisle 5 *AL(S) Aux Live, Left, Aisle 5 ALB Aux Live Bracing Reaction ALB> Aux Live Bracing Reaction, Right <ALB Aux Live Bracing Reaction, Left WALB> Wind, Aux Live Bracing Reaction, Right <WALB Wind, Aux Live Bracing Reaction, Left ALB>( I) Aux Live Bracing Reaction, Right, Aisle I <ALB(!) Aux Live Bracing Reaction, Left, Aisle 1 WALB>(J) Wind. Aux. Live Bracing Reaction, Right, Aisle l <WALB(I) Wind, Aux LiVe Bracing Reaction, Left, Aisle 1 ALB>(2) Aux Live Bracing Re.action, Right, Aisle 2 <ALB(2) Aux. Live Bracing Reaction, Left, Aisle 2 WALB>(2) Wind, Aux. Live Bracing Reaction, Right, Aisle 2 <WALB(2) Wind, Aux Live Bracing Reaction, Left, Aisle 2 ALB>(3) Aux. Live Bracing Reaction, Right, ~isle 3 <ALB(3) Aux Live Bracing Reaction, Left, Aisle 3 WALB>(3) Wind, Aux Live Bracing Reaction, Right, Aisle 3 <WALB(3) Wind, Aux Live Bracing Reaction, Left, Aisle 3 ALB>(4) Aux Live Bracing Reaction, Right, Aisle 4 <ALB(4) Aux Live Bracing Reaction, Left, Aisle 4 WALB>(4) Wind, Aux Live Bracing Reaction, Right, Aisle 4 <WALB(4) Wind, Aux. Live Bracing Reaction, Left, Aisle 4 ALB>(S) Aux Live Bracing Reaction, Right, Aisle 5 <ALB(S) Aux Live Bracing-Reaction, Left, Aisle 5 WALB>(S) Wind, Aux Live Bracing Reaction, Right, Aisle 5 <WALB(S) Wind, Aux Live Bracing Reaction, Left, Aisle 5 WALB Wind, Aux Live Bracing Reaction AD Auxiliary Dead Load uo User Defined Load Ul User Defined Load ~ I U2 User Defined Load ~ 2 U3 User Defined Load • 3 U4 User Defined Load ~ 4 us User Defined Load -5 U6 User Defined Load -6 U7 User Defined Load-7 U8 User Defined Load - 8 U9 User Defined Load -9 UB User Brace Reaction UBI User Brace Reaction -I UB2 User Brace Reaction-2 UB3 User Brace Reaction -3 UB4 User Brace Reaction-4 UBS User Brace Reaction -5 UB6 User Brace Reaction - 6 UB7 User Brace Reaction-7 UB8 User Brace Reaction - 8 UB9 User Brace Reaction -9 R Rain Load T Temperature Load v Shear File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.Ja 0 Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: 1:57:43 PM Page: II of 175 y 15'-0: I S~i$ ! 1fi'.0~ File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.\a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 12 of 175 User Defined Frame Point Loads for Cross Section: 2 Ma I Loci Offset H or Y Su Dir. Coef. Loc. -0.30 16/7/3 J/3/0 Hoci,. N DOWN 1.000 IF y X File: 7079 Chevron Rl_Stress Check !0_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy User Defined F a ne Point Loads for Cros S ct'oll' 3 ' ' s ' ' Side Units Type Description Magi Locl Offset HorV Supp. I k CG PS-41 Pipe Loads -1.70 20/8/6 -2/3/0 Horiz. N I k CG PS-46 Pipe Loads -0.30 1617/3 3/3/0 Horiz. N y X File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 13 of 175 Dir. Coef. Loc. DOWN 1.000 OF DOWN 1.000 IF 07-27053 Calculations Hazardous Materials Occupancy User Defined Frame Point Loads for Cross Section· 4 Side Units Type Description Magi Loc! Offset H orV S"PP· I k CG S-41 Pipe Loads ·1.70 20/8/6 -2/3/0 Horiz. N I k CG PS-46 Pipe Loads ·0.30 I6/7/3 3/3/0 Horiz. N y X File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 14 of 175 Dir. Coef. Loc. DOWN !.000 OF DOWN !.000 IF 07-27053 Calculations Hazardous Materials Occupancy User DeOned Frame Point Loads for Cross Section-5 Side Units Type Desc1ip_!ion Ma£1 Locl Offset H orV Supp, 1 k CG PS~41 Pipe Loads -1.70 20/8/6 -2/3/0 Horiz. N 1 k CG PS-46 Pipe Loads -0.30 1617/3 3/3/0 Horiz. N 1 k CG Lube Tanks -1.50 10/0/0 NA NA N 1 k CG Lube Tanks -1.50 10/0/0 1/0/0 Horiz. N y X File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.!a Date: 10/20/2008 Time: I :57:43 PM Page: 15 of 175 Dir. Coef. Loc. DOWN 1.000 OF DOWN 1.000 1F DOWN 1.000 CL DOWN 1.000 IF 07-27053 Calculations Hazardous Materials Occupancy User Defined Frame Point Loads for Cross Section· 6 Side Units Type Description Magi Loci Offset H orV Supp. I k CG PS~4l Pipe Loads -1.70 2018/6 -21310 Horiz. N I k CG PS-46 Pipe Loads -0.30 161713 31310 Horiz. N I k CG Lube Tanks -1.50 101010 NA NA N I k CG Lube Tanks -1.50 101010 11010 Horiz. N y X File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 16ofl75 Dir. Coef. Loc. DOWN 1.000 OF DOWN 1.000 IF DOWN 1.000 CL DOWN 1.000 IF 07-27053 Calculations Hazardous Materials Occupancy User Defined Frame Point Loads for Cros Sccfon· 7 . s ' Side Units Type Description Magi Loci Offset HorV Supp. l k CG PS-41 Pipe Loads -1.70 20/8/6 -21310 Horiz. N l k CG PS-46 Pipe Loads -0.30 161713 313/0 Horiz. N ® 3 y X File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 17 of 175 Dir. Coef. Loc. DOWN 1.000 OF DOWN 1.000 IF 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 18of175 User Defined Frame Point Loads for Cross Section: 8 LocI Offset H or V Su Dir. Coef. LoC. 20/8/6 -2/3/0 Horiz. N DOWN 1.000 OF y X File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: I 9 of I 75 User Defined Frame Point Loads for Cross Section: 9 Side Units T e Descri tion Ma 1 LocI Offset H or V Su Dir. Coer. Loc. 1 k CG PS-41 Pi e Loads -1.70 20/8/6 -2/3/0 Horiz. N DOWN 1.000 OF y X File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Version: 7.1 a 07-27053 Calculations Hazardous Materials Occupancy User Defined Frame Point Loads for Cross Secticm· 10 Side Units Type Description Magi Loci Offset H orV Supp. I k CG PS-41 Pipe Loads -1.70 20/8/6 -213/0 Horiz. N 2000 k CG PS-42 Pipe Loads -2.20 20/8/6 -2/3/0 Horiz. N 2001 k CG PS42 Pioe Loads -2.20 20/8/6 -2/3/0 Hmiz. N y I 15'D I ms: I '"'-"" File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.·1a Date: 10/20/2008 Time: I :57:43 PM Page: 20 of 175 Dir. Coet: Loc. DOWN 1.000 OF DOWN 1.000 OF DOWN 1.000 OF @ Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: 1:57:43 PM Page: 21 of l75 18'-6" ?Q'.QH 18'.6" 20'.0" 18'-6" ?Q'.O" l 9'-3" I ~ 4 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 22 of 175 Shape: base Builder Contact: Larry Reeves Name: Alta Construction, Inc. Address: 17 Smith Fork Way City, State Zip: Lyman, Wyoming 82937 Country: United States Loads and Codes ~Shape: base Project: Chevron Builder PO#: Jobsite: near DeBeque CO City, State Zip: Rifle, Colorado 81650 County, Country: Gaffield, United States City: Rifle County: Garfield State: Colorado 89AISC 04AISI Country: United States Rainfall: 4.00 inches per hour Building Code: 2003 Intemational Building Code Built Up: Building Use: Hazardous I Special Occuparicy Cold Fonn: Live Load Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf Live Load: 20.00 psf Not Reducible Wind Load Wind Speed: 90.00 mph Snow Load Roof Snow Load: 75.00 psf Design Snow (Sloped): 75.00 psf Seismic Load Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: 1.023 Snow Exposure Category (Factor): 2 Partially Exposed (1.00) Mapped Spectral Response-Ss:43.60 %g Mapped Spectral Response-Sl :9.10 %g Seismic Hazard I Use Group: Group 2 Wind Enclosure: Enclosed Wind Importance Factor: 1.150 Topographic Factor: 1.0000 NOT Windbome Debris Region Base Elevation: 0/0/0 Primary Zone Strip Width: 10/7/3 Parts I Portions Zone·Strip Width: 5/3110 Basic Wind Pressure: 20.74 psf Snow Importance: 1.1.00 Thennal Category (Factor): Heated ( 1.00) Ground/RoofConversion: 0.70 %Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Unobstructed, Slippery Roof Seismic Importance: 1.250 Seismic Performance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Biacing Seismic Period: 0.2691 Framing R-Factor: 3.0000 Bracing R-Factor: 3.0000 Soil Profile Type: Stiff soil (D, 4) Frame Redundancy Factor: 1.0000 Brace Redundancy Factor: 1.0000 Frame Seismic Factor {Cs): 0.1354 x W Brace Seismic FactOr (Cs): 0.1758 x W Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Bul1der has called the local Building Official or Project Engineer to obtain all code and loading information for this specific building site. Load Type Descriptions D Material Dead Weight CG Collateral LQad for Gravity Cases L Live Load "ASL Alternate Span Live Load, Shifted Left L> Live ·Notional Right S Snow Load *US I Unbalanced Snow Load l, Shifted Left *US2 Unbalanced Snow Load 2, Shifted Left SS Sliding Snow Load PF 1 Partial Load, Full, 1 Span PF2 Partial Load, Full, 2 Spans S> Snow ·Notional Right MRS MinfmumRoofSnow <MRS Minimum Roof Snow· Notional Left WI> W2> W3> W4> WS> W6> WP WPL WPA2 WPB2 Wind Load, Case 1, Right Wind Load, Case 2, Right Wind Load, Case 3, Right Wind Load, Case 4, Right Wind Load, Case 5, Right Wind Load, Case 6, Right Wind Load, Parallel to Ridge Wind load, !I Ridge, Left Wind Parallel ·Ref A, Case 2 Wind Parallel· Ref B. Case 2 c cu ASL" PL2 <L US!* US2"' SD RS PHI PH2 <S M~S> w <WI <W2 <W3 <W4 <W5 <W6 WPR WPAI WPBI WPCJ File: 7079 Chevron R !_Stress Check I 0_2008 with 08_2008 Loading Collateral Load Collateral Load for Wind Cases Alternate Span Live Load, Shifted Right Partial Live, Full, 2 Spans Live .• Notional Left Unbalanced Snow Load 1, Shifted Right Unbalanced Snow Load 2, Shifted Right Snow Drift Load Rain Surcharge Load Partial Load, Half, 1 Span Partial Load, Half, 2 Spans Snow · Notional Left Minimum Roof SnoW-Notional Right Wind Load Wind Load, Case l, Left Wind Load, Case 2, Left Wind Load, Case 3, Left Wind Load, Case 4, Left Wind Load, Case 5, Left Wind Load, Case 6, Left Wind Load, II Ridge, Right Wind Parallel -Ref A, Case 1 Wind Parallel· RefB, Case I Wind Parallel-RefC, Case 1 Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 23 of 175 WPC2 Wind Parallel-RefC, Case 2 WPDI Wind Parallel-RefD, Case I WPD2 Wind Parallel-RefD, Case 2 WBI> Wind Brace Reaction, Case I, Right <WBI Wind Brace Reaction, Case I, Left WB2> Wind Brace Reaction, Case 2, Right <WB2 Wind Brace Reaction, Case 2, Left WB3> Wind Brace Reaction, Case 3, Right <WB3 Wind Brace Reaction, Case 3, Left WB4> Wind Brace Reaction, Case 4, Right <WB4 Wind Brace Reaction, Case 4, Left WBS> Wind Brace Reaction, Case 5, Right <WB5 Wind Brace Reaction, Case 5, Left WB6> Wind Brace Reaction, Case 6, Right <WB6 Wind Brace Reaction, Case 6, Left MW Minimum Wind Load MWB Minimum Wind Bracing Reaction E Seismic Load E> Seismic Load, Right <E Seismic Load, Left EG Vertical Seismic Effect EG+ Vertical Seismic Effect, Additive EG-Vertical Seismic Effect, Subtractive EB> Seismic Brace Reaction, Right <EB Seismic Brace Reaction, Left FL Floor Live Load FL' Alternate Span Floor Live Load, Shifted Right 'FL Alternate Span Floor Live Load, Shifted Left FD Floor Dead Load AL Auxiliary Live Load AL*> Auxiliary Live Load, Right, Right *AL> Auxiliary Live Load, Right, Left <AL* Auxiliary Live Load, Left, Right <*AL Auxiliary Live Load, Left, Left AL' Aux Live, Right 'AL Aux Live, Left AL'>(l) Auxiliary Live Load, Right, Right, Aisle I 'AL>(l) Auxiliary Live Load, Right, Left, Aisle I <AL'(l) Auxiliary Live Load, Left, Right, Aisle l <*AL(!) Auxiliary Live Load, Left, Left, Aisle 1 AL*(!) Aux Live, Right, Aisle l 'AL(l) Aux Live, Left, Aisle l AL'>(2) Auxiliary Live Load, Right, Right, Aisle 2 'AL>(2) Auxiliary Live Load, Right, Left, Aisle 2 <AL*(2) Auxiliary Live Load, Left, Right, Aisle 2 <*AL(2) Auxiliary Live Load, Left, Left, Aisle 2 AL*(2) Aux Live, Right, Aisle 2 *AL(2) Aux Live, Left, Aisle 2 AL*>(3) Auxiliary Live Load, Right, Right, Aisle 3 'Al>(3) AUxiliary Live Load, Right, Left, Aisle 3 <AL*(3) Auxiliary Live Load, Left, Right, Aisle 3 <'AL(3) Auxiliary Live Load, Left, Left, Aisle 3 AL'(3) Aux Live, Right, Aisle 3 'AL(3) Aux. Live, Left, Aisle 3 AL'>(4) Auxiliary Live Load, Right, Right, Aisle 4 *AI>(4) Auxiliary Live Load, Right, Left, Aisle 4 <AL*(4) Auxiliary Live Load, Left, Right, Aisle 4 <'AL(4) Auxiliary Live Load, Left. Left, Aisle 4 AL*(4) Aux Live, Right, Aisle 4 *AL(4) Aux Live, Left, Aisle 4 AL'>(S) Auxiliary Live Load, Right, Right, Aisle 5 *Al>(S) Auxiliary Live Load, Right, Left, Aisle 5 <AL*(S) Auxiliary Live Load, Left, Right, Aisle 5 <'AL(S) Auxiliary Live Load, Left, Left, Aisle 5 AL'(S) Aux Live, Right, Aisle 5 'AL(S) Aux Live, Left, Aisle 5 ALB Aux Live Bracing Rea_ction ALB> Aux Live Bracing Reaction, Right <ALB Aux Live Bracing Reaction, Left WALB> Wind, Aux Live Bracing Reaction, Right <WALB Wind, Aux Live Bracing Reaction, Left ALB>( I) Aux Live Bracing Reaction, Right, Aisle 1 <ALB(!) Aux Live Bracing Reaction, Left, Aisle 1 WALB>(l) Wind, Aux Live Bracing Reaction, Right, Aisle 1 <wALB(l) Wind, Aux Live Bracing Reaction, Left, Aisle 1 ALB>(2) Aux. Live Bracing Reaction, Right, Aisle 2 <ALB(2) Aux Live Bracing Reaction, Left, Aisle 2 WALB>(2) Wind, Aux Live Bracing Reaction, Right, Aisle 2 <WALB(2) Wind, Aux Live Bracing Reaction, Left, Aisle 2 ALB>(3) Aux Live Bracing Reaction, Right, Aisle 3 <ALB(3) Aux Live Bracing Reaction, Left, Aisle 3 WALB>(3) Wind, Aux Live Bracing Reaction, Right, Aisle 3 <wALB(3) Wind, Aux Live Bnicing Reaction, Left, Aisle 3 ALB>(4) Aux Live Bracing Reaction, Right, Aisle 4 <ALB(4) Aux Live Bracing Reaction, Left, Aisle 4 WALB>(4) Wind, Aux Live Bracing Reaction, Right, Aisle 4 <WALB(4) Wind, Aux Live Bracing Reaction, Left, Aisle 4 ALB>(S) Aux Live Bracing Reaction, Right, Aisle 5 <ALB(S) Aux Live Bracing Reaction, Left; Aisle 5 WALB>(S) Wind, Aux. Live Bracing Reaction, Right, Aisle 5 <WALB(S) Wind, Aux. Live Bracing Reaction, Left, Aisle 5 WALB Wind, Aux Live Bracing Reaction AD Auxiliary Dead Load uo User Defined Load Ul User Defined Load - l U2 User Defined Load - 2 U3 User Defined Load - 3 U4 User Defined Load -4 us User Defined Load - 5 U6 User Defined Load -6 U7 User Defined Load -7 U8 User Defined Load - 8 U9 User Defined Load - 9 UB User Brace Reaction UBI User Brace Reaction -I UB2 User Brace Reaction-2 UB3 User Brace Reaction -3 UB4 User Brace Reaction-4 UBS User Brace Reaction -5 UB6 User Brace Reaction -6 UB7 User Brace Reacti-on -7 UB8 User Brace Reaction -8 UB9 User Brace Reaction -9 R Rain Load T Temperature Load v Shear File: 7079 Chevron Rl __ Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 24 of 175 0 liB 'ld' D vera Ul In!! escnpt10n Shape Overall Overall Floor Area Wall Area Roof Area Max:. Eave Min. Eave Max. Roof Min. Roof Peak Width Length (SQ. ft.) (sq. ft.) (sq ft.) Heioht Hei~ht 2 Pitch Pitch Hei<>ht base 53/0/0 154/0/0 8!62 13716 8604 32/0/0 32/0/0 4.000:12 4.000:12 401!0/0 Overall Sha e Descrl tion Roof 1 Roof 2 From Grid To Grid Width Lenoth Eave Ht. Eave Ht. 2 Pitch Pitch 2 Dist. to Rid e Peak Heioht A B !·A 1-D 53/0/0 154/0/0 32/0/0 32/0/0 4.000:!2 4.000:12 26/6/0 401!0/0 1 9' 3" 1 ?D'.N 18'-6" 20'.N ?0',0" 18'.6" ?O•.N I 9'-3" I © @ . ro . 4 '· . File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 25 of 175 Wall: 4, Frame at: 0/6/0 D L C esign oad ombinat10ns ~ Framin No. Origin Factor Application DescriP-t-ion I System 1.000 1.0 D+ 1.0 AD+ I.OCG + l.O S D+AD+CG+S 2 System 1.000 1.0 D + l.O AD+ 1.0 CO+ 1.0 US!* D+AD+CG+USI* 3 System 1.000 l.OD + 1.0 AD+ 1.0 CG+ l.O *US\ D +AD+ CG + *USI 4 System 1.000 1.0 D + 1.0 AD+ \.0 CG + 1.0 Wl> D +AD+ CG +WI> 5 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <WI D+AD+CG+<Wi 6 System 1.000 !.0 D + 1.0 AD + 1.0 CG + 1.0 W2> D +AD+ CG + W2> 7 . System 1.000 LOD+ LOAD+ i.OCG+ l.O<W2 D+AD+CG+<W2 8 System 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.750 S + 0.750 WI> P +AD+ CG + S +WI> 9 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <WI D+ AD+CG+S +<WI 10 System 1.000 1.0 D + l.O AD+ 1.0 CG +0.750 S + 0.750 W2> D+AD+CG+S+W2> II System 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System 1.000 1.0 D + l.O AD+ 1.0 CG + 1.0 *AL> D+AD+CG+*AL> 13 System 1.000 1.0 D + 1.0 AD+ t.OCG + 1.0 AL*> D+AD+CG+AL*> 14 System !.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <*AL D +AD+ CG+<*AL IS System !.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <AL* D+ AD+CG+<AL* 16 System !.000 \).600 D+ 0.600 AD +0.600 CU + 1.0 WI> io+AD+CU+Wl> 17 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<Wl 18 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 W2> D+AD+CU+W2> 19 System !.000 0.600 D + 0.600 AD+ 0.600 CU + !.0 <W2 io+AD+CU+<W2 20 System 1.000 !.0 D + 1.0 AD+ 1.0 CO +0.563 S +0.750 'AL> D+AD+CG+S+*AL> 21 System !.000 1.0 D + 1.0 AD+ l.O CG +0.563 S + 0.750 AL*> D+AD+CG+S+AL*> 22 System !.000 1.0 D+ 1.0 AD+ 1.0 CG +0.563 S +0.750 <'*'AL P+ AD+CG+S+<*AL 23 System !.000 1.0 D + !.0 AD+ 1.0 CO +0.563 S +0.750 <AL' D+AD+CG+S+<AL* 24 System 1.000 1.0 D + 1.0 AD+ !.0 CO +0.375 WI> +0.750 'AL> D+AD+CG+WI>t*AI> 25 System 1.000 l.O D + 1.0 AD+ 1.0 CG +0.375 WI> +'0.750 AL*> D+AD+CG+Wl>tAL*> 26 System 1.000 1.0 D + l.OAD + 1.0 CG +0.375 <Wl +0.750<*AL D+ AD+CG+<Wt+<*AL 27 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 <WI+ 0.750 <AL * D+AD+CG+<Wt+<AL* 28 System !.000 l.O D+ 1.0 AD+ 1.0 CG +0.375,W2>+0.750 *AL> D +AD+ CG + W2>t*AL> 29 '. System 1.000 1.0 D + 1.0 AD+ !.0 CO +0.375 W2>+0.750 AL*> D+ AD+CG+W2>+AL*> 30 System !.000 1.0 D + 1.0 AD+ l.O CG +0.375 <W2 +0.750<*AL D+ AD+CG+<W2+<*AL 31 System !.000 1.0 D + l.O'AD + 1.0 CG+0.375 <W2 +0.750<AL"' D +AD+ CG+<W2+<AL"' 32 System !.000 1.0 D + 1.0 AD+ 1.0 CO +0.150 S +0.750 E>+0.700 EG+ D+AD+CG+S+E>tEG+ 33 System 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.150 S +0.750 <E+ 0.700 Ei;+ D+AD+CO+S+<E+EG+ 34 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 E> + 0.700 EO-D+AD+CU+E>+EO- 35 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 <E + 0.700 EO-D+AD+CU+<E+EG~ 36 System Derived 1.000 1.00 + 1.0 AD+ 1.0 CO +0.150 S + 0.750 EB> +0.700 EG+ D+AD+CO+S+EB>+EO+ 37 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0.700 EO-D+AD+CU+EB>+EG~ 38 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.150 S +0.750 <EB +0.700 EG+ D+AD+CO+S+<EB+EG+ 39 System Derived !.000 .600 D + 0.600 AD + 0.600 CU + 0. 700<EB + 0. 700 EO-D+AD+CU+<EB+EG~ 40 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CO+ 1.0 WPAI D+AD+CO+WPA1 41 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S +0.750 WPAI D+AD.+CG+S+WPAI 42 System Derived !.000 .600 D + 0.600 AD +0.600 CU + 1.0 WPAI D+AD+CU+WPAJ 43 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.375 WPAl +0.750 *AL+0.750 ALB> D+AD+CG+WPAI+*AL+ALB> 44 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPAl +0.750 AL* +0.750 ALB> D+AD+CG+WPAI+AL*+ALB> 45 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 WPD1 D +AD+ CG + WPDI 46 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.750 S + 0.750 WPDI D+AD+CG+S+WPDl 47 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPDI D +AD+ CU + WPDI 48 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPDl + 0.750 *AL +0.750 <ALB D+AD+CG+WPD J+* AL +<ALB 49 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDl + 0.750 AL* + 0.750 <ALB D+AD+CG+WPDI+AL *+<ALB 50 System Derived 1.000 1.0 D+ l.OAD+ 1.0 CG + 1.0 WPA2 D +AD+ CG+WPA2 51 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 WPA2 D+AD+CG+S+WPA2 52 System Derived 1.000 0.600 D + 0.600 AD +0.600 CU + 1.0 WPA2 D+AD+CU+WPA2 53 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 +0.750 *AL +0.750 ALB> D+AD+CG+WPA2+*AL+ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 + 0.750 AL* +0.750 ALB> D+AD+CG+WPA2+AL*+ALB> 55 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO + 1.0 WPD2 D+AD+CG+WPD2 56 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPD2 D+AD+CG+S+WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D + AD+CU+ WPD2 58 System Derived 1.000 1.0 D + l.O AD+ LO CG +'0.375 WPD2 + 0.750 *AL +0.750 <ALB D+AD+CG+WPD2+*AL+<ALB 59 System Derived 1000 1.0 D + J.O AD+ 1.0 CO +0.375 WPD2 +0.750 AL* + 0.750 <ALB D+AD+CG+WPD2+AL *+<ALB 60 System Derived 1000 1.0 D + J.O AD+ 1.0 CO+ 1.0 WPBl D+AD+CO+WPBI 61 System Derived 1.000 1.0 D + 1.0 AD+ !.0 CG + 0.750 S + 0.750 WPB! D+ AD +CO +S + WPBI 62 System Derived !.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB I D + AO+CU + WPBI 63 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB I + 0.750 *AL + 0.750 ALB> D+AD+CG+WPB l+*AL +ALB> File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 26 of !75 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPB 1 + 0. 750 AL* + 0.750 ALB> D+AD+CG+WPB 1 +AL *+ALB> 65 System Detived 1.000 1.0 D+ 1.0 AD+ 1.0 CG+ 1.0 WPC1 D+AD+CG+WPC! 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.750 S + 0.750 WPCI D+AD+CG +S + WPCI 67 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC1 D+AD+CU+WPC1 68 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPCI + 0.750 *AL + 0.750 <ALB D+AD+CG+WPCJ+*AL+<ALB 69 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CO +0.375 WPCl +0.750 AL* + 0.750 <ALB D+AD+CG+WPCJ+AL *+<ALB 70 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPB2 D+AD+CG+WPB2 71 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPB2 D+AD+CG+S+WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 D+AD+CU+WPB2 73 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 +0.750 *AL +0.750 ALB> D+AD+CG+WPB2+*AL+ALB> 74 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 + 0.750 AL * + 0.750 ALB> D+AD+CG+WPB2+AL *+ALB> 75 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPC2 D+AD+CG+WPC2 76 System Delived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC2 D+AD+CG+S+WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 D+AD+CU+WPC2 78 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPC2 +0.750 'AL +0.750 <ALB D+AD+CG+WPC2+*AL+<ALB 79 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.375 WPC2 +0.750 AL* + 0.750 <ALB D+AD+CG+WPC2+AL *+<ALB 80 System Derived 1.000 1.0 D + 1.0 AD+ LO CG + l.O S + 1.0 ALB> ~+AD+ CG + S+ALB> 81 System Derived 1.000 LOD+ LOAD+ l.OCO+ LO*AL+ l.OALB> D+AD:t-CO+*AL+ALB> 82 System Derived 1.000 LO D +LOAD+ 1.0 CO+ 1.0 AL*+ 1.0 ALB> !D+ AD+ CG+AL*+ALB> 83 System Derived 1.000 1.0 D + l.O AD+ 1.0 CO+ 0.563 S +0.750 *AL+0.750 ALB> D+AD+CO+S+*AL+ALB> 84 System Derived 1.000 l.O D+ 1.0 AD+ 1.0 CO +0.5.63 S +0.750 AL* + 0.750 ALB> io+AD+CG+S+AL*+ALB> 85 System Derived 1.000 1.0D+ 1.0 AD+ t.OCO +!.OS+ I.O<ALB D + AD +CO + S+<ALB 86 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 *AL + l.O <ALB D +AD+ CG+* AL +<ALB 87 System Derived 1.000 l.OD+ l.OAD+ l.OCG+ 1.0 AL*+ l.O<ALB p +AD+ CG+AL *+<ALB 88 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 *AL +0.750 <ALB fo+AD+CG+S+* AL +<ALB 89 ~Y!>tem Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 AL* +0.750<ALB D_j-AD+CG+S+AL '+<ALB File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la ( ., 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 27 of 175 Wall: 4, Frame at: 0/6/0 Frame ID:Rigid Frame with Endposts y Values shown are resisting forces of the foundation. Reactions-Unfactored Load Tvne at Frame Cross Section: 1 Type Exterior Column X-Loc 01010 Grid I -Grid2 1-D Base Plate W x L (in.) 9 X 13 Base Plate Thickness (in.) 0.500 Anchor Rod Qty/Diam. (in.) 4-1.000 Column Base Elev. 100'-0" Load Tvoe Desc. Hx Hz Vv D Frm 0.9 -4.6 AD Frm 0.1 -1.2 CG Frm 2.7 -10.6 0 s Frm 10.2 -39.7 USl"' Frm 9.1 -23.6 *USl Frm 9.1 -48.0 WI> Frm -7.2 --12.4 <WI Frm 4.7 --4.4 W2> Frm -8.6 -8.4 <W2 Frm 3.3 --0.5 'AL> Frm -0.0 -7.7 AL*> Frm -0.0 -2.1 <*AL Frm 1.4 -9.3 <AL' Frm 1.4 -3.6 cu Frm 1.4 5.3 E> Frm -3.9 --5.4 EG+ Fnn 0.4 -1.4 <E Frm 3.9 -5.4 EG-Frm -0.4 ·1.4 EB> Brc - <EB Brc -0.0 - WPAI Bee 1.9 ·9.6 'AL Frm 0.7 -8.5 ALB> Bee - AL' Fm1 0.7 2.9 WPDI Bee 2.5 -·7.3 <ALB Bee WPA2 Bee 0.4 ·5.6 WPD2 Brc 1.0 ·3.3 WPBI Brc 1.9 ·9.6 WPCI Brc 2.5 ·7.3 WP82 Bee 0.4 ·5.6 Frame Type:Rigid Frame, End Posts Vy Vy Vy Interior Column Interior O.>lumn Exterior Column 15/0/0 38/0/0 53/0/0 1-C 1-B 1-A 8x 16 Sx 16 9x 13 0.375 0.375 0.500 4-0.750 4-0.750 4-1.000 100'-0" 100'-0" 100'-0" Hx Hz Vy Hx Hz Vv-Hx Hz v¥ - -0.8 - -0.8 -0.9 -4.7 - - - - ---0.1 -1.2 --0.0 0.3 --0.0 0.3 -2.7 -10.6 - - - - ---10.2 -39.8 -------9.1 -48.0 - -- - - --9.1 -23.6 7.1 - -7.1 --4.8 --4.4 --6.4 - --6.4 7.3 --12.4 - - - ---3.4 --0.5 - - --. 8.7 --8.4 - - - ---1.4 -3.6 - - ---1.4 -9.3 - --0.0 -2.1 - - - - --0.0 7.7 ---1.4 -5.3 -0.1 -0.1 -4.0 -5.4 --0.0 -0.0 -0.4 -1.4 --0.1 -0.1 -4.0 -5.4 -·0.0 ·0.0 0.4 --1.4 - --- - - --0.0 - ---1.9 ·9.6 - - - --0.7 -2.9 --- - ---0.7 8.5 -- ---2.5 --7.3 -- - --0.4 -5.6 . 1.0 -3.3 -1.9 . -9.6 ---2.5 -7.3 -. ---0.4 -5.6 File: 7079 Chevron R I_ Stress Check I 0 _ 2008 with 08 _ 2008 Loading Version: 7.la - - - - - ---- - - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 28 of 175 L_ WPC2 Brc 1.o I I -3.3 I I · I I -l.o I F rame R r eac 1ons ~ F t dL dC ac ore oa ases a tF rame c s r ross ec 10n: XwLOC 01010 15/0/0 38/0/0 53/0/0 Grid I -Grid2 1-D 1-C 1-B 1-A Ld Description Hx Hz Vy Hx Hz Vv Hx Hz v Hx Hz Vv Cs (application factor not shown (k) (k) k) (k (k) (k) (k) k) k k (k (k 1 D+AD+CG+S 13.9 . 56.1 . ·0.0 1.0 . -0.0 1.0 -13.9 . 56.3 2 D +AD+ CG +US!* 12.9 39.9 . ·0.0 1.0 -0.0 1.0 -12.9 . 64.5 . 3 D+AD+CG+*USl 12.9 64.4 . ·0.0 1.0 -0.0 1.0 -12.9 . 40.1 . 4 D+AD+CG+W!> -3.4 4.0 7.1 1.0 . 7.1 1.0 -8.6 . 12.1 . 5 D+AD+CG+<Wl 8.5 . 11.9 ·6.4 1.0 . -6.4 1.0 3.5 . 4.1 6 D+AD,+CG+W2> -4.9 . 7.9 . -0.0 1.0 -0.0 1.0 -7.1 16.1 . 7 D+AD+CG+<W2 7.0 . 15.9 . ·0.0 1.0 -0.0 1.0 4.9 . 8.1 . 8 D+AD+CG+S+Wl> 6.0 . 36.9 5.3 1.0 . 5.3 1.0 -15.0 . 43.0 . 9 D+AD+CG+S+<Wl 14.9 . 42.9 -4.8 1.0 . -4.8 1.0 -5.9 . 37.0 . 10 D+AD+CG+S+W2> 4.9 . 39.9 -0.0 1.0 . -0.0 1.0 -13.9 . 46.0 11 D+AD+CG+S+<W2 13.8 . 45.8 . -0.0 1.0 . -0.0 1.0 -4.8 . 40.0 12 D+AD+CG+*AL> 3.7 . 24.1 . -0.0 1.0 -0.0 1.0 -5.2 . 20.2 . 13 D+AD+CG+AL*> 3.7 . 18.5 . -o.o 1.0 . -0.0 1.0 -52 . 25.8 . 14 D +AD +CG+<*AL 5.2 . 25.6 -0.0 1.0 . -0.0 1.0 -3.7 . 18.6 . 15 D+AD+CG+<AL* 5.2 . 20.0 . -0.0 1.0 . -0.0 1.0 -3.7 . 24.3 16 D+AD+CU+W!> -5.7 . -5.8 . 7.1 0.5 . 7.1 0.5 -6.2 . 2.3 17 D+AD+CU+<Wl 6.2 . 2.2 . -6.4 0.5 -6.4 0.5 5.8 . -5.7 18 D+AD+CU+W2> -7.2 . -1.8 . . 0.5 . . 0.5 -4.8 . 16.3 . 19 D+AD+CU+<W2 4.7 . 6.2 . . 0.5 . . 0.5 7.3 . -1.7 . 20 D+AD+CG+S+*AL> 9.4 . 44.5 . -0.0 1.0 . -0.0 1.0 -10.5 . 41.6 . 21 D+AD+CG+S+AL*> 9.4 . 40.3 . -0.0 1.0 . -0.0 1.0 -10.5 . 45.8 . 22 D+AD+CG+S+<*AL 10.5 . 45.7 . -0.0 1.0 . -0.0 1.0 -9.4 . 40.5 23 D+AD+CG+S+<AL* 10.5 . 41.5 . .(),0 1.0 . -0.0 1.0 -9.4 . 44.7 . 24 D+AD+CG+Wl>+*AL> 1.0 0. 17.5 . 2.7 1.0 . 2.7 1.0 -6.6 . 17.6 . 25 D+AD+CG+Wl>+AL*> 1.0 . 13.3 2.7 1.0 . 2.7 1.0 -6.6 . 21.8 26 D+AD+CG+<Wl+<"'AL 6.6 . 21.7 ·2.4 1.0 . -2.4 1.0 -1.0 . 13.5 . 27 D+AD+CG+<Wl+<AL* 6.6 . 17.4 . ·2.4 1.0 . -2.4 1.0 -1.0 . 17.7 28 D +AD+ CG + W2>+* AL> 0.5 . 19.0 . -o.o 1.0 . -0.0 1.0 -6.1 . 19.1 . 29 D+AD+CG+W2>+AL*> o.s . 14.8 . -o.o 1.0 . -o.o 1.0 -6.1 . 23.3 . 30 D+AD+CG+<W2+<*AL 6.0 . 23.1 . -0.0 1.0 . -0.0 1.0 -0.5 . 14.9 . 31 D+AD+CG+<W2+<AL* 6.0 . 18.9 . -o.o 1.0 . -0.0 1.0 -0.5 . 19.2 32 D+AD+CG+S+E>+EG+ 2.6 . 19.2 . 0.1 1.1 . 0.1 1.1 -8.6 . 27.5 . 3J D+AD+CG+S+<E+EG+ 8.5 . 27.4 . .(), 1 1.1 . -0.1 1.1 -2.5 19.4 . 34 D+AD+CU+E>+EG--1.6 . 1.9 . 0.1 0.5 . 0.1 0.5 -4.0 . 9.6 . 35 D+AD+CU+<E+EG-3.9 . 9.5 -0.1 0.5 . -0.1 0.5 1.6 . 1.9 . 36 D+AD+CG+S+EB>+EG+ s.s . 23.3 -0.0 1.1 . -0.0 1.1 -5.5 . 23.5 . 37 D+AD+CU+EB>+EGM 1.2 . 5.7 . 0.5 . . 0.5 -1.2 . 5.7 38 D+AD+CG+S+<EB+EG+ s.s 0.0 23.3 . ·0.0 1.1 -0.0 1.1 -5.5 0.0 23.5 39 D+AD+CU+<EB+EG-1.2 0.0 5.7 . . 0.5 . 0.5 -1.2 0.0 5.7 40 D +AD+ CG + WPAI 5.6 . 6.8 . ·0.0 1.0 -0.0 1.0 -5.6 . 6.9 41 D+AD+CG+S+WPAI 12.8 . 39.0 -0.0 1.0 . -0.0 1.0 -12.8 . 39.1 42 D+AD+CU+WPAI 3.3 -2.9 . . 0.5 . 0.5 -3.3 . -2.8 43 D+AD+CG+WPAI+*AL+ALB> s.o . 19.2 . ·0.0 1.0 . -0.0 1.0 -5.0 . 15.1 44 D+AD+CG+WPAI+AL"'+ALB> s.o 14.9 ·0.0 1.0 -0.0 1.0 -5.0 . 19.3 45 D+AD+CG+WPDI 6.2 9.1 -0.0 1.0 -0.0 !.0 -6.2 . 9.3 46 D+AD+CG+S+WPDI 13.2 . 40.7 ·0.0 1.0 -0.0 1.0 -13.2 . 40.9 47 D+AD+CU+WPDl 3.9 . -0.6 . . 0.5 . 0.5 -3.9 . -0.5 48 D+AD+CG+WPD I+* AL +<ALB 5.2 . 20.0 ·0.0 1.0 -0.0 1.0 -5.2 16.0 . 49 D+AD+CG+WPDI+AL*+<ALB 5.2 15.8 ·0.0 1.0 . -0.0 1.0 -5.2 20.2 so D +AD+ CO+ WPA2 4.2 10.8 ·0.0 1.0 -0.0 1.0 -4.2 . 10.9 51 D+AD+CG+S+WPA2 11.7 . 42.0 ·0.0 1.0 -0.0 1.0 -11.7 42.1 52 D+AD+CU+WPA2 1.9 1.0 . 0.5 0.5 -1.9 . 1.1 53 D+AD--l-cG+WPA2+*AL+ALB> 4.4 . 20.6 -0.0 !.0 -0.0 1.0 -4.4 16.6 54 D+AD+CG+WPA2+AL *+ALB> 4.4 16.4 -0.0 1.0 -0.0 1.0 -4.4 20.8 55 D+ AD +CG + WPD2 4.8 . 13.1 -0.0 !.0 -0.0 1.0 -4.8 13.2 56 D +AD+ CG +S + WPD2 !2.1 43.7 -0.0 1.0 -0.0 !.0 -12.1 43.9 57 D+AD+CU+WPD2 2.4 3.3 . 0.5 0.5 -2.4 . 3.4 58 D+AD+CG+WPDZ+*AL+<ALB 4.7 . 21.5 -0.0 1.0 -0.0 1.0 -4.7 17.4 File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Version: 7. ta 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 29 of 175 59 D+AD+CG+WPD2+AL ~~<+<ALB 4.7 17.3 -0.0 1.0 -0.0 1.0 -4.7 21.7 - 60 D+AD+CG+WPBl 5.6 6.8 -0.0 1.0 -0.0 1.0 -5.6 6.9 - 6\ D+AD+CG+S+WPB! \2.8 -39.0 -0.0 1.0 -0.0 1.0 -12.8 -39.1 - 62 D+AD+CO+WPI31 3.3 -2.9 0.5 0.5 -3.3 -2.8 63 D+AD+CG+WPBI+* AL+ALB> 5.0 19.2 -0.0 1.0 -0.0 1.0 -5.0 15.1 64 D+AD+CG+WPB l+AL *+ALB> 5.0 -14.9 --0.0 1.0 -0.0 1.0 -5.0 -19.3 - 65 D+AD+-CG+WPCI 6.2 -9.1 -0.0 1.0 -0.0 1.0 -6.2 9.3 66 D +AD+ CO+ S + WPCI 13.2 40.7 -0.0 1.0 --0.0 1.0 -13.2 40.9 - 67 D+AD+CU+WPC\ 3.9 --0.6 --0.5 --0.5 ·3.9 -0.5 - 68 D+AD+CG+WPCl+*AL+<ALB 5.2 20.0 -0.0 1.0 --0.0 1.0 -5.2 16.0 69 D+ AD+CG+WPC 1 +AL *+<ALB 5.2 15.8 -0.0 1.0 -0.0 1.0 -5.2 -20.2 70 D+AD+CG+WPB2 4.2 10.8 -0.0 1.0 -0.0 1.0 -4.2 -10.9 - 71 D+AD+CG+S+WPB2 11.7 42.0 -0.0 1.0 -0.0 1.0 -I 1.7 42.1 72 D+AD+CU+WPB2 1.9 . 1.0 . . 0.5 -0.5 -1.9 \.1 . 73 D+ AD+CG+WPB2+* AL +ALB> 4.4 . 20.6 . -0.0 1.0 -0.0 1.0 -4.4 \6.6 74 D+AD+CG+WPB2+AL *+ALB> 4.4 -16.4 . -0.0 1.0 . -0.0 1.0 -4.4 . 20.8 - 75 D+AD+CG+WPC2 4.8 -13.1 --0.0 1.0 . -0.0 1.0 -4.8 13.2 - 76 D+AD+CG+S+WPC2 12.1 43.7 . -0.0 1.0 -0.0 1.0 -12.1 . 43.9 77 D+AD+CU+WPC2 2.4 . 3.3 . . 0.5 -. 0.5 -2.4 3.4 . 78 D+AD+CG+WPC2+*AL+<ALB 4.7 . 21.5 . -0.0 1.0 --0.0 1.0 -4.7 . 17.4 . 79 D+AD+CG+WPC2+AL *+<ALB 4.7 -17.3 . -0.0 1.0 -0.0 1.0 -4.7 -21.7 - 80 D+AD+CG+S+ALB> 13.9 -56.1 --0.0 1.0 -0.0 1.0 -13.9 -56.3 - 81 D + AD+ CG..i-* AL+ALB> 4.4 -24.9 --0.0 1.0 --0.0 1.0 -4.4 -19.4 - 82 D + AD+ CG+AL *+ALB> 4.4 -19.3 -0.0 1.0 -0.0 1.0 -4.4 -25.0 83 D+AD+CG+S+*AL+ALB> \0.0 -45.1 --0.0 1.0 . -0.0 1.0 -10.0 -41.0 - 84 D+AD+CG+S+AL *+ALB> 10.0 -40.9 --0.0 1.0 --0.0 1.0 -10.0 . 45.3 . 85 D+AD+CG+S+<ALB 13.9 . 56.1 . -0.0 1.0 . -0.0 1.0 -13.9 . 56.3 . 86 D + AD + CG+* AL+<ALB 4.4 -24.9 --0.0 1.0 . -0.0 1.0 -4.4 -19.4 . 87 D +AD+ CG+AL*+<ALB 4.4 -19.3 . -0.0 1.0 . -0.0 1.0 -4.4 . 25.0 - 88 D+AD+CG+S+*AL+<ALB 10.0 . 45.1 -·0.0 1.0 . -0.0 1.0 -10.0 . 41.0 . 89 D+AD+CG+S+AL *+<ALB 10.0 . 40.9 --0.0 1.0 . -0.0 1.0 -10.0 . 45.3 - Maximum Combined Reactions Summary with Factored Loads~ FraminR X~Loc :;Grid Hrz left Load Hrz Right Load Hrzln Load Hrz Out Load Uplift Load Vrt Down Load Momcw Load Momccw Load (·Hx) Case (~) Case (·Hz) Case ~~ Case (·~t Case (Vy) Case (-Mzz) Case (Mzz) Case (k) (k) oil (in-ki (in·kl 0/0/0 1-D 7.2 18 \4.9 9 --0.0 38 5.8 \6 64.4 3 . . . - 15/0/0 1-C -. . -6.4 5 7.1 16 -. 1.1 32 . --- 38/0/0 1-B . . . . 6.4 5 7.1 16 . 1.1 32 --. - 53/0/0 I·A 15.0 8 7.3 \9 -. 0.0 38 5.7 17 64.5 2 . -. File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.\a 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: 9/3/0 Frame ID:Rigid Frame ' Values shown are resisting forces of the foundation. Reactions~ Unfactored Load Typ~ at F C S 2 rame ross ection: Type Exterior Column XMLoc 0/0/0 Grid! -Grid2 2-D Base Plate W x L (in.)_ 8 X 13 Base Plate Thickness (in.) 0.375 Anchor Rod Qty/Diam. (lil) 4-0.750 Column Base Elev. 100'-0" Load Type Desc. Hx Vy D Frm 0.7 3.8 AD Fnn 0.1 0.8 CG Fnn 2.0 7.9 s Frm 7.3 28.6 USI* Fnn 6.5 !6.9 *USl Fnn 6.5 34.5 WI> Fnn -6.3 -10.4 <WI Fnn 4.0 -3.5 W2> Fnn -7.3 -7.6 <W2 Fnn 2.9 -0.7 *AL> Fnn -0.1 10.0 AL*> Fnn .<!.! 2.7 <*AL Fnn 1.8 12.0 <AL* Fnn 1.8 4.7 cu Fnn 1.0 3.8 E> Fnn -3.2 -4.2 EG+ Fnn 0.3 !.0 <E Fnn 3.2 4.2 EG-Fnn -0.3 -!.0 EB> Bee <EB Brc - WPAI Brc 1.5 -7.7 'AL Fnn 0.9 11.0 ALB> Brc -- AL' Fnn 0.9 3.7 WPDI Brc 1.8 -5.7 <ALB Brc - WPA2 Brc 0.4 -4.8 WPD2 Brc 0.8 -2.8 WPBJ Brc !.I -7.2 WPCI Brc 1.6 -5.4 WPB2 Brc 0.1 -4A Frame Type: Rigid Frame Vy Exterior Column 53/0/0 2-A 8 X 13 0.375 4-0.750 100'..()" Hx YY -0.7 3.8 - -0.1 0.8 - -2.0 7.7 - -7.3 28.6 - -6.5 34.5 - -6.5 16.9 - -4.0 -3.5 - 6.3 -10.4 - -2.9 .<!.7 - 7.3 -7.6 - -1.8 4.7 - -1.8 12.0 - 0.1 2.7 - 0.1 10.0 - -1.0 3.8 - -3.1 4.2 - -0.3 1.0 - 3.1 -4.2 - 0.3 -1.0 - -- -- -1.1 -7.2 - -0.9 3.7 - - -0.9 I 1.0 - -!.6 -5.4 - - -0.1 -4.4 -0.6 -2.6 - -!.5 -7.7 - -!.8 -5.7 -0.4 -4.8 - File: 7079 Chevron R !_Stress Check 10_2008 with 08_2008 Loading - - - - - - - - - - - - - - - - - - - - - - - - - - - - Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 30 of 175 - --- - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy WPC2 Brc 0.6 -2.6 -0.8 -2.8 Frame Reactions Factored L ad Ca at Fra e Cross Section-2 -0 "' m X~Loc 01010 53/010 Grid l * Grid2 2-D 2·A Ld Description Hx Vv Hx Vv Cs application factor not shown (k) (k) (k) (k) 1 D+AD+CG+S 10.0 41.0 -10.0 40.8 - 2 D+AD+CG+USI* 9.3 29.4 -9.3 46.7 - 3 D+AD+CG+*USI 9.3 47.0 -9.3 29.2 - 4 D +AD+ CG +WI> -3.5 2.1 -6.7 8.7 - 5 D +AD+ CG + <WJ 6.7 8.9 3.5 1.8 - 6 D+AD+CG+W2> -4.5 4.9 -5.7 11.5 -- 7 D+AD+CG+<W2 5.7 11.8 4.5 4.7 -- 8 D+AD+CG +S +WI> ).5 26.1 -11.2 31.0 - 9 D+AD+CG+S+<Wl 11.2 31.2 -3.5 25.8 -- 10 D+AD+CG+S+W2> 2.7 28.2 -10.4 33.1 - 11 D+AD+CG+S+<W2 10.4 33.4 .2.7 28.0 - 12 D +AD +CG+* AL> 2.7. 22.5 -4.6 16.9 -- 13 D+AD+CG+AL"'> 2.7 15.2 -4.6 24.2 -- 14 D +AD+CG+<*AL 4.6 24.4 -2.7 15.0 -- 15 D+AD+CG+<AL* 4.6 17.2 -2.7 22.2 -- 16 D+AD+CU+WI> -5.2 -5.4 -5.0 1.5 -- 17 D+AD+CU+<Wl 5.0 1.5 5.2 -5.4 -- 18 D+AD+CU+W2> -6.2 -2.5 -4.0 4.3 -- 19 D+AD+CU+<W2 4.0 4.3 6.2 -2.5 -- 20 D+AD+CG.+S+*Al> 6.8 36.0 -8.2 31.8 -- 21 D+AD+CG+S+AL*> 6.8 30.6 -8.2 37.3 -- 22 D+AD+CG+S+<*AL 8.2 37.5 -6.8 30.4 -- 23 D+AD+CG+S+<AL* 8.2 32.1 -6.8 35.8 -- 24 D+AD+CG+Wl>+*AL> 0.4 16.1 -5.6 14.4 -- 25 D+AD+CG+Wl>+AL*> 0.4 10.6 -5.6 19.9 -- 26 D+AD+CG+<Wl+<*AL 5.6 20.1 -0.4 10.4 -- 27 D+AD+CG+<WI+<AL* 5.6 14.7 -0.4 15.8 -- 28 D +AD+ CG + W2>+*AL> -0.0 17.1 -5.3 15.5 i -- 29 D+AD+CG+W2>+AL*> -0.0 11.7 -5.3 20.9 -- 30 D +AD +CG +<W2+<*AL 5.3 21.2 o.o 11.5 -- 31 D +AD + CG + <W2+<AL * 5.3 15.7 o.o 16.9 -- 32 D+AD+CG+S+E>+EG+ 1.7 14.4 -6.4 20.3 -- 33 D+AD+CG+S+<E+EG+ 6.4 20.6 -1.7 14.1 -- 34 D+AD+CU+E>+EG--1.3 1.4 -3.1 7.2 -- 35 D+AD+CU+<E+EG-3.1 7.2 1.3 1.4 - 36 D+AD+CG+S+EB>+EG+ 4.0 17.5 -4.0 17.2 - 37 D+AD+CU+EB>+EG-0.9 4.3 -0.9 4.3 -- 38 D+AD+CG+S+<EB+EG+ 4.0 17.5 -4.0 17.2 -- 39 D+AD+CU+<EB+EG-0.9 4.3 -0.9 4,3 -- 40 D+AD+CG+WPAI 4.3 4.8 -3.9 5.0 -- 41 D+AD+CG+S+WPAl 9.3 28.1 -9.1 28.2 - 42 D+AD+CU+WPAl 2.6 -2.6 -2.2 -2.2 -- 43 D+AD+CG+WPAl+*AL+ALB> 4.0 17.8 -3.9 12.3 -- 44 D+AD+CG+WPAl+AL"'+ALB> 4.0 12.4 -3.9 17.8 - 45 D+AD+CG+WPDl 4.6 6.8 -4.4 6.8 - 46 D+AD+CG+S+WPDI 9.6 29.6 -9.4 29.6 -- 47 D+AD+CU+WPDI 2.9 -0.6 -2.7 -0.4 -- 48 D+AD+CG+WPDl+*AL+<ALB 4.1 18.6 -4.1 13.0 - 49 D+ AD+CG+WPD I +AL *+<ALB 4.1 13.1 -4.1 18.4 -- 50 D+AD+CG+WPA2 3.2 7.6 -2.8 7.9 51 D+AD+CG+S+WPA2 8.6 30.3 -8.3 30.4 52 D+AD+CU+WPA2 1.5 0.2 -1.1 0.7 - 53 D+AD+CG+WPA2+*AL +ALB> 3.6 18.9 -3.5 13.4 54 D+AD+CG+WPA2+AL *+ALB> 3.6 13.4 -3.5 18.8 55 D+AD+CG+WPD2 3.6 9.7 -3.4 9.7 - 56 D +AD+ CG + S + WPD2 8.8 31.8 -8.7 3!.7 - 57 D+AD+CU+WPD2 1.9 2.2 -1.7 2.5 - 58 D+AD+CG+WPD2+*AL+<ALB 3 7 19.7 -3.7 14.1 File: 7079 Chevron R \_Stress Check I 0_2008 with 08_2008 Loadmg Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 31 of 175 - - - - - - - --- - - - - - - - - - ---- - --- - - - - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM 32 of 175 59 D+AD+CG+WPD2+AL *+<ALB 3. 7 14.2 -3.7 19.5 60 D+AD+CG+WPB! 3.9 5.2 -4.3 4.6 . 61 D+AD+CG+S+WPBl 9.1 28.5 -9.3 27.9 62 D +AD+ CU +WPBI 22 -2.2 -2.6 -2.6 63 D+AD+CG+WPBI+*AL+ALB> 3.9 18.0 A.O 12.1 64 D+AD+CG+WPB I +AL*+ALB> 3.9 12.5 -4.0 17.6 . . 65 D+AD+CG+WPCI 4.4 7.1 -4.6 6.6 66 D+AD+CG+S+WPCI 9.4 29.8 -9.6 29.4 . . 67 D+AD+CU+WPC! 2.7 -0.4 -2.9 ·0.6 . 68 D+AD+CG+WPCI+*AL+<ALB 4.1 18.7 -4.1 12.9 . 69 D+AD+CG+WPCl +AL *+<ALB 4.1 13.2 -4.1 18.3 . 70 D+AD+CG+WPB2 2.8 8.1 ·3.2 7.4 . . . 71 D+AD+CG+S+WPB2 8.3 30.6 ·8.6 30.0 72 D+AD+CU+WPB2 1.1 0.7 -1.5 0.2 . . . 73 D+AD+CG+WPB2+*AL+ALB> 3.5 19.1 -3.6 13.2 . 74 D+ AD+CG+WPB2+AL *+ALB> 3.5 13.6 -3.6 18.7 . . 75 D+AD+CG+WPC2 3.4 9.9 ·3.6 9.4 76 D+AD+CG+S+WPC2 8.7 32.0 -8.8 31.5 . . 77 D+AD+CU+WPC2 1.7 2.5 -1.9 2.2 78 D+AD+CG+WPC2+*AL+<ALB 3.7 19.7 -3.7 14.0 . . 79 D+AD+CG+WPC2+AL*+<ALB 3.7 14.3 -3.7 19.4 . . 80 D +AD+ CG + S+ALB> 10.0 41.0 -10.0 40.8 . . . 81 D +AD+ CG+*AL+ALB> 3.7 23.5 -3.7 16.0 . . . 82 D +AD+ CG+AL*+ALB> 3.7 16.2 -3.7 23.2 . . . 83 D+AD+CG+S+*AL+ALB> 7.5 36.8 -7.5 31.1 . . 84 D+AD+CG+S+AL *+ALB> 7.5 31.3 -7.5 36.5 . . 85 D +AD +CG + S+<ALB 10.0 41.0 -10.0 40.8 . . . 86 D +AD+ CG+* AL +<ALB 3.7 23.5 -3.7 16.0 . . 87 D+AD+CG+AL"'+<ALB 3.7 16.2 -3.7 23.2 . . . 88 D+AD+CG+S+*AL+<ALB 7.5 36.8 -7.5 31.1 . . . 89 D+AD+CG+S+AL *+<ALB 7.5 31.3 -7.5 36.5 . . . 0 M" axamum C b" R om med eactaons s . bF ummjl_D'_ wtt acto red L d F oa s-ramml! X~Loc Grid Hrz left Load Hrz Right Load Hrzln Load HrzOut Load Uplift Load Vrt Down Load .Momcw Load Momccw Load (-Hx) Case (Hx) Case (-Hz) Case (Hz) Case (·Vy) Case (Vy) Case (·Mzz) Case (Mzz) Case (k) (k) (k) (k) {kl (kJ (in-k) (in-k) 0/0/0 2-D 6.2 18 11.2 9 . . . . 5.4 16 47.0 3 . . . . 53/0/0 2-A 11.2 8 6.2 19 . . . . 5.4 17 46.7 2 . . . . File: 7079 Chevron R I_ Stress Check 10 _2008 with 08 _2008 Loading Version; 7. la 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: 29/3/0 Frame ID:Rigid Frame Values shown are resisting forces of the foundation. Reactions· Unfactored Load Tvne at Frame Cross Section: 3 Type Exterior Column X~Loc 0/0/0 Grid I ~ Grid2 3-D Base Plate W x. L (in.) 9x 13 Base. Plate Thifkness (in.) 0.500 Anchor Rod Qty/Dial)l. (in.) 4-!.000 Column Base Elev. 100'-0" Load Tvne Desc. Hx Hz Vv D Fnn 0.8 -4.3 AD Fnn 0.1 -1.1 CG Frm 2.6 -12.3 s Fnn 9.8 -38.3 USl* Fnn 8.8 -22.7 *USl Fnn 8.8 -46.2 WI> Frm -6.9 --12.0 <WI Fnn 4.6 --4.3 W2> Fnn -8.3 --8.1 <W2 Frm 3.2 --Q.4 *AL;>-. Frm -0.1 -10.0 AL*> Frm -0.1 -2.7 <*AL Frm 1.8 -12.0 <AL* Frm 1.8 -4.7 cu Frm 1.3 -5.1 E> Frm -4.2 -5.5 EG+ Frm 0.3 -1.5 <E Frm 4.2 5.5 EG-Fnn -0.3 -1.5 EB> Bro 0.5 -19.3 -32.3 <EB Brc -0.3 0.0 29.0 WPAI Brc 2.1 -4.4 -17.6 'AL Fnn 0.9 -. 11.0 ALB> Bro - AL' Fm> 0.9 -3.7 WPDI Brc 2.4 --1.0 <ALB Brc - WPA2 Brc 0.7 ·4.4 -13.8 WPD2 Brc 1.0 -2.8 WPBI Brc 1.6 -3.8 -16.1 WPCI Brc 2.1 -1.5 WPB2 Brc 0.2 -3.8 -12.3 Frame Type:Rigid Frame Vy Exterior Column 53/0/0 3-A 9x 13 0.500 4-!.000 100'-Q" Hx Hz v¥- -0.8 -4.3 - -Q.I -l.l - -2.6 -10.1 - -9.8 -38.3 - -8.8 -46.2 - -8.8 -22.7 - -4.6 --4.3 - 6.9 --12.0 - -3.2 --Q.4 - 8.3 --8.1 - -1.8 -4.7 - -1.8 12.0 - 0.1 -2.7 - 0.1 -10.0 - -1.3 -5.1 - -4.1 -5.5 -0.3 -1.3 - 4.1 --5.5 - 0.3 --1.3 -0.5 -19.3 -32.4 0.3 0.0 29.0 - -1.6 -3.8 -16.1 - -0.9 -3.7 - -- - -0.9 -I 1.0 - -2.1 --1.5 - - -0.2 ·3.8 -12.3 -0.7 -2.3 -2.1 -4.4 -17.6 -2.4 -1.0 -0.7 -4.4 -13.8 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading - - - - - - - - - - - - - - - - - - - Version: 7.la Date:l0/20/2008 Time: I :57:43 PM Page: 33 of I 75 - - - - - - -- - - - - - - - . 07-27053 Calculations Hazardous Materials Occupancy WPC2 Brc o.1 I . I z.J -l.o 2.8 FeR t'sFtoedLdC ram eac wn -ac r oa ases a t F nune c s f . 3 ross ec mn. X-Loc 0/0/0 53/0/0 ) Grid! -Grid2 3-D 3-A Ld Description Hx Hz Vv Hx Hz Vv Cs (application factor not shown k (k (k) k k (k) . I D+AD+CG+S 13.4 56.0 -13.4 . 53.8 2 D +AD+ CO+ USI * 12.4 40.4 -12.4 6!.8 . . J D+AD+CG+*USI 12.4 . 63.9 -12.4 . 38.3 . 4 D+AD+CG+Wl> -3.4 5.7 -8.1 ILl 5 D+AD+CG+<Wl 8.1 13.4 3.4 3.6 . . 6 D+AD+CG+W2> -4.8 9.6 -6.7 15.1 . . 7 D+AD+CG+<WZ 6.7 . 17.3 4.8 . 7.4 . . 8 D+AD+CG+S+Wl> 5.7 . 37.4 -14.] . 4!.! . 9 D+AD+CG+S+<Wl 14.3 . 43.2 -5.7 . 35.3 . lO D+AD+CG+S+W2> 4.6 . 40.3 .IJ.J 43.9 . . II D+AD+CG+S+<W2 !3.3 46.1 -4.6 . 38.2 . . 12 D +AD +CG+*AL> 3.5 . 27.7 -5.4 . 20.3 . 13 D+AD+CG+AL*> 3.5 . 20A -5.4 . 27.6 . . 14 D +AD +CG+<*AL 5.4 29.7 -3.5 . !8.3 . . 15 D+AD+CG+<AL* 5.4 .. 22.4 -3.5 . 25.6 -- !6 D+AD+CU+Wl> -5.6 ·5.6 -6.0 . 2.1 . 17 D+AD+CU+<Wl 6.0 . 2.! 5.6 . -5.6 . . !8 D+AD+CU+W2> -7.0 . ·!.8 -4.6 . 5.9 . - 19 D+AD+CU+<W2 4.6 . 5.9 7.0 . -!.8 . . 20 D+AD+CG.+S+*AL> 9.0 . 46.7 -10.4 . 40.6 . . 21 D+AD+CG+S+AL*> 9.0 . 4!.3 -!0.4 -46.1 -- 22 D+AD+CG+S+<*AL !0.4 . 48.2 -9.0 . 39.2 . . 23 D+AD+CG+S+<AL"' . !0.4 . 42.8 -9.0 -44.6 . . 24 D+AD+CG+Wl>+*Al> 0.9 . 20.7 ·6.6 -17.5 . . 25. D+AD+CG+Wl>+AL*> 0.9 . 15.3 -6.6 . 23.0 . . 26 D+AD+CG+<Wl+<*AL 6.6 . 25.1 -0.9 . !3.2 . . 27 D+AD+CG+<WI+<AL* 6.6 . 19.6 -0.9 . !8.6 -. 28 D +AD +CG +W2>+*AL> 0.4 . 22.2 -6.1 . 18.9 . . 29 D+AD+CG+W2>tAL*> 0.4 . 16.7 -6.! . 24.4 . . 30 D+AD+CG+<W2+<*AL 6.1 -26.5 -0.4 . !4.6 . . 31 D+AD+CG+<W2+<AL* 6.1 2Ll -0.4 . 20.0 . 32 D+AD+CG+S+E>+EG+ 2.1 . 20.4 -8.3 . 26.4 . . 33 D+AD+CG+S+<E+EG+ 8.4 . 28.6 -2.2 . !8.1 . . 34 D+AD+CU+E>+EG--!.8 . !.4 -4.0 . 9.2 . 35 D+AD+CU+<E+EG-4.1 . 9.! !.7 . !.5 . . 36 D+AD+9G+S+EB>+EG+ 5.6 -14.4 0.3 -5.6 -14.5 -2.1 . . 37 D+AD+CU+EB>+EG-!.5 -!3.5 -17.3 -!.5 -!3.5 -17.3 - 38 D+AD+CG+S+<EB+EG+ 5.1 0.0 46.2 -5.! 0.0 44.0 . . 39 D+AD+CU+<EB+EG-0.9 0.0 25.5 -0.9 0.0 25.7 . . 40 D+AD+CG+WPAI 5.6 -4.4 0.! -5.1 -3.8 ·0.5 . . 41 D+AD+CG+S+WPAI !2.5 -3.3 33.2 -!2.! -2.9 32.2 . 42 . D+AD+CU+WPAl 3.5 -4.4 -11.3 -2.9 -3.8 ·9.8 . 43 D+AD+CG+WPAI+*AL+ALB> 5.0 -!.6 19.] -4.8 -!.4 12.3 . 44 D+AD+CG+WPA l+AL *+ALB> 5.0 -!.6 13.9 -4.8 -1.4 !7.8 . 45 D+AD+CG+WPDI 6.0 16.7 -5.7 . !4.1 . 46 D+AD+CG+S+WPDI 12.7 . 45.6 -12.5 . 43.2 . . 47 D +AD+ CU + WPDl 3.8 5.3 -3.5 . 4.9 48 D+AD+CG+WPDI+*AL+<ALB 5.1 . 25.6 -5.0 . 17.8 . . 49 D+AD+CG+WPDI+AL *+<ALB 5.1 . 20.1 -5.0 23.3 . 50 D+AD+CG+WPA2 4.Z -4.4 3.9 -3.7 -3.8 3.3 51 D+AD+CG+S+WPA2 !!.4 -3.3 36.1 -I !.0 -2.9 35.0 52 D+AD+CU+WPA2 2.1 -4.4 ·7.5 -1.6 -3.8 -6.0 53 D+AD+CG+WPA2+* AL +ALB> 4.5 -1.6 20.8 -4.3 -1.4 13.8 54 D+AD+CG+WPA2+AL *+ALB> 4.5 -1.6 15.3 -4.3 -1.4 19.2 55 D +AD +CG +WPD2 4.6 20.5 4.3 17.9 . 56 D+AD+CG+S+WPD2 I 1.7 48.5 -I I .4 46.0 57 D+ AD +CU + WPD2 2.4 9.1 -2.1 8.7 . 58 D+AD+CG+WPD2+* AL+<ALB 4.6 27.0 -4.5 19.3 . File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 34 of 175 . . . . . . . . . . . . . . . . . . . -. . . . . . . . . . . . . . . . . . 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 35 of 175 59 D+AD+CG+WPD2+AL *+<ALB 4.6 21.6 -4.5 24.7 60 D +AD+ CG + WPBI 5.1 -3.8 1.6 -5.6 -4.4 -2.1 61 D+AD+CG+S+WPBl 12.1 -2.9 34.3 -12.5 -3.3 3l.l . 62 D+AD+CU+WPBl 2.9 -3.8 -9.8 -3.5 -4.4 -11.3 . . . 63 D+AD+CG+WPBl+*AL+ALB> 4.8 -1.4 19.9 -5.0 -1.6 11.8 64 D+AD+CG+WPB l+AL *+ALB> 4.8 -1.4 14.5 -5.0 -1.6 17.2 . . . 65 D+AD+CG+WPCI 5.7 16.2 -6.0 14.6 66 D+AD +CG +S+ WPCI 12.5 45.3 -12.7 . 43.5 . . . 67 D+AD+CU+WPCI 3.5 4.8 -3.8 5.3 68 D+ AD+CG+WPC l +* AL +<ALB 5.0 . 25.4 -5.1 18.0 . 69 D+AD+CG+WPCI+AL*+<ALB 5.0 19.9 -5.1 . 23.5 . . 70 D+AD+CG+WPB2 3.7 -3.8 5.4 -4.2 -4.4 1.8 . 71 D+AD+CG+S+WPB2 11.0 -2.9 37.2 -11.4 -3.3 33.9 . 72 D+AD+CU+WPB2 1.6 -3.8 ·6.0 -2.1 -4.4 -7.5 . . . 73 D+AD+CG+WPB2+*AL+ALB> 4.3 -1.4 21.3 -4.5 -1.6 13.2 . 74 D+AD+CG+WPB2+AL *+ALB> 4.3 -1.4 15.9 -4.5 -1.6 18.6 . . . 75 D+AD+CG+WPC2 4.3 . 20.0 -4.6 . 18.4 . . . 76 D+AD+CG+S+WPC2 11.4 48.1 -11.7 46.4 . . . 77 D+AD+CU+WPC2 2.1 . 8.7 -2.4 . 9.1 . . 78 D+AD+CG+WPC2+*AL+<ALB 4.5 . 26.8 -4.6 . !9.4 . . 79 D+AD+CG+WPC2+AL *+<ALB 4.5 . 21.4 4.6 . 24.9 . . 0 . 80 D+AD+CG+S+ALB> 13.4 . 56.0 -13..4 53.8 . . . 81 D+AD+CG+*AL+ALB> 4.4 . 28.7 -4.4 ' 19.3 . 82 D + AD + CG+AL *+ALB> 4.4 . 2!.4 -4.4 . 26.6 . 83 D+AD+CG+S+*AL+ALB> 9.7 . 47.5 -9.7 . 39.9 . . . 84 D+AD+CG+S+AL *+ALB> 9.7 42.0 -9.7 . 45.3 . 85 D + AD+CG + S+<ALB 13.4 . 56.0 -13.4 -53.8 -. 86 D+AD+CG+*AL+<ALB 4.4 -28.7 -4.4 -19.3 . . 87 D +AD+ CG+AL *+<ALB 4.4 -21.4 -4.4 -26.6 --- 88 D+AD+CG+S+*AL+<ALB 9.7 47.5 -9.7 -39.9 --- 89 D+AD+CG+S+AL*+<ALB 9.7 -42.0 -9.7 -45.3 -- M. ax1mum C bi dR om ne eact ons s I F ummarvw th adore dL d F oa s-ram n2 X-Loc Grid Hrz left Load HrzRight Load Hrzln Load Hrz Out Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-Hx) Case (~) Case (·Hz) Case (Hz) Case (-Vy) Case (Vy) Case (-Mzz) Case (M7.z) Case (k) 'ti<) . (k) (k) (kl (in-k) (in-k) 01010 3-D 7.0 18 14.3 9 14.4 36 0.0 38 17.3 37 63.9 3 --- 53/0/0 3-A 14.3 8 7.0 19 14.5 36 0.0 38 17.3 37 61.8 2 ---- B rae ne X-Loc Grid Description 01010 3-D Diagonal bracing at base is attached to colUmn. Reactions ARE included with frame reactions. 53/0/0 3-A Diagonal bracing at base is attached to column. Reactions ARE included with frame reactions. File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: 47/9/0 Frame ID:Rigid Frame y Values shown are resisting forces of the foundation. Reactions-Unfactored Load Tvoe at Frame Cross Section; 4 Type Exterior Column X-Loc 0/0/0 Grid! -Grid2 4-D Base Plate W x L (in.) 8 X 13 Base Plate Thickness (in.) 0.500 Anchor Rod Qty/Diam. (in.) 4. 0.750 Column Base EleV. 100'-0" Load Type Desc. Hx Hz Vv D Fnn 0.8 -4.3 AD Fnn 0.1 -1.1 CG Fnn 2.6 -12.3 s Frm 9.8 -38.3 US!* G Frm 8.8 -22.7 *USl Fnn 8.8 -46.2 WI> Fnn -6.9 --11.9 <WI Fnn 4.6 --4.3 W2> Fnn -8.3 --8.1 <W2 Frm 3.2 --0.4 'AL> Fnn -0.1 -10.0 AL*> Fnn -0.1 -2.7 <*AL Fnn 1.8 -12.0 <AL* Fnn 1.8 -4.7 cu Fnn 1.3 -5.1 E> Fnn -4.2 . -5.5 EG+ Fnn 0.3 -1.5 <E Fnn 4.2 -5.5 EG-Fnn -0.3 . -1.5 EB> Brc -0.3 . 32.3 <EB Brc 0.4 16.2 -29.0 WPAI Brc 1.9 --2.9 'AL Fnn 0.9 11.0 ALB> Brc . . AU-· Fnn 0.9 . 3.7 WPDI Brc 2.6 3.7 -14.2 <ALB Brc . . WPA2 Brc 0.5 0.9 WPD2 Brc 1.2 3.7 -10.4 WPB! Bee 1.4 -3.2 WPCI Brc 2.3 3.2 -13.0 WPB2 Brc 0.0 . 0.6 Frame Type:Rigid Frame Vy Exterior Column 53/0/0 4-A 8x 13 0.375 4-0.750 100'-0" Hx Hz Vv '0.8 -4.3 - -0.1 . 1.1 - -2.6 -10.1 - -9.8 -38.3 - -8.8 -46.2 - -8.8 -22.7 - -4.6 --4.3 - 6.9 -11.9 - -3.2 --0.4 8.3 --8.1 -1.8 -4.7 - -1.8 -12.0 - 0.1 -2.7 - 0.1 -10.0 - -1.3 -5.1 . -4.1 5.5 - -0.3 . 1.3 . 4.1 -5.5 - 0.3 -1.3 - 0.3 -32.4 . -0.4 16.3 -29.0 . -1.4 . -3.2 . -0.9 3.7 -. . . . -0.9 11.0 -2.3 3.2 -13.0 . -0.0 0.6 -0.9 3.2 -9.2 -1.9 -2.9 -2.6 3.7 -14.2 -0.5 0.9 . File: 7079 Chevron R !_Stress Check I 0_2008 with 08_2008 Loading - - - - - --- - - - - - -. . -. -. . . . . . . . . . Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 36 of !75 - - - - - - - - - - - - - - - - - . . 07-27053 Calculations Hazardous Materials Occupancy WPC'2 Brc o.9 3.2 I -9.2 I -u I 3.7 l-lo3 I Frame Reactions Factored Load Cases at Frame Cross Section· 4 - X-Loc 010/0 53/0/0 Grid! Grid2 4-D 4-A Ld Description Hx Hz Vy Hx Hz Vy Cs (application factor not shown) (k) (k) (k) (k) k k I D+AD+CG+S 13.4 -56.0 -13.4 -53.8 -- 2 D+AD+CG+USI* 12.4 -40.4 -12.4 -61.8 - 3 D +AD+ CG +*US! 12.4 -63.9 -12.4 38.3 - 4 D+AD+CG+Wl> -3.4 -5.8 -8.1 -11.3 5 D+AD+CG+<Wl 8.1 13.4 3.4 -3.6 6 D+AD+CG+W2> -4.8 -9.6 -6.7 -15.1 - 7 D+AD+CG+<W2 6.7 17.3 4.8 -7.5 - 8 D+AD+CG+S+W!> 5.7 -37.4 -14.3 -4l.l -- 9 D+AD+CG+S+<Wl 14.3 -43.2 -5.7 -35.3 - 10 D+AD+CG+S+W2> 4.6 -40.3 -13.3 -43.9 -- 11 D+AD+CG+S+<W2 13.3 -46.1 -4.6 -38.2 -- 12 D+AD+CG+*AL> 3.5 -27.7 -5.4 -20.3 -- 13 D +AD +CG+AL*> 3.5 -20.4 -5.4 -27.6 - 14 D+AD+CG+<*AL 5.4 -29.7 -3.5 -18.3 -- 15 D +AD +CG+<AL* 5.4 22.4 -3.5 -25.6 - 16 D+AD+CU+WI> -5.6 --5.6 -6.0 -2.1 -- 17 D+AD+CU+<WI 6.0 -2.1 5.6 --5.6 -- 18 D+AD+CU+W2> -7.0 -. -1.8 -4.6 -5.9 -- 19 D+AD+CU+<W2 4.6 -5.9 7.0 --1.8 -- 20 D+AD+CG+S+*AL> 9.0 -46.7 -10.4 -40.6 -- 21 D+AD+CG+S+AL*> 9.0 -41.3 -10.4 -46.1 -- 22 D+AD+CG+S+<'*'AL 10.4 -48.2 -9.0 -39.2 -- 23 D+AD+CG+S+<AL* 10.4 -42.8 -9.0 -44.6 -- 24 D+AD+CG+Wl>+*AL> 0.9 -20.7 -6.6 -17.5 -- 25 D+AD+CG+Wl>+AL*> 0.9 -15.3 -6.6 -23.0 -- 26 D+AD+CG+<Wl+<*AL 6.6 -25.1 -0.9 -13.2 -- 27 D+AD+CG+<Wl+<AL* 6.6 -19.6 -0.9 -18.6 -- 28 D +AD + CG + W2>+* AL> 0.4 -22.2 -6.1 -18.9 -- 29 D+AD+CG+W2>+AL*> 0.4 -16.7 -6.1 -24.4 -- 30 D +AD +CG +<W2+<*AL 6.1 -26.5 -0.4 -14.6 -- 31 D +AD +CG +<W2+<AL* 6.1 -21.1 -0.4 -20.0 -- 32 D+AD+CG+S+E>+EG+ 2.1 -20.4 -8.3 -26.4 -- 33 D+AD+CG+S+<E+EG+ 8.4 -28.6 -2.2 -18.1 -- 34 D+AD+CU+E>+EGv -1.8 -1.4 -4.0 -9.2 -- 35 D+AD+CU+<E+EG~ 4.1 -9.1 1.7 -1.5 - 36 D+AD+CG+S+EB>+EG+ 5.0 -48.7 -5.0 -46.5 - 37 D+AD+CU+EB>+EG~ 0.9 -27.9 -0.9 -28.0 - 38 D+AD+CG+S+<EB+EG+ 5.6 12.2 2.7 -5.6 12.2 0.5 - 39 D+AD+CU+<EB+EG-1.4 11.4 -15.1 -1.4 11.4 -14.9 - 40 D+AD+CG+WPAI 5.5 -14.8 -5.0 -12.3 - 41 D+AD+CG+S+WPAI 12.3 -44.2 -12.0 -41.9 - 42 D+AD+CU+WPAI 3.3 -3.4 -2.8 -3.1 43 D+AD+CG+WPAI+*AL+ALB> 4.9 -24.8 -4.8 -17.2 - 44. D+AD+CG+WPA i+AL*+ALB> 4.9 -19.4 -4.8 22.6 45 D +AD+ CG + WPDJ 6.1 3.7 3.5 -5.8 3.2 2.6 - 46 D+AD+CG+S+WPDI 12.8 2.8 35.8 -12.6 2.4 34.5 -- 47 D +AD+ CU + WPD\ 3.9 3.7 -7.8 -3.6 3.2 -6.7 -- 48 D+AD+CG+WPDI+*AL+<ALB 5.2 1.4 20.6 -5.1 1.2 13.5 - 49 D+AD+CG+WPDI+AL*+<ALB 5.2 1.4 15.2 -5.1 1.2 19.0 - 50 D+AD+CG+WPA2 4.1 18.6 -3.6 16.2 51 D+AD+CG+S+WPA2 11.3 -47.1 -10.9 -44.7 52 D+AD+CU+WPA2 1.9 7.2 -1.4 -6.9 53 D+AD+CG+WPA2+*AL+ALB> 4.4 26.3 -4.2 -18.6 - 54 D+AD+CG+WPA2+AL*+ALB> 4.4 20.8 -4.2 -24.0 55 D+AD+CG+WPD2 4.7 3.7 7.3 -4.4 3.2 6.4 - 56 D +AD+CG +S + WPD2 11.8 2.8 38.6 -11.6 2.4 37.4 - 57 D +AD +CU +WPD2 2.5 3.7 -4.0 -2.2 3.2 -2.9 - 58 D+AD+CG+WPD2+*AL+<ALB 4.7 1.4 22.1 -4.5 1.2 14.9 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 Time: ! :57:43 PM Page: 37 of 175 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 38 of 175 59 D+AD+CG+WPD2+AL *+<ALB 4.7 1.4 16.6 -4.5 1.2 20.4 60 D+AD+CG+WPB! 5.0 14.5 -5.5 -12.7 6! D+AD+CG+S+WPBI 12.0 44.0 -12.3 -42.1 - 62 D+AD+CU+WPBJ 2.8 3.1 -3.3 -3.4 - 63 D+AD+CG+WPB!+*AL+ALB> 4.8 24.7 -4.9 -17.3 64 D+AD+CG+WPB l+AL *+ALB> 4.8 -!9.3 -4.9 22.7 - 65 D+AD+CG+WPCI 5.8 3.2 4.7 -6.1 3.7 1.4 - 66 D+AD+CG+S+WPCl 12.6 2.4 36.6 -12.8 2.8 33.7 -- 67 D+AD+CU+WPCJ 3.6 3.2 -6.7 -3.9 3.7 -7.8 68 D+AD+CG+WPCI+*AL+<ALB 5.! 1.2 2l.l -5.2 1.4 !3.! - 69 D+AD+CG+WPCI +AL*+<ALB 5.! L2 15.6 -5.2 1.4 18.5 - 70 D+AD+CG+WPB2 3.6 18.3 -4.! -!6.5 7! D+AD+CG+S+WPB2 !0.9 46.8 -!!.3 -44.9 - 72 D+AD+CU+WPB2 1.4 6.9 -1.9 -7.2 -- 73 D+AD+CG+WPB2+*AL+ALB> 4.2 -26.2 -4.4 -!8.7 -- 74 D+AD+CG+WPB2+AL*+ALB> 4.2 -20.7 -4.4 -24.2 --- 75 D+AD+CG+WPC2 4.4 3.2 8.5 -4.7 3.7 5.2 -- 76 D+AD+CG+S+WPC2 11.6 2.4 39.5 -11.8 2.8 36.5 --- 77 D+AD+CU+WPC2 2.2 3.2 -2.9 -2.5 3.7 -4.0 -- 78 D+AD+CG+WPC2+*AL+<ALB 4.5 !.2 22.5 -4.7 !.4 14.5 -- 79 D+AD+CG+WPC2+AL*+<ALB 4.5 L2 17.0 -4.7 !.4 20.0 --- 80 D+AD'+CG+S+ALB> !3.4 -56.0 -13.4 -53.8 -. - 8! D+AD+CG+*AL+ALB> 4.4 . 28.7 -4.4 . !9.3 . . 82 D+AD+CG+AL*+ALB> 4.4 . 2!.4 -4.4 . 26.6 . . . 83 D+AD+CG+S+*AL+A~> 9.7 . 47.5 -9.7 -39.9 --- 84 D+AD+CG+S+AL*+ALB> 9.7 . 42.0 -9.7 . 45.3 . . - 85 D +AD +CG +S+<ALB !3.4 . 56.0 -!3.4 . 53.8 . . . 86 D +AD + CG+* AL+<ALB 4.4 . 28.7 -4.4 . !9.3 --. 87 D +AD + CG+AL *+<ALB 4.4 . 2!.4 -4.4 . 26.6 --- 88 D+AD+CG+S+' AL+<ALB 9.7 -47.5 -9.7 . 39.9 . . . 89 D+AD+CG+S+AL'+<ALB 9.7 . 42.0 -9.7 . 45.3 . . . M' ax1mum c ombine dR eactions s • h ummarvwd Factore dL d oa s • Framm!! X~Loc Grid Hrz left Load HrzR.ight Load Hrzln Load HrzOut Load Uplift Load VrtDown Load Momcw Load Momccw Load (-H•) Case . (H•) Case (-Hz) Case (Hz) Case (-Vy) Case (Vy) Case (-Mzz) Case (Mzz) Case (k) (k) (k) (k) (kl (k) (in-ki {in-k) 0/0/0 4-D 7.0 18 !4.3 9 . !2.2 38 !5.1 39 63.9 3 . . . . 53/010 4-A !4.3 8 7.0 19 . . !2.2 38 !4.9 39 61.8 2 . . . - B rae oe X~Loc Grid Description 0/0/0 4-D Diagonal bracing at base is attached to column. Reactions ARE included with frame reactions. 53/0/0 4-A Diagonal bracing at base is attached to column. Reactions ARE included with frame reactions. . File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a I ) 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: 671910 Frame ID:Rigid Frame Valu~s shown are resisting forces of the foundation, Reactions M Unfactored Load Tvne at Frame Cross Section: 5 Type Exterior Colwnn XMLoc 0/0/0 Grid! -Grid2 5-D Base Plate W x L (in.) 9x 13 B<ise Plate Thickness (in.) 0.500 Anchor Rod Qty/Diarn. (in.) 4-!.000 Column Base Elev. 100'-0" Load Type Desc. Hx Vv I) Fnn 0.8 4.3 AD Fnn 0.1 l.l CG Fnn 2.6 15.2 s Fnn 9.8 38.3 USl* Fnn 8.8 22.7 *USl Fnn 8.8 46.2 WI> Fnn -6.9 -11.9 <WI Fnn 4.6 -4.3 W2> Fnn -8.3 -8.1 <W2 Fnn 3.2 -0.4 'AL> Fnn -0.1 10.0 AL*> Fnn -0.1 2.7 <*AL Fnn 1.8 12.0 <AL* Fnn !.8 4.7 cu Fnn 1.3 5.1 E> Fnn -4.6 -5.6 EG+ Fnn 0.3 1.8 <E Fnn 4.6 5.6 EG-F1m -0.3 -1.8 EB> Brc -- <EB Brc -- WPA1 Brc 2.0 -10.0 'AL Fnn 0.9 I LO ALB> Brc - AL' Frm 0.9 3.7 WPD1 Bro 2.4 -7.9 <ALB Brc - WPA2 Brc 0.7 -6.1 WPD2 Brc 1.0 A. I WPBI Brc 1.6 -9.4 WPC'I Brc 2.1 -7.5 WPB2 Bro 0.2 -5.6 Frame Type: Rigid Frame ® Exterior Column 53/0/0 5-A 9x 13 0.500 4-1.000 100'~0" Hx Vv -0.8 4.3 - -0.1 l.l - -2.6 10.2 - -9.8 38.3 - -8.8 46.2 - -8.8 22.7 - -4.6 -4.3 - 6.9 -11.9 - -3.2 -0.4 - 8.3 -8.1 - -1.8 4.7 - -1.8 12.0 0.1 2.7 - 0.1 10.0 - -1.3 5.1 - -4.2 5.6 - -0.3 lA - 4.2 -5.6 0.3 ML4 - -- -1.6 -9.4 -0.9 3.7 - -- -0.9 11.0 -2.1 -7.5 - - -0.2 -5.6 - -0.7 -3.7 -2.0 -10.0 -2.4 -7.9 -0.7 -6.1 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading - - - - - --- - - - - - - - - - - Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 39 of 175 - - - - - - - - - - - - - - - - 0 07-27053 Calculations Hazardous Materials Occupancy WPC2 Brc 0.7 -3.7 -1.0 -4.1 F rame R tl eac ons M F toedL dC ac r oa ases a tF rame c s r 5 ross ec wn: X-Loc 01010 5310/0 Gridl -Grid? 5-D 5-A Ld Descriotion Hx Vv Hx Vv Cs application factor not shown .(k (k) -ik) k\ I D+AD+CG+S 13.4 58.9 -13.4 53.9 -- 2 D+AD+CG+US!* 12.4 43.3 -12.4 61.9 - 3 D+AD+CG+*USl 12.4 66.8 -12.4 38.3 -- 4 D +AD+ CG +WI> -3.3 8.7 -8.2 11.4 -- 5 D+AD+CG+<W! 8.2 16.4 3.3 3.7 -- 6 D+AD+CG+WZ> -4.7 12.5 -6.8 15.2 -- 7 D+AD+CG+<WZ 6.8 20.2 4.7 7.5 -- 8 D+AD+CG+S+Wl> 5.8 40.4 -14.4 41.2 -- 9 D+AD+CG+S+<Wl 14.4 46.1 -5.8 35.4 -- 10 D+AD+CG+S+WZ> 4.7 43.2 -13.4 44.0 - II D+AD+CG+S+<W2 13.4 49.0 -4.7 38.3 - 12 D+AD+CG+*AL> 3.6 30.6 -5.5 20.4 -- 13 D +AD+ CG+AL*> 3.6 23.4 -5.5 27.6 -- 14 D+ AD+ CG+<*AL 5.5 32.6 -3.6 18.4 -- 15 D+AD+CG+<AL* 5.5 25.3 -3.6 25.7 -- 16 D+AD+CU+Wl> -5.6 ·-5.6 -6.0 2.1 -- 17 D+AD+CU+<Wl 6.0 2.1 5.6 -5.6 -- 18 D+AD+CU+W2> -7.0 -1.8 -4.6 5.9 -- 19 D+AD+CU+<WZ 4.6 5.9 7.0 -1.8 -- 20 D+AD+CG+S+*AL> 9.1 49.6 -10.5 40.7 -- 21 D+AD+CG +S+AU> 9.1 44.2 -10.5 46.2 -- 22 D+AD+CG+S+<*AL 10.5 51.1 -9.1 39.2 -- 23 D+AD+CG+S+<AL* 10.5 45.7 -9.1 44.7 -- 24 D+AD+CG+Wl>+*Al> 1.0 23.6 -6.7 17.6 -- 25 D+AD+CG+Wl>+AL*> 1.0 18.2 -6.7 23.1 -- 26 D +AD+ CG +<WI+<*AL 6.7 28.0 -1.0 13.2 -- 27 D+AD+CG+<Wl+<AL* 6.7 22.5 -1.0 18.7 -- 28 D +AD+ CG + W2>+*AL> 0.5 25.1 -6.2 19.0 -- 29 D +AD+ CG + WZ>+AL*> 0.5 19.6 -6.2 24.5 -- 30 D +AD + CG + <W2+<* AL 6.2 29.4 -0.5 14.7 -- 31 D+ AD+ CO+ <W2t<AL* 6.2 24.0 -0.5 20.1 -- 32 D+AD+CG+S+E>+EG+ 1.9 23.4 -8.5 26.5 -- 33 D+AD+CG+S+<E+EG+ 8.8 31.8 -2.2 18.2 -- 34 D+AD+CU+E>+EG~ -2.1 1.2 -4.0 9.3 -- 35 D+AD+CU+<E+EG~ 4.3 9.0 1.8 1.5 -- 36 D+AD+CG+S+EB>+EG+ 5.3 27.6 -5.3 22.4 -- 37 D+AD+CU+EB>+EG~ 1.1 5.1 -1.1 5.4 -- 38 D+AD+CG+S+<EB+EG+ 5.3 27.6 -5.3 22.4 -- 39 D+AD+CU+<EB+EG-1.1 5.1 -1.1 5.4 - 40 D +AD+ CG + WPAl 5.7 10.7 -5.2 6.3 -- 41 D+AD+CG+S+WPAl 12.5 41.8 -12.1 37.3 - 42 D+AD+CU+WPAl 3.4 -3.6 -2.9 -3.1 -- 43 D+AD+CG+WPAI+*AL+ALB> 5.1 25.1 -4.9 14.9 - 44 D+AD+CG+WPAI+AL*+ALB> 5.1 19.7 -4.9 20A 45 D+AD+CG+WPD! 6.0 12.7 -5.7 8.1 - 46 D+AD+CG+S+WPDl 12.8 43.4 -12.5 38.7 - 47 D +AD+ CU + WPDI 3.8 -1.6 -3.5 -1.2 - 48 D+AD+CG+WPDI+*AL+<ALB 5.2 25.9 -5.1 15.6 - 49 D+AD+CG+WPDI +AL *+<ALB 5.2 20.4 -5.1 21.1 -- 50 D+AD+CG+WPA2 4.3 14.5 -3.8 10.1 51 D+AD+CG+S+WPA2 11.5 44.7 -II.! 40.2 -- 52 D+AD+CU+WPA2 2.0 0.2 -1.5 0.8 53 D+AD+CG+WPA2+*AL+ALB> 4.5 26.6 -4.4 16.4 - 54 D+AD+CG+WPA2+AL*+ALB> 4.5 21.1 -4.4 21.8 - 55 D +AD+ C'G + WPD2 46 16.5 -4.3 11.9 - 56 D+ AD+ CG +S + WPD2 117 46.2 -11.5 4!.6 - 57 D +AD+ CU + WPD2 2.4 2.2 -2.1 2.6 - 58 D+AD+CG+WPD2+*AL+<ALB 4.7 27.3 -4.6 17.1 -- File: 7079 Chevron R I_ Stress Check I 0 _ 2008 with 08 _ 2008 Loading Version: 7.1a Date: 10/20/2008 Time: I :57:4o PM Page: 40 of 175 - - - - - - - - - - - - - - - - - - - - - ----- - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 41 of 175 59 D+AD+CG+WP02+AL *+<ALB 4.7 21.9 -4.6 22.5 - 60 D+AD+CG+WPBI 5.2 11.2 -5.7 5.7 - 61 D+AD+CG+S+WPBI 12.1 42.3 -12.5 36.9 - 62 D+AD+CU+WPBJ 2.9 -3.1 -3.4 -3.6 - 63 D+AD+CG+WPBI+*AL+ALB> 4.9 25.3 -5.! 14.7 64 D+AD+CG+WPB l+AL *+ALB> 4.9 19.9 -5.! 20.2 -- 65 D+AD+CG+WPC! 5.7 13.1 -6.0 7.8 66 D+AD+CG+S+WPCl 12.5 43.7 -12.8 38.4 - 67 D+AD+CU+WPCI 3.5 -1.2 -3.8 -1.6 -- 68 D+AD+CG+WPCl+*AL+<ALB 5.1 26.0 -5.2 15.5 69 D+AD+CG+WPCI+AL*+<ALB 5.1 20.6 -5.2 20.9 - 70 D+AD+CG+WPB2 3.8 15.0 -4.3 9.5 - 71 D+AD+CG+S+WPB2 ILl 45.1 -ll.5 39.8 - 72 D+AD+CU+WPB2 1.5 0.8 -2.0 0.2 -- 73 D+AD+CG+WPBZ+*AL+ALB> 4.4 . 26.8 -4.5 16.2 -- 74 D+AD+CG+WPBZ+AL*+ALB> 4.4 2!.3 -4.5 21.6 - 75 D+AD+CG+WPC2 4.3 16.9 -4.6 11.6 - 76 D+AD+CG+S+WPC2 l 1.5 46.5 -11.7 4!.3 77 D+AD+CU+WPC2 2.1 2.6 -2.4 2.2 - 78 D+AD+CG+WPCZ+*AL+<ALB 4.6 27.5 -4.7 16.9 -- 79 D+AD+CG+WPC2+AL'+<ALB 4.6 22.0 -4.7 22.4 --- 80 D+AD+CG+S+ALB> !3.4 58.9 -13.4 53.9 --- 81 D +AD + CG+* AL+ALB> 4.5 3!.6 -4.5 19.4 -- 82 D+AD+CG+AL*+ALB> 4.5 24.3 -4.5 26.7 -- 83 D+AD+CG+S+* AL +ALB> 9.8 50.4 -9.8 40.0 - 84 D+AD+CG+S+AL *+ALB> 9.8 44.9 -9.8 45.4 -- 85 D +AD + CG + S+<ALB 13.4 58.9 -13.4 53.9 -- 86 D +AD+ CG+*AL+<ALB 4.5 3!.6 -4.5 19.4 -- 87 D +AD+ CG+AL *+<ALB 4.5 24.3 -4.5 26.7 --- 88 D+AD+CG+S+*AL+<ALB 9.8 50.4 -9.8 40.0 --- 89 D+AD+CG+S+AL *+<ALB 9.8 44.9 -9.8 45.4 --- M" ax1mum Combin.e dR eachons s 'IF ummarv wit 1 actore dL d F oa s-ram ne: X-Loc Grid Hrz left Load Hrz Right Load Hrzln Load Hrz Out Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-Hx) Case (~) Case (-Hz) .Case (Hz) ftase (·Vy) Case (Vy) Case (·Mzz) Case (Mzz) Case (k) (k) (k) (k) (k) (in-k\ (in-k\ 0/0/0 S·D 7.0 18 14.4 9 ---. 5.6 16 66.8 3 . . - - 53/0/0 S·A 14.4 8 7.0 19 . . --5.6 17 6!.9 2 -. -. File: 7079 Chevron R !_Stress Check 10_2008 with 08_2008 Loading Version: 7.\a 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: 86/3/0 Frame ID:Rigid Frame Values shown are ~esisting forces of the foundation. Reactions-Unfactored Load Type at Frame Cross Section: 6 Type Exterior Column X~Loc 0/0/0 Grid! • Grid2 6-D Base Plate W x L (in.) 9x. 13 Base Plate Thickness (in.) 0.500 Anchor RoO. Qty/Diam. (in.) 4. 1.000 Column Base Elev. 100'~0" Load Type Desc. Hx Vy D Fnn 0.8 4.3 AD Fnn 0.1 1.1 CG Fnn 2.6 15.2 s Fnn 9.8 38.3 USl"' Fnn 8.8 22.7 *USl Fnn 8.8 46.2 WI> Fnn -6.9 -11.9 <WI Fnn 4.6 -4.3 W2> Fnn ·8.3 -8.1 <W2 Fnn 3.2 -0.4 *AL> Fnn -0.1 10.0 AL*> Fnn -0.1 2.7 <*AL Fnn 1.8 12.0 <AL* Fnn 1.8 4.7 cu Fnn 1.3 5.1 E> Fnn -4.6 -5.6 EG+ Frrn 0.3 1.8 <E Frm 4.6 5.6 EG-F•m -0.3 -1.8 EB> Brc - - <EB Brc - WPAI Brc 2.4 -7.9 'AL Fnn 0.9 11.0 ALB> Brc - - AL' Fnn 0.9 3.7 WPDI Brc 2.0 -10.0 <ALB Brc WPA2 Brc 1.0 -4.1 WPD2 Brc 0.7 -6.1 WPBI Brc 2.1 -7.5 WPCI Brc 1.6 -9.4 WPB2 Brc 0.7 -3.7 Frame Type: Rigid Frame ~ll Vy "' "' Exterior Column 53/0/0 6-A 9x 13 0.500 4. 1.000 lOO'wO" Hx Vv -0.8 4.3 . -0.1 1.1 . -2.6 10.2 - -9.8 38.3 - -8.8 46.2 - -8.8 22.7 . -4.6 -4.3 - 6.9 -11.9 - -3.2 -0.4 - 8.3 -8.1 - -1.8 4.7 - -1.8 12.0 - 0.1 2.7 0.1 10.0 . -1.3 5.1 - -4.2 5.6 -0.3 1.4 . 4.2 -5.6 0.3 -L4 - -- - -2.1 -7.5 -0.9 3.7 . -- -0.9 11.0 - -1.6 -9.4 -. ·0.7 -3.7 -0.2 -5.6 -2.4 -7.9 - -2.0 -10.0 ·1.0 -4.1 - File: 7079 Chevron R l_Stress Check I 0_2008 with 08_2008 Loading . - - - -. . . . - - - - - - - - Version: 7.1a Date: 10/20/2008 Time: 1:57:43 PM Page: 42 of 175 . . - - - -. - - - - -. . . - . - - - -. - - - . . 07-27053 Calculations Hazardous Materials Occupancy F me Reacti ra ons-Factored L d C at F oa ases rame C oss S fon· 6 r CCI XMLoc 01010 531010 Gridl -Grid2 6-D 6-A Ld Dcscr:ip!ion Hx Vv Hx Vv Cs application factor not shown k k) (k) (k) I D+AD+CG+S 13.4 58.9 -13.4 53.9 2 D+AD+CG+USl* 12.4 43.3 -12.4 61.9 . 3 D + AD+CG+ *US! 12.4 66.8 -12.4 38.3 . 4 D +AD+ CG +WI> -3.3 8.7 -8.2 I 1.4 . 5 D+AD+CG+<Wl 8.2 16.4 3.3 3.7 . 6 D+AD+CG+W2> ·4.7 12.5 -6.8 15.2 . 7 D+AD+CG+<W2 6.8 20.2 4.7 7.5 . 8 D+ AD+CG +S +WI> 5.8 40.4 -14.4 41.2 . 9 D+ AD+CG+S +<WI 14.4 46.1 -5.8 35.4 . . 10 D+AD+CG+S+W2> 4.7 43.2 -13.4 44.0 . II D+AD+CG+S+<W2 13.4 49.0 -4.7 38.3 . . 12 D+AD+CG+*AL> 3.6 30.6 -5.5 20.4 . - 13 D+AD+CG+AL*> 3.6 23.4 -5.5 27.6 -- 14 D +AD +CG+<*AL 5.5 32.6 -3.6 18.4 -. IS D +AD +CG+<AL* 5.5 25.3 -3.6 25.7 . - 16 D+AD+CU+Wi> -5.6 -5.6 -6.0 2.1 -- 17 D+AD+CU+<Wl 6.0 2.1 5.6 -5.6 . - 18 D+AD+CU+W2> -7.0 -1.8 -4.6 5.9 . - 19 D+AD+CU+<W2 4.6 5.9 7.0 -1.8 -- 20 D+AD+CG+S+*AI> 9.1 49.6 -10.5 40.7 -- 21 D+AD+CG+S+AL*> 9.1 44.2 -10.5 46.2 -- 22 D+AD+CG+S+<*AL 10.5 51.1 -9.1 39.2 . - 23 D+AD+CG+S+<AL* 10.5 45.7 -9.1 44.7 -- 24 D+AD+CG+Wl>+*AL> 1.0 23.6 -6.7 17.6 -- 25 D+AD+CG+Wl>+AL*> 1.0 18.2 -6.7 23.1 -- 26 D+AD+CG.+<Wl+<*AL 6.7 28.0 -1.0 13.2 -- 27 D+AD+CG+<Wl+<AL* 6.7 22.5 -1.0 18.7 . - 28 D+AD+CG+W2>+*AL> 0.5 25.1 -6.2 19.0 -- 29 D + AD+CG + W2>+AL*> 0.5 19.6 -6.2 24.5 -- 30 D+AD+CG+<W2+<*AL 6.2 29.4 -0.5 14.7 -- 31 D +AD +CO +<W2+<AL* 6.2 24.0 -0.5 20.1 -- 32 D+AD+CG+S+E>+EG+ 1.9 23.4 -8.5 26.5 -- 33 D+AD+CG+S+<E+EG+ 8.8 31.8 -2.2 18.2 -- 34 D+AD+CU+E>+EG--2.1 1.2 -4.0 9.3 -- 35 D+AD+CU+<E+EG-4.3 9.0 1.8 . 1.5 -- 36 D+AD+CG+S+EB>+EG+ 5.3 27.6 -5.3 22.4 -- 37 D+AD+CU+EB>+EGw 1.1 5.1 -1.1 5.4 -- 38 D+AD+CG+S+<EB+EG+ 5.3 27.6 -5.3 22.4 -- 39 D+AD+CU+<EB+EG· 1.1 5.1 -1.1 5.4 -- 40 D+AD+CG+WPAl 6.0 12.7 -5.7 8.1 -- 41 D+AD+CG+S+WPAl 12.8 43.4 -12.5 38.7 -- 42 D+AD+CU+WPAI 3.8 -1.6 -3.5 -1.2 -- 43 D+AD+CG+WPAl+*AL+ALB> 5,2 25.9 -5.1 15.6 -- 44 D+AD+CG+WPAI+AL*+ALB> 5.2 20.4 -5.1 21.1 -- 45 D +AD +CG+ WPDl 5.7 10.7 ·5.2 6.3 - 46 D+AD+CG+S+WPDI 12.5 41.8 -12.1 37.3 . - 47 D+AD+CU+WPDI . 3.4 -3.6 -2.9 -3.1 . - 48 D+AD+CG+WPDl+*AL+<ALB 5.1 25.1 -4.9 14.9 -. 49 D+AD+CG+WPDI +AL *+<ALB 5.1 19.7 -4.9 20.4 . 50 D+AD+CG+WPA2 4.6 16.5 -4.3 11.9 51 D+AD+CG+S+WPA2 11.7 46.2 -11.5 41.6 52 D+AD+CU+WPA2 2.4 2.2 -2.1 2.6 - 53 D+AD+CG+WPA2+*AL+ALB> 4.7 27.3 -4.6 17.1 54 D+AD+CG+WPA2+AL *+ALB> 4.7 2 !.9 -4.6 22.5 . 55 D + AD+CG +WPD2 4.3 14.5 -3.8 10.1 - 56 D+AD+CG+S + WPD2 11.5 44.7 -11.1 40.2 - 57 D+AD+CU+WPD2 2.0 0.2 -1.5 0.8 - 58 D+AD+CG+WPD2+* AL +<ALB 4.5 26.6 -4.4 16.4 -- File: 7079 Chevron Rl_Stress Check 10_2008 wilh 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 43 of !75 . . . . - . . . - - - -. - - - - . -. - - - - - -. - - - - . - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 44 of 175 59 D+AD+CG+WPD2+AL *+<ALB 4.5 21.1 -4.4 21.8 . 60 D+AD+CG+WPBI 5.7 13.1 -6.0 7.8 . 61 D+AD+CG+S+WPBl 12.5 43.7 -12.8 38.4 . . 62 D+AD+CU+WPBI 3.5 -1.2 -3.8 -1.6 . . 63 D+AD+CG+WPB I +*AL+ALB> 5.1 26.0 -5.2 15.5 . 64 D+AD+CG+WPB I +AL *+ALB> 5.1 20.6 -5.2 20.9 . 65 D+AD+CG+WPCI 5.2 11.2 -5.7 5.7 . . 66 D +AD+ CG + S + WPCI 12.1 42.3 -12.5 36.9 . . 67 D+AD+CU+WPCl 2.9 -3.1 -3.4 -3.6 . 68 D+AD+CG+WPC!+*AL+<ALB 4.9 25.3 -5.1 14.7 . . 69 D+AD+CG+WPCI+AL*+<ALB 4.9 19.9 -5.1 20.2 . 70 D+AD+CG+WPB2 4.3 16.9 -4.6 11.6 . . . 71 D+AD+CG +S +WPB2 11.5 46.5 -11.7 41.3 . . 72 D+AD+CU+WPB2 2.1 2.6 -2.4 2.2 . . 73 D+AD+CG+WPB2+*AL+ALB> 4.6 27.5 -4.7 16.9 . . . 74 D+AD+CG+WPB2+AL *+ALB> 4.6 22.0 -4.7 22.4 . . 75 D+AD+CG+WPC2 3.8 15.0 -4.3 9.5 . . 76 D+AD+CG+S+WPC2 1I.I 45.1 -11.5 39.8 . . 77 D+AD+CU+WPC2 1.5 0.8 -2.0 0.2 . . . 78 D+AD+CG+WPC2+*AL+<ALB 4.4 26.8 -4.5 16.2 . . . 79 D+AD+CG+WPC2+AL*+<ALB 4.4 21.3 -4.5 21.6 . . . 80 D+AD+CG +S+ALB> 13.4 58.9 -13.4 53.9 . . 81 D +AD +CG+*AL+ALB> 4.5 31.6 -4.5 19.4 . . . . 82 D+AD+CG+AL*+ALB> 4.5 24.3 -4.5 26.7 . . . 83 D+AD+CG+S+*AL+ALB> 9.8 50.4 -9.8 40.0 . . . 84 D+AD+CG+S+AL *+ALB> 9.8 44.9 -9.8 45.4 . . 85 D +AD +CG +S+<ALB 13.4 58.9 -13.4 53.9 . . . 86 D + AD+ CG+* AL+<ALB 4.5 31.6 -4.5 19.4 . . . 87 D +AD + CG+AL *+<ALB 4.5 24.3 -4.5 . 26.7 . . . 88 D+AD+CG+S+* AL+<ALB 9.8 50.4 -9.8 40.0 . . . 89 D+AD+CG+S+AL*+<ALB 9.8 44.9 -9.8 45.4 . . . Maximum Combined Reactions Summary with Factored Loads~ Framin2: X~Loc Grid Hrz left Load Hrz Right Load Hrzin Load HrzOut Load Uplift Load Vtt Down Load Momcw Load Momccw Load (-Hx) Case (Hx) Case (·Hz) Case (Hz) Case (-Vy) Case (Vy) Case (-Mzz) Case (Mzz) Case (k) (k) (k) (k) (k) (k) (in-k) (in·k) 0/0/0 6-D 7.0 18 14.4 9 . . . . 5.6 16 66.8 3 . . . 53/0/0 6-A 14.4 8 7.0 19 . . . . 5.6 17 61.9 2 . . . . File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: !06/3/0 Frame ID:Rigid Frame Values shown are resisting forces of the foundation. Reactions· Unfactored Load Tvne at Frame Cross Section: 7 Type Exterior Column X~Loc 0/0/0 Gridl -Grid2 7-D Base Plate W x L (in.) 8 X 13 Base Plate Thickness (in.) 0.500 Anchor Rod Qty/Diam. (in.) 4-0.750 Column Base Elev. 100'-Q" Load Type Desc. Hx Hz vv D Frm 0.8 -4.3 AD Frm 0.1 -1.1 CG Fnn 2.6 -12.3 s Frm 9.8 -38.3 USl* Frm 8.8 22.7 *USl Frm 8.8 -46.2 WI> Frm -6.9 --I 1.9 <WI Frm 4.6 --4.3 W2> Frm -8.3 --8.1 <W2 Frm 3.2 --0.4 *AL> Frm -0.1 -10.0 AL*> Frm -0.1 -2.7 <"'AL Frm 1.8 -12.0 <AL* Frm 1.8 -4.7 cu Fnn 1.3 -5.1 E> Frm -4.2 --5.5 EG+ Frm 0.3 1.5 <E Frm 4.2 -5.5 EG-F1m -0.3 -1.5 EB> Brc 0.4 -16.2 -28.9 <EB Brc -0.3 32.3 WPAI Brc 2.6 -3.7 -14.1 'AL Frm 0.9 -11.0 ALB> Brc AL* Frm 0.9 3.7 WPD1 Bee 1.9 -2.9 <ALB Brc WPA2 Brc 1.2 -3.7 -10.3 WPD2 Brc 0.5 -0.9 WPBI Bee 2.3 -32 -13.0 WPC1 Bee 1.4 -3.2 WPB2 Bee 0.9 -3.2 -9.2 Frame Type: Rigid Frame Exterior Column 53/0/0 7-A 8 X 13 0.375 4-0.750 100'-0" Hx Hz Vv -0.8 -4.3 - -0.1 -1.1 - -2.6 -10.1 - -9.8 -38.3 - -8.8 -46.2 - -8.8 -22.7 - -4.6 --4.3 - 6.9 --11.9 - -3.2 --0.4 - 8.3 --8.1 - -1.8 -4.7 - -1.8 -12.0 - 0.1 -2.7 - 0.1 -10.0 -1.3 -5.1 - -4.1 5.5 - -0.3 -1.3 - 4.1 --5.5 - 0.3 -1.3 -0.4 -16.3 -29.1 0.3 -32.4 -2.3 -3.2 -13.0 - -0.9 -3.7 --- -0.9 11.0 - -1.4 --3.2 - --- -0.9 -3.2 -9.2 -0.0 0.6 -2.6 -3.7 -14.2 - -!.9 --2.9 -1.2 -3.7 -I 0.4 - File: 7079 Chevron R !_Stress Check I 0 _2008 with 08_2008 Loading - - - - - - - - - - - - - - - - - - - - - - - - - - Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 45 of 175 - - - - - - - - - - - - - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy WPC2 0.0 0.6 -0.5 0.9 Frame Reactions M Factored Load Cases at Frame Cross Section: 7 X·Loc 0/0/0 53/0/0 Grid! • Grid2 7-D 7-A Ld Description Hx Hz Vv Hx Hz Vv Cs aoolication factor not shown ik) (kl k Tk) k) Tk) I D+AD+CG+S !3.4 56.0 -13.4 53.8 2 D+AD+CG+USl* 12.4 40.4 -12.4 . 61.8 . . 3 D +AD+ CG + *USl 12.4 . 63.9 -12.4 38.3 . . 4 D +AD+ CG +WI> -3.4 5.8 -8.1 11.3 . . 5 D+AD+CG+<Wl 8.1 13.4 3.4 . 3.6 6 D+AD+CG+W2> -4.8 . 9.6 -6.7 . 15.1 . 7 D+AD+CG+<W2 6.7 17.3 4.8 -7.5 -- 8 D+AD+CG+ S +WI> 5.7 . 37.4 -14.3 4LI -- 9 D+AD+CG+S+<Wl 14.3 -43.2 -5.7 35.3 -- 10 D+AD+CG+S+W2> 4.6 -40.3 -13.3 -43.9 - II D+AD+CG+S+<W2 13.3 46.1 -4.6 -38.2 - 12 D +AD +CG+*AI> 3.5 27.7 -5.4 -20.3 -- 13 D+AD+CG+AL"'> 3.5 20.4 -5.4 -27.6 -- 14 D +AD+ CG+<*AL 5.4 -29.7 -3.5 -18.3 - IS D+AD+CG+<AL* 5.4 -22.4 ~3.5 -25.6 - 16 D +AD+ CU +WI> -5.6 --5.6 -6.0 -2.1 -- 17 D+AD+CU+<Wl 6.0 2.1 5.6 --5.6 -. 18 D+AD+CU+W2> -7.0 --1.8 -4.6 -5.9 - 19 D+AD+CU+<W2 4.6 -5.9 7.0 --1.8 -- 20 D+AD+CG+S+*AL> 9.0 -46.7 -10.4 -40.6 -- 21 D +AD+ CG + S+AL"'> 9.0 -41.3 -10.4 -46.1 - 22 D+AD+CG+S+<*AL 10.4 -48.2 -9.0 -39.2 - 23 D+AD+CG+S+<AL* 10.4 -42.8 -9.0 -44.6 -- 24 D+AD+CG+Wl>+*AL> 0.9 -20.7 -6.6 -17.5 -- 25 D+AD+CG+Wl>+AL*> 0.9 -15.3 -6.6 -23.0 -- 26 D+AD+CG+<Wl+<*AL 6.6 -25.1 -0.9 -13.2 -- 27 D+AD+CG+<Wl+<AL* 6.6 -19.6 -0.9 -18.6 -- 28 D +AD+ CG + W2>+* AL> 0.4 -22.2 -6.1 -18.9 - 29 D+AD+CG+W2>+AL*> 0.4 -16.7 -6.1 -24.4 -- 30 D +AD+ CG+<W2+<*AL 6.1 -26.5 -0.4 -14.6 -- 31 D+AD+CG+<W2t<AL* 6.1 -21.1 -0.4 -20.0 -- 32 D+~G+S+E>+EG+ 2.1 -20.4 -8.3 -26.4 -- 33 D+AD+CG+S+<EfEG+ 8.4 -28.6 -2.2 -18.1 - 34 D+AD+CU+E>+EG~ -1.8 -1.4 -4.0 -9.2 -- 35 D+AD+CU+<E+EG~ 4.1 -9.1 1.7 -1.5 -- 36 D+AD+CG+S+EB>+EG+ 5.6 -12.2 2.8 -5.6 -12.2 0.5 -- 37 D+AD+CU+EB>+EG~ 1.4 -11.4 -15.0 -1.4 -I 1.4 -15.0 -- 38 D+AD+CG+S+<EB+EG+ 5.0 -48.8 -5.0 -46.5 - 39 D+AD+CU+<EB+EG~ 0.9 -27.9 -0.9 -28.0 - 40 D+AD+CG+WPAI 6.1 -3.7 3.6 -5.8 -3.2 2.6 -- 41 D+AD+CG+S+WPAl 12.8 -2.8 35.8 -12.6 -2.4 34.5 - 42 D+AD+CU+WPAl 3.9 -3.7 -7.8 -3.6 -3.2 -6.7 - 43 D+AD+CG+WPAI+*AL+ALB> 5.2 -1.4 20.6 -5.1 -1.2 13.5 . 44 D+AD+CG+WPAI+AL*+ALB> 5.2 -1.4 15.2 -5.1 -1.2 18.9 - 45 D+AD+CG+WPDI s.s 14.8 -5.0 -12.3 - 46 D+AD+CG+S+WPDl 12.3 -44.2 -12.0 41.9 -- 47 D+AD+CU+WPDI 3.3 -3.4 -2.8 -3.1 . 48 D+AD+CG+WPDI+*AL+<ALB 4.9 -24.8 -4.8 -17.2 -- 49 D+AD+CG+WPDl+AL"'-I<ALB 4.9 -19.4 -4.8 -22.6 -- so D+AD+CG+WPA2 4.7 -3.7 7.4 -4.4 -3.2 6.4 . 51 D+AD+CG +S+WPA2 I 1.8 -2.8 38.6 -11.6 -2.4 37.4 52 D +AD +CU + WPA2 2.5 -3.7 -4.0 -2.2 -3.2 -2.9 - 53 D+AD+CG+WPA2+*AL+ALB> 4.7 ~1.4 22.1 ~45 -1.2 14.9 54 D+AD+CG+WPA2+AL *+ALB> 4.7 -1.4 16.6 -45 -1.2 20.4 55 D+AD+CG+WPD2 4.1 18.6 -3.6 -16.2 56 D + AD+CG +S + WPD2 11.3 -47.1 -10.9 44.7 57 D+AD+CU+WPD2 1.9 -7.2 ~1.4 6.9 58 D+AD+CG+WPD2+*AL+<ALB 4.4 26.3 -4.2 . 18.6 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 46 of 175 . . . . . - - . - - - - - - - - - - - - - - - - - - - - --- - - - - - - - - - - - - - - . . - . - - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 47 of 175 59 D+AD+CG+WPD2+AL *+<ALB 4.4 20.8 -4.2 24.0 60 D+AD+CG+WPBI 5.8 -3.2 4.7 -6.1 -3.7 1.4 - 61 D+AD+CG+S+WPBl 12.6 -2.4 36.6 -12.8 -2.8 33.7 -- 62 D+AD+CU+WPBI 3.6 -3.2 -6.7 -3.9 -3.7 -7.8 63 D+AD+CG+WPBl+*AL+ALB> 5.1 -1.2 21.! -5.2 -1.4 13.1 - 64 D+AD+CG+WPBl+AL*+ALB> 5.1 -1.2 15.6 -5.2 -1.4 18.5 65 D+AD+CG+WPC! 5.0 -!4.5 -5.5 12.7 - 66 D+AD +CG +S +WPCI 12.0 -44.0 -12.3 42.1 - 67 D+AD+CU+WPCI 2.8 3.1 -3.3 3.4 - 68 D+AD+CG+WPCI+*AL+<ALB 4.8 -24.7 -4.9 -17.3 - 69 D+AD+CG+WPC I +AL *+<ALB 4.8 -19.3 -4.9 22.7 -- 70 D +AD+ CG +'WPB2 4.4 -3.2 8.5 -4.7 -3.7 5.2 - 71 D+AD+CG+S+WPB2 11.6 -2.4 39.5 -11.8 -2.8 36.5 72 D+AD+CU+WPB2 2.2 -3.2 -2.9 -2.5 -3.7 -4.0 - 73 D+AD+CG+WPB2+*AL+ALB> 4.5 -1.2 22.5 -4.7 -1.4 14.5 --- 74 D+AD+CG+WPB2+AL*+ALB> 4.5 -1.2 17.1 -4.7 -1.4 19.9 -- 75 D+AD+CG+WPC2 3.6 -18.3 -4.1 -16.5 --- 76 D+AD+CG+S+WPC2 10.9 -46.8 -11.3 -44.9 -- 77 D+AD+CU.+WPC2 1.4 -6.9 -!.9 -7.2 --- 78 D+AD+CG+WPC2+*AL+<ALB 4.2 -26.2 -4.4 -,!8.7 -- 79 D+AD+CG+WPC2+AL*+<ALB 4.2 -20.7 -4.4 24.2 --- 80 D+AD+CG+S+ALB> 13.4 -56.0 -13.4 53.8 --- 81 D+AD+CG+*AL+ALB> 4.4 28.7 -4.4 19.3 --- 82 D +AD + CG+AL *+ALB> 4.4 -2!.4 -4.4 -26.6 --- 83 D+AD+CG+S+*AL+ALB> 9.7 -47.5 -9.7 -39.9 --- 84 D+AD+CG+S+AL*+ALB> 9.7 -42.0 -9.7 -45.3 --- 85 D +AD+ CG + S+<ALB 13.4 -56.0 -!3.4 -53.8 --- 86 D +AD + CG+* AL +<ALB 4.4 -28.7 -4.4 -19.3 --- 87 D+AD+CG+AL*+<ALB 4.4 -21.4 -4.4 -26.6 --- 88 D+AD+CG+S+*AL+<ALB 9.7 -47.5 -9.7 -39.9 --- 89 D+AD+CG+S+AL*+<ALB 9.7 -42.0 -9.7 -45.3 --- Maximum Combined Reactions Summary with Factored Loads~ Framin~ X~Loc Grid Hrz left Load Hrz Right Load Hrzln Load Hrz Out Load Uplift Load VrtDOwn Load Molncw Load Moin ccw Load (-Hx) Case <:;;;) <:;ase (-Hz) Case (Hz) Case (-Vy) Case (Vy) Case (-Mzz) Case (Mzz) Case . (k) '(k) (k) (kl rkl (in-k) (in-k) 01010 7-D 7.0 18 14.3 9 12.2 36 --15.0 37 63.9 3 -- - - 53/0/0 7-A 14.3 8 7.0 19 12.2 36 --!5.0 37 6!.8 2 - - -- Bracine X~Loc Grid Description 01010 7-D Diagonal bracing at base is attached to column. Reactions ARE included with frame reactions. 53/0/0 7-A Diagonal bracing at base is attached to column. Reactions ARE included with frame reactions. File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: 12419/0 Frame ID:Rigid Frame y Values shown are resisting forces of the foundation. Reactions~ Unfactored Load Tvoe at Frame Cross Section: 8 Type Exterior Column X~Loc 0/0/0 Grid! -Grid2 8-D Base Plate W x L (in.) 9x 13 Base Plate Thickness (in.) 0.500 Anchor Rod Qty/Diam. (in.) 4-1.000 Column Base Elev. 100'~0" Load Type Desc. Hx Hz Vy D Frm 0.8 -4.3 AD Frm 0.1 -!.1 CG Fnn 2.6 -12.0 s Fnn 9.8 -38.3 US!* Frm 8.8 -22.7 *USl Frm 8.8 -46.2 WI> Frm -6.9 --12.0 <WI Frm 4.6 --4.3 W2> Frm -8.3 --8.1 <W2 Frm 3.2 --0.4 *AL> Frm -0.1 -10.0 AL*> Frm -0.1 -2.7 <*AL Frm 1.8 -12.0 <AL* Frm 1.8 -4.7 cu Frm !.3 -5.1 E> Frm -4.2 --5.5 EG+ Frm 0.3 -1.5 <E Frm 4.2 5.5 EO-Fnn -0.3 -1.5 EB> BrC -0.3 -0.0 29.0 <EB Brc 0.5 19.3 -32.4 WPAI Brc 2.4 --1.0 'AL Fnn 0.9 -11.0 ALB> Brc --- AL' Frm 0.9 3.7 WPDI Brc 2.1 4.4 -17.6 <ALB Brc - - WPA2 Brc 1.0 -2.8 WPD2 Brc 0.7 4.4 -13.8 WPBI Brc 2.1 -1.5 WPCI Brc 1.6 3.8 -16.1 WPB2 Brc 0.7 -2.3 Frame Type: Rigid Frame ® Vy Exterior Column 53/0/0 8-A 9x 13 0.500 4-1.000 100'~0" Hx Hz Vy -0.8 -4.3 - -0.1 -!.1 - -2.6 -10.1 - -9.8 -38.3 - -8.8 -46.2 - -8.8 -22.7 - -4.6 --4.3 - 6.9 --12.0 - -3.2 --0.4 - 8.3 --8.1 -1.8 -4.7 - -1.8 -12.0 0.1 -2.7 - 0.1 -10.0 - -1.3 -5.1 - -4.1 -5.5 - -0.3 -1.3 - 4.1 --5.5 - 0.3 --1.3 0.3 -0.0 29.0 - -0.5 19.3 -32.3 - -2.1 --1.5 - -0.9 -3.7 - -- -0.9 -11.0 - -1.6 3.8 -16.1 - -- -0.7 2.3 - -0.2 3.8 -12.3 -2.4 --1.0 - -2.1 4.4 -17.6 -1.0 2.8 File: 7079 Chevron Rl_StTess Check 10_2008 with 08_2008 Loading - - --- - - - - - - - - - Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 48 of 175 -- - - - - --- - - - - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy WPC2 o.2 38 1-12.3 I -o1 4.4 l-13.s I F rame R ti eac ons-F t dL dC ac ore oa ases a IF rame c s t' 8 ross ec wn: X-Loc 01010 5310/0 Grid 1 -Grid2 8-D 8-A Ld Description Hx Hz Vv Hx Hz Vv Cs (aoolication factor not shown (k k lk1 lk) lk kl I D+AD+CG+S 13.3 55.7 -13.3 . 53.8 . 2 D+AD+CG+USJ* 12.3 . 40.1 -12.3 61.7 . . 3 D+AD+CG+*USJ 12.3 63.6 -12.3 . 38.2 . . 4 D+AD+CG+W!> -3.4 5.5 -8.1 11.3 . . 5 D+AD+CG+<Wl 8.1 13.2 3.4 . 3.6 . . 6 D+AD+CG+W2> -4.8 9.3 -6.7 . 15.1 . 7 D+AD+CG+<W2 6.7 17.0 4.8 7.4 . . 8 D +AD+ CG + S +WI> 5.7 . 37.2 -14.3 .. 4\.l -- 9 D+AD+CG+S+<Wl 14.3 42.9 -5.7 35.3 -- 10 D+AD+CG+S+W2> 4.6 40.0 -13.3 -43.9 -- II D+AD+CG+S+<W2 13.3 -45.8 -4.6 -38.1 -- 12 D +AD+ CG+*AI> 3.5 27.4 -5.4 -20.3 -- 13 D+AD+CG+AL*> 3.5 20.2 -5.4 . 27.5 -- 14 D +AD+ CG+<*AL 5.4 -29.4 -3.5 -18.3 -- 15 D+AD+CG+<AL* 5.4 -22.1 -3.5 -25.6 -- 16 D+AD+CU+Wi> -5.6 -5.6 -6.0 -2.1 -- 17 D+AD+CU+<Wl 6.0 -2.1 5.6 --5.6 -- 18 D+AD+CU+W2> -7.0 . -1.8 -4.6 -5.9 -- 19 D+AD+CU+<W2 4.6 . 5.9 7.0 --1.8 -- 20 D +AD+ CG + S+*AI> 9.0 -46.5 -10.4 -40.6 -- 21 · D+AD+CG+S+AL*> 9.0 -41.0 -10.4 -46.1 -- 22 D+AD+CG+S+<*AL 10.4 -47.9 -9.0 -39.1 -- 23 D+AD+CG+S+<AL* 10.4 -42.5 -9.0 -44.6 -- 24 D+AD+CG+Wl>+*AI> 0.9 -20.5 -6.6 -17.5 -- 25 D +AD+ CG + Wl>+AL"'> 0.9 -15.0 -6.6 . 22.9 -- 26 D+AD+CG +<Wl+<*AL 6.6 24.8 -0.9 -13.1 . - 27 D+AD+CG+<Wl+<AL* 6.6 -19.4 -0.9 -18.6 -- 28 D+AD+Cd+W2>+*AL> 0.4 -21.9 -6.1 -18.9 -- 29 D+AD+CG+W2>+AL*> 0.4 -16.4 -6.1 -24.4 -- 30 D+AD+CG+<W2+<01<AL 6.1 -26.2 -0.4 -14.6 -- 31 D+AD+CG+<W2+<AL* 6.1 20.8 -0.4 -20.0 -- 32 D+AD+CG+S+E>+EG+ 2.1 20.1 -8.3 -26.3 -- 33 D+AD+CG+S+<E+EG+ 8.4 28.3 -2.2 -18.1 -- 34 D+AD.+CU+E>+EG~ -1.8 -1.4 -4.0 -9.2 . - 35 D+AD+CU+<E+EG· 4.1 -9.1 1.7 -1.5 -- 36 D+AD+CG+S+EB>+EG+ 5.0 -0.0 46.0 -5.0 -0.0 44.0 -- 37 D+AD+CU+EB>+·EG~ 0.9 -0.0 25.6 -0.9 -0.0 25.7 - 38 D+AD+CG+S+<EB+EG+ 5.6 14.4 -0.1 -5.6 14.5 -2.0 - 39 D+AD+CU+<EB+EG· 1.5 13.5 -17.4 -1.5 13.5 -17.2 -- 40 D+AD+CG+WPAl 5.9 16.4 -5.7 -14.1 -- 41 D+AD+CG+S+WPAI 12.7 -45.4 -12.5 -43.1 - 42 D +AD+ CU + WPAl 3.8 -5.3 -3.5 4.9 -- 43 D+AD+CG+WPAJ+*AL+ALB> 5.1 -25.3 -5.0 17.8 -- 44 D+AD+CG+WPA l+AL*+ALB> 5.1 19.9 -5.0 23.2 -- 45 D+AD +CG + WPDJ 5.6 4.4 -0.2 -5.1 3.8 -0.5 . 46 D+AD+CG+S+WPD! !2.4 3.3 32.9 -12.1 2.9 32.2 . 47 D+AD+CU+WPDJ 3.5 4.4 -11.3 -2.9 3.8 -9.8 -- 48 D+AD+CG+WPD l +* AL +<ALB 5.0 1.6 19.1 -4.8 1.4 12.3 -- 49 D+AD+CG+WPDl+AL *+<ALB 5.0 1.6 13.6 -4.8 1.4 17.8 -- 50 D+AD+CG+WPA2 4.5 20.2 -4.3 -17.9 - 51 D+AD+CG+S+WPA2 11.6 48.2 -11.4 -46.0 -- 52 D +AD+ CU + WPA2 2.4 9.1 -2.1 -8.7 - 53 D+AD+CG+WPA2+*AL+ALB> 4.6 26.7 -4.5 -19.2 54 D+AD+CG+WPA2+AL*+ALB> 4.6 2\.J -4.5 -24.7 . 55 D+AD+CG+WPD2 4.2 4.4 3.6 -3.7 3.8 3.3 -- 56 D+AD+CG +S + WPD2 I !.4 3.3 35.8 -I \.0 2.9 35.0 - 57 D + AD+CU + WPD2 2.1 4.4 -7.5 -1.6 3.8 -6.0 -- 58 D+AD+CG+WPD2+* AL +<ALB 4.5 \.6 20.5 -4.3 \.4 13.7 -- File: 7079 Chevron R !_Stress Check I 0_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 49 pf !75 . . . . - - - - - -. - - - -. - - - - - - - - - - - - - - - - - - - - . - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 50 of 175 59 D+AD+CG+WPD2+AL *+<ALB 4.5 1.6 15.0 -4.3 1.4 19.2 - 60 D +AD+ CG + WPB1 5.7 16.0 -5.9 14.6 -- 61 D+AD+CG+S+WPBI 12.5 -45.0 -12.7 -43.5 - 62 D+AD+CU+WPBI 3.5 -4.8 -3.8 -5.3 -- 63 D+AD+CG+WPBJ+*AL+ALB> 5.0 -25.1 -5.1 18.0 -- 64 D+AD+CG+WPB l+AL *+ALB> 5.0 19.7 -5.1 -23.4 65 D +AD+ CO+ WPCl 5.1 3.8 1.3 -5.6 4.4 -2.1 66 D +AD+ CO+ S + WPCI 12.1 2.9 34.0 -12.4 3.3 31.0 -- 67 D +AD +,CU + WPCI 2.9 3.8 -9.8 -3.5 4.4 -11.3 - 68 D+AD+CG+WPCI+*AL+<ALB 4.8 1.4 19.6 -5.0 1.6 11.7 -- 69 D+AD+CG+WPCl+AL*+<ALB 4.8 1.4 14.2 -5.0 1.6 17.2 --- 70 D+AD+CG+WPB2 4.3 -19.8 -4.5 -18.4 -- 71 D+AD+CG+S+WPB2 11.4 -47.9 -11.6 46.4 - 72 D+AD+CU+WPB2 2.1 -8.7 -2.4 -9.1 - 73 D+AD+CG+WPB2+*AL+ALB> 4.5 -26.6 -4.6 -19.4 --- 74 D+AD+CG+WPB2+AL *+ALB> 4.5 -21.1 -4.6 24.9 -- 75 D+AD+CG+WPC2 3.7 3.8 5.1 -4.2 4.4 1.8 - 76 D+AD+CG+S+WPC2 11.0 2.9 36.9 -11.4 3.3 33.9 -- 77 D+AD+CU+WPC2 1.6 3.8 -6.0 -2.1 4.4 -7.5 --- 78 D+AD+GG+WPC2+*AL+<ALB 4.3 1.4 21.1 -4.5 1.6 13.2 --- 79 D+AD+CG+WPC2+AL*+<ALB 4.3 1.4 15.6 -4.5 1.6 18.6 -- 80 D+AD+CG+S+ALB> 13.3 -55.7 -13.3 -53.8 --- 81 D+AD+CG+*AL+ALB> 4.4 -28.4 -4.4 -19.3 --- 82 D +AD+ CG+AL *+ALB> 4.4 -21.2 -4.4 -26.5 --- 83 D+AD+CG+S+*AL+ALB> 9.7 -47.2 -9.7 39.9 --- 84 D+AD+CG+S+AL *+ALB> 9.7 -41.7 -9.7 -45.3 -- 85 D+AD+CG+S+<ALB 13.3 -55.7 -13.3 -53.8 --- 86 D +AD+ CG+*AL+<ALB 4.4 -28.4 -4.4 -19.3 --- 87 D +AD + CG+AL *+<ALB 4.4 -21.2 -4.4 -26.5 --- 88 D+AD+CG+S+*AL+<ALB 9.7 -47.2 -9.7 -39.9 --- 89 D+AD+CG+S+AL*+<ALB 9.7 -41.7 -9.7 -45.3 --- Maximum Combined Reactions Summary with Factored Loads~ Framing XMLoc Grid Hrz left Load Hrz Right Load Hrzln Load HrzOut Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-~~) Case <:;:;) Case (-~~) Case (Hz) Case (-Vy) .(k). . (kl. Case (~) Case (-Mzz) (in-ki Case (Mzz) {in-kl Case 0/0/0 8-D 7.0 18 14.3 9 0.0 36 14.4 38 17.4 39 63.6 3 -- - - 53/0/0 8-A 14.3 8 7.0 19 0.0 36 14.5 38 17.2 39 61.7 2 - - - - Bradne X~Loc Grid Descrjption 0/0/0 8-D Diagonal bracing at base is attached to column. Reactions ARE included with frame reactions. 53/0/0 8-A Diagonal bracing at base is attached to column. Reactions ARE included with frame reactions. File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Wall: 4, Frame at: 144/9/0 Frame ID:Rigid Frame Values shown are resisting forces of the foundation. Reactions-Unfactored Load Tvne at Frame Cross Section: 9 Type Exterior Column X-Loc 0/0/0 Gridl -Grid2 9-D Base Plate W x L (in.) 8x 13 Base Plate Thickness (in.) 0.375 Anchor Rod Qty/Diam. (in.) 4-0.750 Column Base Elev. 100'-0" Load Tvoe Desc. Hx Vv D Fnn 0.7 3.8 AD Fnn 0.1 0.8 CG Fnn 1.9 9.4 s Fnn 7.3 28.6 USl* Fnn 6.5 16.9 *USI Fnn 6.5 34.5 WI> Fnn -6.3 -10.4 <WI Fnn 4.0 -3.5 W2> Fnn -7.3 -7.6 <W2 Fnn 2.9 -0.7 'AI> Fnn -0.1 10.0 AL*> Fnn -0.1 2.7 <*AL Fnn 1.8 12.0 <AL* Fnn 1.8 4.7 cu Frm 1.0 3.8 E> Frm -3.3 -4.2 EG+ Fnn 0.3 1.2 <E Frm 3.3 4.2 EG-Fnn -0.3 -1.2 EB> Brc - <EB Brc -- WPAI Brc 1.8 -5.7 'AL Frm 0.9 11.0 ALB> Brc - AL' F1m 0.9 3.7 WPDI Brc 1.5 -7.7 <ALB Brc - WPA2 Brc 0.8 -2.8 WPD2 Brc 0.4 -4.8 WPBl Brc 1.6 -5.4 WPCI Brc !.I -7.2 WPB2 Brc 0.6 -2.6 Frame Type:Rigid Frame Exterior Column 53/010 9-A 8x 13 0.375 4-OJ. 50 100 -0" Hx Hz Vv -0.7 -3.8 - -0.1 -0.8 - -1.9 7.5 - -7.3 28.6 -6.5 -34.5 - -6.5 -16.9 -4.0 --3.5 - 6.3 --10.4 - -2.9 -.(),7 - 7.3 --7.6 - -1.8 -4.7 - -1.8 12.0 - 0.1 2.7 - 0.1 10.0 -1.0 3.8 -3.2 4.2 -0.3 1.0 3.2 -4.2 0.3 -1.0 -0.0 -1.6 -5.4 -0.9 -3.7 - - -0.9 -11.0 -1.1 --7.2 -- -0.6 -2.6 -0.1 -4.4 -1.8 -5.7 -L5 --7.7 -0.8 -2.8 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading - - - - ---- - - - - - - - - - - - Version: ?.Ia Date: 10/20/2008 Time: I :57:43 PM Page: 51 of 175 - - --- - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy WPC2 Brc 0.1 -4.4 -04 I -4.8 I Frame Reactions Factored Load Cases at Frame Cross Section-9 - X-Loc 0/010 531010 Grid 1 -Grid2 9-D 9-A Ld Description Hx Vv Hx Hz Vv Cs (application factor not shovm) lk) k k lk lk\ 1 D+AD+CG+S 10.0 42.6 -10.0 -40.7 - 2 D+AD+CG+USI"' 9.2 30.9 -9.2 46.6 - 3 D+AD+CG+*USl 9.2 48.5 -9.2 29.0 - 4 D+AD+CG+W!> -3.6 3.6 -6.7 8.6 - 5 D+AD+CG+<WI 6.7 10.5 3.6 1.7 -- 6 D+AD+CG+WZ> -4.6 6.4 -5.6 11.4 7 D+AD+CG+<WZ 5.6 13.3 4.6 -4.5 -- 8 D+AD+CG+S+Wl> 3.4 27.6 -11.1 -30.9 -- 9 D+AD+CG+S+<Wl 11.1 32.8 -3.4 25.7 -- 10 D+AD+CG+S+WZ> 2.7 29.7 -10.3 33.0 - 11 D+AD+CG+S+<W2 10.3 34.9 -2.7 27.9 -- 12 D +AD+ CG+*AL> 2.6 24.0 -4.5 -16.8 -- 13 D+AD+CG+AL*> 2.6 16.7 -4.5 24.1 -- 14 D+AD+CG+<*AL 4.5 26.0 -2.6 -14.9 -- 15 D +AD +CG+<AL* 4.5 18.7 -2.6 -22.1 -- 16 D+AD+CU+WI> -5.2 -5.4 -5.0 1.5 -- 17 D+AD+CU+<Wl 5.0 1.5 5.2 --5.4 -- 18 D+AD+CU+W2> -6.2 -2.5 -4.0 -4.3 -- 19 D+AD+CU+<W2 4.0 4.3 6.2 --2.5 -- 20 D+AD+CG+S+*AI> .. 6.7 37.6 -8.2 -31.7 - 21 D+AD+CG+S+AL*> 6.7 32.1 -8.2 37.2 -- 22 D+AD+CG+S+<*AL 8.2 39.0 -6.7 30.2 -- 23 D+AD+CG+S+<AL* 8.2 33.6 -6.7 -35.7 -- 24 D+AD+CG+Wl>+*Al> 0.3 17.6 -5.6 -14.3 -- 25 D+AD+CG+Wl>+AL*> 0.3 12.1 -5.6 -19.8 -- 26 D+AD+CG+<WI+<*AL 5.6 21.6 -0.3 -10.3 -- 27 D+AD+CG+<VVl+<AL* 5.6 16.2 -0.3 -15.7 -- 28 D +AD +CG + W2>+*AL> -0.1 18.7 -5.2 -15.4 -- 29 D+AD+CG+WZ>+AL*> -0.1 13.2 -5.2 -20.8 -- 30 D+AD+CG+<W2+<*AL 5.2 22.7 0.1 -11.3 -- 31 D +AD+ CG + <W2+<AL * 5.2 17.3 0.1 -16.8 -- 32 D+AD+CG+S+E>+EG+ 1.5 15.9 -6.4 -20.3 -- 33 D+AD+CG+S+<E+EG+ 6.4 22.3 -1.6 -13.9 -- 34 D+AD+CU+E>+EGw -1.4 1.3 -3.1 -7.3 -- 35 D+AD+CU+<E+EGw 3.2 7.2 1.3 -1.4 -- 36 D+AD+CG+S+EB>+EG+ 4.0 19.1 -4.0 -0.0 17.1 -- 37 D+AD+CU+EB>+EGw 0.9 4.2 -0.9 -0.0. 4.3 -- 38 D+AD+CG+S+<EB+EG+ 4.0 19.1 -4.0 17.1 -- 39 D+AD+CU+<EB+EG· 0.9 4.2 -0.9 4.3 -- 40 D+AD+CO"+WPAl 4.5 8.3 -4.3 -6.7 -- 41 D+AD+CG+S+WPAl 9.5 31.2 -9.4 -29.5 - 42 D+AD+CU+WPAI 2.9 -0.6 -2.7 -0.4 -- 43 D+AD+CG+WPAI+*AL+ALB> 4.1 20.1 -4.0 -12.9 - 44 D+AD+CG+WPAI+AL*+ALB> 4.1 14.7 -4.0 18.3 - 45 D+AD+CG+WPDl 4.2 6.3 -3.8 4.9 -- 46 D+AD+CG +S+WPDl 9.3 29.7 -9.0 28.1 -- 47 D+AD+CU+WPD! 2.6 -2.6 -2.2 -2.2 -- 48 O+AD+CG+WPDI+*AL+<ALB 3.9 19.4 -3.8 -12.2 -- 49 D+AD+CG+WPDl+AL*+<ALB 3.9 13.9 -3.8 -17.6 so D+AD+CG+WPA2 3.5 11.2 -3.3 9.5 -- 51 D+AD+CG+S+WPA2 8.7 33.3 -8.6 -31.6 - 52 D + AD+CU+ WPA2 1.9 2.2 -1.7 2.5 -- 53 D+AD+CG+WPA2+*AL+ALB> 3.7 21.2 -3.6 -13.9 - 54 D+AD+CG+WPA2+AL*+ALB> 3.7 15.7 -3.6 -19.4 -- 55 0 +AD +CG +WPD2 3.1 9.2 -2.8 -7.7 56 D+AD+CG+S+WPD2 8.5 31.8 -8 2 30.3 57 D+AD+CU+WPD2 1.5 0.2 -1.1 0.7 - 58 D+AD+CG+WPD2+*AL+<ALB 3.5 20.4 -3.4 13.3 -- File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 52 of 175 - - - - - - - - - - - - - - - - - - - - - - - - - - ' - - - - - - - - - - - - - - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 53 of 175 59 D+AD+CG+WPD2+AL *+<ALB 3.5 15.0 -3.4 18.7 - 60 D+AD+CG+WPBl 4.3 8.6 -4.5 6.4 - 61 D+AD+CG+S+WPB1 9.4 31.4 -9.5 29.3 -- 62 D +AD+ CU + WPB1 2.7 -0.4 -2.9 --0.6 - 63 D+AD+CG+WPB I +*AL+ALB> 4.0 20.2 -4.1 12.8 64 D+AD+CG+WPB l+AL *+ALB> 4.0 14.8 -4.1 18)2 - 65 D+AD+CG+WPCI 3.8 6.8 -4.2 4.4 - 66 D +AD+ CO+ S + WPCI 9.0 30.0 -9.3 27.8 -- 67 D+AD+CU+WPCI 2.2 -2.2 -2.6 -2.6 - 68 D+AD+CG+WPCI+*AL+<ALB 3.8 19.5 -3.9 12.0 69 D+AD+CG+WPCI+AL*+<ALB 3.8 14.1 -3.9 17.5 - 70 D+AD+CG+WPB2 3.3 11.4 -3.5 9.3 - 71 D+AD+CG+S+WPB2 8.6 33.5 -8.7 31.4 72 D+AD+CU+WPB2 1.7 2.5 -1.9 -2.2 -- 73 D+AD+CG+WPB2+*AL+ALB> 3.6 21.3 -3.7 -13.8 -- 74 D+AD+CG+WPB2+AL*+ALB> 3.6 15.8 -3.7 -19.3 -- 75 D+AD+CG+WPC2 2.8 9.6 -3.1 -7.3 - 76 D+AD+CG+S+WPC2 8.2 32.1 -8.5 -29.9 -- 77 D+AD+CU+WPC2 1.! 0.7 -1.5 -0.2 --- 78 D+AD+CG+WPC2+*AL-kALB 3.4 20.6 -3.5 -13.1 --- 79 D+AD+CG+WPC2+AL*+<ALB 3.4 15.1 -3.5 -18.5 --- 80 D +AD + CG + S+ALB> 10.0 42.6 -10.0 -40.7 --- 81 D +AD+CG+*AL+ALB> 3.6 25.0 -3.6 -15.8 --- 82 o·+AD+CG+AL*+ALB> 3.6 17.7 -3.6 23.1 -- 83 D+AD+CG+S+* AL +ALB> 7.5 38.3 -7.5 -31.0 --- 84 D+AD+CG+S+AL*+ALB> 7.5 32.9 -7.5 -36.4 -- 85 D +AD + CG + S+<ALB 10.0 42.6 -10.0 -40.7 --- 86 D +AD+ CG+*AL+<ALB 3.6 25.0 -3.6 -15.8 -- 87 D+AD+CG+AL*+<ALB 3.6 17.7 -3.6 -23.1 . . - 88 D+AD+CG+S+* AL+<ALB 7.5 38.3 -7.5 . 31.0 . . . 89 D+AD+CG+S+AL "'+<ALB 7.5 32.9 -7.5 . 36.4 . . . 0 Maximum Combined Reactions Summarv with Factored Loads-Framlmz X-Loc Grid Hrz left Load Hrz Right Load Hrzln Load HrzOut Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-Hx) Case (:t) Case (·Hz) Case (Hz) Case (-~i) Case (Vy) Case (-Mzz) Case (Mzz) Case 'nd· • (k). fk) • fk) lin-kl Cin-kl 0/0/0 9-D 6.2 18 I !.I 9 . . -. 5.4 16 48.5 3 . . -. 53/0/0 9-A 11.1 8 6.2 19 0.0 36 --5.4 17 46.6 2 . . -. File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM 54 of 175 Wall: 4, Frame at: 153/6/0 Frame ID:Rigid Frame with Endposts Frame Type:Rigid Frame, End Posts y Vy Vy Vy Values shown are resisting forces of the foundation. Reactions-U L S . 0 nfactored oad Tvne at Frame Cross ect•on: 1 Type Exterior Column Interior Column Interior Column Exterior Column X-Loc 0/0/0 I5/0/0 38/0/0 531010 Grid 1 -Grid2 !0-D 10-C IO-B !0-A Base Plate W x L (in.) 9x 13 8 X I6 8x16 9 X 13 Base Plate Thickness (in.) 0.500 0.375 0.375 0.500 Anchor Rod Qty/Diam (in.) 4-!.000 4-0.750 4-0.750 4-!.000 Column Base Elev. 100'-0" 100'-0" !00'-0" 100'-0" Load Type Desc. Hx Hz Vv Hx Hz Vv Hx Hz Vv Hx Hz Vv D Fnn 0.9 -4.6 --o:8 -0.8 -0.9 -J4.7 AD Fnn O.I -1.2 ------O.I . -!.2 CG Fnn 2.7 -I2.4 --0.2 2.2 --0.2 2.2 -2.7 !0.5 s Fnn I0.2 -39.7 -------I0.2 -39.8 USl* Fnn 9.I -23.6 -------9.! -48.0 "'USl Frm 9.I -48.0 -------9.I -23.6 WI> Fnn -7.2 -I2.4 -7.I --7.I --4.8 --4.4 <WI Fnn 4.7 -4.4 --6.4 ---6.4 -7.3 --I2.4 W2> Fnn -8.6 --8.4 -------3.4 --0.5 <W2 Fnn 3.3 --0.5 ------8.7 --8.4 "'AL> Fnn -0.0 -7.7 ------I.4 -3.6 AL*> Fnn -0.0 -2.! -----I.4 -9.3 <*AL Fnn !.4 -9.3 -----0.0 -2.I <AL* Fnn 1.4 3.6 ------0.0 7.7 cu Fnn !.4 -5.3 ------I.4 -5.3 E> Fnn -4.I --5.5 -0.0 --0.0 -4.I -5.5 EG+ Fnn 0.4 -1.6 --0.0 0.2 --0.0 0.2 -0.4 -!.4 <E Frm 4.1 5.5 -0.0 -0.0 -4.1 -5.5 EG-Fnn -0.4 -1.6 -0.0 -0.2 0.0 -0.2 0.4 -!.4 EB> Brc -0.0 ----0.0 - <EB Brc -------- WPAI Brc 2.5 -7.3 ------2.5 --7.3 'AL Fnn 0.7 8.5 -------0.7 -2.9 ALB> Brc ---- AL' Frm 0.7 2.9 --0.7 8.5 WPDI Brc !.9 --9.6 ----1.9 -9.6 <ALB Brc - WPA2 Brc 1.0 -3.3 --!.0 --3.3 WPD2 Brc 0.4 --5.6 ---0.4 -5.6 WPBI Brc 2.5 -7.3 --2.5 -7.3 WPCI Brc 1.9 -9.6 --1.9 -9.6 WPB2 Brc 1.0 --3.3 -----1.0 -3.3 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la - - - - - ---- - - - - - 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 55 of 175 WPC2 Brc oA I --5.6 -I I -oA I -5.6 Frame Reactions Factored L d Cases at F ame Cross S ct·on· 10 -oa r e ' X-Loc 01010 151010 381010 531010 Grid 1 * Grid2 10-D 10-C 10-B 10-A Ld Description Hx Hz Vv Hx Hz Vv Hx Hz Vv Hx Hz Vv Cs (application factor not shown (k) (k) (k) (k) (k) (k) (k) (k) (k) (k) (k) (k) I · D+AD+CG+S 13.9 57.9 --02 3.0 -02 3.0 -13.9 562 2 D+AD+CG+USI* 12.8 -41,7 --02 3.0 -02 3.0 -12.8 -64.4 - 3 D +AD+ CG +*US! 12.8 66.2 --0.2 3.0 --0,2 3.0 -12.8 40.0 - 4 D+AD+CG+WI> -3.5 -5.8 -7.rt 3.0 -7.0 3.0 -8.5 12.0 5 D+AD+CG+<Wl 8.4 -13.7 --6,6 3.0 --6.6 3.0 3.6 -4.0 - 6 D+AD+CG+W2> -4.9 -9,7 --0,2 3.0 -02 3.0 -7. I -16,0 - 7 D+AD+CG+<W2 7.0 -17,7 --02 3.0 -02 3.0 5.0 8.0 - 8 D+AD +CG +S+Wl> 5.9 -38.7 -52 3.0 -5.2 3.0 -14.9 -42.9 - 9 D+AD+CG+S+<Wl 14.9 -44,7 --s.o 3.0 --S.O 3.0 -S.9 -36.9 - 10 D+AD+CG+S+W2> 4.9 -41,6 --0,2 3.0 -0,2 3.0 -13.8 -45.9 II D+AD+CG+S+<W2 13-8 -47.6 --0,2 3.0 --0,2 3.0 -4.8 -39.9 - 12 D +AD+ CG+*Al> 3.7 -2S.9 --0,2 3.0 --0.2 3.0 -S. I -20,1 - 13 D+AD+CG+AL*> 3.7 20.3 --02 3.0 --02 3.0 -5.1 25.7 14 D +AD+ CG+<*AL 5.! -27.4 --{),2 3.0 --0.2 3.0 -3.7 -18.5 - IS D+AD+CG+<AL* S.I -21,8 --0.2 3.0 --0.2 3.0 -3.7 -24.2 - 16 D+AD+CU+Wt> -S.7 --5.8 -7,1 0.5 -7.1 0.5 -6.2 -2.3 - 17 D+AD+CU+<Wl 6.2 2.2 --6.4 0.5 --6.4 0.5 5.8 --S.7 - 18 D+AD+CU+W2> -7.2 --L8 --0.5 -0.5 -4.8 -6.3 - 19 D+AD+CU+<w2 4.7 -6.2 --o.s --0.5 7.3 --!.7 - 20 D+AD+CG+S+*AL> 9.4 -46,3 --{).2 3.0 --0.2 3.0 -IO.S -4I.S - 21 D+AD+CG+S+AL*> 9.4 -42.1 --{).2 3.0 --0.2 3.0 -10.5 -45.7 - 22 D+AD+CG+S+<*AL 10.5 -47.5 --0.2 3.0 --{),2 3.0 -9.4 -40.4 - 23 D+AD+CG+S+<AL* 10.5 -43.3 --0.2 3.0 --0.2 3.0 -9.4 -4.4.6 - 24 D+AD+CG+Wl>+*AL> !.0 -19,3 -2.5 3.0 -2.5 3.0 -6.6 -17.5 - 25 D+AD+CG+Wl>+AL*> !.0 -IS.! -2.5 3.0 -2.5 3.0 -6.6 -2!.7 - 26 D+AD+CG +<Wl+<*AL 6.S -23.4 --2.6 3.0 --2.6 3.0 -0.9 -13.4 - 27 D+AD+CG+<Wl+<AL* I 6.s -19.2 --2.6 3.0 --2.6 3.0 -0.9 -17.6 - 28 D+AD+CG+W2>+*AL> 0.4 -20.8 --0.2 3.0 --0.2 3.0 -6.0 -19.0 - 29 D+AD+CG+W2>+AL*> 0.4 --16.6 --{).2 3.0 --0.2 3.0 -6.0 -23.2 - 30 D +AD+ CG +<W2+<*AL 6.0 -24.9 --{).2 3.0 --0.2 3.0 -0.4 -14.9 - 31 D+AD+CG+<W2+<AL* 6.0 -20.7 --0.2 3.0 --0.2 3.0 -0.4 -19.1 - 32 D+AD+CG+S+E>+EG+ 2.4 -2l.l --0.2 3.1 --0.2 3.1 -8.5 -27.5 - 33 D+AD+CG+S+<E+EG+ 8.6 -29.4 --0.2 3.1 --0.2 3.1 -2.4 19.2 34 D+AD+CU+E>+EG~ -!.7 -!.7 --u.o 0.3 --u.o 0.3 -4.0 -9.6 - 3S D+AD+CU+<E+EG-4.1 -9.4 -0,0 0.3 -0.0 0.3 !.7 -!.9 - 36 D+AD+CG+S+EB>+EG+ s.s -0.0 2S.2 --{).2 3.1 --0.2 3.1 -S.5 -0.0 23.4 - 37 D+AD+CU+EB>+EG~ · !.2 -0.0 S.6 -0.0 0.3 -0.0 0.3 -1.2 -0.0 S.8 38 D+AD+CG+S+<EB+EG+ 5.5 -2S.2 --0.2 3.1 --0.2 3.1 -5.5 23.4 - 39 D+AD+CU+<EB+EG-!.2 -S.6 -0.0 0.3 -0.0 0.3 -1.2 S.8 - 40 D+AD+CG+WPAI 6.2 -10.9 --0.2 3.0 --0.2 3.0 -6.2 -9.2 - 41 D+AD+CG+S+WPAI 13.2 -42.S -{).2 3.0 --0.2 3.0 -13.2 -40.8 - 42 D+AD+CU+WPA1 3.9 --0.6 --0.5 --0.5 -3.9 -0.5 43 D+AD+CG+WPAI+*AL+ALB> 5.1 -21.8 --0.2 3.0 -0.2 3.0 -5.1 IS.9 - 44 D+AD+CG+WPAl+AL*+ALB> 5.! 17.6 --0.2 3.0 --0.2 3.0 -5.1 20.1 - 45 D +AD +CO +WPDI 5.6 -8.6 --0.2 3.0 --0.2 3.0 -5.6 6.9 46 D +AD+ CG + S + WPDI 12.7 40.8 -{).2 3.0 --0.2 3.0 -12.7 39.1 - 47 D+AD+CU+WPDI 3.3 --2.9 -0.5 --0.5 -3.3 --2.8 - 48 D+AD+CG+WPD 1 +* AL +<ALB 4.9 -20.9 --{).2 3.0 --0.2 3.0 -4.9 IS.O - 49 D+AD+CG+ WPD l +AL *+<ALB 4.9 -16.7 --0.2 3.0 -0.2 3.0 -4.9 19.2 - 50 D+AD+CG+WPA2 4.7 14.9 --0.2 3.0 --0.2 3.0 -4.7 !3.1 51 D+AD+CG+S+WPA2 12.! 45.5 -0.2 3.0 --0.2 3.0 -12.1 43.8 52 D+AD+CU+WPA2 2.4 3.3 0.5 -0.5 -2.4 3.4 - 53 D+AD+CG+WPAZ+*AL+ALB> 4.6 -23.3 -0.2 3.0 --0.2 3.0 -4.6 17.3 54 D+AD+CG+WPA2+AL*+ALB> 4.6 -19.1 --0.2 3.0 -0.2 3.0 -4.6 2!.6 55 D+AD+CG+WPD2 4.1 -12.6 --0.2 3.0 --0.2 3.0 -4. I -10.8 56 D+ AD+ CG+S + WPD2 1!.6 43.8 --0.2 3.0 --02 3.0 -11.6 42.0 57 D+ AD +CU + WPD2 1.9 1.0 -0.5 --0.5 -1.9 1.1 58 D+AD+CG+WPD2+*AL+<ALB 4.4 -22.4 -0.2 3.0 --0.2 3.0 -4.4 -16.5 - File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 56 ofl75 59 D+AD+CG+WP02+AL*+<ALB 4.4 18.2 --0.2 3.0 --0.2 3.0 -4.4 20.7 60 D+AD+CG+WPBl 6.2 -10.9 --0.2 3.0 --0.2 3.0 -6.2 9.2 61 D+AD+CG+S+WPBI 13.2 42.5 -0.2 3.0 -0.2 3.0 -13.2 40.8 - 62 D+AD+CU+WPBl 3.9 --0.6 --0.5 -0.5 -3.9 --0.5 - 63 D+AD+CG+WPB I+* AL+ALB> 5.1 21.8 --0.2 3.0 --0.2 3.0 -5.1 15.9 64 D+AD+CG+WPB 1 +AL *+ALB> 5,1 17.6 -0.2 3.0 '0.2 3.0 -5.1 20.1 - 65 D+AD+CG+WPCI 5.6 8.6 --0.2 3.0 -0.2 3.0 -5.6 6.9 - 66 D +AD+ CO+ S + WPCl 12.7 40.8 -0.2 3.0 -0.2 3.0 -12.7 39.1 67 D+AD+CU+WPCl 3.3 -2.9 --0.5 -0.5 -3.3 -2.8 68 D+AD+CG+WPCI+*AL+<ALB 4.9 20.9 --0.2 3.0 -0.2 3.0 -4.9 15.0 - 69 D+AD+CG+WPC l+AL *+<ALB 4.9 -16.7 -0.2 3.0 -0.2 3.0 -4.9 19.2 70 D +AD+ CG + WPB2 4.7 14.9 --0.2 3.0 -0.2 3.0 -4.7 13.1 71 D+AD+CG+S+WPB2 12.1 -45.5 -0.2 3.0 -0.2 3.0 -12.1 43.8 - 72 D +AD+ CU + WPB2 2.4 -3.3 -0.5 -0.5 -2.4 -3.4 - 73 D+AD+CG+WPB2+* AL+ALB> 4.6 -23.3 --0.2 3.0 --0.2 3.0 -4.6 17.3 - 74 D+AD+CG+WPB2+AL "+ALB> 4.6 -19.1 -0.2 3.0 --0.2 3.0 -4.6 -21.6 - 75 D+AD+CG+WPC2 4.1 -12.6 --0.2 3.0 --0.2 3.0 -4.1 -10.8 - 76 D+AD+CG+S+WPC2 11.6 -43.8 --0.2 3.0 --0.2 3.0 -11.6 -42.0 - 77 D+AD+CU+WPC2 1.9 -1.0 --0.5 --0.5 -1.9 -1.1 - 78 D+AD+CG+WPC2+*AL+<ALB 4.4 -22.4 --0.2 3.0 --0.2 3.0 -4.4 16.5 - 79 D+AD+CG+WPC2+AL*+<ALB 4.4 -18.2 --0.2 3.0 --0.2 3.0 -4.4 -20.7 - 80 D +AD+ CG + S+ALB> 13.9 57.9 --0.2 3.0 --0.2 3.0 -13.9 -56.2 - 81 D +AD + CG+* AL+ALB> 4.4 -26.7 --0.2 3.0 --0.2 3.0 -4.4 -19.3 82 D +AD+ CG+AL *+ALB> 4.4 -21.0 --0.2 3.0 --0.2 3.0 -4.4 24.9 - 83 D+AD+CG+S+*AL+ALB> 9.9 -46.9 --0.2 3.0 --0.2 3.0 -9.9 -40.9 - 84 D+AD+CG+S+AL*+ALB> 9.9 -42.7 --0.2 3.0 --0.2 3.0 -9.9 -45.2 85 D +AD+ CG + S+<ALB 13.9 -57.9 --0.2 3.0 --0.2 3.0 -13.9 -56.2 - 86 D +AD+ CG+*AL+<ALB 4.4 -26.7 --0.2 3.0 --0.2 3.0 -4.4 -19.3 - 87 D +AD + CG+AL *+<ALB 4.4 -21.0 --0.2 3.0 --0.2 3.0 -4.4 -24.9 - 88 D+AD+CG+S+*AL+<ALB 9.9 -46.9 --0.2 3.0 --0.2 3.0 -9.9 -40.9 89 D+AD+CG+S+AL*+<ALB 9.9 -42.7 --0.2 3.0 --0.2 3.0 -9.9 -45.2 - M1 ax mum C b' dR om 1ne eactlons s 1 F umma_!Y_W th acto red L d F oa s-ram n2: X-Loc Grid Hrz left Load Hrz Right Load Hrzln Load Hrz Out Load Uplift Load Vrt Down Load Momcw Lo"<i Momccw Load (-Hx) Case (Hx) Case (-Hz) Case ~)) Case (-Vy) Case (Vy) Case (-Mzz) Case (Mzz) Case (k) (k) (k) (k) (k) (in-k) (in-k) 0/0/0 10-D 7.2 18 14.9 9 0.0 36 --5.8 16 66.2 3 ---- 151010 10-C ----6.6 5 7.1 16 --3.1 32 ---- 38/0/0 10-B ----6.6 5 7.1 16 --3.1 32 ---- 53/0/0 10-A 14.9 8 7.3 19 0.0 36 --5.7 17 64.4 2 ---- File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: ?.Ia 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: !:57:43 PM Shape: base Loads and Codes -Shape: base City: Rifle County: Garfield State: Colorf!,do 89AISC 04A!Sl Building Code: 2003 International Building C:ode Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind LOad Wind Speed: 90.00 mph Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: 1.023 Wind Enclosure: Enclosed Wind Importance Factor: 1.150 Topographic Factor: 1.0000 NOT Windbome Debris Region Base Elevation: 01010 Primary Zone Strip Width: 10/7/3 Patts I Portions Zone Strip Width: 5/'YIO Basic Wind Pressure: 20.74 psf Deflection Conditions Built Up: Cold Fonn: Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf Snow Load Roof Snow Load: 75.00 psf Design Snow (Sloped): 75.00 psf Snow Exposure Category (Factor): 2 Partially Exposed (!.00) Snow Importance: 1.100 Thennal Category (Factor): Heated (1.00) Ground I Roof Conversion: 0.70 %Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Unobstructed, Slippery Roof Frames are vertically supporting:Metal RoofPurlins and Panels Deflection Limit Override V /240 Fr<ppeS are laterally suppmting:Underhung Crane Deflection Limit Override H/400 Purlins are supporting:Metal Roof Panels Deflection Limit Override V/240 Girts are supporting:Metal Wall Panels Deflection Limit Override H/240 Live Load C0:untry: United States· Rainfall: 4.00 inches per hour Live Load: 20.00 psf Not Reducible Seismic Load Mapped Spectral Response~ Ss:43.60 %g Mapped Spectral Response~ Sl :9.10 %g Seismic Hazard I Use Group: Group 2 Seismic Importance: I .250 Seismic Performance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Bracing Seismic Period: 0.2691 Framing R-Factor: 3.0000 Bracing R~Factor: 3.0000 Soil Profile Type: Stiff soil (D, 4) Frame Redundancy Factor: 1.0000 Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain all code and loading infonnation for this specific building site. Desien Load Combinations -Bracin No. Origin Factor ~pplication Description I System !.000 r.1oo E> E> 2 System !.000 ~.700 <E <E 3 System !.000 l.OWPAI WPAI 4 System !.000 I.OWPDI WPDI s System !.000 !.0 WPA2 WPA2 6 System 1.000 !.0 WPD2 mpoz 7 System 1.000 1.0 WPBI WPBI 8 System 1.000 1.0 WPCI WPCJ 9 System 1.000 !.0 WPB2 WPB2 tO System 1.000 !.0 WPC2 WPC2 II System 1.000 0.375WPAI +0.750AL* WPAJ+AL* 12 System 1.000 0.375 WPDI + 0.750 "'AL WPDI+*AL !3 System 1.000 0.375 WPA2 + 0.750 AL* WPA2+AL* !4 System 1.000 0.375 WPD2 +0.750 *AL WPD2+*AL IS System 1.000 0.375 WPBI +0.750 AL* WPBl+AL* 16 System 1.000 0.375 WPCI + 0.750 *AL WPCJ+*AL 17 System 1.000 0.375 WPB2 + 0.750 AL* WPB2+AL* 18 System 1.000 0.375 WPC2 + 0.750 *AL WPC2+*AL \9 System 1.000 !.0 AL* AL• File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: 1:57:43 PM Page: 58 of 175 'AL File: 7079 Chevron R !_Stress Check I 0 _ 2008 with 08 _ 2008 Loading Version: 7.la ·' 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 59 of 175 Diaeonal Bracine Member Desien Summary: Roof A Mem. Bracing Length Angle Design Seismic Stress Stress Governing Design Conunent No. Shape (ft) Axia((k) Factor Factor Ratio Load Case Status 1 R 0.5 21.84 34.7 -3.09 1.0000 1.0000 0.597 0.700<E passed 2 R0.5 21.84 34.7 -3.06 1.0000 1.0000 0.590 0.700E> passed 3 R0.75 21.24 30.7 -8.54 1.0000 1.0000 0.732 0.700<E passed 4 R0.75 21.24 30.7 -8.46 1.0000 1.0000 0.725 0.700E> passed 5 R0.75 19.66 21.0 -11.54 1.0000 1.0000 0.989 0.700<E passed 6 R0.75 19.66 21.0 -11.75 1.0000 1.0000 1.007 0.700E> passed 7 R0.5 21.84 34.7 -3.06 1.0000 1.0000 0.590 0.700<E passed 8 R0.5 21.85 34.7 -3.Q9 1.0000 1.0000 0.597 0.700E> passed 9 R0.75 21.24 30.7 -8.45 1.0000 1.0000 0.724 0.700<E passed 10 R0.75 21.2 30.7 -8.53 1.0000 1.0000 0.731 0.700E> passed 11 R0.75 19.6 21.0 -11.74 1.0000 1.0000 1.006 0.700<E passed 12 R0.75 19.66 21.0 -1 1.53 1.0000 1.0000 0.988 0.700E> passed Mem. End Diaoonal Connection Design Information 1 Left Slot: web thk = 3/16 in., F = 3.09k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = l/4 in., F = 3.09k, E factor= l.OOO, stress increase = 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK. tensile fracture of web OK>> passed · 2 Left Slot: web thk 1/4 in., F -3.06k, E factor'-1.000, stress increase -1.000, slot offset 2 in., web/flange weld OK, web direct shear OK, web Right jPunching shear OK. tensile--fracture of web OK>> passect ·. · Slot: web thk = 3/16 in., F = 3.06k, E factor= l.OOO, stress increase= l.OOO, slot offset= 2 in., web/flange weld OK, web direct shear OK, web !Punching shear OK, tensile fracture of web OK>> passed 3 Left Slot: web thk = 1/4 in., F = 8.54k, E factor-1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web Right ~unching shear OK, tensile fracture of web OK >>passed Slot: web thk = 114 in., F = 8.54k, E factor= 1.000, stress increase = 1.000, slot offset = 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed 4 Left Slot: web thk-1/4 in., F = 8.46k, E factor-! .000, stress increase= 1.000, slot offset-2 ln., weblflange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = 1/4 in., F = 8.46k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web !Punching shear OK, tensile fracture of web OK >> oassed 5 Left Slot w/ Backing Plate: web thk-1/4 in., F ll.54k, E factor-1.000, stress increase 1.000, slot offset -2 in., web/flange weld OK, web ~irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = 11.54k, E factor= 1.000, stress increase= 1.000, slot oftSet = 2 in., web/flange weld OK, web direct shear OK, web punchin<Y shear OK, tensile fracture of web OK>> passed 6 Left Slot w/ Backing Plate: web thk-114 in., F-J !.75k, E factor 1.000, stress increase= 1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = l/4 in., F = 11.75k, E factor"" 1.000, stress increase= 1.000, slot offset= 2 in., web/t1ange weld OK, web irect shear 0_1<(, web punching shear OK, tensile fracture of web OK >>:_p_(lSsed 7 Lefl Slot: web thk"" 3/16 in., F-3.06k, E factor-1.000, stress increase-!.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web Right tpunching shear OK, tensile fracture of web OK>> passed Slot: web thk"" 1/4 in., F = 3.06k E factor"" 1.000 stress increase= 1.000, slot offset= 2 in., web/flange weld OK web direct shear OK, web File: 7079 Chevron R !_Stress Check I 0 _2008 with 08_2008 Loading Version: 7.la 8 Left Right 9 Left Right 10 Left Right 11 Left Right 12 Left Right 07-27053 Calculations Hazardous Materials Occupancy unchino shea1· OK, tensile fracture of web OK>> passed Date: 10/20/2008 Time: I :57:43 PM Page: 60 of 175 Slot: web thk-114 in., F = 3.09k, E factor-1.000, stress increase-1 .000, slot offset-2 in., web/flange weld OK, web direct shear OK, web ~unching shear OK, tensile fracture of web OK>> passed Slot: web thk = 3/16 in., F"' 3.09k, E factor= 1.000, stress increase"' 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk"' 114 in., F = 8.45k, E factor= 1.000, stress increase= 1 .000, slot offset= 2 in., web!f1ange we!d OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot: web thk = 114 in., F"" 8.45k, E factor= !.000, stress increase"" 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk-1/4 in., F = 8.53k, E factor= 1.000, stress increase""' 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot: web thk = 114 in., F = 8.53k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> oassed Slot w/ Backing Plate: web thk = 1/4 in., F-11.74k, E factor-1.000, stress increase-1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = l/4 in., F = 11.74k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk-1/4 in., F-ll.S3k, E factor= 1.000, stress increase-1.000, slot offset-2 in., web/flange weld OK, web irect shear OK. web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = 114 in., F = 11.53k, E factor= 1.000, stress increase = 1.000, slot offset= 2 in., web/flange weld OK, web irect shear OK. web vunchinll: shear OK, tensile fracture of web OK>> passed Strut Bracine: Member Desie:n Summary: Roof A Mem. Bracing Length Design Seismic Stress Stress Governing Design Description No. Shape (ft) Axlai(k) Factor Factor Ratio Load Cnse Status 12 FF 2.Sx.O.l0Sx8.5 18.50 11.82 2.5000 1.2750 0.981 0.700E> passed Eave Strut, Collector 28 FF 2.5x0.10Sx.8.5 18.50 1!.80 2.5000 1.2750 0.980 0.700<E I passed Eave Strut, Collector . clip to tensile rupture & block shear OK, clip buckling OK, clip to web weld 3/16 fillet one side, clip to File: 7079 Chevron R l_ Stress Check l 0 _2008 with 08 _ 2008 Loading Version: ?.Ia 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 61 of 175 Diagonal Bracine Member Des fen Summary: Roof B Mem. Bracing Length Angle Design Seismic Stress Stress Governing Design Comment No. Shape (ftl Axbl(k) Factor Factor Ratio Load Case Status I RO.S 21.85 34.7 -3.10 1.0000 1.0000 0.599 0.700E> passed 2 RO.S 21.8 34c7 -3.07 1.0000 1.0000 0.592 0.700<E passed 3 R0.75 21.24 30.7 -8.5< 1.0000 1.0000 0.732 0.700E> passed 4 R0.75 21.24 30.7 -8.46 1.0000 1.0000 0.725 0.700<E passed 5 R0.75 19.66 21.0 -11.54 1.0000 1.0000 0.990 0.700E> . passed 6 R0.75 19.66 21.0 -11.7 1.0000 1.0000 1.007 0.700<E passed 7 RO.S 21.84 34.7 -3.08 1.0000 1.0000 0.593 0.700E> passed 8 RO.S 21.84 34.7 -3.11 1.0000 1.0000 0.600 0.700<E passed 9 R0.75 21.24 30.7 -8.47 1.0000 1.0000 0.726 0.700E> passed 10 R0.75 21.24 30.7 -8.55 1.0000 1.0000 0.733 0.700<E passed 11 R0.75 19.66 21.0 -11.71 1.0000 1.0000 1.008 0.700E> passed 12 R0.75 19.66 21.0 -11.55 1.0000 1.0000 0.990 0.700<E I passed Mem. End Dia.1:1onal Connection Design Infonnation 1 Left Slot: web thk = 3/16 in., F-3.1 Ok, E factor, 1 .000, stress increase = 1.000, slot offset-2 in., web/flange weld OK. web direct shear OK, web tpunching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = l/4 in., F = 3.1 Ok, E factor"" 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld Ok, web direct shear OK, web P~nchin.e: shear OK, tensile fracture of web OK>> oassed 2 Left Slot: web thk = l/4 in., F = 3p7k, E factor 1 .000, stress increase-' 1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web !Punching shear OK, tensile fracture of web 6K >> passed Right Slot: web thk = 3/16 in., F = 3.07k, E factor= 1.000, stress increase = 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web Punching shear OK, tensile fracture of web OK>> passed 3 Left lot: web thk = 1/4 in., F-8.54k, E factor= !.000, stress increase= 1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK >> passed Right Slot: web thk = l/4 in., F = 8.S4k, E factor""' 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unchin.Q" shear OK, tensile fracture of web OK >> passed 4 Left Slot: web thk = 1/4 in., F = 8.46k, E factor-I .000, stress increase-1.000, slot offset= 2 in., web/flange weld OK, web di1·ect shear OK, web unching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = 1/4 in., F = 8.46k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK >>passed 5 Left Slot w/ Backing Plate: web thk-1/4 in., F-!1.54k, E factor-1.000, stress increase-1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = JJ.S4k, E factor= 1.000, stress increase= 1.000, slot o!Tset = 2 in., web/flange weld OK, web direct shear OK, web punchin.g shear OK, tensile fracture of web OK>> passed 6 Left Slot w/ Backing Plate: web thk-J/4 in., F-11.75k, E factor-1.000, stress increase 1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = 11.75k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile 11-acture of web OK>> passed 7 Left Slot: web thk-3/16 in., F = 3.08k, E factor= 1.000, stress increase-1.000, slot offset-2 in., weblflange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = 1/4 in., F = 3.08k, E factor"" I .000, stress increase= I .000, slot offset= 2 in., web!J1anoe weld OK, web direct shear OK, web File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.Ja 8 Left Right 9 Left Right 10 Left Right II Left Right 12 Left Right 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 62 of 175 unchin<> shear-OK, tensile fracture of web OK>> passed Slot: web thk = l/4 in., F-3.11k, E factor-1.000, stress increase-1.000, slot offset= 2 in., webtnange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk = 3/16 in., F = 3.llk, E factor= I .000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk = 1/4 in., F-8.47~, E factor"" 1.000, stress increase-1.000, slot offset= 2 in., weblnange weld OK, web direct shear OK, web jPunching shear OK, tensile fracture of web OK>> passed Slot: web thk"" 1/4 in., F = 8.47k, E factor"" 1.000, stress increase·= 1.000, slot offset"" 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk = 1/4 in., F-8.55k, E factor= 1.000, stress increase-1.000, slot offset= 2 in., webltlange weld OK, web direct shear OK, web !Punching shear OK, tensile fracture of web OK>> passed Slot: web thk = 1/4 in., F = 8.55k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unchingshear OK, tensile fracture of web OK >>p?ssed Slot w/ Backing Plate: web thk-l/4 in., F-11.76k, E factor= 1.000, stress increase 1.000, slot offset-2 in., web/flange weld OK, web ~irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = 1/4 in., F = ll.76k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web ~irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = 1/4 in., F = ll.55k, E factor-1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web toirect shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = 1/4 in., F = ll.SSk, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punchi.~g shear OK, tensile fracture of web OK >:::"_.P_assed Strut Bracinll Member Desi.en Summary: Roof B . Mem. Bracing Length Design Seismic Stress Stress Governing Design Description No. Shape (ftl Axia((k) Factor Factor Ratio load Case Status 12 FF 2.5x0.105x8.5 18.50 11.81 2.5000 1.2750 0.981 0.700<E passed Eave Strut, Collector 28 FF 2.5x0.105x8.5 18.50 11.82 2.5000 1.2750 0.982 0.700E> I passed Eave Strut, Collector Mem. End Strut Connection Design Information 12 Left rame Clip GCR1030505 w/ (2) 7/8 in., clip tensile rupture & block shear OK, clip buckling OK. clip to web weld 3/16 fillet one side, clip to flange weld 3/16 fillet one side=> passed Right Frame Clip GCRI030505 w/ (2) 7/8 in., clip tensile rupture & block shear OK, clip buckling OK. clip to web weld 3/16 fillet one side, clip to flange weld 3/16 fillet one side=> passed 28 Left Frame Clip GCRl030505 w/ (2) 7/8 in., clip tensile rupture & block shear OK, clip buckling OK, clip to web weld 3/16 fillet one side, clip to flange weld 3/16 fillet one side =>passed 0 ~ Right Frame Clip GCR1030505 w/ (2} 7/8 in., clip tensile rupture & block shear Ok, clip buckling OK, clip@ web we}d 3/16 fillet one side, clip to .flange weld 3/16 fillet one side => passed File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 63 of 175 '. " •. " Diagonal Bracing Member Design Summary: Sidewall 2 Mem. Bracing Length Angle Design Seismic Stress Stress Governing Design Conunent No. Shape (ftl Axial(k\ Factor Factor Ratio Load Case Status I R 1.0 25.55 43.3 -18.59 1.0000 1.0000 0.897 0.700<E passed 2 R 1.0 25.56 43.3 -15.71 1.0000 1.0000 0.758 0.700E>. passed 3 R 0.875 23.20 38.2 -15.95 1.0000 1.0000 1.005 0.700<E passed 4 R 0.875 23.20 38.2 -15.45 1.0000 1.0000 0.973 0.700E> passed 5 R 1.0 25.56 43.3 -15.71 1.0000 1.0000 0.758 0.700<E passed 6 R 1.0 25.55 43., -18.59 1.0000 1.0000 0.897 0.700E> passed ) 7 R 0.875 23.20 38.2 -15.46 1.0000 1.0000 0.974 0.700<E passed 8 R 0.875 23.20 38.2 -15.96 1.0000 1.0000 1.005 0.700E> I passed Mem. End Diagonal Connection Design Infonnation I Left Slot w/Backing Plate: Web thk-3/16 in., F-18.59k, E factor-1.000, stress increase-1.000, slot offset= 2 in., web/flange weld OK. web irect shear OK. web punching shear OK. tensil~ fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = t 8.59k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web irect shear OK, web pUnching shear OK, tensile fracture of web OK>> passed 2 Left lot: web tbk 3116 in.; F l5.7lk, E factor= 1.000, stress increase-1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = l/4 in., F = 15.71k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed 3 Left Slot w/ Backing Plate: web thk = 3/16 in., F = 15.95k, E factor-1.000, stress increase = 1.000; slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = 15.9Sk, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed 4 Left Slot w/ BaCking Plate: web thk = 1/4 in., F-15.4Sk, E factor-1 .000, stress increase-1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK >> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = I SASk, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web ounchinf.!: shear OK, tensile fiacture of web OK>> oassed 5 Left lot web thk = 1/4 in., F-15.71k, E factor-1.000, stress increase-1.000, slot offset 2 in., web/tlange weld OK, web direct shear OK, web punching shear OK, tensile fracture. of web OK >> passed Right Slot: web thk = l/4 in., F = 15,71 k, E factor= l.OOO, stress increase = 1.000, slot offset= 2 in., web/tlange weld OK, web direct shear OK, web unching shear OK, tensile fraCture of web OK>> passed 6 Left Slot w/ Backing Plate: web thk = 1/4 in., F = 18.59k, E factor=-1.000, stress increase-1.000, slot offset-2 in., web!tlange weld OK. web Right ~ircct shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = 1/4 in., F = 18.59k, E factor= ! .000, stress increase= 1.000, slot offset= 2 in., web/tlange weld OK, web !direct shear OK, web ounchin£?: shear OK, tensile fracture of web OK >:::"_Q!!Ssed 7 Left Slot w/ Backing Plate: web thk-1/4 in., F-15.46k, E factor-1.000, stress increase-1.000, slot offset= 2 in., web/t1ange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK >>passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = IS.46k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., webltlange weld OK, web ~irect shear OK, web punching shear OK, tensile fracture of web OK>> passed 8 Left Slot w/ Backing Plate: web thk = 1/4 in., F-15.96k, E factor-1.000, stress increase-1.000, slot offset-2 in., web/tlange weld OK, web File: 7079 Chevron RI_Stress Check 10_2008 wi1h 08_2008 Loading Version: 7.1 a 07-27053 Calculations Hazardous Materials Occupancy lctirect shear OK, Web punching shear OK, tensile fracture of web OK>> passed Date: 10/20/2008 Time: I :57:43 PM Page: 64 of 175 Right Slot w/ Backing Plate: web thk = 1/4 in., F = 15.96k, E factor= 1.000, stress increase= ! .000, slot offset"" 2 in., web/flange weld OK, web direct shear OK, web unchiJi shear OK, tensile fracture of web OK>> as.sed 0 0 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 65 of 175 Dia11ona IB racine: M b em erDesilm s umm~ry: S1dewa 114 Mem. Bracing Length Angle Design Seismic Stress Stress Goveming Design Comment No. Shaoe (ftl Axia((k) Factor Factor Ratio Load Case Status I RLO 25.55 43.3 "18.5 1.0000 1.0000 0.895 0.700E> pas'sed 2 R 1.0 25.55 43.3 -15.6 1.0000 1.0000 0.757 0.700<E passed 3 R0.875 23.19 38.2 -15.94 1.0000 1.0000 1.004 0.700E> passed 4 R 0.875 23.19 38.2 -15.45 1.0000 1.0000 0.973 0.700<E , passed 5 R l.O 25.55 43.3 -15.70 1.0000 1.0000 0.757 0.700E> passed 6 RLO 25.55 43.3 -18.57 1.0000 1.0000 0.896 0.700<E passed 7 R 0.875 23.20 38.2 -15.45 1.0000 1.0000 0.973 0.700E> passed 8 R 0.875 23.19 38.2 -15.95 1.0000 1.0000 1.004 0.700<E I passed 0 Mem. End Diagonal Connection Design Infonnation 1 Left Jot w/ Backing Plate: web thk 1/4in., F l8.56k, E factor-1.000, stress increase= l.OOO, slot offset 2 in., web/flange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: Web thk = 1/4 in., F = 18.56k, E factor= 1.000, stress increase = 1.000, slot offset= 2 in., web/flange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed 2 Left Slot: web thk-1/4 in., F -15.69k, E factor-1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web Right ~nching shear OK. tensile fracture of web OK >>passed . Jot: web thk = l/4 in., F = I5.69k, E·factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unchlng shear OK tensile fracture of web OK>> passed 3 Left lot w/ Backing Plate: web thk-l/4 in., F = 15.941<, E factor-1.000, stress increase 1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = l5.94k, E factor= 1.000, stress increase= 1.000, Slot offset= 2 in., web/flange weld OK, web irect shear OK, web punchli}_g shear OK, tensile fracture of web OK>> Passed 4 Left Slot w/ Backing Plate: web thk = 1/4 in., F 15.45k, E factor= I .000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK >> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = 15.45k, E factor= !.000, stress increase= I .000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punchin,g shear OK, tensile fracture of web OK>> passed - 5 Left Slot web thk-l/4 in., F = 15.70k, E factor= 1.000, stress increase= 1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = 1/4 in., F = 15.70k, E factor= 1.000, stre~s increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unchingshear OK, terisile fracture of web OK>> oassed 6 Left lot w/ Backing Plate: web thk-1/4 in., F 18.57k, E factor= I .000, stress increase-1.000, slot offset= 2 in., web/t1ange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = 1/4 in., F = J8.57k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/t1ange weld-OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed 7 Left Slot w/ Backing Plate: web thk-i/4 in., F I S.45k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/nange weld OK, web irect shear OK, web punching shear OK, tensile-fracture of web OK>> passed Right Slot w/ Backing Plate: web thk = \14 in., F = I 5.4Sk, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., weblnange weld OK, web direct shear OK, web punchiJ1_g shear OK, tensile Ji-acture of web OK >>_p~ssed 8 Lett Slot w/ Backing Plate: web thk-1/4 in., F l5.95k. E factor= 1.000, stress increase-1.000, slot offset-2 in., weblnange weld OK, web File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Date: 10/20/2008 Time: I :57:43 PM Page: 66 of 175 Right Slot w/ Backing Plate: web thk = 1/4 in., F = 1 S.9Sk, E factor= 1 .000, stress increase= 1 .000, slot offset= 2 in., web/flange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed 0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy City: Rifle County: Building Cod~: 2003 [ntcmational Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind Load Wind Speed: 90.00 mph Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: 1.023 Garfield State: Built Up: Cold Form: Colorado 89AISC 04AISI Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf Snow Load RoofS now Load: 75.00 psf Design Snow (Sloped): 75.00 psf Snow Exposure Category (Factor): 2 Pa1tially Exposed ( 1.00) Live Load Country: United States Rainfall: 4.00 inches per hour Live Load: 20.00 psf Not Reducible Seismic Load Mapped Spectral Response w Ss:43.60 %g Mapped Spectra! Response-S 1:9.10 o/og Seismic Hazard I Use Group: Group 2 Wind Enclosure: Enclosed Snow Importance; 1.100 Seismic Importance: 1.250 t-------;;W':'i!'!nd'::I":m""."o'-lrt':'an':c":e"':F"'ac';'to';;r;;;: ;_,l.C'15;;0c_ ___ . ____ T?;h;;•:;;rma';5'1T1C~a;;te~go?ry~(F;-;•;:;c;,;to"r)C"' ifH"jeaifte::d:.:(c.I:.:.O::O)'----S<;e;:;is;:;m"ici-inPe;yro;;o:;;mli,a;;]nce I Design Category: C Topographic Factor: 1.0000 Ground/ Roof Conversion: 0.70 System NUl detallealOf'S"e;;.Js"'m"wo-''--''-------- NOT Windbome Debris Region Base Elevation: 0/0/0 Primary Zone Strip Width: 10/7/3 % Snow Used in Seismic: 20.00 Framing Seismic Period: 0.4480 Seismic Snow Load: 15.00 psf Bracing Seismic Period: 0.2691 Unobstructed, Slippery Roof Framing RMFactor: 3.0000 Bracing RMFactor: 3.0000 Parts I Portions Zone Strip Width: 5/3/10 Basic Wind Pressure: 20,74 psf Soil Profile Type: Stiff soil (D, 4) Frame Redundancy Factor: 1.0000 Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W Per Article 2,9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain all code and loading information for this specific building site, Desif,!n Load Combinations~ Purlin No. OrigiE Factor Aoolication Description I System 1.000 I.OD+ I.OCG+ !.OS D+CG+S 2 System 1.000 LOD+ LOCG+ LOUSI* D+CG+US!' 3 System 1.000 LOD+ f.OCG+ LO'USI D+CG+*USI 4 System 1.000 1.0 D + 1.0 CG + 1.0 PFI D+CG+PF1(Span I) 5 System 1.000 1.0 D+ 1.0 CG + 1.0 PFI D +CG + PFI(Span 9) 6 System 1.000 1.0 D + 1.0 CG + 1.0 PHI D+CG+PHI(Span I) 7 System 1.000 LOD+LOCG+I.OPHI D + CG + PHI(Span 9) 8 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 D +CO + PF2(Spans 1 and 2) 9 System 1.000 1.0 D+ 1.0 CG + 1.0 PF2 D +CO + PF2(Spans 2 and 3) 10 System 1.000 1.0 D+ l.OCG + 1.0 PF2 D +CO + PF2(Sp"ns 3 and 4) 11 System 1.000 I.OD+I.OCG+I.OPF2 D + CG + PF2(Spans 4 and 5) 12 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 D +CO + PF2(Spans 5 and 6) 13 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 D +CO + PF2(Spans 6 and 7) 14 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 D + CG + PF2(Spans 7 and 8) 15 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 D +CO + PF2(Spans 8 and 9) 16 System 1.000 LO D + 1.0 CO+ LO WI> D+CG+Wl> 17 System 1.000 LOD+ LOCG+ LO<W2 D+CG+<W2 18 System 1.000 0.600 D + 0.600 CU + 1.0 W1> D+CU+Wl> 19 System 1.000 .600 D + 0.600 CU + 1.0 <W2 D+CU+<W2 20 System 1.000 1.0 D + 1.0 CG + 0.750 S +0,750 WI> D+CG+S+Wi> 21 System 1.000 1.0 D + 1.0 CG + 0.750 S + 0.750 <W2 D+CO+S+<W2 22 System Derived 1.000 1.0 D + 1.0 CG + 0.150 S +0.750 EB> + 0.700 EG+ jD+CG+S+EB>+EG+ 23 System Derived 1.200 1.200 D + 1.200 CG + 0.200 S + 1.0 EB> + 0.700 EG+ jo+CG+S+EB>+EG+ 24 System Derived 1.200 .900 D + 0.900 CG + I .0 EB> + 0.700 EG~ D+CG+EB>+EG~ 25 System Derived 1.000 .600 D +MOO CU + 0.700 EB> + 0.700 EG-D+CU+EB>+EG- 26 System Derived 1.000 LOD+ l.OCG + 0.150 S +0.750 <EB +0.700 EG+ D+CG+S+<EB+EG+ 27 System Derived 1.200 1.200 D + 1.200 CG +0.200 S + 1,0 <EB +0.700 EG+ D+CG +S +<EB + EG+ 28 System Derived 1.200 .900 D + 0.900 CG + 1.0 <EB +0.700 EG· D+CG+<EB+EG- 29 System Derived 1.000 .600 D + 0.600 CU + 0.700 <EB + 0,700 EG· D+CU+<EB+EG· 30 System Derived 1.000 l.OD+ I.OCG + 1.0 WPAI D+CG+WPA! 31 System Derived 1.000 .600 D +0.600 CU + l.OWPAl D+CU+WPA! File: 7079 Chevron R I_ Stress Check I 0 _ 2008 with 08 _ 2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 68 of 175 32 System Derived 1.000 1.0 D + 1.0 CO+ 0.750 S + 0.750 Wl'AI D+CG+S+WPAI 33 System Derived 1.000 1.0 D + 1.0 CO+ 1.0 WPD! D+CO+WPDI 34 System Derived 1.000 ~.600 D + 0.600 CU + 1.0 Wl'DI D+CU+WPDI 35 System Derived 1.000 1.0 D + 1.0 CO+ 0.750 S + 0.750 Wl'DI D+CO+S+WPDI 36 System Derived 1.000 !.0 D + 1.0 CO+ 1.0 WPA2 D+CG+WPA2 37 System Derived !.000 ~.600 D + 0.600CU + 1.0 Wl'A2 . D+CU+WPA2 38 System Derived !.000 !.0 D + !.0 CO+ 0.750 S + 0.750 WPA2 D +CO+ S + WPA2 39 System Derived 1.000 1.0 D + 1.0 CG + \.0 WPD2 D+CO+WPD2 40 System Derived !.000 ~.600 D + 0.600 CU + 1.0 WPD2 O+CU+WPD2 41 System Derived !.000 1.0 D + 1.0 CO+ 0.750 S + 0.750 WPD2 D+CG+S+WP02 42 System Derived 1.000 1.0 D + 1.0 CO + 1.0 WPB 1 D+CG+WPBJ 43 System Derived !.000 0.600 D +0.600 CU + 1.0 WPBI D+CU+Wl'BI 44 System Derived !.000 1.0 D + 1.0 CO+ 0.750 S +0.750 WPB 1 D+CG+S +WPBl 45 System Derived 1.000 1.0 D + 1.0 CO+ 1.0 WPCI D+CO+WPCI 46 System Derived 1.000 ~.600 D + 0.600 CU + 1.0 WPC! D+CU+WPCI 47 System Derived !.000 1.0 D + !.0 CO+ 0.750 S + 0.750 Wl'Cl D+CO +S +Wl'Cl 48 System Derived !.000 !.0 D + !.0 CO + 1.0 Wl'B2 D+CO+WPB2 49 System Derived 1.000 r.600 D + 0.600 CU + 1.0 WPB2 D+CU+Wl'B2 so System Derived 1.000 1.0 D + 1.0 CO+ 0.750 S + 0.750 Wl'B2 D+CO+S+WPB2 51 System Derived 1.000 1.0 D + 1.0 CO + 1.0 Wl'C2 D+CG+WPC2 52 System Derived 1.000 ~.600 D + 0.600 CU + 1.0 Wl'C2 D+CU +Wl'C2 53 System Derived 1.000 1.0 D + 1.0 CO +0.750 S + 0.750 Wl'C2 D+CO+S+Wl'C2 D . L dC CSI n oa ombmat ons ~ G" lrt No. Origin Factor Application Description I System 1.000 LOWI> WI> 2 System 1.000 1.0 <W2 j<W2 3 System Derived 1.000 0.700 EB> EB> 4 System Derived 1.000 1.0 Wl'AI Wl'Al 5 System Derived 1.000 1.0 Wl'A2 WPA2 0 6 System Derived 1.000 1.0 WPB! rwral 7 System Derived !.000 1.0 Wl'B2 WPB2 8 System Derived 1.000 .700<EB <EB 9 System Derived 1.000 1.0 Wl'DI WPD! 10 Syst~Derived 1.000 1.0 Wl'D2 WPD2 11 System Derived 1.000 1.0 Wl'CI !WPCl 12 System Derived 1.000 1.0 Wl'C2 Wl'C2 Deflection Load Combinations ~ Purlin No. Origin Factor Deflection APPlication DescriPtion I System 1.000 240 1.0 s s 2 System 1.000 240 l.OUSI* US!' 3 System 1.000 240 l.O*USl *US! Defl tlon L ad C bin t'ons G•rt •• 0 om a 1 -I No. Origin Factor Deflection Application DescriPtion I System 1.000 240 ~.700 WI> WI> 2 System 1.000 240 .700<W2 <W2 File: 7079 Chevron Rl_Stress Check 10_2008 with 08 __ 2008 Loading Version: 7.\a . 07-27053 Calculations Hazardous Materials Occupancy ® ~~ ~~.~~ ~ ·' I Dimension Key 1 4'-0" 2 3'-5 1/4" 3 3'-0" 4 1'-6" 1W180 ~ .4 .. 1 ., 1W181 3.1 , I Maximum Secondary Designs for Sha )C base on Side 1 Detail Des Len Description Design Lap % ld fft) Status lin.) Bnd 1,1 15.00 8.50x0.06S Z Sim Yes 0 1,2 !.50 8.50x0.065 Z Sim Yes 0 2,1 15.00 s:sox0.065 Z Sim Yes 0 2,2 1.50 8.50x0.065 Z Sim Yes 0 3,1 15.00 8.50x0.065 Z Sim Yes 0 3,2 23.00 8.50x0.073 ZC Sim Nest Yes 0 3,3 15.0C 8.50x0.065 Z Sim Yes 0 4,1 15.00 8.50x0.065 Z Sim Yes 0 4,2 23.00 8.50x0.092 Z Sim Yes 0 4,3 15.00 8.50x0.06S Z Sim Yes 0 5,1 15.00 8.50x0.065 Z Sim Yes 0 .. S? <? 321Ne<l\ <> Exterior % % % Ld Shr Cmb Wcp Cs File: 7079 Chevron R l_Sb·ess Check I 0_2008 with 08_2008 Loading ~ -......__ "' "' " 1W1B2 9? Interior Lap % % % % Ld % I on\ Bnd Shr Cmb Wen Cs Bnd 0.82 0.00 0.50 0.00 I O.Ql 0.00 0.01 0.00 I 0.97 0.00 0.59 0.00 I 0.01 0.00 0.01 0.00 I 0.97 0.00 0.59 0.00 I 0.91 0.00 0.00 0.00 I 0.97 0.00 0.59 0.00 I 0.77 0.00 0.47 0.00 I 1.02 0.00 0.00 0.00 I 0.77 0.00 0.47 0.00 I 0.70 0.00 0.00 0.00 I Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Exterior % % % Ld Lap Shr Cmb We Cs ' (in:) 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 70 of 175 5,2 23.00 s.soxo:os2 z Sim Yes 0 1.00 o.oo 0.00 0.00 1 5,3 15.00 8.50x0.065 Z Sim Yes 0 0.68 0.00 0.42 0.00 1 6,1 13.69 8.50x0.065 Z Sim Yes 0 0.44 o.oo 0.27 0.00 1 6,2 23.00 8.50x0.082 Z Sim Yes 0 1.00 o.oo 0.00 0.00 1 6,3 13.69 8.50x0.065 Z Sim Yes 0 0.43 o.oo 0.26 0.00 I 7,1 17.44 8.50x0.092 C Sim Yes 0 1.00 o.oo 1.00 0.00 1 8,1 17.44 8.50x0.092 C Sim Yes 0 1.00 o.oo 1.00 0.00 I 9,1 1.50 8.50x0.065 Z Sim Yes 0 0.01 0.00 0.01 0.00 1 9,2 15.00 8.50x0.065 Z Sim Yes 0 0.82 o.oo 0.50 0.00 1 10,1 1.50 8.50x0.065 Z Sim Yes 0 O.Ql o.oo O.Ql 0.00 1 10,2 15.00 8.50x0.06S·z Sim Yes 0 0.97 o.oo 0.59 0.00 1 11,1 20.00 8.50x0.082 C Sim Yes 0 0.16 o.oo 0.00 0.00 1 12,1 23.00 8.50x0.092 Z Sim Yes 0 0.96 0.00 0.00 0.00 1 Maximum Secondary Deflections for Shape base on Side l Design Id S~g!!!_~?nt Deflection(in)_ Ratio Locatio!l(ft) Load Case Description 1 1 0.28 ( L/646) 7.50 1 W1> 1 2 -- -- 2 1 0.33 ( L/545) 7.50 1 W1> 2 2 -- -- 3 1 0.33 ( L/545) 7.50 1 W1> 3 2 0.84 ( L/329) 26.50 1 W1> 3 3 0.33 ( L/545) 45.50 1 W1> 4 1 0.26 ( L/681) 7.50 1 W1> 4 2 0.93 ( L/298) 26.50 1 W1> 4 3 0.26 (L/681) 45.50 1 W1> 5 1 0.24 ( L/756) 7.50 1 WI> 5 2 0.9I ( L/305) 26.50 I WI> 5 3 0.23 ( LI77I) 45.50 I WI> 6 I O.I3 ( LII308) 7.00 I WI> 6 2 0.9I (L/305) 25.I9 I WI> 6 3 O.I2 ( L/1364) 43.I9 I WI> 7 I 0.86 ( L/245) 8.50 I WI> 8 I 0.86 ( L/245) 8.50 I WI> 9 I ---- 9 2 0.28 ( L/646) 0 9.00 I WI> IO I --- -- IO 2 0.33 ( L/545) 9.00 I WI> II I 0.11 ( LI2I59) 10.00 I WI> I2 I 0.86 .( L/320 i I 1.50 I WI> File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1 a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 71 of 175 . ·' ' , 1 2~1 If"'-"" I Dimension Key l 6" 2 4'~0" 3 3'~5 1/4" 4 3'-3 3/4" 5 1'-3" , '" ?? W2B2,, '-, ').( / "" ""'"/ ' v ?. w~,, W284 v ' 18'-6" Maximum Secondary Designs ·ror Shape base on Side 2 Detail Des Len Description Design Lap % Jd {ft) . Status lin:) Bnd I, I 8.75 8.50x0.059 Z Sim Yes 0 I,2 20.00 8.50x0.073 Z Sim Yes 0 1,3 18.50 8.50x0.065 Z Sim Yes 0 1,4 20.00 8.50x0.07lZ Sim Yes 0 1,5 I8.50 8.50x0.065 Z Sim Yes 0 1,6 20.00 8.50x0.073 Z Sim Yes 0 I,7 18.50 8.50x0.065 Z Sim Yes 0 I,8 20.00 8.50x0.073 Z Sim Yes 0 I,9 8.75 8.50x0.059 Z Sim Yes 0 2,1 8.75 8.50x0.059 Z Sim Yes 0 2,2 20.00 8.50x0.082 Z Sim Yes 0 2,3 I8.50 8.50x0.073 Z Sim Yes 0 2,4 20.00 8.50x0.082 Z Sim Yes 0 2,5 I8.50 8.50x0.073 Z Sim Yes 0 2,6 20.00 8.50x0.082 Z Sim Yes 0 2,7 I8.SO 8.50x0.073 Z Sim Yes 0 2,8 20.00 8.50x0.082 Z Sim Yes 0 2,9 8.75 8.50x0.059 Z Sim Yes 0 3,1 8.75 8.50x0.059 Z Sim Yes 0 3,2 20.00 8.50x0.092 Z Sim Yes 0 3,3 18.50 8.50x0.082 Z Sim Yes 0 3,4 20.00 8.50x0.092 Z Sim Yes 0 3,5 18.50 8.50x0.082 Z Sim Yes 0 3,6 20.00 8.50x0.092 Z Sim Yes 0 3,7 !8.50 8.50x0.082 Z Sim Yes 0 3,8 20.00 8.50x0.092 Z Sim Yes 0 3,9 8.75 8.50x0.059 Z Sim Yes 0 4,1 8.75 8.50x0.059 Z Sim Yes 0 4,2 20.00 8.50X0.092 Z Sim Yes 0 4,3 I8.SO 8.50x0.105 Z Sim Yes 0 4,4 20.00 8.50x0.092 Z Sim Yes 0 4,5 !8.50 8.50x0.0R2 Z Sim Yes 0 " " " W2BS,, Exterior % % % Shr Cmb Wen File: 7079 Chevron R I _Stress Check 10_2008 with 08_2008 Loading iR / fiR 59 ').( ,. V""--- ' I""' " / ' " v ?R ,. 1W2B6 1 , w..,;, ''-W2B8,, 1 2~S v '- 20'..0" I a•.g·~ Interior Exterior Ld Lap % % % % Ld % ?% % % Ld Lap Cs (in:) Bnd Shr Cmb Wen Cs Bnd Shr Cmb We Cs i (in.) 0.33 0.00 0.20 0.00 I 0.97 0.00 0.00 0.00 I 1.03 0.00 0.63 0.00 I 0.97 0.00 0.00 0.00 I 1.03 0.00 0.63 0.00 I 0.97 0.00 0.00 0.00 I 1.03 0.00 0.63 0.00 I 0.97 0.00 0.00 0.00 I 0.33 0.00 0.00 0.00 I 0.36 0.00 0.22 0.00 I 0.93 0.00 0.00 0.00 I 0.95 0.00 0.58 0.00 I 0.93 0.00 0.00 0.00 I 0.95 0.00 0.58 0.00 I 0.93 0.00 0.00 0.00 I 0.95 0.00 0.58 0.00 I 0.93 0.00 0.00 0.00 I 0.36 0.00 0.00 0.00 I 0.43 0.00 0.26 0.00 I 0.98 0.00 0.00 0.00 I 0.96 0.00 0.58 0.00 I 0.98 0.00 0.00 0.00 I 0.96 0.00 0.58 0.00 I 0.98 0.00 0.00 0.00 I 0.96 0.00 0.58 0.00 I 0.98 0.00 0.00 0.00 I 0.43 0.00 0.00 0.00 I 0.43 0.00 0.26 0.00 I 0.98 0.00 0.00 0.00 I 0.00 0.00 0.98 0.00 8 0.98 0.00 0.00 0.00 I 0.96 0.00 0.58 0.00 1 Version: 7.1a 0 07-27053 Calculations Hazardous Materials Occupancy 4,6 20.00 8.50x0.092 Z S1m Yes 0 0.98 0.00 0.00 0.00 I 4,7 I8.50 8.50x0.105 Z Sim Yes 0 0.00 0.00 0.98 0.00 3 4,8 20.00 8.50x0.092 ZSim Yes 0 0.98 0.00 0.00 0.00 I 4,9 8.75 8.50x0.059 Z Sim Yes 0 0.43 o.oo 0.00 0.00 I 5,I 8.75 8.50x0.059 Z Sim Yes 0 0.36 0.00 0.22 0.00 I 5,2 20.00 8.50x0.082 Z Sim Yes 0 0.92 0.00 0.00 0.00 I 5,3 I8.50 8.50x0.073 Z Sim Yes 0 0.94 0.00 0.57 0.00 I 5,4 20.00 8.50x0.082 ZSim Yes 0 0.92 0.00 0.00 0.00 I 5,5 I8.50 8.50x0.073 Z Sim Yes 0 0.94 0.00 0.57 0.00 I 5,6 20.00 8.50x0.082 Z Sim Yes 0 0.92 0.00 0.00 0.00 I 5,7 I8.50 8.50x0.073 Z Sim Yes 0 0.94 0.00 0.57 0.00 I 5,8 20.00 8.50x0.082 Z Sim Yes 0 0.92 0.00 0.00 0.00 I 5,9 8.75 8.50x0.059 Z Sim Yes 0 0.36 0.00 0.00 0.00 I 6,I 8.75 8.50x0.059 Z Sim Yes 0 0.20 0.00 O.I2 0.00 I 6,2 20.00 8.50x0.059 Z Sim Yes 0 0.86 0.00 0.00 0.00 I 6,3 I8.50 8.50x0.059 Z Sim Yes 0 0.74 0.00 0.45 0.00 I 6,4 20.00 8.50x0.059 Z Sim Yes 0 0.86 0.00 0.00 0.00 I 6,5 I8.50 8.50x0.059 Z Sim Yes 0 0.74 0.00 0.45 0.00 I 6,6 20.00 8.50x0.059 Z Sim Yes 0 0.86 0.00 0.00 0.00 I 6,7 I8.50 8.50x0.059 Z Sim Yes 0 0.74 0.00 0.45 0.00 I 6,8 20.00 8.50x0.059 Z Sim Yes 0 0.86 0.00 0.00 0.00 I 6,9 8.75 8.50x0.059 Z Sim Yes 0 0.20 0.00 0.00 0.00 I ' for Shape base on Side 2 Design ld Segment F~ load Case : ; 0.04 4.50 : WI> 0.63 I8.75 WI> I 3 0.53 L/417) 37.75 I WI> I 4 0.63 ( L/38I) 57.25 I WI> I 5 0.53 ( L/4I7) 76.25 I WI> I 6 0.63 ( L/38I) 95.75 I WI> I 7 0.53 ( L/417) II4.75 I WI> I ' 8 0.63 ( L/381) 134.25 I WI> I 9 0.04 ( L/2956) I48.75 I· WI> 2 I 0.04 ( L/2639) 4.50 I WI> 2 2 0.64 ( L/377) 18.75 I WI> 2 3 0.53 ( L/420) 38.25 I WI> 2 4 0.64 ( L/377) 57.25 I WI> 2 5 0.53 ( L/420) 76.75 I WI> 2 6 0.64 ( L/377) 95.75 I WI> 2 7 0.53 (L/420) 115.25 I WI> 2 8 0.64 ( L/377) I34.25 I WI> 2 9 0.04 ( L/2636) I48.75 I WI> 3 I 0.05 ( L/2262) 4.50 I WI> 3 2 0.67 ( L/356) I8.75 I WI> 3 3 0.56 ( L/398) 37.75 I WI> 3 4 0.67 ( L/356) 57.25 I WI> 3 5 0.56 ( L/398) 76.25 I WI> 3 6 0.67 ( L/356) 95.75 I WI> 3 7 0.56 ( L/398) 114.75 I WI> 3 8 0.67 ( L/356) I34.25 I WI> 3 9 0.05 ( L/2260) I48.75 I WI> 4 I 0.05 ( L/2262) 4.50 I WI> 4 2 0.67 ( L/356) 18.75 I WI> 4 3 0.44 ( L/506) 37.75 I WI> 4 4 0.67 ( L/356) 57.25 I WI> 4 5 0.56 ( L/398) 76.25 I WI> 4 6 0.67 ( L/356) 95.75 I WI> 4 7 0.44 ( L/506) Il4.75 I WI> 4 8 0.67 ( L/356) I34.25 I WI> 4 9 0.05 ( L/2260) I48.75 I WI> 5 I 0.04 ( L/2674) 4.50 I WI> 5 2 0.63 ( L/382) 18.75 I WI> 5 3 0.52 ( L/427) 37.75 I WI> 5 4 0.63 ( L/382) 57.25 I WI> 5 5 0.52 ( L/427 ) 76.25 I WI> 5 6 0.63 ( L/382) 95.75 I WI> File: 7079 Chevron R !_Stress Check I 0 _2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 72 ofl7 5 07-27053 Calculations Hazardous Materials Occupancy 5 7 0.52 ( L/427) 114.75 1 W1> 5 8 0.63 ( L/382) 134.25 1 W1> 5 9 0.04 ( L/2672) 148.75 1 W1> 6 1 0.00 ( L/4717) 4.50 1 W1> 6 2 0.49 ( L/488) 18.75 1 W1> 6 3 0.36 ( L/611) 37.75 1 W1> 6 4 0.49 ( L/488) 57.25 1 W1> 6 5 0.36 (L/611) 76.25 1 W1> 6 6 0.49 ( L/488) 95.75 1 W1> 6 7 0.36 (L/611) 114.75 1 W1> 6 8 0.49 ( L/488) 134.25 1 W1> 6 9 0.00 (.L/4713,) 148.75 1 W1> Pile: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 73 of 175 07-27053 Calculations Hazardous Materials Occupancy ~ ~~ ~~ :=-------~ 4.1 4 " ; 1W3BO 11 I Dimension Key I 4'~0" 2 3'-5 1/4" 3 3'..0" 4 1'~6" 1W3B1 .~ Maximum Secondary Designs for Shape base on Side 3 Detail Des Len Description Design Lap % Id Lft) _:_ Status _(in.) Bnd 1,1 15.00 8.SOx0.065 Z Sim Yes 0 1,2 1.50 8.50x.0.065 Z Sim Yes 0 2,1 15.00 8.50x0.065 Z Sim Yes 0 2,2 1.50 8.50x0.065 Z Sim Yes 0 3,I 15.00 8.50x.0.065 Z Sim Yes 0 3,2 23.00 8.50x0.073 ZC Sim Nest Yes 0 3,3 15.00 8.50x0.065 Z Sim Yes 0 4,1 15.00 8.50x0.065 Z Sim Yes 0 4,2 23.00 8.50x0.092 Z Sim Yes 0 4,3 15.00 8.50x0.065 Z Sim Yes 0 5,1 15.00 8.50x0.065 Z Sim Yes 0 -'? .4? 4? '?JN '" Exterior % % % Ld Shr Cmb Wco Cs File: 7079 Chevron R I_ Stress Check I 0 _ 2008 with 08 _ 2008 Loading ~ --------- " " " .10.2. ; 1W3B2 ., Interior Lap % % % % Ld % (in:) Bnd Shr Cmb Wcp Cs Bnd 0.82 0.00 0.50 0.00 I O.ot 0.00 O.oJ 0.00 I 0.97 0.00 0.59 0.00 I 0.01 0.00 0.01 0.00 I 0.97 0.00 0.59 0.00 I 0.91 0.00 0.00 0.00 I 0.97 0.00 0.59 0.00 I 0.77 0.00 0.47 0.00 I 1.02 0.00 0.00 0.00 I 0.77 0.00 0.47 0.00 I 0.70 0.00 0.00 0.00 I Version: 7.la Date: 10/20/2008 Time: 1:57:43 PM Exterior % % % Ld Lap Shr Cmb Wcp Cs lin:) 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 75 of 175 5,2 23.00 8.50x0.082 ZSim Yes 0 1.00 0.00 0.00 0.00 I 5,3 15.00 8.50x0.065 Z Sim · Yes 0 0.68 0.00 0.42 0.00 I 6,1 13.69 8.50x0.065 Z Sim Yes 0 0.44 0.00 0.27 0.00 I 6,2 23.00 8.50x0.082 Z Sim Yes 0 1.00 0.00 0.00 0.00 I 6,3 13.69 8.50x0.065 Z Sim Yes 0 0.43 0.00 0.26 0.00 I 7,1 17.44 8.50x0.092 C Sim Yes 0 1.00 0.00 1.00 0.00 I 8,1 17.44 8.50x0.092 C Sim Yes 0 1.00 0.00 1.00 0.00 1 9,1 1.50 8.50x0.065 Z Sim Yes 0 0.01 0.00 0.01 0.00 1 9,2 15.00 8.50x0.065 Z Sim Yes 0 0.82 0.00 0.50 0.00 1 10,1 1.50 8.50x0.065 Z Sim Yes 0 O.Ql 0.00 O.Ql 0.00 1 10,2 15.00 8.50x.0.065 Z Sim Yes 0 0.97 0.00 0.59 0.00 1 ll,l 20.00 8.50x0.082 C Sim Yes 0 0.16 0.00 0.00 0.00 1 12,1 23.00 8.50X0.092 Z Sim Yes 0 0.96 0.00 0.00 0.00 1 M' S d D 0 • ~ Sh b ax1mum econ arv e ectwns or ape ase on Sid 3 e Design Id Segment Deflection(in.) Ratio Location(ft) Load Case Description 1 1 0.28 ( U646) 7.50 I W1> 1 2 ---- 2 1 0.33 ( L/545) 7.50 I W1> 2 2 ---- 3 1 0.33 ( U545) 7.50 1 WI> 3 2 0.84 ( U329) 26.50 1 W1> 3 3 0.33 ( U545) 45.50 1 W1> 4 1 0.26 ( U681) 7.50 1 W1> 4 2 0.93 ( U298) 26.50 1 W1> 4 3 0.26 ( U681) 45.50 1 WI> 5 1 0.24 (U756) 7.50 I WI> 5 2 0.91 (U305) 26.50 I WI> 5 3 0.23 (U77I) 45.50 I WI> 6 I O.I3 (U1308) 7.00 1 WI> 6 2 0.91 (U305) 25.I9 I WI> 6 3 O.I2 (U1364) 43.19 I WI> 7 I 0.86 ( U245) 8.50 I WI> 8 0 I 0.86 ( U245) 8.50 I 0 WI> 9 I ----- 9 2 0.28 ( U646) 9.00 I W1> 10 I ----- 10 2 0.33 (U545) 9.00 1 WI> 11 I 0.11 ( U2I59) 10.00 I WI> 12 I . 0.86 fU320l Il.50 1 WI> File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: ?.Ia 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 76 of 175 A fi1 4 1. . 1 451 Dimension Key 1 6" 2 4'-0" 3 3'-5 1/4" 4 3'-3 3/4" 5 1'-3" 6 2'..0" 7 1'-63/4" 8 l'-0" A? '" 20'..()" 1'-A? / R ').;( 5 v 43. '- ~:". / ' w~ v " 18'.N Maximum Secondarv Desie:ns for Shape base on Side 4 Detail Des Len Description Design Lap % ld (ft) Status . (in) Bnd 1,1 8.75 8.50x0.059 Z Sim Yes 0 1,2 2.00 8.50x0.059 Z Sim Yes 0 2,1 8.75 8.50x0.059 Z Sim Yes 0 2,2 2.00 8.50x0.059 Z Sim Yes 0 3,1 8.75 8.50x0.059 Z Sim Yes 0 3,2 2.00 8.50x0.059 Z Sim Yes 0 4,1 8.75 8.50x0.059 Z Sim Yes 0 4,2 '20.00 8.50x0.073 Z Sim Yes 0 4,3 18.50 8.SOxO.l05 Z Sim Yes 0 4,4 20.00 8.50x0.073 Z Sim Yes 0 4,5 18.50 8.50x0.082 Z Sim Yes 0 4,6 20.00 8.50X0.073 Z Sim Yes 0 4,7 18.50 8.50x0.105 ZSim Yes 0 4,8 20.00 8.50x0.092 Z Sim Yes 0 4,9 8.75 8.50x0.059 Z Sim Yes 0 5,1 8.75 8.50x0.059 Z Sim Yes 0 5,2 20.00 8.50x0.073 Z Sim Yes 0 5,3 18.50 8.50x0.082 Z Sim Yes 0 5,4 20.00 8.50x0.073 Z Sim Yes 0 5,5 18.50 8.50x0.082 Z Sim Yes 0 5,6 20.00 8.50x0.073 Z Sim Yes 0 5,7 18.50 8.50x0.082 Z Sim Yes 0 5,8 20.00 8.50xQ.092 Z Sim Yes 0 5,9 8.75 8.50x0.059 Z Sim Yes 0 6,1 8.75 8.50x0.059 Z Sim Yes 0 6,2 20.00 8.50x0.082 Z Sim Yes 0 6,3 18.50 8.50:&073 Z Sim Yes 0 6,4 20.00 8.50x0.082 Z Sim Yes 0 6,5 !8.50 8.50x0.073 Z Sim Yes 0 Afi fi5 45_ ,, . "' W4B;,, Exterior % % % Ld Shr Cmb Wcp Cs File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading AA "' A7 / AA AA fi x "' fiQ /n"-._ 4R 49 ~ / . v, '" ,,. w4£'b, '" 1W4B& 1 V411!l. / " 18'-6~ 20'.0" ~ Interior 0 Exterior Lap % % % % Ld % % % % Ld Lap l_(in:) Bnd Shr Cmb Wcp Cs Bnd Shr Cmb Wcp Cs I (in:) 0.33 0.00 0.20 0.00 1 0.02 0.00 0.00 0.00 1 0.36 0.00 0.22 0.00 1 0.02 0.00 0.00 0.00 1 0.43 0.00 0.26 0.00 1 0.02 0.00 o.oo 0.00 1 0.43 0.00 0.26 0.00 1 0.92 0.00 0.00 0.00 1 0.00 0.00 0.98 0.00 3 0.92 0.00 0.00 0.00 1 0.96 0.00 0.58 0.00 1 0.92 0.00 0.00 0.00 1 0.00 0.00 0.98 0.00 8 0.98 0.00 0.00 0.00 1 0.43 0.00 0.00 0.00 1 0.43 0.00 0.26 0.00 1 0.98 0.00 o.oo 0.00 1 0.96 0.00 0:58 0.00 1 0.98 0.00 0.00 0.00 1 0.96 0.00 0.58 0.00 1 0.98 0.00 o.oo 0.00 1 0.96 0.00 0.58 0.00 1 0.98 0.00 0.00 0.00 1 0.43 0.00 o.oo 0.00 1 0.36 0.00 0.22 0.00 1 0.92 0.00 0.00 0.00 1 0.94 0.00 0.57 0.00 1 0.92 0.00 0.00 0.00 1 0.94 0.00 0.57 0.00 1 Version: 7.la . 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 77 of 175 6,6 6,7 6,8 6,9 7,1 7,2 7,3 7,4 7,5 7,6 7,7 7,8 7,9 8,1 9,1 10,1 11;1 11,2 11,3 12,1 13,1 13,2 13,3 14,1 15,1 16,1 17,1 18,1 19,1 20,1 21,1 21,2 21,3 c 21,4 22,1 0 22,2 22,3 22,4 23,1 23,2 23,3 23,4 20.00 18.50 20.00 8.75 8.75 20.00 18.50 20.00 18.50 20.00 18.50 20.00 8.75 17.44 17.44 16.00 2.00 18.50 2.00 16.00 2.00 18.50 2.00 16.00 16.00 . 20.00 17.44 17.4< 17.44 17.44 2.00 18.50 20.00 8.75 2.00 18.50 20.00 8.75 2.00 18.50 20.00 8.75 8.50x0.082 Z Sim 8.50x0.073 Z Sim 8.50x0.082 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.082 C Sim 8.50x0.082 C Sim 8.50x0.059 C Sim 8.50x0.059 Z Sim 8.50x0.073 Z Sim 8.50x0.059 Z Sim 8.50x0.059 C Sim 8.50x0.059 Z Sim 8.SOx0.082 Z Sim 8.50x0.059 Z Sim 8.50x0.082 C Sim 8.50x0.082 C Sim 8.50x0.059 Z Sim 8.50x0.082 C Sim 8.501<0.082 C Sim 8.50x0.082 C Sim 8.50x0.082 C Sim 8.50x0.059 Z Sim 8.50x0.065 Z Sim 8.50x0.073 Z Sim 8.50x0.059 Z Sim 8.SOx0.059 Z Sim 8.50x0.073 Z Sim 8.50x0.082 Z Sim 8.50x0.059 Z Sim 8.50x0.059 Z Sim 8.50x0.082 Z Sim 8.50x0.092 Z Sim 8.50x0.059 Z Sim Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 .. 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 s fl Maximum econdary De ections for Shane base on Side 4 Design ld Segment Deflection(in.) Ratio I I 0.04 ( L/2958) I 2 -- 2 I 0.04 ( L/2639) 2 2 -- 3 I 0.05 (L/2262) 3 2 - - 4 I 0.05 ( L/2262) 4 2 0.96 ( L/251) 4 3 0.44 ( L/506) 4 4 0.96 ( L/251) 4 5 0.56 ( L/398) 4 6 0.96 ( L/251) 4 7 0.44 ( L/506) 4 8 0.67 ( L/356) 4 9 0.05 ( L/2260) 5 I 0.05 ( L/2262) 5 2 0.64 ( L/378) 5 3 0.56 ( L/398) 5 4 0.64 ( L/378) 5 5 0.56 ( L/398) 5 6 0.64 ( L/378) 5 7 0.56 ( L/398) Location(ft) 4.50 - 4.50 - 4.50 - 4.50 18.75 37.75 57.25 76.25 95.75 114.75 134.25 148.75 4.50 18.75 37.75 57.25 76.25 95.75 114.75 0.92 0.00 0.00 0.00 I 0.94 0.00 0.57 0.00 I 0.92 0.00 0.00 0.00 1 0.36 0.00 0.00 0.00 1 0.20 0.00 0.12 0.00 I 0.86 0.00 0.00 0.00 I 0.74 0.00 0.45 0.00 I 0.86 0.00 0.00 0.00 I 0.74 0.00 0.45 0.00 I 0.86 0.00 0.00 0.00 I 0.74 0.00 0.45 0.00 I 0.86 0.00 0.00 0.00 I 0.20 0.00 0.00 0.00 I 0.94 0,09 0.94 O.OQ I 0.94 0.09 0.94 0.00 1 1.00 0.00 0.00 0.00 I 0.02 0.00 0.00 0.00 I 0.95 0.00 0.58 0.00 I 0.02 0.00 0.00 0.00 I 0.78 0.00 0.00 0.00 I 0.02 0.00 0.00 0.00 I 0.96 0.00 0.58 0.00 I 0.02 0.00 0.00 0.00 I 0.12 0.00 0.00 0.00 I 0.18 0.00 0.00 0.00 I 0.94 0.00 0.00 0.00 l 0.94 0.09 0.94 0.00 I 0.94 O.o9 0.94 0.00 I 0.94 0.09 0.94 0.00 I 0.94 0,09 0.94 0.00 1 0.02 0.00 0.00 0.00 l 1.03 0.00 0.63 0.00 I 0.97 0.00 0.00 0.00 I 0.33 0.00 0.00 0.00 I 0.02 0.00 0.00 0.00 1 0.95 0.00 0.58 0.00 I 0.93 0.00 0.00 0.00 I 0.36 0.00 0.00 0.00 1 0.02 0.00 0.00 0.00 I 0.96 0.00 0.58 0.00 1 0.98 0.00 0.00 0.00 I 0.43 0.00 0.00 0.00 I Load Case 1 I - I - I I I I I 1 1 I I I I I I I I I Description WI> WI> - WI> - WI> WI> WI> WI> WI> WI> WI> WI> WI> WI> WI> WI> WI> WI> WI> WI> File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading· Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy 5 8 0.67 ( LIJ56) 134.25 I WI> 5 9 0.05 ( L/2260) 148.75 I WI> 6 I 0.04 ( L/2674) 4.50 I WI> 6 2 0.63 ( L/382) 18.75 I WI> 6 3 0.52 ( L/427) 37.75 I WI> 6 4 0.63 ( L/382) 57.25 I WI> 6 5 0.52 ( L/427) 76.25 I WI> 6 6 0.63 ( LIJ82) 95.75 I WI> 6 7 0.52 ( L/427) I 14.75 I WI> 6 8 0.63 ( L/382) 134.25 I WI> 6 9 0.04 ( L/2672) 148.75 I WI> 7 I 0.00 ( L/4717) 4.50 I WI> 7 2 0.49 ( L/488) 18.75 I WI> 7 3 0.36 (L/611) 37.75 I WI> 7 4 0.49 ( L/488) 57.25 I WI> 7 5 0.36 (L/611) 76.25 I WI> 7 6 0.49 ( L/488) 95.75 I WI> 7 7 0.36 (L/611) 114.75 I WI> 7 8 0.49 ( L/488) 134.25 I WI> 7 9 0.00 . (L/4713) 148.75 I WI> 8 I 0.77 ( LI27I ) 8.50 I WI> 9 I 0.77 ( LI27I ) 8.50 I WI> 10 I 0.39 (L/492) 8.00 I WI> II I ----- II 2 0.53 ( L/420) 11.50 I WI> II 3 ---- 12 I 0.30 ( L/632) 8.00 I WI> 13 I ----- 13 2 0.56 ( L/398) 11.00 I WI> I3 3 ---. . I4 I 0.05 ( L/3760) 8.00 I WI> IS I 0.08 (L/2410) 8.00 I WI> 16 I 0.54 (L/446) IO.OO I WI> 17 I 0.77 ( LI27I) 8.50 I ) WI> I8 I 0.77 ( LI27I ) 8.50 I WI> 19 I 0.77 ( LI27I) 8.50 I WI> 20 I 0.77 ( L/271) 8.50 I WI> 21 I . . -. . 2I 2 0.53 (L/417) 11.00 I WI> 21 3 0.63 ( LI38I ) 30.50 I WI> 2I 4 0.04 ( L/2956) 45.00 I WI> 22 I . . . . . 22 2 0.53 ( L/420) Il.50 I WI> 22 3 0.64 ( L/377) 30.50 I WI> 22 4 0.04 ( L/2636) 45.00 I WI> 23 I . -. . . 23 2 0.56 ( L/398) . 11.00 I WI> 23 3 0.67 / L/356,\ 30.50 I WI> 23 4 0.05 L/2260 45.00 I WI> File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008loading Version: 7.1a [)ate: 10/20/2008 Time: I :57:43 PM Page: 78 ofl75 . Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy _/i2_ 57 R 1 20'-0" 18'.6" 20'.0" 21)'.0" 18'.6' I a•.g~ !'f(' Maximum Secondarv Deshms for Sba e base on Side A Detail Exterior Interior Exterior Des Len Description Design Lap % % % % Ld Lap % % % % Ld % % % % Ld Lap ld (ft) Status (in:) Bnd Shr Cmb Wcp Cs (in:) Bnd Shr Cmb Wcp Cs Bnd Shr Cmb Wcp Cs I (in:) 1,1 9.25 11.50x0.065 Z Sim Yes 0 0.02 1.01 1.01 0.00 3 2,1 9.25 11.50x0.065 Z Sim Yes 0 O.ol 0.78 0.78 0.00 3 3,1 9.25 ll.SOx0.065 Z Sim Yes 0 O.ol 0.42 0.42 0.00 3 4,1 20.00 11.50x0.120 Z Con Yes 24 0.77 0.00 0.77 0.00 3 0.57 0.22 0.61 0.00 3 24 4,2 18.50 11.50x0.120 ZCon Yes 36 0.57 0.18 0.60 0.00 3 36 0.13 0.06 0.79 0.00 23 0.52 0.24 0.57 0.00 3 36 4,3 20.00 11.50x0.08231Z Con Yes 48 0.52 0.27 0.59 0.00 3 36 0.38 0.81 0.89 0.00 3 0.74 0.58 0.94 0.00 3 36 4,4 18.50 ll.SOx0.082 Z Con Yes 36 0.74 0.53 0.91 0.00 3 36 0.49 0.71 0.86 0.00 3 0.74 0.53 0.91 0.00 3 36 4,5 20.00 11.50x0.082 Z Con Yes 48 0.74 0.58 0.94 0.00 3 36 0.38 0.81 0.89 0.00 3 0.52 0.27 0.59 0.00 3 36 4,6 18.50 ll.SOxO.l20 Z Con Yes 36 0.52 0.24 0.57 0.00 3 36 0.13 0.06 0.79 0.00 27 0.57 0.18 0.60 0.00 3 36 4,7 20.00 ll.SOxO.l20 ZCon Yes 24 0.5, 0.22 0.61 0.00 3 24 0.77 0.00 0.77 0.00 3 5,1 20.00 11.50x0.082 Z Con Yes 36 0.98 0.00 0.98 0.00 3 0.76 0.55 0.93 0.00 3 36 5,2 18.50 11 .50x0.082 Z 'Con Yes 36 0.76 0.45 0.88 0.00 3 36 0.67 0.63 0.92 0.00 3 0.51 0.38 0.64 0.00 3 36 5,3 20.00 l1.50x0.082 Z Con Yes 48 0.51 0.44 0.68 0.00 3 48 0.54 0.73 0.91 0.00 3 0.69 0.60 0.92 0.00 3 48 5,4 18.50 11.50x0.065 Z Con Yes 36 0.69 0.55 0.88 0.00 3 24 0.29 0.94 0.98 0.00 3 0.69 0.55 0.88 0.00 3 24 5,5 20.00 ll.S0x0.082 Z Con Yes 48 0.69 0.60 0.92 0.00 3 48 0.54 0.73 0.91 0.00 3 0.51 0.44 0.68 0.00 3 48 5,6 18.50 ll.S0x0.082 Z Con Yes 36 0.5! 0.38 0.64 0.00 3 36 0.67 0.63 0.92 0.00 3 0.76 0.45 0.88 0.00 3 36 5,7 20.00 11.50x0.082 Z Con Yes 36 0.76 0.55 0.93 0.00 3 36 0.98 0.00 0.98 0.00 3 6,1 20.00 ll.SOx0.065 Z Con Yes 36 0.36 0.89 0.96 0.00 3 0.61 0.59 0.85 0.00 3 36 6,2 18.50 ll.50x0.065 Z Con Yes 36 0.61 0.48 0.78 0.00 3 36 0.54 0.67 0.86 0.00 3 0.41 0.40 0.57 0.00 3 36 6,3 20.00 11.50x.0.065 Z Con Yes 48 0.41 0.47 0.62 0.00 3 24 0.43 0.78 0.89 0.00 3 0.46 0.49 0.67 0.00 3 24 6,4 18.50 11.50x0.065 Z Con Yes 36 0.46 0.44 0.64 0.00 3 24 0.48 0.69 0.84 0.00 3 0.46 0.44 0.64 0.00 3 24 6,5 20.00 11 .50x0.065 Z Con Yes 48 0.46 0.49 0.67 0.00 3 24 0.43 0.78 0.89 0.00 3 0.41 0.47 0.62 0.00 3 24 6,6 18.50 ll.50x0.065 Z Con Yes 36 0.41 0.40 0.57 0.00 3 36 0.54 0.67 0.86 0.00 3 0.61 0.48 0.78 0.00 3 36 6,7 20.00 ll.50x0.065 Z Con Yes 36 0.61 0.59 0.85 0.00 3 36 0.36 0.89 0.96 0.00 3 7,1 9.25 ll.S0x0.065 Z Sim Yes 0 0.02 1.0 I 1.01 0.00 3 8,1 9.25 11.50x0.065 Z Sim Yes 0 O.ot 0.78 0.78 0.00 3 9,1 9.25 11.50x0.065 Z Sim Yes 0 O.oi 0.42 0.42 0.00 3 Maximum Secondary Deflections for Shape base on Side A DesigD Id Seg_rnent Deflectioqfin_)_ Ratio Locatio!:l([t) Load Case Description I I -o.o8 ( L/1337) 5.00 3 *US! 2 I -0.06 ( L/1725) 5.00 3 *US! 3 I -0.03 ( L/3257) 5.00 3 *USl 4 I -0.55 ( L/435) 8.50 3 "'USl 4 2 0.08 ( L/2678) 24.00 3 *US! 4 3 -0.35 ( L/695) 48.50 3 *US! 4 4 -0.06 ( L/3525) 67.50 3 *US! 4 5 -0.35 ( L/694) 87.00 3 "'US! 4 6 0.08 ( L/2676) 111.50 3 *US I File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 80 of 175 4 7 -0.56 ( L/432 ) 126.50 3 "'US! 5 I -0.60 ( L/399) 8.50 3 *US! 5 2 0.08 ( L/2731) 24.00 3 *US! 5 3 -0.28 ( L/852) 48.00 3 *USl 5 4 -0.08 ( L/2852) 67.50 3 *US I 5 5 -0.28 ( L/848) 87.00 3 *US! 5 6 0.08 ( L/2703) 111.50 3 *US! 5 7 -0.61 ( L/396) 126.50 3 *US! 6 I -0.41 ( L/589) 8.50 3 *US! 6 2 0.05 ( L/4054) 24.00 3 *US! 6 3 -0.20 (L/1180) 48.00 3 *US! 6 4 -0.03 ( L/6564) 67.50 3 *US I 6 5 -0.20 (L/1176) 87.00 3 *US! 6 6 0.05 (L/4110) 111.50 3 *USl 6 7 -0.41 ( L/585) 126.50 3 *USl 7 1 -0.08 ( L/1337) 4.50 3 "'US! 8 1 -0.06 ( L/1726) 4.50 3 ·*USI 9 I -0.03 i L/3257) 4.50 3 *US! Purlfn Ancboraee Forces for Shape base Roof A Panel TYl te is PR. Pitch= 4.000:12 Bay Thickness Force(k) Ld Case # Purlins Length Simple?· Diaphragm fA11owable Defl Actual Deft Width I 0.065 -35.24 3 10 9.25 y 27.93 0.308 0.000 2 0.082 -76.20 3 10 20.00 N 27.93 0.667 0.000 3 0.082 -70.49 3 10 18.50 N 27.93 0.617 0.000 4 0.082 -76.20 3 10 20.00 N 27.93 0.667 0.000 5 0.065 -70.49 3 10 18.50 N 27.93 0.617 0.000 6 0.082 -76.20 3 10 20.00 N 27.93 0.667 0.000 7 0.082 -70.49 3 10 18.50 N 27.93 0.617 0.000 8 0.082 -76.20 3 10 20.00 N 27.93 0.667 0.000 9 0.065 -35.24 3 10 9.25 y 27.93 0.308 0.000 Frm~Line Force k) Anch.Allow Required Clips Actual Clips Diaphragm Allow Diaphragm Shr Stress 1 0.08 0.00 0 0 0.134 0.000 0.000 2 0.87 0.00 0 0 0.134 0.000 0.000 3 1.40 0.00 0 0 0.134 0.000 0.000,. 4 1.40 0.00 0 0 0.134 0.000 0.000- 5 1.74 0.00 0 0 0.134 0.000 0.000 6 1.74 0.00 0 0 0.134 0.000 0.000 7 1.40 0.00 0 0 0.134 0.000 0.000 8 1.40 0.00 0 0 0.134 0.000 0.000 9 0.87 0.00 0 0 0.134 0.000 0.000 10 0.08 0.00 0 0 0.134 0.000 0.000 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 81 of 175 ) . . ,, ·' 20'..0" 18'-6" 20'.0" 18'-6" 20'.0" 18'.6" 20'.0" J 8'-9" !fl' Maximum Secondary Designs for Shape base on Side B Detail Exterior Interior Exterior Des Len Description Design Lap % % % % Ld Lap % % % % Ld % % % % Ld Lap ld (ft) Status on:) Bnd Sh' Cmb Wcp Cs fin:) Bnd Sh' Cmb Wcp Cs Bnd Sh' Cmb Wcp Cs lin:) 1,1 9.25 11.50x0.065 Z Sim Yes 0 0.02 1.01 1.01 0.00 2 2,1 9.25 l1.50x0.065 Z Sim Yes 0 0.01 0.78 0.78 0.00 2 3,1 9.25 11.50x0.065 Z Sim Yes 0 0.01 0.42 0.42 0.00 2 4,1 20.00 11.50x0.120 Z Con Yes 24 0.77 0.00 0.77 0.00 2 0.57 0.22 0.61 0.00 2 24 4,2 !8.50 ll.50x0.120 ZCon Yes 36 0.57 0.18 0.60 0.00 2 36 0.13 0.06 0.79 0.00 27 0.52 0.24 0.57 0.00 2 36 4,3 20.00 11.50x0.082 Z Con Yes 48 0.52 0.27 0.59 0.00 2 36 0.38 0.81 0.89 0.00 2 0.7'\: 0.58 0.94 0.00 2 36° 4,4 18.50 ll.50x0.082 Z Con Yes 36 0.74 0.53 0.91 0.00 2 36 0.49 0.71 0.86 0,00 2 0.74 0.53 0.91 0.00 2 36 4,5 20.00 ll.SOx0.082 ZCon Yes 48 0.74 0.5§ 0.94 0.00 2 36 0.38 0.81 0.89 0.00 2 0.52 0.27 0.59 0.00 2 36 4,6 18:5o l1.50x0.120 Z Con Yes 36 0.52 0.24 0.57 0.00 2 36 0.13 0.06 0.79 0.00 23 0.57 0.18 0.60 0.00 2 36 4,7 20.00 ll.50x0.120 ZCon Yes 24 0.57 0.22 0.61 0.00 2 24 0.77 0.00 0.77 0.00 2 . 5,1 20.00 11.50x0.082 Z Con Yes 36 0.98 0.00 0.98 0.00 i 0.76 0.55 0.93 0.00 2 36 5,2 18.50 11.50x0.082 Z Con Yes 36 0.76 0.45 0.88 0.00 2 36 0.67 0.63 0.92 0.00 2 0.51 0.38 0.64 0.00 2 36 5,3 20.00 11.50x0.082 ZCon Yes 48 0.51 0.44 0.68 0.00 2 48 0.54 0.73 0.91 0.00 2 0.69 0.60 0.92 0.00 2 48 5,4 18.50 11.50x0.065 Z Con Yes 36 0.69 0.55 0.88 0.00 2 24 0.29 0.94 0.98 0.00 2 0.69 0.55 0.88 0.00 2 24 5,5 20.00 11.50x0.082 ZCon Yes 48 0.69 0.60 0.92 0.00 2 48 0.54 0.73 0.91 0.00 2 0.51 0.44 0.68 0.00 2 48 5,6 18.50 ll.50x0.082 Z Con Yes 36 0.51 0.38 0.64 0.00 2 36 0.67 0.63 0.92 0.00 2 0.76 0.45 0.88 0.00 2 36 5,7 20.00 11.50x0.082 Z Con Yes 36 0.76 0.55 0.93 0.00 2 36 0.98 0.00 0.98 0.00 2 6,1 20.00 l1.50x0.065 Z Con Yes 36 0.36 0.89 0.96 0.00 2 0.61 0.59 0.85 0.00 2 36 6,2 18.50 11.50x0.065 Z Con Yes 36 0.61 0.48 0.78 0.00 2 36 0.54 0.67 0.86 0.00 2 0.41 0.40 0.57 0.00 2 36 6,3 20.0 ll.50x0.065 z Con Yes 48 0.41 0.47 0.62 0.00 2 24 0.43 0.78 0.89 0.00 2 0.46 0.49 0.67 0.00 2 24 6,4 18.50 11.50x0.065 z Con Yes 36 0.46 0.44 0.64 0.00 2 24 0.48 0.69 0.84 0.00 2 0.46 0.44 0.64 0.00 2 24 6,5 20.00 ll.SOx0.065 ZCon Yes 48 0.46 0.49 0.67 0.00 2 24 0.43 0.78 0.89 0.00 2 0.41 0.47 0.62 0.00 2 24 6,6 18.50 II.SOx.0.065 ZCon Yes 36 0.41 0.40 0.57 0.00 2 36 0.54 0.67 0.86 0.00 2 0.61 0.48 0.78 0.00 2 36 6,7 20.00 11.50x0.06S ZCon Yes 36 0.61 0.59 0.85 0.00 2 36 0.36 0.89 0.96 0.00 2 7,1 9.25 1 J.50x0.065 Z Sim Yes 0 0.02 1.0 I 1.01 0.00 2 8,1 9.25 II .S0x0.06S Z Sim Yes 0 O.QI 0.78 0.78 0.00 2 9,1 9.25 11.50x0.065 Z Sim Yes 0 0.01 0.42 0.42 0.00 2 Maximum Secondarv Deflections for Shape base on Side B Design Id Segment Deflection in.) Ratio Location(ft) Load Case Description 1 I -0.08 ( L/1337) 5.00 2 US!* 2 I -0.06 (L/1725) 5.00 2 US!* 3 I -0.03 ( L/3257) 5.00 2 US!* 4 I -0.55 ( L/435) 8.50 2 US!* 4 2 0.08 ( L/2678) 24.00 2 US I* 4 3 -0.35 ( L/695) 48.50 2 US!* 4 4 -0.06 ( L/3525) 67.50 2 US!* 4 5 -0.35 ( !./694) 87.00 2 US!* 4 6 0.08 ( l./2676) Ill. SO 2 US!* File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: ?.la 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 82 of 175 4 7 -0.56 ( U432) 126.50 2 US!* 5 I -0.60 ( L/399) 8.50 2 US!* 5 2 0.08 ( L/2731) 24.00 2 US!* 5 3 -0.28 ( U852) 48.00 2 US!* 5 4 -0.08 ( U2852) 67.50 2 US!* 5 5 -0.28 ( U848) 87.00 2 US!* 5 6 0.08 ( U2703) 111.50 2 US!* 5 7 -0.61 ( L/396) 126.50 2 USl* 6 I -0.41 ( U589) 8.50 2 US!* 6 2 0.05 ( U4054) 24.00 2 US!"' 6 3 -0.20 (L/1180) 48.00 2 US!* 6 4 -0.03 ( L/6564) 67.50 2 US I* 6 5 -!).20 (UII76) 87.00 2 US!* 6 6 0.05 (U4110) Ill .SO 2 USl* 6 7 -0.41 ( U585) 126.50 2 US!* 7 I -0.08 ( L/1337) 4.50 2 US!* 8 I -0.06 ) L/172~ ~ 4.50 2 USI* 9 I -0.03 L/3257 4.50 2 US!* Purlin Anchoraf'e Forces for Shane base Roof B, Panel Tvr e is PR. Pitch= 4.000:12 Bay Thickness Force(k) Ld Case # Purlins Length Simple? Diaphragm Allowable Deft Actual Defl Width I 0.065 -35.24 2 10 9.25 y 27.93 0.308 0.000 2 0.082 -76.20 2 10 20.00 N 27.93 0.667 o.ooo 3 0.082 -70.49 2 10 18.50 N 27.93 0.617 o.ooo 4 0.082 -76.20 2 10 20.00 N 27.93 0.667 o.ooo 5 0.065 -70.49 2 10 18.50 N 27.93 0.617 0.000 6 0.082 -76.20 2 10 20.00 N 27.93 0.667 0.000 7 0.082 -70.49 2 10 18.50 N 27.93 0.617 o.ooo 8 0.082 -76.20 2 10 20.00 N 27.93 0.667 o.ooo 9 0.065 -35.24 2 10 9.25 y 27.93 0.308 0.000 Fnn~Line Forcefk) Anch.Allow Reouired Clios Actual Clios Diaohra1m1 Allow Diaohra1m1 Shr Stress 1 0.08 0.00 0 0 0.134 0.000 0.000 2 0.87 0.00 0 0 0.134 0.000 0.000 3 1.40 0.00 0 0 0.134 0.000 0.000 4 1.40 0.00 0 0 0.134 0.000 0.000 5 1.74 0.00 0 0 0.134 0.000 0.000 6 1.74 0.00 0 0 0.134 0.000 0.000 7 1.40 0.00 0 0 0.134 0.000 o.ooo 8 1.40 0.00 0 0 0.134 0.000 o.ooo 9 0.87 0.00 0 0 0.134 0.000 0.000 10 . 0.08 0.00 0 0 0.134 0.000 0.000 File: 7079 Chevron RI_S1ress Check 10_2008 with 08_2008 Loading Version: ?.Ia 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Loads and City: Rifle County: Garfield State: Colorado 89AISC · 04AISI Building Code: 2003 International Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind Load Wind Speed: 90.00 mph Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: 1.023 Wind Enclosure: Enclosed Wind Importance Factor: 1.150 Topographic Factor: 1.0000 NOT Windbome Debris Region Base Elevation: 0/0/0 Primacy Zone Strip Width: 10/7/3 Parts I Portions Zone Strip Width: 5/3110 Basic Wind Pressure: 20.74 psf Deflection Conditions Built Up: Cold Form: Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf Snow Load Roof Snow Load: 75.00 psf Design Snow (Sloped): 75.00 psf Snow Exposure Category (Factor): 2 Partially Exposed ( 1.00) Snow Importance:· 1.100 Thermal Category (Factor): Heated (1.00) Ground I Roof Conversion: 0.70 %Snow Used in Seismic: 20.00 Seismic Snow'Load: 15.00 psf Unobstructed, Slippery Roof Frames are vertically supporting:Metal RoofPurlins and Panels Deflection Limit Ovenide V /240 Frames are laterally supporting:Underhung Crane Deflection Limit Override H/400 Purlins are supporting:Metal Roof Panels Deflection Limit OveJTicid V/240 Girts are supporting:Metal Wall Panels Deflection Limit Override W240 Crane Schedule Information 0 0 Live Load Country:· United States Rainfall: 4.00 inches per hour Live Load: 20.00 psf Not Reducible Seismic Load Mapped Spectral Response~ Ss:43.60 %g Mapped Spectral Response~ Sl :9.10 %g Seismic Hazard I Use Group: Group 2 Seismic Importance: 1.250 Seismic Performance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Bracing Seismic Period: 0.2691 Framing RMFactor: 3.0000 Bracing RMFactor: 3.0000 Soil Profile Type: Stiff soH (D, 4) Frame Redundancy Factor:l.OOOO Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W Name I Type Service Classification Method of Operation Capacity Bridge I Bridge Construction (Ton) Span 5tonUH Underhung Crane C (Moderate Service) Pendant Operated 5.00 421010 I Single Girder W II 4 a : Namel Name2 5 ton UH Type Wide Flange -Hot Rolled TYPe Rigid Suspension M jDesigned & .I. Provided NBVP Brackets Size WI6 Bracket Shape Start Start End End Aisle Start Frame Adjust. Frame Adjust. Elev. 3 Plate BuiltMup I 0/3/0 10 0/3/0 I 26/6/0 Size Rail Size 1 Vertical !Horizontal Ob/yd) JDeflection Deflection Vertical Lateral Impact(%)1Impact(% o I -10.00 20.00 Fr'Om From Left Right Edge Edge 51610 51610 Longitudinal Impact(%) IO.OO Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain all code and loading information for this specific building site. · File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy (2)FB (2)FB FB FB X ......... ,.. •• , .......... ,....,,.., ...................... ,,....., 1\"T" I'"'I">AO•r I 1'-1,-/,..\ A Dimension Key I 5'~6" BL to CL of Runway Beam 2 I 5/8" 3 4'~0" 4 3'~5 114" s 3'-3 3/4" 6 1'~3" 7 1'-9 13/16" 8 2@2'-47/16" 9 4 1/2" 10 40'¥10" Ridge Ht. Frame Clearances Horiz. Clearance between members I(CXOOO) and 6(C'XOOO): 45'~0 314" File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM 0 07-27053 Calculations Hazardous Materials Occupancy Ve1t. Cleararice at member I (CXOOO): 28'*3 1/4" Vert. Clearance at member 6(CXOOO): 28'-3 1/4" Finished Floor Elevation= 100'-0" (Unless Noted Otherwise) Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA 1-l(Left): 2'-5 3/4H Hori. Clearance at CRANE DATA 1-1 (Left): I '-8 l/2" V,ert. Clearance at CRANE DATA 1-l(Right): 2'-5 3/4" Horz.ClearanceatCRANEDATA !-\(Right): 1'-81/2" File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading 0 Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 85 of 175 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 86 of 175 Trib. Override Desi n Status 20/0/0 Stress Check Desi n Load Combinations-Framin No. Origin Factor Application Description I System 1.000 !.OD+ LOAD+ l.OCG+ !.OS D+AD+CG+S 2 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 US'* D+AD+CG+USI* 3 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 *US I D+AD+CG+'USI 4 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WI> D+AD+CG+Wl> 5 System 1.000 1.0 D+ 1.0 AD+ 1.0 CG + LO<Wl D+AD+CG+<Wl 6 System 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 W2> D+AD+CG+W2> 7 System 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 <W2 D+AD+CG+<W2 8 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 Wl> D+ AD+CG+S +WI> 9 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 <WI D+AD+CG+S+<Wl 10 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 W2> D+AD+CG+S+W2> II System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System 1.000 1.0 D + 1.0 AD+ l.OCG + 1.0 *Al> D+AD+CG+*AL> 13 System 1.000 1.0 D + 1.0 AD+ l.OCG + 1.0 AL*> D+AD+CG+AL*> 14 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <'AL D +AD+ CG+<*AL 15 System 1.000 1.0 D + 1.0 AD+ 1.0 CG+ l.O<AL* D + AD+ CG+<AL * 16 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WI> D+AD+CU+Wl> 17 System LOOO 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<WI 18 System LOOO 0.600 D + 0.600 AD+ 0.600 CU + 1.0 W2> D+AD+CU+W2> 19 System LOOO .600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System LOOO LO D +LOAD+ 1.0 CG +0.563 S +0.750 'Al> D+AD+CG+S+*AL> 21 System LOOO 1.0 D + 1.0 AD+ LO CG +0.563 S +0.750 AL'> D+AD+CG+S+AL*> 22 System LOOO l.O D+ 1.0 AD+ 1.0 CG +0.563 S +0.750_ <*AL D+AD+CG+S+<*AL 23 System LOOO LO D + LOAD+ LO CG + 0.563 S + 0.750 <AL• D+AD+CG+S+<AL* 24 System LOOO LO D+ LOAD+ LO CG +0.375 W!>+0.750 *Al> D+AD+CG+Wl>+*Ai> 25 System LOOO LO D+ LOAD+ I.OCG +0.375 WI>+0.7SOAL*> D+AD+CG+WI>+AL*> 26 Syste~ LOOO 1.0 D + 1.0 AD+ 1.0 CG +0.375 <Wl + 0.750 <*AL D+ AD+CG + <Wl+,<*AL 27 System 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 <W1 + 0.750 <AL* D+AD+CG +<Wl+<AL* 28 System LOOO LO D +LOAD+ 1.0 CG +0.375 W2> +0.750 *Al> D +AD+ CG +W2>+*Al> 29 System 1.000 LO D + 1.0 AD+ 1.0 CG+0.375 W2> +0.750 AL*> D +AD+ CG + W2>+AL *> 30 System 1.000 1.0 D+ LOAD+ 1.0 CG +0.375<W2 +0.750<*AL D+AD+CG+<W2+<*AL 31 System 1.000 l.O D+ LOAD+ 1.0 CG +0.375 <W2 +0.750<AL* D +AD+ CG + <W2+<AL"' 32 System 1.000 LO D+ 1.0 AD+ LOCG +0.150 S +0.750 E>+0.700 EG+ D+AD+CG+S+E>+EG+ 33 System 1.000 1.0 D+ 1.0 AD+ LOCG +0.150 S +0.750 <E+0.700 EG+ D+AD+<:G+S+<E+EG+ 34 System LOOO 0.600 D + 0.600 AD+ 0.600 CU + 0.700 E> + 0.700 EG-D+AD+CU+E>+EG~ 35 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 <E+ 0.700 EG-D+AD+CU+<E+EG~ 36 System Derived LOOO LO D + 1.0 AD+ 1.0 CG + 0.150 S + 0.750 EB>+ 0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System -Derived 1.000 .600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0.700 EG-D+AD+CU+EB>+EG~ 38 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.150 S + 0.750 <EB + 0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 <EB + 0.700 EG-D+AD+CU+<EB+EG~ 40 System Derived 1.000 l.OD+ LOAD+ l.OCG+ l.OWPAI D+AD+CG+WPAI 41 System Derived 1.000 LO D+ LOAD+ !.OCG +0.750 S +0.750 WPAI D+AD+CG+S+WPAl 42 System Derived 1.000 0.600 D.+ 0.600 AD+ 0.600CU + 1.0 WPAI D+AD+CU+WPAI 43 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPA1 +0.750 *AL + 0.750 ALB> D+AD+CG+WPA1+*AL+ALB> 44 System Derived 1.000 1.0 D + l.O AD+ 1.0 CO+ 0.375 WPAl +0.750 AL* + 0.750 ALB> D+AD+CG+WPAI+AL*+ALB> 45 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPDI D+AD+CG+WPDI 46 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.7508 + 0.750 WPD! D+AD+CG+S+WPDI 47 System Derived 1.000 0.600 D +0.600 AD +0.600 CU + 1.0 WPDI D+AD+CU+WPD1 48 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPD1 + 0.750 *AL+0.7SO <ALB D+AD+CG+WPDl+*AL+<ALB 49 System Derived 1.000 1.0 D+ 1'.0 AD+ 1.0 CG +0.375 WPDl + 0.750 AL* +0.750 <ALB D+AD+CG+WPD1+AL*+<ALB so System Derived LOOO 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA2 D+AD+CG+WPA2 51 System Derived 1.000 1.0 D + l.O AD+ !.0 CO+ 0.750 S + 0.750 WPA2 D+AD+CG+S+WPA2 52 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPA2 D+AD+CU+WPA2 53 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPA2 + 0.750 *AL + 0.750 ALB> D+AD+CG+WPA2+*AL+ALB> 54 System Derived 1.000 l.O D + 1.0 AD+ l.O CG +0.375 WPA2 + 0.750 AL* + 0.750 ALB> D+AD+CG+WPA2+AL*+ALB> 55 System Derived 1.000 1.0 0 + 1.0 AD+ 1.0 CG + 1.0 WPD2 D+AD+CG+WPD2 56 System Derived 1.000 1.0 D+ 1.0 AD+ \.0 CG +0.750 S +0.750 WPD2 D+AD+ CG +S + WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived 1.000 1.0 D + ·1.0 AD+ 1.0 CG +0.375 WPD2 + 0.750 *AL + 0.750 <:ALB D+AD+C'G+WPD2+* AL +<ALB File: 7079 Chevron R !_Stress Check !0_2008 with 08_2008 Loading Version: 7.1a 07-2 7053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 87 of 175 59 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPD2 + 0.750 AL * + 0.750 <ALB 60 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 WPB1 61 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPB1 62 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPB1 63 System Derived !.000 l.O D + l.O AD+ 1.0 CG +0.375 WPBI + 0.750 *AL +0.750 ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPBI +0.750 AL* +0.750 ALB> 65 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + l.OWPC1 66 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC1 67 SYstem Derived 1.000 0.600 D +0.600 AD +0.600 CU + 1.0 WPC1 68 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPC1 + 0.750 'AL +0.750 <ALB 69 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG + 0.375 WPCI + 0.750 AL* +0.750 <ALB 70 System Derived 1.000 1.0 D + !.0 AD + 1.0 CG + 1.0 WPB2 71 System Derived 1.000 1.0 D + J.O AD+ l.O CG +0.750 S +0.750 WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 73 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 + 0.750 *AL +0:750 ALB> 74 System Derived 1.000 l.O D + J.O AD+ 1.0 CG + 0.375 WPB2+ 0.750 AL' +0.750 ALB> 75 System Derived 1.000 1.0 D + l.O AD + l.O CG + l.O WPC2 76 System Derived 1.000 J.O D + 1.0 AD+ l.O CG + 0.750 S + 0.750 WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 78 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPC2 +0.750 'AL + 0.750 <ALB 79 System Derived 1.000 1.0 D + 1.0 AD+ LO CG + 0.375 WPC2 +0.750 AL' +0.750 <ALB 80 System Derived 1.000 J.O D + 1.0 AD+ LOCO+ 1.0 S + 1.0 ALB> 81 System Derived 1.000 J.O D + 1.0 AD+ LO CG + 1.0 'AL+ 1.0 ALB> 82 System Derived 1.000 1.0 D + 1.0 AD.+ I~ CG + 1.0 AL* + 1.0 ALB> 83 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 'AL + 0.750 ALB> 84 System Derived 1.000 l.O D + l.O AD+ 1.0 CG +0.563 S +0.750 AL* + 0.750 ALB> 85 System-Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 S + 1.0 <ALB 86 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG + l.O *AL + 1.0 <ALB 87 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 AL* + 1.0 <ALB 88 System Derived 1.000 l.OD + 1.0 AD+ 1.0 CG+0.563 S +0.750 'AL+0.750 <ALB 89 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG+0.563 S +0.750AL' +0.750 <ALB F M b S1 rame em er zes Mem. Fig Width F1gThk WebThk Depthl Depth2 Length Weight F1gFy No. -(in.) (in.) (in.) (in.) (in.) (ftl (pj <ksii 1 6.00 0.5000 0.2500 12.00 46.00 31.03 1314.3 55.00 2 6.00 0.6250 0.2500 46.00 23.00 18.62 1078.2 55.00 3 6.00 0.6250 0.1644 23.00 28.60 9.17 371.2 55.00 4 6.00 0.6250 0.1644 28.60 23.00 9.17 371.2 55.00 5 6.00 0.6250 0.2500 23.00 46.00 18.62 1078.2 55.00 6 6.00 0.6250 0.2500 12.00 46.00 31.03 1452.4 55.00 7 7.00 0.2500 0.1875 15.00 15.00 37.00 717.5 55.00 8 7.00 0.2500 0.1875 15.00 15.00 37.00 717.5 55.00 Tota!FrameWe1ght 7100.5 (p) Frame Pricing Weight= 7713.2 (p) Joint 1 Joint 2 No Yes No Yes Boundary Condition Summary Member X~Loc Y~Loc Suoo. X Suoo.Y Moment Disolacement X(in.) 1 0/0/0 0/0/0 Yes Yes No 0/0/0 6 53/0/0 0/0/0 Yes Yes No 0/0/0 7 15/0/0 0/0/0 Yes Yes No 0/0/0 0 15/0/0 371010 Yes No No 0/0/0 8 38/0/0 0/0/0 Yes Yes No 0/0/0 0 38/0/0 37/0/0 Yes No No 0/0/0 2 51610 33/J0/0 Yes Yes Yes 01010 5 47/6/0 33/J0/0 Yes Yes Yes 0/0/0 Values shown are resisting forces of the foundation. Reactions-Unfactored Load T eat Frame Cross Section: 1 Type Exterior Column X~Loc 0/0/0 Grid I Grid2 l ~D Interior Column 15/0/0 J.c File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Interior Column 38/0/0 I·B D+AD+CG+WPD2+AL *+<ALB D+AD+CG+WPBl D+ AD+CG +S+WPBI D+AD+CU+WPBI D+AD+CG+WPBI+*AL+ALB> D+AD+CG+WPB l+AL *+ALB> D +AD+ CG + WPCl D+ AD+CG +S+WPC! D +AD+ CU ~ WPCI D+AD+CG+WPCJ+*AL+<ALB D+AD+CG+WPCl+AL *+<ALB D+AD+.CG+WPB2 D+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+AL *+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2. D+AD+CU+WPC2 O+AD+CG+WPC2+* AL +<ALB D+AD+CG+WPC2+AL *+<ALB D +AD+ CG + S+ALB> D+AD+CG+*AL+ALB> D+AD+CG+AL*+ALB> D+AD+CG+S+* AL +ALB> D+AD+CG+S+AL *+ALB> D+AD+CG+S+<ALB D +AD+ CG+*AL+<ALB D +AD+ CG+AL '+<ALB O+AD+CG+S+*AL+<ALB D+AD+CG+S+AL*+<ALB WebFy Splice (ksi). Jt.1 55.00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP 55.00 BP 55.00 BP (Includes all plates) (Includes all pieces) Codes Jt.2 ,.., KN ss SP ss KN KN ss ss Shape 3P 3P· 3P 3P 3P 3P 3P 3P Disolacement Y(in.)_ Displacement ZZ{rad.) 0/0/0 0/0/0 0/0/0 0/0/0 0/0/0 0/0/0 0/0/0 0/0/0 Exterior Column 53/0/0 I·A Version: 7.1a 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 . 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 88 of 175 Base Plate W x L (in.) 9 X \3 8 X J6 8 X 16 9 X 13 Base Plate Thickness (in.) 0.500 0.375 0.375 0.500 Anchor Rod Qty/Diam. (in.) 4" 1.000 4 "0.750 4" 0.750 4 " 1.000 Column Base Elev. 100'-0" . 100'·0" 100'·0" 100'-0" Load Tvoe Desc. Hx Hz v¥ Hx Hz Vv Hx Hz Vy Hx Hz Yv D Fnn 0.9 4.6 0.8 " 0.8 -0.9 4.7 AD Frm 0.1 1.2 " " " " -0.1 1.2 " CG Frm 2.7 " 10.6 " -0.0 0.3 " -0.0 0.3 -2.7 " 10.6 s Fnn 10.2 " 39.7 " " -10.2 39.8 " USl* Frm 9.1 " 23.6 " " " " -9.1 " 48.0 " *USl Frm 9.1 " 48.0 " " " " " -9.1 -23.6 - WI> Frm -7.2 --12.4 7.1 --7.1 -4.8 --4.4 - <WI Fnn 4.7 --4.4 -6.4 --6.4 -7.3 --12.4 - W2> Fnn -8.6 -8.4 ------3.4 --0.5 - <W2 Frm 3.3 --0.5 " ----8.7 " -8.4 - *AL> Frm -0.0 7.7 ------1.4 -3.6 - AL*> Frm -0.0 2.1 ----1.4 -9.3 - <*AL Frm 1.4 9.3 ----0.0 -2.1 - <AL* Fnn 1.4 -3.6 -" ----0.0 -7.7 - cu Fnn 1.4 -5.3 -------1.4 -5.3 - E> Frm -3.9 --5.4 -0.1 --0.1 . -4.0 -5.4 - EG+ Fnn 0.4 -1.4 --0.0 . -0.0 -0.4 . 1.4 . <E Frm 3.9 . 5.4 . -0.1 . . -0.1 -4.0 . ·5.4 - EG-Fnn -0.4 --1.4 . -0.0 . --0.0 0.4 -·1.4 . EB> Brc ---. . . -. . -. . <EB Brc . 0.0 . -" . -. -" 0.0 -- WPAI Brc 1.9 . -9.6 -. . . . . -1.9 . -9.6 - *AL Frm 0.7 . 8.5 " " . -. . -0.7 . 2.9 - ALB> Brc . " ---. . . " . --. AL* Fnn 0.7 -2.9 . . -. ---0.7 " 8.5 - WPDI Brc 2.5 --7.3 . -. -. . -2.5 -·7.3 - <ALB Brc -. . . -. . . . . --- WPA2 ' Brc 0.4 " -5.6 . . . ----0.4 -·5.6 - WPD2 Brc 1.0 --3.3 . . . . ---1.0 -,3.3 . WPBI Brc 1.9 . -9.6 . •) . . . -. -1.9 . ·9.6 . 0 WPCI Brc 2.5 . -7.3 -. . . . . -2.5 . -7.3 . WPB2 Brc 0.4 . -5.6 -. . . . . -0.4 . ·5.6 . WPC2 Brc 1.0 --3.3 . . . . -. -1.0 . ·3.3 . Maximum Combined Reactions Summarv with Factored Loads-Framin~ X-Loc Grid Hrz left Load Hrz Right Load Hrzln Load HrzOut Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-~~) Case ~~) Case (-~~) Case (~~ Case (-Yy) Case (~~) Case (-Mzz) Case (Mzz) Case {ki (in-k) (in-k) 0/0/0 1-D 7.2 18 14.9 9 . . 0.0 38 5.8 16 64.4 3 -. . . 15/0/0 1-C . . . 6.4 5 7.1 16 . . 1.1 32 . -. . 15/0/0 37/0/0 . -. . 6.1 17 6.8 4 0.8 I . -. . . . 38/0/0 1-B . . . . . 6.4 5 7.1 16 . . 1.1 32 . . . . 38/0/0 37/0/0 . -. 6.1 17 6.8 4 0.8 I . . . -. . 53/0/0 1-A 15.0 8 7.3 19 . 0.0 38 5.7 17 64.5 2 -. -. Sum of Forces with React1ons Check-Framinv . Horizontal Vertical Load Type L~~d Re~~~ion ~~d Reaction lk (k\ D 0.0 0.0 10.9 9.3 AD 0.0 0.0 2.5 2.4 CG 0.0 0.0 21.7 21.7 s 0.0 0.0 79.5 79.5 US!* 0.0 0.0 71.5 71.5 *US! 0.0 0.0 71.5 71.5 WI> 12.0 12.0 16.8 16.8 <WI 12.0 12.0 16.8 16.8 W2> 12.0 12.0 8.9 8.9 <W2 12.0 12.0 8.9 8.9 *AL> 1.5 1.5 12.0 11.4 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.Ja Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: 1:57:43 PM Page: 89 of 175 AL*> 1.5 1.5 12.0 11.4 <*AL 1.5 1.5 12.0 11.4 <AL* 1.5 1.5 12.0 11.4 cu 0.0 0.0 10.6 10.6 E> 7.9 8.0 0.0 0.0 EG+ 0.0 0.0 2.8 2.8 <E 7.9 8.0 0.0 0.0 EG-0.0 0.0 2.8 2.8 EB> 0.0 0.0 0.0 0.0 <EB 0.0 0.0 0.0 0.0 WPAI 0.0 0.0 19.1 19.2 'AL 0.0 0.0 12.0 11.4 ALB> 0.0 0.0 0.0 0.0 AL' 0.0 0.0 12.0 11.4 WPDI 0.0 0.0 14.5 14.5 <ALB 0.0 0.0 0.0 0.0 WPA2 0.0 0.0 11.2 11.2 WPD2 0.0 0.0 6.6 6.6 WPBI 0.0 0.0 19.1 19.2 WPCI 0.0 0.0 14.5 14.5 WPB2 0.0 0.0 11.2 11.2 WPC2 0.0 0.0 6.6 6.6 B PI teS ase a ummarv X~LoC Grid Mem. Thickness Width Length Num.Of BoltDilim. Type Welds to Welds to No. (in.) (in.) (in~) Bolts (in.) Flane:e Web 01010 1-D I 0.500 9 13 4 LOOO A36 OS-0.1875 OS-0.1875 15/0/0 1-C 7 0.375 8 16 4 0.750 A36 OS-0.1875 OS-0.1875 38/0/0 1-B 8 0.375 8 16 4 0.750 A36 OS-0.1875 OS-0.1875 53/0/0 1-A 6 0.500 9 13 4 1.000 A36 OS-0.1875 OS-0.1875 w s f! eb ti ener Summar Mem. Stiff. Desc. ~~;· Web Depth hit alh a Thick. Width Side .) Welding N'J. No. fin.) . (in.) (in.) (in.) Description 2 I S9 4.02 43.176 172.71 NIA NIA 0.5000 2.500 Both W-OS-0.1875 2 2 Sl 13.02 29.981 119.92 3.00 89.65 0.1875 2.000 Both Std 5 I 89 14.60 43.176 172.71 NIA NIA 0.6250 2.500 Both W-OS-0.1875 5 2 Sl 13.13 41.012 164:05 3.00 122.35 0.1875 2.000 Both F-QS-0.1875,W-OS-D.I875 Brackets Part Summary Mem. Loc. Total Length Bracket Cut Bracket Fig Width FlgTbk WebThk Hole Pitch Stiffener or Plate Pa1t No. (ft) (in.) (in.) Depth (in.) (in.) (in.) (in.) (in.) 2 3.98 15.125 4.750 10.000 6.000 0.2500 0.2500 3.500 UP070411000 WUI5141234 5 14.64 15.125 4.750 10.000 6.000 0.2500 0.2500 3.500 UP070411 000 WUI5141234 Brackets Desi2n Summ~_ry __ (verticalllve load Is with the lmuact factor Mem. Loc. Vert. Live Vert. Dead Lateral Longitudinal CL Distto Member Member WebTbk Fig Tbk Fig Width No. (ft) Load (k) Load(k) lmoact (k) Impact (k:) Flan"" lin.) Deothl lin.) Deoth2 lin. lin.) lin.) -lin.) 2 3.98 10.61 !.27 0.73 1.47 13.318 42.208 39.669 0.2500 0.6250 6.0000 5 14.64 10.61 1.27 0.73 1.47 13.318 40.919 40.958 0.2500 0.6250 6.0000 Bolted End-Plate Moment Connections (AISC DG-16)-Fv =55 ksi End-Plate Dimensions Bolt Outside Flange Inside Flange Mem. Jt. Type Thick. Width Length Diam. Spec/Joint Gages In/Out Configuration Pitches J st/2nd Configuration Pitches 1st/2nd No. No. (in.) (in.) (in~.) (in.) · (in.) ID Desc. in. ID Desc. in.) I 2 KN(Top) 0.625 6.00 47.00 0.750 A325XIST 3.50 12 Flush 2.00 II Flush 2.00 2 I KN(Top) 0.625 6.00 47.00 0.750 A325XIST 3.50 12 Flush 2.00 11 Flush 2.00 3 2 SP 0.500 6.00 33.49 0.750 A325XIST 3.00 II Flush 0.00 31 Extended 3.75 4 I SP 0.500 6.00 33.49 0.750 A325XIST 3.00 II Flush 0.00 31 Extended 3.75 5 2 KN(Top) 0.625 6.00 47.00 0.750 A325XIST 3.50 12 Flush 2.00 11 Flush 2.00 6 2 KNiTo~l 0.625 6.00 47.00 0.750 A325XIST 3.50 12 Flush 2.00 II Flush 2.00 Reauired Strength -Out Available Strength-Out Reauired Strength-In Available Strenoth-In Memj_ Jt L~ I Axial Shear Moment Design Shear Moment l.d Axial Shear Moment Design I Shear Moment No. No. Cs (k) (k) (in-k) Proc. (k) (in-k) Cs (k) (k) (in-k) Proc. (k) (in-k) I I 2 2 I -40.5 10.9 3694.4 Thin plate 159.0 2879.8 16 5.8 1.3 I 147.1 Thick plate 1 106.0 1729.6 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 90 of i 75 2 I 2 -40.5 10.9 3694.4 Thin plate IS9.0 2879.8 16 S.8 1.3 1147.1 Thick plate 106.0 !729.6 3 2 16 4.9 1.8 13.0 Thin plate 106.0 894.3 I -13.S 3.3 1790.3 Thin plate IS9.0 182S.S 4 I 16 4.9 1.8 13.0 Thin plate . 106.0 894.3 I -U.S 3.3 1790.3 Thin plate IS9.0 182S.5 s 2 3 -40.7 10.9 3696.6 Thin plate IS9.0 2907.1 17 S.8 1.4 1179.0 Thick plate 106.0 1727.1 6 2 3 -40.7 10.9 3696.6 Thin plate IS9.0 2907.1 17 S.8 1.4 1179.0 Thick plate 106.0 1727.1 Flange Brace Summary Member From Member Joint 1 From Side Point l Part Design Note I 12/S/4 12/S/4 SFB2114 I 22/S/4 22/S/4 SFB4044 I 27/S/4 27/S/4 FBSOSO 2 S/3/8 22/9113 FBS080 2 14/3/8 1319113 FB4024 2 17/3/8 10/9/13 FB3030 3 7/8/0 1/9/13 FB4014 4 116/0 ' 1/9/13 FB4014 s 1/4/0 10/9/13 FB3030 s 4/4/0 13/9113 FB4024 s 13/4/0 22/9/13 FBS080 6 17/S/4 17/5/4 FB4000 6 27/S/4 27/S/4 FBSOSO 7 7/S/4 71514 FB2044 7 17/5/4 17/5/4 (2)FB2044 7 2S/S/4 2S/S/4 (2)FB2044 8 7/S/4 7/S/4 FB2044 8 17/S/4 17/S/4 (2)FB2044 8 2S/5/4 25/S/4 (2lFB2044 Top of Post s ummary X~Loc Grid Top Conn. Condition FlgMn Rb Allow Comp FB Force FB Angle Miri FB/SFB Purlin Bolt Shear FB/WSF Reaction Force Moment Shear R1 R2 Purlin Bearing Bearing 1S/0/0 1-C 6.80 S.94 Stub-1 186.79 5.94 -11.77 S.84 . . . - - 38/0/0 1-B 6.77 5.91 Stub~ l 186.Ql 5.91 . 11.72 S.SI . . -. - 0 Frame Design Member Summary~ Controlling Load Case and Maximum Combined Stresses per Member (Locations are from Joint 1) Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear Mom~x Mom~y Axial Shear Bnd-X Bnd·Y ·-· Stress /Force ·--Sum% % No. ft in. Case k k in·k in~k ksi ksi ksi ksi Axial Shear Bnd-X Bnd~Y Bnd+Ax Shear 1 22.47 38.98 1 -56.8 -11.1 -2988.9 0.0 3.66 1.17 18.29 0.00 21.97 3.60 25.76 41.2S 0.84 0.32 2 17.23 23.00 3 -16.3 5.9 2034.5 o.o L2f 1.09 20.29 0.00 29.47 10.99 33.00 41.25 0.65 0.10 3 1.67 24.11 3 -14.4 3.1 2139.0 0.0 1.28 0.83 23.12 0.00 29.86 4.30 32.89 41.2S 0.74 0.19 4 7.10 24.11 2 -14.4 -3.1 2145.7 0.0 1.28 0.83 23.19 0.00 29.86 4.30 32.89 41.25 0.74 0.19 5 0.00 23.00 2 -16.3 -S. 2041.4 0.0 L26 LOS 20.36 0.00 29.47 10.99 33.00 41.25 0.65 0.10 6 17.46 32.97 1 ·56.9 11.1 -2321.3 0.0 3.69 1.40 15.50 0.00 24.70 5.H 18.16 41.25 0.97 0.27 7 17.44 15:00 4 .0.8 -0. -790.5 0.0 0.13 0.1 26.26 0.00 18.5S 13.90 28.37 28.37 0.93 0.01 8 17.44 15.00 4 -0.8 -0.4 -789.9 0.0 0.13 0.1 26.24 0.00 18.SS 13.90 28.37 28.37 0.93 O.Ql Mem. Loc. Depth Area Rx Ry L< Ly-1 Ly-2 Klx Kly1 Kly2 S< Lb1 Rt·l Lb2 Rt·2 Qs Qa Cb1 Cb2 No. ft in. in.2 in. in. in. in. in. IRx /Ry /Ry in.3 in. in. in. in. 1 22.47 38.98 15.50 14.73 1.08 339.6 60.1 60.1 34.6 55.7 5S.7 163.41 120.2 1.45 60.1 1.43 1.00 0.84 1.26 L09 2 17.23 23.00 12.94 9.44 1.32 295.91 36.0 0.0 31.3 27.3 0.0 100.29 36.0 1.61 0.0 0.00 1.00 1.00 LOS 0.00 3 1.67 24.11 11.26 10.32 1.41 29S.91 36.0 36.0 28.7 25.5 25.5 92.52 36.0 1.6f 36.0 1.66 1.00 1.00 LOS 1.01 4 7.10 24.11 11.26 10.32 1.41 295.91 36.0 36.0 28.7 2S.S 2S.S 92.S2 36.0 1.66 36.0 1.66 1.00 1.00 1.01 !.OS s 0.00 23.00 12.9 9.44 1.32 295.91 36.0 0.0 31.3 27.3 0.0 100.29 36.0 1.61 0.0 0.00 1.00 1.00 1.05 0.00 6 17.46 32.97 IS.43 13.0S 1.21 339.6 60.1 60.1 39.1 49.7 49.7 149.80 209.5 1.64 120.2 1.57 1.00 0.92 1.7S 1.2 7 17.44 IS.OO 6.22 6.19 1.52 444.00 120.0 96.0 71.8 79.1 63.3 30.10 120.0 1.87 96.0 1.86 0.86 1.00 1.00 1.00 8 17.44 15.00 6.22 6.19 1.52 444.00 120.0 96.0 71.8 79.1 63.3 30.10 120.0 1.87 96.0 1.86 0.86 LOO 1.00 1.00 File: 7079 Chevron R 1_ Stress Check I 0 _2008 with 08 _ 2008 Loading Version: 7.Ja 07-27053 Calculations Hazardous Materials Occupancy User Defined Frame Point Loads for Cross Section· 1 Side Units Type Description Magi Locl Offset HorV Supp. 2000 k CG S-43 Pipe Loads ·0.25 15/6/0 -1/9/0 Horiz. N 2001 k CG PS-43 Pipe Loads ·0.25 15/6/0 -1/9/ Horiz. N y 1fi'.il" Deflection Load Combinations~ Framin No. Ori2in FaCtor DefH DefY Aoolication 1 System 1.000 0 240 1.0 s s 2 System 1.000 0 240 l.OUSl' USl' 3 System 1.000 0 240 1.0 *US! •ust 4 System 1.000 0 240 0.700Wl> WI> ) 5 System 1.000 0 2400 0.700<Wl WI 6 System 1.000 0 240 &iOOW2> W2> 7 System 1.000 0 240 ·.700<W2 W2 8 System Derived 1.000 0 240 p.700 WPAI WPAI 9 System Derived 1.000 0 240 0.700WPDI WPDI 10 System Derived 1.000 0 240 0.700 WPA2 WPA2 11 System Derived 1.000 0 240 0.700WPD2 WPD2 I2 System Derived 1.000 0 240 0.700 WPBI WPBI I3 System Derived 1.000 0 240 0.700WPCI WPC1 I4 System Derived 1.000 0 240 0.700 WPB2 WPB2 I5 System Derived 1.000 0 240 0.700 WPC2 WPC2 I6 System 1.000 400 0 .700WI> WI> I7 System 1.000 400 0 0.700<WI f<wi 18 System 1.000 400 0 .700 W2> ~:z I9 System 1.000 400 0 0.700<W2 20 System Derived 1.000 400 0 0.700WPA1 !WPA1 21 System Derived 1.000 400 0 0.700WPD1 WPDI 22 System Derived 1.000 400 0 0.700WPA2 WPA2 23 System Derived 1.000 400 0 0.700 WPD2 WPD2 24 System Derived 1.000 400 0 0.700 WPBI WPB1 25 System Derived 1.000 400 0 .700 WPCl WPCl 26 System Derived I · 1.000 400 0 0.700 WPB2 WPB2 27 System Derived 1.000 400 0 0.700WPC2 WPC2 28 System 1.000 100 0 0.600 E> + 0.700 EG· E>+EG- 29 System 1.000 100 0 .600 <E + 0.700 EG· E+EG· 30 System Derived 1.000 100 0 .600 EB> ~B> 31 System Derived 1.000 IOO 0 0.600 <EB fEB 32 System 1.000 400 0 l.O<AL* <AL* 33 ~ystem 1.000 400 0 1.0 *AL> 'AL> File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 91 of\75 Dir. Coef Loc. DOWN 1.000 OF DOWN 1.000 OF Description ; . Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Frame Cross Section: 2 ) (2)Faf::::f-l_ _____ ~------------------~rt==1<2)Fa Dimension Key I 5'-6" BL to CL of Runway Beam 2 I 5/8" 3 4'·0" 4 3'-5 1/4" 5 2@5'-0" 6 2@2'-6" 7 3'·3 3/4" 8 1'-3" 9 1'·9 13/16" 10 2@ 2'-4 7116" II 4 1/2" 12 40'-!0" Ridge Ht. 0 0 0 X FRAME CROSS SECTION AT FRAME LINE(S) 2 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Frame Clearances Horiz. Clearance between members l(CXOOO) and 6(CXOOO): 44'-10 3/4" Vert. Clearance at member I (CXOOO): 28'~3 5/8" Vert. Clearance at member 6(CXOOO): 28'~3 5/8" Finished Floor Elevation= 100'-0" (Unless Noted Otherwise) '1> Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA l·l(Left): 2'-5 5/8" Horz. Clearance at CRANE DATA 1-l(Left): 1'-7 5/8" Vert. Clearance at CRANE DATA 1-l(Right): 2'-5 5/8" Horz. Clearance 3.tCRANE DATA 1-l(Right): 1'-7 5/8" File: 7079 Chevron R !_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM 93 of 175 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 94 of 175 Descri tion An le Grou Trib. Override Desi n Status Stress Check Ri id Frame 90.0000 Desil:!n Load Combinations-Framin No. Origin Factor AvPlication Descriotion I System 1.000 1.0 D+ LOAD+ l.OCG+ !.OS D+AD+CG+S 2 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 US I' D+AD+CG+USI* 3 System 1.000 1.0 D+ 1.0 AD+ 1.0 CG+ 1.0 *US! D+AD+CG+*USI 4 System 1.000 1.0 o·+ 1.0 AD+ 1.0 CG + 1.0 WI> D+AD+CG+Wl> 5 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <WI D+AD+CG+<Wl 6 System 1.000 LOD+ LOAD+ l.OCG+ l.OW2> D+AD+CG+W2> 7 System 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 <W2 D+AD+CG+<W2 8 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 WI> D+AD+CG+S+Wl> 9 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 <WI D+AD+CG+S+<Wl 10 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 W2> D+AD+CG+S+W2> II " System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 *AI> D+AD+CG+*Al> 13 System 1.000 J.OD+ t.OAD+ l.OCG+ l.OAL*> D +AD+ CG+AL*> . 14 System 1.000 1.0 D + 1.0 AD+ 1.0 CO+ l.O<*AL D+AD+CG+<*AL IS System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <AL* D +AD+ CG-t<AL * 16 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WI> D+AD+CU+Wl> 17 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<Wl 18 System !.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 W2> D+AD+CU+W2> 19 System !.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 l.O D+ 1.0 AD+ 1.0 CG+0.563 S +0.750 *AL> D+AD+CG+S+*Al.> 21 System 1.000 1.0 D + 1.0 AD+ l.OCG +0.563 S +0.750 AL*> D+AD+CG+S+AL*> 22 System 1.000 !.0 D + !.0 AD+ 1.0 CG +0.563 S +0.750 <*AL D+AD+CG+S+<*AL 23 System !.000 1.0 D + 1.0 AD+ !.0 CG + 0.563 S + 0.750 <AL' !o + AD+CG + S+<AL* 24 System 1.000 1.0 D+ 1.0 AD+ !.0 CG +0.375 Wl>+0.750 *AL> jo +AD+ CG + Wl>+*Al> 25 System 1.000 !.0 D+ !.0 AD+ l.OCG +0.375 W1>+0.750 AL*> [D+AD+CG+WI>+AL*> 26 System !.000 1.0 D + t.OAD + 1.0 CG +0.375 <Wl +0.750<*AL !o+AD+CG+<Wl+<*AL 27 System !.000 1.0 D+ 1.0 AD+ !.0 CG +0.375 <WI +0.750 <AL' !o+AD+CG+<Wl+<AL* 28 System !.000 !.0 D+ 1.0 AD+ 1.0 CG + 0.375 W2>+0.750 *AL> ID +AD+ CG + W2>+* AI> 29 System !.000 !.0 D + 1.0 AD+ !.OCG +0.375 W2>+0.750 AL*> lo +AD+ CG + W2>+AL *> 30 System 1.000 1.0 D +LOAD+ 1.0 CG +0.375 <W2+0.750<*AL lo + AD+ CG + <W2+<* AL 31 System !.000 1.0 D+ !.0 AD+ !.0 CG +0.375 <W2+0.750 <AL* P +AD+ CG +<W2+<AL* 32 System 1.000 !.0 D+ 1.0 AD+ 1.0 CG +0.150 S+0.750 E>+0.700 EG+ P+AD+CG+S+E>+EG+ 33 System 1.000 l.O D + !.0 AD+ !.OCG+O.ISO S +0.750 <E+0.700 EG+ P+AD+CG+S+<E+EG+ 34 System !.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 E> + 0.700 EG-D+AD+CU+E>+EG· 35 System !.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-D+AD+CU+<E+EG~ 36 System Derived !.000 !.0 D+ !.0 AD+ 1.0 CG +0.150 S +0.750 EB> +0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 Q.600 D+0.600 AD+ 0.600 CU +0.700 EB> +0.700 EG-io+AD+CU+EB>+EG· 38 System Derived 1.000 1.0 D+ 1.0 AD+ !.0 CG +0.!50 S+0.750<EB +0.700 EG+ P+AD+CG+S+<EB+EG+ 39 System Derived 1.000 Q.600 D+0.600 AD +0.600CU +0.700<EB +0.700 EG-jo +AD+ CU + <EB + EG· 40 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + !.0 WPAI D+AD+CG+WPAl 41 System Derived 1.000 1.0 D + !.0 AD+ !.0 CG +0.750 S +0.750 WPAI b+AD+CG+S+WPAI 42 System Derived !.000 0.600 D+ 0.600 AD +0.600 CU + 1.0 WPAI D+AD+CU+WPAl 43 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CO+ 0.375 WPAl +0.750 *AL +0.750 ALB> D+AD+CG+WPAl+*AL+ALB> 44 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPA.I +0.750 AL* +0.750 ALB> ;l)+AD+CG+WP A 1 +AL *+ALB> 45 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPDI D+AD+CG+WPDI 46 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPD! D+AD+CG+S+WPD! 47 System Derived 1.000 0.600 D +0.600 AD +0.600CU + 1.0 WPDI D+AD+CU+WPDl 48 System Derived 1.000 !.0 D + !.0 AD+ 1.0 CG + 0.375 WPDI +0.750 'AL +0.750 <ALB D+AD+CG+WPD!+*AL+<ALB 49 System Derived 1.000 l.O D + 1.0 AD+ 1.0 CO +0.375 WPDt +0.750 AL * + 0.750 <ALB D+AD+CG+WPD I +AL *+<ALB 50 System Derived 1.000 LOD+ LOAD+ l.OCG+ I.OWPA2 D+AD+CG+WPA2 51 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPA2 D+AD+CG+S+WPA2 52 System Derived 1.000 Q.600 D + 0.600 AD+ 0.600 CU + !.0 WPA2 D+AD+CU+WPA2 53 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPA2 +0.750 *AL + 0.750 ALB> D+AD+CO+WPAZ+*AL+ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO + 0.375 WPA2 + 0.750 AL"' + 0.750 ALB> D+AD+CG+WPAZ+AL*+ALB> 55 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CO+ 1.0 WPD2 D +AD+ CO+ WPD2 56 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPD2 D+AD+CG+S+WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ o.600 ClJ + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPD2 + 0.750 *AL + 0.750 <ALB D+AD+CG+WPDZ+*AL-I<ALB 59 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPD2 + 0.750 AL * + 0.750 <ALB D+AD+CG+WPDZ+A L *+<ALB File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: ?.Ia 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20(2008 Time: I :57:43 PM 95 of 175 60 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPB I 0+ AD +CG + WPBJ 61 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPB1 D+AD+CG+S+WPBI 62 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPB1 D+AD+CU+WPBI 63 System Derived 1.000 1.0 D + 1.0 AD+ LOCO+ 0375 WPBI + 0.750 *AL + 0.750 ALB> /o+AD+CG+WPB I+* AL+ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0375 WPBI + 0.750 AL* + 0.750 ALB> D+AD+CG+WPB I +AL *+ALB> 65 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPC1 D+AD+CG+WPCI 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPC1 D+AD+CG+S+WPC! 67 System Derived 1.000 0.600 D +0.600 AD +0.600 CU + 1.0 WPC1 /o +AD+ CU + WPCJ 68 System Derived 1.000 l.OD+ LOAD+ I.OCG+0.375WPCI +0.750*AL+0.750<ALB D+AD+CG+WPC I+* AL +<ALB 69 System Derived . 1.000 1:0 D + 1.0 AD+ 1.0 CG +0.375 WPCI + 0.750 AL* + 0.750 <ALB D+AD+CG+WPCJ+AL *~<ALB 70 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPB2 D+AD+CG+WPB2 71 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPB2 /D+AD+CG+S+WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 D+AD+CU+WPB2 73 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0375 WPB2 +0.750 *AL + 0.750 ALB> ID+AD+CG+WPBZ+*AL+ALB> 74 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPB2 + 0.750 AL* + 0.750 ALB> D+AD+CG+WPB2+AL *+ALB> 75 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPC2 /o+AD +CG+WPC2 76 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC2 D+AD+CG+S+WPC2 77 System Derived 1.000 0.600 D + o.600 AD+ 0.600 CU + 1.0 WPC2 D+AD+CU+WPC2 78 System Derived 1.000 l.O D+ 1.0 AD+ l.O CG +0.375 WPC2 + 0.750 *AL +0.750<ALB D+AD+CG+WPC2+* AL +<ALB 79 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPC2 + 0.750 AL' +0.750 <ALB D+AD+CG+WPC2+AL '+<ALB 80 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 S + 1.0 ALB> D +AD+ CG + S+ALB> 81 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 'AL + 1.0 ALB> lo +AD + CG+* AL+ALB> 82 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 AL' + 1.0 ALB> jo+AD+CG+AL*+ALB> 83 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.563 S +0.750 'AL+0.750 ALB> D+AD+CG+S+*AL+ALB> 84 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.563 S +0.750 AL"' +0.750 ALB> D+AD+CG+S+AL*+ALB> 85 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 S + 1.0 <ALB to + AD + CG + s+<ALB 86 System Derived 1.000 1.0 D + l.OAD + 1.0 CG + 1.0 *AL + l.O<ALB D +AD+ CG+"'AL+<ALB 87 System Derived 1.000 l.O D + 1.0 AD+ 1.0 CG + 1.0 AL"' + l.O <ALB D+AD+CG+AL*+<ALB 88 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 'AL+0.750<ALB ID+AD+CG+S+"'AL+<ALB 89 Svstem Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.563 S +0.750 AL' +0.750<ALB iD+AD+CG+S+AL'+<ALB B c d s oundary_' on ition ummar Member X-Loc Y~Loc Supp. X Supp. Y Moment DiSPTacement XlinS Di$Pl"acement Yt1fl5 Disolacement ZZ(rad. 1 0/0/0 01010 Yes Yes No 0/0/0 0/0/0 0.0000 6 531010 0/0/0 Yes Yes No 0/0/0 0/0/0 0.0000 2 5/6/0 33/10/0 Yes Yes Yes 01010 0/0/0 0.0000 5 47/6/0 33/10/0 Yes Yes Yes 0/0/0 0/0/0 0.0000 Values shown are resisting forces of the foundation. r d Reactions-Un actore Load Type at Frame Cross Section: 2 Type Exterior Column Exterior Column X~Loc 01010 53/0/0 Grid I -Grid2 2-D 2-A Base Plate W x L (in.) 8 X 13 8 X }3 Base Plate Thickness (in.) 0.375 0.375 .. Anchor Rod Qty/Diam. (in.) 4-0.750 4. 0.750 Column Base Elev. 100'-0" !00'-0" Load Type Desc. Hx Vv Hx Vv D Frm 0.7 3.8 -0.7 3.8 . AD Frm 0.1 0.8 -0.1 0.8 -. CG Frm 2.0 7.9 -2.0 77 - s Frm 7.3 28.6 -7.3 28.6 US!"' Frm 6.5 16.9 -6.5 34.5 - *US I Frm 6.5 34.5 -6.5 16.9 . W1> Frm -6.3 -10.4 -4.0 -3.5 . - File: 7079 Chevron Rl_Stress Check !0_2008 with 08_2008 Loading Version: 7.la ) 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 96 of 175 <W1 Fm1 4.0 -3.5 6.3 -10.4 - W2> FJID -7.3 -7.6 -2.9 -0.7 - <W2 Fnn 2.9 -0.7 7.3 -7.6 - *AL> Fnn -0.1 10.0 -1.8 4.7 - AL*> Fnn -0.1 2.7 -1.8 12.0 - <*AL Fn:n 1.8 12.0 0.1 2.7 - <AL* Fnn 1.8 4.7 0._1 10.0 cu Fnn 1.0 3.8 -1.0 3.8 --- E> Fnn -3.2 -4.2 -3.1 4.2 - EG+ Fnn 0.3 1.0 -0.3 1.0 - <E Fnn 3.2 . 4.2 3.1 -4.2 -- EG-Fnn -0.3 -1.0 0.3 -1.0 --- EB> Brc - -- ---- <EB Brc - - - --- WPA1 Brc 1.5 -7.7 -l.l -7.2 -- 'AL Fnn 0.9 11.0 -0.9 3.7 -- ALB> Brc - - ---- AL' Fnn 0.9 3.7 -0.9 11.0 --- WPD1 Brc 1.8 -5.7 -1.6 -5.4 --- <ALB Brc -- - ---- WPA2 Brc 0.4 -4.8 -0.1 -4.4 --- WPD2 Brc 0.8 -2.8 -0.6 -2.6 --- WPB1 Brc l.l -7.2 -1.5 -7.7 --- WPC1 Brc 1.6 -5.4 -1.8 -5.7 --- WPB2 Brc 0.1 -4.4 -0.4 -4.8 --- WPC2 Brc 0.6 ~2.6 -0.8 -2.8 --- Maximum Combined Reactions Summarv with Factored Loads M Framing X~Loc Grid Hrz left Load HrzRight Load Hrzln Load Hrz Out Load Uplift Load Vrt Down Load Morncw Load Momccw Load (-Hx) -(k). Case (~) Case (-Hz) -(k). Case ~~) Case (~i) Case (~~) Case (-Mzz) lin-kl Case (Mzz) iin-ki Case 0/0/0 2-D 6.2 18 11.2 9 - -- -5.4 16 47.0 3 - -- - 531010 2-A 11.2 8 6.2 19 - -- -5.4 17 46.7 2 - -- - Sum of Forces with Reactions Check~ Framine: Horizontal Vertical Load Type L~~ Re~~~ion Load Reaction (k) (k) . D 0.0 0.0 7.7 7.5 AD 0.0 0.0 1.7 1.6 CG 0.0 0.0 15.5 15.5 s 0.0 0.0 57.1 57.1 USl* 0.0 0.0 51.4 51.4 *USl 0.0 0.0 51.4 51.4 WI> 10.2 10.2 13.9 13.9 <W1 10.2 10.2 13.9 13.9 W2> 10.2 10.2 8.2 8.2 <W2 10.2 10.2 8.2 8.2 'AL> 1.9 1.9 15.5 14.7 AL*> 1.9 1.9 15.5 14.7 <*AL 1.9 1.9 15.5 14.7 <AL* 1.9 1.9 15.5 14.7 cu 0.0 0.0 7.6 7.6 E> 6c2 6.3 0.0 0.0 EG+ 0.0 0.0 2.0 2.0 <E 6.2 6.3 0.0 0.0 EG-0.0 0.0 2.0 2.0 EB> 0.0 0.0 0.0 0.0 <EB 0.0 0.0 0.0 0.0 WPAI 0.4 0.4 14.9 14.9 'AL 0.0 0.0 15.5 14.7 ALB> 0.0 0.0 0.0 0.0 AL' 0.0 0.0 15.5 14.7 WPD1 0.2 0.2 II.! 11.1 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 97 of !75 WPA2 0.4 0.4 9.2 9.2 WPD2 0.2 0.2 5.4 5.4 WPBl 0.4 0.4 14.9 14.9 WPCl 0.2 0.2 ll.l ll.l WPB2 0.4 0.4 9.2 9.2 WPC2 0.2 0.2 5.4 5.4 Base Plate Summary X-Loc Grid Mem. Thickness Width Length Nurn.Of Bolt Diam. Type Welds to Welds to No. (in.) lin.) (in~) Bolts (in.) Flam~e Web 0/0/0 2-D l 0.375 8 13 4 0.750 A36 OS-0.1875 OS-0.1875 53/0/0 2-A 6 0.375 8 13 4 0.750 A36 OS-0.1875 OS-0.1875 Web Stiffener Summar Mem. Stiff. Desc. Loc. Web Depth hit alh a Thick. Width Side Welding No. No. (ft) (;n.). (in.) (in.) (in.) Description 2 l 89 4.11 43.400 173.60 N/A N/A 0.3750 2.500 Both W-OS-0.1875 2 2 Sl 14.05 28.739 114.96 3.00 85.99 0.1875 2.000 Both Std 5 l 89 14.51 43.401 173.60 N/A N/A 0.3750 2.500 Both W-OS-0.1875 5 2 Sl 11.44 38.869 155.48 3.00 116.03 0.1875 2.000 Both F-OS-0. l875,W-OS-O. 1875 B k P S rae ets art ummarv Merri. Loc. Total Length Bracket Cut Bracket Fig Width FlgThk WebThk Hole Pitch Stiffener or Plate Part No. (ftl (in.) (in.) Deoth (in,\ -lin.) lin.) lin.) (in.) . 2 3.98 15.000 4.750 10.000 6.000 0.2500 0.2500 3.500 UP0704ll 000 WU15041234 5 14.65 15.000 4.750 10.000 6.000 0.2500 0.2500 3.500 UP0704 Ll 000 WU15041234 Brackets Desie.n Summary (vertical live load is with the impact factor Mem. Loc. Vert. Live Vert, Dead Lateral Longitudinal CL Distto Member Member WebThk FlgThk Fig Width No. (ft) Load (k) Load (k) Impact (k) Impact (k) Flange (in.) Depth! (in.) Depth2 (in.) On.) fin.) -lin.) 2 3.98 13.72 0.86 0.94 1.47 13.191 42.305 40.010 0.2500 0.5000 6.0000 5 14.65 13.72 0.86 0.94 1.47 13.191 41.010 41.306 0.2500 0.5()l)J) 6.0000 Bolted EndwPJate Moment Connections (AISC DG-16)-Fy =55 ksl End-Plate Dimensions Bolt Outside Flange Ii1side Flange Mem. Jt. Type Thick. Width Length Diam. Spec/Joint Gages In/Out Configuration Pitches 1st/2nd ConfiRuration Pitches 1st/2nd No. No. (in.) (in.) (in.) (in.) (in.) lD Desc. (in.) lD Desc. (in.) 1 2 KN(Top) 0.500 6.00 48.00 0.750 A325X/ST 3.50 12 Flush 2.00 ll Flush 2.00 2 l KN(Top) 0.500 6.00 48.00 0.750 A325X/ST 3.50 12 Flush 2.00 ll Flush 2.00 3 2 SP 0.375 6.00 33.92 0.750 A325X/ST 3.00 ll Flush 0.00 32 Extended 3.56/2.00 4 l SP 0.375 6.00 33.92 0.750 A325X/ST 3.00 11 Flush o.oo 32 Extended 3.56/2.00 5 2 KN(Top) 0.500 6.00 48.00 0.750 A325X/ST 3.50 12 Flush 2.00 ll Flush 2.00 6 2 KN(Top) 0.500 6.00 48.00 0.750 A325X/ST 3.50 12 Flush 2.00 ll Flush 2.00 Required Strength -Out Available Strength-Out Required Strength -In Available Strength -In Mem. Jt. Ld Axial Shear Moment Design Shear Moment Ld Axial Shear Moment Design Shear Moment No. No. Cs (k) (k) (in-k) Pro c. (k) (in-k) Cs (k) (k) (in-k) Proc. (k) lin-k) l 2 2 -29.5 7.8 2636.7 Thin plate 159.0 1914.5 16 5.4 l.l 1020.3 Thin plate 106.0 1465.3 2 I 2 -29.5 7.8 2636.7 Thin plate 159.0 1914.5 16 5.4 l.l 1020.3 Thin plate 106.0 1465.3 3 2 17 2.7 3.1 41.2 Thin plate 106.0 595.5 l -9.8 2.4 1314.3 Thin plate 212.1 1206. 4 l 17 2.7 3.1 41.2 Thin plate 106.0 595.5 l -9.8 2.4 1314.3 Thin plate 212.1 1206.4 5 2 J -29.6 7.8 2655.3 Thin plate 159.0 1938.9 17 5.4 l.l 1020.3 Thin plate 106.0 1466.6 6 2 J -29.6 7.8 2655.3 Thin plate 159.0 1938.9 17 5.4 l.l 1020.3 Thin plate 106.0 1466.6 . Flanee Brace Summary Member From Member Joint I From Side POint l Part De~ign Note I 12/5/4 12/5/4 FB2114 l 22/514 22/5/4 FB4050 l 27/5/4 27/5/4 (2)FB5060 2 5/3/8 22/9/13 (2)FB5080 3 1/8/0 719113 FB3024 3 7/8/0 l/9113 FB4020 4 l/6/0 1/9113 FB4020 5 7/4/0 16/9113 FB4054 5 1314/0 22/9113 (2)FB5084 6 12/5/4 12/5/4 FB2\14 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 98 of !75 22/5/4 27/5/4 22/5/4 27/5/4 Frame Design Member Summary_~ Controlli!_lg l.<l\~ Case and Maximum Combined Stresses oer Member (Locations are from Joint 1) Actual Forces Actual Stresses A!!owable Stress Condition Mem. Loc. Depth Load Axial Shear Mom~x Mom-y Axial Shear Bnd-X Bnd-Y . .. Stress /Force . .. Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear I 22.47 39.75 I -41.2 -7. -2120.7 0.0 2.89 0.81 14.84 0.00 25.15 3.42 24.20 41.25 0.72 0.24 2 17.19 23.00 3 -11.8 4.3 1490.3 0.0 1.02 0.77 17.46 0.00 29.38 10.74 33.00 41.25 0.56 0.07 3 1.67 24.20 3 -10.4 2.3 1565.9 0.0 1.06 0.59 20.03 0.00 29.81 4.18 32.82 41.25 0.64 0.14 4 7.10 24.20 2 -10.4 -2.3 1560.7 0.0 1.06 0.61 19.9 0.00 29.81 4.18 32.82 41.25 0.64 0.15 5 0.00 23.00 2 -11.8 -4.3 1484.0 0.0 1.02 0.78 17.39 0.00 29.38 10.74 33.00 41.25 0.56 O.o7 6 22.47 39.75 I -41.3 7.9 -2139.5 0.0 2.90 0.81 14.97 0.00 21.49 3.42 24.22 41.25 0.72 0.24 Mem. Loc. Depth Area Rx Ry Lx Ly-1 Ly-2 Klx Klyl Kly2 Sx Lbl Rt-1 Lb2 Rt-2 Qs Qa Cb! Cb2 No. ft in. in.2 in. in. in. in. in. /Rx /Ry /Ry in.3 in. in. in. in. I 22.47 39.75 14.25 14.46 0.98 340.05 30.0 60.1 35.3 30.8 61.6 142.90 120.2 1.35 60.1 1.34 1.00 0.86 1.26 1.09 2 17.19 23.0 11.50 9.24 1.25 294.79 36.0 0.0 31.9 28.8 0.0 85.33 36.0 1.56 0.0 0.00 1.00 1.00 1.05 0.00 3 1.67 24.20 9.81 10.16 1.35 294.79 36.0 36.0 29.0 26.6 26.6 78.18 36.( 1.62 36.0 1.62 1.00 1.00 1.05 1.01 4 7.10 24.20 9.81 10.!6 1.35 294.79 36.0 36.0 29.0 26.6 26.6 78.18 36.0 1.62 36.0 1.62 1.00 1.00 1.00 1.05 5 0.0( 23.00 11.50 9.24 1.25 294.7 36.0 0.0 31.9 28.8 0.0 85.33 36.0 1.5 0.0 0.00 1.00 1.00 1.05 0.00 6 22.47 39.75 14.25 14.46 0.98 340.05 60.1 60.1 35.3 61.6 61.6 142.90 120.2 1.35 60.1 1.3 1.00 0.86 1.26 1.0 0 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 99 of 175 User Defined Frame Point Loads for Cross Section: 2 Side Units T e Descri tion Ma I Loci Offset H orV Su Dir. Coef. Loc. I k CG PS-46 Pi e Loads ·0.30 16/713 31310 Horiz. N DOWN 1.000 IF y X Deflection Load Combinations ~ Framin No. Origin Factor DefH DefY Application Description I System 1.000 0 240 1.0 s s 2 System 1.000 0 240 l.OUSI' ~sr• 3 System 1.000 0 240 1.0 *USt •us1 4 System 1.000 0 240 0.700WI> twl> 5 System 1.000 0 240 0.700<WI ~~ 6 System 1.000 0 240 0.700WG> f'2> 7 System 1.000 0 240 0.700<W2 pv2o 8 System Derived 1.000 0 240 0.700WPAI WPAI 9 System Derived 1.000 0 240 0.700WPDI f'PDI 10 System Derived 1.000 0 240 0.700WPA2 WPA2 II System Derived 1.000 0 240 0.700WPD2 twPo2 12 System Derived 1.000 0 240 0.700WPBI WPBI 13 System Derived 1.000 0 240 0.700WPCI [WPCI 14 System Derived 1.000 0 240 0.700WPB2 WPB2 15 System Derived 1.000 ·o 240 0.700WPC2 WPC2 16 System 1.000 400 0 0.700WI> WI> 17 System 1.000 400 0 0.700<WI <WI 18 System 1.000 400 0 .700W2> W2> 19 System 1.000 400 0 0.700<W2 W2 20 System Derived 1.000 400 0 0.700WPAI WPAI 21 System Derived 1.000 400 0 0.700WPDI WPDI 22 System Derived 1.000 400 0 0.700WPA2 WPA2 23 System Derived 1.000 400 0 0.700WPD2 WPD2 24 System Derived 1.000 400 0 0.700WPBI WPBI 25 System Derived 1.000 400 0 0.700WPCI WPCI 26 System Derived 1.000 400 0 0.700 WPB2 WPB2 27 System Derived 1.000 400 0 0.700 WPC2 WPC2 28 System 1.000 100 0 0.600 E> + 0.700 EO· E>+EO- 29 System 1.000 100 0 0.600 <E + 0.700 EO-<E +EO- 30 System Derived 1.000 100 0 0.600 EB> EB> 31 System Derived 1.000 100 0 0.600<EB EB 32 System 1.000 400 0 1.0 <AL* <AL' 33 System 1.000 400 0 1.0 *AL> *AL> Controlling Frame Dellection Ratios for Cross Section: 2 Description Ratio Deflection in. Member Joint Load Case Load Case Description MaX. Horizontal Deflection ( H/466) -0.762 6 2 19 <W2 . !Max. Vertical Deflection for Soan I ( L/737 ) -0.792 4 I I s File: 7079 Chevron R !_Stress Check 10 _2008 with 08_2008 Loading Version: 7.1a ) 07-27053 Calculations Hazardous Materials Occupancy "' Negative horizontal deflection is left * Negative vertical deflection is down Date: 10/20/2008 Time: I :57:43 PM Page: IOOof 175 Lateral deflections of primary frames are calculated on a bare frame basis and do not include resistance from systems such as roof and endwa\1 diaphragms. Therefore, these deflections may be considerably overstated. 0 0 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy y Dimension Key I 5'~6" BL to CLofRunway Beam 2 I 5/8" 3 4'...(}" 4 3'-5 1/4" 5 2@ 5'-0" 6 2@2'-6" 7 3'-33/4" 8 l'-3" 9 l'-9 13/16" !0 2@ 2'-4 7/16" II 4 1/2" 12 40'-10" Ridge Ht. X FRAME CROSS SECTION AT FRAME LINE(S) 3 File: 7079 Chevron R 1_ Stress Check I 0 _2008 with 08 _ 2008 Loading Version: 7.1a Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Frame Clearances Horiz. Clearance between members l(CXOOO) and 6(CXOOO): 45'-4 3/4" Vert. Clearance at member l(CXOOO): 28'-0 1/2" Vert. Clearance at member 6(CXOOO): 28'-0 \/2" Finished Floor Elevation= 100'-0" (Unless Noted Otherwise) Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA 1-l(Left): 2'-4 3116" Horz. Clearance at CRANE DATA 1-l(Left): I '-10 1/8" Vert. Clearance at CRANE DATA !-!(Right): 2'-4 3116" Horz. Clearance at CRANE DATA !-!(Right): 1'-10 11811 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: 102ofl75 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: l03ofl75 Desc1i tion An \e Grou Trib. Override Desi n Status Stress Check 90.0000 Desi n Load Combinations-Framin No. Origin Factor Application Descriotion I System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 S D+AD+CG+S 2 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 US!' D'+AD+CG+USl* 3 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 *US1 D+AD+CG+"'USI 4 System 1.000 l.OD+ LOAD+ l.OCG+ l.OWl> D +AD+ CG +WI> 5 System 1.000 !.0 D+ !.0 AD+ 1.0 CG + l.O <WI D+AD+CG+<Wl 6 System !.000 !.0 D + l.O AD+ l.O CG + l.O W2> D+AD+CG+W2> 7 System !.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <W2 D+AD+CG+<W2 8 System !.000 !.0 D+ 1.0 AD+ 1.0 CG +0.750 S +0.750 WI> D+AD+CG+S+Wl> 9 System !.000 !.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 <WI D+AD+CG+S+<Wl 10 System !.000 l.O D + 1.0 AD+ l.O CG + 0.750 S + 0.750 W2> D+AD +CG+S+W2> 11 System !.000 l.O D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System 1.000 1.0 D + l.O AD+ LOCO+ 1.0 *AL> D +AD +CG+*AL> 13 System !.000 l.OD +LOAD+ l.OCG+ l.OAL"'> D+AD+CG+AL*> 14 System 1.000 1.0 D + 1.0 AD+ l.OCG + 1.0 <*AL D +AD +CG+<*AL 15 System 1.000 l.OD + 1.0 AD+ 1.0 CG + 1.0 <AL* D+AD+CG+<AL' 16 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WI> D+AD+CU+Wl> 17 System 1.000 Q.600 D + o.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<Wl 18 System . 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 W2> D+AD+CU+W2> 19 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 1.0 D+ 1.0 AD+ l.OCG +0.563 S +0.750 'AL> D+AD+CG+S+*AL> 2I System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL '> jo+AD+CG+S+AL*> 22 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750<'AL [o +AD+ CG + S+<*AL 23 System 1.000 1.0 D+ 1.0 AD+ l.OCG +0.563 S +0.750 <AL' io + AD+CG+S+<AL' 24 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WI>+0.750 'AL> D+AD+CG+Wl>+*AL> 25 System 1.~00 1.0 D + 1.0 AD+ 1.0 CG +0.375 Wl>+0.750 AL*> ID+AD+CG+Wl>+AL*> 26 System I. 00 1.0 D +LOAD+ 1.0 CO +0.375 <WI +0.750<*AL lo+AD+CG+<WI+<*AL 27 System 1.000 1.0 D+ 1.0 AD+ l.OCG +0.375 <WI +.0.750 <AL' jo+AD+CG+<Wt+<AL* 28 System 1.000 1.0 D +LOAD+ 1.0 CG+0.375 W2>+0.750 'AL> jo +AD + CG + W2>+* AL> 29 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 W2> +0.750 AU·> In+ AD +CO + W2>+AL *> 30 System 1.000 1.0 D+ 1.0 AD+ l.OCG +0.375 <W2 +0.750<'AL P+AD+CG +<W24<*AL 31 System 1.000 1.0 D+ 1.0 AD+ 1.0 CG+0.375 <W2+0.750 <AL' ID +AD + CG + <W2+<AL * 32 System 1.000 1.0 D + l.O AD+ 1.0 CG +0.150 S +0.750 E>+0.700 EG+ io+AD+CG+S+E>+EG+ 33 System 1.000 1.0 D+ I.OAD + l.OCG+0.150 S +0.750 <E+0.700 EG+ io+AD+CG+S+<E+EG+ 34 System 1.000 .600 D+0.600 AD+0.600 CU +0.700 E>+0.700 EG-lo+AD+CU+E>+EG~ 35 System 1.000 o.600 D + 0.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-!o+AD+CU+<E+EG~ 36 System Derived 1.000 1.0 D + 1.0 AD+ l.OCG +0.150 S +0.750 EB>+0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 .600 D + 0.600 AD+ o.600 CU + 0.700 EB> + 0.700 EG-/D+AD+CU+EB>+EG~ 38 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.150 S +0.750 <EB +0.700 EG+ ~AD+CG+S+<EB+EG+ 39 System Derived 1.000 Q.600 D + 0.600 AD+ 0.600 CU + 0.700 <EB + 0.700 EG-D+AD+CU+<EB+EG~ 40 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 1.0 WPAI D+AD+CG+WPAI 41 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPAI D+AD+CG+S+WPAI 42 System Derived 1.000 o.600 D +0.600 AD+ 0.600CU + 1.0 WPAI D +AD+ CU + WPAI 43 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPAI + 0.750 'AL +0.750 ALB> D+AD+CG+WPAl+*AL+ALB> 44 System Derived 1.000 l.O D+ 1.0 AD+ l.O CG + 0.375 WPAl +0.750 AL* +0.750 ALB> D+AD+CG+WPA l+AL *+ALB> 45 System Derived !.000 !.0 D + 1.0 AD+ 1.0 CG + 1.0 WPDI D+AD+CG+WPDI 46 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 WPDI jo +AD+ CG + S + WPDt 47 System Derived 1.000 .600 D+0.600 AD +0.600 CU + !.0 WPDI D+AD+CU+WPDl 48 System Derived 1.000 l.O D + 1.0 AD+ 1.0 CG + 0.375 WPDI +0.750 *AL + 0.750 <ALB D+AD+CG+WPD I+"' AL +<ALB 49 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDI + 0.750 AL' + 0.750 <ALB D+AD+CG+WPDI+AL*+<ALB 50 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA2 D+AD+CG+WPA2 51 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPA2 D+AD+CG+S+WPA2 52 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPA2 D+AD+CU+WPA2 53 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 + 0.750 *AL + 0.750 ALB> p+AD+CG+WPAi+*AL+ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 + 0.750 AL * + 0.750 ALB> D+AD+CG+WPA2+AL *+ALB> 55 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO + 1.0 WPD2 D+AD+CG+WPD2 56 System Derived 1.000 l.O D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 WPD2 p+AD+CG+S+WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPD2 + 0.750 *AL +0.750 <ALB D+AD+CO+WPD2+"' AL +<ALB 59 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPD2 + 0.750 AL* + 0.750 <ALB D+AD+CG+WPD2+AL *+<ALB File: 7079 Chevron Rl_Stress Check 10_2008 wiih 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: I 04 of 175 60 sYstem Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + I.OWPB! 61 System Derived 1.000 1.0 D + 1.0 AD +.1.0 CG + 0.750 S +0.750 WPB! 62 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + !.0 WPB 1 63 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0375 WPBJ +0.750 *AL + 0.750 ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPBI + 0.750 AL* +0.750 ALB> 65 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPC! 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC! 67 System Derived _ 1.000 0.600 D+ 0.600 AD+ 0.600 CU + 1.0 WPC! 68 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPCl + 0.750 *AL +0.750 <ALB 69 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 0.375 WPCI + 0.750 AL * +0.750 <ALB 70 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPB2 71 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 73 System Derived !.000 !.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 + 0.750 'AL+0.750 ALB> 74 System Derived !.000 1.0 D + 1.0 AD+ 1.0 Cd +0.375 WPB2 +0.750 AL* +0.750 ALB> 75 System Derived !.000 !.0 D + !.0 AD + 1.0 CG + !.0 WPC2 76 System Derived !.000 !.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPC2 77 System Derived !.000 0.600 D + 0.600 AD+ 0.600 CU + !.0 WPC2 78 System Derived !.000 !.0 D + !.0 AD+ 1.0 CG +0.375 WPC2 +0.750 'AL +0.750 <ALB 79 System Derived !.000 !.0 D + !.0 AD+ 1.0 CG + 0.375 WPC2 + 0.750 AL' + 0.750 <ALB 80 System Derived !.000 l.OD+ LOAD+ l.OCG+ LOS+ l.OALB> 81 S Y$tem Derived !.000 1.0 D + 1.0 AD + l.O CG + l.O "'AL + 1.0 ALB> 82 System Derived !.000 1.0 D + 1.0 AD + 1.0 CO + 1.0 AL"' + 1.0 ALB> 83 System Derived !.000 !.0 D + 1.0 AD+ l.OCG +0.563 S +0.750 'AL+ 0.750 ALB> 84 System Derived !.000 !.0 D+ !.0 AD+ 1.0 CG +0.563 S +0.750 AL' + 0.750 ALB> 85 System Derived !.000 i.O D + 1.0 AD + 1.0 CG + !.0 S + !.0 <ALB 86 System Derived !.000 1.0 D+ 1.0 AD+ 1.0 CG + 1.0 *AL + 1.0 <ALB 87 System Derived !.000 1.0 D + l.O AD+ l.O CO+ 1.0 AL* + l.O<ALB 88 System Derived !.000 !.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 'AL+0.750 <ALB 89 System Derived !.000 !.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL' + 0.750 <ALB Frame Member Sizes 0 Mem. Fig Width F!gThk WebThk Dct>,t~l Depth2 Length w(t' FlgFy No. ~(in.) (in.) (in.) . (in. (in.) (ft) {ksi) 1 6.00 0.5000 0.2500 !2.00 44.00 3!.03 1278.0 55.00 2 6.00 0.5000 0.2500 48.00 24.00 !7.79 974.2 55.00 3 6.00 0.5000 0.1644 24.00 28.00 !0.00 343.6 55.00 4 6.00 0.5000 0.!644 28.00 24.00 10.00 343.5 55.00 5 6.00 0.5000 0.2500 24.00 48.00 17.79 974.2 55.00 6 6.00 0.5000 0.2500 12.00 44.00 3!.03 1278.0 55.00 Total Ftame We1ght-519!.5 (p) Frame Pricing Weight= 5740.1 (p) 6 2 53/0/0 5/6/0 01010 33/!0/0 Yes Yes Yes Yes No Yes 0/0/0 01010 Values shown are resisting forces of the foundation. Reactions-Unfactored Load T_ype at Frame Cross Section: 3 Type Exterior Column Exterior Colurrm X-Loc 01010 53/0/0 Grid!-Grid2 3~D 3-A Base Plate W x L (in.) 9 X 13 9x l3 Base Plate Thickness (in.) 0.500 0.500 Anchor Rod Qty/Diam. (in.) 4. 1.000 4. !.000 Column Base Elev. 100'-0" 100'-0" Load Type Desc. Hx Hz Yv Hx Hz Vy D Frm 0.8 . 4.3 -0.8 4.3 . AD Frm 0.1 !.! -0.1 . 1.1 CG Fnn 2.6 . 12.3 -2.6 10.! s Frm 9.8 . 38.3 -9.8 38.3 . US!* Frm 8.8 . 22.7 -8.8 46.2 . *US! Fnn 8.8 46.2 -8.8 22.7 . WI> Fnn -6.9 . -12.0 -4.6 -4.3 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading D +AD+ CG + WPBt D+AD+CG+S+WPBI D+AD+CU+WPBI D+AD+CG+WPB I+* AL +ALB> D+AD+CG+WPB l+AL *+ALB> D +AD+ CG + WPC! D+AD+ CG +S +WPCl p+AD+CU+WPC! D+AD+CG+WPCI+*AL+<ALB D+AD+CG+WPCl+AL*+<ALB D+AD+CG+WPB2 jo+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+AL *+ALB> [?+AD+CG+WPC2 D+AD+CG+S+WPC2 D+AD+CU+WPC2 io+AD+CG+WPC2+*AL+<ALB !rHAD+CG+WPC2+AL *+<ALB D+AD+CG+S+ALB> iD + AD+ CG+* Ai.+ALB> ~+AD+ CG+AL *+ALB> r+AD+CG+S+*AL+ALB> P+AD+CG+S+AL*+ALB> D+AD+CG+S+<ALB D +AD + CG+* AL+<ALB D + AD + CG+AL *+<ALB [D+AD+CG+S+* AL+<ALB P+AD+CG+S+AL '+<ALB WebFy Splice (ksi). Jt.l 55.00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP (Includes all plates) (Includes all pieces) 01010 01010 . . . . . . Version: 7. ta Codes Jt.2 KN ss SP ss KN KN 0.0000 0.0000 . ' . . . . Shape 3P 3P 3P 3P 3P 3P 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: l :57:43 PM Page: l 05 of 175 <WI Fm1 4.6 --4.3 6.9 --12.0 -- W2> Fm1 -8.3 --8.1 -3.2 --0.4 -- <W2 Fnn 3.2 --0.4 8.3 --8.\ -- *AL> Fm1 -0.\ 10.0 -1.8 4.7 -- AL*> Fm1 -0.1 2.7 -\.8 -12.0 -- <*AL Fnn \.8 12.0 0.\ -2.7 -- <AL"' Fm1 1.8 -4.7 0.\ 10.0 cu Fom 1.3 -5.\ -1.3 -5.\ -- E> Fm1 -4.2 --5.5 -4.\ 5.5 - EG+ Fm1 0.3 \.5 -0.3 -\.3 -- <E Fnn 4.2 -5.5 4.\ --5.5 -- EG-Fnn -0.3 --1.5 0.3 --1.3 --- EB> Brc 0.5 -19.3 -32.3 -0.5 -19.3 -32.4 --- <EB Brc -0.3 0.0 29.0 0.3 0.0 29.0 -- WPAI Brc 2.\ -4.4 -17.6 -1.6 -3.8 -16.\ -- 'AL Fnn 0.9 -1\.0 -0.9 -3.7 -- ALB> Brc - - ----- AL' Fnn 0.9 -3.7 -0.9 -11.0 - WPDI Brc 2.4 --1.0 -2.1 --1.5 -- <ALB Brc ------ -- WPA2 Brc 0.7 -4.4 -13.8 -0.2 -3.8 -\2.3 --- WPD2 Brc 1.0 -2.8 -0.7 -2.3 --- WPBI Brc \.6 -3.8 -16.1 -2.1 4.4 -17.6 -- WPCI Brc 2.1 --1.5 -2.4 --1.0 --- WPB2 Brc 0.2 -3.8 -12.3 -0.7 -4.4 -13.8 --- WPC2 Brc 0.7 -2.3 -1.0 -2.8 --- Maximum Combined Reactions Summary with Factored Loads M Framinu XMLoc Grid Hrz left Load HrzRight Load Hrzln Load Hrz Out Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-~~) Case (~) Case (-~~) Case ~~) Case (-Vy) Case (Vy) Case (-Mzz) Case (Mzz) Case (kl ... (k) fin-k) (in-k) 0/0/0 3-D 7.0 I8 I4.3 9 14.4 36 0.0 38 I7.3 37 63.9 3 ---- 53/010 3-A I4.3 8 7.0 I9 14.5 36 0.0 38 I7.3 37 61.8 2 ---- Sum of Forces with Reactions Check-Framin£!: . Horizontal Vertical Load Type L~~d Re~~ion ~~d Rea~~ion D 0.0 0.0 8.8 8.7 AD 0.0 0.0 2.3 2.2 CG ' 0.0 0.0 22.4 22.4 s 0.0 0.0 76.5 76.5 USl* 0.0 0.0 68.9 68.9 *USl 0.0 0.0 68.9 68.9 WI> II.S I\.5 I6.2 I6,2 <WI I\.5 ll.5 I6.2 I6.2 W2> 11.5 !l.S 8.6 8.6 <W2 11.5 !l.5 8.6 8.6 'AL> \.9 1.9 15.5 I4.7 AL*> \.9 \.9 I5.5 I4.7 <*AL \.9 \.9 15.5 I4.7 <AL* 1.9 1.9 I5.5 14.7 cu 0.0 0.0 10.2 !0.2 E> 8.3 8.3 0.0 0.0 EG+ 0.0 0.0 2.9 2.9 <E 8.3 8.3 0.0 0.0 EG-0.0 0.0 2.9 2.9 EB> 0.0 0.0 0.0 64.7 <EB 0.0 0.0 0.0 58.0 WPAI 0.5 0.5 19.9 33.7 'AL 0.0 0.0 I S.S 14.7 ALB> 0.0 0.0 0.0 0.0 AL' 0.0 0.0 15.5 14.7 WPDI 0.3 0.3 14.8 2.5 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la . 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 T;me: I :57:43 PM Page: 106ofl75 WPA2 0.5 0.5 12.3 26.1 WPD2 0.3 0.3 7.2 5.2 WPB! 0.5 0.5 19.9 33.7 WPC! 0.3 0.3 !4.8 2.5 . WPB2 0.5 0.5 12.3 26.1 WPC2 0.3 0.3 7.2 5.2 Base PI S ate urn mary X·Loc Grid Mem. Thickness Width Length Num.Of Bolt Diam. Type Welds to Welds to No. (in.) lin.) (in~) Bolts (in.) Flange Web 010/0 3-D l 0.500 9 13 4 !.000 A36 08-0.!875 08-0.1875 531010 3-A 6 0.500 9 13 4 !.000 A36 08-0.!875 OS-0.1875 w 8-8 eb tlffener Uffiffil:\f Mem. Stiff. Desc. Loc. Web Depth hit alh a Thick. Width Side Welding No. No. (ft) (in.)· (in.) (in.) (in.) Description 2 l 89 3.85 45.069 180.27 NIA NIA • 0.5000 2.500 Both W-08-0.1875 2 2 81 13.17 30.308 12!.23 3.00 90.78 0.2500 2.000 Both 8td 5 l 89 13.94 45.069 180.27 NIA NIA 0.5000 2.500 Both W-08-0.!875 5 2 81 12.29 42.460 169.84 3.00 !27.00 0.2500 2.000 Both F-08-0.!875,W-OS-0.!875 Brackets Part Summary . Mem. Loc. Total Length Bracket Cut Bracket Fig Width Flg~k WebThk Hole Pitch Stiffener or Plate Part No. (ft) (in.) (in.) Depth (in. -(in.) (in. _(in.) _(in.) 2 3.96 14.500 4.8!3 10.000 6.000 0.2500 0.2500 3.500 UP0704!!000 WU!444!334 5 !3.87 !2.375 4.375 10.000 6.000 0.2500 0.2500 3.500 UP0704ll 000 WU!2340634c_ Brackets Design Summ;:t_!Y_(verticallive load is with the imDact factor Mem. Loc. Vert. Live Vert. Dead Lateral Longitudinal CL Dist to Member Member WcbThk FlgThk Fig Width No. (ft] . Load_{!<) Loadlkl lmoact (k) Impact (k) Flange (in.) Deothl (in.) Deoth2 (in.) (in.) (in.) -(in.) 2 3.96 13.72 !.!5 0.94 !.47 1!.741 43.403 4!.012 0.2500 0.5000 6.0000 5 !3.87 13.72 !.!5 0.94 !.47 1!.741 42.012 42.403 0.2500 0.5000 6.0000 0 Bolted End-Plate Moment .Connections (AISC DG-16)-Fv =55 ksl End-Plate Dimensions Bolt Outside Flange Inside Flange Mem. Jt. Type Thick. Width Length Diam. Spec/Joint Gages In/Out Co.nfiouration Pitches 1st/2nd Config!:lration Pitches 1st/2nd No. No. (in.) (in.) (in~) (in.) -(in.) ID DeSc. (in.) ID Desc. (in.) l 2 KN(fop) 0.625 6.00 45.00 0.750 A325XIST 3.50 12 Flush 2.00 ll Flush 2.00 2 l ; KN(Top) 0.625 6.00 45.00 0.750 A325XIST 3.50 12 Flush 2.00 ll Flush 2.00 3 2 SP 0.375 6.00 33.00 0.750 A325XIST 3.00 ll Flush 0.00 42 Ext/Gusset 3.69/2.00 Gusset In 3.000 x 0.2500 x 5.25 FO-BS-0.1875, I 4 I l I SP I 0.375 I 6.00 I 33.00 I 0.750 I A325XIST I 3.00 Itt I Flush 0.00 142 I Ex11Gusset I 3.69/2.00 Gusset In 3.000 x 0.2500 X 5.25 FO-BS-0.1875, I 5 I 2 I KN(Top) I 0.625 I 6.00 I 45.00 I 0.75~ I A325XIST I 3.50 6 2 KN(Tooi 0.625 6.00 45.00 0.750 A325XIST 3.50 Required Strength -Out Available Strength -Out Mem. Jt. Ld Axial Shear Moment Design Shear Moment No. No. Cs (k) (k) (in-k) Proc. (k) (in-k) l 2 2 -38.9 !0.5 3585.5 Thin plate !59.0 28!4.0 2 l 2 -38.9 !0.5 3585.5 Thin plate !59.0 28!4.0 3 2 17 3.1 3.6 17.8 Thin plate !06.0 574.5 4 l 17 3.1 3.6 !7.8 Thin plate !06.0 574.5 5 2 3 -38.8 10.5 3550.5 Thin plate 159.0 2814.0 6 2 3 -38.8 !0.5 3550.5 Thin plate 159.0 28!4.C 2215/4 22/5/4 l 27/5/4 27/5/4 2 2/!l/l 25/214 3 216/0 7/91!3 3 816/0 119113 4 1/6/0 J/9113 5 6/610 !6191!3 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading I :; I Flush I. 2.00 Flush 2.00 Required Strength -In Ld Cs !6 !6 l l 17 17 Axial (k) 5.7 5.7 -13.0 -13.0 5.7 5.7 SFB4034 (2)FB5040 (2)FB5114 FB3030 FB3050 FBJQ50 FB4060 Shear Moment (k) (in-k) !.4 !!27.8 !.4 1127.8 3.3 1698.7 3.3 1698.7 1.4 1127.8 !.4 !!27.8 I:: I Flush j 2.00 I Flush 2.00 Available Streng h-In Design Shear Moment Proc. (k) (in-k) Thick plate !06.0 !660.0 Thick plate !06.0 1660.0 Thin plate 2!2.1 1547.4 Thin plate 2\2.! 1547.4 Thick plate !06.0 !660.0 Thick plate 106.0 1660.0 Verslon: 7.1a ' 5 6 6 6 07-27053 Calculations Hazardous Materials Occupancy 14110/7 12/5/4 22/5/4 27/5/4 25/2/4 12/5/4 22/5/4 27/5/4 (2)FB5114 FB2110 FB4034 (2)FB5040 Date: 10/20/2008 Time: I :57:43 PM Page: 107ofl75 Frame Desig11 Member Summary_-Controlli_!!g Load Case and Maximum Combined Stresses ocr Membet:_f_~ocatlons are from ,Joint 1 ) Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear Mom-x Mom-y Axial Shear Bnd-X Bnd-Y ---Stress /Force ---Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear 1 22.46 37.61 1 -54.5 -10.8 -2940.8 0.0 3.60 l.l8 18.93 0.00 25.11 3.88 26.10 41.25 0.85 0.30 2 1.61 47.39 2 -24.2 26.7 -3259.6 0.0 1.38 2.30 15.11 0.00 28.56 2.42 19.48 41.25 0.82 0.95 3 2.50 25.08 3 -13.9 2.9 2045.4 0.0 1.39 0.72 25.02 0.00 29.89 3.87 32.69 41.25 0.81 0.19 4 7.11 25.08 2 -13.8 -2.8 2055.1 0.0 1.39 0.70 25.14 0.00 29.89 3.87 32.69 41.25 0.81 0.18 5 0.00 24.00 2 -16.4 -7.5 1881.7 0.0 1.40 1.30 20.87 0.00 29.50 9.82 33.00 41.25 0.67 0.13 6 22.46 37.61 1 -54.4 10.8 -2905.4 0.0 3.59 l.l8 18.70 0.00 22.48 3.88 26.03 41.25 0.84 0.30 Mem. Loc. Depth Area Rx Ry Lx Ly-1 Ly-2 K1x K1y1 K1y2 Sx Lb1 Rt-1 Lb2 Rt-2 Qs Qa Cbl Cb2 No. ft in. in.2 in. in. in. in. in. !Rx !Ry /Ry in.3 in. in. in. in. 1 22.46 37.61 15.15 14.27 1.09 336.87 30.0 60.1 35.4 27.5 55.0 155.38 120.1 1.4 60.1 1.44 1.00 0.8 1.27 1.09 2 1.61 47.39 17.60 17.48 1.01 298.83 4.7 28.5 17.1 4.6 28.1 215.79 4.7 !.37 172.8 1.40 1.00 0.95 1.02 1.81 3 2.50 25.08 9.96 10.50 1.34 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 !.00 1.00 1.05 1.01 4 7.11 25.08 9.9~ 10.50 1.34 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 I.OC 1.00 1.01 1.05 5 0.00 24.00 11.75 9.60 1.24 298.83 36.0 0.0 3l.l 29.1 0.0 90.16 36.0 1.55 0.0 0.00 I.OC 1.0 1.0 0.0 6 22.46 37.61 15.15 14.27 1.09 336.87 60.1 60.1 35.4 55.0 55.0 155.38 120.1 1.4 60.1 1.44 1.00 0.86 1.26 1.09 File: 7079 Chevron R I_ Stress Check 10 _2008 with 08 _2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date; 10/20/2008 Time: I :57:43 PM Page: l08of 175 User Defined Frame Point Loads for Cross Section• 3 Side Units Tvoe Description Magi I k CG PS-41 Pipe Loads -1.70 I k CG PS~46 Pipe Loads -0.30 y X D eflectlon Loa dCo mbmations ~ F ramm No. Origin Factor DefH DefY Application I System 1.000 0 240 1.0 s 2 System 1.000 0 240 !.OUSI' 3 System 1.000 0 240 1.0 'US I 4 System 1.000 0 240 0.700Wl> 5 System 1.000 0 240 ~-700<Wl 6 System fuoo 0 240 0.700 W2> j' System 1.000 0 240 0.700<W2 8 System Derived 1.000 0 240 p.700WPAI 9 System Deri~ed 1.000 0 240 ~-700WPD1 10 System-Derived 1.000 0 240 0.700WPA2 II System Derived 1.000 0 240 0.700WPD2 12 System Derived 1.000 0 240 0.700 WPB! 13 System Derived 1.000 0 240 0.700WPC1 14 System Derived 1.000 0 240 0.700WPB2 15 System Derived 1.000 0 240 0.700WPC2 16 System 1.000 400 0 ~-700Wl> 17 System 1.000 400 0 0.700<Wl 18 System 1.000 400 0 0.700W2> 19 System 1.000 400 0 0.700<W2 20 System Derived 1.000 400 0 0.700WPAI 21 System Derived 1.000 400 0 0.700WPDI 22 System Derived 1.000 400 0 0.700WPA2 23 System Derived 1.000 400 0 0.700 WPD2 24 System Derived 1.000 400 0 0.700 WPBI 25 System Derived 1.000 400 0 0.700 WPCI 26 System Derived 1.000 400 0 0.700 WPB2 27 System Derived 1.000 400 0 0.700 WPC2 28 System 1.000 100 0 0.600 E> + 0.700 EG- 29 System 1.000 100 0 0.600 <E + 0.700 EG- 30 System Derived 1.000 100 0 0.600 EB> 31 System Derived 1.000 100 0 0.600 <EB 32 System 1.000 400 0 J.O<AL"' 33 Svstem 1.000 400 0 LO *AL> Controllin Frame Deflection Ratios for Cross Section: 3 Descri tlon Dellection in. Max. Horizontal Deflection -0.820 ax. Vertical Det1ection for Span -1.033 File; 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Locl 20/8/6 1617/3 ® Offset HorV Suoo. Dir. Coef. -2/3/0 Horiz. N DOWN 1.000 3/3/0 Horiz. N DOWN 1.000 Description s US I' c US! WI> <WI W2> <W2 WPA! WPDl WPA2 WPD2 WPBl :~I B2 WPC2 WI> <WI W2> <W2 WPAl WPD! WPA2 frPD2 WPBI WPCI WPB2 WPC2 E>+EG~ fE +EG-~B> fEB fAL' *AL> Load Case Descri tion Version: 7.1a <W2 s Loc. OF IF • 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 109ofl75 *Negative horizontal deflection is left * Negative vertical deflection is down Lateral deflections of primary frames are calculated on a bare frame basis and do not include resistance from systems such as roof and end wall di.aphragms. Therefore, these deflections may be considerably overstated . File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy FB y Dimension Key 1 5'·6" BL to CL of Runway Beam 2 I 5/8" 3 4'-0" 4 3'·5 !14" 5 2@5'·0" 6 2@2'·6" 7 3'-3 3/4" 8 1'-3" 9 1'-9 13/16" 10 2@ 2'-4 7116" II 4 J/2" 12 40'-\0" Ridge Ht. 0 X FRAME CROSS SECTION AT FRAME LINE(S) 4 File: 7079 Chevron R I_ Stress Check I 0 _2008 with 08 _ 2008 Loading Version: ?.Ia Date: 10/20/2008 FB 07-27053 Calculations Hazardous Materials Occupancy Frame Clearances Horiz. Clearance between members I(CXOOO) and 6(CXOOO): 45'-4.3/4" Vert. Clearance at member l(CXOOO): 28'-0 1/2" Vert. Clearance at member 6(CXOOO): 28'-0 112" Finished Floor Elevation= 100'-0" (Unless Noted Otherwise) Crane Clearances at bottom of RUnway Beam 0 Vert. Clearance at CRANE DATA 1-l(Left): 2'-4 3/16" Horz.ClearanceatCRANEDATA 1-l(Left): 1'-10 1/8" Vert. Clearance at CRANE DATA 1-l(Right): 2'-4 3/16" Horz. Clearance at CRANE DATA !-!(Right): 1'-10 l/8" 0 0 File: 7079 Chevron R !_Stress Check I 0 _2008 with 08 _2008 Loading 0 Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: Ill ofl75 0 Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: 1:57:43 PM Page: 112ofl75 Descri tion An Je Grou Trib. Override Desi Status 47/9/0 90.0000 Stress Check Desi n Load Combinations~ Framin No. Origin Factor Ann!ication DescriPtion I System 1.000 !.OD+ LOAD+ LOCG+ !.OS D+AD+CG+S 2 System LOOO l.OD+ 1.0 AD+ LOCG + l.O USI* D+AD+CG+USI* 3 System LOOO LO D + LO AD + LO CG + 1.0 'US I D +AD+ CG +*US! 4 System !.000 LO D +LOAD+ LO CG + 1.0 WI> D+AD+CG+Wl> 5 System LOOO LOD+ LOAD+ LOCG+ !.O<WI D+AD+CG+<Wl 6 System LOOO LO D + LO AD + LO CG + 1.0 W2> o-+ AD+ CG + W2> 7 System 1.000 LO D + LO AD+ LO CG + 1.0 <W2 D+AD+CG+<W2 8 System 1.000 LO D +LOAD+ LO CG +0.750 S +0.750 WI> D+ AD+CG +S+.Wl> 9 System !.000 LO D + !.0 AD+ LO CG +0.750 S + 0.750 <WI D+ AD +CG+S+<Wl 10 System 1.000 LO D +LOAD+ !.0 CG + 0.750 S +0.750 W2> D+AD+CG+S+W2> II System LOOO f.O D + !.0 AD+ !.0 CG +0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System !.000 l.OD+ l.OAD+ l.OCG + 1.0 *AL> D +AD + CG+* AL> 13 System 1.000 LO D + 1.0 AD+ !.OCG + 1.0 AL'> D+ AD+CG+AL*> 14 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <*AL D +AD+ CG+<*AL 15 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <AL* D +AD + CG+<AL * 16 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WI> D+AD+CU+WJ> 17 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<WI 18 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + !.0 W2> D+AD+CU+W2> 19 System 1.000 Q.600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 1.0 D+ LOAD+ LO CG +0.563 S +0.750 'AL> D+AD+CG+S+*AL> 21 System 1.000 LO D+ LOAD+ LOCG+0.563 S + 0.750 AL*> D+AD+CG+S+AL*> 22 System LOOO LO D+ LOAD+ LO CG +0.563 S +0.750 <*AL lo +AD+ CG + S+<*AL 23 System LOOO LO D + LOAD+ LO CG + 0.563 S + 0.750 <AL* /D +AD +CG + S+<AL' 24 System 1.000 1.0 D+ LOAD+ I.OCG +0.375 WI> +0.750 'AL> D+AD+CG+Wl>+*AL> 25 System LOOO 1.0 D + 1.0 AD+ LO 00 +0.375 W.l> +0.750 AL'> .J !o+AD+CG+Wl>+AL*> 26 System 1.000 1.0 D+ LOAD+ I.OCG +0.375 <WI +0.750 <'AL !o+AD+CG+<Wl+<*AL 27 System LOOO LO D+ 1.0 AD+ 1.0 CG+0.375 <WI +0.750 <AL' D+AD+CG+<Wl+<AL* •. 28 System LOOO LO D+ LOAD+ LO CG +0.375 W2>+0.750 *AL> D + AD + CG + W2>+* AL> 29 System 1.000 1.0 D+ 1.0 AD+ I.OCG+0.375 W2>+0.750 AL*> D+AD+CG+W2>+AL*> 30 System 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.375 <W2+0.750 <'AL D+AD+CG+<W2+<*AL 31 System LOOO 1.0 D+ LOAD+ 1.0 CG+0.375 <W2 +0.750<AL' D +AD +CG +<W2+<AL' 32 System 1.000 1.0 D+ 1.0 AD+ I.OCG+O.I50 S +0.750 E>+0.700 EG+ D+AD+CG+S+E>+EG+ 33 System 1.000 1.0 D+ 1.0 AD+ LO CG +0.150 S +0.750 <E+0.700 EG+ D+AD+CG+S+<E+EG+ 34 System 1.000 0.600 D +0.600 AD+ Q.600 CU + 0.700 E> + 0.700 EG-D+AD+CU+E>+EG- 35 System 1.000 .600 D +0.600 AD+ 0.600 CU + 0.700 <E +0.700 EG· D+AD+CU+<E+EG· 36 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG+0.150 S +0.750 EB>+0.700 EG+ D+AD+CG+s+EB>+EG+ 37 System Derived 1.000 .600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0.700 EG-D+AD+CU+EB>+EGw 38 System Derived 1.000 1.0 D+ 1.0 AD+ LO CG +0.150 S +0.750 <EB +0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived LOOO .600 D + 0.600 AD+ 0.600 CU + 0.700 <EB + 0.700 EG-\o +AD +CU +<EB + EG~ 40 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 1.0 WPAI D+AD+CG+WPAl 41 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPA I io+AD+CG+S+WPAl 42 System Derived 1.000 .600 D+0.600 AD +0.600 CU + 1.0 WPAI jo+AD+CU+WPAl 43 System Derived 1.000 1.0 D+ 1.0 AD+ l.O CO+ 0.375 WPAl +0.750 *AL +0.750 ALB> P+AD+CO+WPAl+*AL+ALB> 44 System Derived LOOO 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPAl +0.750 AL* +0.750 ALB> P+AD+CG+WPAl+AL*+ALB> 45 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 1.0 WPDI D+AD+CG+WPDI 46 System Derived 1.000 1.0 D + 1.0 AD+ LO CG + 0.750 S +0.750 WPDI D + AD+CG +S +WPDI 47 System Derived 1.000 0.600 D +0.600 AD +0.600 CU + LO WPDI D+AD+CU+WPDI 48 System Derived LOOO !.0 D+ l.O AD+ 1.0 CO +0.375 WPDI +0.750 *AL+0.750 <ALB D+AD+CG+WPD l +* AL +<ALB 49 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDI +0.750 AL' + 0.750 <ALB io+AD+CO+WPDl+AL *+<ALB so System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA2 p+AD+CG+WPA2 51 System Derived 1.000 1.0 D+ 1.0 AD+ LO CG + 0.750 S +0.750 WPA2 D +AD+CG +S + WPA2 52 System Derived 1.000 Q.600 D +0.600 AD+ 0.600 CU + 1.0 WPA2 D+AD+CU+WPA2 53 System Derived LOOO 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPA2 + 0.750 *AL +0.750 ALB> p+AD+CG+WPA2+* AL +ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG + 0.375 WPA2 + 0.750 AL"' +0.750 ALB> D+AD+CG+WPA2+AL *+ALB> 55 System Derived 1.000 LO D + LOAD+ 1.0 CG + 1.0 WPD2 b+ AD+ CG + WPD2 56 System Derived LOOO 1.0 D+ 1.0 AD+ 1.0 CG +0.750S +0.750 WPD2 D+AD+CG+S+WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D+ AD+ C'U + WPD2 58 System Derived LOOO 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPD2 + 0.750 *AL +0.750 <ALB b+AD+CG+WPD2+*AL+<ALB 59 System Derived 1.000 1.0 D + ! .0 AD+ 1.0 CG + 0.375 WPD2 + 0.750 AL"' + 0.750 <ALB D+AD+CG+WPD2+AL *+<ALB File: 7079 Chevron ~!_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 113 of 175 60 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPBl 61 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPBJ 62 System Derived 1.000 .600 D+0.600 AD +0.600 CU + 1.0 WPBl 63 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPBJ +0.750 *AL + 0.750 ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPBl +0.750 AL* + 0.750 ALB> 65 System Derived 1.000 LOD+ LOAD+ l.OCG+ l.OWPCJ 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPCJ 67 System Derived 1.000 0.600 D+0.600 AD +0.600 CU + 1.0 WPCl 68 System Derived 1.000 l.O D + !.0 AD+ 1.0 CG + 0.375 WPCl +0.750 *AL + 0.750 <ALB 69 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPCI + 0.750 AL* + 0.750 <ALB 70 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPB2 71 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 73 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG+ 0.375 WPBZ+ 0.750 'AL + 0.750 ALB> 74 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 + 0.750 AL' + 0.750 ALB> 75 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPC2 76 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 78 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG+0.375 WPC2+0.750 'AL+ 0.750 <ALB 79 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPC2 +0.750 AL' + 0.750 <ALB 80 System Derived 1.000 1.0 D + l.O AD + 1.0 CG + 1.0 S + 1.0 ALB> 81 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG+ 1.0 'AL + 1.0 ALB> 82 System Derived 1.000 l.O D + l.O AD + 1.0 CG + 1.0 AL * + 1.0 ALB> 83 System Derived 1.000 1.0 D +.1.0 AD+ 1.0 CG +0.563 S +0.750 'AL+0.750 ALB> 84 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL' + 0.750 ALB> 85 System Derived 1.000 l.OD+ LOAD+ LOCG+ LOS+ l.O<ALB 86 System Derived 1.000 1.0 D + l.O AD+ 1.0 CG + l.O * AL + 1.0 <ALB 87 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 AL"' + 1.0 <ALB 88 System Derived 1.000 1.0 D+l.O AD+ 1.0 CG+0.563 S+0.750 *AL+0.750 <ALB 89 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S+0.750 AL' +0.750 <ALB Frame Member Sizes Mem. Fig Width Flg Thk WebThk Depth I Depth2 Length w~t' Flg,i{ No. (in.) (in.) (in.) (in.) <in.) (ftl (ksi 1 6.00 0.5000 0.2500 12.00 44.00 31.03 1276.1 55.00 2 6.00 0.5000 0.2500 48.00 24.00 17.79 974. 55.00 3 6.00 0.5000 0.1644 24.00 28.00 10.00 343.6 55.00 4 6.00 0.5000 0.1644 28.00 24.00 10.00 343.5 55.00 5 6.00 0.5000 0.2500 24.00 48.00 17.79 974.2 55.00 6 6.00 0.5000 0.2500 12.00 44.00 31.03 1272.7 55.00 Total Frame Wetght = 5184.4 (p) Frame Pricing Weight= 5725.8 (p) Values shown are resisting forces of the foundation. R · U f dL d F C S . 4 eactions-n actore •• Tvne at rame ross ectwn: Type Exterior Column Exterior Column X·Loc 0/0/0 531010 Grid I • Grid2 4-D 4-A Base Plate W x L (in.) 8 X 13 8 X 13 Base Plate Thickness (in.) 0.500 0.375 Anchor Rod Qty/Diam. (in.) 4-0.750 4-0.750 Column Base Elev. 100'-Q" 100'-0" Load Type Desc. Hx Hz Vv Hx Hz Vy D Fnn 0.8 -4.3 -0.8 4.3 AD Fnn 0.1 -1.1 -0.1 1.1 - CG Frm 2.6 -12.3 -2.6 10.1 s Frm 9.8 -38.3 -9.8 -38.3 US!* Fnn 8.8 -22.7 -8.8 46.2 "'USJ Fnn 8.8 -46.2 -8.8 -22.7 WI> Fnn -6.9 --11.9 -4.6 -4.3 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading D+AD+CG+WPBl D+AD+CG+S+WPBI D+AD+CU+WPBl /D+AD+CG+WPB!+*AL+ALB> D+AD+CG+WPB l+AL *+ALB> D+AD+CG+WPCl D+AD+CG+S+WPCl D+AD+CU+WPCl D+AD+CG+WPCJ+*AL+<ALB D+AD+CG+WPC !+AL *+<ALB D+AD+CG+WPB2 D+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+AL *+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2 D+AD+CU+WPC2 D+AD+CG+WPC2+*AL+<ALB jo+AD+CG+WPC2+AL *+<ALB D+AD+CG+S+ALB> lr> +AD + CG+* AL +ALB> lo +AD+ CG+AL*+ALB> ~AD+cG+S+*AL+ALB> D+AD+CG+S+AL *+ALB> D +AD + CG + S+<ALB D+AD+CG+*AL+<ALB !D+AD+CG+AL*+<ALB D+AD+CG+S+* AL+<ALB D+AD+CG+S+AL "'+<ALB 0 WebFy Splice Codes Shape (ksi). Jt.l 55.00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP (Includes all plates) (Includes aU pieces) 0/0/0 01010 - - - Version: 7.1a Jt.2 KN ss SP ss KN KN 0.0000 0.0000 - - - - - 3P 3P 3P 3P 3P 3P 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: l :57:43 PM Page: 114 of 175 <WI Fnn 4.6 -4.3 6.9 ·11.9 " " W2> Fnn -8.3 -8.1 ·3.2 -0.4 " <W2 Fnn 3.2 " -0.4 8.3 " -8.1 " 'AL> Fnn -0.1 10.0 -1.8 " 4.7 " " AL*> Fnn -0.1 2.7 -!.8 " 12.0 " <*AL Fnn 1.8 " 12.0 0.1 " 2.7 " " " <AL* Fnn !.8 " 4.7 0.1 " 10.0 " " cu Fnn 1.3 " 5.1 . -1.3 5.1 E> Fnn -4.2 " -5.5 -4.1 " 5.5 " " EG+ Frm 0.3 " 1.5 . -0.3 " l.3 " <E Fnn 4.2 " 5.5 4.1 " -5.5 " " " EG-Frm -0.3 -1.5 0.3 " -1.3 " " " EB> Brc -0.3 " 32.3 0.3 " 32.4 " <EB Brc . 0.4 16.2 -29.0 -0.4 16.3 ·29.0 " " " WPAl Brc !.9 " -2.9 -1.4 " -3.2 " 'AL Fnn 0.9 " ll.O -0.9 " 3.7 " " ALB> Brc " " " " " " " " AL' Fnn 0.9 " 3.7 -0.9 " ll.O " " " WPDl Brc 2.6 3.7 -14.2 -2.3 3.2 -13.0 " " " <ALB Brc " " " " " " " " " WPA2 Brc 0.5 " 0.9 -0.0 " 0.6 " " " WPD2 Brc 1.2 3.7 -10.4 -0.9 3.2 -9.2 " " " WPBl Brc 1.4 " -3.2 -!.9 " -2,9 " " " WPCl Bro 2.3 3.2 -13.0 -2.6 3.7 ·14.2 " " " WPB2 Bro 0.0 " 0.6 .0.5 " 0.9 " " WPC2 Brc 0.9 3.2 -9.2 -1.2 3.7 -10.3 " " " d Maximum Combined Reactions Summary w1th Factored Loa s-Framing X-Loc Grid Hrz left Load Htz Right Load Hrzln Load HrzOut Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-Hx) Case (Hx) Case (-Hz) Ca'se (Hz) Case (-Vy) Case (Vy) Case (·Mzz) Case (Mzz) CaSe .(k) (k) (k) M (ki <kl (in-k) iin-k) 0/0/0 4-D 7.0 18 14.3 9 " " 12.2 38 15.! 39 63.9 3 " " " " 53/0/0 4-A 14.3 8 7.0 19 " " 12.2 38 14.9 39 61.8 2 " " " " Sum of Forces with Reactions Check -Framing Horizontal Vertical · Load Type Load Reaction Load Reaction (k) (k) (k) (k) D 0.0 0.0 8.8 8.7 AD 0.0 0.0 2.3 2.2 CG 0.0 0.0 22.4 22.4 s 0.0 0.0 76.5 76.5 USl* 0.0 0.0 68.9 68.9 "'USl 0.0 0.0 68.9 68.9 Wl> 11.5 1!.5 16.2 16.2 <WI 11.5 ll.S 16.2 16.2 W2> ll.S 11.5 8.6 8.6 <W2 11.5 ll.5 8.6 8.6 'AL> 1.9 1.9 15.5 14.7 AL*> 1.9 1.9 15.5 14.7 <•AL 1.9 1.9 15.5 14.7 <AL* 1.9 !.9 15.5 14.7 cu 0.0 0.0 10.2 10.2 E> 8.3 8.3 0.0 0.0 EG+ 0.0 0.0 2.9 2.9 <E 8.3 8.3 0.0 0.0 EG-0.0 0.0 2.9 2.9 EB> 0.0 0.0 0.0 64.7 <EB 0.0 0.0 0.0 58.0 WPAJ 0.5 0.5 19.9 6.2 'AL 00 0.0 15.5 14.7 ALB> 0.0 0.0 00 0.0 AL' 0.0 0.0 15.5 14.7 WPDl 0.3 0.3 14.8 27.2 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1 a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: l!5of!75 WPA2 0.5 0.5 12.3 1.4 WPD2 0.3 0.3 7.2 19.5 WPBI 0.5 0.5 19.9 6.2 WPCI 0.3 0.3 14.8 27.2 WPB2 0.5 0.5 12.3 1.5 WPC2 0.3 0.3 7.2 19.5 Base Plate Summary X-Loc Grid Mem. Thickness Width Length Num.Of BoltDiam. Type Welds to Welds to No. (in.) (in.) (in.) Bolts (in.) Flange Web 0/0/0 4-D I 0.500 8 13 4 0.750 A36 OS-0.1875 OS-0.1875 53/0/0 4-A 6 0.375 8 13 4 0.750 A36 OS-0.1875 08-0.1875 w 8 eb tiffener Summar Mem. Stiff. Desc. Loc. Web Depth hit alb a Thick. ~idth Side Welding No. No. -(ft) (in.)-(in) (in)_ n.) Description 2 I 89 3.85 45.069 180.27 NIA N/A 0.5000 2.500 Both W-OS-0.1875 2 2 81 13.17 30.308 121.23 3.00 90.78 0.2500 2.000 Both 8td 5 0. 1 89 13.94 45.069 180.27 NIA N/A 0.5000 2.500 Both W-08-0.1875 5 2 81 12.29 42.460 169.84 3.00 127.00 0.2500 2.000 Both F-08-0.1875,W-OS-0.1875 Brackets Part Summary Mem. Loc. Total Length Bracket Cut Bracket Fig Width FlgThk WebThk Hole Pitch Stiffener or Plate Part No. (ft) (in.) (in.) Depth (in.l -(in.) (in.) (in.) (in.) 2 3.99 15.500 4.750 10.000 6.000 0.2500 0.2500 3.500 UP070411000 WU15441234 5 13.85 13.375 4.250 10.000 6.000 0.2500 0.2500 3.500 UP070411000 WU\3340434 Brackets Design Summary (vertical live load Is with the impact factor Mem. Loc. Vert. Live Vert. Dead Lateral Longitudinal CL Dist to Member Member WebThk Fig Thk Fig Width No. (ft) Load(k) Load(k) Impact(k) Impact (k) Flange (in.} Depth I (in,) Depth2 (in,) (in.) {in.) -(in.) 2 3.99 13.72 !.15 0.94 1.47 11.741 43.403 41.012 0.2500 0.5000 6.0000 5 13.85 13.72 !.15 0.94 1.47 0 11.741 42.012 42.401) 0.2500 0.5000 6.0000 Bolted End-Plate Moment Connection~ (AISC DG~l_6)~ I!)= SS ksl . End~Plate Dimensions Bolt Outside Flange Inside Flange Mem. lt. Type Thick. Width Length Diam. Spec/Joint Gages In/Out ConfigUration Pitches 1st/2nd Configuration Pitches tst12nd No. No. Cin.) lin.) (i,;:) lin.) lin.) ID Desc. On. ID Desc. lin.}_ I 2 KN(Top) 0.625 6.00 45.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 2 1 KN(Top) 0.625 6.00 45.00 0.750 A325X/8T 3.50 12 Flush 2.00 II Flush 2.00 3 2 8P 0.375 6.00 33.00 0.750 A325X/8T 3.00 II Flush 0.00 42 Ext/Gusset 3.69/2.00 4 I 1 I 3.00 Ill I Flush o.oo I 42 I Ext/Gusset I 3.69/2.00 Required Strength ~ Out Available Strength~ Out Required Stren,gth -In Available Stren_g:h-In Mem. lt. Ld Axial Shear Moment Design Shear Moment Ld Axial Shear Moment Design Shear Moment No. No. Cs (k) (k) (in-k) Proc. (k) (in-k) Cs lk) (k) (in-k) Proc. (k) lin-k) I 2 2 -38.9 10.5 3585.5 Thin plate 159.0 2814.0 16 5.7 !.4 1126.2 Thick plate 106.0 1660.0 2 I 2 -38.9 10.5 3585.5 Thin plate 159.0 2814. 16 5.7 1.4 1126.2 Thick plate 106.0 1660.0 3 2 17 3.1 3.6 17.6 Thin plate 106.0 574.5 I -13.0 3.3 1698.7 Thin plate 212.1 1547.4 4 I 17 3.1 3.6 17.6 Thin plate 106.0 574.5 I -13.0 3.3 1698.7 Thin plate 212.1 1547.4 5 2 3 -38.8 10.5 3550.5 Thin plate 159.0 2814.0 17 5.7 1.4 1126.2 Thick plate 106.( 1660.0 6 2 3 -38.8 10.5 3550.5 Thin plate 159.0 2814.0 17 5.7 1.4 1126.2 Thick plate 106.0 1660.0 Flanee Brace Summary Member From Member Joint I From Side Point I Part Design Note I 12/5/4 12/5/4 FB2JIO I 2215/4 22/5/4 8FB4034 I 27/5/4 27/5/4 (2)FB5040 2 2/11/1 25/2/4 (2)FB5114 3 2/6/0 7/9/13 FB3030 3 8/610 1/9113 FB3050 4 11610 1/9113 FB3050 5 61610 16/9113 FB4060 File: 7079 Chevron R !_Stress Check I 0 _ 2008 with 08 _ 2008 Loading Version: 7.\a 5 6 6 6 07-27053 Calculations Hatardous Materials Occupancy 14/10/7 12/5/4 22/5/4 27/5/4 25/2/4 12/5/4 22/5/4 27/5/4 (2)FB5114 FB21!0 FB4034 f2lFB5040 Date: 10/20/2008 Time: l :57:43 PM Page: 116ofl75 Frame Design Member Summary~ ContrOlling Load Case and Maximum Combined Stresses per Member ___ {Locations are from Joint 1 ) Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear Mom-x Mom-y Axial Shear Bnd-X Bnd-Y ---Stress /Force ---Sum% % No, ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear I 22.46 37.61 I -54.5 -10.8 -2940.8 0.0 3.60 LIS 18.93 0.00 25.11 3.88 26.10 41.25 0.85 0.30 2 1.61 47.39 2 -24.2 26.7 -3259.6 0.0 1.38 2.30 15,11 0.00 28.56 2.4L 19.4 41.2 0.82 0.95 3 2.50 25,08 3 -13.9 2,1 2045.4 0.0 L3 0,72 25,02 0.00 29.89 3.87 32.69 41.25 0.81 0.19 4 7.11 25,08 2 -13.8 -2.8 2055.1 0.0 1.39 0.70 25.14 0.00 29.89 3.87 32.69 41.25 0.81 0.18 5 0.00 24.00 2 -16.4 -7.5 1881.7 0.0 1.40 1.30 20.87 0.00 29,50 9.82 33.00 41.2 0.67 0.13 6 22.46 37.61 I -54.4 10.8 -2905.4 0.0 3.59 LIS 18.70 0.00 22.48 3,88 26,03 41.25 0.84 0.30 Mem. Lac. Depth Area Rx Ry Lx Ly-1 Ly-2 Klx Klyl Kly2 Sx Lbl Rt-1 Lb2 Rt-2 Qs Qa Cbl Cb2 No. ft in. in.2 in. in. in. in. in. !Rx fRy fRy in.3 in. in. in. in. I 22.4~ 37.61 15,15 14,27 1.09 336,87 30.0 60.1 35.4 27.5 55.0 155.38 120.1 1.46 60.1 1.44 LOO 0,86 1.27 1.09 2 1.61 47.3 17.60 17.48 LOI 298.83 4,7 28.5 17.1 4,6 28.1 215.79 4.7 1.37 172.8 1.40 LOO 0.95 1.02 1.81 3 2.50 25.08 9.96 10.50 L3 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 LOO LOO 1.05 LOI 4 7,11 25,08 9.9 10,5( 1.34 298.83 36.0 36.0 28.5 26.8 26,8 81.76 36.0 1.61 36,0 1.61 1.00 LOO LOI LOS s 0.00 24.00 I 1.75 9,60 L24 298.83 36.0 0.0 3Ll 29.1 0.0 90.16 36.0 1.55 0,0 0.00 LOO LOO LOS 0.00 6 22.4 37.61 15.15 14.27 1.09 336,87 60.1 60.1 35, 55,0 55.0 155.38 120,1 1.46 60.1 1.44 LOO 0.86 1.26 1.09 0 0 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.Ia 0 07.:27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: l :57:43 PM Page: 117 of 175 User Defined Frame Point Loads f Cr ss Sect' on· 4 or 0 I Side Units Type Description Mag! Loci Offset HorV Supp, Dir. Coef. Loc. I k co PS-41 Pipe Loads -1.7.0 20/8/6 ~2/3/0 Horiz. N DOWN 1.000 OF I k co PS-46 Pipe Loads -0.30 !6/7/3 3/3/0 Horiz. N DOWN !.000 IF y 0 X Deflection Load Combinations-Framin No. Origin Factor DefH DefV Aoolication Descrintion I System 1.000 0 240 1.0 s s 2 System 1.000 0 240 l.OUSl* USl* 3 System !.000 0 240 1.0 'US! *USl 4 System 1.000 0 240 0.70lbWI> WI> 5 System 1.000 0 240 0.700 <WI ~I 6 System 1.000 0 240 .700 W2> jW2> 7 System 1.000 0 240 .700<W2 kw2 8 System Derived !.000 1> 240 0.700WPAI ' WPA! 9 System Derived 1.000 0 240 .700WPDI WPD! 10 System Derived 1.000 0 240 0.700WPA2 WPA2 II System Derived . 1.000 0 240 0.700WPD2 WPD2 12 System Derived 1.000 0 240 0.700WPBI WPBI 13 System Derived 1.000 0 240 0.700WPCI WPCI 14 System Derived !.000 0 240 0.700 WPB2 ~~2 IS System Derived 1.000 0 240 0.700WPC2 C2 16 System 1.000 400 0 fJ.700Wl> WI> 17 System 1.000 400 0 . p.700<Wl ~WI 18 System 1.000 400 0 r.1oow2> W2> 19 System 1.000 400 0 0.700<W2 W2 20 System Derived 1.000 400 0 0.700 WPAI WPA! 21 System Derived 1.000 400 0 0.700WPDI WPDI 22 System Derived 1.000 400 0 0.700WPA2 WPA2 23 System Derived 1.000 400 0 0.700 WPD2 WPD2 24 System Derived 1.000 400 0 0.700WPBI WPBI 25 System Derived 1.000 400 0 0.700WPCI WPCI 26 System Derived 1.000 400 0 0.700 WPB2 WPB2 27 System Derived 1.000 400 0 0.700 WPC2 WPC2 28 System 1.000 100 0 0.600 E> + 0.700 EO· E> + EG- 29 System 1.000 100 0 0.600 <E + 0.700 EO· E+EG- 30 System Derived 1.000 100 0 Q.600 EB> EB> 31 System Derived 1.000 100 0 0.600 <EB <EB 32 System 1.000 400 0 l.O<AL* <AL* 33 ~ystem 1.000 400 0 1.0 *AL> 'AL> Controllut_g_Frame DO e ection Ratios for Cross Section: 4 I Description Ratio Deflection in. Member Joint Load Case Load Case Descliotion ~:x· Horizontal Det1ection ( H/431) -0.819 6 2 19 <W2 ax. Vertical Deflection for Span 1 ( L/568) • !.033 3 2 I s File: 7079 Chevron R I_ Stress Check l 0 _ 2008 with 08 _ 2008 Loading Version: 7.1a " 07-27053 Calculations Hazardous Materials Occupancy *Negative horizontal deflection is left *Negative vertical deflection is down Date: 10/20/2008 Time: I :57:43 PM Page: 118 of 175 Lateral deflections of primary frames are calculated on a bare frame basis and do not include resistance from systems such as roof and end wall diaphragms. Therefore, these deflections may be considerably overstated. 0 0 0 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: 1:57:43 PM FS y Dimension Key I 5'~6" BL to CL of Runway Beam 2 1 5/8" 3 4'~0" 4 3'~5 1/4" 5 2@5'-0" 6 2@ 2'-6" 7 3'-3 3/4" 8 l'-3" 9 1'-9 13/16" 10 2@ 2'·4 7/16" 11 4 1/2" 12 40'-lO"RidgeHt. ) X FRAME CROSS SECTION AT FRAME LJNE(S) 5 File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Page: 119 of 175 0 07-27053 Calculations Hazardous Materials Occupancy Frame Clearances Horiz. Clearance between members l(CXOOO) and 6(CXOOO): 45'-4 3/4" Vert. Clearance at member l(CXOOO): 28'-0 1/2" Vert. Clearance at member 6(CXOOO): 28'-0 112'' Finished Floor Elevation"" 100'-0" (Unless Noted Otherwise) Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA l-1 (Left): 2'-4 3/16" Horz.ClearanceatCRANEDATA 1-I(Left): l'-10 118" Vert. Clearance at CRANE DATA l-l(Right): 2'-4 3/16" Horz. Clearance at CRANE DATA 1-l(Right): 1'-10 1/8" File: 7079 Chevron Ri_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20(2008 Time: l :57:43 PM Page: 120 of 175 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20(2008 Time: I :57:43 PM Page: 121 of 175 Descri tion An le Grou Trib. Override Desi n Status 671910 Ri id Frame 90.0000 Stress Check Desie:n Load Combinations ~ Framin No. Origin Factor Application Descriotion [ System LOOO LO D+ LOAD+ LOCG+ LOS D+AD+CG+S 2 System LOOO LO D +LOAD+ LO CG + LO US!' D+AD+CG+USI"' 3 System LOOO LO D+ 1.0 AD+ l.OCG + 1.0 "'US! D +AD +CG +*US! 4 System LOOO LO D +LOAD+ LO CG + l.O WI> ~+AD+CG+WI> 5 System LOOO LO D + 1.0 AD+ LO CG + l.O <WI D+AD+CG+<Wi 6 System LOOO LO D + 1.0 AD + l.O CG + l.O W2> D+AD+CG+W2> 7 System LOOO 1.0 D + 1.0 AD + 1.0 CG + 1.0 <W2 D+AD+CG+<W2 8 System LOOO LO D +LOAD+ l.O CG + 0.750 S + 0.750 WI> D+AD+CG+S+Wl> 9 System LOOO LO D+ l.O AD+ l.O CG +0.750 S +0.750 <WI D+AD+CG+S+<Wl lO System LOOO 1.0 D + 1.0 AD+ LO CG + 0.750 S +0.750 W2> ln+AD+CG+S.+W2> II System LOOO LO D + 1.0 AD+ 1.0 CG +0.750 S +0.750 <W2 D+AD+CG+S+<W2 12 System LOOO 1.0 D + 1.0 AD+ l.O.CG+ 1.0 *AL> D +AD+ CG+*AL> [J System 1.000 1.0 D + l.O AD+ 1.0 CG+ 1.0 AL*> jo+AD+CG+AL"'> 14 System !.000 1.0 D + 1.0 AD+ l.OCG + 1.0 <*AL ~+AD +CG+<*AL 15 System 1.000 l.O D+ 1.0 AD+ 1.0CG + l.O<AL* D +AD +CG+<AL* 16 System !.000 ~.600 D + 0.600 AD+ 0.600 CU + 1.0 WI> P+AD+CU+Wt> 17 System 1.000 Q.600 D + 0.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<Wl 18 System 1.000 ~.600 D + 0.600 AD+ 0.600 CU + 1.0 W2> D+AD+CU+W2> 19 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 'AL> D+AD+CG+S+*Al> 21 System [.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL'> D +AD+ CG + S+AL*> 22 System !.000 1.0 D + !.0 AD+ 1.0 CG +0.563 S + 0.750 <*AL D+AD+CG+S+<*AL 23 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 <AL' D+AD+CG+S+<AL* 24 System 1.000 1.0 D + l.O AD+ 1.0 CG + 0.375 WI>+ 0.750 'AL> D +AD+CG+Wl>+'AL> 25 System 1.000 1.0 D + 1.0 AD+ !.OCG +0.375 Wl>+0.750 AL'> io +AD+CG+Wl>+AL*> 26 System !.000 1.0 D + I.liAD + !.0 CG+O.J75 <WI+ 0.750 <'AL P:>+AD+CG+<WI~L 27 System 1.000 1.0 D +leO AD+ l.OCG +0.375 <WI +0.750 <RL• ~ +AD+CG+<Wt+<AL* 28 System 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.375 W2>+ 0.750 'AL> io +AD + CG + W2>+*AI> 29 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 W2> + 0.750 AL'> to+ AD+ CG + W2>+AL*> 30 System 1.000 1.0 D + !.OAD+ 1.0 CG +0.375 <W2+0.750 <'AL P+AD+CG+<W2+<*AL 31 System 1.000 1.0 D+ 1.0 AD+ l.OCG +0.375 <W2 +0.750<AL* io +AD + CG + <W2+<AL"' 32 System 1.000 1.0 D+ 1.0 AD+ I.OCG+0.150 S +0.750 E>+0.700 EG+ P,.AD+CG+S+E>+EG+ 33 System 1.000 1.0 D + 1.0 AD+ !.OCG +0.150 S +0.750 <E+0.700 EG+ p.tAD+CG+S+<E+EG+ 34 System 1.000 P.600 D +0.600 AD+ 0.600 cu + 0.700 E> + 0.700 EG-~+AD+CU+E>+EG~ 35 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-D+AD+CU+<E+EG- 36 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG +0.!50 S+0.750 EB> +0.700EG+ P+AD+CG+S+EB>+EG+ 37 System Derived LOOO 0.600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0.700 EG-IO+AD+CU+EB>+EG~ 38 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.150 S + 0.750 <EB + 0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived LOOO 0.600 D + 0.600 AD+ 0.600 CU + 0.700 <EB + 0.700 EG-lo +AD+ CU +<EB + EG~ 40 System Derived [.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPAl ~+AD+CG+WPAl 41 System Derived [.000 1.0 D + 1.0 AD+ l.OCG +0.750 S + 0.750 WPAI D +AD+ CG + s + WPAl 42 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPAI D+AD+CU+WPAI 43 System Derived 1.000 1.0 D + 1.0 AD+ l.OCG +0.375 WPAl + 0.750 *AL +0.750 ALB> D+AD+CG+WPAl+*AL+ALB> 44 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPAl + 0.750 AL* + 0.750 ALB> D+AD+CG+WPAI+AL*+ALB> 45 System Derived 1.000 !.0 D + 1.0 AD+ 1.0 CG + 1.0 WPDl D+AD+CG+WPDI 46 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPD! D +AD+ CG + S + WPDI 47 System Derived LOOO 0.600 D + 0.600 AD+0.600 CU + 1.0 WPDl D+AD+CU+WPDl 48 System Derived LOOO 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDl + 0.750 *AL + 0.750 <ALB b+AD+CG+WPD I+* AL +<ALB 49 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.375 WPD\ + 0.750 AL* +0.750 <ALB D+AD+CG+WPDl+AL*+<ALB 50 System Derived LOOO 1.0 D + 1.0 AD+ 1.0 CG + l.O WPA2 D+AD+CG+WPA2 51 System Derived LOOO 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPA2 D+AD+CG+S+WPA2 52 System Derived [.000 0.600 D+0.600 AD+ 0.600 CU + LO WPA2 D +AD+ CU + WPA2 53 System Derived !.000 1.0 D + \.0 AD+ 1.0 CO+ 0.375 WPA2 + 0.750 *AL +0.750 ALB> D+AD+CG+WPA2+*AL+ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPA2 + 0.750 AL"' + 0.750 ALB> D+AD+CG+WPA2+AL *+ALB> 55 System Derived LOOO LO D + 1.0 AD + LO CG + 1.0 WPD2 D+AD+CG+WPD2 56 System Derived LOOO LO D +LOAD+ LO CG + 0.750 S + 0.750 WPD2 D + AD+CO +S + WPD2 57 System Derived LOOO 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived [.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPD2 + 0.750 *AL +0.750 <ALB D+AD+CG+WPD2+* A L +<ALB 59 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPD2 + 0.750 AL* + 0.750 <ALB D+AD+CG+WPD2+AL *+<ALB File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 0 Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Time: l :57:43 PM 60 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CO + l.O WPB 1 61 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPB J 62 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPBJ 63 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPBI + 0.750 *AL +0.750 ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPBJ + 0.750 AL* + 0.750 ALB> 65 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPCI 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 WPCJ 67 System Derived 1.000 0.600 D +0.600 AD +0.600 CU + 1.0 WPCJ 68 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPCI + 0.750 *AL +0.750 <ALB 69 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPCI + 0.750 AL* + 0.750 <ALB 70 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPB2 1! System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPB2 72 System Derived 1.000 ~.600 D + 0.600 AD+ 0.600 CU + 1.0. WPB2 73 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 +0.750 'AL+ 0.750 ALB> 74 System Derived 1.000 1.0 D + !.0 AD+ 1.0 CG +0.375 WPB2 + 0.750 AL* +0.750 ALB> 75 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPC2 76 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 78 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPC2 + 0.750 *AL +0.750 <ALB 79 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPC2 + 0.750 AL' +0.750 <ALB 80 System Derived 1.000 1.0 D + 1.0 AD + !.0 CG + 1.0 S + 1.0 ALB> 81 System Derived !.000 1.0 D+ 1.0 AD+ 1.0 CG+ 1.0 •AL+ 1.0 ALB> 82 System Derived 1 · 1.ooo 1.0 D + 1.0 AD+ 1.0 CG + 1.0 AL * + l.O ALB> 83 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG+0.563 S +0.750 'AL+ 0.750 ALB> 84 System Derived !.000 !.0 D+ 1.0 AD+ 1.0 CG +0.563 S +0.750 AL' +0.750 ALB> 85 System Derived !.000 !.0 D + 1.0 AD+ 1.0 CG + 1.0 S + 1.0 <ALB 86 System Derived !.000 !.0 D + !.0 AD + 1.0 CG + 1.0 'AL + 1.0 <ALB 87 System Derived !.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 AL"' + 1.0 <ALB 88 SYstem Derived !.000 1.0 D + 1.0 AD+ !.0 CG +0.563 8+0.750 *AL +0.750 <ALB 89 Svstem Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG+O.S63 8+0.750 AL' +0.750 <ALB F M b Sf rame em er zes Mem. FlgWidlh Fig Thk WebThk Depth! Depth2 Length Weight FlgFy No. -(in.) iin.) (in.) (i~.) (in.) oi) (p) (l(s;) I 6.00 0.5000 0.2500 12.00 44.00 31.03 1278.0 55.00 2 6.00 0.5000 0.2500 48.00 24.00 17.79 974.2 55.00 3 6.00 0.5000 0.1644 24.00 28.00 10'110 343.6 55.00 4 6.00 0.5000 0.1644 28.00 24.00 10.00 343.5 55.00 5 6.00 0.5000 0.2500 24.00 48.00 17.79 974.2 55.00 6 6.00 0.5000 0.2500 12.00 44.00 3!.03 1278.0 55.00 Tota!FrameWetght=519!.5 (p) Frame Pricing Weight =5712.5 (p) B d C dT S oun arv · on t ton umma Member X-Loc Y-Loc Supp.X Supp. Y Moment Displacement X(in.) J 01010 01010 Yes Yes No 0/0/0 6 53/0/0 010/0 Yes Yes No 0/0/0 2 5/6/0 33110/0 Yes Yes Yes 010/0 5 47/6/0 33/10/0 Yes Yes Yes 01010 Values shown are resisting forces of the foundation. R . U f dL dT F C S 5 eacttons-n actore oa 1 voe at rame ross echon: Type Exterior ColUmn Exterior Column X~Loc 0/010 53/0/0 Grid I -Grid2 5-D 5-A Base Plate W x L (in.) 9x 13 9x. 13 Base Plate Thickness (in.) 0.500 0.500 Anchor Rod Qty/Diam. (in.) 4-1.000 4-1.000 Column Base Elev. 100'-0" 100'-0" Load 'l'Y2.~ Desc. Hx Vv Hx Vv D Frm 0.8 4.3 -0.8 4.) - AD Frm 0.1 !.1 ·0.1 l.J - CG Frm 2.6 15.2 -2.6 10.2 s Frm 9.8 38.3 ·9.8 38.3 - US!* Fnn 8.8 22.7 ·8.8 46.2 *USl Frm 8.8 46.2 -8.8 22.7 WI> Frm -6.9 -1 1.9 -4.6 -4.3 File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading Page: l22ofl75 D+AD+CG+WPBl D +AD+ CG + S + WPBI D+AD+CU+WPB! D+AD+CG+WPHI+*AL+ALB> D+AD+CG+WPBl +AL *+ALB> D+AD+CG+WPC! D+ AD +CG+S +WPCJ D+AD+CU+WPCI D+AD+CG+WPCl+*AL+<ALB D+AD+CG+WPCI +AL *+<ALB D+AD+CG+WPB2 D+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+A L *+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2 D+AD+CU+WPC2 D+AD+CG+WPC2+* AL +<ALB D+AD+CG+WPC2+AL *+<ALB D+AD+CG +S+ALB> ID+AD+CG+•AL+ALB> ~+AD+CG+AL*+ALB> D+AD+CG+S+*AL+ALB> P.AD+CG+S+AL'+ALB> D + AD+CG +S+<ALB D +AD + CG+* AL+<ALB fo + AD + CG+AL *+<ALB P+AD+CG+s+•AL+<ALB D+AD+CG+S+AL *+<ALB WebFy Splice (ksi) · Jt.l 55.00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP (Includes all plates) (Includes all pieces) Codes Jt.2 KN ss SP ss KN KN Shape 3P 3P 3P 3P 3P 3P Displacement Y(in.) Displacement ZZ(rad.) 01010 0.0000 01010 0.0000 0/010 0.0000 01010 0.0000 - -- Version: 7.la . , 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 123of!75 <WI Frm 4.6 -4.3 6.9 .l!.9 . . W2> Frm ·8.3 -8.1 -3.2 ·0.4 <W2 Fnn ).2 -0.4 8.3 ·8.1 *AL> Fnn -0.1 10.0 -1.8 4.7 . AL*> Frm -0.1 2.7 -1.8 12.0 <*AL Frm !.8 12.0 0.1 2.7 . <AL* Frm 1.8 4.7 0.1 10.0 cu Fnn 1.3 5.1 -!.3 5.1 . E> Frm -4.6 ·5.6 -4.2 5.6 . EO+ Frm 0.3 1.8 -0.3 1.4 . <E Fnn 4.6 5.6 4.2 ·5.6 . EO-Fnn -0.3 -!.8 0.3 ·1.4 . . EB> Brc . . . . -- <EB Brc --. -- WPA1 Brc 2.0 -!0.0 -!.6 -9.4 - 'AL Fnn 0.9 1!.0 -0.9 3.7 -- ALB> Bee --- AL' Fnn 0.9 3.7 -0.9 1!.0 - WPDI Brc 2.4 -7.9 -2.1 -7.5 - <ALB Brc ---- -- WPA2 Bee 0.7 -6.1 -0.2 -5.6 -- WPD2 Brc l.O -4.1 -0.7 -3.7 -. - WPB1 Brc !.6 -9.4 -2.0 . -10.0 --- WPCI Brc 2.1 -7.5 -2.4 -7.9 --- WPB2 Brc 0.2 -5.6 -0.7 -6.1 -. - WPC2 Brc 0.7 -3.7 -!.0 -4.1 --- M aximum Combined Reactions s ummarywith F actored Loads ~ F ramina XwLOC Grid Hrz left Load HrzRight Load Hrzln Load HrzOut Load Uplift Load V1tDown Load Momcw Load Momccw Load (-Hx) CaSe (Hx) Case (-Hz) CaSe (Hz) Case (-Vy) Case (Vy) Case (-Mzz) Case (Mzz) Case .(k) (k) (k) (k) (k) (k) (in-k) (in-k) 0!010 5-D 7.0 18 14.4 9 - - - -5.6 16 66.8 3 --- 53/0/0 5-A 14.4 8 7.0 19 -' - -5.6 17 6!.9 2 -- -. . s urn· of Forces wit h React ons Check-. ramlng: ., . ) Horizontal . Vertical Lead Type Load Reaction Load Reaction (k) (k) (k) (k) D 0.0 0.0 8.8 8.7 AD 0.0 0.0 2.3 2.2 CG 0.0 0.0 25.4 25.4 s 0.0 0.0 76.5 76.5 US!* 0.0 0.0 68.9 68.9 *USI 0.0 o:o 68.9 68.9 W1> 1!.5 ll.5 16.2 16.2 <W1 11.5 1!.5 16.2 16.2 W2> 11.5 1!.5 8.6 . 8.6 <W2 11.5 ll.5 8.6 8.6 'AL> !.9 !.9 15.5 14.7 AL*> !.9 !.9 15.5 14.7 <*AL !.9 !.9 15.5 14.7 <AL* !.9 !.9 15.5 14.7 cu 0.0 0.0 10.2 10.2 E> 8.7 8.7 0.0 0.0 EO+ 0.0 0.0 3.1 3.1 <E 8.7 8.7 o.o 0.0 EO-0.0 0.0 3.1 3.1 EB> 0.0 0.0 0.0 0.0 <EB 0.0 0.0 0.0 0.0 WPAI 0.5 0.5 19.3 19.3 "AL 0.0 0.0 15.5 14.7 ALB> 0.0 0.0 0.0 0.0 AL* 0.0 0.0 15.5 14.7 WPDI 0.3 0.3 15.4 15.4 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 124 of 175 WPA2 0.5 0.5 I 1.7 I 1.7 WPD2 0.3 0.3 7.8 7.8 WPBI 0.5 0.5 19.3 19.3 WPCI 0.3 0.3 15.4 15.4 WPB2 0.5 0.5 11.7 11.7 WPC2 0.3 O.J 7.8 7.8 B PI S ase ate ummarv X-Loc Grid Mem. Thickness Width Length Num.Of BoltDiam. Type Welds to Welds to No. (in.) fin.) fin~) Bolts fin.) Flang~ Web 01010 5-D I 0.500 9 13 4 1.000 A36 OS-0.1875 OS-0.!875 53/0/0 5-A 6 0.500 9 13 4 1.000 A36 OS-0.1875 OS-0.1875 WbSff S • t1 ener umma Mem. Stiff. Desc. Loc. Web Depth hit a/h a Thick. Width Side Welding No. No. (ft) (in.) (in.) lin.) lin.) Descriotion 2 I S9 3.85 45.069 180.27 N/A N/A 0.5000 2.500 Both W-OS-0.1875 2 2 Sl 13.17 30.308 121.23 3.00 90.78 0.2500 2.000 Both Std 5 I S9 13.94 45.069 180.27 N/A N/A 0.5000 2.500 Both W-OS-0.1875 5 2 S1 12.29 42.460 169.84 3.00 127.00 0.2500 2.000 Both F-OS-0.1875,W-OS-0.1875 Brackets Part Summary Mem. Loc. Total Length Brack~.\Cut Bracket Fig Width FlgThk WebThk Hole Pitch Stiffener or Plate Part No. (ft) (in.) (in. Depth (in.) :(in.) (in.) (in.) (in.) 2 3.94 13.750 4.875 10.000 . 6.000 0.2500 0.2500 3.500 UP070411000 WU13641434 5 13.85 13.750 4.875 10.000 6.000 0.2500 0.2500 3.500 UP070411 000 WU13641434 Brackets Desil!n Summ_~!Y (vertical live load is with the iJ!lpl)ct factor Mem. Loc. Vert Live Vert. Dead Lateral Longitudinal CL Distto Member Member WebThk Flg~k Fig Width No. (ft) ' Load (k) Load fk) lmoact lkl lmoact fk) 2 3.94 13.72 1.15 0.94 1.47 5 13.85 13.72 1.15 0.94 1.47 Bolted End-Plate Moment Connections CAISC DG-16)-Fv =55 ksl Mem. Jt. No. No. 1 2 2 I 3 2 End-Plate Dimensions Bolt Type Thick. Width Length Diam. Spec/Joint (in.) (in.) (i,;:) (in.) KN(Top) 0.625 6.00 45.00 0.750 A325X/ST KN(Top) 0.625 6.00 45.00 0.750 A325X/ST SP 0.375 6,00 33.00 0.750 A325X/ST Gusset In 3.000 x 0.2500 x 5.25 FO-BS-0.1875, SP I 0.375 I 6.00 I 33.00 I 0.750 I A325X/ST I Gusset In 3.000 x 0.2500 x 5.25 FO-BS-0.1875, I 5 12 ,.KN(Top) I 0.625 I 6.00 I 45.00 I ,0.750 I A325X/ST I 6 2 KN(Top) 0.625 6.00 45.00 0.750 A325X/ST Flange lin.) Deothl lin.) Deoth2 lin.) _(in)_ (in. -(in,) 11.741 43.403 41.012 0.2500 0.5000 6.0000 11.741 42.012 42.403 0.2500 0.5000 6.0000 Outside Flange Inside FlanO"e Gages l'l/Out Configuration Pitches 1st/2nd Configuraticn Pitches ::.St12nd . (in.) ID Desc. (in. JD Desc. in.) 3.50 12 Flush 2.00 11 Flush 2.00 3.50 12 Flush 2.00 11 Flush 2.00 3.00 11 Flush 0.00 42 Ext/Gusset 3.69/2.00 3.00 I 11 I Flush I o.oo I 42 I Ext/Gusset! 3.69/2.00 3.50 I :i I Flush I 2.00 I :: I Flush I 2.00 3.50 Flush 2.00 Flush 2.00 Required Strength -Out Available Sn·ength-Out Required Strength -In Available Strength-In Mem. Jt. Ld Axial Shear Moment Design Shear Moment No. No. Cs (k) (k) (in-k) Pro c. (k) (in-k) 1 2 2 -38.8 10.6 3557.7 Thin plate 159.0 2814.0 2 I 2 -38. 10.6 3557.7 Thin plate 159.0 2814.0 3 2 17 3.1 3.6 17.6 Thin plate 106.0 574.5 4 I 17 3.1 3.6 17.6 Thin plate 106.0 574.5 5 2 3 -38.9 10.6 3572.7 Thin plate 159.0 2814.0 6 2 3 -38.9 10.6 3572.7 Thin plate 159.0 2814.0 I 22/5/4 22/5/4 1 27/5/4 27/5/4 2 2/1111 25/2/4 3 2/6/0 7/9/13 3 8/6/0 1/9113 4 1/6/0 1/9/13 5 6/6/0 16/9113 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Ld Cs 16 16 I I 17 17 Axial (k) 5.7 5.7 -13.0 ·13.0 5.7 5.7 FB4034 (2)FB5040 (2)FB5114 FB3030 FB3050 FB3050 FB4060 Shear Moment Design (k) (in·k) Proc. 1.4 1126.2 Thick plate 1.4 1126.2 Thick plate 3.4 1693.2 Thin plate 3.4 1693.2 Thin plate 1.4 1126.2 Thick plate 1.4 1126.2 Thick plate Version: 7.la Shear Moment (k) (in-k) 106.0 1660.0 106.0 1660. 212.1 1547.4 212.1 1547.4 106.0 1660. 106.0 1660.0 I 0 0 5 6 6 6 07-27053 Calculations Hazardous Materials Occupmtcy 14/10/7 12/5/4 22/5/4 27/5/4 25/2/4 12/5/4 22/5/4 271514 (2)FB5114 FB2110 SFB4034 . (2)FB5040 Date: 10/20/2008 Time: I :57:43 PM Page: 125 of 175 Frame Desh!n Member Summary~ Controllinl! Load Case and Maximum Combined Stresses per Member (LocatiOns are from Joint l } Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear Mom-x Mom-y Axial Shear Bnd~X Bnd-Y ... Stress /Force . .. Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear I 22.46 37.61 I -54.5 -10.8 -2908.0 0.0 3.59 1.19 18.71 0.00 25.12 3.88 26.15 41.25 0.84 0.31 2 1.61 47.39 2 -24.3 26.6 -3235.0 0.0 1.38 2.29 14.99 0.00 28.55 2.42 19.50 41.25 0.81 0.95 3 2.50 25.08 3 -13.9 2. 2048.1 0.0 1.40 0.70 25.05 0.00 29.89 3.87 32.69 41.25 0.81 0.18 4 7.11 25.08 2 -13.9 -2.8 2044.0 0.0 1.40 0.71 25.00 0.00 29.89 3.87 32.69 41.25 0.81 0.18 5 0.00 24.00 2 . -16.5 -7.5 1868.7 0.0 1.40 1.31 20.73 0.00 29.50 9.82 33.00 41.25 0.67 0.13 6 22.46 37.61 I -54.5 10.8 -2923.1 0.0 3.60 1.18 18.81 0.00 22.47 3.88 26.03 41.25 0.85 0.31 Mem. Loc. Depth Area Rx Ry Lx Ly-1 Ly-2 Klx Klyl Kly2 Sx Lbl Rt-1 Lb2 Rt-2 Qs Qa Cbl Cb2 No. ft in. in.2 in. in. in. in. in. /Rx fRy /Rv in.3 in. in. in. in. 1 22.46 37.61 15.15 14.27 1.09 336.87 30.0 60.1 35.4 27.5 55.0 155.38 120.1 1.46 60.1 \.44 1.00 0.86 1.27 \.09 2 1.61 47.39 17.60 17.48 1.01 298.83 4.7 28.5 17.1 4.6 28.1 215.79 4.7 1.37 172.8 1.40 1.00 0.95 1.02 1.82 3 2.50 25.08 9.9 10.50 1.3 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 1.00 1.00 1.05 1.01 4 7.11 25.08 9.9 10.5( \.3 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 1.00 1.00 1.01 1.05 5 0.00 24.00 11.75 9.60 1.24 298.83 36.0 0.0 31.1 29.1 0.0 90.16 36.0 1.55 0.0 0.00 1.00 1.00 1.05 0.00 6 22.4 37.61 15.15 14.27 1.09 336.87 60.1 60.1 35.4 55.0 55.0 155.38 120.1 1.46 60.1 1.44 1.00 0.8 1.26 1.09 0 • File: 7079 CheVTon RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 0 07~27053 Calculations Hazardous J;faterials Occupancy User Defined Frame Point Loads for Cross Sect'on· 5 ' Side Units Type Description Mag1 Loci Offset HorV Supp. 1 k CG PS·41 Pipe Loads -1.70 20/8/6 -2/3/0 Horiz. N 1 k CG PS·46 Pipe Loads -0.30 16/713 3/3/0 Horiz. N 1 k CG Lube Tanks -1.50 10/0/0 NA NA N 1 k CG Lube Tanks -1.50 10/0/0 1/0/0 Horiz. N y X fl L C De ectlon oad ombinatlons ~ Framin No. Origin Factor DefH DefY Application ·:> 1 System 1.000 0 240 1.0 s s 2 System 1.000 0 240 1.0 USl* USl* 3 System 1.000 0 240 1.0 *USl *USl 4 System 1.0000 0 240 0.700W1> W1> 5 Systein 1.000 0 240 0.700<W1 f<W1 6 System 1.000 0 240 0.700 W2> W2> 1 System 1.000 0 240 0.700<W2 } <W2 8 System Derived 1.000 0 240 0.700WPA1 ~A1 9 System Derived 1.000 0 240 0.700WPD1 r.wo1 10 System Derived 1.000 0 240 ~.700WPA2 WPA2 11 System Derived 1.000 0 240 0.700WPD2 WPD2 12 System Derived 1.000 0 240 0.700WPB1 ~B1 13 System Derived 1.000 0 240 0.700WPC1 r.wc1 14 System Derived 1.000 0 240 0.700WPB2 WPB2 15 System Derived 1.000 0 240 ~.700 WPC2 WPC2 16 System 1.000 400 0 r.1oow1> ~1> 17 System 1.000 400 0 0.700<W1 ~W1 18 System 1.000 400 0 0.700W2> w2> 19 System 1.000 400 0 0.700<W2 W2 20 System Derived 1.000 400 0 0.700WPA1 WPA1 21 System Derived 1.000 400 0 0.700WPD1 WPD1 22 System Derived 1.000 400 0 0.700 WPA2 WPA2 23 System Derived 1.000 400 0 0.700WPD2 WPD2 24 System Derived 1.000 400 0 0.700 WPB1 WPB1 25 System Derived 1.000 400 0 0.700 WPC1 WPC1 26 System Derived 1.000 400 0 0.700WPB2 WPB2 27 System Derived 1.000 400 0 0.700 WPC2 WPC2 28 System 1.000 100 0 0.600 E> +0.700 EG-E>+EG~ 29 System 1.000 100 0 0.600 <E + 0.700 EG-E+EG~ 30 System Derived 1.000 100 0 0.600 EB> EB> 31 System Derived 1.000 100 0 0.600 <EB EB 32 System 1.000 400 0 J.O<AL* AL' 33 Svstem 1.000 400 0 1.0 *AL> *AL> Controllin Frame Deflection Ratios for Cross Section: 5 Date: 10/20/2008 Time: I :57:43 PM Page: l26ofl75 Dir. Coef. Loc. DOWN 1.000 OF DOWN 1.000 1F DOWN 1.000 CL DOWN 1.000 1F DescriPtion ' Descri tion Ratio Deflection in. Member Joint Load Case Load Case Descri tion File: 7079 Chevron R !_Stress Check 10 _2008 with 08_2008 Loading Version: 7.la 0 07-27053 Calculations Hazardous Materials Occupancy * Negative horizontal deflection is left * Negative vertical deflection is down -0.819 -1.033 Date: 10/20(2008 Time: I :57:43 PM Page: 127 of 175 <W2 s Lateral deflections of primary frames are calculated on a bare frame basis and do not include resistance from systems such as roof and endwall diaphragms. Therefore, these deflections may be considerably overstated. File: 7079 Chevron R !_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Dimension Key I 5'·6" BL to CL of Runway Beam 2 I S/8'' 3 4'·0" 4 3'-5 !14" s 2@2'-6" 6 3'-3 3/4" 7 1'-3" 8 1'-913/16" 9 2@2'-47116" 10 4 1/2" II 40'-10" Ridge Ht Frame Clearances X FRAME CROSS SECTION AT FRAME LINE(S) 6 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.\a Date: 10/20/2008 Time: I :57:43 PM Page: 128 of 175 07-27053 Calculations Hazardous Materials Occupancy Horiz. Clearance between members l(CXOOO) and 6(CXOOO): 45'·4 3/4" Vert. Clearance at member I (CXOOO): 28'-0 1/2" Vert. Clearance at member 6(CXOOO): 28'-0 J/2" Finished Floor Elevation= 100'-0" (Unless Noted Otherwise) Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA !-!(Left), 2'-4 3/16" Horz. Clearance at CRANE DATA 1-l(Left): l'-10 l/8" Vert. Clearance at CRANE DATA \-!(Right): 2'-4 3/16" Horz. Clearance at CRANE DATA \-\(Right): 1'-10 1/8" File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: I :57:43 PM Page: l29ofl75 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 130 of 175 Descri tion An le Grou Trib. Override Desi n Status 86/3/0 Ri id Frame 90.0000 Stress Check D I dC e~gn Loa ombinatmns-Framin No. Origin Factor Application DescriPtion I System !.000 l.OD+ l.OAD+ l.OCG+ 1.08 D+AD+CG+S 2 System !.000 !.0 D + !.0 AD+ !.0 CG +.l.OUSI' D+AD+CG+USI* 3 System !.000 l.OD+ LOAD+ LOCO+ LO*USI D +AD+ CG + *USI 4 System !.000 LO D + 1.0 AD+ 1.0 CG + LO WI> D +AD+ CG +WI> s System !.000 1.0 D + !.0 AD+ !.0 CG + !.O<Wl p+AD+CG+<Wl 6 System !.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 W2> D+AD+CG+W2> 7 System !.000 l.O D + !.0 AD+ !.0 CG + !.0 <W2 D+AD+CG+<W2 · 8 System !.000 LO D + 1.0 AD+ 1.0 CG +0.750 S +0.750 Wl> D+AD+CG+S+Wl> 9 System !.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 <WI D+AD+CG+S+<Wl 10 System !.000 l.O D + 1.0 AD+ 1.0 CO+ 0.750 S +0.750 W2> D+AD+CG+S+W2> II Syst()m !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 <W2 D+AD+CG+S+<W2 12 System !.000 1.0 D +LOAD+ l.O CG + 1.0 "'AL> D +AD +CG+*AL> !3 System 1.000 1.00+ l.OAD+ l.OCG+ l.OAL"'> D+AD+CG+AL*> !4 System 1.000 l.O D + 1.0 AD+ 1.0 CG+ 1.0 <*AL D +AD+ CG+<"' AL IS System 1.000 1.0 D + 1.0 AD+ !.OCG + 1.0 <AL' D +AD+ CG+<AL • !6 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WI> D+AD+CU+Wl> 17 System 1.000 ~.600 D+ 0.600 AD+0.600 CU + !.0 <WI D+AD+CU+<Wl 18 System !.000 0.600 D + 0.600 AD+ 0.600 CU + !.0 W2> D+AD+CU+WZ> !9 System 1.000 p.600 D + 0.600 AD+ 0.600 CU + !.0 <W2 io+AD+CU+<W2 20 System 1.000 1.0 D+ 1.0 AD+ !.0 CG+0.563 S +0.750 *AL> P+AD+CG+.S+"'AI> 21 System !.000 1.0 D + 1.0 AD+ !.0 CG +0.563 S+0.7SO AL'> D+AD+CG+S+AL*> 22 System !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S+0.750<'AL D+AD+CG+S+<*AL 23 System !.000 l.O D+ !.0 AD+ l.OCG +0.563 S +0.750 <AL' D+AD+CG+S+<AL"' 24 System 1.000 1.0 D+ !.0 AD+ !.0 CG+0.3JS W!>+0.750 'AL> D+AD+CG+Wl>+*AL> 0 25 System !.000 1.0 D +LOAD+ l.O CO +0.375 Wl> +0.750 AL"'> D+ AD+CG+WI>+AL*> 26 System !.000 1.0 D + !.0 AD+ !.0 CG+0.375 <WI +0.750 <'AL D+AD+CG+<Wl+<*AL 27 ·system !.000 1.0 D + 1.0 AD+ !.0 CG + 0.375 <WI + 0.750 <AL' D+AD+CG+<Wt+<AL* ' 28 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 W2> + 0.750 'AL> D +AD+ CG +W2>+*AL> 29 System 1.000 l.OD+ !.0 AD+ !.0 CG +0.375 W2>+0.750 AL'> D+ AD+CG+W2>+AL*> 30 System 1.000 !.0 D + !.0 AD+ !.0 CG+0.375 <W2+0.750 <'AL D +AD+ CG + <W2+<*AL 31 System !.000 l.O D.+ LOAD+ 1.0 CG+0.375 <WZ +0.750 <AL* D +AD+ CG + <WZ+<AL * 32 System !.000 1.0 D+ !.0 AD+ l.OCG +0.150 S+0.7SO E>+0.700 EG+ D+AD+CG+S-I:E>+EG+ 33 System !.000 !.0 D+ !.0 AD+ !.OCG +0.!50 S +0.750 <E+0.700 EG+ b+AD+CG+S+<E+EG+ 34 System !.000 p.600 D + 0.600 AD+ 0.600 CU +0.700 E> +0.700 EG-D+AD+CU+E>+EG· 35 System 1.000 p.600 D + 0.600 AD+ 0.600 CU +0.700 <E + 0.700 EG· D+AD+CU+<E+EG· 36 System Derived !.000 !.0 D+ !.0 AD+ !.0 CG +0.150 S +0.750 EB> +0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0.700 EG-D+AD+CU+EB>+EG- 38 System Derived !.000 l.O D + !.0 AD+ !.0 CG + 0.150 S + 0.750 <EB + 0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived !.000 p.600 D+ 0.600 AD +0.600CU +0.700 <EB +0.700 EG-D+AD+CU+<EB+EG~ 40 System Derived !.000 1.0 D+ !.0 AD+ !.0 CG + !.0 WPA! D+AD+CG+WPAl 41 System Derived !.000 1.0 D + !.0 AD+ !.0 CG +0.750 S +0.750 WPA! D+AD+CG+S+WPAI 42 System Derived !.000 0.600 D+ 0.600 AD+ 0.600 CU + !.0 WPA! D+AD+CU+WPAl 43 System Derived !.000 1.0 D + !.0 AD+ !.0 CG +0.375 WPA! +0.750 'AL+0.7SO ALB> D+AD+CG+WPAI+"'AL+ALB> 44 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPAI + 0.750 AL* +0.750 ALB> D+AD+CG+WPA I +AL *+ALB> 45 System Derived !.000 1.0 D+ !.0 AD+ !.0 CG + !.0 WPD! D +AD+ CG + WPDI 46 System Derived 1.000 !.0 D + !.0 AD+ !.0 CG +0.750 S +0.750 WPD! D+AD+CG+S+WPDI 47 System Derived !.000 0.600 D+ 0.600 AD+ 0.600 CU + !.0 WPD! D+AD+CU+WPDI 48 System Derived !.000 l.O D + 1.0 AD+ 1.0 CG+0.375 WPDl +0.750 "'AL +0.750 <ALB D+AD+CG+WPDI+*AL+<ALB 49 System Derived !.000 1.0 D+ 1.0 AD+ 1.0 CG +0.375 WPDI + 0.750 AL * +0.750 <ALB D+AD+CG+WPDI+AL*+<ALB so System Derived !.000 1.0 D + !.0 AD+ 1.0 CG + 1.0 WPA2 D+AD+CG+WPAZ 51 System Derived !.000 1.0 D + !.0 AD+ 1.0 CG +0.750 S + 0.750 WPA2 D+AD+CG +S + WPAZ 52 System Derived !.000 0.600 D +0.600 AD +0.600CU + !.0 WPA2 D+AD+CU+WPA2 53 System Derived !.000 l.O D + 1.0 AD+ 1.0 CG + 0.375 WPAZ + 0.750 *AL +0.750 ALB> D+ADtCG+WPA2+*AL+ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 + 0.750 AL* +0.750 ALB> D+AD+CG+WPA2+AL *+ALB> ss System Derived !.000 l.O D + 1.0 AD + 1.0 CO + 1.0 WPD2 D+AD+CG+WPD2 56 System Derived !.000 1.0 D + 1.0 AD+ !.0 CG +0.750 S + 0.750 WPD2 D+AD+CG+S+WPD2 57 System Derived !.000 0.600 D + 0.600 AD +0.600CU + !.0 WPD2 D+AD+CU+WPD2 58 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDZ + 0.750 *AL +0.750 <ALB D+AD+CG+WPD2+*AL+<ALB 59 System Derived !.000 1.0 D + !.0 AD+-!.0 CG + 0.375 WPD2 + 0.750 AL * + 0.750 <ALB D+AD+CG+WPD2+AL*-i<ALB File: 7079 Chevron R !_Stress Check I 0_2008 with 08_2008 Loading Version: 7.la " 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 131 of175 60 System Derived 1.000 1.0 D+ !.OAD+ !.OCG + I.OWPBI 61 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPBI 62 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB I 63 System Derived 1.000 1.0 D + l.O AD+ 1.0 CO+ 0.375 WPBI + 0.750 *AL + 0.750 ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPBl + 0.750 AL* + 0.750 ALB> 65 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 WPC1 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPC1 67 System Derived 1.000 .600 D+0.600 AD +0.600 CU + 1.0 WPCI 68 System Derived 1.000 1.0 D +LOAD+ 1.0 CG + 0.375 WPCl + 0.750 *AL + 0.750 <ALB 69 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPCJ + 0.750 AL * + 0.750 <ALB 70 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CO + 1.0 WPB2 71 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 73 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPB2 +0.750 *AL + 0.750 ALB> 74 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPB2 +0.750 AL* + 0.750 ALB> 75 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPC2 76 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 78 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPC2 +0.750 *AL +0.750 <ALB 79 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPC2 +0.750 AL* +0.750 <ALB 80 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CO + 1.0 S + 1.0 ALB> 81 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 *AL+ 1.0 ALB> 82 System Derived 1.000 I.OD +.LOAD+ 1.0 CO+ 1.0 AL* + 1.0 ALB> 83 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.563 S +0.750 *AL+0.750ALB> 84 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.563 S + 0.750 AL' + 0.750 ALB> 85 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CO + 1.0 S + 1.0 <ALB 86 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CO + 1.0 * AL + 1.0 <ALB 87 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO + 1.0 AL' + 1.0 <ALB 88 System Derived · 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.563 S +0.750 'AL+0.750 <ALB 89 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 C0+0.563 S + 0.750 AL* +0.750<ALB . F M b Sl rame em er zcs Mem. Fig Width Flf;Thk WebThk Depth! Depth2 Length w7t' FlgFy No. (in.) . in.) . (in.) (in.) (in.) aii cksi) I 6.00 0.5000 0.2500 12.00 44.00 31.03 1278.0 55.00. 2 6.00 o.sooo 0.2500 48.00 24.00 17.79 974.2 55.00 3 6.00 0.5000 0.1644 24.00 28.00 10.00 343.6 55.00 4 6.00 o.sooo 0.1644 28.00 24.00 IO.oti' 343.5 55.00 5 6.00 0.5000 0.2500 24.00 48.00 17.79 974.2 55.00 6 6.00 0.5000 0.2500 12.00 44.00 31.03 1278.0 55.00 Total Frame We1ght-5191.5 (p) Frame Pricing Weight= 5712.5 (p) 6 2 53/0/0 5/6/0 47/6/0 01010 33/10/0 Yes Yes Yes Yes Yes No Yos 0/0/0 01010 Values shown are resisting forces of the foundation. Reactions-Unfactored Load Type at Frame Cross Section: 6 Type Exterior Column Exterior Column X·Loc 01010 5310/0 Grid I • Grid2 6-D 6-A Base Plate W XL (in.) 9x 13 9x 13 Base Plate Thickness (in.) 0.500 0.500 Anchor Rod Qty/Diam. (in.) 4-1.000 4-1.000 Column Base Elev. !00'·0" 100'-0" Load Type DeSc. Hx Vy Hx Vy D Fnn 0.8 4.3 -0.8 4.3 AD Fnn 0.1 1.1 -0.1 1.1 - C'G Fnn 2.6 15.2 ·2.6 I 0.2 s Fnn 9.8 38.3 -9.8 38.3 US I* Fnn 8.8 22.7 -8.8 46.2 - *US! Fnn 8.8 46.2 -8.8 22.7 - WI> Fnn -6.9 -1 1.9 -4.6 -4.3 - File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading D+AD+CG+WPBl D +AD +CG +S+WPBI D+AD+CU+WPBI D+AD+CG+WPB l +* AL +ALB> D+AD+CG+WPBI+AL *+ALB> D +AD+ CO+ WPCI D+AD+CG+S+WPCI D +AD+ CU + WPCI D+AD+CG+WPC!+*AL+<ALB D+AD+CG+WPCl+AL*+<ALB D+AD+CO+WPB2 D+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+"' AL +ALB> D+AD+CG+WPB2+AL "'+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2 D +AD+ CU + WPC2 D+AD+CG+WPC2+*AL+<ALB D+AD+CG+WPC2+AL "'t<ALB D+AD+CG+S+ALB> lo +AD+ CG+* AL+ALB> io +AD+ CG+AL *+ALB> P+AD+CG+S+*AL+ALB> D+AD+CG+S+AL*+ALB> p +AD+ CO+ S+<ALB iD + AD+ CG+* ALt<ALB ~+AD+ CG+AL *+<ALB P+AD+CG+S+* AL+<ALB D+AD+CO+S+AL*+<ALB WebFy Splice Codes Shape (ksi\ Jt.l 55.00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP (Includes all plates) (Includes all pieces) 0/010 0/0/0 0/010 - - - Version: ?.Ia Jt.2 KN ss SP ss KN KN 0.0000 0.0000 0.0000 - - - 3P 3P 3P JP 3P 3P 0 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 132ofl75 <WI Frm 4.6 -4.3 6.9 -11.9 -- W2> Frm -8.3 -8.1 -3.2 -0.4 -- <W2 Frm 3.2 -0.4 8.3 -8.1 --- 'AL> Frm -0.1 10.0 -1.8 4.7 -- AL*> Frm -0.1 2.7 -1.8 12.0 -- <*AL Frm 1.8 12.0 0.1 2.7 -- <AL* Fnn 1.8 4.7 0.1 10.0 -- cu Frm 1.3 5.1 -1.3 5.1 -- E> Fnn -4.6 -5.6 -4.2 5.6 -- EG+ Fnn 0.3 1.8 -0.3 1.4 --- <E Fnn 4.6 5.6 4.2 -5.6 --- EG-l'nn . -0.3 -1.8 0.3 -1.4 -- EB> Brc ------ <EB Brc ------- WPAI Brc 2.4 -7.9 -2.1 -7.5 - 'AL Fnn 0.9 11.0 -0.9 3.7 ALB> Brc ---- AL' Fnn 0.9 3.7 -0.9 11.0 --- WPDI Brc 2.0 -10.0 -1.6 -9.4 -- <ALB Brc ------- WPA2 Brc 1.0 -4.1 -0.7 -3.7 -- WPD2 Brc 0.7 -6.1 -0.2 -5.6 --- WPBI Brc 2.1 -7.5 -2.4 -7.9 -. . ·WPCI Brc 1.6 -9.4 -2.0 -10.0 . . - WPB2 Brc 0.7 -3.7 -1.0 -4.1 -. . WPC2 Brc 0.2 -5.6 .().7 -6.1 --. MaximUm Combined Reactions Summarv with Factored Loads-Frainin2' X-Loc Grid Hrz left Load Hrz Right Load Hrz In Load Hrz Out Load Uplift Load V11 Down Load Momcw Load Momccw Load (·H•) Case (&) case (·Hz) Case (Hz) case (-Vy) Case (Vy) Case (·Mzz) case (Mzz) Case (k). (k) 'ik) (k) (k) <kl (in-k) (in-k) 01010 6-D 7.0 18 14.4 9 . . . . 5.6 16 66.8 3 . . . . 531010 6-A 14.4 8 7.0 19 . ~ . -5.6 17 61.9 2 . . -. '" Sum of Forces with Reactions Check -Framinf' 0 Horizontal Vertical Load Type L~~d Re~~ion L~~d Re~~ion D 0.0 0.0 8.8 8.7 AD 0.0 0.0 2.3 2.2 CG 0.0 0.0 25.4 25.4 s 0.0 0.0 76.5 76.5 US!* 0.0 0.0 68.9 68.9 *USl 0.0 0.0 68:9 68.9 W1> 11.5 11.5 16.2 16.2 <W1 ll.5 ll.5 16.2 16.2 W2> 11.5 11.5 8.6 8.6 <W2 ll.5 11.5 8.6 8.6 'AL> 1.9 1.9 15.5 14.7 AL*> 1.9 1.9 15.5 14.7 <*AL 1.9 1.9 15.5 14.7 <AL* 1.9 1.9 15.5 14.7 cu 0.0 0.0 10.2 10.2 E> 8.7 8.7 0.0 0.0 EG+ 0.0 0.0 3.1 3.1 <E 8.7 8.7 0.0 0.0 EG-0.0 0.0 3.1 3.1 EB> 0.0 0.0 0.0 0.0 <EB 0.0 0.0 0.0 0.0 WfAI 0.3 0.3 15.4 15.4 'AL 0.0 0.0 15.5 14.7 ALB> 0.0 0.0 0.0 0.0 AL* 0.0 0.0 I 5.5 14.7 WPD1 0.5 0.5 19.3 19.3 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 133ofl75 WPA2 0.3 0.3 7.8 7.8 WPD2 0.5 0.5 1!.7 1!.7 WPBI 0.3 0.3 15.4 I 5.4 WPCI 0.5 0.5 19.3 19.3 WP82 0.3 0.3 7.8 7.8 WPC2 0.5 0.5 1!.7 11.7 Base Plate Summary X~Loc Grid Mem. Thickness Width Length Num.Of Bolt Diam. Type Welds to Welds to No. (in.) (in.) (in~) Bolts (in.) Flange Web 01010 6-D 1 0.500 9 13 4 !.000 [A36 OS-0.1875 OS-0.1875 53/0/0 6-A 6 0.500 9 13 4 !.000 A36 OS-0.1875 OS-0.1875 Web Stiffener Summar Mem. Stiff. Desc. Loc. Web Depth hit alh a Thick: Width Side Welding No. No. (ft) (in.) (in.) (in.) (in.) Description 2 I S9 3.85 45.069 180.27 N/A NIA 0.5000 2.500 Both W-OS-0.1875 2 2 Sl 13.!7 30.308 12!.23 3.00 90.78 0.2500 2.000 Both Std 5 I S9 13.94 45.069 180.27 NIA NIA 0.5000 2.500 Both W-OS-0.1875 5 2 Sl 12.29 42.460 169.84 3.00 127.00 0.2500 2.000 Both F-OS-0.!875,W-OS-0.!875 . Brackets p s art ummarv Mem. Loc. Total Length Bracket Cut Bracket Fig Width FlgThk WebThk Hole Pitch Stiffener or Plate Part No. (ft) (in.) lin.) Deoth (in.' lin.) iin.) lin.) lin.) 2 3.94 13.750 4.875 10.000 6.000 0.2500 0.2500 3.500 UP070411000 WUI3641434 5 13.85 13.750 4.875 10.000 6.000 0.2500 0.2500 3.500 UP070411000 WU!364!434 Brackets Desie:n Summary (vertical live load Is with the impact factor Mem. Loc. Vert. Live Vert. Dead Lateral Longitudinal CL Distto Member Member WcbThk Fig Thk Fig Width No. 1ft) Load (k) Load (k) Impact lk) Impact (k) 2 3.94 13.72 !.15 0.94 !.47 5 13.85 13.72 l.l5 0.94 !.47 0 Bolted End-Plate Moment Connections (AlSC DG-16)-Fy"" 55 ksl Mem. Jt. No. No. I 2 2 I 3 2 End-Plate Dimensions Bolt TypO Thick. Width Length Diam. Spec/Joint · (in.) (in.) (in.) (in.) KN(Top) 0.625 6.00 45.00 0.750 A325X/ST KN(Top) 0.625 6.00 45.00 0.750 A325X/ST SP 0.375 6.00 33.00 0.750 A325X/ST Gusset In 3.000 x 0.2500 x 5.25 FO-BS-0.1875, SP I 0.375 I 6.00 I 33.00 I 0.750 I A325X/ST I Gusset In 3.000 x 0.2500 x 5.25 FO-BS-0.1875, l 5 121 KN(Top) I 0.625 I 6.00 I 45.00 I 0.750 I A325X/ST I 6 2 KNiTo~l 0.625 6.00 45.00 0.750 A325X/ST Flane.e (in.) De )th 1 (ln.) Dcpth2 (in.) (in.) (in.) 0 (in.) ll.74I 43.403 4!.012 0.2500 0.5000 6.0000 1!.741 42.012 42.403 0.2500 0.5000 6.0000 'J Outside Flange Inside Flamzc Gages In/Out Confl,.uratio~} Pitches 1st/2nd Configuration Pitches 1st/2nd (in.) ID Desc. · (in.) ID Desc. (in.) 3.50 12 Flush 2.00 ll Flush 2.00 3.50 12 Flush 2.00 1I Flush 2.00 3.00 11 Flush 0.00 42 Ext/Gusset 3.69/2.00 3.00 Ill I Flush I 0.00 142 I Ext/Gusset I 3.69/2.00 3.50 I:; I Flush I 2.00 I :: I Flush I 2.00 3.50 Flush 2.00 Flush 2.00 Reauired Strength -Out Available Stremrth -Out Reouircd Strength -In Available Strcmnh-In Mem. Jt. Ld Axial Shear Moment Design s~~ Moment Ld Axial Shear Moment Design s~~r Moment No. No. Cs (k) (k) fin-k) Proc. fin-k) Cs (k) lk) lin-k) Proc. lin-k) 1 2 2 -38.8 10.6 3557.7 Thin plate 159.0 2814.0 16 5.7 1.4 !126.2 Thick plate 106.0 !660.0 2 1 2 -38.8 10.6 3557.7 Thin plate 159.0 2814.0 16 5.7 1.4 !126.2 Thick plate 106.0 !660.0 3 2 17 3.1 3.6 17.6 Thin plate 106.0 574.5 1 -13.0 3.4 1693.2 Thin plate 212.1 1547.4 4 1 17 3.1 3.6 17.6 Thin plate 106.0 574.5 1 -13.0 3.4 1693.2 Thin plate 212.1 1547.4 5 2 3 -38.9 10.6 3572.7 Thin plate 159.0 2814.0 17 5.7 1.4 !126.2 Thick plate !06.0 1660.0 6 2 3 ·38.9 10.6 3572.7 Thin olate 159.0 2814.0 17 5.7 1.4 !126.2 Thick olate 106.0 !660.0 Flange n. Member ~oint! From Side Point I Part Design Note : i~~;: FB2!10 i2/5/4 FB4034 1 271514 27/5/4 (2)FB5040 2 2/!l/l 25/2/4 (2)FB5!l4 3 2/6/0 719113 FB3030 3 8/6/0 !19113 FB3050 4 1/6/0 1/9113 FB3050 5 61610 16/9113 F84060 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version~ ?.Ia I 0 5 6 6 6 07-27053 Calculations Hazardous Materials Occupancy 1411017 121514 221514 271514 251214 121514 2215/4 27/5/4 (2)FB5114 FB2110 SFB4034 12lFB5040 Date: 10/20/2008 Time: I :57:43 PM Page: 134 of 175 Frame Design Member Summary-Controlling Load Case and Maximum Combined Stresses per Member (Locations are from Joint J ) Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear MomMx Mom-y Axial Shear Bnd-X Bnd-Y ---Stress /Force ---Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear 1 22.4 37.61 I -54.5 -10.8 -2908.0 0.0 3.59 1.19 18.71 0.00 25.12 3.88 26.15 41.25 0.84 0.31 2 1.61 47.39 2 -24.3 26.6 -3235.0 0.0 1.38 2.29 14.91 0.00 28.55 2.42 19.50 41.25 0.81 0.95 3 2.50 25.08 3 -13.9 2.8 2048.1 0.0 1.40 0.70 25.05 0.00 29.89 3.87 32.69 41.25 0.81 0.18 4 7.11 25.08 2 -13.9 -2.8 2044.0 0.0 1.40 0.71 25.00 0.00 29.89 3.87 32.69 41.25 0.81 0.18 5 0.00 24.00 2 -16.5 -7.5 1868.7 0.0 1.40 1.31 20.73 0.00 29.50 9.82 33.00 41.25 0.67 0.13 6 22.46 37.61 I -54.5 10.8 -2923.1 0.0 3.60 1.18 18.81 0.00 22.47 3.88 26.03 41.25 0.85 0.31 Mem. Loc. Depth Area Rx Ry Lx Ly-1 Ly-2 Klx Kly1 K!y2 Sx Lbl Rt-1 Lb2 Rt-2 Qs Qa Cbi Cb2 No. ft ln. in.2 in. in. in. in. in. !Rx fRy /Rv in.3 in. in. in. in. I 22.46 37.61 15.15 14.27 1.0 336.87 30.0 60.1 35. 27.5 55.0 155.38 120.1 1.46 60.1 1.44 1.00 0.86 1.27 1.0 2 1.61 47.3 17.6 17.48 1.01 298.83 4.7 28.5 17.1 4. 28.1 215.79 4.7 1.37 172.8 1.40 1.00 0.95 1.02 1.82 3 2.50 25.08 9.96 10.50 1.34 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 1.00 1.00 LOS 1.01 4 7.11 25.08 9.96 10.50 1.34 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 1.00 1.00 1.01 1.05 5 0.00 24.00 11.75 9.60 1.24 298.83 36.0 0.0 31.1 29.1 0. 90.16 36.0 1.55 0.0 0.00 1.00 1.0 1.05 0.00 6 22.46 37.61 15.15 14.27 1.09 336.87 60.1 60.1 35.4 55.0 55.0 155.38 120.1 1.46 60.1 1.44 1.00 0.86 1.26 l.o9 0 0 File: 7079 Chevron R !_Stress Check I 0 _2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy User Defined Frame Point Loads for Cross Section· 6 Side Units Type Description Mag! Locl Offset HorV Supp. I k CG PS-41 Pipe Loads -1.70 20/8/6 -2/3/0 Horiz. N I k CG PS-46 Pipe Loads -0.30 I617/3 3/3/0 Horiz. N I k CG Lube Tanks -1.50 I0/0/0 NA NA N I k CG Lube Tanks -1.50 10/0/0 I/0/0 Horiz. N 0 y X Deflect·o L d C b"natlo F m"no 'n oa om • ns-ra ' No. Qrioin Factor DefH DefY Application I System 1900 0 240 1.0 s s 2 System 1.000 0 240 I.OUSl* USI* 3 System 1.000 0 240 l.O*USl "'USI 4 System 1.000 0 240 .700Wl> lwl> 5 System 1.000 0 240 .700<Wl <> ·' WI 6 S19'tem 1.000 0 240 0.700W2> W2> 7 System 1.000 0 240 0.700<W2 ) f:w2 8 System Derived 1.000 0 240 0.700WPA1 WPAl 9 System Derived ].000 0 240 0.700WPD1 ~Dl 10 System Derived 1.000 0 240 0.700WPA2 WPA2 ll System Derived 1.000 0 240 0.700WPD2 'lv!>nz 12 System Derived 1.000 0 240 0.700WPB1 M'J'Bl 13 System Derived 1.000 0 240 0.700WPC1 WPCl I4 System Derived 1.000 0 240 0.700WPB2 WPB2 I5 System Derived 1.000 0 240 0.700WPC2 WPC2 I6 System 1.000 4ll0 0 0.700Wl> WI> I7 System 1.000 400 0 0.700<Wl fWI I8 System 1.000 400 0 ~.700W2> W2> 19 System 1.000 400 0 0.700<W2 W2 20 System Derived 1.000 400 0 ~.700WPA1 WPAl 2I System Derived 1.000 400 0 0.700WPD1 WPDl 22 System Derived 1.000 400 0 ~.700 WPA2 WPA2 23 System Derived 1.000 400 0 0.700 WPD2 WPD2 24 System Derived 1.000 400 0 0.700 WPBI WPBl 25 System Derived 1.000 400 0 0.700 WPCI WPCl 26 System Derived 1.000 400 0 0.700 WPB2 WPB2 27 System Derived 1.000 400 0 0.700 WPC2 WPC2 28 System 1.000 100 0 0.600 E>+0.700 EG-E>+EG- 29 System 1.000 IOO 0 IJ.600 <E + 0.700 EG-E+EG- 30 System Derived 1.000 100 0 0.600 EB> EB> 31 System Derived 1.000 100 0 0.600 <EB <EB 32 System 1.000 400 0 l.O<AL* AL* 33 System 1.000 400 0 1.0 *AL> *AL> Controllin Date: 10/20/2008 Time: I :57:43 PM Page: l35ofl75 Dir. Coet: Loc. DOWN 1.000 OF DOWN 1.000 IF DOWN 1.000 CL DOWN 1.000 IF Description ) Deflection (in. Member Joint Load Case Load Case Descri tion File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.Ja 07-27053 Calculations Hazardous Materials Occupancy * Negative horizontal deflection is left * Negative vertical deflection is down -0.819 ·1.033 Date: 10/20/2008 Time: I :57:43 PM 136 of 175 <WZ s Lateral deflections of primary frames are calculated on a bare frame basis and do not' include resistance from systems such as roof and endwall diaphragms. Therefore, these deflections may be considerably overstated. File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 0 07-27053 Calculations Hazardous Materials Occupancy y Dimension Key 1 5'~6'' BL to CL of Runway Beam 2 I 518" 3 4'-0" 4 3'-5 l/4" 5 2@2'-6" 6 3'-3 314" 7 1'-3" 8 1'-9 13116" 9 2@2'-47116" 10 4 112" 1! 40'-10" Ridge Ht. Frame Clearances X FRAME CROSS SECTION AT FRAME LINE(S) 7 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: ?.Ia Date: 10/20/2008 Time: I :57:43 PM 07-27053 Calculations Hazardous Materials Occupancy Hodz. Clearance between-members I (CXOOO) and 6(CXOOO): 45'-4 3/4" Ve1t. Clearance at member l(CXOOO): 28'-0 1/2" Vert. Clearance at member 6(CXOOO): 28'-0 1/2" Finished Floor Elevation= 100'-0" (Unless Noted Otherwise) Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA 1-l(Left): 2'-4 3/16" Horz. Clearance at CRANE DATA 1-l(Left): 1 '·10 1/8" Vert. Clearance at CRANE DATA !-!(Right): 2'-4 3/16" Horz. Clearance at CRANE DATA 1-I (Right): 1 '-1 0 1 /8'' File: 7079 Chevron R l_ Stress Check l 0 _ 2008 with 08 _2008 Loading Version: 7.1a Date: 10/20/2008 Time: l :57:43 PM Page: 138 of 175 .. 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 139 of 175 D I L dC bi es n oa om nat10ns ~ Framin No. Origin Factor Application ) Descrintion I System 1.000 J.OD+ LOAD+ LOCG+ LOS D+AD+CG+S 2 System 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 US I* D+AD+CG+USl* 3 System 1.000 1.0 D + \.0 AD + 1.0 CG + 1.0 *US I D+AD+CG+*USI 4 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WI> D +AD+ CG +WI> 5 System 1.000 LO D + LOAD+ LO CG + LO <WI D+AD+CG+<Wl 6 System LOOO LO D + LO AD + LO CG + LO W2> D+AD+CG+W2> 7 System 1.000 LO D + 1.0 AD+ 1.0 CG + LO <W2 D+AD+CG+<W2 8 System 1.000 1.0 D +LOAD+ 1.0 CG + 0.750 S +0.750 Wl> D+AD+CG+S+Wl> 9 System LOOO LO D + 1.0 AD+ LO CG+ 0.750 S + 0.750 <WI D+AD+CG+S+<Wl 10 System LOOO 1.0 D + 1.0 AD+ LO CG + 0.750 S + 0.750 W2> D+AD+CG+S+W2> I I System 1.000 LO D +LOAD+ LO CG + 0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System LOOO 1.0 D + 1.0 AD+ 1.0 CG + 1.0 *AL> D+AD+CG+*AL> 13 System 1.000 1.0 D + l.O AD + l.O CG + 1.0 AL"'> D+AD+CG+AL*> 14 System 1.000 1.0 D + l.O AD+ 1.0 CG + 1.0 <*AL D+AD+CG+<*AL 15 System 1.000 LO D+ 1.0 AD+ 1.0 CG + LO <AL' D +AD+ CG+<AL * 16 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + LO W1> D+AD+CU+Wl> 17 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <W1 D+AD+CU+<W1 18 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + I .0 W2> D+AD+CU+W2> 19 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 1.0 D + l.OAD+ 1.0 CG +0.563 S +0.750 'AL> D+AD+CG+S+*AL> 21 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL '> D+AD+CG+S+AL*> 22 System 1.000 1.0 D+ LOAD+ 1.0 CG +0.563 S +0.750 <'AL D+AD+CG+S+<*AL 23 System 1.000 1.0 D+ LOAD+ LO CG +0.563 S + 0.750 <AL* 0 D+AD+CG+S-AAL' 24 System 1.000 LO D + 1.0 AD+ 1.0 CG + 0.375 W1> + 0.750 'AL> D+AD+CG+Wl>+*AL> 25 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WI>+ 0.750 AL'> D+AD+CG+Wl>+AL*> 26 System 1.000 1.0 D + l.OAD + 1.0 CG +0.375 <WI +0.750<*AL b+AD+CG +<Wt+<*AL 27 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 <W1 + 0.750 <AL' D+ AD+ CG +<Wl+<AL* 28 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 W2>+ 0.750 'AL> D +AD + CG + W2>+"' AL> 29 System 1.000 1.0 D + 1.0 AD+ 1.0 CG+O.J75 W2>+0.750 AL'> D +AD +CG + W2>+AL*> 30 System 1.000 1.0 D + l.OAD+ l.O CG +0.375 <W2 +0.750 <*AL D+AD+CG+<W2+<*AL 31 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 <W2+ 0.750 <AL' D + AD+ CG + <W2+<AL * 32 System 1.000 1.0 D + 1.0 AD+ l.OCG +0.150 S +0.750 E>+0.700 EG+ D+AD+CG+S+E>+EG+ 33 System 1.000 1.0 D+ 1.0 AD+ l.OCG +0.150 S +0.750 <E+ 0.700 EG+ D+AD+CG+S+<E+EG+ 34 System 1.000 .600 D +0.600 AD+ 0.600 CU + 0.700 E>+ 0.700 EG-D+AD+CU+E>+EG- 35 System 1.000 .600 D +0.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-D+AD+CU+<E+EG- 36 System Derived 1.000 1.0 D+ l.OAD + 1.0 CG +0.150 S+0.750EB>+0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 0.600 D +0.600 AD+0.600CU +0.700 EB>+0.700 EG-D+AD+CU+EB>+EG- 38 System Derived 1.000 1.0 D + l.OAD + LO CG + 0.150 S +0.750<EB +0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived 1.000 0.600 D +0.600 AD+0.600CU + 0.700<EB +0.700 EG-D+AD+CU+<EB+EG- 40 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA1 D+AD+CG+WPAl 41 System Derived 1.000 1.0 D +LOAD+ 1.0 CG +0.750 S +0.750 WPA1 D+AD+CG+S+WPAI 42 System Derived LOOO 0.600 D +0.600 AD+ 0.600 CU + LO WPA1 D +AD+ CU + WPA1 43 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPAI +0.750 *AL +0.750 ALB> D+AD+CG+WPAI+*AL+ALB> 44 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPAI +0.750 AL* +0.750 ALB> D+AD+CG+WPAI+AL*+ALB> 45 System Derived 1.000 LO D+ LOAD+ 1.0 CG + 1.0 WPDI D+AD+CG+WPDl 46 System Derived 1.000 1.0 D +LOAD+ 1.0 CG +0.750 S + 0.750 WPD1 D+AD+CG+S+WPDI 47 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPDI D+AD+CU+WPDl 48 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG + 0.375 WPDI + 0.750 *AL +0.750 <ALB D+AD+CG+WPD 1 +"' AL +<ALB 49 System Derived 1.000 l.O D + 1.0 AD+ 1.0 CG + 0.375 WPDI + 0.750 AL* +0.750 <ALB D+AD+CG+WPDI+AL*+<ALB 50 System Derived 1.000 1.0 D +LOAD+ LO CG + LO WPA2 D+AD+CG+WPA2 51 System Derived 1.000 1.0 D +LOAD+ 1.0 CG + 0.750 S + 0.750 WPA2 D+AD+CG+S+WPA2 52 System Detived LOOO 0.600 D + 0.600 AD +0.600 CU + LO WPA2 D +AD+ CU + WPA2 53 System Derived 1.000 1.0 I.)+ 1.0 AD+ 1.0 CG +0.375 WPA2 +0.750 *AL +0.750 ALB> D+AD+CG+WPA2+* AL +ALB> 54 System Derived LOOO 1.0 D + \.0 AD+ 1.0 CG +0.375 WPA2 +0.750 AL * +0.750 ALB> D+AD+CG+WPA2+AL*+ALB> 55 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPD2 D+AD+CG+WPD2 56 System Derived LOOO LO D +LOAD+ 1.0 CG +0.750 S + 0.750 WPD2 D + AD+CG +S+ WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPD2 + 0.750 *AL + 0.750 <ALB D+AD+CG+WPD2+* AL +<ALB 59 System Derived LOOO 1.0 D + \.0 AD+ I .0 CG + 0.375 WPD2 + 0.750 AL * + 0.750 <ALB D+AD+CG+WPD2+AL *+<ALB File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10(20(2008 Time: I :57:43 PM Page: 140of 175 60 System Derived 1.000 61 System Derived LOOO 62 System Derived LOOO 63 System Derived LOOO 64 System Derived LOOO 65 System Derived LOOO 66 System Derived LOOO 67 System Derived LOOO 68 System Derived LOOO 69 System Derived LOOO 70 System Derived LOOO 71 System Derived LOOO 72 System Derived LOOO 73 System Derived LOOO 74 System Derived LOOO 75 System Derived LOOO 76 System Derived 1.000 77 System Derived LOOO 78 System Derived LOOO 79 System Derived LOOO 80 System Derived LOOO 81 System Derived LOOO 82 System Derived LOOO 83 System Derived LOOO 84 System Derived LOOO 85 System Derived 1.000 86 System Derived LOOO 87 System Derived LOOO 88 System Derived LOOO 89 System Derived LOOO F M b s· rame em er IZCS Mem. Fig Width FlgThk No. -(in.) (in.) 1 6.00 0.5000 2 6.00 0.5000 3 6.00 0.5000 4 6.00 0.5000 5 6.00 0.5000 6 6.00 0.5000 B C dil S oundarv 1 on ton umma LOD+ LOAD+ LO CG + 1.0 WPB I l.OD+ LOAD+ LO CG + 0.750 S + 0.750 WPBI .600 D + 0.600 AD +0.600 CU + 1.0 WPBI I.OD+ LOAD+ I.OD+ I.OAD+ l.OD+ LOAD+ I.OD+ LOAD+ LO CG + 0.375 WPBI + 0.750 'AL + 0.750 ALB> 1.0 CG + 0.375 WPBI + 0.750 AL' +0.750 ALB> 1.0 CG + 1.0 WPC I 1.0 CG+0.750 S + 0.750 WPCI 0.600 D + D.600 AD+ 0.600 CU + 1.0 WPC! I.OD+ LOAD+ I.OD+LOAD+ l.OD+l.OAD+ LOD+l.OAD+ 1.0 CG + 0.375 WPCI + 0.750 *AL +0.750 <ALB LOCO +0.375 WPCl +0.750 AU+ 0.750 <ALB 1.0 CG + LO WPB2 LO CG + 0.750 S + 0.750 WPB2 0.600 D + D.600 AD+ 0.600 CU + LO WPB2 l.OD+ LOAD+ l.OD.+!.OAD+ LOD+ LOAD+ 1.0 D+ LOAD+ 1.0 CG + 0.375 WPB2+ 0.750 'AL +0.750 ALB> 1.0 CG +0.375 WPB2 +0.750 AL* + 0.750 ALB> 1.0 CG + 1.0 WPC2 1.0 CG + 0.750 S + 0.750 WPC2 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 I.OD+ LOAD+ l.OD+I.OAD+ I.OD+LOAD+ 1.0 CG + 0.375 WPC2 + 0.750 *AL +0.750 <ALB l.O CG +0.375 WPC2 +0.750 AL* + 0.750 <ALB l.O CG + LO S + l.O ALB> I.OD+LOAD+ I.OD+ LOAD+ l.OD+ LOAD+ LOD+LOAD+ LOD+ LOAD+ I.OD+ LOAD+ LOD+ LOAD+ LOD+ LOAD+ I.OD+LOAD+ l.OCG+ 1.0 *AL+ l.OALB> 1.0 CG + LO AL * + 1.0 ALB> I.OCG +0.563 S +0.750 *AL+0.750 ALB> LO CG+0.563 S +0.750 AL' +0.750 ALB> LO CG + 1.0 S + LO <ALB 1.0 CG+ 1.0 *AL+ 1.0 <ALB l.O CG + 1.0 AL * + 1.0 <ALB 1.0 CG +0.563 S +0.750 *AL +0.750 <ALB t,.O CO +0.563 S + 0.750 AL* + 0.750 <ALB WebThk Depth I Depth2 Length Weight FlgFy (ftl On.) (in.) (in.) 02l (ksi) 0.2500 12.00 44.00 31.03 1276.1 55.00 0.2500 48.00 24.00 17.79 974.2 55.00 0.1644 24.00 28.00 10.00 343.6 55.00 0.1644 28.00 24.00 10.00 343.5 55.00 0.2500 24.00 48.00 17.79 974.2 55.00 0.2500 12.00 44.00 31.03 1272.7 55.00 Total Frame We1ght-5184.4 (p) Frame Pricing Weight= 5725.8 (p) Member X-Loc Y~Loc Supp. X Supp.Y Moment Displacement X( in. 1 0/010 0/0/0 Yes Yes No 01010 6 531010 01010 Yes Yes No 01010 2 51610 33110/0 Yes Yes Yes 0/0/0 5 4716/0 33110/0 Yes Yes Yes 010/0 Values shown are resisting forces of the foundation. Reactions-Uf Ld F C S 7 n actored oa Typ~ at rame ross ecbon: Type Exterior Column Exterior Column XwLOC 01010 53/0/0 Grid 1 -Grid2 7-D 7-A Base Plate W x. L (in.) 8 X. 13 8 X. 13 Base Plate Thickness (in.) 0.500 0.375 Anchor Rod Qty/Diam. (in.) 4-0.750 4-0.750 Column Base Elev. 100'-0" 100'-()" Load Type Desc. Hx Hz Vy_ Hx Hz Vv D Fnn 0.8 -4.3 -0.8 4.3 AD Fnn 0.1 -1.1 -0.1 -1.1 - C'G Frm 2.6 12.3 -2.6 10.1 s Frm 9.8 -38.3 ·9.8 -38.3 US I* Frm 8.8 22.7 ·8.8 -46.2 *US I Fnn 8.8 46.2 -8.8 -22.7 WI> Fnn ·6.9 ·11.9 -4.6 -4.3 File: 7079 Chevron RJ_Stress Check 10_2008 with 08_2008 Loading D+AD+CG+WPBl D+AD+CG+S+WPBl D+AD+CU+WPB! D+AD+CG+WPBI+*AL+ALB> D+AD+CG+WPB lfAL *+ALB> D+AD+CG+WPC! D+AD+CG+S+WPCI ) D+AD+CU+WPCl D+AD+CG+WPCl+*AL+<ALB D+AD+CG+WPCl+AL*+<ALB D+AD+CG+WPB2 D+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+AL *'+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2 D +AD+ CU + WPC2 D+AD+CG+WPC2+*AL+<ALB +AD+CG+WPC2+AL *+<ALB D +AD+ CG + S+ALB> D+AD+CG+*AL+ALB> +AD+CG+AL*+ALB> +AD+CG+S+*AL+ALB> +AD+CG+S+AL*+ALB> D +AD+ CG + S+<ALB +AD + CG+* AL+<ALB +AD+ CG+AL *+<ALB +AD+CG+S+*AL+<ALB D+AQ+CG+S+AL *+<ALB Webfy Splice (ksi). It.! 55.00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP (Includes all plates) (Includes all pieces) Codes Jt.2 " KN ~s p ss KN KN Shape 3P 3P 3P 3P 3P 3P Displacement Y(in.) Displacement ZZ rad.) 0/010 0.0000 0/010 0.0000 0/0/0 0.0000 0/0/0 0.0000 -- -- - - - - Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 141 of175 <WI Fnn 4.6 --4.3 6.9 -11.9 W2> Fnu -8.3 -8.1 -3.2 -0.4 <W2 Fnn 3.2 --0.4 8.3 -8.1 - 'AL> Frm -0.1 -10.0 -1.8 4.7 - AL*> F•m -0.1 -2.7 -1.8 -12.0 - <*AL Frm 1.8 12.0 0.1 2.7 <AL* Frm 1.8 -4.7 0.1 -10.0 - cu F•m 1.3 5.1 -1.3 -5.1 --- E> Fnu -4.2 -5.5 -4.1 5.5 EG+ Frm 0.3 -1.5 -0.3 -1.3 - <E Frm 4.2 -5.5 4.1 -5.5 - EG-Frm -0.3 -1.5 0.3 --1.3 EB> Brc 0.4 -16.2 -28.9 -0.4 -16.3 -29.1 <EB Brc -0.3 32.3 0.3 32.4 WPAl Bro 2.6 -3.7 -14.1 -2.3 -3.2 -13.0 'AL Frm 0.9 -11.0 -0.9 -3.7 - ALB> Brc ----- AL' Fnn 0.9 3.7 -0.9 J 1.0 - WPDJ Brc 1.9 --2.9 -1.4 --3.2 - <ALB Brc --- - -. . WPA2 Brc 1.2 ·3.7 -10.3 -0.9 -3.2 -9.2 - WPD2 Brc 0.5 . 0.9 -0.0 . 0.6 -. . WPBJ Brc 2.3 -3.2 -13.0 ·2.6 -3.7 -14.2 . . . WPCJ Brc 1.4 . -3.2 -1.9 . -2.9 . - WPB2 Brc 0.9 -3.2 ·9.2 -1.2 -3.7 .JQ.4 . . WPC2 Brc 0.0 . 0.6 -0.5 . 0.9 . . . Maximum Combined Reactions Summarv with Factored-Loads~ Framinu X-Loc Grid Hrz left Load :fin.: Right Load Hrzln Lo11d Hrr.Q;t Load Uplift Lond V1t Down '-"":romcw Lend Momccw I ood (-Hx) Case (Hx) . Case (-Hz) Case (i;lz) Case (-Vy) Case (Vy) Cn<:c (-Mzz) Case (Mzz) Case (k) (k) (k) (k) (k) (~ (m-k) ---..J~'·k) -0/0/0 7-D 7.0 18 14.3 9 12.2 36 . . 15.0 37 63.9 -~ 1-·:- 53/0/0 7-A 14.3 8 7.0 19 12.2 36 . 'i't . 15.0 37 618 . Sum of Forces with Reactions Checkr\ Framin!! •. Horizontal Vertical Load Type Load Reaction Load Re~~ion (k) (k) (Jd D 0.0 0.0 8.8 8.7 AD 0.0 0.0 2.3 2.2 CG 0.0 0.0 22.4 22.4 s 0.0 0.0 76.5 76.5 USI* 0.0 0.0 68.9 68.9 "'USl 0.0 0.0 68.9 68.9 WI> 11.5 11.5 16.2 16.2 <WI 1 1.5 11.5 16.2 16.2 W2> 11.5 11.5 8.6 8.6 <W2 J 1.5 11.5 8.6 8.6 'AL> 1.9 1.9 15.5 14.7 AL*> 1.9 1.9 15.5 14.1 <*AL 1.9 1.9 15.5 14.7 <AL* 1.9 1.9 15.5 14.7 cu 0.0 0.0 10.2 10.2 E> 8.3 . 8.3 0.0 0.0 EG+ 0.0 o.o 2.9 2.9 <E 8.3 8.3 0.0 0.0 EG-0.0 0.0 2.9 2.9 EB> 0.0 0.0 0.0 58.0 <EB 0.0 0.0 0.0 64.7 WPAI 0.3 0.3 14.8 27.2 'AL 0.0 0.0 15.5 14.7 ALB> 0.0 0.0 0.0 0.0 AL' 0.0 0.0 15.5 14.7 WPDI 0.5 0.5 19.9 6.2 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM 142of175 WPA2 0.3 0.3 7.2 19.5 WPD2 0.5 0.5 12.3 1.4 WPBI 0.3 0.3 14.8 27.2 WPCI 0.5 0.5 19.9 6.2 WPB2 0.3 0.3 7.2 19.5 WPC2 0.5 0.5 12.3 !.4 B PI t S ase •• ummarv X~Loc Grid Mem. Thickness Width Length Num.Of BoltDiam. Type Welds to Welds to No. (in.) (in.) (in~) Bolts (in.) Flan"e Web 01010 7-D I 0.500 8 13 4 0.750 A36 OS-0.1875 OS-0.1875 5310/0 7-A 6 0.375 8 13 4 0.750 A36 OS-0.1875 OS-0.1875 Web Stiffener Summa Mem. Stiff. Desc. Loc. Web Depth hit alh a 1l1ick. Width Side Welding No. No. (ft) (in.)· (in.) (in.) (in.) Description 2 I S9 3.85 45.069 180.27 NIA NIA 0.5000 2.500 Both W-OS-0.1875 2 2 Sl 13.17 30.308 12!.23 3.00 90.78 0.2500 2.000 Both Std 5 I S9 13.94 45.069 180.27 NIA N/A 0.5000 2.500 Both W-OS-0.1875 5 2 Sl 12.29 42.460 169.84 3.00 127.00 0.2500 2.000 Both F-OS-0.1875,W-OS-0.1875 B S rackets Part umm~IT- Mem. Loc. Total Length Bracket Cut Bracket Fig Width Fli:Thk WebThk Hole Pitch Stiffener or Plate Part No. (ft) (in.) (in.) Deoth Cin.) (in.) (ln.) (in.) (in.) 2 3.99 15.500 4.750 10.000 6.000 0.2500 0.2500 3.500 UPo70411ooo WUI5441234 5 13.85 13.375 4.250 10.000 6.000 0.2500 0.2500 3.500 UP0704IIOOO WUI3340434 Brackets Desie:n Summarv (vertical live load Is with the lmoact factor Mem. Loc. Vert. Live Vert. Deml Literal r.ongitudina! CL Oi$-tto Member Member WcbThk Flg Thk Flg Wldt_h No. (ftP Load (k) Load (k) Im 'act (k) lill)OCt{k) Fk11;~c (in.) Depth! (i11.) Dcptl1::! (in.? (in.) (in.) (in.) 2 3.99 13.72 1.15 0 0.94 1.47 I 1.741 43.403 41.012 0.2500 0.5000 6.0000 5 D.R:5 13.72 !, 15 OJ>.: 1.47 11.74 J 42.01:2 42.40] 0.2500 {1 .. ~000 (,_()()(10 Bolted End-Plate Moment Connections (ATSC DCM16)-Fv"" 55 ksi End-Plate Dimensions Bolt Outside Flan~e Inside F!an)?;e Mem. Jt. Type Thick. Width Length Diam. Spec/Joint Gages In/Out Configuration Pitches Jst'l2ild Configttration Pitches 1st/2nd No. No. (in.) (in.) (in~) (in.) . . . (in.) ID Desc. (in.) ID Desc. (in.) I 2 KN(Top) 0.625 6.00 45.00 0.750 A325XIST 3.50 12 Flush 2.00 II F:Qsh 2.00 2 I KN(Top) 0.625 6.00 45.00 0.750 A325XIST 3.50 12 Flush 2.00 !I Flush 2.00 3 2 SP 0.375 6.00 33.00 0.750 A325XIST 3.00 II Flush 0.00 42 Ext/Gusset 3.6912.00 4 I I I 3.00 lu I Flush 0.00 . Required Strength -Out Available Strength M Out Required Strength -In Available Strength M In Mem. Jt. Ld Axial Shear Moment Design Shear Moment Ld Axial Shear Moment Design Shear Moment No. No. Cs (k) (k) (in-k) Proc. (k) _(in-k) Cs (k) (k) (in-k) Proc. (k) (in-k) I 2 2 -38.9 10.5 3585.5 Thin plate 159.0 2814.0 16 5.7 1.4 1126.2 Thick plate 106.0 1660.0 2 I 2 -38.9 10.5 3585.5 Thin plate 159.0 2814.0 16 5.7 1.4 1126.2 Thick plate 106.0 1660.0 3 2 17 3.1 3.6 17.6 Thin plate 106.0 574.5 I -13.0 3.3 1698.7 Thin plate 212.1 1547.4 4 I 17 3.1 3.6 17.6 Thin plate 106.0 574.5 I -13.0 3.3 1698.7 Thin plate 212.1 1547.4 5 2 3 -38.8 10.5 3550.5 Thin plate 159.0 2814.0 17 5.7 1.4 1126.2 Thick plate 106.0 1660.0 6 2 3 -38.8 10.5 3550.5 Thin plate 159.0 2814.0 17 5.7 1.4 1126.2 Thick plate 106.0 1660.0 F S la11:ge Brace ummary Member From Member Joint l From Side Point I Part Design Note I 121514 12/5/4 FB2110 I 221514 221514 SFB4034 I 27/514 27/514 (2)FB5040 2 2111/J 251214 (2)FB5114 3 2/610 719113 FB3030 3 81610 I/9/J3 FB3050 4 116/0 119/13 FB3050 5 61610 1619113 FB4060 File: 7079 Chevron Rl_Stress Check l0_2008 with 08_2008 Loading Version: 7.la 5 6 6 6 07-27053 Calculations Hazardous Materials Occupancy 14110/7 12/5/4 22/5/4 27/5/4 25/214 12/5/4 22/5/4 27/5/4 (2)FB5114 FB2110 FB4034 (2)FB5040 Date: 10/20/2008 Time: 1:57:43 PM Page: 143 of 175 ~ arne Design Member Summary-Controlling Load Case and Maximum Combined Stresses per Member (Locations are from Joint 1 ) Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear Mom-x Mom-y Axial Shear Bnd-X Bnd-Y ---Stress /Force ---Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear I 22.46 37.61 I -54.5 -10.8 -2940.8 o.c 3.60 !.I 18.9 0.00 25.11 3.8 26.10 41.25 0.85 0.30 2 !.61 47.39 2 -24.2 26.7 -3259.6 0.0 1.38 2.30 15.11 0.00 28.56 2.42 19.48 41.25 0.82 0.95 3 2.50 25.08 3 -13.9 2.9 2045A 0.0 1.39 0.72 25.02 0.00 29.89 3.87 32.69 41.25 0.81 0.19 4 7.11 25.08 2 -13.8 -2.8 2055.1 0.0 !.39 0.70 25.14 0.00 29.89 3.87 32.69 41.25 0.81 0.18 5 o.oo 24.00 2 -16.4 -7.5 1881.7 0.0 1.40 1.30 20.87 0.00 29.50 9.82 33.00 41.25 0.67 0.13 6 22.46 37.61 1 -54. 10.8 -2905.4 0.0 3.59 1.1 18.70 0.00 22.48 3.88 . 26.03 41.25 0.84 0.30 Mem. Loc. Depth Area Rx Ry Lx Ly-1 Ly-2 Klx Klyl Kly2 Sx Lbl Rt-1 Lb2 Rt-2 Qs Qa Cbl Cb2 No. ft in. in.2 in. in. in. in. in. /Rx /Ry /Rv in.3 in. in. in. in. 1 22.46 37.61 15.15 14.27 1.09 336.87 30.0 60.1 35.4 27.5 55.0 155.38 120.1 1.46 60.1 1.44 1.00 0.86 1.27 1.09 2 1.61 47.39 17.60 17.48 1.01 298.83 4.7 28. 17.1 4. 28.1 215.79 4.7 1.37 172.8 1.40 1.00 0.95 1.0 1.81 3 2.50 25.08 9.96 10.50 1.3 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 !.00 1.00 1.05 1.01 4 7.11 25.08 9.96 10.50 1.34 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 1.00 1.00 1.01 1.05 5 0.00 24.00 11.75 9.60 1.24 298.83 36.0 0.0 31.1 29.1 0.0 90.16 36.0 1.55 0.0 0.00 1.00 1.00 1.05 0.00 6 22.4 37.61 15.15 14.27 1.09 336.87 60.1 60.1 35.4 55.0 55.0 155.38 120.1 1.46 60.1 1.44 1.00 0.86 1.26 1.09 File: 7079 Chevron R1_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 144ofl75 User Defined Frame Point Loads for Cross Section-7 Side Units Type Description Magi Locl Offset HotV Supp. Dir. Coef. Loc. I k CG PS~4l Pipe Loads -1.70 20/816 -2/310 Holiz. N DOWN !.000 OF I k CG PS-46 Pipe Loads -0.30 1617/3 3/3/0 Horiz. N DOWN 1.000 IF y X Deflection Load Combinations -Framln No. Orhrin Factor DefH DefY Aoolication Description I System 1.000 0 240 1.0 s s 2 System 1.000 0 240 1.0 US\* US I* 3 System 1.000 0 240 !.0 *USI *US! 4 System 1.000 0 240 0.700 Wl> WI> 5 System 1.000 0 240 0.700<WI 0 <WI ) 6 System 1.000 0 240 0.700 W2> W2> ' 7 System -1.000 . 0 240 ~J.700 <W2 W2 8 System Derived 1.000 0 240 0.700 WPAI " WPAJ· 0 9 System Derived 1.000 0 240 0.700WPDI WPDI IO System Derived 1.000 0 240 0.700 WPA2 WPA2 I 1 System Derived 1.000 0 240 0.700 WPD2 WPD2 12 System Derived 1.000 0 240 0.700WPB1 WPBJ 13 System Derived 1.000 0 240 G.700WPCI WPCI 14 System Derived 1.000 0 240 0.700WPB2 WPB2 IS System Derived 1.000 0 240 0.700WPC2 WPC2 I6 System 1.000 400 0 0.700Wl> WI> I7 System I.ooo 400 0 0.700<Wl <WI I8 System 1.000 400 0 0.700 W2> W2> 19 System 1.000 400 0 0.700<W2 W2 20 System Derived 1.000 400 0 0.700WPA1 WPAI 21 SyStem Derived 1.000 400 0 0.700WPDI WPDJ 22 System Derived 1.000 400 0 0.700 WPA2 WPA2 23 System Derived 1.000 400 0 0.700 WPD2 WPD2 24 System Derived 1.000 400 0 0.700 WPBI WPBJ 25 System Derived 1.000 400 0 0.700 WPCI WPCJ 26 System Derived 1.000 400 0 0.700WPB2 WPB2 27 System Derived 1.000 400 0 0.700WPC2 WPC2 28 System 1.000 100 0 0.600 E> +0.700 EG-E>+EG- 29 System 1.000 100 0 0.600 <E + 0.700 EG-E+EG- 30 System Derived 1.000 100 0 o.600 EB> EB> 31 System Derived 1.000 100 0 0.600 <EB f'EB 32 System 1.000 400 0 1.0 <AL* AL* 33 ~y§_tem 1.000 400 0 1.0 *AL> *AL> c F fl on trolling rame De ect on R ' I C attos or ross s ection: 7 Description Ratio Deflection in.) Member Joint Load Case Load Case Description Max. Horizontal Deflection ( H/431) -0.819 6 2 19 <W2 Max. Ve1tica! Denection for Span I ( L/568) -1.033 3 2 I s File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy * Negative horizOntal deflection is left * Negative vertical deflection is down Date: 10/20/2008 Time: I :57:43 PM Page: l45ofl75 Lateral deflections of primary frames are calculated on a bare frame basis and do not include resistance from systems such as roof and endwall diaphragms. Therefore, these deflections may be considerably overstated. ) 0 0, File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading VersiOn: 7.!a 07-27053 Calculations Hazardous Materials Occupancy . X FRAME CROSS SECTION AT FRAME LINE(S) 8 Dimension Key 1 5'-6" BL toCL of Runway Beam 2 1 5/8" 3 4'..1)" 4 3'-5 1/4" 5 3'~3 3/4" 6 1'-3" 7 1'-9 13116" 8 Z@ Z'-4 7116" 9 4 1/Z" 10 40'-10" Ridge Ht. Frame Clearances Horiz. Clearance between members J(CXOOO) and 6(CXOOO): 45'-4 3/4" File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 c 07-27053 Calculations Hazardous Materials Occupancy Ve!t, Clearance at member l(CXOOO): 28'-0 1/2" Vert. Clearance at member 6(CXOOO): 28'..0 112" Finished Floor Elevation= 100'-0" (Unless Noted Othetwise) Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA l·l(Left): zq 3/16" Horz. Clearance at CRANE DATA l·l(Left): 1 '·10 1/8" Vert. Clearance at CRANE DATA 1-l(Right): 2~4 3/16" Horz. Clearance at CRANE DATA 1-l(Right): 1 -10 1/8" 0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading 0 Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: !47of 175 0. 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 148ofl75 Descri tion An le Grou Desi Status Ri id Frame 90.0000 Stress Check Desi n Load Combinations ~ Framin No. Origin Factor Annlication Description I Systel',} 1.000 I.OD+ LOAD+ I.OCG+ !.OS :!) D+AD+CG+S 0 2 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 US!* D +AD+ CO+ USl * 3 System 1.000 1.0 D + 1.0 AD+ 1.0 CO+ LO *US\ D+AD+CG+*USI 4 System 1.000 1.0 D +LOAD+ 1.0 CG + 1.0 WI> D+AD+CG+Wl> 5 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <WI P+AD+CG+<Wl 6 System 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 W2> D+AD+CG+W2> 7 System 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 <W2 D+AD+CG+<W2 8 System 1.000 LO D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 WI> D+AD+CG+S+Wl> 9 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 <WI D+AD+CG+S+<Wl 10 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 W2> D+AD+CG+S+W2> II System 1.000 1.0 D +LOAD+ 1.0 CG + 0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System 1.000 LO D + l.O AD+ 1.0 CG+ l.O '"AL> D +AD+ CG+*AL> 13 System 1.000 LOD+ LOAD+ LOCO+ l.OAL*> D+AD+CG+AL*> 14 System LOOO 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <*AL D+AD+CG+<*AL 15 System LOOO 1.0 D +LOAD+ 1.0 CG + LO <AL* D+AD+CG+<AL* 16 System 1.000 Q.600 D + Q.600 AD+ 0.600 CU + LO WI> D+AD+CU+W1> 17 System LOOO 0.600 D + 0.600 AD+ 0.600 CU + LO <WI D+AD+CU+<Wl 18 System LOOO 0.600 D + 0.600 AD+ 0.600 CU + 1.0 W2> D+AD+CU+W2> 19 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + LO <W2 D+AD+CU+<W2 20 System LOOO LO D + 1.0 AD+ LO CG +0.563 S +0.750 *AL> D+AD+CG+S+"'AL> 21 System LOOO 1.0 D + 1.0 AD+ LO CG +0.563 S +0.750 AL*> II?+ AD+ CG + S+AL*> 22 System LOOO 1.0 D +LOAD+ 1.0 CG +0.563 S +0.750 <*AL ·' D+AD+CG+S+<*AL 23 System 0 1.000 1.0 D +LOAD+ l.Ot:G +0.563 S + 0.750 <AL* , D+AD+CO+S+<AL* 24 System LOOO 1.0 D + 1.0 AD+ 1.0 CG +0.375 Wl>+ 0.750 *AL> D +AD+ CG + Wl>+*AL> 25 System LOOO l.O D + l.O AD+ 1.0 CO +0.375 WI>+0.750 AL*> D +AD+ CG + Wl>+AL*> 26 S~tem LOOO 1.0 D +LOAD+ 1.0 CO +0.375 <WI +0.750 <*AL D+AD+CG+<Wl+<*AL 27 System LOOO 1.0 D + l.O AD+ 1.0 CG +0.375 <Wl + 0.750 <AL* jo+AD+CG +<Wl+<AL* 28 System LOOQ 1.0 D + 1.0 AD+ t.O CG +0.375 W2>+0.750 *AL> D +AD+ CO+ W2>+*AL> 29 System 1.000 LO D + LOAD+ 1.0 CG + 0.375 W2> + 0.750 AL *> D+AD+CG +W2>+AL*> 30 System LOOO 1.0 D+ l.OAD + 1.0 CG+0.375 <W2 +0:750 <*AL D +AD + CG + <W2+<* AL 31 System 1.000 1.0 D+ l.OAD + 1.0 C0+0.375 <W2+0.750 <AL"' D+ AD+ CG +<W2+<AL* 32 System 1.000 1.0 D+ LOAD+ 1.0 CG+0.150 S+0.750 E>+0.700 EG+ io+AD+CG+S+E>+EG+ 33 System 1.000 LO D +LOAD+ LO CG +0.150 S +0.750 <E+0.700 EG+ D+AD+CG+S+<E+EG+ 34 System 1.000 0.600 D + Q.600 AD+ 0.600 CU + 0.700 E> + 0.700 EG-D+AD+CU+E>+EG- 35 System LOOO ~.600 D + Q.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-lo+AD+CU+<E+EG~ 36 System Derived 1.000 LO D+ LOAD+ 1.0 CG +0.150 S+0.750 EB>+0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 0,600 D + 0.600 AD+ 0.600 CU + 0.700 EB>;, 0.700 EG-D+AD+CU+EB>+EG~ 38 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.!50 S +0.750<EB +0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived 1.000 0.600 D + Q.600 AD+ 0.600 CU + 0.700 <EB + 0.700 EG· D+ AD+ CU +<EB +.EGw 40 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA1 D +AD+ CO+ WPAI 41 System Derived 1.000 LO D + 1.0 AD+ LO CG +0.750 S + 0.750 WPA1 D+AD+CG+S+WPAl 42 System Derived 1.000 0.600 D+0.600 AD +0.600 CU + 1.0 WPAI D +AD+ CU + WPAl 43 System Derived 1.000 1.0 D + 1.0 AD+ LO CG +0.375 WPAI +0.750 *AL + 0.750 ALB> D+AD+CG+WPAl+*AL+ALB> 44 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPAI +0.750 AL* + 0.750 ALB> io+AD+CG+WP A I +AL *+ALB> 45 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPDI D +AD+ CG + WPDI 46 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 WPDI D+AD+CG+S+WPDI 47 System Derived 1.000 r.600 D + o.600 AD+ 0.600 CU + 1.0 WPDI D +AD+ CU + WPDI 48 System Derived 1.000 1.0 D + l.O AD+ !.0 CG +0.375 WPDI + 0.750 *AL +0.750 <ALB D+AD+CG+WPD I+"' AL +<ALB 49 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDI + 0.750 AL* +0.750 <ALB D+AD+CG+WPD I+AL *+<ALB 50 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA2 D +AD+ CG + WPA2 51 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 WPA2 D+AD+CO+S+WPA2 52 System Derived 1.000 0.600 D + 0.600 AD+ 0.600CU + 1.0 WPA2 J?+AD+CU+WPA2 53 System Derived 1.000 1.0 D + l.O AD+ 1.0 CO+ 0.375 WPA2 + 0.750 *AL + 0.750 ALB> D+AD+CG+WPA2+*AL+ALB> 54 System Derived 1.000 LO D + 1.0 AD+ 1.0 CO+ 0.375 WPA2 + 0.750 AL* +0.750 ALB> D+AD+CG+WPA2+AL*+ALB> 55 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CO + l.O WPD2 D+AD+CG+WPD2 56 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPD2 D+AD+CO+S+WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU +I .0 WPD2 D+AD+C'U+WPD2 58 System Derived 1.000 1.0 D + \.0 AD+ \.0 CO+ 0.375 WPD2 +0.750 *AL + 0.750 <ALB D+AD+CG+WPD2+*AL+<ALB 59 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPD2 +0.750 AL* +0.750 <ALB D+AD+CG+WPD2+AL*+<ALB File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: ?.Ia 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 149 of 175 60 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 WPBJ 61 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPBI 62 System Derived 1.000 0.600 D +0.600 AD+ 0.600 CU + 1.0 WPBI 63 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPBI + 0.750 'AL +0.750 ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPBI +0.750 AL' +0.750 ALB> 65 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 WPCI 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPCI 67 System Derived 1.000 D.600 D +0.600 AD+ 0.600 CU + 1.0 WPCI 68 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPCI +0.750 'AL +0.750 <ALB 69 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPC! +0.750 AL* +0.750 <ALB 70 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 1.0 WPB2 71 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S +0.750 WPB2 72 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 73 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 + 0.750 *AL + 0.750 ALB> 74 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPB2 +0.750 AL* + 0.750 ALB> 75 System Derived 1.000 LO D + 1.0 AD+ LOCO+ LO WPC2 76 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 78 System Derived 1.000 1.0 D + 1.0 AD+ LO CG + 0375 WPC2 + 0.750 *AL + 0.750 <ALB 79 System Derived 1.000 1.0 I)+ LOAD+ LO CG +0.375 WPC2 + 0.750 AL* + 0.750 <ALI3 80 System Derived 1.000 l.OD +LOAD+ LOCG +LOS+ l.OALB> 81 System Derived 1.000 LO D +LOAD+ LO CG + 1.0 *AL + l.O ALB> 82 System Derived 1.000 LOD+ LOAD+ LOCG+ LOAL* + LOALB> 83 System Derived 1.000 1.0 D + 1.0 AD+ LOCO +0.563 S +0.750 'AL+ 0.750 ALB> 84 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 C0+0.563 S+0.750 AL' +0.750 ALB> 85 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CO+ 1.0 S + 1.0 <ALB 86 System Derived 1.000 l.OD+ LOAD+ LOCG+ l.O*AL+ LO<ALB 87 System Deriv'ed 1.000 LO D +tO AD+ 1.0 CG + 1.0 AL* + 1.0 <ALB 88 System Derived 1.000 LO D + 1.0 AD+ 1.0 CG +0.503 S +0.750 *AL + 0.750 <ALB 89 ~_y_:;tem Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.563 S + 0.750 AL * + 0.750 <ALI3 F rame '"' '" Mem. Fig Width FlgThk Web Thk Depth! Depth2 Length Weight Flg Fy No. lin.) iin.i lin.) fin.) lin.) rrii (p) lksil I 6.00 0.5000 0.2500 12.00 44.00 31.03 1278.0 55.00 2 6.00 0.5000 0.2500 48.00 24.00 17.79 974., 55.00 3 6.00 0.5000 0.1644 24.00 28.00 10.00 343.6 55.00 4 6.00 0.5000 0.1644 28.00 24.00 10.00 31;1.5 55.00 5 6.00 0.5000 0.2500 24.00 48.00 17.79 974.2 55.00 6 6.00 0.5000 0.2500 12.00 44.00 31.03 1278.0 55.00 -TotalFrameWetght-5191.5 (p) Frame Pricing Weight= 5739.5 (p) Boundary Condition Summa y Member X~Loc Y~Loc Suoo.X Supp. Y Moment Displacement Xfin.) I 0/0/0 0/0/0 Yes Yes No 0/0/0 6 53/0/0 0/0/0 Yes Yes No 0/0/0 2 5/6/0 33/10/0 Yes Yes Yes 0/0/0 5 47/6/0 33/10/0 Yes Yes Yes 0/0/0 Values shown are resisting forces of the foundation. ReactionS-Unfactored Load Type at Frame Cross Section: 8 Type Exterior Column Exterior Column X~Loc 0/0/0 53/010 Grid l ~ Grid2 8-D 8-A Base Plate W x L (in.) 9x 13 9x 13 Base Plate Thickness (in.) 0.500 0.500 Anchor Rod Qty/Diam. (in.) 4-1.000 4-1.000 Column Base Elev. \00'~0" 100'-0" Load Type Desc. Hx Hz Vy Hx Hz Vy D Fnn 0.8 -4.3 -0.8 -4.3 AD Fnn 0.1 1.1 -0.1 -1.1 - CO Fnn 2.6 -\2.0 -2.6 \0.1 - s Fnn 9.8 38.3 -9.8 -38.3 - US!* Fnn 8.8 -22.7 ·8.8 46.2 - *US\ Fnn 8.8 46.2 -8.8 22.7 - WI> Fnn -6.9 -12.0 -4.6 -4.3 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading D+AD+CG+WPBJ D +AD+ CO+ S + WPBl D +AD+ CU + WPBI lo+AD+CG+WPBl+*AL+ALB> D+AD+CG+WPBJ+AL*+ALB> D+AD+CG+WPCl D+AD+CG+S+WPCI p+AD+CU+WPCI fo+AD+CG+WPCl+*AL+<ALB !D+AD+CG+WPC!+AL *+<ALB D+AD+CG+WPB2 D +AD+ CG +S + WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+AL *+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2 D+AD+CU+WPC2 D+A D+CG+WPC2+* AL +<ALB D+AD+CG+WPC2+AL *+<ALB D+AD+CG+S+ALB> D+AD+CG+*AL+ALB> In+ AD+ CG+AL*+ALB> !o+AD+CG+S+* AL +ALB> f!?+AD+CG+S+AL*+ALB> iD + AD+ CG + S+<ALB D+.AD+CG+*AL+<ALB D +AD+ CG+AL *+<ALB D·iAD+CG+S-I:"'AL +<ALB D+,\D+CG+S+AL*+<ALB \Neb Fy Splice (ksi) JLI 55.00 UP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP (Includes all plates) (Includes all pieces) Codes Jt.2 KN ss SJj ss KN KN Shnpc JP JP 3P 31:) 3P 3P Displacement Y in.) Displacement ZZ rad.) 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 - -- - - - - Version: 7.1a c 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM 150ofl75 <WI Fnn 4.6 --4.3 6.9 -12.0 --- W2> Fnn -8.3 --8.1 -3.2 -0.4 --- <W2 Frm 3.2 --0.4 8.3 --8.1 --- *AL> Fnn -0.1 -10.0 -1.8 4.7 - AL*> Fnn -0. I -2.7 -1.8 -12.0 -- <*AL Frm 1.8 -12.0 0.1 -2.7 --- <AL* Fnn 1.8 4.7 0.1 -10.0 --- cu Frm 1.3 -5.1 -1.3 5.1 --- E> Frm -4.2 -5.5 -4. I 5.5 --- EG+ Frm 0.3 -1.5 -0.3 -1.3 -- <E Fnn 4.2 5,5 4.1 -5.5 - EG-Fnn -0.3 --1.5 0.3 --1.3 -- EB> Brc -0.3 -0.0 29.0 0.3 -0.0 29.0 -- <EB BrC 0.5 19.3 -32.4 -0.5 19.3 -32.3 - WPAJ Brc 2.4 --1.0 -2.1 --1.5 --- 'AL Fnn 0.9 11.0 -0.9 -3.7 ALB> Brc - - ------ AL' Fnn 0.9 -3.7 -0.9 -11.0 -- WPDI Brc 2.1 4.4 -17.6 -1.6 3.8 -16.1 -- <ALB Brc --- ---- WPA2 Brc 1.0 -2.8 -0.7 -2.3 -() -- WPD2 Brc 0.7 4.4 -13.8 -0.2 3.8 -12.3 --- WPBI Brc 2.1 --1.5 -2.4 --1.0 --- WPCI Brc 1.6 3.8 -16.1 -2.1 4.4 -17.6 --- WPB2 Brc 0.7 -2.3 -1.0 -2.8 --- WPC2 Brc 0.2 3.8 -12.3 -0.7 4.4 -13.8 --. - i\·lnximum Combined Reactions Summarv with F:lc!On'd J.,,ads-F'r:unirti! . X-Loc Gt·iU Hrz !eft Load Hr;; Right Loud Hrz Jn Lond ! lrz Out L\Xll! Uplirt LDa,l Vn Do\1 n r .• Jad ivh.•m~:w Lo:•~l~!·.·m t:(,,., :.~•.1d f (-Hx) Case (Hx) Case ,(-Hz) case (Hz) Case (-Vy)., Cri.~e (Yy) sasc ( -~1zz) Case I; (Mzz) C<l::c, I (k) (k) (k) (k) (k) (k) (in-k) J (in-k) 0/0/0 8-D 7.0 18 14.3 9 0.0 36 14.4 38 I 7.4 39 63.6 3 -: I -- 53/0/0 8-A 14.3 8 7.0 19 0.0 36 14.5 38 J7.2 39 61.7 2 --. - Sum of Forces with Reactions Check-Framh1<1 .. Horizontal ) Vertical Load Type L~~d Reacti011 L~~d Reaction (k) (kl 0 D ·0.0 0.0 8.8 8.7 AD o.o 0.0 2.3 2.2 CG 0.0 0.0 22.1 22.1 s 0.0 0.0 76.5 76.5 USl* o.o 0.0 68.9 68.9 *USI 0.0 0.0 68.9 68.9 WI> 11.5 11.5 16.2 16.2 <WI 11.5 11.5 16.2 16.2 . W2> 11.5 11.5 8.6 8.6 <W2 11.5 11.5 8.6 8.6 *AL> 1.9 1.9 15.5 14.7 AL"'> 1.9 1.9 15.5 14.7 <*AL 1.9 1.9 15.5 14.7 <AL* 1.9 1.9 15.5 14.7 cu 0.0 0.0 10.2 10.2 E> 8.2 8.3 0.0 0.0 EG+ 0.0 0.0 2.8 2.8 <E 8.2 8.3 0.0 0.0 EG-0.0 0.0 2.8 2.8 EB> 0.0 0.0 0.0 58.0 <EB 0.0 0.0 0.0 64.7 WPAI 0.3 0.3 14.8 2.5 *AL 0.0 0.0 15.5 14.7 ALB> 0.0 0.0 0.0 0.0 AL' 0.0 0.0 15.5 14.7 WPDI 0.5 0.5 19.9 33.7 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 151 of 175 WPA2 0.3 0.3 7.2 5.2 WPD2 0.5 0.5. 12.3 26.1 WPB1 0.3 0.3 14.8 2.5 WPCI 0.5 0.5 19.9 33.7 WPB2 0.3 0.3 7.2 5.2 WPC2 0.5 0 .. 5 12.3 26.1 B PI t S ase ae ummarv X~Loc Grid Mem. Thickness Width Length Num.Of Bolt Diam. Type Welds to Welds to No. (in.) (in.) (in~) Bolts (in.) Flange Web 01010 8-D 1 0.500 9 13 4 1.000 A36 OS-0.1875 OS-0.1875 53/010 8-A 6 0.500 9. 13 4 1.000 A36 OS-0.1875 OS-0.1875 Web Stiffener Summar Mem. Stiff. Desc. Loc. Web Depth h/t .~, a Tilick. Width Side Welding No. No. (ft) (in.), (in.) (in.) (in.) Description 2 1 S9 3.85 45.069 180.27 N/A NIA 0.5000 2.500 Both W-OS-0.1875 2 2 S1 13.17 30.308 121.23 3.00 90.78 0.2500 2.000 Both Std 5 I S9 13.<14 45.069 180.27 N/A NIA 0.5000 2.500 Both W-OS-0.1875 5 2 S1 12.29 42.460 169.84 . 3.00 127.00 0.2500 2.000 Both F-OS-0.1875,W-O!l;O.J875 . Brackets Part Summary_ . Mem. Loc. Total ~ngth Bracket Cut Bracket FlgWidth FlgThk WebThk Hole Pitch Stiffener or Plate Part No. (ft) fin. lin.) Denth (in.) "nn.l iin.) (in,) lin.) 2 3.85 10.250 4.875 10.000 6.000 0.2500 0.2500 3.500 UP070411000 WU10241434 5 13.89 12.000 4.750 10.000 6.000 0.2500 0.2500 3.500 UP070411000 WU12041234 . Bolted Eml·Piate Moment ConnecttHJS (AJSC DG·16)-f'v"" 55 ksl . End-Plate Dimensions Bo!t Outside F1anue 3 InSide nan!.!~ Mem. Jt. Type Thick. Width Length N67 No. (in.) (in.) (in~) 1 2 KN(Top) 0.625 6.00 45.00 2 1 KN(Top) 0.625 6.00 45.00 3 2 SP 0.375 6.00 33.00 4 I 1 I Required Strength ~Out Mem. Jt. Ld Axial Shear Moment No. No. Cs (k) (k) (in-k) I 2 2 -39.0 10.5 3596.7 2 I 2 -39.0 10.5 3596.7 3 2 17 3.1 3.6 17.8 4 I 17 3.1 3.6 17.8 5 2 3 -38.8 10.5 3543.5 6 2 3 -38.8 10.5 3543.5 Flan,!!e Brace Summary Member From Member Joint 1 1 12/5/4 1 2'}}5/4 I 27/5/4 2 2/lJ/l 3 21610 3 8/6/0 4 1/6/0 5 61610 Diam. Spec/Joint Gages In/Out Confiouration Pitches !sll2nd (in.) ~ (in.) 1D Des c. ) in.) 0.750 A325X/ST 3.50 12 Flush 2.00 0.750 A325X/ST 3.50 12 Flush 2.00 0.750 A325X/ST 3.00 11 Flush 0.00 3.00 111 I Flush 0.00 Available Strength~ Out Design Shear Moment Ld Pro c. (k) (in-k) Cs Thin plate 159.0 2814.0 16 Thin plate 159.0 2814.0 16 Thin plate 106.0 574.5 1 Thin plate 106.0 574.5 1 Thin plate 159.0 2814.0 17 Thin plate 159.0 2814.0 17 . From Side Point l 12/5/4 22/5/4 27/5/4 25/2/4 7/9/l3 1/9/13 1/9/13 16/9113 2.00 2.00 Required Strength -In Axial Shear Moment (k) (k) (in-k) 5.7 1.4 ll27.8 5.7 1.4 ll27.8 -13.0 3.2 1699.4 -13.0 3.2 1699.4 5.7 1.4 1127.8 5.7 1.4 1127.8 Part FB2110 SFB4034 (2)FB5040 (2)FB5114 FB3030 FB3050 FB3050 FB4060 C'on1i2:urmion Pitches !·st/2nd ID Des.c. (in.) ~ " Flush 2.00 " Flush 2.00 42 Ext/Gusset 3.69/2.00 1421 Ext/Gusset! 3.69/2.00 Available Strengjh -In Design Shear Moment Proc. (k) (in-k) Thick plate 106.0 1660.0 Thick plate 106.0 1660.0 Thin plate 212.1 1547.4 Thin plate 212.1 1547.4 Thick plate 106.0 1660.0 Thick plate 106.0 1660.0 Design Note File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.Ja 0 '.) ) 5 6 6 6 07-27053 Calculations Hazardous Materials Occupancy 14/10/7 121514 221514 271514 251214 121514 ' 221514 271514 (2)FB5114 FB2110 FB4034 (2)FB5040 Date: 10/20/2008 Time: I :57:43 PM Page: 152 of 175 Frame Desil!n Member Summarv ~ Controlline Load Case and Maximum Combined Stresses oer Member (Locations are from Joint 1 ) Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear Mom~x Mom-y Axial Shear Bnd~X Bnd-Y '" Stress /Force "' Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear 1 22.46 37.61 I -54. -10.7 -2953.5 0.0 3.60 1,17 19.01 0.00 22.47 3.88 26.12 4L25 0.85 0,30 2 L61 4739 2 -24,2 26.7 -3269.5 0.0 ],38 2.31 15.15 0.00 28.56 2.42 19.47 4L25 0.82 0,95 3 2.50 25.08 3 -13.9 2.9 2043.1 0.0 ],3 0.73 24.9 0.00 29.89 3.87 32.69 41.25 0.81 OJ 9 4 7,11 25.08 2 -13.8 -2.7 2057.9 0.0 ],39 0.69 25.17 0.00 29.89 3.87 32.69 41,25 0.81 0.18 5 0.00 24.00 2 -16,4 -7.4 1885.1 0.0 L39 L29 20.91 0.00 29.50 9.82 33.00 4 L25 0.68 0.13 6 22.4 37.61 1 -54,4 10.8 -2899.7 0.0 3.59 Ll8 18.66 0.00 22.48 3.88 26,03 4L25 0.84 0.30 Mem. Loc. Depth Area Rx Ry Lx Ly-1 Ly-2 Klx K1y1 K1y2 Sx Lb1 Rt-1 Lb2 Rt-2 Qs Qa Cbi Cb2 No. ft in. in.2 in. in. in. in. in. !Rx fRy /Ry in.3 in. in. in. in. 1 22.46 37.61 15.15 14,27 1.09 336.87 60.1 60.1 35.4 55.0 55.0 155.38 120.1 L46 60.1 1.44 1.00 0.86 1.27 1.09 2 L61 47.3 17.6 17.48 1.01 298.8 4.7 28.5 17.1 4.6 28.1 215.79 4.7 1,37 172.8 1.40 LOO 0.95 1.02 1.81 3 2.50 25.08 9.96 10.50 ],3 298.83 36.0 36.0 28.5 26.8 26.8 81,76 36.0 1.61 36.0 1,61 1.00 1.00 1.05 1.01 4 7.11 25.08 9.9 10.50 1,34 298.83 36.0 36.0 28.5 26.8 26.8 81.76 36.0 1.61 36.0 1.61 1.00 1.00 1.01 1.05 5 0.00 24.00 11.75 9.60 1.24 298.83 36.0 0.0 3Ll 29.1 0.0 90.16 36.( 1.55 0.0 0.00 LOO 1.00 1.05 0.00 6 22.46 37.61 15.15 14.27 1.09 336.87 60.1 60.1 35.4 55.0 55.0 155.38 120.1 1.46 60:1 1.44 1.00 0.86 L26 L09 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.\a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 153 of 175 User Defined Frame Point Loads for Cross Section: 8 Ma I Locl Offset H orV Su Dir. Coef. Loc. -!.70 20/8/6 -2/3/0 Horiz. N DOWN !.000 OF y X on e ection L d oa Combmat10ns ~ F ramm No. Origin Factor DefH DefV · ,Application Description I System 1.000 0 240 !.0 s . ~ 2 System !.000 0 240 1.0 USI"' US I• 3 System !.000 0 240 l.O *USl *US I 0 4 System !.000 0 240 0.700 WI> WI> 5 System !.000 0 240 .700 <WI WI 6 System !.000 0 240 0.700 W2> W2> 7 System !.000 0 240 0.700<W2 <W2 8 System Derived 1.000 ~ 240 0.700 WPA1 WPA1 9 System Derived 1.000 240 .700 Wl'D1 , 0 WPDI 10 System Dcri'J:'d 1.000 0 . 240 0.700 WPA2 " WPA2 11 System Derived 1.000 0 240 0.700 WPD2 WPD2 12 System Derived 1.000 0 240 0.700 WPBI WPBI I3 System Derived 1.000 0 240 .700WPCI WPCI 14 System Derived 1.000 0 240 0.700WPB2 WPB2 IS System Derived 1.000 0 . 240 0.700WPC2 WPC2 I6 System 1.000 400 0 0.700 WI> WI> 17 System 1.000 400 0 0.700 <Wl <WI 18 System 1.000 400 0 . 0.700W2> W2> I9 System 1.000 400 0 0.700<W2 W2 20 System Derived 1.000 400 0 0.700WPA1 WPAI 21 System Derived 1.000 400 0 0.700 WPD1 WPD1 22 System Derived 1.000 400 0 0.700WPA2 WPA2 23 System Derived !.000 400 0 0.700WPD2 WPD2 24 System Derived 1.000 400 0 0.700WPB1 WPB1 25 System Derived 1.000 400 0 0.700WPC1 WPC1 26 System Derived 1.000 400 0 0.700 WPB2 WPB2 27 System Derived 1.000 400 0 0.700 WPC2 WPC2 28 System 1.000 100 0 0.600 E>+0.700 EG-E>+Eo~· 29 System 1.000 100 0 0.600 <E + 0.700 EG-<E+EG- 30 System Derived 1.000 !00 0 0.600 EB> EB> 3I System Derived 1.000 !00 0 0.600 <EB <EB 32 System 1.000 400 0 1.0 <AL* <AL' 33 System 1.000 400 0 1.0 *AL> 'AL> Controlline Frame Denection RatiOs for Cross Section: 8 Description Ratio Deflection (inJ Member Joint Load Case Load Case Description Max. Horizontal Deflection ( H/431) -0.820 6 2 19 <W2 Max. Vertical Deflection for~pan 1 ( L/568) -!.033 3 2 I s File: 7079 Chevron R1_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a ' " 07-27053 Calculations Hazardous Materials Occupancy * Negative horizontal deflection is left * Negative vertical deflection is down Date: 10/20(2008 Time: I :57:43 PM Page: 154ofl75 Lateral deflections of primary frames are calculated on a bare frame basis and do not include resistance from systems such as roof and endwall diaphragms. Therefor~ these deflections may be considerably overstated. ) 0 0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a l:r- 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM ~={_I_-:-----------~-----------~[r=1(2)Fs ~ ~,_ (2)FB FB 0 ~ .~ (') ? ') FB y ~,_ E ~~ t X FRAME CROSS SECTION AT FRAME LINE(S) 9 Dimension Key 1 5'~6" BL to CL of Runway Beam 2 ! 518" 3 4'-0" 4 3'·5 1/4" 5 3'-3 3/4" 6 1'-3" 7 1'-913/16" 8 2@ 2'-4 7/16" 9 4 1/2" \0 40'-10" Ridge Ht. Frame Clearances Horiz. Clearance between members l(CXOOO) and 6(CXOOO): 44'-\0 3/4" File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a FB FB ) 07-27053 Calculations Hazardous Materials Occupancy Ve11. Clearance at member l(CXOOO): 28'~3 5/8" Vert. Clearance at member 6(CXOOO): 28'·3 5/8" Finished Floor Elevation= lOO'·O" (Unless Noted Otherwise) Crane Clearances at bottom of Runway Beam Vert. Clearance !'it CRANE DATA 1-l(Left): 2'-5 5/8" Horz. Clearance at CRANE DATA 1-l(Left): I '-7 5/8" Vert. Clearance at CRANE DATA 1-l(Right): 2'-5 5/8" Horz. Clearance at CRANE DATA 1-l(Right): 1'-7 5/8" 0 0 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading 0 Version: 7.Ja Date: 10/20/2008 Time: I :57:43 PM Page: 156 of 175 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: !57 of 175 Location DeScri tion An le Grou Tlib. Oven·ide Desi n Status 144/9/0 Ri id Frame 90.0000 Stress Check Desi n Load Combinations-Framin . No. OriRin Factor APplication Descrintion I System !.000 l.OD+ !.0 AD+ !.0 CG+ !.0 S D+AD+CG+S 2 System !.000 l.OD+ l.OAD+ l.OCG+ l.OUS!* D+AD+CG+USI* 3 System !.000 l.OD+ LOAD+ J.OCG+ I.O*USI ) D+AD+CG+*USJ 0 4 System !.000 l.O D + !.0 AD+ !.0 CG + !.0 WI> D +AD+ CG +WI> 5 System !.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <Wl D+AD+CG+<Wl 6 System !.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 W2> O+AD+CG+W2> 7 System !.000 LO D + 1.0 AD+ 1.0 CG + LO <W2 D+AD+CG+<W2 8 System !.000 !.0 D + !.0 AD+ !.0 CG + 0.750 S + 0.750 WI> D+AD+CG+S+Wl> 9 System !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 <Wl D+AD+CG+S+<Wl 10 System !.000 l.O D+ !.0 AD+ !.OCG +0.750 S +0.750W2> D+AD+CG+S+W2> II System !.000 !.0 D + !.0 AD+ !.0 CG +0.750 S +0.750 <W2 D+AD+CG+S+<W2 12 System !.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 *AL> D+AD+CG+*AL> 13 System !.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 AL *> D+AD+CG+AL*> 14 System 1.000 1.0 D + 1.0 AD+ l.OCG+ 1.0 <*AL D+AD+CG+<*AL 15 System !.000 1.0 D + !.0 AD + 1.0 CG + !.0 <AL' D +AD+ CG+<AL * 16 System !.000 .600D + 0.600 AD +0.600 CU+ !.0 WI> ~+AD+CU+Wl> 17 System 1.000 .600 D + Q.600 AD+ 0.600 CU + 1.0 <WI ID+AD+CU+<Wl 18 System 1.000 0.600 D +Q.600 AD+0.600 CU + 1.0 W2> D+AD+CU+W2> 19 System !.000 0.600 D + 0.600 AD + Q.600 CU + !.0 <W2 D+AD+CU+<W2 20 System !.000 !.OD + 1.0 AD+ 1.0 CG +0.563 S +0.750 *AL> D+AD+CG+S+*Al> 21 System 1.000 1.0 D + 1.0 AD+ !.0 CG+0.563 S + 0.750 AL'> D +AD+ co+ S+AL"'> 22 System 1.000 1.0 D + l.O AI)+ 1.0 CG +0.563 S +0.750 <*AL D+AD+CG+S+<*AL 23 System !.000 1.0 D+ !.0 AD+ 1.0 CG +0.563 S +0.750 <AL' D +AD+ CG +S+<l!'L• 24 System !.000 1.0 D+ 1.0 AD+ !.0 CG+0.375 WI>+ 0.750 'AL> D +AD+ CG + Wl>+*AL> 25 System 1.000 LO D + 1.0 AD+ l.OCG +0.375 Wl> + 0.750 AL*> b+AD+ CG +\~>'i:AL*> 26 System 1.000 l.O D + t.OAD + 1.0 CG +0.375 <WI+ 0.750 <*AL D+AD+CG +<Wl+<*AL 27 System !.000 1.0 D+ l.OAD + 1.0 CG+0.375 <Wl + 0.750 <AL* D+AD+CG+<VVI+<AL* 28 System 1.000 1.0 D +LOAD-+ l.O CG +0.375 W2> + 0.750 *AL> D+AD+CG+W2>+*AL> 29 System 1.000 1.0 D + 1.0 AD+ 1.0 Cfj +0.375 W2> +0.750 AL*> 0 +AI)+ CG + W2>+AL *> I) 30 System !.000 1.0 D +.1.0 AD+ 1.0 CO +0.375 <W2 + 0.750 <*AL D +AD+ CG + <W2+<*AL 31 System 1.000 1.0 D +LOAD+ 1.0 CG+0.375 <W2 + 0.750 <AL* D +AD +CG +<W2+<AL* 32 System !.000 1.0 D+ !.0 AD+ 1.0 CG +0.!50 S +0.750 E>+0.700 EG+ . D+AD+CG+S+E>+EG+ 33 System !.000 1.0 D+ 1.0 AD+ 1.0 CG+O.I50 S +0.75d <E+0.700 EG+ D+AD+CG+S+<E+EG+ 34 System !.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 E> + 0.700 EG-D+AD+CU+E>+EG- 35 System !.000 ~.600 D + Q.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-D+AD+CU+<E+EG- 36 System Derived 1.000 1.0 D+ l.OAD+ !.0 CG +0.150 8+0.750 EB>+0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived !.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0.700 EG-D+AD+CU+EB>+EG- 38 System Derived 1.000 !.0 D + !.0 AD+ 1.0 CG+ 0.150 S +0.750 <EB +0.700 EG+ D+AD+CG+S+<EB+EG+ 39 System Derived 1.000 0.600 D + 0.600 AD +0.600 CU + 0.700 <EB + 0.700 EG-D +AD+ CU + <EB + EG- 40 System Derived !.000 l.OD+ LOAD+ !.OCG+ !.OWPAI D+AD+CG+WPAl 41 System Derived 1.000 !.0 D+ 1.0 AD+ 1.0 CG +0.750 S +0.750 WPA! D+AD+CG+S+WPA! 42 System Derived !.000 0.600 D + 0.600 AD +0.600 CU + 1.0 WPAI D+AD+CU+WPAl 43 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 WPAl + 0.750 *AL+0.750 ALB> D+AD+CG+WPAI+*AL+ALB> 44 System Derived !.000 l.O D + 1.0 AD+ 1.0 CG +0.375 WPA! + 0.750 AL' +0.750 ALB> D+AD+CG+WPAI+AL*+ALB> 45 System Derived 1.000 l.O D + 1.0 AD+ 1.0 CG + 1.0 WPD! D+AD+CG+WPD! 46 System Derived !.000 1.0 D + 1.0 AD+ !.0 CG +0.750 S +0.750 WPD! D+AD+CG+S+WPDl 47 SYstem Derived !.000 Q.600 D + 0.600 AD +0.600 CU + 1.0 WPDI D+AD+CU+WPDl 48 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDl + 0.750 *AL +0.750 <ALB D+AD+CG+WPD l +* AL +<ALB 49 System Derived 1.000 l.O D+ l.O AD+ 1.0 CG +0.375 WPDl + 0.750 AL* +0.750 <ALB D+AD+CG+WPDJ+AL *+<ALB 50 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA2 D+AD+CG+WPA2 51 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPA2 D+AD+CG+S+WPA2 52 System Derived 1.000 0.600 D + 0.600 AD +0.600CU + !.0 WPA2 D +AD+ CU + WPA2 53 System Derived 1.000 1.0 D + J.O AD+ J.O'CG +0.375 WPA2 + 0.750 *AL + 0.750 ALB> D+AD+CG+WPA2+* AL +ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 + 0.750 AL* +0.750 ALB> D+AD+CG+WPA2+AL *+ALB> 55 System Derived !.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPD2 D+AD+CG +WPD2 56 System Derived 1.000 !.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPD2 D+AD+CG+S+WPD2 57 System Derived 1.000 0.600 D + 0.600 AD +0.600 CU + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 WPD2 + 0.750 *AL +0.750 <ALB D+AD+CG+WPD2+* AL +<ALB 59 System Derived 1.000 1.0 D + !.0 AD+ 1.0 CO +0.375 WPD2 + 0.750 AL * + 0.750 <ALB D+AD+CG+WPD2+AL *+<ALB File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 158ofl75 60 System Derived 1.000 6! System Derived !.000 62 System Derived !.000 63 System Derived !.000 64 System Derived !.000 65 System Derived !.000 66 System Derived !.000 67 System Derived !.000 68 System Derived !.000 69 System Derived !.000 70 System Derived !.000 7! System Derived !.000 72 System Derived !.000 73 System Derived !.000 74 System Derived !.000 75 System Derived !.000 76 System Derived '' !.000 77 System Derived LOOO 78 System Derived LOOO 79 System Derived 1.000 80 System Derived !.000 8! System Derived 1.000 82 System Derived 1.000 83 System Derived 1.000 84 System Derived 1.000 85 System Derived 1.000 86 System Derived 1.000 87 System Derived ' 1.000 88 System Derived LOOO 89 Svstem Derived 1.000 Frame Member Sizes Mem. Fig Width F!g Thk No. (in,) · iin.) l MO 0.3750 2 MO 0.5000 3 , @O 0.5000 4 MO 0,5000 5 MO 0.5000 6 MO 03750 1.0 D + 1.0 AD+ LOCG+ 1.0 WPBI 1.0 D + 1.0 AD+ !.0 CG + 0.750 S + 0.750 WPB! 0.600 D+ 0.600 AD+ 0.600 CU + !.0 WPB! 1.0 D + 1.0 AD+ !.0 CG +OJ75 WPB! + 0.750 *AL + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPBI + 0.750 AL* + 0.750 ALB> !.0 D + !.0 AD+ 1.0 CG + 1.0 WPC! !.0 D + !.0 AD+ LO CG + 0.750 S + 0.750 WPC! MOOD+ MOO AD+ MOO CU + l ,0 WPC! 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPCI +0.750 *AL + 0.750 <ALB !.0 D + !.0 AD+ !.0 CG + OJ75 WPC! +0.750 AL* +0.750 <ALB !.0 D + !.0 AD+ !.0 CG + !.0 WPB2 0 1.0 D + !.0 AD+ !.0 CG + 0.750 S +0.750 WPB2 MOOD+ MOO AD+ MOO CU + !.0 WPB2 \.0 D + 1.0 AD+ l.OCG+0.375 WPB2 +0.750 "'AL+0.7SO ALB> 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPB2 + 0.750 AL* +0.750 ALB> LO D +LOAD+ LO CG + l.O WPC2 l.O D +LOAD+ l.O CG +0.750 S +0.750 WPC2 MOO D + MOO AD +MOO CU + l.O WPC2 LO D + l.O AD+ l.O CG + 0375 WPC2 + 0.750 'AL +0.750 <ALB 1.0 D + l.O AD+ l.O CG +0.375 WPC2 + O)SO AL* +0.750 <ALB 1.0 D + 1.0 AD+ LO CG+ LOS+ l.O ALB> 1.0 D + l.O AD + l.O CG + l.O * AL + 1.0 ALB> 1.0 D + 1.0 AD + 1.0 CG + 1.0 AL * + I.O ALB> !.0 D + 1.0 AD+ 1.0 CG + 0.563 S +0.750 *AL+0.750 ALB> LO D + l.O AD+ 1.0 CG +0.563 S +0.750 AL' + 0.750 ALB> 1.0 D + 1.0 AD+ l.O CG+ LOS+ l.O <ALB 1.0 D + 1.0 AD+ 1.0 CG + l.O *AL + J.O <ALB 1.0 D + l.O AD + 1.0 CG + 1.0 AL * + 1.0 <ALB 1.0 D + l.O AD+ I .0 CG +0.563 S + 0.750 "'AL + 0.750 <ALB 1.0 D + 1.0 AD+ 1.0 CO +0.563 S + 0.750 AL* + 0.750 <ALB . Web Thk Depth! Dcpth2 Length \rv.i:lght F~:.; (;n.) dn.) (in.) (ft) (p) 0.2500 12.00 02500 46.00 0.!644 ;23.00 0.!644 29.00 0.2500 23.00 0.2500 12.00 47.00 31.03 ll75A 55.00 23.00 !8.62 977.2 55.00 29.00 9.!7 :) 322.4 55.00 23.00 9.!7 322.3 55.00 46.00 18.62 977.3 55.00 47.00 3!.03 ll75A 55.00 Total Frame We1ght 4949.9 (p) Frame Pricing Weight= '5429.1 (p) 0/0/0 0/0/0 Values shown are resisting forces of the foundation. Reactions-Unfactored Load Type at Frame c ross Section: 9 Type Exterior Column Exterior Column X-Loc 0/0/0 53/0/0 Gridl ~ Grid2 9-D 9-A Base Plate W x L (in.) 8 X 13 8 X )3 Base Plate Thickness (in.) 0375 0.375 Anchor Rod Qty/D!i:tm. (in.) 4. 0.750 4-0.750 Column Base Elev. l00'-0" !00'-0" Load Type Desc. Hx Vy Hx Hz Vy D Fnn 0.7 3.8 ·0,7 -3.8 - AD Fnn 0.! 0.8 -0, t 0.8 CG Fnn L9 9A ·L9 -7.5 s Fnn 73 28.6 -73 -28.6 - US!"' Fnn 6.5 !6.9 ·6,5 -345 *US! Fnn 6.5 345 ·65 !6.9 - Wt> Frm ·63 ·lOA -4,0 -·35 File: 7079 Chevron R1_Stress Check 10_2008 with 08_2008 Loading D+AD+CG+WPBI D+AD+CG+S+WPB! D +AD+ CU + WPBI D+AD+CG+WPB 1 +* AL +ALB> D+AD+CG+WPB I+AL *+ALB> D+AD+CG+WPC! D+AD+CG+S+WPCl D+AD+CU+WPCI [D+AD+CG+WPCl+*AL+<ALB D+AD+CG+WPCl+AL*+<ALB D+AD+i:G+WPB2 D+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+AL *+ALB> D+AD+CO+WPC2 D+AD+CG+S+WPC2 D+AD+CU+WPC2 D+AD+CG+WPC2+*AL+<ALB D+AD+CO+WPC2+AL *+<ALB D +AD+ CG + S+ALB> D+AD+CG+*AL+ALB> D +AD+ CG+AL *+ALB> D+AD+CG+S+*AL+ALB> D+AD+CG+S+AL *+ALB> D + AP+ CG +S+<ALB D + AD+ CO+* AL+<ALB D +AD+ CG+AL*+<ALB D+AD+CG+S+*AL+<ALB O·i .\D~CG! S"·:\L *·1<,\LD Webfy Splice (ksi) Jt! 55,00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP (Includes all plu1es) (Includes all pieces) 0/0/0 0/0/0 - - - Version: 7.\a Codes Jt2 KN ss SP ss KN KN 0.0000 0.0000 Shape 3P 3P JP 'p 3P 3P 0 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time:\ :57:43 PM Page: l59ofl75 <W1 Fnn 4.0 -3.5 6.3 -10.4 - W2> F•m -7.3 -7.6 -2.9 -0.7 <W2 Fnn 2.9 -0.7 7.3 --7.6 -- *AL> Fnn -0.1 10.0 -1.8 4.7 - AL'> Fnn -0.1 2.7 -1.8 12.0 --- <*AL Fnn 1.8 12.0 0.1 -2.7 -- <AL* Fnn 1.8 4.7 0.1 10.0 --- cu Fnn 1.0 3.8 -1.0 3.8 - E> Fnn -3.3 -4.2 -3.2 -4.2 -- EG+ Fnn 0.3 1.2 -0.3 1.0 --- <E Fnn 3.3 4.2 3.2 --4.2 - EG-Fnn -0.3 -1.2 0.3 -1.0 ' --- EB> Brc --0.0 - --- <EB Brc -- WPA1 Bee 1.8 -5.7 -1.6 -·5.4 -- 'AL Fnn 0.9 11.0 -0.9 3.7 - ALB> Bro -- -- AL' Fnn 0.9 3.7 -0.9 -11.0 --- WPD1 Brc 1.5 -7.7 -1.1 --7.2 -- <ALB <l> Soc - WPA2 Bee 0.8 -2.8 -0.6 --2.6 - WPD2 Bro 0.4 -4.8 -0.1 -4.4 --- WPB1 Bee 1.6 -5.4 -1.8 --5.7 -- WPC1 Brc 1.1 -7.2 -1.5 --7.7 --- WPB2 Bee 0.6 -2.6 -0.8 --2.8 --- WPC2 Brc 0.1 -4.4 -0.4 --4.8 - -- . M ··mum Combh ed React" sSt II'\' 'rhF·1 hr ll Ill' F·amin<> ax1 ' 1011 mun; WI . ' ) l'l .E : l S • ,, ~ -----~ X-Lu..: GriJ Hrzleft Load !lrz Right LouJ Hrz In Lu;td JlrzOut L\!:td' Uplift 1 "'"I\" Uo "' t(!;hl i\l<>lll C\1' Lu:Jti :\·Jni:l ~(IV L~•ad' (-Hx) case (Hx) Case (-Hz) Case (Hz) Case (-Vy) CCJSC (Vy) Ca$e (-Mzz) Cnse (Mzz) Cnse -(ki (k) (k) (k) (k) (k) (in-k) (in-k) 01010 9-D 6.2 18 1!.1 9 --- -5.4 16 T 48.5 3 - - - - 53/0/0 9-A 11.1 8 6.2 19 0.0 36 -5.4 17 46 6 2 - -- . s ... urn o fF 1 R t' C orccs w th eac lOllS l F heck-rannnrr Horizontal Vertical Load Type L~~ Re~~ion Load Reaction .. (k) (k) D 0.0 0.0 7.7 7.5 AD 0.0 0.0 1.7 1.6 CG 0.0 0.0 16.9 16.9 s 0.0 0.0 57.1 57.1 USl* 0.0 0.0 51.4 51.4 *USl 0.0 0.0 51.4 51.4 W1> 10.2 10.2 13.9 13.9 <W1 10.2 10.2 13.9 13.9 W2> 10.2 10.2 8.2 8.2 <W2 10.2 10.2 8.2 8.2 'AL> 1.9 1.9 15.5 14.7 AL*> 1.9 1.9 15.5 14.7 <*AL 1.9 1.9 15.5 14.7 <AL* 1.9 1.9 15.5 14.7 cu 0.0 0.0 7.6 7.6 E> 6.4 6.5 0.0 0.0 EG+ 0.0 0.0 2.2 2.2 <E 6.4 6.5 0.0 0.0 EG-0.0 0.0 2.2 2.2 EB> 0.0 0.0 0.0 o.o <EB 0.0 0.0 0.0 0.0 WPA1 0.2 0.2 1!.1 11.1 'AL 0.0 0.0 155 14.7 ALB> 0.0 0.0 0.0 0.0 AL' 0.0 0.0 15.5 14.7 WPD1 0.4 0.4 14.9 14.9 <ALB 0.0 0.0 0.0 0.0 File: 7079 Chevron RJ_Stress Check \0_2008 with 08_2008 Loading Version: 7.\a 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: 160 of 175 WPA2 0.2 0.2 5.4 5.4 WPD2 0.4 0.4 9.2 9.2 WPBI 0.2 0.2 11.1 II.! WPC! 0.4 0.4 !4.9 14.9 WPB2 0.2 0.2 5.4 5.4 WPC2 0.4 0.4 9.2 9.2 Base Pate Summary X*Loc Grid Mem. Thickness Width Length Num.Of BoltDiam. Type Welds to Welds to No. (in.) (in.) . (in.) Bolts (in.) Flange Web 010!0 9-D I 0.375 8 13 4 0.750 A36 OS-0.1875 OS-0.1875 531010 9-A 6 0.375 8 13 4 0.750 A36 OS-0.1875 OS-0.1875 Web Stirfener Summar Mem. Stiff. Desc. Loc. Web Depth hit o/h a Thick. Width Side Welding No. No. _(ft) _(in.) (in,) (in) _ (in.)_ Description 2 I S9 4.11 43.400 173.60 NIA N/A 0.3750 2.500 Both W-OS-0.1875 2 2 Sl 14.05 28.739 114.96 3.00 85.99 0.1875 2.000 Both Std 5 I S9 14.51 43.401 173.60 NIA N/A 0.3750 2.500 Both W-OS-0.1875 5 2 SI 1!.44 38.869 155.48 3.00 !l6.03 0.1875 2.000 Both F-OS-0.1875,W-OS-0.1875 Brackets Part Summuy Mem. Loc. Total Length Bracket Cut Bracket FlgWidth Fig Thk WebThk Hole Pitch Stiffener or Plate Part No. (ft) (in.) (in.) Depth (in.) -(in.) (in.) (in.) (in.) 2 3.98 15.000 4.750 10.000 6.000 0.2500 0.2500 3.500 UP0704ll 000 WU!504!'234 5 14.65 !5.000 4.750 10.000 6.000 0.2500 0.2500 3.500 UP0704!!000 WUI5041234 Brackets Desif!n Summarv (vertical live load is wit~j_!~c Impact factor --~------~--! Mem. L0c. Vert. Uve Vert. D~';H!T Litcrnl T.unghudinal CL t)~il(~ ~l..:mber I l\kmb..:1 I \\\·h Thk j- Frg ·r hk H):! \\'idth i No. (ft) l.o:ld (k) Load (k) lm)Xld (k) lmp.-lct.(k) Fl;m>:<.' {in.) l D..-•,th I (i11.l l)q•th2 (ill.ll (in.) (1•1.) {j~L) I 2 3.98 !3.72 0.86 0.94 1.47 13.191 j ~2.30§ 40.010 r 0.2500 0.5000 6.0000 5 14.65 13.72 0.86 0.94 1.47 D.l9l 41.010 4\.306 0.2500 0.5000 6.0000 Bolted End-Plate Moment Connections (AJSC OG-l~).:-Fv =55 k~i End-Plate Dimensions Bolt Outside F!m1""e Inside FI;:~Me Mr~m. Jt. T}'pe Thick. Width Length Diam. Spec/Joint Gages In/Out Confic:urutio1·. Pitches 1st/2nd ('t>nfiaurntion P.itcllcs lst/2nd Nb. No. 011.) (in.) (irl?) (in.) (i!l.) lD De~s_-,.. .... ,,) i n_l_ .. ID __ ,_gs_"S.,_,_ ,,_]i_JJ_L_ I 2 KN(fop) 0.500 6.00 48.DO 0.750 A325X/ST 3.50 !3 Flush 2.00/2.00 II Flush 2.0Ui2.00 2 I KN(Top) 0.500 6.00 48.00 0.750 A325X/ST 3.50 l3 Flush 2.00/2.00 11 Flush 2.00/2.00 3 2 SP 0.375 6.00 33.92 0.750 A325X/ST 3.00 11 Flush 0.00 32 Extcnd..:cl J.S(i/2.00 4 I SP 0.375 6.00 33.92 0.750 A325X/ST 3.00 II Flush 0.00 32 Extended 3.56/2.00 5 2 ~g~~~ 0.500 6.00 48.00 0.750 A325XIST 3.50 12 Flush 2.00 II Flush 2.00 6 2 KNTo 0.500 6.00 48.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 Required Stren~ll -Out Available Stren<?th-Out Rt!,qtJired Strength -In Available Strength-In Mem. Jt. Ld Axial Shear Moment Design s~~' Moment Ld A~~~ s~;r Moment Design Shear Moment No. No. Cs (k)_ (!<)_ (in-lc)_ Proc. (in-k) Cs lin-k) Proc. (k) (in-k) I 2 2 -29.7 7.7 2682.9 Thin plate 212.1 2208.0 !6 5.4 1.! 1020.3 Thin plate 106.0 1465.3 2 I 2 -29.7 7.7 2682.9 Thin plate 212.1 2208.0 !6 5.4 1.! 1020.3 Thin plate 106.0 1465.3 3 2 17 2.7 3.! 4!. Thin plate 106.0 595.5 I ·9.7 2.2 !3!3.0 Thin plate 212.1 1206.4 4 I 17 2.7 3.1 4!.2 Thin plate 106.0 595.5 I -9.7 2.2 13!3.0 Thin plate 212.1 1206.4 5 2 3 -29.5 7.7 2630.0 Thin plate 159.0 1938.9 17 5.4 1.! !020.3 Thin plate !06.0 1466.6 6 2 3 -29.5 7.7 2630.0 Thin Plate 159.0 1938.9 17 5.4 !.! !020.3 Thin plate 106.0 1466.6 Fla11_g~ B S race ummarv Member From Member Joint I From Side Point l Part Design Note I 12/5/4 12/5/4 FB2ll4 I 22/5/4 22/5/4 FB4050 I 27/5/4 27/5/4 (2)FB5060 2 5/3/8 22/9113 (2)FB5080 3 1/8/0 7/9/13 FB3024 3 7/8/0 l/9113 FB4020 4 1/6/0 l/91!3 FB4020 5 7/4/0 16/9/13 FB4054 5 13/4/0 22/9/J 3 (2)FB5084 6 12/5/4 121514 FB2114 File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 0 07-27053 Calculations Hazardous Materials Occupancy 22/5/4 27/5/4 22/5/4 27/5/4 FB4050 2 FB5060 Date: 10/20/2008 Time: 1:57:43 PM Page: 161 of 175 Frame Design Member Summary::-Controlll11g: Load Case and Maximum Combined Stresses_ per Member (1:-ocations are from Joint 1 ) . Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear MomwX Mom-y Axial Shear Bnd-X Bnd-Y ---Stress /Force ---Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear l 22.47 39.75 l -4!.3 -7. -2173.1 0.0 2.90 0.81 !5.21 0.00 2 !.48 3,42 24.34 4!.25 0.73 0.24 2 17.19 23.00 3 -IL7 4.4 1475.0 0.0 !.02 0.80 17.28 0.00 29.38 10.74 33.00 41.25 0.55 0.07 3 !.67 24.20 p -10.4 2.4 1553.4 O.J 1.0 0.63 19.87 0.00 29.8! 4.18 3202 41.25 0.64 0.15 4 7.10 24.20 2 -10.3 -2.2 1568.1 0.0 !.05 0.58 20.06 0.00 29.81 4.18 32.82 41.25 0.64 0.!4 5 0.00 23.00 2 -11.7 -4.2 1493.3 0.0 !.01 0.77 !7.50 0.00 29.38 10.74 33.00 41.2 0.56 0.07 6 22.47 39.75 l -4!.! 7.9 -2!!9.5 0.0 2.89 0.8! 14.83 0.00 2!.SO 3.42 24.22 4 !.25 0.71 0.24 Mem. Loc. Depth Area Rx Ry Lx Ly-1 Ly-2 Klx Klyl Kly2 Sx Lbl Rt-1 Lb2 Rt-2 Qs Qa Cbl Cb2 No. ft in. in.2 in. in. in. in. in. /Rx /Ry /Rv in.3 in. in. in. in. l 22.~ 39.75 14.25 !4.46 0.98 340.05 60.1 60.! 3S.3 6!.6 6!.6 142.90 120.2 1.35 60.1 0 1.34 !.00 0.86 1.27 !.09 2 17. 9 23.00 !!.SO 9.24 !.25 294.79 36.0 0.0 3L9 28.8 0.0 85.33 36.0 1.56 0.0 0.00 !.00 !.00 LOS 0.00 3 !.67 24.20 9.81 !0.!6 !.35 294.79 36.0 36.0 29.0 26.6 26.6 78.18 36.0 !.62 36.0 !.62 LOO LOO LOS !.00 4 7.!0 24.20 9.8! !0.!6 L35 294.79 36.0 36.0 29.0 26.6 26.6 78.!8 36.0 !.62 36.0 !.62 !.00 !.00 LO I 1.05 5 0.00 23.00 !!.SO 9.24 !.25 294.79 36.0 0.0 3L 28.8 0.0 8S.33 36.0 !.56 0.0 0.00 !.00 !.00 LOS 0.00 6 22.47 39.75 !4.25 !4.46 0.98 340.05 60.! 60.! 3S.3 61.6 61.6 142.90 120.2 1.3 60.! !.3 !.00 0.86 !.2 LOS ,, 0 0 0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7. Ia ' 07-27053 Calculations Hazardous Materials Occupancy User Defined Frame Point Loads for Cross Section: 9 Ma l Locl Offset HorV Su -1.70 20/8/6 -2/3/0 Horiz. N ® '} y X ·-. Deflection Load Combinations Framina - No. Origin Factor DefH DefY Aoolication I System 1.000 0 240 1.0 s 2 System 1.000 0 240 LOUSI* US!* 3 System 1.0~~ ~ 240 1.0 *US! *US! 4 System 1.00 240 (1.700 WJ> 'WI> 5 System 1.000 0 240 0.700<WI WI 6 System 1.000 0 240 0.700 W2> W2> 7 . System 1,000 0 240 0:700 <W2 <"''2 8 System Derived I.QOO 0 240 0.700\VPAI 0 WPAI 9 System Derived 1.00.0 0 240 0.700 WPDI WPDI· l) 10 System Derived 1.000 0 ( 240 0.700 WPA2 ' WPA-s; II System Derived 1.000 0 240 0.700 WPD2 WPD2 12 System Derived 1.000 0 240 0.700 WPBI WPBI 13 System Derived 1.000 0 240 0.700WPCI WPCI 14 Syste·m Derived 1.000 0 240 0.700WPB2 WP132 15 System Derived 1.000 0 240 0.700WPC2 WPC2 16 System 1.000 400 0 .700WI> WI> 17 System 1.000 400 0 0.700<WI <WI 18 System 1.000 400 0 0.700W2> W2> 19 System 1.000 400 0 0.700<W2 W2 20 System Derived 1.000 400 0 0.700WPAI WPAI 21 System Derived 1.000 400 0 0.700WPDI WPDI 22 System Derived 1.000 400 0 0.700 WPA2 WPA2 23 System Derived 1.000 400 0 0.700 WPD2 WPD2 24 System Derived 1.000 400 0 0.700WPBI WPBI 25 System Derived 1.000 400 0 0.700WPCI wPCI 26 System Derived 1.000 400 0 0.700 WPB2 WPB2 27 System Derived 1.000 400 0 0.700WPC2 WPC2 28 System 1.000 100 0 0.600 E> + 0.700 EG-E>+EG- 29 System 1.000 100 0 0.600 <E + 0.700 EG-E+EG- 30 System Derived 1.000 100 0 0.600 EB> EB> 31 System Derived 1.000 100 0 0.600 <EB <EB 32 System 1.000 400 0 l.O<AL* <AL* 33 Svstem 1.000 400 0 1.0 *AL> *AL> c lr F ontro ml!. rame Dfl e ectlon Ratios for c ross s ectwn: 9 Date: 10/20/2008 Time: l :57:43 PM Page: !62 of 175 Dir. Coef. Loc. DOWN 1.000 OF ·oescriotion . Description Ratio Deflection (in.) Member Joint Load Case Load Case DescriPtion Max. Horizontal Deflection ( H/466) -0.762 6 2 \9 <W2 Max. Vertical Deflection for Span I ( U737) -0.792 4 I I s File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Yerslon: 7.1a ) j 07-27053 Calculations Hazardous Materials Occupancy *Negative horizontal deflection is left *Negative ve1tical deflection is down Date: 10/20/2008 Time: I :57:43 PM 163ofl75 Lateral deflections of primary frames are calculated on a bare frame basis and do not include resistance from systems such as roof and end wall diaphragms. Therefo~, these deflections may be considerably overstated. 0 0 0 0 ) ' ) File: 7079 Chevron RI_Stress Check 10 _2008 with 08_2008 Loading Version: 7.la 07-27053 Calculations Hazardous Materials Occupancy 1:,_ ~ ~,.... FB (2)FB (2)FB " 0 ~ (2}FB (2)FB ~ ~ '::) y -,-B FB E _,.... < '· . ,...,..,,..~,.. ,..,...,.....,,.. ......... ,..,...,..,,...,.,, ,..,.. r-n11••r-o ,.,,,-,,.., ,...., Dimension Key I S'w6" BL to CL of Runway Beam 2 I 5/8" 3 4'w0" 4 3'w5 l/4" 5 3'-3 3/4" 6 1'-3" 7 1'-9 13/16" 8 2@2'-47116" 9 4 1/2" 10 40'-10" Ridge Ht, Frame Clearances Horiz. Clearance between members I(CXOOO) and 6(CX000): 45'-0 3/4" File: 7079 Chevron RI_Stress Check 10_2008 with 08_2008 Loading Version: 7.Ia Date: 1 o I 20 I 2008 Time: I :57:43 PM Page: 164ofl75 FB ® ) 07-27053 Calculations Hazardous Materials Occupancy Vett. Clearance at member 1 (CXOOO): 28'-3 J/4" Vert. Clearance at member 6(CXOOO): 28'-3 1/4" Finished Floor Elevation= 100'-0" (Unless Noted Othetwise) Crane Clearances at bottom of Runway Beam Vert. Clearance at CRANE DATA 1-l(Left): 2'-5 3/4" Horz. Clearance at CRANE DATA H(Left): 1'-8_ 1/2" Vert. Clearance at CRANE DATA !-!(Right): 2'-5 3/4" Horz. Clearance at CRANE DATA 1-l(Right): l'-8 1/2" 0. 0 File: 7079 Chevron R !_Stress Check 10_2008 with 08_2008 Loading 0 Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM Page: 165ofl75 Location 153/6/0 07-27053 Calculations Hazardous Materials Occupancy Descri tion R. id Frame with End osts An le Grou 90.0000 Trib. Override 20/0/0 Date: 10/20/2008 Time: 1:57:43 PM Page: 166of175 Desi Status Stress Check Desi n Load Combinations-Framin No. Origin Factor Application Descr!otion I System 1.000 !.OD+ LOAD+ !.OCG+ !.OS D+AD+CG+S 2 System 1.000 l.O D +LOAD+ 1.0 CG + 1.0 USJ* D+AD+CG+USI* 3 System 1.000 LO D+ 1.0 AD+ 1.0 CG+ 1.0 *US\ D +AD+ CG + *USl 4 System 1.000 1.0 D+ l.O AD+ 1.0 CG+ l.OWl> D +AD+ CG +WI> 5 System 1.000 l.O D+ 1.0 AD+ l.OCG+ l.O<Wl D +AD+ CG +<WI 6 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 W2> D+AD+CG+W2> 7 System 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 <W2 D+AD+CG+<W2 8 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 WI> D+AD+CG+S+Wl> 9 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 <WI D+AD+CG+S+<Wl 10 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 W2> D +AD+ CG + S + W2> II System !.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System 1.000 1.0 D + 1.0 AD + .1.0 CG + 1.0 'AL> D+AD+CG+*AL> 13 System 1.000 1.0 D + l.O AD+ 1.0 CG+ l.O AL*> D+AD+CG+AL*> 14 System 1.000 1.0 D + 1.0 AD+ 1.0 CG+ 1.0 <'AL D+AD+CG+<*AL 15 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 <AL* D+Ai>+CG+<AL"' 16 System 1.000 0.600 D +0.600 AD +0.600 CU + 1.0 WI> D+AD+CU+WI> 17 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <W1 D+AD+CU+<Wl 18 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 W2> D+AD+CU+Wi.> 19 System 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 'AL> D+AD+CG+S+*AL> 21 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL'> D+AD+CG+S+AL*> 22 System 1.000 1.0 D + 1.0 /f;v + 1.0 CG + 0.563 S +0. 7 50'>' AL C) D +-/,D + CG +S·f'.l*AL 23 System 1.000 l.O D + 1.0 AD+ 1.0 CG+ 0.563 S +0.750 <AL* D+AD+CG+S+<AL* 24 System 1.000 1.0 D + l.O AD+ J.O CG+0.375 WI>+ 0.750 *AL> D+AD+CG +W!>+*AL> 25 .System 1.000 l.OD + 1.0 AD+ LO-CG +0.375 WI> +0.750c}L*> 0 + 1\D + CG + W!>+AL*>' 26 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 <WI+ 0.750 <*AL ·p + t\I) + CG + <Wl+<*AL 27 System 1.000 1.0 D +LOAD+ l.OCG+0.375 <WI +0.750 <AL' ~+AD+ CO +<Wl+<AL* 28 System 1.000 LO D + 1.0 AD+ 1.0 CG+0.375 W2> + 0.750 *AL> D +AD+ CG ·I· W>+*AL> 29 ·System 1.000 1.0 D + 1.0 AD+ tl/CG-+0.375 W2> +0.750 AL*> D+AD+CG+W2>+AL*> 30 I System 1.000 l.OD+ LOAD+ l.OCG+0.375<W2+0.750<*AL D +AD+ CO +<W2+<*AL 31 System 1.000 1.0 D + 1.0 AD+ 1.0 CG+0.375 <W2 +0.750 <AL* io +AD+ CG + <W2+<AL"' 32 System 1.000 1.0 D+I.O AD+ 1.0 CG+O.I50 S +0.750 E>+0.700 EG+ D+AD+CG+S+E>+EG+ 33 _System 1.000 1.0 D + 1.0 AD+ 1.0 CG+O.I50 S +0.750 <E+0.700 EG+ P+AD+CG+S+<E+EG+ 34 System 1.000 ~.600 D + 0.600 AD+ 0.600 CU + 0.700 E> + 0.700 EG-p+AD+CU+E>+EG· 35 System· 1.000 ~.600 D +0.600 AD+ 0.600 CU + 0.700 <E + 0.700 EG-D+AD+CU+<E+EG· 36 System.Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.150 S + 0.750 EB> + 0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 ~.600 D+0.600 AD +0.600CU +0.700 EB>+0.700 EG-D+AD+CU+EB>+EG~ 38 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG +0.150 S +0.750 <EB + 0.700 EG+ D+AD+CO+S+<EB+EG+ 39 System Derived 1.000 ~.600 D +0.600 AD+0.600CU +0.700 <EB +0.700 EG-!o +AD+ CU + <EB + EG- 40 System Derived 1.000 I.OD + 1.0 AD+ 1.0 CG + 1.0 WPA1 D+AD+CG+WPAI 41 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750S +0.750 WPAI D+AD+CG+S+WPAI 42 System Derived 1.000 0.600 D +0.600 AD+0.600CU + 1.0 WPAI D+AD+CU+WPAl 43 System Derived 1.000 1.0 D + l.O AD+ 1.0 CG +0.375 WPAI + 0.750 *AL +0.750 ALB> D+AD+CG+WPAI+*AL+ALB> 44 System Derived 1.000 1.0 D + I.O AD+ 1.0 CG +0.375 WPAI +0.750 AL* +0.750 ALB> D+AD+CG+WPA1+AL*+ALB> 45 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPDI D+AD+CG+WPDI 46 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 WPDI D+AD+CG+S+WPDl 47 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPDI D+AD+CU+WPDI 48 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPDI +0.750 'AL +0.750 <ALB D+AD+CG+WPD I+* AL +<ALB 49 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 WPDI +0.750 AL* +0.750 <ALB D+AD+CG+WPD I+AL *+<ALB 50 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPA2 D+AD+CG+WPA2 51 System Derived 1.000 I.OD+ 1.0 AD+ 1.0 CG +0.750S +0.750 WPA2 D +AD+ CG + S + WPA2 52 System Derived 1.000 0.600 D + 0.600 AD + 0.600 CU + 1.0 WPA2 D+AD+CU+WPA2 53 System Derived 1.000 1.0 D +LOAD+ 1.0 CG + 0.375 WPA2 +0.750 *AL +0.750 ALB> D+AD+CG+WPA2+*AL+ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 + 0.750 AL* + 0.750 ALB> D+AD+CG+WPA2+AL*+ALB> 55 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPD2 D+AD+CG+WPD2 56 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPD2 D+AD+CG +S + WPD2 57 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPD2 D+AD+CU+WPD2 58 System Derived 1.000 1.0 D + !.0 AD+ 1.0 CO +0.375 WP02 + 0.750 *AL + 0.750 <ALB D+AD+CG+ Wi)f)2+* A L +<ALB File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a I I 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: I :57:43 PM Page: !67of!75 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 :~9 System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived System Derived S stem Derived Frame l\"fcm!Jcr Sizes M ... m. f!g Width No. 1.!11.) 1 6.00 2 6.00 3 6.00 4 6.00 5 6.00 6 6.00 7 7.00 8 7.00 Frame Member Releases Member Joint l 7 No 8 No 53/0/0 15/0/0 15/0/0 38/0/0 38/0/0 51610 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 Flg Thk _(in.) 0.5000 0.6250 0.6250 0.6250 0.6250 0.6250 0.2500 0.2500 1.0 D + 1.0 AD+ l.O CG + 0.375 WPD2 + 0.750 AL * + 0.750 <ALB I.O D+ 1.0 AD+ LOCO+ 1.0 WPBI LO D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPBI .600 D + 0.600 AD+0.600 CU + 1.0 WPB1 1.0 D + 1.0 AD+ t.O CG + 0.375 WPB! +0.750 *AL + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPBt + 0.750 AL* + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPC1 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPCI .600 D + 0.600 AD +0.600 CU + 1.0 WPCI l.O D + 1.0 AD+ 1.0 CO +0.375 WPCJ + 0.750 *AL +0.750 <ALB l.O D + 1.0 AD+ 1.0 CO +0.375 WPCJ +0.750 AL* + 0.750 <ALB 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPB2 1.0 D + 1.0 AD+ 1.0 CO+ 0.750 S + 0.750 WPB2 .600 D + 0.600 AD+ Q.600 CU + 1.0 WPB2 LO D + LOAD+ LO CG +0375 WPB2 + 0.750 "'AL + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPB2 +0.750 AL"' + 0.750 ALB> 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPC2 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S +0.750 WPC2 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPC2 1.0 D + 1.0 AD+ 1.0 CG+0.375 WPC2 +0.750 *AL + 0.750 <ALB 1.0 D + 1.0 AD+ 1.0 CO +0.375 WPC2 + 0.750 AL * + 0.750-<ALB 1.0 D + 1.0 AD+ 1.0 CG + 1.0 S + 1.0 ALB> l.O D + 1.0 AD+ LO CG +.1.0 *AL + 1.0 ALB> l.O D + 1.0 AD+ 1.0 CO+ 1.0 AL* + 1.0 ALB> 1.0 D +LOAD+ 1.0 CO +0.563 S +0.750 *AL + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 AL* + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG + 1.0 S + 1.0 <ALB l.O D+ LOAD+ 1.0 CG + LO *AL+ t.O<ALB l.O D + 1.0 AD+ 1.0 CO+ 1.0 AL * + 1.0 <ALO 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 *AL + 0. 750 <ALB 1:0 D + l.O ,;'D + 1.0 CG +0.5G3 S ·.'· 0.7::0 Al. * .'· C.7."D <>,u; Wt:b Thk (in:)__ .:: D'"pthl (in.) Depth:! (in.) L<:ngLh (CL) w~·i~;:.-:. (p) Flg Fy (ksi) 0.2500 0.2500 0.1644 0.1644 0.2500 0.2500 • 0.1875 0.1875 12.00 46.00 23.00 28.60 23.00 12.00 15.00 15.00 46.00 23.00 28.60 23.00 46.00 46.00 15.00 15.00 31.03 18.62 9.17 9.17 18.62 31.03 37.00 37.00 1:> 14.3 j(j/.~.2 371.2 37L2 1078.2 1452.4 717.5 717.5 55.00 55.00 55.00 55.00 55.00 55.00 55.00 55.00 Total Frame Wetght -7100.5 (p) Frame Pricing Weight= 7718.2 (p) Joint 2 Yes Yes 0/0/0 Yes Yes No 0/0/0 0/0/0 Yes Yes No 0/0/0 37/0/0 Yes No No 0/0/0 0/0/0 Yes Yes No 0/0/0 37/0/0 Yes No No 0/0/0 33/10/0 Yes Yes Yes 01010 I Values l>hown are resisting forces of the foundation. Reactions-Unfactored Load T eat Frame Cross Section: 10 Type Exterior Column Interior Column Interior Column X-Loc 0/0/0 15/0/0 38/0/0 Grid! -Grid2 IO·D 10-C 10-B File: 7079 Chevron R I_ Stress Check I 0 _ 2008 with 08 _2008 Loading D+AD+CG+WPD2+AL *+<ALB D+AD+CG+WPBI D+AD+CG+S+WPBI D+AD+CU+WPB1 D+AD+CG+WPB l+*AL+ALB> D+AD+CG+WPBl+AL *+ALB> D+AD+CG+WPC1 D +AD+ CG + S + WPCI D+AD+CU+WPCI D+AD+CG+WPCI+*AL+<ALB +AD+CG+WPC 1 +A L *+<ALB D+AD+CG+WPB2 D +AD+CG +S +WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> D+AD-t:CG+WPB2+AL *+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2 D+AD+CU+WPC2 D+AD+CG+WPC2+*AL+<ALB D+AD+CG+WPC2+AL *+<ALi3 D+AD+CG+S+ALB> D +AD+ CG+*AL+ALB> +AD+ CG+AL *+ALB> D+AD+CG+S+*AL+ALB> D+AD+CG+S+AL *+ALB> D+AD+CO +S+<ALB +AD+ CG+*AL+<ALB D + 1\D + CG+AL *+<ALB Dt,\0·1 CG+S+*AL-t<,-\LB 1D !·,\D-!·CG ·S 1·,\L<l<·I<.-\LB _I' web Fy-·r--srli~~:- (ksi) JL.J 55.00 LIP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP 55.00 BP 55.00 BP (Includes all plates) (Includes all pieces) 0/0/0 0/0/0 0/0/0 0/0/0 0/0/0 0/0/0 Exterior Column 531010 10-A Version: 7.\a ·--.,----------· Codes Sk1pv• JL2 KN :;p SS 3P SP :W SS JP KN 3P KN 3P SS 3P SS 3P 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 ') ') 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: l68of175 Base Plate W x L (in.) Base Plate Thickness (in.) Anchor Rod Qty/Diam. (in.) Column Base Elev, Load Type Desc. D Frrn AD Frm CG Frm S Fnn US!* Fnn *USJ Frm WI> Frm <WI F1m W2> Frm <W2 Fnn *AL> Fnn AL*> Fnn <*AL Fnn <AL* Fnn CU Fm1 E> Fnn EG+ Fnn <E Frm EG-Frm EB> Brc <EB Brc WPA1 Brc *AL Fnn ALB> Brc AL* Fml \V!'i) I Brc <ALB Brc Hx 0.9 0.! 2.7 10.2 9.! 9.1 -7.2 4.7 -8.6 3.3 -0.0 -0.0 1.4 1.4 1.4 -4.1 0.4 4.1 -0.4 2.5 0.7 0.7 1.9 9 X 13 0.500 4-1.000 100'-0" Hz -. -0.0 Vy 4.6 1.2 12.4 39.7 23.6 48.0 -12.4 -4.4 -8.4 -0.5 7.7 2.1 9.3 3,6 5.3 -5.5 1.6 5.5 -1.6 -7.3 8.5 Hx - 8 X 16 0.)75 4-0.750 100'-0" Hz -0.2 7.1 -6.4 -0.0 -0.0 0.0 0.0 Vy Hx 0.8 2.2 0.2 -0.2 8 X 16 0.)75 4-0.750 100'-0" Hz -0.2 7.1 -6.4 -0.0 -0.0 0.0 0.0 o. Vv 0.8 2.2 0.2 -{).2 Hx -0.9 -0.1 -2.7 -10.2 -9.1 -9.1 -4.8 7.3 -3.4 8.7 -lA -lA 0.0 0.0 -lA -4.1 -0.4 4.1 0.4 -2.5 -0.7 -0.7 . f"} -1.9 9 X 13 0.500 4-1.000 100'-0" Hz -0.0 Vv 4.7 1.2 10.5 39.8 48.0 23.6 -4.4 -12.4 -0.5 -8.4 3.6 9.) 2.1 7.7 5.3 5.5 1.4 -5.5 -1.4 -7.3 2.9 8.5 -9.6 WPA2 Brc 1.0 -3.3 --- --l.O --3.3 \Vl'D2 Brc 0.4 --5.6 ;J ---OA --5.6 \\'Pill Brc 1.5 --7.3 -I <!.5 -7.3 L_ __ .:.;~"·~"'g""~---·_,_-"~.,;~'---'-""i"'•~._L--_.[_,~9'";:~~-'--::___J__,: _ _Jc_:_: --~--=-L~ __ J__,::_L.:~.l"•~~_,_I__;;:_·..J.__:it Maximum Combined Reactions Summar\' with Fadnred Lnads ~ Fra."11in<~' X-Loc Grid Hrz left Load HrzRight Load Hrz!n Load Hrz Out Load Uplift Load V1t Down Load Momcw (-~x) Case (~) Case (-~~~) Case (~~) Case (-~i) Case (~) Case (-Mzz) k) fin-kl 01010 10-D 7.2 18 14.9 9 0.0 36 --5.8 16 66.2 3 - 15/0/0 10-C - -- -6.6 5 7.1 16 -3.1 32 15/0/0 37/0/0 - -- -6.1 17 6.9 4 0.8 I - -- 38/0/0 10-B --6.6 5 7.1 16 --3.1 32 - 38/0/0 37/0/0 - -- -6.1 17 7.0 4 0.8 I - - - 53/0/0 10-A 14.9 8 7.3 19 0.0 36 --5.7 17 64.4 2 - Sumo fF . bR eact ons Chec orces w1t k F -ram ne Horizontal Vertical Load Type L1~d Reaction Load Reaction (k) (k) (k) D 0.0 0.0 10.9 9.3 AD 0.0 0.0 2.5 2.4 CG 0.0 0.0 27.3 27.3 s 0.0 0.0 79.5 79.5 US I* 0.0 0.0 71.5 71.5 •us1 0.0 0.0 71.5 71.5 WI> 12.0 12.0 16.8 16.8 <WI 12.0 12.0 16.8 16.8 W2> 12.0 12.0 8.9 8.9 <W2 12.0 12.0 8.9 8.9 "AL> 1.5 1.5 12.0 11.4 File: 7079 Chevron R1_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 0 ·:J Load Momccw Lo<~d Case (Mzz) iin-kl Case -- - -- - -- - ------- - - . 07-27053 Calculations Hazardous Materials Occupancy AL*> 1.5 1.5 12.0 11.4 <*AL 1.5 1.5 12.0 11.4 <AL* 1.5 1.5 12.0 11.4 cu 0.0 0.0 lo.6 10.6 E> 8.1 8.2 0.0 0.0 EG+ 0.0 0.0 3.3 3.3 <E 8.1 8.2 0.0 0.0 EG-0.0 0.0 3.3 3.3 EB> 0.0 0.0 0.0 0.0 <EB 0.0 0.0 0.0 0.0 WPAI 0.0 0.0 14.5 14.5 'AL 0.0 0.0 \2.0 11.4 ALB> 0.0 0.0 0.0 0.0 AL' 0.0 0.0 12.0 11.4 WPDI 0.0 0.0 19.1 \9.2 <ALB 0.0 0.0 0.0 0.0 WPA2 0.0 0.0 6.6 6.6 WPD2 0.0 0.0 11.2 11.2 WPBI 0.0 0.0 14.5 145 " WPCJ 0.0 0.0 19.1 19.2 WPB2 0.0 0.0 6.6 6.6 WPC2 0.0 0.0 11.2 11.2 B S ase Plate ummarv X~Loc Grid Mem. Thickness Width Length Num.Of BoltDiam. Type Welds to No. (in.) (in.) (in~) Bolts (in.) Flan£e 0/0/0 10-D I 0.500 9 13 4 1.000 A36 OS-0.1875 15/0/0 10-C 7 0.375 8 16 4 0.750 A36 OS-0.1875 38/0/0 JO-B 8 0.375 8 16 4 0.750 A36 OS-0.1g75 53/0/0 10-A 6 0.500 9 13 4 1.000 A36 OS-0.\875 Wei) Stiffener Summarv -T ·i:hi"Z"k:-· --\\lklth ------·-·· ···-Mcm. Stiff. Desc. Loc. Web Depth hit a/h n Side ''1 No. No. (ft) (in.)· (in.) (in.) (in.) 2 I S9 4.02 43.176 172.71 N/A. Nlr\ 0.5000 2.500 Doth 2 2' SJ '12.47 30.777 123.11 3.00 92.01. 0.1!:!75 2.000 l3vth Date: 10/20/2008 Time: 1:57:43 PM Page: 169 of 175 Welds to Web OS-0.1875 OS-0.1875 OS-0.!875 OS-0.1875 - ................. --.----- Welding Description · w-os·-o.JS75 Std 4 I Sl 7.17 23.04\ 140.15 3.00 69.1:2 0.1875 2.000 Doth r-OS-0.1 K75,W-OS.-O.I R75 5 I S9 14.60 43.176 172.71 N/A N/A 0.6250 2.500 Doth W-OS-0.1875 5 2 Sl 13.13 41.012 164.05 3.00 122.35 0.1875 2.000 Both F-OS-0.1875, W-OS-0.1875 Brackets Part s ••mmarv ----Mem. Loc. Total Length Bracket Cut Bracket Fig Width Fig Thk WebThk Hole Pitch Stiffener or JJbte Prut No. (ft) (in.) (in.) .. Deoth On.\ -(in.) . iin.) (in.) (in.) 2 3.98 15.125 4.750 10.000 6.000 0.2500 0.2500 3.500 UP0704\IOOO WU\5\41234 5 14.64 15.125 4.750 10.000 6.000 0.2500 0.2500 3.500 UP0704ll000 WU\5141234 Brackets Desien Summary (vertical live load is with the impact factor Mem. Loc. Vert. Live Vert. Dead Lateral Longitudinal CL Dist to Member Member WebThk Fig Thk FlgWidth No. (ft) Load (k) Load (k) Impact (k) Impact (k) Flange (in.) Depth! (in.) Depth2 (in.) (in.) (in.) (in.) 2 3.98 10.61 1.27 0.73 1.47 13.318 42.208 39.669 0.2500 0.6250 6.0000 5 14.64 10.61 1.27 0.73 1.47 13.318 40.919 40.958 0.2500 0.6250 6.0000 Bolted End~ Plate Moment Connections (AISC DG-16) ~ Fy =55 ksl End-Plate Dimensions Bolt Outside Flange Inside Flange Mem, Jt. Type Thick. Width Length Diam. Spec/Joint Gages In/Out Configuration Pitches I st/2nd Configuration Pitches 1st/2nd No. No. (in.) (in.) (in.) ~ (in.) .. (in.) ID Desc. (in. ID Desc. _(in.) I 2 KN(Top) 0.625 6.00 47.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 2 I KN(Top) 0.625 6.00 47.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 3 2 SP 0.500 6.00 33.49 0.750 A325X/ST 3.00 II Flush 0.00 31 Extended 3.75 4 I SP 0.500 6.00 33.49 0.750 A325X/ST 3.00 II Flush 0.00 31 Extended 3.75 5 2 KN(Top) 0.625 6.00 47.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 6 2 KN(Tooi 0.625 6.00 47.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 Required Strength-Out Available Strength-Out Required Strenoth -In Available Strcn<>th -In IMeml Jt L~ I Axial ! Shear I Moment Design I Shear I Moment L~ I Axial l Shear l Moment Design I Shear ! Moment No. No. Cs (k) (k) (in-k) Proc. (k) (in-k) Cs (k) (k) (;n-k) Proc. (k) (in~k) . File: 7079 Chevron R I_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a 0 0 I 2 2 2 1 2 3 2 16 4 1 16 5 2 3 6 2 3 F1an.e· Membec ; 1 2 2 2 3 4 5 5 5 6 6 7 7 7 8 : 07-27053 Calculations Hazardous Materials OcClipancy Date: 10/20/2008 Time: I :57:43 PM Page: 170 of 175 -40.6 10.8 3729.1 Thin plate 159.0 2879.8 16 5.8 1.3 1147.1 Thick plate 106. 1729. -40.6 10.8 3729.1 Thin plate 159.0 2879.8 16 5.8 1.3 1147.1 Thick plate 106.0 1729.6 4.9 1.8 13.0 Thin plate 106.0 894.3 1 -13.5 3.2 1788.8 Thin plate 159.0 1825.5 4.9 1.8 13.0 Thin plate 106.0 894.3 1 -13.5 3.2 1788.8 Thin plate 159.0 1825.5 -40.6 10.8 3678.4 Thin plate 159.0 2907.1 17 5.8 1.4 1179.0 Thick plate 106.0 1727.1 -40.6 10.8 3678.4 Thil!._fllate 159.0 2907.f 17 5.8 1.4 1179.0 Thick olate 106.0 1727.1 Fcom~oint1 Fcom Side Point Pa1t Design Note ~;;;;: ~~~~6!: 221514 271514 271514 FB5050 51318 2219113 FB5080 141318 13/9113 FB4024 171318 1019113 FB3030 71810 119113 FB4014 11610 119113 FB4014 l/410 10/9/13 FB3030 4/4/0 1319/13 FB4024 1314/0 22/9113 FB5080 J 17/5/4 17/5/4 FB4000 27/5/4 27/5/4 FB5050 715/4 7/5/4 FB2044 1715/4 17/514 {2)FB2044 2515/4 2515/4 (2)FB2044 7/5/4 71514 FB2044 ~~;;;: ~;;;;: :~; T '~'Pf'~"f~I~'"Tst~S~II~In?"~w~<·y~~~~~~~~~~~-~~~ r X-Loc Grid Top Corin. C11ndition fig Mn Rb Allo\;·Comp "f'.l)f;;l-t ·j::i;· A~1gk~ ---~ii~;···-FBI:-; 1:1~· --· Punm ·----- h<lll )lol.-~!1 j 11/\\:::.1 Reaction Force Momem Shc:11· Rl R2 Purlin Bc~ring 15/0/0 10-C 6.9~ 6.06 Swb-2 190.64 6.06 1:2.02 5.% 38/0/0 10-B 6.95 6.08 Stub-2 191.42 6.08 -12.06 5.98 : lllc.<~ <ng ' -----· ·---· _:__,:..::.......:...:.-.. -~...::..: ,; . .:........:. ... : .... __ __,.__:;,_ --~---~-,_ ·->··--·· .•... .. --' ""' ··-· .... ·-----··-.. Actual Forces Actual Stresses · · Allowob!c Stress Condition Mem. Loc. Depth Load• Axial Shear Mom-x Mom·y Axial Shear 13m!-X UnJ-Y ---Stres:> /l~"on.:e ---Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear 1 22.4.7 38.98 1 -56.8 -1 1.0 -3028.0 0.0 3.67 1.16 18.53 0.00 21.96 3.60 25.84 41.25 0.85 0.32 2 17.23 23.00 3 -16.3 6.0 2022.7 0.0 1.26 1.11 20.17 0.00 29.47 10.99 33.00 41.25 0.65 0.10 3 1.67 24.11 . 3 -14.4 3.2 2129.2 0.0 1.28 0.86 23.01 0.00 29.86 4.30 32.89 41.25 0.74 0.20 4 7.10 24.11 2 -14.3 -3.( 2150.7 0.0 1.27 0.81 23.24 0.00 29.86 4.30 32.89 41.25 0.75 0.19 5 0.00 23.00 2 -16.2 -5.9 2047.7 0.0 1.25 1.08 20.42 0.00 29.47 10.99 33.00 4125 0.66 0.10 6 17.46 32.97 1 -56.8 11.0 -2310.1 0.0 3.68 1.39 15.42 0.00 24.71 5.16 18.16 41.25 0.97 0.27 7 17.44 15.00 16 -0.5 -0.4 -786.1 0.0 o:os 0.14 26.12 0.00 18.55 13.90 28.37 28.37 0.92 0.01 8 17.44 15.00 16 -0.5 -0.4 -786.8 0.0 0.08 0.1 26.14 0.00 18.55 13.90 28.37 28.37 0.93 0.01 Mem. Loc. Depth Area Rx Ry L< Ly-1 Ly-2 Klx Kly1 K1y2 Sx Lb1 Rt-l Lb2 Rt-2 Qs Qa Cb1 Cb2 No. ft in. in.2 in. in. in. in. in. /Rx !Ry /Ry in.3 in. in. in. in. 1 . 22.47 38.98 15.50 14.73 1.08 339.6 60.1 60.1 34.6 55.7 55.7 163.41 120.2 1.4 60.1 1.43 1.00 0.84 1.27 1.09 2 17.23 23.00 12.94 9.44 1.32 295.91 36.0 0.0 31.3 27.3 0.0 100.29 36.0 1.61 0.0 0.00 1.00 1.00 1.05 0.00 3 1.67 24.11 11.26 10.3 1.41 295.91 36.0 36.0 28.7 25.5 25.5 92.52 36.0 1.6 36.0 1.66 1.00 1.00 1.05 1.00 4 7.10 24.11 11.26 10.32 1.41 295.91 36.0 36.0 28.7 25.5 25.5 92.52 36.0 1.6 36.0 1.66 1.00 1.00 1.01 1.05 5 0.00 23.00 12.9 9.44 1.32 295.91 36.0 0.0 31.3 27.3 0.0 100.29 36.0 1.61 0.0 0.00 1.00 1.00 1.05 0.00 6 17.46 32.97 15.43 13.05 1.21 339.6 60.1 60.1 39.1 49.7 49.7 149.80 209.5 1.64 120.2 !.57 1.00 0.92 1.75 1.20 7 17.44 15.00 6.22 6.19 1.52 444.00 120.0 96.0 71.8 79.1 63.3 30.10 120.0 1.87 96.0 1.86 0.86 1.00 1.00 1.00 8 17.44 15.00 6.22 6.19 !.52 444.00 120.0 96.0 71.8 79.1 63.3 30.10 120.0 1.87 96.0 1.86 0.86 1.00 1.00 1.00 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la 0 ) 07-27053 Calculations Hazardous Materials Occupancy Date: 10/20/2008 Time: 1:57:43 PM Page: 171 of 175 User D f1 cd Fr ''" a me Pol tL d fore n oa s ross S t'o 10 ec 1 n: Side Units Type Description I k CG PSM4l Pipe Loads 2000 k CG /PSA2 Pipe Loads 2001 k CG PS-42 Pip~ Loads y Denection Load Combinations Framin" --I ;>:o. ! Ori"in ! I I S\···:-·m 2 Sy:;wrn -3 Sy:;tem 4 System 5 System 6 Sys.tem I 7 System I ' ~)·~t~'"l fkriwd . 9 System Derived 10 System Derived II System Derived 12 System Derived 13 System Derived 14 System Derived IS System Derived 16 System 17 System 18 System 19 System 20 System Derived 21 System Derived 22 System Derived 23 System Derived 24 System Derived 25 System Derived 26 System Derived 27 System Derived 28 System 29 System 30 System Derived 31 System Derived 32 System 33 fu:r?tem Factor Dcfl! DefY !.000 0 2.-10 \.fl.< I.OOU 0 240 1.\J US I* l.QOO 0 240 I.O*I)Sl 1.000 0 240 0.700 \\'J> Lebo 0 240 0.7(:)0 <WI ") 1.000 0 240 0.700 W2> 1.()()0 0 240 0.700 <W2 I.OOQ 0 140 IPnr, \\'1\-\ 1 1.000 () 240 r.700 \VI'Ul 1.000 0 240 0.700 WPA2 1.000 0 240 0.700WPD2 1.000 0 240 0.700 WPOl 1.000 0 240 0.700 WPCI 1.000 0 240 0.700 WPD2 1.000 0 240 0.700 WPC2 1.000 400 0 0.700 WI> 1.000 400 0 0.700 <WI 1.000 400 0 0.700 W2> 1.000 400 0 0.700<W2 1.000 400 0 0.700 WPAI 1.000 400 0 0.700WPDI 1.000 400 0 0.700WPA2 1.000 400 0 0.700WPD2 1.000 400 0 0.700\VPBI 1.000 400 0 0.700 WPCI 1.000 400 0 0.700 WPB2 1.000 400 0 0.700WPC2 1.000 100 0 0.600 E>+0.700 EG- 1.000 100 0 0.600 <E + 0.700 EG- 1.000 100 0 0.600 EB> 1.000 100 0 0.600 <EB 1.000 400 0 I.O<AL* 1.000 400 0 1.0 *AL> at Bottom of Beam Lett Bracket Length Lefi MaRl Loci Offset HorV Suoo. Dir. Coef. Loc. -1.70 20/8/6 -21310 Horiz. N DOWN 1.000 OF -2.20 20/8/E -2/3/ Horiz. N DOWN 1.000 OF -2.20 20/8/6 -2/3/0 Horiz. N DOWN 1.000 OF 15'-0" ·-----·--·----·-·;--·--------· ,\"·~licntle>n .. _. , ----~cripti:~--~ ·. s 0 US!"' "'US! WI> <Wl W2> <'vVl WP:\1 WPDJ WPA2 WPD2 WPOI WPC! WPB2 WPC2 WI> ' <WI o W2> j<W2 WPAI WPDI WPA2 WPD2 WPOI WPCI WPB2 WPC2 E> + EG- E+EG- EB> f<EB <AL* *AL> Right Bracket Length Hoist Room Clear Lift File: 7079 Chevron RI_Stress Check 10_2008 wilh 08_2008 Loading Version: 7.Ja 07-27053 Calculations Hazardous Materials Occupancy 1 0/0/0 215/12 11115 2/5/12 \1115 4/8/0 2 0/0/0 215/10 \1\13 2/5/10 11113 4/8/0 3 01010 2/4/3 0/11/12 2/4/3 0/11/12 4/8/0 4 0/0/0 2/4/3 0/11/12 2/4/3 0/11/12 4/8/0 5 0/0/0 2/4/3 0/11112 2/4/3 0/11/12 4/8/0 6 0/0/0 2/4/3 0/\1/12 2/413 0/11/12 4/8/0 7 0/0/0 2/413 0/11/12 2/413 0/11/12 4/8/0 8 0/0/0 2/413 0/1\/12 21413 0111112 4/8/0 9 0/0/0 215110 111/3 2/S/10 1/1/3 41810 \0 010/0 215112 \1115 215112 11115 4/8/0 Ho. t IF nzon a rarne C1 earances w 114 a ' Frame Required at Bottom of Beam at Bottom of Beam Left Right I 113/0 \/8/8 \/8/8 2 11310 \17110 1/7/10 3 113/0 1/1012 \/10/2 4 113/0 1/1012 1/10/2 5 1/3/0 1/10/2 1/10/2 6 \1310 111012 "' 11\012 7 1/3/0 111012 111012 8 113/0 1110/2 \/1012 9 113/0 117110 117110 10 i/3/0 11818 118/8 ,) 0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.la Date: 10/20/2008 Time: 1:57:43 PM Page: 172 of 175 21/10/0 21/10/0 21110/0 21/10/0 21/10/0 21/10/0 21/10/0 21/10/0 21/10/0 2\/\0/0 0 Date: 10/20/2008 07-27053 Calculations Hazardous Materials Occupancy Shape: base Loads and Codes -Shape: base City: Rifle County: Garfield State; Built Up: Colorado 89AISC 04AISI Building Code: 2003 Jntemational Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind Load Wind Speed: 90.00 mph Wind Exposure (Factor): C ( 1.023) Parts Wind Exposure Factor: 1.023 Wind Enclosure: Enclosed Wind Importance Factor: 1.150 Topographicg'actor: 1.0000 NOT Windbome Debris.Region Base Elevation: 0/0/0 Primary Zone Strip Width: 10n13 Parts I Po1tions Zone Strip Width: 513110 Basic Wind Pressure: 20.74 psf >' Cold Fonn: Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):S.OO psf ) Snow Load Roof Snow Load: 75.00 psf Design Snow (Sloped): 75.00 psf SnoW Exposure Category (Factor): 2 Partially Ex.posed (1.00) Snow Imp011ance: 1.100 The1mal Catego1y (Factor): Heated (1.00) Ground I Roof Conversion: 0.70 %Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Unobstructed, Slippe1y Roof Live Load Country: United States Rainfall: 4.00 inches per hour Live Load: 20.00 psf Not Reducible Seismic Load Mapped Spectral Response w Ss:43.60 %g Mapped Spectral Response. Sl :9.10 %g Seismic HaZard I Use Group: Group 2 Seismic Importance: 1.250 Seismic Perfonn::mce I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Bracing Seismic Period: 0.2691 Framing R-Factor: 3.0000 Bracing R-Factor: 3.0000 Soil Profile Type: Stiff soil (D, 4) Frame Redundancy Factor:l.OOOO Brace Redundancy Factor:l.OOOO Frame Seismic Factor (Cs): 0.1354 x W B1·ace Seismic Factor (Cs): 0.1758 x W Per Anic1e 2.9 in the I3uilJer Agreement, VI' Building~ JS.:iUII><:.:i ;iwlt!".<.: Build(;r h;1s ~:;dkd ,:,-: l·x·:1l :Juiidin);, O!":"i..:i:.l vr l'r\;j~..:t i::n:,;ilk!..l·tu ,,1;t;.1in ~II wdo..: <liH..i loading infonnation for this specific buildi11g si1c. Covcrino Desien Loath-Wall: 1 ZOne Units Type Description A_c.!_~~~J L11cl Allow. Ratio Oir. C'ocf. End Zone psf W1> Need Lower ond Upper Girt 32.77 0/U/0 51.000 0.64 OUT ol.580 End Zone psf <W2 Standard Spacing is Adequate 24.47 01010 26.000 0.94 IN 1.180 End Zone psf WI> Need Lower and Upper Girt 32.77 471816 5I.OOC 0.64 OUT ·1.580 End Zone psf <W2 Standard SpaCing is Adequate 24.47 471816 26.000 0.94 IN 1.180 Interior Area psf WI> Need Lower Girt 26.55 513/10 29.000 0.92 OUT Ml.280 Interior Area psf <W2 Standard· Spacing is Adequate 24.47 513110 26.000 0.94 IN 1.I80 Coverlnl:!" Design Loads-w all: 2 Zone Units Type Description Actual Locl Allow. Ratio Dir. Coef. End Zone psf W1> Need Lower and Upper Girt 32.77 DIDIO 51.000 0.64 OUT -1.580 End Zone psf <W2 Standard Spacing is Adequate 24.47 01010 26.000 0.94 1N 1.180 End Zone psf WI> Need Lower and Upper Girt 32.77 I481816 51.000 0.64 OUT -1.580 End Zone psf <W2 Standard Spacing is Adequate 24.47 I481816 26.000 0.94 IN 1.180 Interior Area psf WI> Need Lower Girt 26.55 513110 29.000 0.92 OUT -1.280 Interior Area psf <W2 Standard Spacing is Adeauate 24.47 513110 26.000 0.94 IN 1.180 Coverine: Desie:n Loads M Wall: 3 Zone Units Type Description Actual Locl Allow. Ratio Dir. Coef. End Zone psf WI> Need Lower and Upper Girt 32.77 01010 51.000 0.64 OUT -1.580 End Zone psf <W2 Standard Spacing is Adequate 24.47 01010 26.000 0.94 1N 1.180 End Zone psf W1> Need Lower and Upper Girt 32.77 471816 51.000 0.64 OUT -1.580 End Zone psf <W2 Standard Spacing is Adequate 24.47 471816 26.000 0.94 IN 1.180 Interior Area psf WI>: Need Lower Girt 26.55 513110 29.00 0.92 OUT -1.280 Interior Area psf <W2 Standard Spacing is Adequa.te 24.47 513110 26.000 0.94 IN 1.180 Covering Design Loads-Wall: 4 Zone Units Type Desc~iption Actual Loci Allow. Ratio Dir. Coef. End Zone psf W1> Need Lower and Upper Girt 32.77 01010 51.000 0.64 OUT -1.580 End Zone psf <W2 Standard Spacing is Adequate 24.47 01010 26.000 0.94 1N 1.180 End Zone psr W1> Need Lower and Upper Girt 32.77 148/S/6 51.000 0.64 Ot1T -1.580 File: 7079 Chevron RI_S~·ess Check 10_2008 with 08_2008 Loading Version: 7.la (} 07-27053 Calculations Hazardous Materials Occupancy Date: 10 I 20 I 2008 Time: I :57:43 PM Page: !74 of 175 I End Zone psf <W2 Standard Spacing is Adequate . 24:47 148/8/6 26.000 0.94 IN 1.180 Interior Area psf WI> Need Lower Girt 26.55 5/3/10 29.000 0.92 OUT -1.280 Interior Area psf <W2 Standard Spacin~ is Adequate 24.47 5/3/10 26.000 0.94 IN 1.180 Coverine: Deshm Loads-Roof: A Zone Units Type Description Actual Loci Allow. Ratio Dir. Coef. Entire Surface psf s Non~std Spacing: 4/0/0 Required 76.12 0/010 78.000 0.98 IN 1.000 Entire Surface psf *US! Non-std Spacing: 3/0/0 Required 113.62 01010 117.000 0.97 IN 1.500 Comer Zone psf WI> Non-std Spacing: 4/3/0 Required 60.68 5/3/10 59.000 1.03 OUT -2.980 Comer Zone psf <W2 Standard Spacing is Adequate 15.22 5/3/10 51.00 0.30 IN 0.680 Side Zone psf WI> Standard Spacing is Adequate 37.87 5/3/10 44.000 0.86 OUT -1.880 Side Zone psf <W2 Standa~ Spacing is-Adequate 15.22 5/3/10 51.000 0.30 IN 0.680 Comer Zone psf WI> Non-std pacing: 4/3/0 Required 60.68 5/3/10 59.000 1.03 OUT -2.980 Comer Zone psf <W2 Standard Spacing is Adequate 15.22 5/3/10 51.000 0.30 IN 0.680 Side Zone psf WI> Standard Spacing is Adequate 37.87 148/8/6 44.000 0.86 OUT -1.880 Side Zone psf <W2 Standard Spacing is Adequate 15.22 148/8/6 51.000 0.30 IN 0.680 Comer Zone psf WI> Non~std Spacing: 4/3/0 Required 60.68 148/8/6 59.000 1.03 OUT -2.980 Corner Zone psf <W2 Standard Spacing is Adequate 15.22 148/816 51.000 0.30 IN 0.680 Side Zone psf WI> Standard Spacing is Adequate 37.87 148/8/6 44.000 0.86 OUT -1.880 Side Zone psf <W2 Standard Spacing is Adequate 15.22 148/8/6 51.000 0.30 IN 0.680 Corner Zone psf WI> Non~std Spacing: 4/3/0 Required 60.68 148/8/6 59.000 1.03 OUT -2B80 Comer Zone psf <W2 Standard Spacing is Adequate 15.22 148/8/6 51.000 0.30 IN 0.680 Side Zone psf WI> Staridard Spacing is Adequate 37.87 5/3/10 44.000 0.86 OUT -1.880 Side Zone psf <W2 Standard Spacing is Adequate 15.22 5/3/10 51.000 0.30 IN 0.680 Interior Area psf WI> Standai'd Spacing is Adequate 21.28 5/3/10 44.000 0.48 OUT -1.080 Interior Area psf <W2 Standard SpUci11g_is Adequate 15.22 5/3/10 51.000 0.30 IN 0.680 D R Coveri_rtg_ esiun Loads -oof: B Zone Units Type Dcscripti0n Actu:1l Lr>cl Allow. [J§iiil P~r. -~ Entire Surface p$f s Nl'll·St(-fSp:leing: 4/0f() l{eqt~irc(l )7t,,l ~ 154/(l/( l ,,-- 7?UJ(J{f {l_tJ.~ 1 :•.~: l.l"'iJ Entire Surface psf US!"' Non~std Spncing: 3/0/0 Required 113.62 154/0/0 117.000 0.97 1,\l 1.500 0 Comer Zone psf WI> Non.std Spncing: 4/3/0 Rcqt;~rcd 60.61'-: 5/3/10 59.000 1.03 ()\ rr -2.9FO Corner Zone psf <W2 Standard Spacing is Adequate 1.5.22 5/3/10 51.000 0.30 IN O.Gf-:0 Side Zone psf WI> :Standard Spacing is Adequate 37.87 5/J/10 44.000 0.86 OL:T -1.880 Side Zone psf <W2 Standard Spacing is 1\dequate 15.22 5/3/10 51.000 0.30 JN 0.680 Comer Zone psf WI> :-.ion·std Spadng: 4/3kJ Required 60.68 5/J/10 SY.OOO 1.03 OlJT ¥2.%0 Comer Zone psf <W2 Standard Spacing is Adequate !5.22 5/3/10 51.000 0.30 j;-..J 0.680 Side Zone; psf WI> Standard Spacing is Adequate 3 7.87 148/8/6 44.00~ 0.86 OUT -1.880 Side Zone psf <W2 Standard Spacing is i\dequate 15.22 148/8.'6 51.000 0.30 1:-l 0.680 Comer Zone psf WI> Non~std Spacing: 4/3/0 Required 60.68 148/8/6 59.000 1.03 OUT ¥2.900 Comer Zone psf <W2 Standard Spacing is Adequate 15.22 148/8/6 51.000 0.30 IN 0.680 Side Zone psf WI> Standard Spacing is Adequate 37.87 148/8/6 44.000 0.86 OUT -1.880 Side Zone psf. <W2 Standard Spacing is Adequate 15.22 148/8/6 51.000 0.30 IN 0.680 Corner Zone psf WI> Non~std Spacing: 4/J/0 Required 60.68 148/8/6 59.000 1.03 OUT -2.980 Comer Zone psf <W2 Standard Spacing is Adequate 15.22 148/816 51.000 0.30 IN 0.680 Side Zone psf WI> Standard Spacing is Adequate 37.87 513110 44.000 0.86 OUT -1.880 Side Zone psf <W2 Standard Spacing is Ade'quate 15.22 5/3110 51.000 0.30 IN 0.680 Interior Area psf WI> Standard Spacing is Adequate 21.28 5/3110 44.006 0.48 OUT -1.080 Interior Area osf <W2 Standard Spacing is AdeQuate 15.22 5/3110 51.000 0.30 IN 0.680 Panel Data Wall/Roof Type Thickness Finish Color Direction Gable Dir Max. Length Wall: 1 Panel Rib 24 Special Request Desert Tan Left to Right Peak Out 41/0/0 Wa11:2 Panel Rib 24 Special Request Desert Tan Left to Right Peak Out 41/0/0 Waii:J Panel Rib 24 Special Request Desert Tan Left to Right Peak Out 41/0/0 Wa11:4 Panel Rib 24 Special Request Desert Tan Left to Right Peak Out 41/0/0 ~oof: A Panel Rib 24 Special Request Desert Tan System Generated Not Applicable 41/0/0 Roof: B Panel Rib 24 Special Request Desert Tan System Generated Not Applicable 41/0/0 Fastener Data Wai!/Roof Type Length Soacing Washers lnsul. Block Mod. Ctrl. lee Damming Wall:! Color Match Carbon Standard Option Standard Option No None No Yes Wa11:2 Color Match Carbon Standard Option Standard Option No None No Yes WaH:3 Color Match Carbon Standard Option Standard Option No None No Yes Wa!l:4 Color Match Carbon Standard Option Standard Option No None No Yes Roof: A Stainless Steel Capped Standard Option lee Damming Yes None No Yes File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: ?.Ia 07-27053 Calculations Hazardous Materials Occupancy /Roofc B Siainless Steel Capped Standnrd Option Ice Dammin2: Yes I None ) 0 0 File: 7079 Chevron Rl_Stress Check 10_2008 with 08_2008 Loading Version: 7.1a Date: 10/20/2008 Time: I :57:43 PM 175ofl75 No Yes (mp)2 '"1_, <"f'"f I ./1~-, I ;::::Lllli.LJ [IJJ J~T--8 T R U C f{fJI"A L ENGINEERS, LLC PEMB MODIFICATION-END POST RELOCATION CHEVRON 07-27053 RIFLE, COLORADO PREPARED FOR: VP BUILDINGS MP-SQUARED PROJECT NO. 085118CO PHASE II NOVEMBER 4, 2008 ~<'~~ Mark L. Puccio P.E., S.E. 583 D'Onofrio Drive, Suite 201, WI53719 Phone: 608-82!-4770 Fax: 608-821-4780 www.rnpsqrd.com Chevron -endpost relocate VP Buildings 3200 Players Club Circle Memphis, TN 38125-8843 STRUCTURAL DESIGN DATA Project: Chevron Name: Chevron-Endpost Changes Builder PO #: Jobsite: near DeBeque CO City, State: Rifle, Colorado 81650 County: Garfield Country: United States TABLE OF CONTENTS Date: 11/4/2008 Time: 11:28:27 Page: 1 of26 Reactions-Summary Report ................................................................................................................................. 2 Bracing-Summary Report····························································································'······································· 9 Secondary-Summary Report .............................................................................................................................. 13 Framing -Summary Report ................................................................................................................................. 17 Supplement to original design calculations for relocation and addition of end posts. File: Chevron -Endpost Changes Version: 7.1a Shape: base Builder Contact: Lany Reeves Name: Alta Construction, Inc. Address: 17 Smith Fork Way City, State Zip: Lyman, Wyoming 82937 Country: United States Loads and Codes-Shape: base Chevron -endpost relocate Project: Chevron Builder PO#: Jobsite: near DeBeque CO City, State Zip: Rifle, Colorado 81650 County, Country: Garfield, United States Date: 11/4/2008 Time: 11:28:27 City: Rifle County: Garfield Stare: Colorado 89AISC 04AISI O:mntry: United Stiltes Rainfall: 4.00 inches per hour Building Code: 2003 International Building Code Built Up: Building Use: Hazardous I Special Occupancy ColdFonn: Live Load Dead and Collateral Loads Collateral Gravity:20.00 psf Co1\ateral Uplift: 10.00 psf Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf Live Load: 20.00 psf Not Reducible Wind Load Wind Speed: 90.00 mph Wind Exposure {Factor): C (1.023) Parts Wind Exposure Factor: l .023 Wind Enclosure: Enclosed Wind Importance Factor: 1,150 Topographic Factor: 1.0000 NOT Windbome Debris Region Base Elevation: 0/0/0 Primary Zone Strip Width: 10/7/3 Parts I Portions Zone Strip Width: 5/3/10 Basic Wind Pressure: 20.74 psf Snow Load Roof Snow Load: 75.00 psf Design Snow (Sloped): 75.00 psf Snow Exposure Category (Factor): 2 Partially Exposed (1.00) Snow Importance: 1.100 Thermal Category (Factor): Heated (1.00) Ground I Roof Conversion: 0.70 %Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Unobstructed, Slippery Roof Seismic Load Mapped Spectral Response-Ss:43.60 %g Mapped Spectral Response-.81:9.10 %g Seismic Ha7..ard I Use Group: Group 2 Seismic Importance: 1.250 Seismic Perfonnance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Bracing Seismic Period: 0.2691 Framing R-Factor: 3.0000 Bracing R~Fae!:or: 3.0000 Soil Profile Type: Stiff soil (D, 4) Frame Redundancy Factor: 1.0000 Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W Per' Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain aU code and loading information for this specific building site. Load Type Descriptions D Material Dead Weight c Collateral Load CG Collateral Load for Gravity Cases cu Collateral Load for Wind Cases L Live Load ASL" Alternate Span Live Load, Shifted Right "ASL Alternate Span Live Load, Shifted Left PL2 Partial Live, Full, 2 Spans L> Live -Notional Right <L Live -Notional Left s Snow Load USl* Unbalanced Snow Load I, Shifted Right *USI Unbalanced Snow Load I, Shifted Left US2* Unbalanced Snow Load 2, Shifted Right *US2 Unbalanced Snow Load 2, Shifted Left SD Snow Drift Load ss Sliding Snow Load RS Rain Surcharge Load PFI Partial Load, Full, 1 Span PHI Partial Load, Half, 1 Span PF2 Partial Load, Full, 2 Spans PH2 Partial Load, Half, 2 Spans S> Snow -Notional Right <S Snow -Notional Left MRS Minimum Roof Snow MRS> Minimum Roof Snow-Notional Right <MRS Minimum Roof Snow· Notional Left w Wind Load WI> Wind Load, Case l, Right <WI Wind Load, Case l, Left W2> Wind Load, Case 2, Right <W2 Wind Load, Case 2, Left W3> Wind Load, Case 3, Right <W3 Wind Load, Case 3, Left W4> Wind Load, Case 4, Right <W4 Wind Load, Case 4, Left W5> Wind Load, Case 5, Right <W5 Wind Load, Case 5, Left W6> Wind Load, Case 6, Right <W6 Wind Load, Case 6, Left WP Wind Load, Parallel to Ridge WPR Wind Load, II Ridge, Right WPL Wind Load, II Ridge, Left WPAI Wind ParaliC!-Ref A, Case I File: Chevron -Endpost Changes Version: 7.1a Chevron -endpost relocate Date: 11/4/2008 Time: II :28:27 Page: 3 of26 WPA2 Wind Parallel • Ref A, Case 2 WPBI Wind Parallel· RefB, Case 1 WPB2 Wind Parallel· RefB, Case 2 WPCI Wind Parallel • Ref C, Case I WPC2 Wind Parallel-RefC, Case 2 WPDI Wind Parallel -RefD, Case I WPD2 Wind Parallel-RefD, Case 2 WBI> Wind Brace Reaction, Case I, Right <WB! Wind Brace Reaction, Case 1, Left WB2> Wind Brace Reaction, Case 2, Right <WB2 Wind Brace Rel:iction, Case 2, Left WB3> Wind Brace Reaction, Case 3, Right <WB3 Wind Brace Reaction, Case 3, Left WB4> Wind Brace Reaction, Case 4, Right <WB4 Wind Brace Reaction, Case 4, Left WBS> Wind Brace Reaction, Case 5, Right <WB5 Wind Brace Reaction, Case 5, Left WB6> Wind Brace Reaction, Case 6, Right <WB6 Wind Brace Reaction, Case 6, Left MW Minimum Wind Load MWB Minimum Wind Bracing Reaction E Seismic Load E> Seismic Load, Right <E Seismic Load, Left EG Vertical Seismic Effect EG+ Vertical Seismic Effect, Additive EG-Vertical Seismic Effect, Subtractive EB> Seismic Brace Reaction, Right' <EB Seismic Brace Reaction, Left FL Floor Live Load FL' Aftemate Span Floor Live Load, Shifted Right 'FL Alternate Span Floor Live Load, Shifted Left FD Floor Dead Load AL Auxiliary Live Load AL*> Auxiliary Live Load, Right, Right *AL> Auxiliary Live Load, Right, Left <AL* Auxiliary Live Load, Left, Right <*AL Auxiliary Live Load. LCft, Left AL' Aux. Live, Right 'AL Aux Live, Left AL'>(I) Auxiliary Live Load, Right, Right, Aisle 1 'AL>(I) Auxiliary Live Load, Right, Left, Aisle l <AL*(l) Auxiliary LiVe Load, Left, Right, Aisle l <'AL(I) Auxiliary Live Load, Left, Left, Aisle 1 AL'(I) Aux Live, Right, Aisle 1 'AL(I) Aux Live, Left, Aisle 1 AL'>(2) Auxiliary Live Load, Right, Right, Aisle 2 'AL>(2) Auxiliary Live Load, Right. Left; Aisle 2 <AL'(2) Auxiliary Live Load, Left, Right. Aisle 2 <'AL(2) Auxiliary Live Load, Left, Left, Aisle 2 AL'(2) Aux Live, Right, Aisle 2 'AL(2) Aux Live, Left, Aisle 2 AL'>(3) Auxiliary Live Load, Right, Right, Aisle 3 'AL>(3) Auxiliary Live Load, Right. Left, Aisle 3 <AL*(3) Auxiliary Live Load, Left, Right, Aisle 3 <'AL(3) Auxiliary Live Load, Left, Left, Aisle 3 AL'(3) Aux Live, Right, Aisle 3 'AL(3) Aux Live, Left, Aisle 3 AL'>(4) Auxiliary Live Load, Right, Right. Aisle 4 'Al>(4) Auxiliary Live Load, Right. Left, Aisle 4 <AL'(4) Auxiliary Live Load. Left, Right. Aisle 4 <*AL(4) Auxiliary Live Load, Left, Left, Aisle 4 AL'(4) Aux Live, Right, Aisle 4 *AL(4) Aux Live, Left, Aisle 4 AL'>(S) Auxiliary Live Load, Right, Right, Aisle 5 'AL>(S) Auxiliary Live Load, Right. Left, Aisle 5 <AL*(5) Auxiliary Live L<>ad, Left, Right, Aisle 5 <*AL(5) Auxiliary Live Load, Left, Left, Aisle 5 AL*(S) Aux Live, Right, Aisle 5 'AL(5) At.ix Live, Left, Aisle 5 ALB Aux Live Bracing Reaction ALB> Aux Live Bracing Reaction, Right <ALB Aux Live Bracing Reaction, Left WALB> Wind, Aux Live Bracing Reaction, Right <WALB Wind, Aux Live Bracing Reaction, Left ALB>(!) Aux Live Bracing Reaction, Right. Aisle l <ALB(!) Aux Live Bracing Reaction, Left, Aisle 1 WALB>(I) Wind, Aux Live Bracing Reaction, Right, Aisle 1 <WALB(I) Wind, Aux Live Bracing Reaction, Left, Aisle_ 1 ALB>(2) Aux Live Bracing Reaction, Right, Aisle 2 <ALB(2) Aux Live Bracing Reaction, Left, Aisle 2 WALB>(2) Wind, Aux Live Bracing Reaction, Right, Aisle 2 <WALB(2) Wind, Aux Live Bracing Reaction, Left, Aisle 2 ALB>(3) Aux Live Bracing Reaction, Right, Aisle 3 <ALB(3) Aux Live Bracing Reaction, Left, Aisle 3 WALB>(3) Wind, Aux Live Bracing Reaction, Right, Aisle 3 <WALB(3) Wind, Aux Live Bracing Reaction, Left, Aisle 3 ALB>(4) Aux Live Bracing Reaction, Right, Aisle 4 <ALB(4) Aux Live Bracing Reaction, Left, Aisle 4 WALB>(4) Wind, Aux Live Bracing Reaction, Right, Aisle 4 <WALB(4) Wind, Aux Live Bracing Reaction, Left, Aisle 4 ALB>(5) Aux Live Bracing Reaction, Right, Aisle 5 <ALB(5) Aux Live Bracing Reaction, Left, Aisle 5 WALB>(S) Wind, Aux Live Bracing Reaction, Right, Aisle 5 <WALB(5) Wind, Aux Live Bracing Reaction, Left, Aisle 5 WALB Wind, Aux Live Bracing. Reaction AD Auxiliary Dead Load uo User Defined Load Ul User Defined Load ~ I U2 User Defined Load - 2 U3 User Defined Load -3 U4 User Defined Load - 4 us User Defined Load -5 U6 User Defined Load - 6 U7 User Defined Load ~ 7 U8 User Defined Load • 8 U9 User Defined Load-9 UB User Brace Reaction UBI User Brace Reaction-I UB2 User Brace Reaction - 2 UB3 User Brace Reaction-3 UB4 User Brace Reaction -4 UBS User Brace Reaction -5 UB6 User Brace Reaction· - 6 UB7 User Brace Reaction -7 UB8 User Brace Reaction - 8 UB9 User Brace Reaction -9 R Rain Load T Temperature Load v Shear File: Chevron-Endpost Changes Version: ?.Ia Chevron -endpost relocate OveraU Bulldin2 Description Shape Ovem\1 Overall Floor Area Wall Area Roof Area Max. Eave Width Length (SQ. ft.) (sQ. ft.) (SQ. ft.) Heillht base 53/0/0 154/0/0 8162 13716 8604 32/0/0 Min. Eave Height2 32/0/0 Date: 11/4/2008 Time: II :28:27 Page: 4 of26 Max. Roof Min. Roof Peak Pitch Pitch Height 4.000:12 4.000:12 40/10/0 From Grid To Grid Width Len h Eave Ht. Eave Ht. 2 Pitch Pitch 2 Dist. to Rid Peak Hei ht 1-A 1-E 53/0/0 154/0/0 32/0/0 32/0/0 4.000:12 4.000:12 26/6/0 40/10/0 20'-0" 18'.6" 20'.0" 20',0" I 9'-3" I M @ 4 ·-. File: Chevron-Endpost Changes Version: ?.Ia Wall: 4, Frame at: 0/6/0 D . L C b" . esum oad om mabons -Framin No. Origin Factor l System LOOO 2 System LOOO 3 System LOOO 4 System LOOO 5 System LOOO 6 System 1.000 7 System 1.000 8 System 1.000 9 System 1.000 10 System 1.000 ll System LOOO 12 System 1.000 13 System LOOO 14 System 1.000 15 System 1.000 16 System 1.000 17 System 1.000 18 System 1.000 19 System 1.000 20 System 1.000 21 System 1.000 22 System 1.000 23 System 1.000 24 System 1.000 25 System 1.000 26 System 1.000 27 System 1.000 28 System 1.000 29 System 1.000 30 System 1.000 31 System 1.000 32 System 1.000 33 System 1.000 34 System 1.000 35 System LOOO 36 System Derived 1.000 37 System Derived 1.000 38 System Derived 1.000 39 System Derived 1.000 40 System Derived 1.000 41 System Derived 1.000 42 System Derived 1.000 43 System Derived LOOO 44 System Derived LOOO 45 System Derived 1.000 46 System Derived 1.000 47 System Derived 1.000 48 System Derived 1.000 49 System Derived 1.000 so System Derived 1.000 51 System Derived 1.000 52 System Derived 1.000 53 System Derived LOOO 54 System Derived 1.000 55 System Derived 1.000 56 System Derived 1.000 57 System Derived LOOO 58 System Derived 1.000 59 System Derived LOOO 60 System Derived LOOO 61 System Derived LOOO 62 System Derived 1.000 File: Chevron -Endpost Changes Chevron -endpost relocate Application LOD+ LOAD+ LOCO+ LOS l.OD+ LOAD+ I.OCG+ 1.0 USl* LO D + LOAD+ LO CG + LO *US! l.OD+ LOAD+ l.OCG+ !.OWl> l.OD+ LOAD+ l.OCG+ l.O<Wl 1.0 D + LO AD+ 1.0 CG + 1.0 W2> 1.0 D + l.O AD+ 1.0 CG + LO <W2 1.0 D + 1.0 AD+ LO CG + 0.750 S +0.750 Wl> 1.0 D + l.O AD+ 1.0 CG + 0.750 S + 0.750 <Wl 1.0 D + l.O AD+ 1.0 CG + 0.750 S + 0.750 W2> l.O D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <W2 1.0 D + l.O AD+ 1.0 CG + 1.0 *Al> 1.0 D + l.O AD+ l.O CG + l.O AL*> 1.0 D + l.O AD+ l.O CG + 1.0 <* AL 1.0 D + l.O AD+ 1.0 CG + 1.0 <AL* .600 D + o.600 AD+ o.600 CU + 1.0 Wl> .600 D + 0.600 AD+ Q.600 CU + 1.0 <Wl .600 D + 0.600 AD+ 0.600 CU + 1.0 W2> .600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 1.0 D + l.O AD+ l.O CG +0.563 S +0.750 *AI> 1.0 D + 1.0 AD+ 1.0 CG +0.563 S +0.750 AL*> 1.0 D+ 1.0 AD+ 1.0 CG +0.563 S +0.750 <*AL 1.0 D+ l.O AD+ l.OCG +0.563 5+0.750 <AL* 1.0 D+ 1.0 AD+ 1.0 CG +0.375 W1>+0.750 *AL> 1.0 D+ 1.0 AD+ 1.0 CG +0.375 Wl>+0.750AL*> 1.0 D + 1.0 AD+ 1.0 CG +0.375 <Wl +0.750<*AL 1.0 D + l.O AD+ 1.0 CG +0.375 <Wl +0.750<AL* 1.0 D + l.O AD+ 1.0 CG +0.375 W2>+0.750 *AL> 1.0 D + 1.0 AD+ 1.0 CG + 0.375 W2> + 0.750 AL *> 1.0 D+ l.O AD+ 1.0 CG +0.375 <W2 +0.750<*AL 1.0 D+ 1.0 AD+ 1.0 CG +0.375 <W2 +0.750 <AL* 1.0 D+ 1.0 AD+ 1.0 CG + 0.150 S +0.750 E>+0.700 EG+ 1.0 D + 1.0 AD+ l.O CG +0.150 S +0.750 <E+0.700 EG+ .600 D + o.600 AD+ o.600 CU + 0.700 E>+ 0.700 EG· .600 D + o.600 AD+ o.600 CU + 0.700 <E + 0.700 EG· 1.0 D+ l.O AD+ LO CG +0.150 S +0.750 EB> +0.700 EG+ .600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0. 700 EG- 1.0 D+ l.O AD+ 1.0 CG +0.150 5+0.750 <EB +0.700 EG+ 0.600 D + 0.600 AD+ Q.600 CU + 0.700 <EB + 0.700 EG- 1.0 D+ l.O AD+ 1.0 CG + 1.0 WPAl 1.0 D + l.O AD+ 1.0 CG +0.750 S +0.750 WPAl .600 iH0.600 AD+ 0.600 CU + 1.0 WPAl 1.0 D+ 1.0 AD+ 1.0 CG +0.375 WPAI +0.750 *AL +0.750 ALB> 1.0 D+ 1.0 AD+ 1.0 CG +0.375 WPAI +0.750 AL* + 0.750 ALB> LO D + l.O AD+ 1.0 CG + LO WPDl LO D + LOAD+ 1.0 CG + 0.750 S + 0.750 WPDl 0.600 D + 0.600 AD +0.600 CU + LO WPDl 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPDl +0.750 *AL +0.750 <ALB 1.0 D+ 1.0 AD+ J.OCG +0.375 WPDl +0.750 AL* +0.750<ALB 1.0 D + 1.0 AD+ LO CG + LO WPA2 1.0 D + l.O AD+ LO CG + 0.750 S +0.750 WPA2 0.600 D +0.600 AD +0.600 CU + 1.0 WPA2 1.0 D+ 1.0 AD+ 1.0 CG + 0.375 WPA2 +0.750 *AL + 0.750 ALB> l.O D + l.O AD+ 1.0 CG + 0.375 WPA2 +0.750 AL* + 0.750 ALB> LO D + 1.0 AD + 1.0 CG + l.O WPD2 LO D + l.O AD+ LO CG + 0.750 S + 0.750 WPD2 o.600 D + 0.600 AD+ o.600 CU + 1.0 WPD2 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPD2 +0.750 *AL + 0.750 <ALB 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPD2 +0.750 AL* + 0.750 <ALB 1.0 D + 1.0 AD+ 1.0 CG + LO WPBl 1.0 D + l.O AD+ 1.0 CG + 0.750 S + 0.750 WPBl 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPBl Date: 11/4/2008 Time: II :28:27 Page: 5 of26 Descrintion )HAD+CG+S D+AD+CG+USI* D+AD+CG+*USI D+AD+CG+Wl> D+AD+CG+<Wl D+AD+CG+W2> D+AD+CG+<W2 D+AD+CG+S+Wl> D+Ari+CG+S+<Wl D+AD+CG+S+W2> D+AD+CG+S+<W2 D+AD+CG+*AL> D +AD+ CG+AL •> D +AD+ CG+<*AL D +AD+ CG+<AL * D+AD+CU+WI> D+AD+CU+<Wl D+AD+CU+W2> D+AD+CU+<W2 fD+AD+CG+S+*AL> fD+AD+CG+S+AL*> io+AD+CG+S+<*AL io+AD+CG+S+<AL* io+AD+CG+Wl>+*Al> D+AD+CG+Wl>+AL*> D+AD+CG+<Wtf<*AL D+AD+CG +<Wl+<AL* D +AD+ CG + W2>+*AL> D+AD+CG+W2>+AL*> D +AD+ CG + <W2+<*AL D+AD+CG+<W2+<AL* D+AD+CG+S+E>+EG+ D+AD+CG+S+<E+EG+ D+AD+CU+E>+EG· D+AD+CU+<E+EG- D+AD+CG+S+EB>+EG+ D+AD+CU+EB>+EG- D+AD+CG+S+<EB+EG+ D+AD+CU+<EB+EG- D+AD+CG+WPAl D+AD+CG+S+WPAl D+AD+CU.+WPAl p+AD+CG+WPAI+*AL+ALB> :0+AD+CG+WPA1+AL*+ALB> D+AD+CG+WPDl D+AD+CG+S+WPDl D+AD+CU+WPDl D+AD+CG+WPDl+*AL+<ALB D+AD+CG+WPDI+AL*+<ALB D+AD+CG+WPA2 D+AD+CG+S+WPA2 D +AD+ CU + WPA2 D+AD+CG+WPA2+*AL+ALB> D+AD+CG+WP A2+AL *+ALB> D+AD+CG+WPD2 D+AD+CG+S+WPD2 D+AD+CU+WPD2 D+AD+CG+WPD2+*AL+<ALB D+AD+CG+WPD2+AL *+<ALB D+AD+CG+WPBI D+AD+CG+S+WPBI D+AD+CU+WPBI Version: 7.Ja 63 System Derived !.000 64 System Derived 1.000 65 System Derived 1.000 66 System Derived 1.000 67 System Derived 1.000 68 System Derived 1.000 69 System Derived 1.000 70 System Derived !.000 71 System Derived 1.000 72 System Derived 1.000 73 SYstem Derived 1.000 74 System Derived 1.000 75 System Derived 1.000 76 System Derived !.000 77 System Derived !.000 78 System Derived !.000 79 System Derived 1.000 80 System Derived 1.000 81 System Derived 1.000 82 System Derived 1.000 83 System Derived 1.000 84 System Derived 1.000 85 System Derived 1.000 86 System Derived 1.000 87 System Derived 1.000 88 System Derived 1.000 89 Svstem Derived 1.000 File: Chevron -Endpost Changes Chevron -endpost relocate 1.0 D + l.O AD+ 1.0 CG +0.375 WPBI +0.750 *AL + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPBI +0.750 AL' + 0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPCI 1.0 D + !.0 AD+ 1.0 CG + 0.750 S +0.750 WPCI 0.600 0+0.600 AD+0.600 CU + !.0 WPCI 1.0 D + !.0 AD+ 1.0 CG +0.375 WPCI +0.750 *AL + 0.750 <ALB 1.0 D -f 1.0 AD+ 1.0 CG +0.375 WPCl + 0.750 AL* + 0.750 <ALB 1.0 D + !.0 AD+ 1.0 CG + 1.0 WPB2 1.0 D + !.0 AD+ 1.0 CG + 0.750 S + 0.750 WPB2 0.600 D + 0.600 AD+ 0.600 CU + 1.0 WPB2 1.0 D+ LOAD+ 1.0 CG +0.375 WPB2 +0.750 *AL +0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPB2 +0.750 AL* + 0.750 ALB> !.0 D + 1.0 AD+ 1.0 CG + !.0 WPC2 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC2 0.600 D + 0.600 AD+ 0.600 CU + !.0 WPC2 1.0 D + 1.0 AD+ l.O CG + 0.375 WPC2 +0.750 "'AL + 0.750 <ALB !.0 D + !.0 AD+ 1.0 CG +0.375 WPC2 +0.750 AL* + 0.750 <ALB 1.0 D + 1.0 AD + 1.0 CG + 1.0 S + 1.0 ALB> 1.0 D+ 1.0 AD+ 1.0 CG + 1.0 "'AL+ 1.0 ALB> 1.0 D + 1.0 AD+ l.O CG + 1.0 AL* + l.OALB> 1.0 D + 1.0 AD+ 1.0 CG +0.563 S+0.750 *AL +0.750 ALB> 1.0 D+ 1.0 AD+ J.OCG +0.563 8+0.750 AL* +0.750 ALB> 1.0 D + 1.0 AD+ 1.0 CG + 1.0 S + 1.0 <ALB 1.0 D + 1.0 AD + 1.0 CG + 1.0 * AL + 1.0 <ALB l.OD+ l.OAD+ l.OCG+ l.OAL*+ l.O<ALB 1.0 D + 1.0 AD+ 1.0 CG +0.563 S + 0.750 *AL+0.750 <ALB 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 AL * + 0.750 <ALB Date: 11/4/2008 Time: 11:28:27 Page: 6 of26 D+AD+CG+WPBI+*AL+ALB> jD+AD+CG+WPB HAL *+ALB> D+AD+CG+WPCI D+AD +CG+S+WPCI D+AD+CU+WPCI D+AD+CG+WPCI+*AL+<ALB D+AD+CG+WPCI+AL*+<ALB D+AD+CG+WPB2 D+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AO+CG+WPB2+*AL+ALB> D+AD+CG+WPB2+AL *+ALB> D+AD+CG+WPC2 D+AD+CG+S+WPC2 D+AD+CU+WPC2 D+AD+CG+WPC2+*AL+<ALB D+AD+CG+WPC2+AL*+<ALB D+AD+CG+S+ALB> D+AD+CG+*AL+ALB> D +AD+ CG+AL "'+ALB> D+AD+CG+S+*AL+ALB> I_?+AD+CG+S+AL*+ALB> D+AD +CG+S+<ALB D +AD + CG+* AL +<ALB D +AD + CG+AL *+<ALB D+AD+CG+S+*AL+<ALB D+AD+CG+S+AL *+<ALB Version: 7.la Chevron -endpost relocate Date: 11/4/2008 Time: II :28:27 Page: 7 of26 Wall: 4, Frame at: 0/6/0 Frame ID:FL l :Rigid Frame with Endposts Frame Type:Rigid Frame, End Posts y Vy Vy Vy Vy Values shown are resisting forces of the foundation. Reactions~ Unfactored Load Tvne at Frame Cross Section: 1 Type Exterior Column Interior Column Interior Column Interior Colwnn Exterior Column X-Loc 0/0/0 15/0/0 2!19/0 44/9/0 53/0/0 Gridl -Grid2 1-E 1-D 1-C 1-B I-A Base Plate W x L (in.} 9 X 13 8x16 8 X 16 8x 16 9 X 13 Base Plate Thickness (in.) 0.500 0.375 0.375 0.375 0.500 Anchor Rod Qty/Diam. (in.) 4-!.000 4-0.750 4. 0.750 4-0.750 4-!.000 Colunm Base Elev. 100'-0" 100'..()" 100'-0" 100'-0" 100'-0" Load Tvoe Desc. Hx Hz vi Hx Hz Vv Hx Hz Vy Hx Hz Vv Hx Hz Vv D Fnn 0.9 -4.8 --0.8 --!.0 --0.7 -0.9 -4.8 AD Fnn 0.1 -!.2 ---------0.1 !.2 CG Fnn 2.7 -!0.6 ----------2.7 -10.6 s Fnn 10.2 -39.8 ---------10.2 -39.7 USl* Fnn 9.1 -23.6 ---------9.1 -48.0 *USI Frm 9.1 -48.0 ---------9.1 -23.6 WI> Fnn -7.2 --12.4 -4.2 --5.9 --5.5 --4.8 --4.4 <WI Frm 4.8 --4.4 --3.7 ---5.3 ---5.0 -7.2 --12.4 W2> Fnn -8.7 --8.4 --------3.3 --0.5 <W2 Frm 3.3 --0.5 --------8.7 -8.4 *AL> Frm -0.0 -7.7 ---. ------!.4 -3.6 AL*> Frm -0.0 -2.1 ---. -----1.4 -9.3 <*AL Frm !.4 -9.3 ------0.0 -2.1 <AL* Frm !.4 -3.6 --------0.0 7.7 cu Frm 1.4 -5.3 --------1.4 -5.3 E> Frm -4.0 --5.4 -0.1 --0.1 --0.1 --4.0 -5.4 EG+ Frm 0.4 -!.4 -. -----0.4 -!.4 <E Fnn 4.0 -5.4 --0.1 --0.1 ---0.1 -4.0 --5.4 EG· Fnn -0.4 --1.4 --------0.4 -1.4 EB> Brc --0.0 ----------- <EB Brc -0.0 ------0.0 WPAI Brc !.9 --9.6 --------!.9 -9.6 'AL Fnn 0.7 -8.5 --------0.7 2.9 ALB> Brc ------------ AL' Frm 0.7 2.9 -. -----0.7 8.5 WPDI Brc 2.5 --7.3 -------2.5 --7.3 <ALB Brc -----. --. - WPA2 Brc 0.4 -5.6 ---------0.4 -5.6 WPD2 Brc !.0 -. -3.3 ---. ----!.0 -3.3 WPBI Brc !.9 --9.6 -------!.9 -9.6 WPC1 Brc 2.5 --7.3 . -----2.5 -7.3 File: Chevron -Endpost Changes Version: 7.1a WPB2 WPC2 Brc Brc 0.4 1.0 Chevron -endpost relocate -5.6 -3.3 Maximum Combined Reactions Summary with Factored Loads~ Framine XwLOC Grid Hrz left Load Hrz Right Load Hrzln Load Hrz Out Load Uplift (-Hx) Case (~~) Case (-~;) Case (Hz) Case (-Vy) • (k) (k). fk) 01010 1-E 7.2 18 15.0 9 0.0 36 0.0 38 5.6 15/0/0 1-D " " 3.7 5 4.2 4 " 2119/0 1-C " " " 5.3 5 5.9 4 " 441910 1-B " " " -5.0 5 5.5 4 - 5310/0 1-A 15.0 8 7.2 19 " -0.0 38 5.6 File: Chevron -Endpost Changes Load Case 16 " " 17 Vrt Down Load (Vy) Case fk) 64.6 3 0.8 1 1.0 I 0.7 1 64.6 2 Date: 11/4/2008 Time: II :28:27 Page: 8 of26 -0.4 -5.6 -1.0 -3.3 Momcw Load Momccw Load (-Mzz) Case (Mzz) Case fin-ki (in-k) - ---" " - " " " " " " -" ---- Version: 7.la Chevron -endpost relocate Shape: base Loads and Codes ~ Shape: base City: Rifle County: Garfield State: Colorado 89AISC 04AISI Building Code: 2003 International Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind Load Wind Speed: 90.00 mph Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: 1.023 Wind Enclosure: Enclosed Wind Importance Factor: 1.150 Topographic Factor: 1.0000 NOT Windbome Debris Region Base Elevation: 01010 Primary Zone Strip Width: 101713 Parts I Portions Zone Strip Width: 513110 Basic Wind Pressure: 20.74psf Defledion Conditions Built Up: ColdFonn: Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf Snow Load Roof Snow Load: 75.00 psf Design Snow (Sloped): 75.00 psf Snow Exposure Category (Factor): 2 Partially Exposed (1.00) Snow Importance: t.IOO Thermal Category (Factor): Heated (l.OO) Ground I Roof Conversion: 0.70 % Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Unobstructed, Slippery Roof Frames are vertically supporting:Metal RoofPur1ins and Panels Deflection Limit Override Vl240 Frames are laterally supporting:Underhung Crane Deflection Limit Override H/400 Purlins are supporting:Metal Roof Panels Deflection Limit Override V /240 Girts are supporting:Metal Wall Panels Deflection Limit Override Hl240 Date: 11/4/2008 Time: II :28:27 Country: United_States Rainfall: 4.00 inches per hour Live Load Live Load: 20.00 psf Not Reducible Seismic Load Mapped Spectral Response ~· Ss:43.60 %g Mapped Spectral Response~ Sl:9.10 %g Seismic Hazard I Use Group: Group 2 Seismic Importance: 1.250 Seismic Perfonnance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Bracing Seismic Period: 0.2691 Framing R~Factor: 3.0000 Bracing R~Factor: 3.0000 Soil Profile Type: Stiff soil (D, 4) Frame Redundancy Factor: 1.0000 Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer tO obtain all code and loading information for this specific building site. Design Load Combinations-Bracin No. Origin Factor Aoolicatioil Descrintion I System 1.000 0.700 E> E> 2 System 1.000 0.700 <E <E 3 System 1.000 1.0 WPAI WPAI 4 System 1.000 1.0 WPDI WPDI 5 System 1.000 I.OWPA2 WPA2 6 System 1.000 I.OWPD2 WPD2 7 System 1.000 1.0 WPBI WPBI 8 System. 1.000 I.OWPCI WPCI 9 System 1.000 1.0 WPB2 WPB2 10 System 1.000 1.0 WPC2 WPC2 11 System 1.000 0.375 WPAI + 0.750 AL* WPAI+AL* 12 System 1.000 0.375 WPDI + 0.750 'AL WPDI+*AL 13 System 1.000 0.375 WPA2 +0.750 AL* WPA2+AL* 14 System 1.000 0.375 WPD2 +0.750 *AL WPD2+*AL IS System 1.000 0.375 WPBl + 0.750 AL* WPBI+AL* 16 System 1.000 .375 WPCJ + 0.750 *AL WPCI+*AL 17 System 1.000 0.375 WPB2 + 0.750 AL' WPB2+AL* File: Chevron -Endpost Changes Version: 7.Ia 181 19 20 System System Svstem Chevron -endpost relocate 1.000 .375 WPC2 + 0.750 *AL 1.000 1.0 AL * 1.000 1.0 'AL File: Chevron -Endpost Changes WPC2+*AL AL' *AL Version: 7.la Date: 11/4/2008 Time: 11 :28:27 Page: 10 of 26 Chevron -endpost relocate Date: 11/4/2008 Time: 11:28:27 Page: 11 of 26 Dia2onal Bracim:! Member Deshm Summarv: Roof A Mem. Bracing Length Angle Design Seismic Stress Stress Governing Design Connnent No. Shape (ftl Axial(!<) Factor Factor Ratio Load Case Status I R0.5 19.43 17.5 -2.25 1.0000 1.0000 0.435 0.700<E passed 2 RO.S 19.43 17.5 -2.23 1.0000 1.0000 0.431 0.700E> passed 3 RO.S 20.07 23.4 -3.00 1.0000 1.0000 0.579 0.700<E passed 4 R0.5 20,07 23.4 -2.98 1.0000 1.0000 0.575 o.7ooE> passed s R0.75 21.24 30.7 -8.43 I.OOQO 1.0000 0.723 0.700<E passed 6 R0.75 21.24 30.7 -8.37 1.0000 1.0000 0.717 0.700E> passed 7 R0.75 19.66 21.0 -11.44 1.0000 1.0000 0.981 0.700<E passed 8 R0.75 19.66 21.0 -11.66 1.0000 1.0000 1.000 0.700E> passed 9 RO.S 19.43 17.5 -2.23 1.0000 1.0000 0.431 0.700<E passed 10 R0.5 19.43 17.5 -2.25 1.0000 1.0000 0.435 0.700E> passed 11 RO.S 20,07 23.4 -2.98 1.0000 1.0000 0.575 0.700<E passed 12 RO.S 20,07 23.4 -3.00 1.0000 1.0000 0.579 0.700E> passed 13 R0.75 21.24 30.7 -8.37 1.0000 1.0000 0.717 0.700<E passed 14 R0.75 21.24 30.7 -8.43 1.0000 1.0000 0.723 0.700E> passed 15 R0.75 19.66 21.0 -11.66 1.0000 1.0000 1.000 0.700<E passed 16 R0.75 19.66 21.0 -11.44 1.0000 1.0000 0.981 0.700E> I passed Mem. End Diagonal Connection Design Information I Left Slot: web thk = 3/16 in., F -2.25k, E-factor = 1.000, stress increase = 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = 3/16 in., F = 2.25k, E factor= 1 .000, stress increase= 1 .000, slot offset"" 2 in., web/flange weld OK, web direct shear OK, web unchine shear OK, tensile fracture of web OK>> passed 2 Left Slot: web thk -3/16 in., F -2.23k, E factor 1.000, stress increase 1.000, slot offset 2 in., web/flange weld OK, web direct shear OK, web [punching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = 3116 in., F = 2.23k, E factor= 1.000, stress increase = 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK tensile fracture of web OK>> passed 3 Left Slot: web thk = 3116 in., F"" 3.00k, E factor= 1.000, stress increase.= 1 .000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web Right !J>unching shear OK, tensile fracture of web OK>> passed Jot: web thk = 1/4 in., F = 3.00k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed 4 Left Slot: web thk-1/4 in., F-2.98k, E factor= 1.000, stress increase-1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Right Slot: web thk = 3/16 in., F = 2.98k, E factor= 1.000, stress increase= 1 .000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed 5 Left Slot: web thk-1/4 in., F-8.43k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Right Slot:.web thk = l/4 in., F = 8.43k, E factor= 1 .000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK tensile fracture of web OK>> passed 6 Left Slot: web thk = J/4 in., F-8.37k, E factor= 1.000, stress increase-1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web File: Chevron -Endpost Changes Version: 7.la Right 7 Left Right 8 Left Right 9 Left Right lO Left Right II Left Right 12 Left Right 13 Left Right 14 Left Right 15 Left Right 16 Left Right Chevron -endpost relocate unching shear OK, tensile fracture of web OK>> passed Date: 11/4/2008 Time: 11:28:27 Page: 12 of 26 Slot: web thk = 1/4 in., F = 8.37k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> p~ssed Slot w/ Backing Plate: web thk-1/4 in., F = 11.44k, E factor= 1.000, stress increase 1.000, slot offset -2 in., web/flange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = 1/4 in., F = 11.44k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK web ounchin.l!: shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk-l/4 in., F-l1.66k, E factor 1.000, stress increase -1.000, slot offset - 2 in., web/flange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = 1/4 in., F = 11.66k, E factor= 1.000, stress increase=, 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot: web thk = 3/16 in., F-2.23k, E factor= I .000, stress increase-1.000, slot offset= 2'in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> pcissed Slot: web thk = 3/16 in., F = 2.23k, E factor= 1.000, stress increase = 1 .000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unchingshear OK, tensile fracture of web OK>> oassed . Slot: web thk 3116 in., F 2.25k, E factor-l .000, stress increase 1.000, slot offset-2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Slot: web thk = 3/16 in., F = 2.25k, E factor= 1.000, stress increase= 1 .000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK tensile fracture of web OK>> passed Slot: web thk = 3/16 in., F = 2.98k, E factor= 1.000, stress increase-1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web punching shear OK, tensile fracture of web OK>> passed Jot: web thk = l/4 in., F = 2.98k, E factor= 1.0001 stress increase= l.OOO,slot offset =2 in., web/flange weld OK, web direct shear OK, web unchine: shear OK tensile fracture of web OK>> oassed Slot: web thk = 1/4 in., F = 3.00k, E factor= 1 .000, stress increase= 1.000, slot offset-2 in., web/flange weld OK. web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Jot: web thk = 3/16 in., F = 3.00k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK. web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk = l/4 in., F = 8.37k, E factor-1.000, stress increase = 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk = 1/4 in., F = 8.37k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web direct shear OK, web unchin2 shear OK tensile fracture of web OK>> passed Slot: web thk = 1/4 in., F = 8.43k, E factor-1.000, stress increase = 1.000, slot offSet 2 in., web/flange weld OK, web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot: web thk = l/4 in., F = 8.43k, E factor= 1.000, stress increase = 1.000, slot offse~ = 2 in., web/flange weld OK. web direct shear OK, web unching shear OK, tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk -114 in., F = ll.66k, E factor-1.000, stress increase-1.000, slot offset-2 in., web/flange weld OK, web irect shear OK, web punching shear OK. tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk = I/4 in., F = ll.66k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web irect shear oi. web punching shear OK tensile fracture of web OK>> passed Slot w/ Backing Plate: web thk-114 in., F 11.44k, E factor= 1.000, stress increase 1.000, slot offset= 2 in., web/flange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed lot w/ Backing Plate: web thk = l/4 in., F = 11.44k, E factor= 1.000, stress increase= 1.000, slot offset= 2 in., web/flange weld OK, web irect shear OK, web punching shear OK, tensile fracture of web OK>> passed Strut Bracine: Member Desie.n Summary: Roof A Mem. Bracing Length Design Seismic Stress Stress Governing Design Description No. Shape (ftl Axial(k) Factor Factor Ratio Load Case Status 13 FF 2.5xO.l 05x8.5 18.50 11.73 2.5000 1.2750 0.974 0.700E> passed Eave Strut, Collector 30 FF 2.5x0.105x8.5 18.50 11.74 2.5000 1.2750 0.975 0.700<£ passed Eave Strut, Collector clip to to tensile rupture & block shear OK, clip buckling OK, clip to web weld 3/16 fillet one side, clip to File: Chevron -Endpost Changes Version: 7.la Loads and Codes-Shape: base City: Rifle County: Building Code: 2003 International Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind Load Wind Speed: 90.00 mph Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: l .023 Wind Enclosure: Enclosed Wind Importance Factor; 1.150 Topographic Factor: 1.0000 NOT Windbome Debris Region Base Elevation: 01010 Primary Zone Strip Width: 10/7/3 Parts I PQrtions Zone Strip Width: 5/3/l 0 Basic Wind Pressure: 20.74 psf Chevron -endpost relocate Garfield State: Built Up: Cold Fonn: Colorado 89AISC 04AISI Roof Covering+ Second. Dead Load: 3.3'9 psf Frame Weight (assumed fOr seismic):8.00 psf Snow Load Roof Snow Load; 75.00 psf Design Snow (Sloped): 75.00 psf Snow Exposure Category (Factor): 2 Partially Exposed (l.OO) Snow Importance: 1,100 Thennal Category (Factor): Heated (1.00) Ground I Roof Conversion: 0.70 %Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Unobstructed, Slippery Roof . Date: 11/4/2008 Time: II :28:27 Country: United States Rainfall: 4.00 inches per hour Live Load Live Load: 20.00 psf Not Reducible Seismic Load Mapped Spectral Response~ Ss:43.60 %g Mapped Spectral Response~ Sl :9.10 %g Seismic Hazard I Use Group: Group 2 Seismic Importance: 1.250 Seismic Performance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Brilcing Seismic Period: 0.2691 Framing R~Factor: 3.0000 Bracing RwFactor: 3.0000 Soil Profile Type: Stiff soH (D, 4) Frame Redundancy Factor: l.OOOO Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain all code and loading infonnation for this specific building site. Desitm Load Combinations~ Purlin No. Origin Factor Application Description I System 1.000 l.OD+ l.OCG+ !.OS ID+CG+S 2 System 1.000 1.0 D + I.OCG + 1.0 USl* D+CG+USl* 3 System !.000 1.0 D + l.O CG + 1.0 'US! ~+CG+"USI 4 System !.000 1.0 D + I.O CG + 1.0 PFI D+CG+PFI(Span I) 5 System l.OOO 1.0 D + l.O CG + 1.0 PFI D +CG +PFI(Span 9) 6 System !.000 1.0 D + l.O CG + 1.0 PHI D+CG+PHI(Span I) 7 System 1.000 I.O D + l.O CG + 1.0 PHI D + CG + PHI(Span 9) 8 System 1.000 .0 D + l.O CG + 1.0 PF2 fo+CG+PF2(Spans 1 and2) 9 System 1.000 1.0 D + l.O CG + 1.0 PF2 D + CG + PF2(Spans 2 and 3) 10 System 1.000 !.0 D + l.O CG + 1.0 PF2 D + CG + PF2(Spans 3 and 4) II System 1.000 1.0 D + l.O CG + 1.0 PF2 jo + CG + PF2(Spans 4 and 5) I2 System 1.000 1.0 D + 1.0 CG + 1.0 PF2 jD + CG + PF2(Spans 5 and 6) I3 System 1.000 1.0 D + l.O CG + !.0 PF2 D + CG + PF2(Spans 6 and 7) I4 System 1.000 1.0 D + l.O CG + 1.0 PF2 0 + CG + PF2(Spans 7 and 8) IS System 1.000 1.0 D + l.O CG + 1.0 PF2 D + CG + PF2(Spans 8 and 9) I6 System 1.000 1.0 D + l.O CG + 1.0 Wl> D+CG+Wl> I7 System 1.000 1.0 D + 1.0 CG + 1.0 <W2 D+CG+<W2 I8 System I.OOO p.600 D + 0.600 CU + LO W1> D+CU+Wl> 19 System !.000 ~.600 D + 0.600 CU + !.0 <W2 io+CU+<W2 20 SyStem l.OOO 1.0 D + 1.0 CG + 0.750 S +0.750 WI> !o+CG+S+WJ> 2I System l.OOO 1.0 D+ 1.0 CG + 0.750 S +0.750 <W2 D+CG+S+<W2 22 System Derived 1.000 1.0 D + 1.0 CG +O.ISO S +0.750 EB> + 0.700 EG+ D+CG+S+EB>+EG+ 23 System Derived 1.200 1.200 D + 1.200 CG + 0.200 S + 1.0 EB> +0.700 EG+ ID+CG+S+EB>+EG+ 24 System Derived !.200 0.900 D + 0.900 CG + 1.0 EB> + 0.700 EG-D+CG+EB>+EGw 25 System Derived l.OOO Q.600 D +0.600 CU +0.700 EB> + 0.700 EG-io+CU+EB>+EG~ 26 System Derived 1.000 !.0 D + l.O CG +0.150 S + 0.750 <EB + 0.700 EG+ D+CG+S+<EB+EG+ 27 System Derived 1.200 1.200 D+ 1.200 CG + 0.200 S + I.O <EB +0.700 EG+ D+CG+S+<EB+EG+ 28 System Derived 1.200 0.900 D +0.900 CG + 1.0 <EB + 0.700 EG-D+CG+<EB+EGw 29 System Derived !.000 0.600 D + 0.600 CU +0.700 <EB + 0.700 EG-P+CU+<EB+EG- 30 System Derived 1.000 l.O D + l.O CG + 1.0 WPAl D+CG+WPAl File: Chevron -Endpost Changes Version: 7.la Chevron -endpost relocate 31 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPAI 32 System Derived 1.000 1.0 D+ 1.0 CG +0.750 S + 0.750 WPAI 33 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPDI 34 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPD I 35 System Derived 1.000 1.0 D + 1.0 CG +0.750 S + 0.750 WPDI 36 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPA2 37 System Derived 1.000 0.600 D +0.600 CU + 1.0 WPA2 38 System Derived 1.000 1.0 D + 1.0 CG +0.750 S + 0.750 WPA2 39 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPD2 40 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPD2 41 System Derived 1.000 1.0 D + 1.0 CG + 0.750 S + 0.750 WPD2 42 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPBI 43 SyStem Derived 1.000 o.600 D +0.600 CU + 1.0 WPB! 44 System Derived 1.000 1.0 D + 1.0 CG +0.750 S+ 0.750 WPBI 45 System Derived 1.000 1.0 D+ 1.0 CG + 1.0 WPCI 46 System Derived 1.000 0.600 D+ 0.600 CU + 1.0 WPC! 47 System Derived 1.000 1.0 D + 1.0 CG + 0.750 S + 0.750 WPCI 48 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPB2 49 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPB2 50 System Derived 1.000 1.0 D + 1.0 CG + 0.750 S + 0.750 WPB2 51 System Derived 1.000 1.0 D + 1.0 CG + 1.0 WPC2 52 System Derived 1.000 0.600 D + 0.600 CU + 1.0 WPC2 53 Svstem Derived 1.000 1.0 D + 1.0 CG +0.750 S + 0.750 WPC2 D I L C b" Gi ., n oad om mations -rt No. Origin Factor Application I System 1.000 1.0 Wl> 2 System 1.000 1.0 <W2 3 System Derived 1.000 0.700EB> 4 System Derived 1.000 I.OWPA! 5 System Derived 1.000 I.OWPA2 6 System Derived 1.000 1.0 WP!3! 7 System Derived 1.000 1.0 WPB2 8 System Oerived 1.000 0.700 <EB 9 System Derived 1.000 I.OWPD! 10 System Derived 1.000 !.OWPD2 II System Derived 1.000 LOWPC! 12 System Derived 1.000 LOWPC2 Deflection Load Combinations Purlin - No. Origin Factor Deflection Application I System !.000 240 1.0 s 2 System 1.000 240 LOUSl* 3 Svstem 1.000 240 1.0 *US! Deflection Load Combinations Girt - No. Origin Factor Deflection Application I System !.000 240 0.700WJ> 2 System 1.000 240 0.700<W2 File: Chevron -Endpost Changes Date: 11 I 4 I 2008 Time: II :28:27 Page: 14 of26 D+CU+WPAI lo+CG+S+wPAJ !D+CG+WPDI D+CU+WPDI !o+CG+S+WPDI D+CG+WPA2 !l)+CU+WPA2 D+CG+S+WPA2 D+CG+WPD2 D+CU+WPD2 ~+CG+S+WPD2 D+CG+WPBI I?+CU+WPBI D+CG+S+WPBl D+CG+WPCI D+CU+WPCI D+CG+S+WPCI !D+CG+WPB2 D+CU+WPB2 r+CG+S+WPB2 D+CG+WPC2 !D+CU +WPC2 lo+CG+S+WPC2 Description pvl> <W2 EB> WPAI WPA2 !wrBI WPB2 ~DI WPD2 WPCI WPC2 Description s US!' *US! Description WI> W2 Version: 7.Ia Chevron -endpost relocate ~· q,'' 8'-9" l 20'-D" 18'.6~ 18'.6" ?O'.N 18'.6" Maximum Secondary Desie.ns for Sba e base on Side A Detail Exterior Interior Des Len Description Design Lap % % % % Ld Lap % % % ld (ft\ Status (in:) Bnd Shr Cmb We£ Cs _(;i) Bnd Shr Cmb I, I 9.25 11.50x0.065 Z Sim Yes 0 0.02 1.01 1.01 2,1 9.25 I 1 .50x0.065 Z Sim Yes 0 O.Ql 0.78 0.78 3,1 9.25 II .50x0.065 Z Sim Yes 0 O.Ql 0.42 0.42 4,1 20.00 11.50x0.120 Z Con Yes 24 0.77 0.00 0.77 4,2 18.50 -. ll.50x0.120ZCon Yes 36 0.57 0.18 0.60 0.00 3 36 0.13 0.06 0.79 4,3 20.00 11.50x0.082ZCon Yes 48 0.52 0.27 0.59 0.00 3 36 0.38 0.81 0.89 4,4 18.50 l1.50x0.082 Z Con Yes 36 0.74 0.53 0.91 0.00 3 36 0.49 0.71 0.86 4,5 20.00 l1.50x0.082 Z Con Yes 48 0.74 0.58 0.94 0.00 3 36 0.38 0.81 0.89 4,6 18.50 l 1.50x0.120 Z Con Yes 36 0.52 0.24 0.57 0.00 3 36 0.13 0.06 0.79 4,7 20.00 1l.50xO.l20 Z Con Yes 24 0.57 0.22 0.61 0.00 3 24 0.77 0.00 0.77 5,1 20.00 11.50x0.082 Z Con Yes 36 0.98 o.oo 0.98 5,2 18.50 11.50x0.082 Z Con Yes 36 0.76 0.45 0.88 0.00 3 36 0.67 0.63 0.92 5,3 20.00 ll.50x0.082 Z Con Yes 48 0.51 0.44 0.68 0.00 3 48 0.54 0.73 0.91 5,4 18.50 I 1.50x0.065 Z Con Yes 36 0.69 0.55 0.88 0.00 3 24 0.29 0.94 0.98 5,5 20.00 11.50x0.082 Z Con Yes 48 0.69 0.60 0.92 0.00 3 48 0.54 0.73 0.91 5,6 18.50 ll.50x0.082 Z Con Yes 36 0.51 0.38 0.64 0.00 3 36 0.67 0.63 0.92 5,7 20.00 ll.50x0.082 Z Con Yes 36 0.76 0.55 0.93 0.00 3 36 0.98 0.00 0.98 6,1 20.00 II.50x0.082 Z Con Yes 36 0.98 0.00 0.98 6,2 18.50 11.50x0.082 Z Con Yes 36 0.76 0.45 0.88 0.00 3 36 0.67 0.63 0.92 6,3 20.00 11.50x0.082 Z Con Yes 48 0.51 0.44 0.68 0.00 3 48 0.54 0.73 0.91 6,4 18.50 11.50x0.065 Z Con Yes 36 0.69 0.55 0.88 0.00 3 24 0.29 0.94 0.98 6,5 20.00 1J.S0x0.082 Z Con Yes 48 0.69 0.60 0.92 0.00 3 48 0.54 0.73 0.91 6,6 18.50 11.50x0.082 Z Con Yes 36 0.51 0.38 0.64 0.00 3 36 0.67 0.63 0.92 6,7 20.00 I L50x0.082 Z Con Yes 36 0.76 0.55 0.93 0.00 3 36 0.98 0.00 0.98 7,1 20.00 11.50x0.06S Z Con Yes 36 0.36 0.89 0.96 7,2 18.50 II .50x0.065 Z Con Yes 36 0.61 0.48 0.78 0.00 3 36 0.54 0.67 0.86 7,3 20.00 11.50x0.065 Z Con Yes 48 0.41 0.47 0.62 0.00 3 24 0.43 0.78 0.89 7,4 18.50 1 I.SOx0.065 Z Con Yes 36 0.46 0.44 0.64 0.00 3 24 0.48 0.69 0.84 7,5 20.00 li.S0x:0.065 Z Con Yes 48 0.46 0.49 0.67 0.00 3 24 0.43 0.78 0.89 7,6 18.50 11.50x0.065 Z Con Yes 36 0.41 0.40 0.57 0.00 3 36 0.54 0.67 0.86 7,7 20.00 ll.50x0.065 Z Con Yes 36 0.61 0.59 0.85 0.00 3 36 0.36 0.89 0.96 8,1 9.25 lJ.50x0.06S Z Sim Yes 0 0.02 1.01 1.01 9,1 9.25 1 L50x0.065 Z Sim Yes 0 0.01 0.78 0.78 10,1 9.25 11.50x0.065 Z Sim Yes 0 O.o! 0.42 0.42 Location ft Load Case File: Chevron -Endpost Changes % Wcp 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 o.oo o.oo 0.00 0.00 o.oo o.oo 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 20'.0" Ld % Cs Bnd 3 3 3 3 0.57 23 0.52 3 0.74 3 0.74 3 0.52 27 0.57 3 3 0.76 3 0.51 3 0.69 3 0.69 3 0.51 3 0.76 3 3 0.76 3 0.51 3 0.69 3 0.69 3 0.51 3 0.76 3 3 0.61 3 0.41 3 0.46 3 0.46 3 0.41 3 0.61 3 3 3 3 Date: 11/4/2008 Time: II :28:27 Exterior % % % Ld Lap Shr Cmb Wcp Cs '(in) 0.22 0.61 0.00 3 24 0.24 0.57 0.00 3 36 0.58 0.94 0.00 3 36 0.53 0.91 0.00 3 36 0.27 0.59 0.00 3 36 0.18 0.60 0.00 3 36 0.55 0.93 0.00 3 36 0.38 0.64 0.00 3 36 0.60 0.92 0.00 3 48 0.55 0.88 0.00 3 24 0.44 0.68 0.00 3 48 0.45 0.88 0.00 3 36 0.55 0.93 0.00 3 36 0.38 0.64 0.00 3 36 0.60 0.92 0.00 3 48 0.55 0.88 0.00 3 24 0.44 0.68 0.00 3 48 0.45 0.88 0.00 3 36 0.59 0.85 0.00 3 36 0.40 0.57 0.00 3 36 0.49 0.67 0.00 3 24 0.44 0.64 0.00 3 24 0.47 0.62 0.00 3 24 0.48 0.78 0.00 3 36 Descri tion Version: ?.Ia I I -0.08 2 I -0.06 3 I -0.03 4 I -0.55 4 2 0.08 4 3 -0.35 4 4 -0.06 4 5 -0.35 4 6 0.08 4 7 -0.56 5 I -0.60 5 2 0.08 5 3 -0.28 5 4 -0.08 5 5 -0.28 5 6 0.08 5 7 -0.61 6 I -0.60 6 2 0.08 6 3 -0.28 6 4 -0.08 6 5 . -0.28 6 6 0.08 6 7 -0.61 7 I -0.41 7 2 0.05 7 3 -0.20 7 4 -0.03 7 5 -0.20 7 6 0.05 7 7 -0.41 8 I -0.08 9 I -0.06 10 I -0.03 Chevron -endpost relocate ( L/1337) 5.00 3 ( L/1725) 5.00 3 ( L/3257) 5.00 3 ( L/435) 8.50 3 ( L/2678) 24.00 3 ( L/695) 48.50 3 ( L/3525) 67.50 3 ( L/694) 87.00 3 ( L/2676) 111.50 3 ( L/432) 126.50 3 ( L/399) 8.50 3 ( L/2731) 24.00 3 ( L/852) 48.00 3 ( L/2852) 67.50 3 ( L/848) 87.00 3 ( L/2703) 111.50 3 ( L/396) 126.50 3 ( L/399) 8.50 3 (L/2731) 24.00 3 ( L/852) 48.00 3 ( L/2852) 67.50 3 ( L/848) 87.00 3 ( L/2703) 111.50 3 ( L/396) 126.50 3 ( L/589) 8.50 3 ( L/4054) 24.00 3 ( L/1180) 48.00 3 ( L/6564) 67.50 3 ( L/1176) 87.00 3 ( L/4110) 111.50 3 ( L/585) 126.50 3 ( L/1337) 4.50 3 ( L/1726) 4.50 3 ( L/3257) 4.50 3 "'USJ *US I *USJ *US! *USl *USJ *US! *USl *USI *US1 *USl *USl *USl *US! *USl *USl *USI *USI *US I *US! *USl *USJ *US! *USI *USI *USI *USl *US1 *US1 *US! "'USI *USl *USl *USl Date: 11/4/2008 Time: II :28:27 Page: 16 of 26 Purlin Anchoraee Forces for Shape base Roof A, Panel Type is PR, Pitch = 4.000:12 Bay Thickness Force(k) Ld Case # Purlins Length Simple? Diaphmgm Allowable Defl Actual Deft . Width I 0.065 -35.24 3 10 9.25 y 27.93 0.308 o.ooo 2 0.082 -76.20 3 10 20.00 N 27.93 0.667 o.ooo 3 0.082 -70.49 3 10 18.50 N 27.93 0.617 o.ooo 4 0.082 -76.20 3 10 20.00 N 27.93 0.667 0.000 5 0.065 -70.49 3 10 18.50 N 27.93 0.617 0.000 6 0.082 -76.20 3 10 20.00 N 27.93 0.667 0.000 7 0.082 -70.49 3 10 18.50 N 27.93 0.617 0.000 8 0.082 -76.20 3 10 20.00 N 27.93 0.667 0.000 9 0.065 -35.24 3 10 9.25 y 27.93 0.308 0.000 Fnn-Line Force(k) Anch, Allow Reouired Clios Actual Clios Diaohragm Allow Diaohragm Shr Stress I 0.08 0.00 0 0 0.134 0.000 0.000 2 0.87 0.00 0 0 0.134 0.000 0.000 3 1.40 0.00 0 0 0.134 0.000 0.000 4 1.40 0.00 0 0 0.134 0.000 o.ooo 5 1.74 0.00 0 0 0.134 0.000 0.000 6 1.74 0.00 0 0 0.134 0.000 0.000 7 1.40 0.00 0 0 0.134 0.000 0.000 8 1.40 0.00 0 0 Oc134 . 0.000 0.000 9 0.87 0.00 0 0 0.134 0.000 0.000 10 0.08 0.00 0 0 0.134 0.000 0.000 File: Chevron -Endpost Changes Version: 7.la Chevron -endpost relocate Loads and Codes -Shape: base City: Rifle County: Garfield State: Colorado 89AISC 04AISI Building Code: 2003 International Building Code Building Use: Hazardous I Special Occupancy Dead and Collateral Loads Collateral Gravity:20.00 psf Collateral Uplift: 10.00 psf Wind Load Wind Speed: 90.00 mph Wind Exposure (Factor): C (1.023) Parts Wind Exposure Factor: 1.023 Wind Enclosure: Enclosed Wind Importance Factor: 1.150 Topographic Factor: 1.0000 NOT Windbome Debris Region Base Elevation: 0/010 Primary Zone Strip Width: 10/713 Parts I Portions Zone Strip Width: 5/3/10 Basic Wind Pressure: 20.74 psf Deflection Conditions Built Up: Cold Fonn: Roof Covering+ Second. Dead Load: 3.39 psf Frame Weight (assumed for seismic):8.00 psf Snow Load Roof Snow Load: 75.00 psf Design Snow {Sloped): 75.00 psf Snow Exposure Category (Factor): 2 Partially Exposed (!.00) Snow Importance: l.lOO Thermal Category (Factor): Heated (1.00) Ground I Roof Conversion: 0.70 %Snow Used in Seismic: 20.00 Seismic Snow Load: 15.00 psf Unobstructed, Slippery Roof Frames are vertically supporting:Metal RoofPurlins and Panels Deflection Limit Override Vl240 Frames are laterally supporting:Underhung Crane Deflection Limit Override H/400 Purlins are supporting:Metal Roof Panels Deflection Limit Override V 1240 Girts are supporting:Metal Wall Panels Deflection Limit Override Hl240 C S hedul I t atio rane < e norm n Date: 11/4/2008 Time: II :28:27 Country: United States Rainfall: 4.00 inches per hour Live Load Live Load: 20.00 psf Not Reducible Seismic Load Mapped SpeCtral Response· Ss:43.60 %g Mapped Spectral Response· SI :9.10 %g Seismic Hazard I Use Group: Group 2 Seismic Importance: 1.250 Seismic Performance I Design Category: C System NOT detailed for Seismic Framing Seismic Period: 0.4480 Bracing Seismic Period: 0.2691 Framing R-Factor: 3.0000 Bracing R-Factor: 3.0000 Soil Profile Type: Stiff soil (0, 4) Frame Redundancy Factor: 1.0000 Brace Redundancy Factor: 1.0000 Frame Seismic Factor (Cs): 0.1354 x W Brace Seismic Factor (Cs): 0.1758 x W I Name Type Service Classification Method of Operation Capacity Bridge Bridge Construction _ __j (Ton). Soan 5tonUH Underhung Crane C (Moderate Service Pendant Operated 5.00 42/0/0 Sirigle Girder Wall·4 Namel Name2 Type Bracket Shape Start Start End End Aisle Start From From Frame Adjust. Frame Adjust. Elev. Left Right Edge Edge 5 ton UH Rigid Suspension • 3 Plate Built-up I 0/3/0 10 0/3/0 I 26/6/0 51610 5/6/0 Brackets Type Designed & Size Size Rail Size Vertical Horizontal Vertical Lateral Longitudinal Provided (lb/yd) Deflection Deflection Impact(%) Impact(% Impact(%) Wide Flange -Hot Rolled NBVP W!6 0 - -10.00 20.00 10.00 Per Article 2.9 in the Builder Agreement, VP Buildings assumes that the Builder has called the local Building Official or Project Engineer to obtain all code and loading information for this specific building site. File: Chevron -Endpost Changes Version: 7.1a I Chevron -endpost relocate Frame cross Seot;on: 1 (DESIGN TYPICAL FOR FRAME LINE 1 & 10) .• y Dimension Key I 5'-6" BL to CL of Runway Beam 2 1 5/8" 3 4'-0" 4 3'·5 1/4" 5 3'-3 3/4" 6 1'·3" 7 1'-913116" 8 2@2'-47116" 9 4 1/2" to 40'-10" Ridge Ht File: Chevron · Endpost Changes (2)FB FB X r,...,,.. •• ,... ,...,.....,...,...,... ,...,...,......,.,,....,, ,..,... ,....,...,,. •• .-o u.1r-1.-.' .. Version: 7.Ja Date: 11/4/2008 Time: II :28:27 Chevron -endpost relocate Frame Clearances Horiz. Clearance between members l(CXOO!) and 6(CX002): 45'~0 3/4" Vert. Clearance at member l{CXOOI): 28'·3 114" Vert. Clearance_at member 6(CX002): 28'~3 1/4" Finished Floor Elevation= 100'-0"{Unless Noted Otherwise) Crane Clearances at bottom of Runway Beam Vert, Clearance at CRANE DATA 1-l(Left): 2'-5 7/8" Horz. Clearance at CRANE DATA 1-l(Left): 1'-8 1/2" Vert. Clearance at CRANE DATA 1-l(Right): 2'-5 7/8" Horz. Clearance at CRANE DATA 1-1 (Right): 1 '-8 1/2" File: Chevron -Endpost Changes Version: 7.la Date: 11/4/2008 Time: II :28:27 Page: 19 of 26 Chevron -endpost relocate Date: 11/4/2008 Time: II :28:27 Page: 20 of 26 Descri tion An le Grou Trib. Override Desi Status 01610 FL l : Ri id Frame with End osts 90.0000 201010 Stress Check D . e~nLoad c b om inations • raming No. Origin Factor Application Description I System 1.000 !.OD+ LOAD+ !.OCG+ !.OS D+AD+CG+S 2 System 1.000 1.0 D + 1.0 AD+ l.O CG + 1.0 US!* D+AD+CG+USJ* 3 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 'US I D+AD+CG+*USI 4 System 1.000 1.0 D+ LOAD+ 1.0 CG + 1.0 WI> D+AD+CG+Wl> 5 System 1.000 I.OD+ l.OAD+ 1.0 CG + t.O<Wl D+AD+CG+<WI 6 System 1.000 l.OD+ l.OAD+ I.OCG + 1.0 W2> D+AD+CG+W2> 7 System 1.000 l.OD+ l.OAD+ I.OCG + l.O<W2 D+AD:I-CG+<W2 8 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WI> D+AD+CG+S+Wl> 9 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 <WI D+AD+CG+S+<Wl 10 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 W2> D+AD+CG+S+W2> II System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 <W2 D+AD+CG+S+<W2 12 System 1.000 1.0 D + 1.0 AD+ l.O CG + l.O *AL> D+AD+CG+*AL> 13 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + l.O AL*> D+AD+CG+AL*> 14 System 1.000 1.0 D + LO AP + 1.0 CG + 1.0 <*AL D+AD+CG+<~AL 15 System 1.000 I.OD+ t.OAD+ 1.0 CG+ l.O<AL* D+AD+CG+<AL* 16 System 1.000 r.600 D + 0.600 AD+ 0.600 CU + 1.0 WI> D+AD+CU+Wl> 17 System 1.000 r.600 D + 0.600 AD+ 0.600 CU + 1.0 <WI D+AD+CU+<Wl 18 System 1.000 0.600 D + D.600 AD+ D.600 CU +.1.0 W2> D+AD+CU+W2> 19 System 1.000 .600 D + 0.600 AD+ 0.600 CU + 1.0 <W2 D+AD+CU+<W2 20 System 1.000 1.0 D+ LOAD+ 1.0 CG +0.563 S +0.750 'AL> D+AD+CG+S+*AL> 21 System 1.000 1.0 D+ !.0 AD+ 1.0 CG +0.563 S + 0.750 AL'> D +AD+ CG + S+AL "'> 22 System 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.563 S +0.750<'AL D+AD+CG+S+<*AL 23 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 <AL' D+AD+CG+S+<AL' 24 System 1.000 l.O D+ l.O A.D+ 1.0 CG +0.375 WI> +0.750 *AI> D +AD+ CG + Wl>+*AL> 25 System 1.000 l.O D + 1.0 AD+ l.O CG +0.375 Wl>+0.750 AL*> D+ AD+CG+Wt>+AL*> 26 System 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 <WI +0.750<*AL D+AD+CG+<Wl+<*AL 27 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 <WI +0.750<AL* D +AD+ CG + <Wl+<AL * 28 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 W2> +0.750 "'AL> D + AD+ CG + W2>+* AL> 29 System 1.000 1.0 D + 1.0 AD+ l.O CG +0.375 W2>+0.750 AL*> D+AD+CG+W2>+AL*> 30 System 1.000 t.O D+ 1.0 AD+ 1.0 CG + 0.375 <W2 +0.750<*AL D+ AD+CG+<W2+<'AL 31 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 <W2 +0.750 <AL* D+AD+CG+<W2+<AL* 32 System 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.150 S + 0.750 E>+0.700 EG+ D+AD+CG+S+E>+EG+ 33 System 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.150 S + 0.750<E +0.700 EG+ D>AD+CG+S+<E+EG+ 34 System 1.000 .600 D + D.600 AD+ D.600 CU + 0.700 E> + 0.700 EG-D+AD+CU+E>+EG- 35 System 1.000 .600 D + 0.600 AD+ D.600 CU + 0.700 <E + 0.700 EG-D+AD+CU+<E+EG4 36 System DeriVed 1.000 !.0 D + 1.0 AD+ 1.0 CG +0.150 S +0.750 EB> +0.700 EG+ D+AD+CG+S+EB>+EG+ 37 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + 0.700 EB> + 0.700 EG-D+AD+CU+EB>+EG- 38 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.150 S +0.750 <EB +0.700 EG+ D>AD+CG+S+<EB+EG+ 39 System Derived 1.000 0.600 D + 0.600 AD+ D.600 CU + 0. 700 <EB + 0. 700 EG-D+ AD+Cl) +<EB + EG- 40 System Derived 1.000 1.0 D + 1.0 AD+ l.O CG + 1.0 WPA1 D+AD+CG+WPAI 41 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S +0.750 WPAI D+AD+CG+S+WPAI 42 System Derived 1.000 0.600 D + 0.600 AD+0.600 CU + 1.0 WPAI D+AD+CU+WPAI 43 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPAI + 0.750 *AL + 0.750 ALB> D+AD+CG+WPAI+*AL+ALB> 44 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPAI + 0.750 AL* +0.750 ALB> D+AD+CG+WPAI+AL*+ALB> 45 System Derived 1.000 J.OD+ I.OAD+ l.OCG + 1.0 WPDI. D+AD+CG+WPDI 46 System Derived 1.000 1.0 D + 1.0 AD+ !.0 CG + 0.750 S + 0.750 WPDI D+AD+CG+S+WPDl 47 System Derived 1.000 0.600 D + 0.600 AD +0.600 CU + 1.0 WPDI D+AD+CU+WPDI 48 System Derived 1.000 1.0 D + l.O AD+ 1.0 CG +0.375 WPDI + 0.750 *AL +0.750 <ALB D+AD+CG+WPDl+*AL+<ALB 49 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPDl + 0.750 AL* +0.750 <ALB D+AD+CG+WPD!+AL'+<ALB so System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG + 1.0 WPA2 D+AD+CG+WPA2 51 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.750 S +0.750 WPA2 I?+ AD+ CG +S + WPA2 52 System Derived 1.000 0.600 D + D.600 AD+ 0.600 CU + 1.0 WPA2 jo+AD+CU+WPA2 53 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPA2 + 0.750 *AL +0.750 ALB> D+AD+CG+WPA2+*AL+ALB> 54 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPA2 + 0.750 AL* + 0.750 ALB> D+AD+CG+WPA2+AL *+ALB> 55 System Derived 1.000 1.0 D + 1.0 AD + 1.0 CG + 1.0 WPD2 jo+AD+CG+WPD2 56 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.750 S + 0.750 WPD2 ID+AD+CG+S+WPD2 57 System Derived 1.000 D.600 D + 0.600 AD+ 0.600 CU + I .0 WPD2 D+AD+CU+WPD2 File: Chevron -Endpost Changes Version: 7.1 a Chevron -endpost relocate 58 System Derived 1.000 1.0 D + l.O AD+ 1.0 CG + 0.375 WPD2 + 0.750 *AL + 0.750 <ALB 59 System Derived 1.000 1.0 D + 1.0 AD+ LO CG + 0.375 WPD2 +0.750 AL* + 0.750 <ALB 60 System Derived 1.000 1.0 D +1.0 AD + 1.0 CG + 1.0 WPB 1 61 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPB1 62 System Derived 1.000 0.600 D + 0.600 AD +0.600 CU + 1.0 WPB1 63 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.375 WPBl +0.750 *AL+ 0.750 ALB> 64 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CO+ 0.375 WPBl +0.750 AL* + 0.750 ALB> 65 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPC1 66 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.750 S + 0.750 WPC1 67 System Derived 1.000 0.600 D+0.600 AD+0.600 CU + 1.0 WPC1 68 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPCI + 0.750 *AL+ 0.750 <ALB 69 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG +0.375 WPC1 + 0.750 AL* + 0.750<ALB 70 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 1.0 WPB2 71 System Derived 1.000 1.0 D+ 1.0 AD+ 1.0 CG +0.750 S +0.750 WPB2 72 System Derived 1.000 0.600 D + Q.600 AD+ 0.600 CU + 1.0 WPB2 73 System Derived 1.000 l.O D + l.O AD+ l.O CG+0.375 WPB2+ 0.750 'AL +0.750 ALB> 74 System Derived 1.000 1.0 D + l.O AD+ 1.0 CG +0.375 WPB2 + 0.750 AL* + 0.750 ALB> 75 System Derived 1.000 l.O D + l.O AD+ l.O CG + l.O WPC2 76 System Derived 1.000 l.O D + l.O AD+ l.O CG + 0.750 S + 0.750 WPC2 77 System Derived 1.000 0.600 D + 0.600 AD+ 0.600 CU + l.O WPC2 78 System Derived 1.000 l.O D + l.O AD+ l.O CG + 0.375 WPC2+0.750 *AL+0.750 <ALB 79 System Derived 1.000 LO D t 1.0 AD+ l.O CG + 0.375 WPC2 + 0.750 AL * + 0.750 <ALB 80 System Derived 1.000 l.OD+ l.OAD+ !.'OCG+ l.OS+ l.OALB> 81 System Derived 1.000 l.OD+ t.OAD+ l.OCG+ 1.0 *AL+ l.OALB> 82 System Derived 1.000 1.0 D + 1.0 AD + l.O CG + l.O AL * + 1.0 ALB> 83 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S + 0.750 *AL + 0.750 ALB> 84 System Derived 1.000 1.0 D+ l.O AD+ l.OCG +0.563 S +0.750 AL* +0.750 ALB> 85 System Derived 1.000 l.O D + l.O AD + 1.0 CG + l.O S + 1.0 <ALB 86 System Derived 1.000 l.OD+ l.OAD+ l.OCG+ l.O*AL+ l.O<ALB 87 System Derived 1.000 1.0 D + l.OAD+ 1.0 CG + 1.0 AL* + l.O<ALB 88 System Derived 1.000 l.O D+ l.O AD+ 1.0 CG +0.563 S +0.750 *AL+0.750 <ALB 89 System Derived 1.000 1.0 D + 1.0 AD+ 1.0 CG + 0.563 S +0.750 AL* +0.750<ALB Frame Member Sizes Mem. F1gWidth F1gThk WebThk Depthl Depth2 Length Weight F1gFy No. -(in.) (in.) (in.) (in.) (in.) (ft) (p) (ksi). 1 6.00 0.6250 0.2500 12.00 46.00 31.03 1452.4 55.00 2 6.00 0.6250 0.2500 46.00 23.00 17.79 1033.3 55.00 3 6.00 0.6250 0.2500 23.00 28.53 10.00 472.6 55.00 4 6.00 0.6250 0.2500 28.53 23.00 10.00 472.6 55.00 5 6.00 0.6250 0.2500 23.00 46.00 17.79 1033. . 55.00 6 6.00 0.6250 0.2500 12.00 46.00 31.03 1452.4 55.00 7 7.00 0.2500 0.1875 15.00 15.00 37.00 719.4 55.00 8 7.00 0.3125 0.1875 15.00 15.00 39.25 875.8 55.00 9 7.00 0.2500 0.1875 15.00 15.00 34.75 650.7 55.00 Total Frame Wc1ght-8162.6 (p) Frame Pricing Weight= 8809.4 (p) Frame Member Releases Member Joint 1 Joint 2 7 No Yes 8 No Yes 9 No Yes B d C ct·. S oun arv• on lt!OD ummar Member X~Loc Y~Loc Supp. X Supp. Y Moment Displacement X(in.) 1 0/0/0 0/0/0 Yes Yes No 0/0/0 6 53/0/0 0/0/0 Yes Yes No 0/0/0 7 15/0/0 0/0/0 Yes Yes No 0/0/0 0 15/0/0 37/0/0 Yes No No 0/0/0 8 21/9/0 0/0/0 Yes Yes No 0/0/0 0 2l/9/0 39/3/0 Yes No No 0/0/0 9 44/9/0 0/0/0 Yes Yes No 0/0/0 0 44/9/0 34/9/0 Yes No No 0/0/0 2 51610 33/10/0 Yes Yes Yes 0/0/0 5 47/6/0 33110/0 Yes Yes Yes 0/0/0 File: Chevron -Endpost Changes Date: 11/4/2008 Time: II :28:27 Page: 21 of 26 D+AD+CG+WPD2+*AL+<ALB D+AD+CG+WPD2+AL*+<ALB D+AD.+CG+WPB1 jo+AD+CG+S+WPBl D+AD+CU+WPBI D+AD+CG+WPBl+*AL+ALB> D+AD+CG+WPBl+AL*+ALB> D+AD+CG+WPC1 D+AD+CG+S+WPCl D+AD+CU+WPC1 D+AD+CG+WPCJ+*AL+<ALB lo+AD+CG+WPCI+AL *+<ALB D+AD+CG+WPB2 ~+AD+CG+S+WPB2 D+AD+CU+WPB2 D+AD+CG+WPB2+*AL+ALB> jo+AD+CG+WPB2+AL *+ALB> D+AD+CG+WPC2 ~+AD+CG+S+WPC2 PJ+AD+CU+WPC2 ~AD+CG+WPC2+*AL+<ALB D+AD+CG+WPC2+AL*+<ALB ID +AD+ CG + S+ALB> jo+AD+CG+"'AL+ALB> ~+AD+ CG+AL *+ALB> !o+AD+CG+S+*AL+ALB> jo+AD+CG+S+AL*+ALB> PJ +AD + CG + S+<ALB !o +AD + CG+* AL+<ALB D +AD+ CG+AL *+<ALB io+AD+Cti+S+*AL+<ALB b+AD+CG+S+AL '+<ALB WcbFy Splice (ksi). Jt.1 55.00 BP 55.00 KN 55.00 ss 55.00 SP 55.00 ss 55.00 BP 55.00 BP 55.00 BP 55.00 BP (Includes all plates) (Includes all pieces) Codes Jt.2 KN ss SP ss KN KN ss ss ss shape 3P 3P 3P 3P 3P 3P 3P 3P 3P Displacement Y(in. Displacement ZZ rad.) 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 0/0/0 0.0000 01010 0.0000 Version: ?.la . Chevron -endpost relocate Values shown are resisting forces of the foundation. Reactions-Unfactored Load Type at Frame Cross Section: 1 Date: 11/4/2008 Time: 11:28:27 Page: 22 of 26 Type Exterior Column Interior Column Interior Column Interior Column Exterior Column X~Loc 0/0/0 I 5/0/0 21/9/0 441910 53/0/0 Grid 1 -Grid2 1-E 1-D 1-C 1-B I·A Base Plate W x L (in.) 9x 13 8 X 16 8 X 16 8x 16 9x 13 Base Plate Thickness (in.) 0.500 0.375 0.375 0.375 0.500 Anchor Rod Qty/Diam. (in,) 4. 1.000 4. 0.750 4. 0.750 4 ·.0.750 4. 1.000 Column Base Elev. 100'-0" 100'-0" 100'-0" 100'-0" 100'-0" Load Type Desc. Hx Hz Vy Hx Hz Vy Hx Hz Vy Hx Hz Vv Hx Hz Vy D Fnn 0.9 . 4.8 . 0.8 . . 1.0 . 0.7 -0.9 4.8 AD Fnn 0.1 1.2 . . . . . . . . ·0.1 . 1.2 CG Fnn 2.7 10.6 . . . . . . . . ·2.7 . 10.6 s Fnn 10.2 . 39.8 . . . . . . . . ·10.2 . 39.7 US I* Fnn 9.1 . 23.6 . . . . . . . -9.1 48.0 *US I Fnn 9.1 . 48.0 . . . . . . . . . -9.1 23.6 WI> Fnn -7.2 . -12.4 . 4.2 . . 5.9 . 5.5 . -4.8 -4.4 <WI Fnn 4.8 -4.4 . ·3.7 . . ·5.3 . . ·5.0 . 7.2 . -12.4 W2> Fnn -8.7 . -8.4 . . . . . . . . . -3.3 . -0.5 <W2 Fnn 3.3 . -0.5 . . . . . . . . . 8.7 . ·8.4 *AL> Fnn ·0.0 . 7.7 . . . . . . . . . ·1.4 3.6 AL*> Fnn -0.0 . 2.1 . . . . . . . . . -1.4 9.3 <*AL Frm 1.4 . 9.3 . . . . . . . . 0.0 . 2.1 <AL* Frm 1.4 . 3.6 . . . . . . . . . 0.0 . 7.7 cu Frm 1.4 . 5.3 . . . . . . . . . -1.4 . 5.3 E> Frm -4.0 ·5.4 . 0.1 . . 0.1 . . 0.1 . -4.0 . 5.4 EG+ Fnn 0.4 . 1.4 . . . . . . . . . ·0.4 . 1.4 <E Fnn 4.0 . 5.4 . ·0.1 . . ·.o.l . . ·0.1 . 4.0 . ·5.4 EG-Fnn -0.4 . ·1.4 . . . . . . . . . 0.4 . -1.4 EB> Brc . ·0.0 . . . . . . . . . . . . <EB Brc . 0.0 . . . . . . . . . . . 0.0 WPA1 Brc 1.9 . -9.6 . . . . . . . . -1.9 -9.6 *AL Fnn 0.7 8.5 . . . . . . . . . -0.7 . 2.9 ALB> Brc . . . . . . . . . . . . . . AL* Fnn 0.7 . 2.9 . . . . . . . . . -0.7 . 8.5 WPD1 Brc 2.5 . -7.3 . . . . . . . . -2.5 . -7.3 <ALB Brc . . . . . . . . . . . . . WPA2 Brc 0.4 . -5.6 . . . . . . . . . -0.4 . ·5.6 WPD2 Brc 1.0 . -3.3 . . . . . . . . . -1.0 -3.3 WPB1 Brc 1.9 . -9.6 . . . . . . . . ·1.9 ·9.6 WPC1 Brc 2.5 . ·7.3 . . . . . . . . . ·2.5 . ·7.3 WPB2 Brc 0.4 . •5.6 . . . . . . . ·0.4 . ·5.6 WPC2 Brc 1.0 . ·3.3 . . . . . . . . . -1.0 -3.3 Maximum Combined Reactions Su • b mmary~nt Factored ads-F ramm!:! X-Loc Grid Hrz left Load Hrz Right Load Hrz In Load HrzOut Load Uplift Load Vrt Down Load Momcw Load Momccw Load (-Hx) Case ~~) Case (-Hz) Case (~)) Case (-(~\) Case (~~) Case (-Mzz) Case (Mzz) Case (k) (k) (k (in-k) (in-k) 0/0/0 1-E 7.2 18 15.0 9 0.0 36 o.o 38 5.6 16 64.6 3 . . 15/0/0 1-D . . . 3.7 5 4.2 4 . 0.8 I . . 15/0/0 37/0/0 . . . 3.4 5 3.8 4 0.8 I . . . . 2119/0 1·C . . . . 5.3 5 5.9 4 . . 1.0 I . . . 2119/0 39/3/0 . . . 4.9 5 5.5 4 1.0 1 . . . . . . 44/9/0 1·B . . . . 5.0 5 5.5 4 . . 0.7 1 . . 44/9/0 34/9/0 . . . 4.8 5 5.4 4 0.7 I . . . 53/0/0 1-A 15.0 8 7.2 19 . . 0.0 38 5.6 17 64.6 2 . . . Sum of Forces with Reactions Check w Framine: Horizontal Vertical Load Type Load Reaction Load Reaction (k) (k) (k) (k) D 0.0 0.0 12.0 9.6 AD 0.0 0.0 2.5 2.4 File: Chevron · Endpost Changes Version: 7.la CG 0.0 8 0.0 USI* 0.0 *USI 0.0 WI> 12.0 <WI 12.0 W2> 12.0 <W2 12.0 'AI> 1.5 AL*> 1.5 <*AL 1.5 <AL* 1.5 cu 0.0 E> 7.9 EG+ 0.0 <E 7.9 EG-0.0 EB> 0.0 <EB 0.0 WPAI 0.0 'AL 0.0 ALB> 0.0 AL' 0.0 WPDI 0.0 <ALB 0.0 WPA2 0.0 WPD2 0.0 WPBI 0.0 WPCI 0.0 WPB2 0.0 WPC2 0.0 Base Plate Summary Chevron -endpost relocate 0.0 21.2 21.2 0.0 79.5 79.5 0.0 71.5 71.6 0.0 71.5 71.5 12.0 16.8 16.8 12.0 16.8 16.8 12.0 8.9 8.9 12.0 8.9 8.9 1.5 12.0 11.4 1.5 12.0 11.4 I 1.5 12.0 11.4 1.5 12.0 11.4 0.0 10.6 10.6 8.0 0.0 0.0 0.0 2.8 2.8 8.0 0.0 0.0 0.0 2.8 2.8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 19.1 19.2 0.0 12.0 I 1.4 0.0 0.0 0.0 0.0 12.0 I 1.4 0.0 14.5 14.5 0.0 0.0 0.0 0.0 11.2 I 1.2 0.0 6.6 6.6 0.0 19.1 19.2 0.0 14.5 14.5 0.0 11.2 I 1.2 0.0 6.6 6.6 Date: 11/4/2008 Time: II :28:27 Page: 23 of 26 X~Loc Grid Mem. Thickness Width Length (in~) Num.Of BoltDiam. Type Welds to WeldS to No. (in.) (in.) Bolts (in.) Flan.a:e Web 0/0/0 1-E I 0.500 9 13 4 1.000 A36 08.0.1875 08-0.1875 15/0/0 1-D 7 0.375 8 16 4 0.750 A36 08-0.1875 08.0.1875 2119/0 I-C 8 0.375 8 16 4 0.750 A36 08-0.1875 08-0.I875 44/9/0 1-B 9 0.375 8 16 4 0.750 A36 08·0.1875 08-0.1875 53/0/0 I-A 6 0.500 9 I3 4 1.000 A36 08-0.1875 08.0.1875 Web Sti ener Summan MCm. Stiff. Desc. Loc. Web Depth hit alh a Thick. Wi~~h Side Welding No. No. (ft) lin.)' lin.) lin.) (in. Description 2 I 89 4.02 43.078 I72.31 NIA N!A 0.6250 2.500 Both W-08-0.I875 2 2 8I 12.96 29.229 II6.92 3.00 87.42 O.I875 2.000 Both Std 2 3 S5 3.89 38.909 I55.64 NIA NIA 0.2500 3.000 Both F-BS-O.I875,W-OS-0.1875 2 4 S5 4.79 37.650 150.60 NIA NIA 0.2500 3.000 Both F-BS-O.I875,W-OS-0.1875 5 I S9 I3.77 43.078 I72.3I N/A N/A 0.6250 2.500 Both W-OS-0.1875 5 2 81 I2.29 40.793 I63.17 3.00 I21.69 0.1875 2.000 Both F-08-0.1875, W-08-0. I 875 5 3 85 13.90 38.910 155.64 NIA NIA 0.2500 3.000 Both F-B8-0.1875,W -08-0.1875 5 4 85 13.00 37.651 150.60 NIA NIA 0.2500 3.000 Both F-88-0.1875, W -08-0.1875 Brackets Part Summary Mem. ILoc. (ft) Total Length Bracket Cut Bracket Fig Width Fig Thk (in.) WebThk Hole Pitch Stiffener or Plate Part No. (in.) (in.) Depth (in.) -(in.) . (in.) (in.) 2 3.98 15.375 4.813 10.000 6.000 0.2500 0.2500 3.500 UP07041 1000 WUI5341334 5 13.81 15.375 4.813 10.000 6.000 0.2500 0.2500 3.500 UP07041 1000 WU15341334 Brackets Design Summary (yerticallive load is with the im ad factor) Mem. Loc. (ft) Vert. Live Vert. Dead Lateral Longitudinal CL Distto Member Member Web Thk (in.) ·lgThk(in.) Fig Width No. Load (k) Load (k) lmoact (k) Imoact (k) Flange (in.) Deothl lin.) Deoth2 (in.) -(in.) 2 3.98 !0.61, 1.27 0.73 1.47 13.465 41.986 39.375 0.2500 0.6250 6.0000 5 13.81 10.61 1.27 0.73 1.47 13.465 40.626 40.737 0.2500 0.6250 6.0000 File: Chevron -Endpost Changes Version: 7.Ia Chevron -endpost relocate Date: 11/4/2008 Time: 11:28:27 Page: 24 of 26 Bolted EndMPiate Moment Connections (AISC DGM16) M Fy =55 ksi End·Plate Dimensions Bolt Outside Flam~e Inside Flange Mem. Jt. Type Thick. Width Length Diam. Spec/Joint Gages In/Out Configuration Pitches 1st/2nd Confi,guration Pitches I stl2nd No. No. (in.) (in.) (in.) (in.) (in.) ID Desc. (in.) ID Desc. (in.) I 2 KN(Top) 0.625 6.00 47.00 0.750 A325XIST 3.50 12 Flush 2.00 II Flush 2.00 2 I KN(Top) 0.625 6.00 47.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 3 2 SP 0.500 6.00 33.54 0.750 A325X/ST 3.50 II Flush 0.00 31 Extended 3.75 4 I SP 0.500 6.00 33.54 0.750 A325X/ST 3.50 II Flush o.oo 31 Extended 3.75 5 2 KN(Top) 0.625 6.00 47.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 6 2 KN(Tooi 0.625 6.00 47.00 0.750 A325X/ST 3.50 12 Flush 2.00 II Flush 2.00 Rcequired Stremrth • OUt Available Strength ·Out Required Strength • In Available Strensrth • In Mem. Jt. Ld Axial Shear Moment Design Shear Moment Ld A~~ I Shear Moment Design Shear Moment No. No. Cs (k) (k) fin-k) Proc. (k) (in-k) Cs (k) fin-k) Proc. (k) fin-k) I 2 2 -40.7 10.9 3703.1 Thin plate 159.0 2907.1 16 5.7 I. 1159.0 Thick plate 106. 1727.1 2 I 2 -40.7 10.9 3703.1 Thin plate 159.0 2907.1 16 5.7 I. 1159.0 Thick plate 106. 1727.1 3 2 17 3.3 3.7 15.7 Thin plate 106.0 890.2 I -13.6 3. 1793.1 Thin plate 159. 1733.8 4 I 17 3.3 3.7 15.7 Thin plate 106.0 890.2 I -13.6 3.4 1793.1 Thin plate 159.0 1733.8 5 2 3 -40.7 10.9 3703.1 Thin plate 159.0 2907.1 17 5.7 I. 1159.0 Thick plate 106.0 1727.1 6 2 3 -40.7 10.9 3703.1 Thin olate 159.0 2907.1 17 5.7 I. 1159.0 Thickolate 106.0 1727.1 Flane.e Brace Summarv Member From Member Joint 1 From Side Point 1 Part Design Note I 17/5/4 17/514 FB4000 I 271514 271514 FB5050 2 51318 2219/13 FB5080 2 1413/8 1319113 FB4014 2 171318 1019113 FB3020 3 5/610 419113 FB3040 3 8/610 119113 FB4014 4 11610 119113 FB4014 5 61610 16/9/13 FB4050 5 91610 1919113 FB4084 5 1216/0 22/9113 FB5080 6 171514 1715/4 FB4000 6 271514 271514 FB5050 7 71514 715/4 (2)FB2044 7 17/514 1715/4 (2)FB2044 7 321514 32/514 (2)FB2044 8 71514 715/4 FB2044 8 171514 171514 (2)FB2044 8 32/514 32/514 (2)FB2044 9 7/514 71514 FB2044 9 17/514 1715/4 (2)FB2044 9 0/010 321514 FB2080 T fP S OPO ost ummar_y X·Loc Grid Top Conn. Condition FlgMn RbAllow Comp FB Force FB Angle Min FBISFB Pur lin Bolt Shear FBIWSF Reaction Force Moment Shear Rl R2 Pur lin Bearing Bearing 151010 1-D 3.81 3.08 Std 281.25 19.04 N 2.48 45.50 0.065 FB 2.73 4.71 3.43 N 2.11 50.76 0.065 FB 2.73 4.71 3.43 211910 1-C 5.45 4.63 Stub-l 131.81 4.63 -8.75 4.12 - -- 44/910 1-B 5.40 4.66 Stub-2 197.48 6.17 -10.83 6.17 - --- - Frame Design Member Summa ~Controlling Load Case and Maximum Combined Stresses per Member (Locations are from Joint 1 Actual Forces Actual Stresses Allowable Stress Condition Mem. Loc. Depth Load Axial Shear Mom·x Mom-y Axial Shear Bnd-X Bnd-Y ---Stress /Force ---Sum% % No. ft in. Case k k in-k in-k ksi ksi ksi ksi Axial Shear Bnd-X Bnd-Y Bnd+Ax Shear I 17.46 32.97 I -57.0 -II.! -2326.8 0.0 3.69 1.40 15.53 0.00 24.70 5.16 18.16 41.25 0.98 0.27 2 15.90 23.76 3 -17.7 9.1 1907.7 0.0 1.35 1.62 19.52 0.00 29.60 10.25 33.00 41.25 0.63 0.16 3 2.50 24.50 3 -14.5 3.1 2147.1 0.0 1.09 0.53 21.12 0.00 29.73 9.61 33.00 41.25 0.67 0.06 4 7.10 24.50 2 -14.5 -3.1 2147.1 0.0 1.09 0.53 21.12 0.00 29.73 9.61 33.00 41.25 0.67 0.06 5 0.00 23.00 2 -17.2 -7.9 1959.1 0.0 1.33 1.46 19.53 0.00 29.47 10.99 33.00 41.25 0.63 0.13 6 17.46 32.97 I -57.0 II.! -2326.8 0.0 3.69 1.40 15.53 0.00 24.70 5.16 18.16 41.25 0.98 0.27 File: Chevron -Endpost Changes Version: 7.la . Mem. Loc. Depth Area Rx No. ft in. in.2 in. I 17.46 32.97 15.43 13.05 2 15.90 23.76 13.13 9.73 3 2.50 24.50 13.31 10.00 4 7.10 24.50 13.31 10.00 5 0.00 23.00 12.94 9.44 6 17.46 32.97 15.43 13.05 7 17.44 15.00 6.22 6.19 8 17.44 15.00 7.07 6.32 9 17.44 15.00 6.22 6.19 Deflection Load Combinations~ Framinl! No. Origin Factor DefH I System 1.000 0 2 System 1.000 0 3 System 1.000 0 4 System 1.000 0 5 System 1.000 0 6 System 1.000 0 7 System 1.000 0 8 System Derived 1.000 0 9 System Derived 1.000 0 10 System Derived 1.000 0 11 System Derived 1.000 0 12 System Derived 1.000 0 13 System Derived 1.000 0 14 System Derived 1.000 0 15 System Derived 1.000 0 16 System 1.000 400 17 System 1.000 400 18 System 1.000 400 19 System 1.000 400 20 System Derived 1.000 400 21 System Derived 1.000 400 22 System Derived 1.000 400 23 System Derived 1.000 400 24 System Derived 1.000 400 25 System Derived 1.000 400 26 System Derived 1.000 400 27 System Derived 1.000 400 28 System 1.000 100 29 System 1.000 100 30 System Derived 1.000 100 31 System Derived 1.000 100 32 System 1.000 400 33 System 1.000 400 * Negative horizontal deflection is left * Negative vertical deflection is down Ry in. 1.21 1.3 I 1.30 1.30 1.32 1.21 1.52 1.59 1.52 DefY 240 240 240 240 240 240 240 240 240 240 240 240 240 240 240 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Chevron -endpost relocate Lx Ly-1 Ly-2 Klx Klyl Kly2 Sx in. in. in. IRx fRy fRy in3 339.69 60.1 60.1 39.1 49.7 49.7 149.80 295.94 36.1 36.0 30.4 27.5 27.5 97.74 295.94 36.0 36.0 29.6 27.7 27.7 101.65 295.94 36.0 36.0 29.6 27.7 27.7 101.65 295.94 36.0 0.0 31.3 27.3 o.o 100.29 339.69 60.1 60.1 39.1 49.7 49.7 149.80 444.00 120.0 96.0 71.8 79.1 63.3 30.10 471.00 120.0 96.0 74.5 75.5 60.4 35.63 417.00 120.0 96.0 67.4 79.1 63.3 30.10 Aoolication 1.0 s 1.0 US!* l.O*USI ~.700Wl> 0.700<Wl 0.700 W2> 0.700<W2 0.700WPA1 0.700WPD1 ~.700WPA2 ~.700WPD2 0.700WPB1 r.700 WPCl 0.700WPB2 0.700WPC2 p.700Wl> ~.700<Wl ~.700W2> p.700<W2 0.700WPA1 0.700WPD1 0.700WPA2 0.700 WPD2 0.700WPB1 0.700WPCI 0.700WPB2 0.700WPC2 Q.600 E> + 0.700 EG- p.600 <E + 0.700 EG- r.600 EB> . r.600<EB l.O<AL* I.O *AL> Lbl Rt~l in. in. 209.5 1.64 36.1 1.61 36.0 1.60 36.0 1.60 36.0 1.61 209.5 1.64 120.0 1.87 120.0 1.93 120.0 1.87 Date: 11/4/2008 Time: II :28:27 Lb2 Rt-2 Qs Qa Cbl Cb2 in. in. 120.2 1.57 1.00 0.92 1.75 1.20 36.0 1.61 1.00 1.00 1.13 1.05 36.0 1.60 1.00 1.00 1.05 1.01 36.0 1.60 1.00 1.00 1.01 1.05 0.0 0.00 1.00 1.00 1.05 0.00 120.2 1.57 1.00 0.92 1.75 1.20 180.0 1.91 0.86 1.00 1.00 1.00 180.0 1.98 0.95 1.00 1.00 1.00 180.0 1.91 0.86 1.00 1.00 1.00 Descriotion s USI* *US1 Wl> Wl W2> <W2 WPAl WPDl WPA2 WPD2 WPBl WPCl >VJ>B2 WPC2 Wl> <Wl w~ WPAl WPDl WPA2 WPD2 WPBl >VJ>CI WPB2 WPC2 E>+ EG~ E+EG~ EB> <EB <AL* 'AL> Lateral deflections of primary frames are calculated on a bare frame basis and do· not include resistance from systems such as roof and end wall diaphragms. Therefore, these deflections may be considerably overstated. at Bottom of Beam Left Bracket Length Left File: Chevron -Endpost Changes Right Bracket Length H~istRoom Clear Lift Version: 7.la 010/0 2/Sil4 Horizontal Frame Clearances Wall· 4 Frame Required at Bottom of Beam Left I 1/3/0 1/8/8 File: Chevron -Endpost Changes Chevron -endpost relocate 1/1/7 2/5/14 111/7 at Bottom of Beam Right 1/8/8 I 4/8/0 Version: 7.la Date: 11/4/2008 Time: I I :28:27 Page: 26 of 26 21110/0 Parcel Detail Garfield County Assessor /Treasurer Parcel Detail Information Page I of 5 Assess~r)T rea surer PropJJrJy_ Search I ~Ji~essor Subset Uu!:l.CY I Assessor Sale~_Mi)rch Clerk H R~~;;!!rder Reception S!:l.!lrch Basic Building~_haracteristics I Tax lnformatiqn Par~JJ)gtail I Valu~Detajl I Sales Dgtail I ResidenttCJVCommerciallmgmy~_ment Detail illJI.ll.etail I Photogr~hs I Mill Leyy_Revenues Detail I Tax Area II Account Number II Parcel Number 112007 Mill levy I I D28 II R28D444 II 2138183DDOI4 II 28.87 I Owner Name and Mailing Address !CHEVRON USA INC IC/0 CHEVRON TEXACO PROPERTY TAX IP 0 BOX 285 !HOUSTON. TX 77001 Assessor's Parcel Description (Not to be used as a legal description) ISECT.TWN.RNG:IB-5-88 DESC: SEC.7: iTHAT PT OF LOTS 12.14 AND NESENE !LYING OESC: BELOW THE ESCARPMENT I(NET 14.20AC) ALSO THAT PT OF DESC: ITRS. 50.51 AND 58 LYING BELOW THE !ESCARPMENT (NET DESC: 175.17). ISEC.8: THAT PT OF LOTS 2.4.7.8. http:/ I www.garcoact.coml assessor I parcel.asp?ParceiNumber= 21381 B30 0014 I I I I I I I I I I I 121512008 Parcal Oatail Page 3 of 5 Location Physical Address: IITWN 5 RGE 98 SEC 16 I Subdivision: I land Acres: 112840.21 I land Sq Ft: I 0 Section II Township I Range 16 II 5 II 98 I 21lllB Property Tax Valuation Information ;·J·; II Actual Value II Assessed Value I I land: II 60.30011 17.4901 I Improvements: II oil ol I Total: II 60.30011 17.4901 . Additional ValuB O~truJ Most Recent Sale II Additional SaiBs O~til.il Basic Building Characteristics Number of Residential In I Buildings: Number of Comm/lnd In I Buildings: No Building Records Found http:// www.garcoact.com/ assassor I parcal.asp?ParceiNumber= 21381630 DO 14 12/512008