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HomeMy WebLinkAbout34411-Z10/6/2011 Town of Southold Annex 54375 Main Road Southoid, New York 11971 CERTIFICATE OF OCCUPANCY No: 35258 Date: 10/6/20 ! 1 THIS CERTIFIES that the building Location of Property: SCTM #: 473889 Subdivision: RESIDENTIAL ADDITION 1465 PINE TREE RD CUTCHOGUE, Sec/Block/Lot: 98.-1-26 Filed Map No. Lot No. conforms substantially to the Application for Building Permit heretofore fried in this officed dated 2/2/2009 pursuant to which Building Permit No. 34411 dated 2/2/2009 was issued, and conforms to all of the requirements of the applicable provisions of the law. The occupancy for which this certificate is issued is: sunroom addition to an existing one family dwelling as applied for. The certificate is issued to Horton Jr, Richard & Horton, Debra (OWNER) of the aforesaid building. SUFFOLK COUNTY DEPARTMENT OF HEALTH APPROVAL ELECTRICAL CERTIFICATE NO. PLUMBERS CERTIFICATION DATED FORM NO. 3 TOWN OF SOUTHOLD BUILDING DEPARTMENT Town Hall Southold, N.Y. BUII~ING PERMIT (THIS PERMIT MUST BE KEPT ON THE PREMISES UNTIL FULL COMPLETION OF THE WORK AUTHORIZED) PERMIT NO. 34411 Z Date FEBRUARY 2, 2009 Permission is hereby granted to: RICHARD L & DEBRA S HORTON, JR 1465 PINE TREE RD CUTCHOGUE,NY 11935 for : SUNROOM ADDITION TO EXISTING SFD AS APPLIED FOR at premises located at County Tax Map No. 473889 Section 098 pursuant to application dated FEBRUARY Building Inspector to exl~ire on AUGUST 1465 PINE TREE RD CUTCHOGUE Block 0001 Lot No. 026 2, 2009 and approved by the 2, 2010. Fee $ 200.00 Authorized Signature ORIGINAL Rev. 5/8/02 Form No. 6 TOWN OF SOUTHOLD BULLDI~G DEPARTMENT TOWN HALL 765-1802 APPLICATION FOR CERTIFICATE OF occUPANcy ~ ~pplieation must be filled in by typewrites or ink and submitted to the Building Department with the following: A. For new building or ne~v use: 1. Final ~wvey 9f property with accarate location 0fall buildingsi prope~'ty lines, streets, and unusual natural or · topographic features. 2. Finnl Approval from Health Dept. of water supply and sewernge-disposal (8_9 form). 3.. ApPwval of eloetrieal installation fxom Board 6f Fire Underwriters. 4. 8worn statement from plumber certifying that the solder used in system contains le~s than 2/10 of l%'lead.. 5. C0mmoreial building, industrial building, mtfltiple residences and similar buildings and installations, a certificate of Code Compliance from architect or engineer responsible for the bulling. 6, Submit Planning Board Approval of completed site plan requirements. B. For existing buildings (prior to April 9, 1957) non-conforming uses, or buildings and "pre-existing" land uses:· 1. Accurate survey of property shgwing all property line~, streets, building and:unusufil naturai or topographic features. 2. A properly completed application and consent to inspect signed by the applicant. If a Certificate of Occupancy i~ denied, the Building inapector shaH state the reasons therefor in writing to the applicant. Fees t. Certificate of Occupancy - New dwelling $50.00, Additions to dwelling $50.00, Alterations to dwelling $50.00, · Swimming po91 $50~00, Accessory building $50.00, Additions to accessory building $50.00, Businesses $50.00~. 2_ Ceytifieate of Occupancy on Pre-existing Building- $100.00 3. Copy of Certificate of Occupancy - $.25 4. Updated C~rtifmate of Occupancy - $50.00 5. Temporary Certificate of Occupancy - Residential $15.00, Commercial $15.00 New Construction: ~ Old or Pre-existing Building: LoeationofOroperty: · I c'~b'~ ~tDe T~(' l?¢( Ho~e No. Stree~ Owner or Owners of Property: ~i'C ~ r d 'Suffolk County Tax Map lqo 1000, Section C~3 S~lxlivisi~n I"Ie~lth Dept. Approval: Planning Board Approval: Request for: Temporary Certificate Foe Submitted: $ · Date of Permit. Date. (cheek one) Final Certificate: / (check one) ADolicant Sivnatm'e Underwriter~ Approval: mo [ / Lot Filed Map. Lot:. TOWN OF SOUTHOLD BUILDING DEPT. 765-1802 INSPECTION ~FOUNDATION 1ST [ ] FOUNDATION 2ND [ ] FRAMING / STRAPPING [ ] FIREPLACE & CHIMNEY [ ] FIRE RESISTANT CONSTRUCTION REMARKS: [ ] ROUGH PLBG. [ ] INSULATION [ ] FINAL [ ] FIRE SAFETY INSPECTION [ ] FIRE RESISTANT PENETRATION INSPECTOR DATE TOWN OF SOUTHOLD BUILDING DEPT. 765-1802 INSPECTION [ ]FOUNDATION 1ST [ ]ROUGH PLBG. [ ]FOUNDATION 2ND [ ]INSULATION ~~ STRAPPING [~J~FINAL [ ] FIREPLACE & CHIMNEY [ ] FIRE SAFETY INSPECTION [ ] FIRE RESISTANT CONSTRUCTION [ ] FIRE RESISTANT PENETRATION REMARKS: DATE INSPECTOR ~-~ ~~--- FIELD INSPECTION REPORT I DATE COMMENTS FOUNDATION (2ND) ROUGH F~G & PLUMBING INSULATION PER N. Y. STATE ENERGY CODE ~DITION~ CO~ENTS TOWN OF SOUTHOLD BUILDING DEPARTM'ENT TOWN HALL SOUTHOLD, NY 11971 TEL: (631) 765-1802 FAX: (631) 765-9502 www. northfork.net/Southold/ Examined 2~/Z ., 20tY ¢ Approved ?~ / E ,200 c~ Disapproved aJc Expiration ( PERMIT NO. BLDG. DEPT. TOWN OF SOUTHOLO Building Inspector BUILDING PERMIT APPLICATION CHECKLIST Do you have or need the following, before applying'? Board of Health 4 sets of Building Plans Planning Board approval Survey_ Check Septic Form N.Y.S.D.E.C. Trustees Contact: .50 5 qe~s. 14~x4 .h%l~ok N,/I nqt PLICATION FOR BUILDING PERMIT Date INSTRUCTIONS a. This application MUST be completely filled in by typewriter or in ink and submitted to the Building Inspector with 4 sets of plans, accurate plot plan to scale. Fee according to schedule. b. Plot plan showing location of lot and of buildings on premises, relationship to adjoining premises or public streets or areas, and waterways. c. The work covered by this application may not be commenced before issuance of Building Permit. d. Upon approval of this application, the Building Inspector will issue a Building Permit to the applicant. Such a permit shall be kept on the premises available for inspection throughout the work. e. No building shall be occupied or used in whole or in part for any purpose what so ever until the Building Inspector issues a Certificate of Occupancy. f. Every building permit shall expire if the work authorized has not commenced within 12 months after the date of issuance or has not been completed within 18 months from such date. If no zoning amendments or other regulations affecting the property have been enacted in the interim, the Building Inspector may authorize, in writing, the extension of the permit for an addition six months. Thereafter, a new permit shall be required. A~Pb,~.xON IS HEREBY MADE to tn~ Bailumg w*p,um,~att foJ .......... ~ ~":'~: o : .............. ~- Building Zone Ordinance of the Town of Southold, Suffolk County, New York, and other applicable Laws, Ordinances or Regulations, for the construction of buildings, additions, or alterations or for removal or demolition as herein described. The applicant agrees to comply with all applicable laws, ordinances, building code, housing code, and regulations, and to admit authorized inspectors on premises and in building for necessary inspections. State whether applicant is owner, lessee, agent, architect, engineer, general contractor, electrician, plumber or builder (fin nn ,t.~, If applicant is a corporation, signature of duly authorized officer (Name and title of corporate officer) Builders License No. q I'~ q I - H Plumbers License No. Electricians License No. Other Trade's License No. Location of land on which proposed work will be done: House Number Street Hamlet County Tax Map No. 1000 Section 6~> Block / Subdivision Filed Map No. (Name) Lot cQ/.a Lot State existing use and occupancy ofprem~ses and ln~ded use and occupancy of proposed,.9onstm¢ ton: a. Existing use and occupancy 5~T'~P- al'T~\? ~UOt~[\~CIt~ '. b. Intended use and occupancy .g(l~.._~_) 3. Nature of work (check which applicable): New Building_ Repair Removal Demolition 4. Estimated Cost .~IDoOI:' 5. If dwelling, number of dwelling units If garage, number of cars Fee Addition Other Work Alteration (Description) (To be paid on filing this application) Number of dwelling units on each floor 6. If business, commercial or mixed occupancy, specify nature and extent of each type of use. Ix3/~ 7. Dimensions of existing structures, if any: Front I..0,~' Rear [.oS ~ Depth Height Number of Stories oq, ' ' Dimensions of same structure with alterations or additions: Front t,.1:3%1,; Rear Depth L-4~x Height Number of ~Ibties~..~t.. 8. Dzmenszons of entzre new constructzon: Front i~. ~ Rear I ¢ tl~ I Depth I Height q ~ I I" Number of Stories [ [ ~'----5; : ia 9. Size of lot: Front I ~ Re~ J ~ O Depth 11. Zone or use district in which premises are situated 12. Does proposed construction violate any zoning law, ordinance or regulation? YES__ xo w' 5. Z2 L. L~ - _ = 1 1P,YES NO ~ Will excess fill be removed from.~remises? YES NO Nme of Architect 0)ffXt~ ~Wm. A~dress I1~ WilSOn ~r. ~J~hone X~~ x*~meofCon~actor~r ~nS ~l~ Address~°b% ~e~-~. IF YES~ SOUTHOLD TO~ TRUSTEES ~ D.E.C. PE~ITS MAY BE REQUIRED. ~b. Is th~s propu~y ~iu 300 [~ut o~a t~da] ~et~d? ~ Y~S__ NO ~ IF Y~S~ D.E.C. PE~ITS MAY B~ REQUIRED. I6. Provide survey, to scale, with accurate foundation plan and distances to property lines. 17. If elevation at any point on property is at 10 feet or below, must provide topographical data on survey. STATE OF NEW YORK) SS: COUNTY OF SU'~dBI Jq ) being duly sworn, deposes and says that (s)he is the applicant (S)He is the (DO) tx~.. ,C of said owner or owners, and is duly authorized to perform or have performed the said work and to make and file this application; that all statements contained in this application are tree to the best of his knowledge and belief; and that the work will be performed in the manner set forth in the application filed therewith. DE~RORE O. FEOUN Nolwy pul~ic, ~ta~e of N~ Y~ ~. 4~281 ~ifl~ in Suffolk County Commission Fx~ir~s ,,l~r~ '3 ~0 , Four Seasons Solar Products LLC ENGINEERING CALCULATIONS STANDARD SYSTEM 4E MODEL ECLT-13GG WITH 4GBA ROOF RAFTERS WITH RAFTER STIFFENERS AT 30" ON CENTER BAYS FOR THE HORTON RESIDENC[~ LOCATED AT 1465 PINE TREE DRIVE CUTCHOQUE, NY 11935 DATE: January 27, 2009 THE ABOVE INDICATED PROJECT HAS BEEN EXAMINED FOR A.s. Enginee~ng Serv~e~p.C. 112 W~ ~ 30 psf ROOF LOAD (63~.)8o7-2s9~ 120 mph EXPOSURE C WIND LOAD AS PER THE 2007 NEW YORK STATE BUILDING CODE AND EITHER MEETS OR EXCEEDS THESE LOADINGS NOTES: 1. THIS SUMMARY PERTAINS TO THE STRUCTURAL INTEGRITY OF OUR UNIT UP TO, BUT NOT INCLUDING, THE CONNECTIONS TO THE EXISTING STRUCTURE AND/OR ANY NEW CONSTRUCTION. ALL SUBSTRUCTURE DESIGN REQUIREMENTS AND CONNECTIONS TO THE EXISTING STRUCTURE ARE NOT INCLUDED IN THE SCOPE OF WORK FOR THE FOUR SEASONS PRODUCT, AND MUST BE DESIGNED BY A DESIGN PROFESSIONAL. 2. THE ENGINEERING DESIGN SCOPE FOR THE FOUR SEASONS PRODUCT DOES NOT ACCOUNT FOR SPECIAL LOAD CONDITIONS CREATED BY ATTACHMENT TO THE EXISTING STRUCTURE. THESE MAY INCLUDE SNOW DRIFTING OR UNBALANCE SNOW LOADING. ANY SPECIAL LOADING CONDITIONS MUST BE EVALUATED BY A DESIGN PROFESSIONAL. 5005 Veterans Memorial Highway · Holbrook, NY 11741 · Telephone (631) 563-4000 · Facsimile (631) 563-4010 · wv~v, FourSeasonsSunrooms.com New York State Insurance Fund Workers"Compensation & DisabilitY B~nefits Specialists Sittce 1914 199 CHURCH STREET, NEW YORK, N.Y. 10007-1100 Phone: (888) 997-3863 CERTIFICATE OF WORKERS' COMPENSATION INSURANCE LOVELL SAFETY MGMT CO.. LLC 110 WILLIAM STREET 12TH FLR NEW YORK NY 10038 POLICYHOLDER FOUR SEASON I,LLC D/B/A FOUR SEASON HOLBROOK 5005 VETERANS MEMORIAL HIGHWAY HOLSROOK NY 11741 ' CERTIFICATE HOLDER TOWN OF SOUTHOLD 53095 MAIN ROAD SOUTHOLD NY 11971 POLICY NUMBER CERTIFICATE NUMBER i PERIOD COVERED BY THIS CERTIFICATE i DATE I G lO56 031-4 490584 ~ 07/01/2005 TO 07/01/2009 i 4/15/2008 THIS IS TO CERTIFY THAT THE POLICYHOLDER NAMED ABOVE IS INSURED WITH THE NEW YORK STATE INSURANCE FUND UNDER POLICY NO. 1256 031-4 UNTIL 07/01/2009, COVERING THE ENTIRE OBLIGATION OF THIS POLICYHOLDER FOR WORKERS' COMPENSATION UNDER THE NEW YORK WORKERS' COMPENSATION LAW WITH RESPECT TO ALL OPERATIONS IN THE STATE OF NEW YORK. EXCEPT AS INDICATED BELOW, AND, WITH RESPECT TO OPERATIONS OUTSIDE OF NEW YORK, TO THE POLICYHOLDER'S REGULAR NEW YORK STATE EMPLOYEES ONLY. IF SAID POLICY IS CANCELLED, OR CHANGED PRIOR TO 07/01/2009 IN SUCH MANNER AS TO AFFECT THIS CERTIFICATE, 10 DAYS WRITTEN NOTICE OF SUCH'CANCELLATION WILL BE GIVEN TO THE CERTIFICATE HOLDER ABOVE. NOTICE BY REGULAR MAIL SO ADDRESSED SHALL BE SUFFICIENT COMPLIANCE WITH THIS PROVISION. THE NEW YORK STATE INSURANCE FUND DOES NOT ASSUME ANY LIABILITY IN THE EVENT OF FAILURE TO GIVE SUCH NOTICE. THIS CERTIFICATE DOES NOT APPLY TO BUILDING DEMOLITION. THIS CERTIFICATE IS ISSUED AS A MATTER OF INFORMATION ONLYAND CONFERS NO RIGHTS NOR INSURANCE COVERAGE UPON THE CERTIFICATE HOLDER. THIS CERTIFICATE DOES NOT AMEND, EXTEND OR ALTER THE COVERAGE AFFORDED BY THE POLICY. NEW YORK STATE INSURANCE FUNC DIRECTOR.INSURANCE FUND UNDERWRITING This certificate can be validated on our web site at https://www.nysif.com/cert/certval.asp or by calling (888) 875-5790 VALIDATION NUMBER: 1007736026 U-26.3 118/CD 19480-20/987 STATE OF NEW YORK WORKERS' COMPENSATION BOARD CERTIFICATE OF INSURANCE COVERAGE UNDER THE NYS DISABILITY BENEFITS LAW PART 1. To be completed by Disability Benefits Carrier or Licensed Insurance Agent of that Carrier 1 a. Legal Name and Address of Insured (Use street address only) Four Seasons Sunrooms of NY, LLC 5005 Veterans Memorial Highway Holbrook, NY 11741 1 b. Business Telephone Number of Insured I c. NYS Unemployment Insurance Employer Registration Number of Insured DBA: 2. Name and Address of the Entity Requesting Proof of Coverage Id. Federal Employer Identification Number of Insured or Social Security Number 205809702 3a. Name of Insurance Carrier (Entity Being Listed as the Certificate Holder) Town of Southold 53095 Main Road Southold, NY 11971 Zurich American Insurance Company 3b. Policy Number of entity listed in box "la": 5291935.004 3c. Policy effective period: 03/01/08 to 03/01/09 4. Policy covers: a.[~ All of the employer's employees eligible under the New York Disability Benefits Law b.['-] Only the following class or classes of the employer's employees: Under penalty of perjury, 1 certify that I am an authorized representative or licensed agent of the insurance carrier referenced above and that the named insured has NYS Disability Benefits insurance coverage as described above. Date Signed 1/30/2009 By ~ ~ (Signature of insurance carrier's authorized representative or NYS Licensed Insurance Agent of that insurance carrier) Telephone Number (631)845-2200 Title Administrative Services Manaeer IMPORTANT: If box "4a" is checked, and this form is signed by the insurance carrier's authorized representative or NYS Licensed Insurance Agent of that carrier, this certificate is COMPLETE. Mail it directly to the certificate holder. If box "4b" is checked, this certificate is NOT COMPLETE for purposes of Section 220, Subd. 8 of the Disabilit3, Benefits Law. It must be mailed for completion to the Workers' Compensation Board, DB Plans Acceptance Unit, 20 Park Street. Albany, New York 12207. PART 2. To be completed by NYS Workers' Compensation Board (Only if box "4b" of Part I has been checked) State Of New York Workers' Compensation Board According to information maintained by the NYS Workers' Compensation Board, the above-named employer has complied with the NYS Disability Benefits Law with respect to all of his/her employees. Date Signed By (Signature of NYS Workers' Compensation Board Employee) Telephone Number Title Please Note: Only insurance carriers licensed to write NYS disability benefits insurance policies and NYS licensed insurance agents of those insurance carriers are authorized to issue Form DB-120.1. Insurance brokers are NOT authorized to issue this form. DB-120.1 (5-06) Feb 02 2009 ~:32P~ HP LASE~3ET FAX p-! Town of $out old .Erosion, Sedimentation & Sto~ AS~E&SMENT FORM _t__ ~L~Z_ ........... ~,~ EXEMFrllC~: Yes No Ooea Udet ~ro~ec~ m~M ~e minimum ~ndm~js fo~ c~ndlh~ as ~m AGflculb~al pm~c~? Mote: If yo~ Aniw~red yelio thlB Ckledlon, i Stixm.WMmr, Grmdlag, Drainage & Ero~on Conlz(N p~ ~ ~ ~e~dI FORM - 0~7 Commission Expires Mar~ !UILDING PEP, MI'[' E)'L4MINEI~ CItECFd, IST CTM# 1000 'roperty Address: ~uilding permits (Open/E×pired): SpO~O-Z/C/O Z-~le~ : P~ -Z/C/O Z- __, hlfo: BP -Z/C/O z- Ingle & Separate Search Required? or.~Determmatmn. .BQ. Lot Size: ACT. Lot Size: .BQ. Front ACT. Front REQ Side ACT. Side .F,Q. Height __ ACT Height rojed D es ¢ r jla ti o tl~,f,,ff..~ utoalvtsmn: ...... Zone: ~ Conforming? ~ Ci y: 4T/O Pre COs? -- , BP .... -Z / C/O Z- ,lafo: REQ. Lot Coy. ~ ACT. Lot 1KEQ. Rear~ PROP. Rear Yate~floaa~? Y' oa' N9 [3, es, watea body . Pa,el# .. _ Flood Zone: I~ulkh('ad"Bh~fl Dis(ance: ,D D lTl () N A L A P P 11 O V A I~S lEE Q U [ IH; D uffolkC(~uuh Ileal(h: '~ ,,~ [I yes, ~tted/4 / :outhohl PlaLnaiug: 3 oi,J.4- Date: / / / ?own l..audmarlc CoI A: 5' oiN £)TE / Permil #:. __ Noles: {ores: CODE Coml)liance (page 2): Y m N ~_ee ~tlllk ItJl t'L { alculali<m: ;'it'st FI,,,)~ ,/ ~econd l?[o,~ ;: F Dthel: _:: I total: ¢ Initial Fee $ Additional Fee ( ): $ TOTAL: NEW YORK STATE CODE COMPLIANCE C[IECI iL[ST CLIMATIC/GEOGRAPHIC DESIGN CRITERIA: Grountl Snow Load: 45 Weathering: Severe Frost Depth: 36" Design Temp: 1l _ Ice Shield Underlay: YE8 USE/OCCUPANCY CLASSIFICATION: ' HEIGHT/FII~ AKEA: TYPE OF CONSTRUC FION: D ES IGN CIMTEIU~ ENOINEEPdED/PKES CK[PTIVE F .JLL FP6Kh'f[N© DESIGN ELEMENTS: HEADERS: yflN WALL STU'DS: CEILING JOISTS: ¥/f'q' FLOORJ }[,qTS LUk[BER SPE('IES ).NI) GIL-\DIg: DESIGN l-_O?X.D ( AL _I. JLAI IONo LIV'I,~: Y/'N [}lr)&l '(/N SNO'~V: Y/IN L;l£1ShIIC: TIN ~,, l]ql_)O ~ /,,I'4T~ k)q()R SCHEDULE -'- ?' S.? E(~RLS,5 S.F.: y/IN 5QT~NT 4%: NA[LING/CONST/KUCT[ON SCHEDULE ¥/N IOCA~Ic.[q OF FII:/-' I'I?.t)TP("TI~)I! ,.~ttll,l,ll.5'd~ TOTAL (O¢IPl IlC¢('['~ h,'/¢ (l'{lC'lLIltN 1TI l'A(i[t Wind Speed: I:Z01V[PIt Seismic Desigu Category: B Termite: M-H Decsy: S-M Flood Ha[ard~: I,'. ,) 0 [? l~,k I?TEP, $: V,,'N Town Hall Annex 54375 Main Road P.O. Box 1179 Southold, New York 11971 0959 Telephone (631 ) 765-1802 Fax (631) 76549502 BUILDING DEPARTMENT TOWN OF SOUTHOLD February 25,2009 Mr.&Mrs. R. Horton 1465 Pine Tree Rd. Cutchogue N.Y. 11935 We are unable to complete your Certificate of Occupancy because of the following reasons: ~'~An application for Certificate of Occupancy is not on file. (Enclosed) No Electrical Certificate on file ~'"'~The Check is not on file - $ 25.00 No Final Health Department Approval on file. No final inspection has been made. No Plumber Solder Certificate on file. (All permits involving plumbing being issued after April 1, 1984) Certificate of Compliance from Southold Town Trustees. Approval of the Zoning Board of Appeals* Final Planning Board Approval B.P. # 34411 Sunroom Addition Town Hall Annex 54375 Main Road P.O. Box 1179 Southold, NY 11971-0959 Telephone (631 ) 765-1802 Fax (631) 765-9502 BUILDING DEPARTMENT TOWN OF SOUTHOLD August 26, 2011 Richard Horton 1465 Pine Tree Rd Cutchogue, NY 11935 TO WHOM IT MAY CONCERN: The Following Item(s) Are Needed To Complete Your Certificate of Occupancy: v~Application for Certificate of Occupancy. (Enclosed) Electrical Underwriters Certificate. ~Afee of $25.00. Final Health Department Approval. Plumbers Solder Certificate. (All permits involving plumbing after 4/1/84) __ Trustees Certificate of Compliance. (Town Trustees#765-1892) Final Planning Board Approval. Final Fire Inspection from Fire Marshall. Final Landmark Preservation approval. BUILDING PERMIT: 34411 - Sunroom Addition -- mOAD uCUT¢:I./ OS U E l'ow~v OF $ou~w~.D, N.Y. FOUR SEA SONS CURVED EAVE IOl,el s u N n O O. S . ENGINEERING AND STRUGTURAL LOADING INFORMATION EFFECTIVE DATE: 12-08 RL REVISION C BW GG XH ~ TS 2 SYSTEM 4E GLAZING BAR GLAZ]NG BAR ROOF LIVE WIND SPEED (mph) WIND SPEED (mph) WIND SPEED (mph) WIND SPEED (mph) MODELS D.C. SPACING TYPE LOAD EXPOSURE EXPOSURE EXPOSURE EXPOSURE (~)sf~ B C D B C O B C D I~ C D ECLT-3z 2'~ 5/8" 4GBA 240 200 180 160 200 180 160 150 135 120 150 135 120 ECLT-5 2 2'415/8" 4GBA 75 200 180 160 180 160 145 110 100 90 140 125 115 2'~ 5/8" 4GBA 25 130 115 105 130 115 105 90 80 70 130 115 105 ECLT'8 2 2'~ 5/8" 4HBA 33 140 125 115 140 125 115 90 80 70 130 115 105 2'~ 5/8" 4GBA 10 95 85 75 95 85 75 85 75 70 N/A N/A N/A ECLT-10 2'dl 5/8" 4HBA 15 105 95 85 105 95 85 85 75 70 NIA N/A N/A 2'~ 5/8" 4GBA+4RS 39 145 130 115 120 105 95 85 75 70 N/A N/A N/A ECLT'13 ~ 2'-6 5/8' 4HBA+4RS 48 145 130 115 120 105 95 85 75 70 N/A N/A N/A 2'-6 5/8' 4GBA+4RS 24 125 110 100 105 95 85 85 75 70 N/A N/A N/A 2'~ $/8" 4HBA+4RS 27 130 115 105 105 95 85 85 75 70 N/A N/A N/A ECLT-32 3'-0 5/8" 4GBA 200 200 180 160 200 180 160 140 125 115 150 135 120 ECLT-52 3'-05/8" 4GBA 62 185 165 150 180 160 145 110 100 90 140 125 115 3'-0 5/8" 4GBA 21 120 105 95 120 105 95 90 80 70 120 105 95 ECLT-8 2 3'~) 5/8" 4HBA 29 135 120 110 135 120 110 90 80 70 130 115 105 3'-0 5/8' 4HBA 14 105 95 85 105 95 85 85 75 70 N/A N/A N/A ECLT-10 3'4) 5/8" 4GBA+4RS 65 170 150 140 130 115 105 85 75 70 N/A N/A N/A 3'-0 5/8' 4GBA+4RS 33 140 125 115 120 105 95 85 75 70 N/A N/A N/A ECLT'13 ~ 3'~ 5/8" 4HBA+4RS 39 145 130 115 120 105 95 85 75 70 N/A N/A N/A 3'435/8" 4GBA+4RS 20 115 100 90 105 95 85 85 75 70 N/A N/A N/A ECLT-15 ~ 3'-0 5/8" 4HBA+4RS 23 120 105 95 105 95 85 85 75 70 N/A N/A N/A NOTE 1: 13XH AND 15XH MODELS REQUIRE (2)AND (3) HEAVY GABLE MULLION BARS EACH GABLE RESPECTIVELYTO OBTAIN WIND LOAD NOTE 2: 3TS, 5TS AND 8TS MODELS REQUIRE VERTICAL RAFTER STIFFENERS ON ALL VERTICAL BARS TO OBTAtN WIND LOAD OKLAHOMA OREGON 4GB4RS - 25 LITE BAR WtTH STIFFENER 4HBA4RS - 2 5 H E A'v'¢ BAR WITH STIFFENER 2 ALUMINUM ALLOY FOR GLAZING BARS IS 6005-T5 3/ DEAD LOAD OF ROOF SYSTEM IS 7 PSF 4~ ALL UNI3$ SHOWN ON TH~S pAGE ARE ACCEPTABLE FOR CONSTRUCTION IN SEISMIC ZONE 4 5~ DEFLECTION ARE BASED ON L120 LIVE CRITERIA 6~ WINDS ARE BASED ONAN ENCLOSED STRUCTURE 7~THIS SUMMARY PERTAINS TO THE STRUCTURAL INTEGRITY OF OUR UNIT UP TO, BUT NOT INCLUDING, THE CONNECTtONS TO THE EXISTING STRUCTURE ANDIORANYNEWCONSTRUCTION ALLSUBSTRUCTURE DESIGN REQUIREMENTS AND CONNECTIONS TO THE EXISTING STRUCTURE ARE NOT INCLUDED IN THE SCOPE OF WORK FOR THE FOUR SEASONS PRODUCT, AND MUST BE DESIGNED BY OTHERS. 8J THE ENGINEERING DESIGN SCOPE FOR THE FOUR SEASONS PRODUCT DOES NOT ACCOUNT FOR SPECIAL LOAD CONDITIONS CREATED BY ATTACHMENT TO THE EXISTING STRUCTURE THESE MAY INCLUDE SNOW DRIFTING OR UNBAEANCE SNOW LOADING ANY SPECIAL LOADING CONDITIONS MUST BE EVALUATED BY OTHERS 9) ENGINEERS CERTIFICATION I CERTIFy THAT THESE SPECIFICATIONS HAVE BEEN PREPARED UNDER MY DIRECT SUPERVISION AND THAT I AM A REGISTERED PROFESSIONAL ENGINEER IN THE STATES SHOWN SEASON5 ~'~ ~ ·-- ~ '- HO! BROOK. 14( 5 PINETREE DRIVE CUTCI-IO@UE, NY ~ MEMORIAL HWY HOLBROOK., NY 11741 (Off,cc) 63 I 563 4000 DRAWING INDEX PLOT PLAN HOt-.TON ,.51 - PLOT PLAN ...... - RJ%51PENCE 52 - GEN. NOTES z.,~,~ ~. /,,,,,,~, ¢',.,~o#~'J L........................................ ~ / 53 - FND PLAN i ~i~,/~t o/ r,,',~y -~f- ,--. ~, .-'- S4 I=ND DETAILS ' I '"' ,,,.~-~.+'~-... - ,¢~.o', ._J_ ENGINEERING 55 RD01= CONN. DTLS ,,,.~ · .. - ... ,~,~[ ,~,,~-., .... .. · . '~ '-,"-,'. ' ~,,..,", ,. !SERVICF::5. ?.C. .,*~.~ !.. ,: ,"~'I, '~; , · 112 WILSON DRIVE '"' ' ~' ' ' ;-!: PORT JEF~:ER.~ON, NY I 1777 I ffA..STENER. 5CIJEDULE FOR SYSTEM 4E ¢ 4EL ~ · ¢ ~_ / OFFICE: (63 I 474 '-.' - ,; ','. ' · . .-. .. ,-.. USE Jba, WFUL / ,,,,.-~, -o.,.o.~.,.,~., . .4 · ' · ' ,,~ WITHOUT CERTIFICAT~ "~'"~"'" "" ""'"" i" .. ;:' '. , ." '., ""'O.&OCCUPANCY -. ;£ - ~,~:.- & ' .' ' , PROVI~DBYALIC[NS[D~ND¢UR~R. ~[ '; ' ' ' -------~ ~1 ~- ' 765-!802 8Ak! : : ~ ~VISION5 P~DED~: - 224~Q.~. (0.5%) . ~ ~ ~ ~ ¢~ ' '. ~1 ~ FOR POURu2 (';. ~,,;,ETE ~=-' ~ ~ ~ucn,,r,~mL TOT~: = 2.~1 ~e.~. (5.~) N - · '-~ ~ ;/'~ ' ' ' I I ~ '. : 2. ROUGH - ~.~L~A~A~T~O ' ' ~ ' ~ .',?~ ' · ~1 ~ ' 3. INSULATION U*~n~T E~L:~L: '= ,"~ZS ~..~25 SQ. ~ ~ ~ "" .~// ~ ~";' :j ' - ' 'i~ ; ,, 4. FINAL- COF;~TRUC~:.ON MUST TOT~IDTING:~ 3.~5050.~ (~) ' ' " ": ' '¢'""~ ~ "' ' : *~"1 "' " BE COMPLET~ ~()R CO. PROP~[D ~A: - Z24 50. ~ ' ' ~ ~' ~ ' I ~ ' ' ' ALL CONSTRUCT; 3N SPA' L MEET THE r.A.~.(ffL~E~TIO)=D.D% J "~ % I ' ' " ';' ' l~l ' :4.."' · REQUIREMENTS OF THE CODES OF NEW .~{ .~ .f~ ' · .~ .1 ,r ', ~ . ..J ' · ,. ~. ;.. j · I~] ' .. '; YORK STATE. NOT RESPONSIBLE FOR ~VIE~D BY: ~ ~ -' ¢ '~ I t f -' . .': . ". · f 1 , ~ . . DES GN OR CONSTRUCTION ERRORS. 56~: SEE P~N FA..STENER. SCHEDULE ~OR SYSTEM 4E ¢ ,,4EL TO EXI~T1NG STRUCTURe5 ¢ FOUNDATION5 POUR. GENPRAL NO-it5 SEASON5 HO115ROOK 5005 VETEP-,AN5 4 ~L MC-SG (COD~ 74) CLE~ ARGON WALL GLO5 H~ THff POLLING CONFORM5 ~T~ PAETIALLY ENCLOSED DEDIGN AND DOE5 NOT ~QUI~ HU~IC~E 5fl~E~ D ~T~UCTU~L LUMDER MINIMUM P~P~RTI[~: ~ ~ AND ~0 ASH~* ~NTER R V~Ue ~ 40 5. LAT~ DESIGN CONTEND DY ~ND. POKT JEFPE~ON, NY I I 777 i. ~L 5T~CTU~L ALUMINUM CONFO~5.0 TH, MINIMUM "QUI"M[NT5 OF ~5-T5 FOR ~L~ ~O T[MPER' D[FL[¢,O. UMITS: I T.[5[ D~.G5 O0 NOT CONTAIN "[C[55'~ COMPON,NT5 FOR 5AF[~ GENE~ CLIMATIC * GEOG~PHIC DESIGN CEITEEIA D~WN DY: A5 DESIGN UNOER~[NT FLOOD F~ZING ~CALE: 5Eft P~N DESIGN FROST LIN~ TEEMITE5 DECAY TEMPE~TU~ ~OUl~O H~A~ , LOAD 5FEED (MPH) CATEGORY ~ATHERING DE~H IND~ DATE: 1-2 1-0~ 52 or 5 DOUR 5005 VETEP..AN5 MEMORIAL HWY HOLE$P-.OOK., NY I 174 (O~flce) ~;3 I 5~3 4000 EXISTING 5TP-.UCTU RE ~ HORTON RESIDEIXlCE 1 4~5 PINETREE DRIVE CUTC.OOU=, ), ENGINEERJNG n,~ 5ERVlCE~, I I 2 WIL.~ON DRIVE PORT JEPFER-.~ON, NY 11777 OPFICE: EXISTING BRICK, PATIO FACE CONCRETE / CURB, TYP UON~ DENOTE5 OUT~IDE FACE OF CONCRETE CURB TTP. UON DENOTE~ OUT~IDE · / FACE OF ~UNROOM1 . / FOUNDATION I 5L I I 3/4" REVI.,~ION5 ( POUNDATION ?LAN ~O1~: ELEVATION = 0'-0" (~FEKENCE) )~WN ~EVIE~D ~CALE: ~EE PLAN ~ATE: 1-21-09 ~3 o~ 5 ., FOUR. HOI I~RO01~ 5005 VETEP~AN~ MEMORIAL HWY IflOLDROOK., NY II 741 (Office) G3 I 5~3 4000 OUT~IDE EDGE oF~^~.~ HORTON ~ .. ~,N~,OR ~L~., R~51DENCE --; ~ - c~ CUTCHOQUF. NY  _ #4 DOWEL ;~ I'-~ ~ NOT~: LONG ~, UON -- OUTSID~ EDG~ FLAN VIEW NEW FINISHED FLOR ~ ~ FOUNDATION Or ~OOM I I WALL , ~ ENGINEE~NG t_ ~j J,' ~o~ ~ s~v~c~,~.c GROUT ~ WALL = POE ANGlO.GE ~ ..... I T~ICKN~55 5, , , 3/4" FOET J~FE~ON, NY I 1777 314" CHAFER ~ ~' EXP JOINT I , CONT ~3 ~I~T D~C~ j ........ ~ ~ OFFICE: (G3 I ) 474 I ~,~ or cu~ , ~ I - --~ I ~ , ..- x · ~ ~ FOUNDATION ~O~OM Of NEW ~G ~ ~ ~ FIOUNDATION DETAIL ~ ~ POUNDATION DETAIL AT ~IST 5TRU~U~ ~ UOT~ ~VIDION~ D~ DY: ~CALE: ~EE P~N DATE: 1-21-0~ 54 o~ 5 POUR ~EA..~ON~ I-I01 5OO5 VETERAN5 MEMORIAL HWY PIOL[3ROOK,, NY 117,41 (Off, cc) g3 I 5G3 4000 HOR.TON RESIDENCE I 4G5 ?INETREE DRIVI~ CUTCI'IOQUE, NY ENGINI=I=~NG NEW PLYWOOD D(15TING / / FASTEN TO ~ND ~ ~ OF ~ ~ ~ ~ ~ I I 2 WILSON DRIV~ D~NOT~5 ~O~nON / /..., = ~,*~ ~ J ~ ~ I PO~T J~P~ON, NY I ~ 777 ~1 ~ · . / ~ .~ ~ ~ ~ . ~/L?:.. :'~ ~ ~-~ ............ n . . ~ t l I ~ NEW (2) 2x~ LEDGER f~TEN W/U) 3/~ ~G DOLT,W~IN. ~ II ~ 3" EM~EDMENT TO END5 Off ~IST. ~E~ .~ 1 g' O.C. N~W POU~ 5E~ON5 D~ ............ '1 , * TO ~IDTING TOP P~TE ~ G" 0 C COU~Td~IN~NG DOLT5 P~TEN TO(2) 2x8 LEDGER W/3/~ ¢ ~G DOLT5 I~ I ~ ~QUI~D TO INSTALL DUNRo~ ~IDGE W~IN.3" EMDEDMENT ~ 4" O,C. 5TAGER~D zJ ~ P 5T~IGHT EAVE CONNECTION D~AIL AT ~I¢T 5T~UCTU~ ~VI~iON5 D~ BY: &CALE: SEE DATE: I 55 o~ 5 I 5L¢ l/4" ~ 5'-4 5/i G" 5'-4" R.O. CONTP4~,Cf DATE: 01/20/09 ~ ELE~:VATION 13'-4 l/4' DATE: 01/23/09 S6/k[: I/4'=1'-0' JOB ~: ~ el~Aq~n A.~. EN~IN~IN~ DOCUMENT~ A~ VALID ONLY ~:,.'-,'-o' SERVICE5 P.e. HOETON WITH AN ORIGINAL DTAMP ~ 12 WILSON DR. AND DATED 51GNATU~ PORT JEFffE~ON . N.Y. I 1777 J OP ~ (63 I ) ~07-25~6 DOCUMENTS ABE VALID ONLY ~x,s:*.G 'WITH AN ORIGINAL DTAMP COUNTERP~"ING AND DATED 51GNATU~Ill G' G~ING TAP[G~INGE~'D~IDG=~a (~Y OT~[~)(A. AG~ALUMiNuMALUMiNUMcAp (A'4GC~) (4G~B) MINIMUM CONN[~ION~ ~ MUNTIN DETAIL MUST D= ~'D ALUMINU~ - / ~ OF TH~S[ CONNE~ONS (4G~) G~ING DAK Il MUST ~E OETEmINE~ [~D ~UMINUM ~ )~ DY: AKW I /b,, ~ : 3/b" DATE: 01/23~9 / 30 314" O.C. GASLE ~ ~ 2 7/I *" ~ A.5. ENGINEERING -- 13'-4 I/4" OUT TO OUT Or SILL - SERVICE5 P.e. HORTOh 51LLDETAIL ~ D ~WALLDA~DETAIL 112WILSONDR. (631 ~ DOCUMENTS ARE VALID ONLY '- WITH AN ORIGINAL .~TAMP ~2 I/4"~_ .'~0 ~,/~" 0 C. P, AY% AND DATED SIGNATURE /8" INDUCTED MULLION O~ ~F . _____ ~ SABLE MULLION / I I ~ ~ U U I ~ EEVE~[ ADA~O~ ~ it, ~ % I MUST eE DE~IN~D -- GADLEMULLIONST~P( NGI ~) ~ P~N D~AIL AT ~ILL = G~ING DAR ~ . ~ G~IN'G DAB WITH GABLE END ~ m O[ T"~5~ 60NN[¢ION5 -- 5/¢ X 2 W~D ~ I I ~ -- DiLL CUP fCN46~} NOI DATE P~N D~AIL AT ~ILL sc~ 6-- ~ ~ 60NT~ DATE: 01/20/0~ ~.'o~uuJ ~ 2 I/4'~ BEAU~ C~ ~ DATE: 0 1/2 OUT TO OUT OF DILL , A.5. ENGINEERING POET JEP~E~ON , N.Y. I 1777 ~ ~u4 0 A~UAL DEblGN Of TH~S[ CONNEXION5 ~ % I -- % - ~ ~ ~ J ' 0 Z MUSTBEDET~INEDBYOTIE~. % ~ i I~ ~GAB~ MULUON (4GMA) J T ~ ~ ' B~u~ cAP - 5'-0" DOOR / G I I/2" ~L TO ~L (4~c~ (2 GAD~ DA~) , v ~ ~v 'N~T*LLER SLIDING DOOR  SLIDING DOOR D~AIL ]~WN BY: AKW (EVIE~D ~ATE: 01/25/0¢ A.5. ENGINEEEING DOCUMENT5 A~E VALID ONLY $EBVICE5 P.C. =HO TON WITH AN O~IGINAL 5TAMP J J 2 WIL5ON DK. AND DATED 51GNATU~ PORT JEFFE~ON, N.Y. (~3 J ) ~o7-25¢~ AWNING DETAIL~ ~ D~.ILLING r' ~. 5ILL (4GSU ~ ~ ~ 0 SILICONE SE~T~ . MINIMUM CONNE~IONS ~Y OTHE~ //~ mN THE ~H~UU~ ON A.~. ENGINEERING ~o~: DOCUMENT~ A~ VALID ONLY ~ERVICE~ P.C. HORTON WITH AN OEIGINAL ~TAMP I 12 WILDON DK. AND DATED DIGNATU~ PORT JEFFE~ON HATCH LLJ / ~TCH P~T5 R~HI ~ ~ ~ ~ / .~ ?~ 7/6" INSULTED G~5 x / A~ SUPPLIED / , ~ DU~ TAP~ ~ I~ HAT~ HK, 02G ~ r / ~-- -~lOx I l/~5~. ' ~ ~ 0 < A.5. ENGINEERING ~o~: POCUMENTSA~VALOONLY 5ERVICE~ D.C. ~O~TON WITH AN ORIGINAL ~TAMP ~ ~ a Wl~ON AND DATED 51GNATU~ POET JE~E~ON , N.Y. I ~ 777 lob T~le ob No Part Ref Sheet NoI Rev By Da*~27.Jan.09 Chd File 13GG30RR.std IDate/Time 28-Jan-2009 14:01 Z Print Time/Date: 28101/2009 14:23 STAAD.Pro for Windows Release 2006 Print Run 1 of 1 Rev lob Title Ctient Job No Sheet No Pad Ref By Date27.Jan.09 Chd Fi)e 13GG30RR.std IDate/Time 28-Jan-2009 14:01 Load Print Time/Date: 28/01/2009 1423 STA,AD.Pro for Windows Release 2006 Print Run 1 of 1 lob Title 3b No S~eet No 1 Rev Par[ Ref By Date27_Jan_09 Chd File 13GG30RR.std IDa[e/Time 28-Jan-2009 14:01 193 20O 111 ~. Yx 42 105 172 107 169 Load Print Time/Date: 28/0112009 1423 STAAD.Pro for Windows Release 2006 Print Run I of 1 Wednesday, January 28, 2009, 02:23 PM PAGE NO. 1 * STAAD.Pro * * Version 2006 Bld 1002.US * * Proprietary Progr~ of * * Research Engineers, Intl. * * Date= JAN 28, 2009 * * USER ID: Four Seasons Solar Products * 1. STAAD SPACE SYSTEM 4E CLT-13GG INPUT FILE: 13GG30RR.STD 2. *4GBA WITH R~FTER STIFFENER 3. *30" ON CENTER 4. START JOB INFORMATION 5. ENGINEER DATE 27-JA~-09 6. END JOB INFORMATION 7. INPUT WIDTH 72 8. UNIT INCHES PO~/ND 9. JOINT COORDINATES 10. 1 0 0 0; 2 0 0 30.75; 3 0 0 61.5; 4 0 0 92.25; 5 0 0 123; 6 0 0 158.875 11. 7 0 46.75 0; 8 0 81.199 0; 9 0 114 0; 10 30.625 0 158.875 12. 11 30.625 114 0; 12 61.25 0 158.875; 13 61.25 114 0 13. 14 14. 17 15. 21 16. 24 17. 27 18. 31 19. 34 20. 37 21. 39 22. 41 23. 43 24. 45 25. 47 26. 50 27. 52 28. 55 29. 58 30. 61 31. 64 32. 67 33. 70 34. 73 35. 76 36. 78 37. 81 38. 84 39. 87 40. 90 91.875 0 158.875; 15 91.875 114 0; 16 122.5 0 158,875 122.5 114 0; 18 153.125 0 158.875; 19 153.125 114 0; 20 183,75 0 0 183.75 0 30.75; 22 183.75 0 92.25; 23 183.75 0 123 183.75 0 158.875; 25 183.75 46.75 0; 26 183.75 81.199 0 183.75 114 0; 28 0 46.75 30.75; 29 0 46.75 61.5; 30 0 46.75 92.25 0 46.75 123; 32 0 46.75 158.875; 33 0 54.346 158.875 0 81.199 30.75; 35 0 81.199 61.5; 36 0 81.199 92.25 30.625 46.75 158.875; 38 30.625 54.346 158.875 61.25 46.75 158.875; 40 61.25 54.346 158.875 91.875 46.75 158.875; 42 91.875 54.346 158.875 122.5 46.75 158.875; 44 122.5 54.346 158.875 153.125 46.75 158.875; 46 153.125 54.346 158.875 183.75 46.75 30.75; 48 183.75 46.75 92.25; 49 183.75 46.75 123 183.75 46.75 158.875; 51 183.75 54.346 158.875 183.75 81.199 30.75; 53 183.75 81.199 61.5; 54 183.75 81.199 92.25 0 63.787 156.307; 56 0 71.395 149.107; 57 0 77.191 138.679 0 81.199 123; 59 0 89.399 92.25; 60 0 97.599 61.5 0 105.799 30.75; 62 30.625 63.787 156.307; 63 30.625 71.395 149.107 30.625 77.191 138.679; 65 30.625 81.199 123; 66 30.625 89.399 92.25 30.625 97.599 61.5; 68 30.625 105.799 30.75; 69 61.25 63.787 156.307 61.25 71.395 149.107; 71 61.25 77.191 138.679; 72 61.25 81.199 123 61.25 89.399 92.25; 74 61.25 97.599 61.5; 75 61.25 105.799 30.75 91.875 63.787 156.307; 77 91.875 71.395 149.107 91.875 77.191 138.679; 79 91.875 81.199 123; 80 91.875 89.399 92.25 91.875 97.599 61.5; 82 91.875 105.799 30.75; 83 122.5 63.787 156.307 122.5 71.395 149.107; 85 122.5 77.191 138.679; 86 122.5 81.199 123 122.5 89.399 92.25; 88 122.5 97.599 61.5; 89 122.5 105.799 30.75 153.125 63.787 156.307; 91 153.125 71.395 149.107 C: \at work\HORTON\6 BAYS\13GG3ORR.ani Page 1 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 2 *4GBA WITH RAFTER STIFFENER 41. 92 153.125 77.191 138.679; 93 153.125 81.199 123 42. 94 153.125 89.399 92.25; 95 153.125 97.599 61.5 43. 96 153.125 105.799 30.75; 97 183.75 63.787 156.307 44. 98 183.75 71.395 149.107; 99 183.75 77.191 138.679 45. 100 183.75 81.199 123; 101 183.75 89.399 92.25; 102 183.75 97.599 61.5 46. 103 183.75 105.799 30.75 47. MEMBER INCIDENCES 48. 1 1 7; 2 2 28; 3 3 29; 4 4 30; 5 5 31; 6 6 32; 7 32 33; 8 33 55; 9 7 8 49. 10 28 34; 11 29 35; 12 30 36; 13 31 58; 14 36 59; 15 35 60; 16 34 61 50. 17 8 9; 18 10 37; 19 37 38; 20 38 62; 21 12 39; 22 39 40; 23 40 69 51. 24 14 41; 25 41 42; 26 42 76; 27 16 43; 28 43 44; 29 44 83; 30 18 45 52. 31 45 46; 32 46 90; 33 20 25; 34 21 47; 35 22 48; 36 23 49; 37 24 50 53. 39 50 51; 41 51 97; 43 25 26; 44 47 52; 45 48 54; 46 49 100; 47 54 101 54. 48 53 I02; 49 52 103; 50 26 27; 51 7 28; 52 28 29; 53 29 30; 54 30 31 55. 55 31 32; 56 8 34; 57 34 35; 58 35 36; 59 36 58; 60 32 37; 61 58 65 56. 62 59 66; 63 60 67; 64 61 68; 65 37 39; 66 65 72; 67 66 73; 68 67 74 57. 69 68 75; 70 39 41; 71 72 79; 72 73 80; 73 74 81; 74 75 82; 75 41 43 58. 76 79 86; 77 80 87; 78 81 88; 79 82 89; 80 43 45; 81 86 93; 82 87 94 59. 83 88 95; 84 89 96; 85 45 50; 86 93 100; 87 94 101; 88 95 102 68. 89 96 103; 90 47 25; 91 49 48; 92 50 49; 93 52 26; 94 53 52; 95 54 53 61. 96 100 54; 97 55 56; 98 56 57; 99 57 58; 100 58 59; 101 59 60 62. 102 60 61; 103 61 9; 104 97 98; 106 98 99; 108 99 100; 110 100 101 63. 112 101 102; 114 102 103; 116 103 27; 118 62 63; 119 63 64; 120 64 65 64. 121 65 66; 122 66 67; 123 67 68; 124 68 11; 125 69 70; 126 70 71 65. 127 71 72; 128 72 73; 129 73 74; 130 74 75; 131 75 13; 132 76 77 66. 133 77 78; 134 78 79; 135 79 80; 136 80 81; 137 81 82; 138 82 15 67. 139 83 84; 140 84 85; 141 85 86; 142 86 87; 143 87 88; 144 88 89 68. 145 89 17; 146 90 91; 147 91 92; 148 92 93; 149 93 94; 150 94 95 69. 151 95 96; 152 96 19 70. ELEMENT INCIDENCES SHELL 71. 38 1 2 28 7; 40 2 3 29 28; 42 3 4 30 29; 105 4 5 31 30; 107 5 6 32 31 72. 109 31 32 55 58; 111 7 28 34 8; 113 28 29 35 34; 115 29 30 36 35 73. 117 30 31 58 36; 153 58 36 59; 154 35 36 59 60; 155 34 35 60 61 74. 156 8 34 61 9; 157 20 21 47 25; 158 22 21 47 48; 159 22 23 49 48 75. 160 23 24 50 49; 161 49 50 97 100; 162 25 47 52 26; 163 48 47 52 54 76. 164 48 49 100 54; 165 100 54 101; 166 53 54 101 102; 167 52 53 102 103 77. 168 26 52 103 27; 169 6 10 37 32; 170 32 37 38 33; 171 33 38 62 55 78. 172 10 12 39 37; 173 37 39 40 38; 174 38 40 69 62; 175 12 14 41 39 79. 176 39 41 42 40; 177 40 42 76 69; 178 14 16 43 41; 179 41 43 44 42 80. 180 42 44 83 76; 181 16 18 45 43; 182 43 45 46 44; 183 44 46 90 83 81. 184 18 24 50 45; 185 45 50 51 46; 186 46 51 97 90; 187 55 62 63 56 82. 188 56 63 64 57; 189 57 64 65 58; 190 58 65 66 59; 191 59 66 67 60 83. 192 60 67 68 61; 193 61 68 11 9; 194 62 69 70 63; 195 63 70 71 64 84. 196 64 71 72 65; 197 65 72 73 66; 198 66 73 74 67; 199 67 74 75 68 85. 200 68 75 13 11; 201 69 76 77 70; 202 70 77 78 71; 203 71 78 79 72 86. 204 72 79 80 73; 205 73 80 81 74; 206 74 81 82 75; 207 75 82 15 13 87. 208 76 83 84 77; 209 77 84 85 78; 210 78 85 86 79; 211 79 86 87 80 88. 212 80 87 88 81; 213 81 88 89 82; 214 82 89 17 15; 215 83 90 91 84 89. 216 84 91 92 85; 217 85 92 93 86; 218 86 93 94 87; 219 87 94 95 88 90. 220 88 95 96 89; 221 89 96 19 17; 222 90 97 98 91; 223 91 98 99 92 91. 224 92 99 100 93; 225 93 100 101 94; 226 94 101 102 95 92. 227 95 102 103 96; 228 96 103 27 19 93. DEFINE MATERIAL START 94. ISOTROPIC ALUMINUM 95. E 1E+007 96. POISSON 0.33 C:lat work\HORTON\6 BAYS\13GG3ORR.anl Page 2 of 89 SYSTEM 4E CLT-13GG *4GBA WITE RA~TER STIFFENER 97. DENSITY 0.098 98. ALP}{A 1.28E-005 99. DAMP 0.03 100. ISOTROPIC MATERIAL1 101. E 12000 102. POISSON 0.22 103. DENSI~ 0.0902778 104. DAMP 2.8026E-044 105. ISOTROPIC STEEL 106. E 2.9E+007 107. POISSON 0.3 108. DENSITY 0.283 109. ALPHA 6.5E-006 110. DAMP 0.03 111. END DEFINE MATERIAL 112. STABT USER TABLE 113. TAMLE 1 STARS.TXT 114. TABLE 2 BACK TABLE.TXT 115 . END 116. MEMBER PROPERTY AMERICAN 117. 6 TO 8 18 TO 32 37 39 41 97 TO 104 106 108 110 112 114 116 118 125 - 118. 132 139 146 UPTAMLE 1 4GBA 119. 51 TO 93 96 UPTAMLE 1 4MUNTIN 120. 119 TO 124 126 TO 131 133 TO 138 140 TO 145 147 TO 151 - 121. 152 UPTABLE 1 4GBA4RSB 122. 94 95 PRIS A~ 1.613 IX 9.65091 IY 2.8823 IZ 1.4676 YD 2.44 ZD 3.5 123. MEMBER PROPERTY AMERICAN 124. 1 TO 5 9 TO 17 33 TO 36 43 TO 50 UPTANLE 2 4GMA4RSB 125. ELEMEN=f PROPERTY 126. 38 40 42 105 107 109 111 113 118 117 153 TO 228 THICKNESS 0.25 127. MEMBER RELF~ASE 128. 1 TO 6 18 21 24 27 30 33 TO 37 START MY MZ 129. 13 TO 17 46 TO 94 96 103 116 124 131 138 145 152 END MY MZ 130. 51 TO 93 95 96 START MY MZ 131. UNIT FEET POUND 132. CONST;~NTS 133. BETA 90 MEMB 6 7 18 19 21 22 24 25 27 28 30 31 37 39 51 TO 60 65 70 - 134. 75 80 85 90 TO 96 135. BETA 14 MEMB 61 TO 64 66 TO 69 71 TO 74 76 TO 79 81 TO 84 86 TO 89 136. MATERIAL ALUMINIIM MEMB 1 TO 37 39 41 43 TO 93 96 TO 104 106 108 110 - 137. 112 114 116 118 TO 152 138. MATERIAL MATERIAL1 MEMB 38 40 42 105 107 109 111 113 115 117 153 TO 228 139. MATERIAL STEEL MEMB 94 95 140 . SUPPORTS 141. 1 TO 27 PINNED 142. LOAD 1 DEAD SELFWEIGHT OF STRUCTURE 143. SELFWEIGHT Y -1 144. LOAD 2 LIVE 30 PSF ROOF LOAN 145. MEMBER LOAB 146. 98 TO 103 106 108 110 112 114 116 119 TO 124 126 TO 131 133 TO 138 - 147. 140 TO 145 147 TO 152 URI GY -76.6 148. LOAD 3 LIVE 120 MPH EXP C WIND LOAD-X 149. ELEMENT LOAD 150. 38 40 42 105 107 109 111 113 115 117 153 TO 156 PR GX 32.8 151. 157 TO 168 PR GX 26 152. 169 TO 187 194 201 208 215 222 PR GZ 30.5 Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 3 c:\at work\HORTON\6 BAYS\13GG3ORR.ani Page 3 of 89 SYSTEM 4E CLT-13GG *4GBA WITH Rg~FTER STIFFENER 153. 171 174 177 180 183 186 TO 228 PR 35.02 Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 4 154. LOAD 4 LIVE 120 MPH EXP C WIND LOAD-Z 155. ELEMENT LOAD 156. 38 40 42 105 107 109 111 113 115 117 153 TO 156 PR GX -30.5 157. 157 TO 168 PR GX 30.5 158. 169 TO 187 194 201 208 215 222 PR GZ -32.8 159. 171 174 177 180 183 186 TO 228 PR 35.02 160. LOAD COMB 5 DEAD + ROOF 161. 1 1.0 2 1.0 162. LOAD COMB 6 0.6 DEAD + SIDE WIND 163. 1 0.6 3 1.0 164. LOAD COMB 7 0.6 DEAD + FRONT WIND 165. 1 0.6 4 1.0 166. LOAD COMB 8 DEAD + .75 ROOF + .75 SIDE WIND 167. 1 1.0 2 0.75 3 0.75 168. LOAD COMB 9 DEAD + .75 ROOF + .75 FRONT WIND 169. 1 1.0 2 0.75 4 0.75 170. UNIT INCHES POUND 171. PERFOR/~ A~ALYSIS ** WARNING ** A SOFT MATERIAL WITH (1.0 / 2.625E+02) TIMES THE STIFFNESS OF CONCRETE ENTERED. PLEASE CHECK. PROBLEM STATISTICS NUMBER OF JOINTS/MEMbER+ELEMENTS/SUPPORTS = 103/ 228/ 27 ORIGIN;tL/FINALBAND-WIDTH= 84/ 16/ 102 DOF TOTAL PRIMARY LOAD CASES = 4, TOTAL DEGREES OF FREEDOM = 618 SIZE OF STIFFNESS MATRIX = 64 DOUBLE KILO-WORDS REQRD/AVAIL. DISK SPACE 13.4/ 43632.7 ME 172. LOAD LIST 5 TO 9 173. PRINT SUPPORT REACTION C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 4 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 5 *4GBA WITH RAFTER STIFFENER SUPPORT BEACTIONS -UNIT POUN INCH STRUCTURE TYPE = SPACE JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z 5 0.00 13.10 0.18 0.00 0.00 0.00 6 -81.83 7.22 -0.30 0.00 0.00 0.00 7 76.11 8.12 0.35 0.00 0.00 0.00 8 -61.37 12.65 -0.11 0.00 0.00 0.00 9 57.09 13.33 0.38 0.00 0.00 0.00 5 0.00 335.88 -0.18 0.00 0.00 0.00 6 -370.44 -54.13 -0.75 0.00 0.00 0.00 7 344.46 -53.89 1.16 0.00 0.00 0.00 8 -277.83 189.15 -0.71 0.00 0.00 0.00 9 258.35 189.34 0.73 0.00 0.00 0.00 5 0.00 304.05 ~0.88 0.00 0.00 0.00 6 -341.81 -61.31 -1.06 0.00 0.00 0.00 7 317.82 -63.18 2.08 0.00 0.00 0.00 8 -256.36 161.11 -1.43 0.00 0.00 0.00 9 238.36 159.71 0.93 0.00 0.00 0.00 5 0.01 296.69 -1.22 0.00 0.00 0.00 6 -313.10 -56.43 -1.52 0.00 0.00 0.00 7 291.10 -55.13 2.94 0.00 0.00 0.00 8 -234.82 161.02 -2.02 0.00 0.00 0.00 9 218.33 162.00 1.33 0.00 0.00 0.00 5 0.00 313.82 -0.63 0.00 0.00 0.00 6 -302.32 -57.62 -3.38 0.00 0.00 0.00 7 281.11 -87.30 3.59 0.00 0.00 0.00 8 -226.74 173.19 -3.00 0.00 0.00 0.00 9 210.83 150.93 2.23 0.00 0.00 0.00 5 0.54 198.03 0.17 0.00 0.00 0.00 6 -183.73 -495.35 -77.59 0.00 0.00 0.00 7 88.16 -78.85 83.82 0.00 0.00 0.00 8 -137.42 -237.92 -58.05 0.00 0.00 0.00 9 66.50 74.45 63.01 0.00 0.00 0.00 5 0.00 23.84 37.09 0.00 0.00 0.00 6 -142.22 13.24 -58.15 0.00 0.00 0.00 7 132.29 13.22 93.19 0.00 0.00 0.00 8 -106.66 23.20 -70.62 0.00 0.00 0.00 9 99.22 23.19 42.89 0.00 0.00 0.00 5 0.00 20.55 -0.67 0.00 0.00 0.00 6 -113.03 9.86 -67.27 0.00 0.00 0.00 7 105.09 10.24 -1.14 0.00 0.00 0.00 8 -84.77 19.01 -51.03 0.00 0.00 0.00 9 78.82 19.29 -1.43 0.00 0.00 0.00 5 0.02 103.07 -24.26 0.00 0.00 0.00 6 -189.07 93.50 -546.24 0.00 0.00 0.00 7 53.91 -35.44 -63.65 0.00 0.00 0.00 8 -141.79 144.05 -427.00 0.00 0.00 0.00 9 40.44 47.34 -65.06 0.00 0.00 0.00 5 0.99 613.45 -94.21 0.00 0.00 0.00 6 -172.81 711.55 -107.81 0.00 0.00 0.00 7 -0.66 -502.63 294.17 0.00 0.00 0.00 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 5 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT~13GG -- PAGE NO. 6 *4GBA WITH RAFTER STIFFENER SUPPORT REACTIONS -UNIT POUN INCH STRUCTURE TYPE = SPACE JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z 8 -128.88 -99.88 -149.05 0.00 0.00 0.00 9 0.22 56.81 152.44 0.00 0.00 0.00 11 5 0.03 513.05 155.52 0.00 0.00 0,00 6 -276.71 -291.96 -856.27 0.00 0.00 0.00 7 9.62 ~477.73 -294.14 0.00 0.00 0.00 8 -207.51 152.59 ~529.61 0.00 0.00 0.00 9 7.16 13.26 -108.02 0.00 0.00 0.00 12 5 0.20 667.04 -97.28 0.00 0.00 0.00 6 -173.60 -753.57 -105.64 0.00 0.00 0.00 7 0.79 -561.00 297.66 0.00 0.00 0.00 8 -130.06 -92.60 -149.63 0.00 0.00 0.00 9 0.74 51.83 152.84 0.00 0.00 0.00 13 5 -0.04 530.59 100.34 0.00 0.00 0.00 6 -274.83 -302.90 -822.95 0.00 0.00 0.00 7 4.90 -498.57 -227.89 0.00 0.00 0.00 8 -206.15 157.09 -544.59 0.00 0.00 0.00 9 3.64 10.33 -98.30 0.00 0.00 0.00 14 5 0.03 668.45 -97.27 0.00 0.00 0,00 6 -173,39 -756.11 -105.63 0.00 0.00 0.00 7 0.12 -562.08 297.65 0.00 0.00 0.00 8 -130.02 -93.48 -149.62 0.00 0,00 0.00 9 0.12 52.04 152.84 0.00 0.00 0.00 15 5 -0.01 531.29 97.71 0.00 0.00 0.00 6 -274.64 -303.00 -822.59 0.00 0.00 0.00 7 0.06 -499.50 -224.38 0.00 0.00 0.00 8 -205.98 157.51 -546.22 0.00 0.00 0.00 9 0.04 10.14 -97.56 0.00 0.00 0.00 16 5 -0.14 667.04 -97.28 0.00 0.00 0.00 6 -173.14 -756.39 -105.61 0.00 0.08 0.00 7 -0.56 -560.86 297.66 0.00 0.00 0.00 8 -129.95 -94.71 -149.61 0.00 0.00 0.00 9 -0.52 51.93 152.84 0.00 0.00 0.00 17 5 0.03 530.60 100.30 0.00 0.00 0.00 6 -276.45 -302.17 -825.75 0.00 0.00 0.00 7 -5.03 -498.62 -227.70 0.00 0.00 0.00 8 -207.32 157.64 -546.72 0.00 0.00 0.00 9 -3.75 10.30 -98.18 0.00 0.00 0.00 18 5 -0.95 613.66 -94.23 0.00 0.00 0.00 6 -170.46 -717.04 -107.91 0.00 0.00 0.00 7 0.83 -502.65 294.20 0.00 0.00 0.00 8 -128.54 -103.84 -149.13 0.00 0.00 0.00 9 -0.06 56.95 152.45 0.00 0.00 0.00 19 5 -0.10 513.28 154.72 0.00 0.00 0.00 6 -279.54 -290.06 -862.85 0.00 0.00 0.00 7 -10.17 -478.38 -291.71 0.00 0.00 0.00 8 -209.72 154.17 -535.13 0.00 0.00 0.00 9 -7.69 12.93 -106.77 0.00 0.00 0.00 20 5 0.00 13.50 0.32 0.00 0.00 0.00 C:\at work\HORTON\6 BAYS\13GG3ORR.ani Page 6 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 7 *4GBA WITH RAFTER STIFFENER SUPPORT REACTIONS -UNIT POUN INCE STRUCTURE TYPE = SPACE JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z 6 -64.86 7.50 -0.04 0.00 0.00 0.00 7 -76.12 7.53 -0.04 0.00 0.00 0.00 8 -48.65 13.15 0.19 0.00 0.00 0.00 9 -57.09 13.17 0.19 0.00 0.00 0.00 21 5 -0.03 498.62 -1.91 0.00 0.00 0.00 6 -411.20 -86.07 -5.75 0.00 0.00 0.00 7 -499.42 -86.14 6.96 0.00 0.00 0.00 8 -308.42 275.81 -5.73 0.00 0.00 0.00 9 -374.59 275.76 3.80 0.00 0.00 0.00 22 5 -0.03 452.01 -4.70 0.00 0.00 0.00 6 -404.18 -92.34 -6.81 0.00 0.00 0.00 7 -453.91 -85.73 9.48 0.00 0.00 0.00 8 -303.16 239.45 -8.49 0.00 0.00 0.00 9 -340.46 244.41 3.73 0.00 0.00 0.00 23 5 0.00 313.67 -4.59 0.00 0.00 0.00 6 -239.66 -1.66 -10.17 0.00 0.00 0.00 7 -281.12 -98.30 13.25 0.00 0.00 0.00 8 -179.74 215.09 -10.97 0.00 0.00 0.00 9 -210.84 142.61 6.60 0.00 0.00 0.00 24 5 -0.50 190.08 -2.65 0.00 0.00 0.00 6 -162.26 199.98 -83.14 0.00 0.00 0.00 7 -88.20 -58.16 90.75 0.00 0.00 0.00 8 -122.04 277.78 -64.26 0.00 0.00 0.00 9 -66.50 84.18 66.16 0.00 0.00 0.00 25 5 0.00 24.34 -1.50 0.00 0.00 0.00 6 -112.74 12.78 -9.05 0.00 0.00 0.00 7 -132.33 13.39 6.89 0.00 0.00 0.00 8 -84.56 23.20 -7.93 0.00 0.00 0.00 9 -99.25 23.65 4.03 0.00 0.00 0.00 26 5 0.00 20.59 -2.84 0.00 0.00 0.00 6 -89.62 10.79 -117.02 0.00 0.00 0.00 7 -105.11 10.60 25.74 0.00 0.00 0.00 8 -67.21 19.72 -90.16 0.00 0.00 0.00 9 -78.84 19.88 16.91 0.00 0.00 0.00 27 5 -0.06 103.21 -45.89 0.00 0.00 0.00 6 -178.17 -87.38 141.91 0.00 0.00 0.00 7 -53.66 -41.12 -34.15 0.00 0.00 0.00 8 -133.67 8.80 73.63 0.00 0.00 0.00 9 -40.29 43.19 -58.41 0.00 0.00 0.00 ************** END OF LATEST ANALYSIS RESULT ************** 174. PRINT JOINT DISPLACEMENTS ALL C:\at work\HORTON\6 BAYS\I3GG3ORR.anl Page 7 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER -- PAGE NO. 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JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE JOINT LOAD X-TRANS Y-TRANS Z-TRAN$ X-ROTAN Y-ROTAN Z-ROTAN 8 0.00000 0.00000 0.00000 0.00202 -0.00093 -0.00288 9 0.00000 0.00000 0.00000 -0.00170 -0.00003 0.00008 11 5 0.00000 0.00000 0.00000 0.01476 0.00016 -0.00062 6 0.00000 0.00000 0.00000 -0.01245 0.00586 -0.00110 7 0.00000 0.00000 0.00000 -0.01484 -0.00035 0.00083 8 0.00000 0.00000 0.00000 0.00136 0.00451 -0.00127 9 0.00000 0.00000 0.00000 -0.00044 -0.00014 0.00018 12 5 0.00000 0.00000 0.00000 0.01256 0.00003 0.00001 6 0.00000 0.00000 0.00000 -0.00676 -0.00129 -0.00380 7 0.00000 0.00000 0.00000 -0.01647 -0.00004 0.00004 8 0.00000 0.00000 0.00000 0.00402 -0.00095 -0.00285 9 0.00000 0.00000 0.00000 -0.00325 -0.00001 0.00004 13 5 0.00000 0.00000 0.00000 0.02168 0.00002 -0.00009 6 0.00000 0.00000 0.00000 -0.01852 0.00594 -0.00134 7 0.00000 0.00000 0.00000 -0.02182 -0.00014 0.00012 8 0.00000 0.00000 0.00000 0.00182 0.00447 -0.00107 9 0.00000 0.00000 0.00000 -0.00065 -0.00009 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0.00257 -0.27637 0.01080 0.00020 0.00008 8 0.17889 0.00061 0.05586 0.00296 -0.00093 -0.00269 9 -0.00263 -0.00018 -0.03868 0.00259 -0.00003 0.00011 39 5 -0.00059 -0.00279 0.28032 -0.00311 0.00003 -0.00002 6 0.21068 0.00329 -0.16927 0.00068 -0.00130 -0.00375 C:\at work\HORTON\6 BAYS\13GG3ORR.ani Page 12 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 13 *4GBA WITH RAFTER STIFFENER JOINT DISPLACEMENT (INCH RADIANS) STRUCTUR~ TYPE = SPACE JOINT LOAD X-TRANS Y-TRANS Z-TP~S X-ROTA~ Y-ROTAN Z-ROTAN 7 -0.00084 0.00245 ~0.34621 0.00520 -0.00004 0.00007 8 0.15758 0.00048 0.07599 -0.00174 -0.00095 -0.00283 9 -0.00105 -0.00015 -0.05672 0.00165 -0.00001 0.00004 40 5 -0.00031 -0.00322 0.23941 -0.00788 0.00003 -0.00005 6 0.23784 0.00383 -0.15497 0.00359 -0.00130 -0.00345 7 -0.00153 0.00286 -0.28384 0.01110 -0.00004 0.00010 8 0.17816 0.00057 0.05712 -0.00301 -0.00095 40.00262 9 -0.00137 -0.00016 -0.03953 0.00262 -0.00001 0.00004 41 5 -0.00003 -0.00279 0.28029 -0.00311 0.00000 0.00000 6 0.20992 0.00330 -0.16929 0.00068 -0.00129 -0.00374 7 -0.00017 0.00246 -0.34617 0.00520 0.00001 0.00001 8 0.15742 0.00048 0.07596 -0.00174 -0.00097 -0.00281 9 -0.00015 -0.00015 -0.05671 0.00165 0.00001 0.00000 42 5 -0.00002 -0.00323 0.23939 -0.00788 0.00000 0.00000 6 0.23710 0.00384 -0.15498 0.00359 -0.00129 "0.00346 7 -0.00022 0.00286 -0.28381 0.01110 0.00001 0.00001 8 0.17781 0.00058 0.05709 -0.00301 0.00097 -0.00259 9 -0.00019 -0.00016 -0.03953 0.00262 0.00001 0.00000 43 5 0.00053 0.00279 0.28032 -0.00311 -0.00003 0.00002 6 0.20956 0.00330 -0.16934 0.00069 -0.00126 -0.00376 7 0.00050 0.00245 -0.34621 0.00520 0.00006 -0.00005 8 0.15755 0.00049 0.07594 -0.00174 -0.00097 -0.00281 9 0.00076 -0.00015 -0.05671 0.00165 0.00002 -0.00003 44 5 0.00026 -0.00322 0.23941 -0.00788 -0.00003 0.00005 6 0.23701 0.00384 -0.15503 0.00359 -0.00127 -0.00350 7 0.00106 0.00286 -0.28383 0.01110 0.00006 -0.00009 8 0.17794 0.00058 0.05708 -0.00301 -0.00097 -0.00259 9 0.00098 -0.00016 -0.03953 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0.00882 -0.00009 0.00087 -0.00331 9 0.12562 -0.00048 -0.00450 0.00005 -0.00009 0.00004 c:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 13 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 14 *4GBA WITH P~AFTER STIFFENER JOINT DISPLACEMENT (INCH RADIALS) STRUCTURE TYPE = SPACE JOINT LOAD X-TRANS Y-TBANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 49 5 -0.00084 -0.00066 0.00427 -0.00001 -0.00054 0.00002 6 0.27565 0.00003 0.00812 -0.00004 ~0.00055 -0.00430 7 0.07107 0.00026 -0.01041 0.00007 0.00055 0.00035 8 0.20613 -0.00044 0.00919 -0.00004 -0.00080 -0.00321 9 0.05269 -0.00027 -0.00471 0.00004 0.00002 0.00028 50 5 0.00140 -0.00071 0.00459 0.00009 0.00064 -0.00025 6 0.21020 -0.00024 0.00873 -0.00017 -0.00148 -0.00395 7 0.00206 0.00027 -0.01126 0.00018 -0.00040 -0.00017 8 0.15866 -0.00067 0.00989 -0.00006 -0.00065 -0.00315 9 0.00256 -0.00029 -0.00510 0.00020 0.00016 -0.00031 51 5 0.00340 -0.00080 0.00522 -0.00001 0.00063 -0.00016 6 0.23944 40.00017 0.00680 -0.00031 -0.00148 -0.00383 7 0.00387 0.00032 -0.00915 0.00040 -0.00040 -0.00039 8 0.18205 -0.00068 0.00890 -0.00024 -0.00065 -0.00299 9 0.00536 -0.00031 -0.00306 0.00029 0.00016 -0.00041 52 5 0.00005 -0.00178 0.00003 -0.00001 -0.00018 0.00000 6 0.31431 0.00045 0.00098 0.00000 0.00563 0.00237 7 0.19106 0.00048 -0.00022 0.00000 -0.00015 0.00575 8 0.23577 -0.00091 0.00076 ~0.00001 0.00410 0.00178 9 0.14333 -0.00088 -0.00014 -0.00001 -0.00024 0.00431 53 5 0.00008 -0.01264 0.00004 -0.00002 0.00000 0.00000 6 0.36447 0.00472 0.00105 0.00000 0.00158 0.00168 7 0.10908 0.00483 -0.00023 0.00001 -0.00220 0.00595 8 0.27341 -0.00543 0.00082 -0.00001 0.00119 0.00126 9 0.08187 -0.00535 -0.00015 0.00001 ~0.00165 0.00446 54 5 0.00020 -0.00159 0.00006 ~0.00007 -0.00013 0.00000 6 0.41014 0.00047 0.00113 -0.00006 0.00130 0.00087 7 0.05419 0.00048 -0.00026 0.00014 0.00001 0.00535 8 0.30775 -0.00076 0.00089 -0.00010 0.00088 0.00065 9 0.04079 -0.00076 -0.00015 0.00005 -0.00008 0.00401 55 5 -0.00136 -0.00109 0.00293 ~0.00024 -0.00058 -0.00027 6 0.28572 0.00196 0.00187 0.00007 -0.00014 -0.00381 7 -0.01195 0.00109 -0.00260 0.00034 0.00006 0.00091 8 0.21330 0.00071 0.00355 -0.00012 -0.00053 -0.00305 9 -0.00995 0.00006 0.00020 0.00008 -0.00038 0.00049 56 5 0.00569 -0.00404 -0.00006 -0.00041 -0.00031 -0.00055 6 0.31456 0.00299 0.00275 0.00012 -0.00048 -0.00346 7 -0.01924 0.00418 0.00062 0.00036 -0.00023 0.00107 8 0.24004 -0.00067 0.00203 -0.00021 -0.00059 -0.00299 9 -0.01031 0.00022 0.00043 -0.00003 -0.00040 0.00041 57 5 0.00918 -0.00627 -0.00128 0.00009 0.00034 -0.00054 6 0.34336 0.00335 0.00282 -0.00010 -0.00125 -0.00348 7 -0.02046 0.00572 0.00151 -0.00013 -0.00078 0.00105 8 0.26416 -0.00204 0.00119 -0.00001 -0.00069 -0.00300 9 -0.00870 -0.00026 0.00020 -0.00003 -0.00034 0.00040 58 5 0.00151 -0.00109 0.00000 0.00011 0.00056 -0.00055 6 0.37937 0.00031 0.00197 -0.00014 -0.00103 -0.00332 7 -0.00941 0.00043 0.00023 -0.00025 -0.00082 0.00109 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 14 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 15 *4GBA WITH RAFTER STIFFENER JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE JOINT LOAD X-TRANS Y-TRAN$ Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 8 0.28562 -0.00054 0.00148 -0.00003 -0.00037 -0.00289 9 -0.00596 -0.00044 0.00017 -0.00011 -0.00021 0.00042 59 5 -0.00017 -0.00112 -0.00009 -0.00004 0.00016 -0.00077 6 0.39893 0.00035 0.00203 0.00004 0.00132 -0.00256 7 -0.00900 0.00035 0.00034 0.00006 -0.00021 0.00134 8 0.29907 -0.00053 0.00146 0.00000 0.00110 -0.00247 9 -0.00687 -0.00053 0.00019 0.00002 -0.00004 0.00045 60 5 0.00003 -0.00123 -0.00020 0.00003 0.00022 -0.00082 6 0.34140 0.00041 0.00194 -0.00001 0.00356 -0.00187 7 -0.01154 0.00043 0.00037 -0.00001 -0.00035 0.00136 8 0.25608 -0.00056 0.00132 0.00002 0.00283 -0.00199 9 -0.00863 -0.00055 0.00014 0.00001 -0.00010 0.00043 61 5 0.00001 -0.00149 -0.00034 -0.00013 0.00022 -0.00084 6 0.20986 0.00042 0.00139 -0.00002 0.00591 -0.00120 7 -0.00949 0.00043 0.00028 -0.00001 -0.00053 0.00133 8 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Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 6 0.20729 0.49145 0.13215 -0.01348 0.00588 -0.00109 7 -0.00669 0.57975 0.15484 -0.01612 -0.00037 0.00082 8 0.15548 -0.04823 -0.01210 0.00136 0.00453 -0.00127 9 -0.00501 0.01799 0.00492 -0.00062 -0.00016 0.00017 69 5 0.00028 -0.03222 0.13491 -0.01407 0.00003 -0.00009 6 0.27272 0.02032 -0.09721 0.00900 -0.00135 -0.00329 7 -0.00265 0.04037 -0.14775 0.01704 -0.00004 0.00015 8 0.20474 -0.00805 0.02481 -0.00344 -0.00099 -0.00253 9 -0.00179 0.00699 -0.01309 0.00260 -0.00001 0.00005 70 5 0.00078 -0.15156 0.00953 -0.01779 0.00003 -0.00009 6 0.30796 0.10638 -0.00745 0.01410 -0.00148 -0.00334 7 -0.00356 0.17506 -0.00589 0.01881 -0.00004 0.00016 8 0.23153 -0.02991 0.00134 -0.00231 0.00109 -0.00257 9 -0.00211 0.02160 0.00251 0,00122 -0.00001 0.00005 71 5 0.00098 -0,33707 -0.09337 -0.01740 0,00004 -0.00009 6 0.34304 0.25604 0.07526 0.01427 -0.00150 -0.00335 7 -0.00402 0.36905 0.10183 0.01799 -0.00005 0.00015 8 0.25799 -0.05205 -0.01116 -0.00190 -0.00109 -0.00257 9 -0.00230 0.03271 0.00876 0.00089 -0.00001 0.00005 72 5 0.00063 -0.59541 -0.15925 -0.01504 0.00005 -0.00008 6 0.37659 0.47294 0.13020 0.01285 -0.00088 -0.00318 7 -0.00382 0.63235 0.16909 0.01511 -0.00005 0.00015 8 0.28290 -0.07653 -0.01769 -0.00126 -0.00062 -0.00244 9 -0.00240 0.04303 0.01148 0.00044 0.00000 0.00005 73 5 -0.00004 -0.92997 -0.24823 -0.00584 0.00003 -0.00009 6 0.39531 0.77006 0.20843 0.00553 0.00132 -0.00258 7 -0.00432 0.96118 0.25668 0.00547 0.00002 0.00017 8 0.29645 -0.09610 -0.02349 -0.00008 0.00101 -0.00200 9 -0.00327 0.04723 0.01270 -0.00013 0.00004 0.00006 74 5 0.00003 -0.93016 -0.24812 0.00592 0.00002 -0.00009 6 0.33708 0.78627 0.21174 -0.00465 0.00360 -0.00197 7 -0.00642 0.94775 0.25299 -0.00638 -0.00004 0.00015 8 0.25283 0.08414 -0.02094 0.00080 0.00272 -0.00154 9 -0.00479 0.03698 0.01000 0.00050 -0.00001 0.00005 75 5 0.00001 -0.58187 -0.15517 0.01603 0.00003 0.00009 6 0.20577 0.49618 0.13336 -0.01362 0.00592 -0.00135 7 -0.00394 0.58714 0.15671 -0.01634 -0.00015 0.00012 8 0.15434 -0.04943 -0.01240 0.00140 0.00446 -0.00108 9 -0.00295 0.01879 0.00512 -0.00064 -0.00010 0.00003 76 5 -0.00001 -0.03223 0.13491 -0.01407 0.00000 0.00000 6 0.27219 0.02033 -0.09721 0.00900 -0.00135 -0.00333 7 -0.00031 0.04037 -0.14774 0.01704 0.00001 0.00001 8 0.20414 -0.00805 0.02480 0.00344 -0.00101 -0.00249 9 -0.00024 0.00699 -0.01309 0.00259 0.00001 0.00000 77 5 0.00000 -0.15154 0.00955 -0.01779 0.00000 0.00000 6 0.30769 0.10639 -0.00746 0.01410 -0.00148 -0.00337 7 -0.00042 0.17504 -0.00591 0.01881 0.00001 0.00001 8 0.23077 -0.02989 0.00135 -0.00231 -0.00111 -0.00253 C:lat work\HORTON\6 BAYS\13GG3ORR.anl Page 16 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 17 *4GBA WITH RAFTER STIFFENER JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE JOINT LOAD X-TRANS Y-TRAN$ Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 9 0.00032 0.02160 0.00251 0.00122 0.00001 0.00000 78 5 0.00001 -0.33704 -0.09334 -0.01739 0.00000 0.00000 6 0.34295 0.25605 0.07525 0.01427 -0.00149 -0.00338 7 -0.00056 0.36900 0.10180 0.01799 0.00001 0.00001 8 0.25722 -0.05202 -0.01115 -0.00190 -0.00112 -0.00254 9 -0.00041 0.03270 0.00875 0.00089 0.00001 0.00000 79 5 0.00003 -0.59536 -0.15923 ~0.01504 0.00000 0.00000 6 0.37645 0.47294 0.13019 0.01285 -0.00086 -0.00321 7 -0.00079 0.63228 0.16905 0.01511 0.00002 0.00001 8 0.28235 -0.07649 -0.01768 -0.00126 ~0.00065 -0.00241 9 -0.00057 0.04301 0.01147 0.00044 0.00001 0.00000 80 5 0.00003 -0.92991 -0.24820 -0.00584 0.00000 0.00000 6 0.39474 0.77006 0.20842 0.00553 0.00135 -0.00261 7 -0.00195 0.96109 0.25664 0.00547 0.00007 0.00002 8 0.29607 -0.09606 -0.02347 -0.00008 0.00101 -0.00196 9 -0.00144 0.04722 0.01269 0.00013 0.00005 0.00001 81 5 0.00003 -0.93011 -0.24810 0.00592 0.00000 0.00000 6 0.33587 0.78627 0.21173 -0.00465 0.00361 -0.00200 7 -0.00399 0.94768 0.25296 -0.00637 -0.00001 0.00000 8 0.25192 -0.08410 -0.02093 0.00080 0.00271 -0.00150 9 -0.00297 0.03696 0.00999 -0.00050 -0.00001 0.00000 82 5 0.00001 -0.58184 0.15516 0.01603 0.00000 0.00000 6 0.20528 0.49618 0.13335 -0.01362 0.00591 -0.00139 7 -0.00119 0.58710 0.15670 -0.01634 -0.00008 -0.00002 8 0.15397 -0.04941 -0.01240 0.00140 0.00443 -0.00104 9 -0.00089 0.01878 0.00511 -0.00064 -0.00006 -0.00002 83 5 -0.00030 -0.03222 0.13491 -0.01407 -0.00003 0.00009 6 0.27259 0.02033 -0.09723 0.00900 -0.00132 -0.00340 7 0.00198 0.04037 -0.14775 0.01704 0.00005 -0.00013 8 0.20422 -0.00804 0.02480 -0.00344 -0.00101 -0.00249 9 0.00127 0.00699 -0.01309 0.00260 0.00002 -0.00004 84 5 -0.00077 -0.15156 0.00953 -0.01779 -0.00003 0.00009 6 0.30846 0.10642 -0.00745 0.01410 -0.00145 -0.00345 7 0.00266 0.17506 -0.00589 0.01881 0.00005 -0.00014 8 0.23079 -0.02988 0.00134 -0.00231 0.00111 -0.00252 9 0.00144 0.02160 0.00251 0.00122 0.00002 -0.00004 85 5 -0.00095 -0.33707 -0.09337 -0.01740 -0.00004 0.00008 6 0.34383 0.25610 0.07528 0.01427 -0.00146 -0.00345 7 0.00286 0.36904 0.10182 0.01799 0.00007 -0.00013 8 0.25719 -0.05201 -0.01115 -0.00190 -0.00112 -0.00253 9 0.00146 0.03270 0.00876 0.00089 0.00002 -0.00004 86 5 -0.00058 -0.59541 -0.15925 -0.01504 0.00005 0.00008 6 0.37706 0.47302 0.13022 0.01285 -0.00083 0.00328 7 0.00224 0.63234 0.16909 0.01511 0.00008 -0.00013 8 0.28238 -0.07647 -0.01767 -0.00126 -0.00066 -0.00240 9 0.00126 0.04302 0.01147 0.00044 0.00002 -0.00004 87 5 0.00010 -0.92997 -0.24823 -0.00584 -0.00003 0.00009 6 0.39501 0.77015 0.20845 0.00553 0.00139 -0.00268 C: \at work\HORTON\6 BAYS\i3GG3ORR.ani Page 17 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 18 *4GBA WITH P, AETER STIFFENER JOINT DISPLACEMENT (INCH P. ADIAlqS) STRUCTI/RE TYPE = SPACE JOINT LOAD X-TRANS Y-TRANS Z-TPJ~NS X-ROTA~ Y-ROTAN Z-ROTAN 7 0.00048 0.96117 0.25668 0.00547 0.00012 -0.00012 8 0.29633 -0.09604 -0.02347 -0.00008 0.00102 -0.00194 9 0.00043 0.04723 0.01270 -0.00013 0.00006 -0.00003 88 5 0.00004 -0.93016 -0.24812 0.00592 -0.00002 0.00009 6 0.33525 0.78634 0.21176 -0.00465 0.00362 -0.00208 7 -0.00167 0.94774 0.25299 -0.00638 0.00001 -0.00015 8 0.25147 -0.08408 -0.02093 0.00080 0.00270 -0.00149 9 -0.00123 0.03697 0.01000 -0.00050 -0.00001 -0.00005 89 5 0.00001 -0.58187 -0.15517 0.01603 -0.00002 0.00009 6 0.20583 0.49622 0.13337 -0.01362 0.00591 -0.00147 7 0.00162 0.58713 0.15671 -0.01634 0.00002 -0.00015 8 0.15438 -0.04940 -0.01239 0.00140 0.00441 -0.00104 9 0.00122 0.01879 0.00511 -0.00064 -0.00003 -0.00005 90 5 0.00080 -0.03104 0.13167 -0.01367 0.00021 0.00030 6 0.27320 0.01944 -0.09475 0.00869 -0.00147 -0.00361 7 0.00349 0.03904 -0.14406 0.01659 -0.00018 -0.00046 8 0.20548 -0.00785 0.02431 -0.00338 -0.00095 -0.00249 9 0.00320 0.00685 -0.01267 0.00254 0.00002 -0.00013 91 5 -0.00374 -0.14749 0.00934 -0.01746 -0.00004 0.00056 6 0.31228 0.10331 -0.00731 0.01385 -0.00139 -0.00386 7 0.00901 0.17046 -0.00566 0.01844 0.00013 -0.00075 8 0.23151 -0.02926 0.00131 -0.00226 -0.00108 -0.00248 9 0.00405 0.02109 0.00254 0.00118 0.00007 -0.00015 92 5 -0.00535 -0.32987 -0.09179 -0.01713 ~0.00028 0.00051 6 0.34853 0.25056 0.07404 0.01407 -0.00122 -0.00382 7 0.01060 0.36089 0.10005 0.01769 0.00040 -0.00068 8 0.25753 -0.05095 -0.01094 -0.00186 -0.00112 -0.00250 9 0.00408 0.03180 0.00857 0.00086 0.00010 -0.00014 93 5 -0.00117 -0.58480 -0.15676 -0.01487 -0.00036 0.00051 6 0.37842 0.46483 0.12828 0.01272 -0.00057 -0.00368 7 0.00524 0.62034 0.16628 0.01492 0.00045 -0.00069 8 0.28296 -0.07493 -0.01733 -0.00123 -0.00069 -0.00238 9 0.00308 0.04170 0.01117 0.00042 0.00008 -0.00015 94 5 0.00018 -0.91673 -0.24495 -0.00583 -0.00014 0.00059 6 0.39618 0.75989 0.20589 0.00552 0.00152 -0.00312 7 0.00296 0.94621 0.25298 0.00546 0.00027 -0.00076 8 0.29726 -0.09415 -0.02302 -0.00008 0.00103 -0.00191 9 0.00235 0.04560 0.01230 -0.00013 0.00010 -0.00015 95 5 0.00003 -0.91872 -0.24523 0.00580 -0.00016 0,00060 6 0.33518 0.77745 0.20950 -0.00456 0.00373 -0.00254 7 0.00050 0.93483 0.24974 -0.00624 0.00017 -0.00081 8 0.25141 -0.08247 -0.02053 0.00078 0.00268 -0.00147 9 0.00040 0.03557 0.00965 -0.00048 0.00001 -0.00017 96 5 0.00001 -0.57534 -0.15351 0.01584 -0.00016 0.00061 6 0.20747 0.49114 0.13207 -0.01347 0.00601 -0.00193 7 0.00456 0.57978 0.15485 -0.01612 0.00018 -0.00081 8 0.15561 -0.04848 -0.01217 0.00137 0.00439 -0.00101 9 0.00343 0.01800 0.00492 0.00062 0.00002 -0.00017 c:\at work\HORTON\6 BAYS\I3GG3ORR.anl Page 18 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT 13GG -- PAGE NO. 19 *4GBA WITH P~AFTER STIFFENER JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 97 5 0.00140 -0.00136 0.00358 -0.00035 0.00060 0.00025 6 0.27954 -0.00090 0,00360 -0.00029 -0.00146 -0.00384 7 0.01039 0.00173 -0.00412 0.00060 -0.00030 -0.00070 8 0.21067 -0.00163 0.00532 -0.00047 -0.00066 -0.00270 9 0.00880 0.00035 -0.00047 0.00020 0.00021 -0.00034 98 5 -0.00559 -0.00495 -0.00011 -0.00047 0.00033 0.00051 6 0.31887 -0.00238 0.00177 -0.00012 -0.00138 -0.00378 7 0.01728 0.00623 0.00064 0.00047 -0.00002 -0.00069 8 0.23511 -0.00536 0.00125 -0.00044 -0.00080 -0.00247 9 0.00891 0.00110 0.00040 0.00001 0.00023 -0.00015 99 5 -0.00904 -0.00731 -0.00142 0.00012 -0.00032 0.00049 6 0.35373 -0.00225 0.00155 0.00010 -0.00111 -0.00359 7 0.01820 0.00784 0.00161 ~0.00021 0.00054 -0.00045 8 0.25875 -0.00699 0.00013 0.00017 -0.00106 -0.00234 9 0.00711 0.00058 0.00018 -0.00007 0.00018 0.00002 100 5 -0.00146 -0.00108 0.00010 0.00019 -0.00054 0.00048 6 0.38022 0.00010 0.00177 0.00008 -0.00054 -0.00318 7 0.00785 0.00047 -0.00014 -0.00035 0.00056 -0.00018 8 0.28411 -0.00069 0.00140 0.00019 -0.00080 -0.00204 9 0.00483 -0.00041 -0.00003 -0.00013 0.00003 0.00021 101 5 0.00022 0.00170 -0.00017 -0.00030 -0.00013 0.00064 6 0.39834 0.00052 0.00116 0.00007 0.00130 -0.00219 7 0.00560 0.00052 0.00013 0.00019 0.00002 0.00021 8 0.29892 -0.00080 0.00075 -0.00016 0.00088 -0.00118 9 0.00436 -0.00080 -0.00002 -0.00008 -0.00008 0.00062 102 5 0.00004 -0.01277 -0.00315 0.00003 -0.00015 0.00064 6 0.33556 0.00479 0.00160 0.00000 0.00315 -0.00117 7 0.00246 0.00490 0.00136 -0.00002 -0.00046 0.00064 8 0.25169 0.00548 -0,00104 0.00003 0.00225 -0.00042 9 0.00187 -0.00539 -0.00121 0.00001 -0.00046 0.00095 103 5 0.00001 -0.00212 -0.00044 0.00015 -0.00018 0.00066 6 0.21028 0.00059 0.00005 -0.00012 0.00563 -0.00053 7 0.00770 0.00062 0.00023 -0.00012 -0.00017 0.00069 8 0.15772 -0.00105 0.00027 0.00001 0.00410 0.00008 9 0.00579 -0.00102 0.00013 0.00001 -0.00025 0.00099 ************** END OF I~TEST ANALYSIS RESULT ************** 175. PRINT SECTION MAX DISPL NSECT 12 ALL C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 19 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 20 *4GBA WITH RAFTER STIFFENER M~ MEMBER SECTION DISPLACEMENTS UNIT= INCH FOR FPS AND CM FOR METRIC/SI SYSTEM MEMBER MA~ DISP LOCATION LOA/) L/DISPL 1 0.00002 27.27 8 0 2 0.02739 27.27 6 1706 3 0.02360 27.27 6 1980 4 0.01980 27.27 6 2361 5 0.01656 27.27 6 2822 6 0.00289 27.27 9 16173 7 0.00028 4.43 7 27359 8 0,00065 4.89 5 14970 9 0.00003 17.22 8 0 10 0.02498 17.22 6 1379 11 0.01948 17.22 6 1768 12 0.01397 17.22 6 2465 13 0.00899 14.35 6 3831 14 0.00020 3.42 6 40123 15 0.00163 6.83 6 10075 16 0.00549 10.25 6 4481 17 0.00003 13.67 5 0 18 0.10980 27.27 7 425 19 0.00545 3.80 7 1393 20 0.00741 4.89 5 1320 21 0.11272 27.27 7 414 22 0.00561 3.80 7 1354 23 0.00757 4.89 5 1292 24 0.11270 27.27 7 414 25 0.00561 3.80 7 1354 26 0.00757 4.89 5 1293 27 0.11271 27.27 7 414 28 0.00561 3.80 7 1354 29 0.00757 4.89 5 1292 30 0.10983 27.27 7 425 31 0.00545 3.80 7 1393 32 0.00741 4.89 5 1320 33 0,00002 27.27 8 0 34 0.03592 27.27 7 1301 35 0.03003 27.27 7 1556 36 0.01561 27.27 7 2994 37 0.00585 27.27 6 7995 39 0.00029 3.80 7 25763 41 0.00063 4.89 5 15617 43 0.00002 17.22 6 0 44 0.03153 17.22 7 1092 45 0.02279 17.22 7 1511 46 0.00849 14.35 7 4056 47 0.00024 3.42 7 33594 48 0.00101 6.83 7 16200 49 0.00656 10.25 6 3752 50 0.00002 13.67 6 0 51 0.00101 15.38 5 30471 52 0.00101 15.38 5 30471 c:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 20 of 89 SYSTEM 4E CLT-13GG *4GBA WITH P~TER STIFFENER 53 0.00101 15.38 54 0.00101 15.38 55 0.00187 17.94 56 0.00101 15.38 57 0.00101 15.38 58 0.00101 15.38 59 0.00101 15.38 60 0.00099 15.31 61 0.00046 15.31 62 0.00046 15.31 63 0.00046 15.31 64 0.00046 15.31 65 0.00099 15.31 66 0.00046 15~31 67 0.00046 15.31 68 0.00046 15.31 69 0.00046 15.31 70 0.00099 15.31 71 0.00046 15.31 72 0.00046 15,31 73 0.00046 15.31 74 0.00046 15.31 75 0.00099 15.31 76 0.00046 15.31 77 0.00046 15.31 78 0.00046 15.31 79 0.00046 15.31 80 0.00099 15.31 81 0.00046 15.31 82 0.00046 15.31 83 0.00046 15.31 84 0.00046 15.31 85 0.00099 15.31 86 0.00046 15.31 87 0.00046 15.31 88 0.00046 15.31 89 0.00046 15.31 90 0.00101 15.38 91 0.00101 15.38 92 0.00187 17.94 93 0.00101 15.38 94 0.00289 12.81 95 0.00253 17.94 96 0.00101 15.38 97 0.00025 3.49 98 0.00117 5.97 99 0.00075 12.14 100 0.00985 15.91 101 0.00932 15.91 102 0.00972 15.91 103 0.00725 13.26 104 0.00033 6.11 106 0.00136 5.97 108 0.00132 8.09 110 0.00820 18.56 112 0.00823 13.26 5 30471 5 30471 9 19188 5 30471 5 30471 5 30471 5 30471 9 30845 9 67279 9 87279 9 67279 9 67279 9 30845 9 67279 9 67279 9 67279 9 67279 9 30845 9 67279 9 67279 9 67279 9 67279 9 30845 9 67279 9 67279 9 67279 9 67279 9 30845 9 67279 9 67279 9 67279 9 67279 9 30845 9 67279 9 67279 9 67279 9 67279 5 30471 5 30471 9 19188 5 30471 7 10651 7 12170 5 30471 5 42132 5 10234 6 21612 6 3230 6 3414 6 3274 6 4387 7 31390 7 8750 6 12258 6 3882 6 3866 Wednesday, January 28, 2009, 02:23 PM PAGE NO. 21 c:\a5 work\HORTON\6 BAYS\I3GG3ORR.ani Page 21 of 89 SYSTEM 4E CLTwl3GG *4GBA WITH R3tFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 22 114 0.01022 15.91 6 3114 116 0.00792 13.26 6 4016 118 0.00676 5.24 6 1549 119 0.00120 6.96 7 9914 120 0.00560 8.09 7 2890 121 0.03764 15.91 7 845 122 0.04657 15.91 5 683 123 0.04023 15.91 5 790 124 0.01760 13.26 5 1808 125 0.00669 5.24 6 1566 126 0.00124 6.96 7 9648 127 0.00582 8.09 7 2779 128 0.03836 15.91 7 829 129 0.04712 15.91 7 675 130 0.04055 15.91 5 784 131 0.01770 13.26 5 1798 132 0.00669 5.24 6 1566 133 0.00124 6.96 7 9654 134 0.00582 8.09 7 2780 135 0.03835 15.91 7 829 136 0.04711 15.91 7 675 137 0.04055 15.91 5 784 138 0.01770 13.26 5 1798 139 0.00669 5.24 6 1566 140 0.00124 6.96 7 9648 141 0.00582 8.09 7 2779 142 0.03835 15.91 7 829 143 0.04712 15.91 7 675 144 0.04055 15.91 5 784 145 0.01770 13.26 5 1798 146 0.00676 5.24 6 1550 147 0.00121 6.96 7 9888 148 0.00560 8.09 7 2888 149 0.03763 15.91 7 845 150 0.04657 15.91 5 683 151 0.04024 15.91 5 790 152 0.01760 13.26 5 1808 ************ END OF SECT DISPL RESULTS *********** 176. *SECTION 0.5 ALL 177. PRINT MEMBER FORCES ALL C:\a~ work\HORTON\6 BAYS\13GG3ORR.anl Page 22 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 23 *4GSA WITH RAFTER STIPFENER ~-44BER END FORCES STRUCT~ TYPE = SPACE ALLONITSAP, E -- POUN INCH (LOC;iL) ~.MBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MO~4-Z 4 5 1 4 . 68 0 . 00 0.02 -0 . 01 0 . 00 0 . 00 7 4.68 0.00 -0.02 0.01 -1.05 0.00 7 2.81 0.02 -0.02 0.16 -1.06 -0.79 7 1 2.81 0.01 -0.01 -0.05 0.00 0.00 7 2.81 -0.01 0.01 0.05 0.60 0.38 7 4.68 0.01 -0.03 0.13 -1.56 -0.59 9 1 4.68 0.01 0.01 -0.04 0.00 0.00 7 4.68 -0.01 -0.01 0.04 -0.32 0.28 5 2 319.03 0.00 -0.10 -0.03 0.00 0.00 28 -309.66 0.00 0.10 0.03 4.67 -0.06 6 2 -63.20 206.72 -0.11 -0.53 0.00 0.00 28 68.82 -206.72 0.11 0.53 4.98 9664.27 7 2 -64.13 -192.22 0.32 -0.08 0.00 0.00 28 69.75 192.22 -0.32 0.08 -15.09 -8986.43 8 2 173.01 155.04 -0.15 -0.43 0.00 0.00 28 -163.64 -155.04 0.15 0.43 7.13 7248.16 9 2 172.31 -144.17 0.17 -0.08 0.00 0.00 28 -162.94 144.17 -0.17 0.08 -7.92 -6739.87 5 3 286.77 0.00 -0.26 -0.04 0.00 0.00 29 -277.40 0.00 0.26 0.04 12.11 -0.06 6 3 -70.25 178.08 -0.22 -0.58 0.00 0.00 29 75.87 -178.08 0.22 0.58 10.42 8325.29 7 3 -73.37 -165.57 0.69 0.14 0.00 0.00 29 78.99 165.57 -0.69 -0.14 -32.06 -7740.58 8 3 144.77 133.56 -0.36 0.46 0.00 0.00 29 -135.40 -133.56 0.36 0.46 16.63 6243.92 9 3 142.43 -124.18 0.33 0.08 0.00 0.00 29 -133.06 124.18 -0.33 -0.08 -15.23 -5805.48 5 4 279.47 -0.01 -0.39 0.04 0.00 0.00 30 -270.11 0.01 0.39 0.04 18.19 -0.24 6 4 -65.34 149.36 -0.34 -0.29 0.00 0.00 30 70.96 -149.36 0.34 0.29 16.11 6982.76 7 4 -65.31 -138.86 1.06 0.17 0.00 0.00 30 70.93 138.86 -1.06 -0.17 -49.46 -6491.53 8 4 144.74 112.02 -0.54 -0.25 0.00 0.00 30 -135.37 -112.02 0.54 0.25 25.31 5236.90 9 4 144.75 -104.15 0.51 0.10 0.00 0.00 30 -135.39 104.15 0.51 -0.10 -23.87 -4868.82 5 5 295.18 0.00 -0,22 -0.04 0.00 0.00 31 -285.81 0.00 0.22 0.04 10.15 0.10 C:\at work\HORTON\6 BAYS\I3GG3ORR.ani Page 23 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 24 *4GEA WITH P, AFTER STIFFENER ~4BER E~D FORCES STRUCTL~ TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT AXI;tL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 6 5 -66.21 124.95 -0.51 -0.08 0.00 0.00 31 71.83 -124.95 0.51 0.08 24.05 5841.32 7 5 -98.32 -116.18 1.03 0.23 0.00 0.00 31 103.94 116.18 -1.03 -0.23 -47.98 -5431.47 8 5 156.36 93.71 -0.54 -0.09 0.00 0.00 31 -146.99 -93.71 0.54 0.09 25.41 4381.06 9 5 132.27 -87.13 0.61 0.14 0.00 0.00 31 -122.90 87.13 -0.61 -0.14 -28.61 -4073.53 5 6 176.60 1.54 -1.13 -0.39 0.80 0.00 32 -171.65 -1.54 1.13 0.39 52.77 72.18 6 6 -374.16 -1.28 -0.46 0.21 0.00 0.00 32 377.13 1.28 0.46 -0.21 21.31 -59.75 7 6 -86.10 0.59 -0.89 0.67 0.00 0.00 32 89.07 -0.59 0.89 -0.67 41.79 27.51 8 6 -159.45 0.17 -1.16 -0.12 0.00 0.00 32 164.39 -0.17 1.16 0.12 54.20 8.06 9 6 56.60 1.57 1.49 0.22 0.00 0.00 32 -51.65 -1.57 1.49 -0.22 69.57 73.50 5 32 140.46 -45.93 29.77 -1.62 -64.53 -106.43 33 -139.66 45.93 -29.77 1.62 -161.61 -242.48 6 32 -245.23 20.15 -21.83 1.03 0.10 76.10 33 245.71 -20.15 21.83 -1.03 165.75 76.96 7 32 -96.54 32.14 -24.75 2.39 -36.65 -2.71 33 97.02 -32.14 24.75 -2.39 224.63 246.85 8 32 -83.89 -18.26 5.18 -0.40 -46.63 -20.75 33 84.69 18.26 -5.18 0.40 7.28 -117.96 9 32 27.63 -9.27 3.00 0.62 -74.20 -79.86 33 ~26.83 9.27 -3.00 -0.62 51.45 9.45 5 33 130.99 -8.47 0,74 -46.95 150.98 242.44 55 -129.99 8.74 -0.74 46.95 -158.21 -326.63 6 33 -199.34 5.48 -8.69 43.83 -142.43 -76.93 55 199.94 -5.32 8.69 -43.83 227.42 129.78 7 33 -85.90 -7.10 15.24 67.81 -222.81 -246.78 55 86.50 7.26 -15.24 -67.81 73.66 176.51 8 33 -55.60 -2.40 -5.98 -1.11 2.49 117,95 55 56.60 2.67 5.98 1.11 55.99 -142.72 9 33 29.48 -11.83 11.97 16.88 57,79 -9.43 55 -28.48 12.10 -11.97 -16.88 -59.34 -107.67 5 7 3.45 0.00 -0.11 -0.04 0.19 0.00 8 3.45 0.00 0.11 0.04 3.44 0.01 6 7 2.07 -0.01 0.04 0.22 -1.46 -0.86 8 2.07 0.01 -0.04 -0.22 -0.08 0.50 7 7 2 .07 -0 .02 0.05 -0.74 -0.04 0.21 8 2.07 0.02 -0.05 0.74 -1.82 -0.97 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 24 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 25 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 8 7 3.45 -0.01 -0.04 0.13 -0.94 -0.64 8 3.45 0.01 0.04 -0.13 2.46 0.39 9 7 3.45 -0.02 -0.04 -0.59 0.12 0.16 8 3.45 0.02 0.04 0.59 1.16 -0.72 5 28 281.70 0.00 0.05 -0.10 -4.46 0.05 34 -274.80 0.00 -0.05 0.10 2.83 -0.08 6 28 -85.93 -77.57 0.63 -0.81 -6.81 -9663.14 34 90.07 77.57 -0.63 0.81 -14,93 6991.07 7 28 -87.43 72.13 -0.76 -0.46 15,62 8985.50 34 91.57 -72.13 0.76 0.46 10.72 -6500.61 8 28 135.61 -58.17 0.51 -0.68 -8.35 -7247.31 34 -128.70 58.17 -0.51 0.68 -9.17 5243.24 9 28 134.48 54.10 -0.54 -0.42 8.48 6739.16 34 -127.58 -54.10 0.54 0.42 10.06 -4875.51 5 29 248.24 0.00 0.57 -0.11 -11.89 0.06 35 -241.33 0.00 -0.57 0.11 -7.83 -0.12 6 29 -92.85 -106.29 1.18 -1.56 -12.81 -8325.12 35 96.99 106.29 -1.18 1.56 -27.90 4663.38 7 29 -96.47 98.84 -1.64 0.63 31.48 7740.72 35 100.61 -98.84 1.64 -0.63 24.98 -4335.63 8 29 106.61 -79.72 1.31 -1.25 -18.29 -6243.79 35 -99.71 79.72 -1.31 1.25 -26.77 3497.45 9 29 103.90 74.13 -0.81 0.40 14.93 5805.59 35 -96.99 -74.13 0.81 -0.40 12.89 -3251.81 5 30 241.09 0.00 1.03 -0.11 -20.41 0.24 36 -234.19 0.00 -1.03 0.11 -15.20 -0.36 6 30 -88.22 -135.01 1.58 -0.87 -18.01 -6982.38 36 92.36 135.01 -1.58 0.87 -36.41 2331.31 7 30 -88.58 125.56 -2.84 0.69 52.18 6491.57 36 92.72 -125.56 2.84 -0.69 45.55 -2166.10 8 30 106.48 -101.26 1.94 -0.73 28.37 -5236.61 36 -99.57 101.26 -1.94 0.73 -38.47 1748.22 9 30 106.20 94.17 -1.37 0,44 24.27 4868.85 36 -99.30 -94.17 1.37 -0.44 23.01 -1624.83 5 31 253.33 0.00 1.14 -0.14 -39.24 0.03 58 -246.42 0.00 -1.14 0.14 0.00 0.00 6 31 -87.37 -169.57 0.05 -0.40 -1.63 -5841.37 58 91.51 169.57 -0.05 0.40 0.00 0.00 7 31 -118.12 157.67 -2.10 0.84 72.41 5431.65 58 122.27 -157.67 2.10 -0.84 0.00 0.00 8 31 117.16 -127.17 0.86 -0.40 -29.75 -4381.00 58 -110.25 127.17 -0.86 0.40 0.00 0.00 9 31 94.09 118.25 -0.75 0.53 25.78 4073.76 58 -87.19 -118.25 0.75 -0.53 0.00 0.00 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 25 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG PAGE NO. 26 *4GBA WI~ RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ;iRE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 18 5 5 36 218.12 0.02 -1.79 -0.17 14.67 0.17 59 -216.48 -0.02 1.79 0.17 0.00 0.00 6 36 -101.50 -284.29 -5.39 -1.14 44.16 -2331.19 59 102.49 284.29 5.39 1.14 0.00 0.00 7 36 -101.12 264.28 4.72 1.11 -38.73 2167.10 59 102.10 -264.28 -4.72 -1.11 0.00 0.00 8 36 83.80 -213.20 -5.36 -0.98 43.93 -1748.27 59 -82.16 213.20 5.36 0.98 0.00 0.00 9 36 84.09 198.23 2.22 0.71 -18.24 1625.45 59 -82.45 -198.23 -2.22 -0.71 0.00 0.00 5 35 222.49 0.01 -0.16 -0.20 2.61 0.18 60 -219.20 -0.01 0.16 0.20 0.00 0.00 6 35 -107.74 -284.32 -1.98 -2.26 32.48 -4662.78 60 109.71 284.32 1.98 2.26 0.00 0.00 7 35 -110.42 264.34 1.25 1.40 -20.57 4335.10 60 112.39 -264.34 -1.25 -1.40 0.00 0.00 8 35 81.25 -213.23 -1.61 -1.84 26.37 -3496.95 60 -77.97 213.23 1.61 1.84 0.00 0.00 9 35 79.24 198.26 0.82 0.91 -13.41 3251.46 60 -75.96 -198.26 -0.82 -0.91 0.00 0.00 5 34 255.05 0.01 -0.04 -0.17 0.92 0.13 61 -250.12 -0.01 0.04 0.17 0.00 0.00 6 34 -102.59 -284.26 -0.75 -0.84 18.86 -6992.88 61 105.55 284.26 0.75 0.84 0.00 0.00 7 34 -103.95 264.32 0.34 -0.53 -8.27 6502.37 61 106.91 -264.32 -0.34 0.53 0.00 0.00 8 34 108.74 -213.19 -0.60 -0.75 14.80 -5244.56 61 -103.81 213.19 0.60 0.75 0.00 0.00 9 34 107.71 198.25 0.22 -0.52 -5.32 4876.87 61 102.78 -198.25 -0.22 0.52 0.00 0.00 5 8 3.29 0.00 -0.11 -0.09 3.51 0.01 9 3.29 0.00 0.11 0.09 0.00 0.00 6 8 1 . 97 0 · 02 -0 · 02 0 . 71 0 . 63 0 . 77 9 1.97 -0.02 0.02 -0.71 0~00 0.00 7 8 1.97 -0.03 0.06 -1.21 -1.88 -1.06 8 8 3.29 0.02 -0.09 0.47 3.04 0.58 9 3.29 -0.02 0.09 -0.47 0.00 0.00 9 3.29 0.02 0.04 0.98 0.00 0.00 10 593.50 -94.22 -0.75 -0.47 0.00 0.00 37 -588.55 94.22 0.75 0.47 35.19 -4404.65 c:\at work\HORTON\6 BAYS\I3GG3ORR.ani Page 26 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 27 MEMBER END FORCES STRUCTUP. E TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL ) MEMBER LOAD JT AXIAL SHEA~-¥ SEEAR-Z TORSION MOM-Y MOM-Z 2O 22 6 10 -716.75 43.81 -2.90 0.44 0.00 0.00 37 719.72 -43.81 2.90 -0.44 135.72 2048.22 7 10 -508.21 131.12 0.47 0.63 0.00 0.00 37 511.18 -131.12 -0.47 -0.63 -21.77 6129.89 8 10 -115.35 -35.33 -2.72 0.00 0.00 0.00 37 120.30 35,33 2.72 0.00 127.28 -1651.75 9 10 41.05 30.15 -0.20 0.14 0.00 0.00 37 -36.11 -30.15 0.20 ~0.14 9.16 1409.50 5 37 570.51 -94.30 26.88 -1.82 -52.62 4406.29 38 -569.71 94.30 -26.88 1.82 -151.54 -5122.60 6 37 -739.33 220.10 -8.97 1.67 -126.05 -2048.65 38 739.81 -220.10 8.97 -1.67 194.17 3720.53 7 37 -518.96 -58.30 -30.40 2.35 45.65 -6132.45 38 519.44 58.30 30.40 -2.35 185.26 5689.59 8 37 -144.64 96.82 12.73 -0.06 -132.62 1652.62 38 145.45 -96.82 -12.73 0.06 35.90 -917.15 9 37 20.63 -111.98 -3.34 0.44 -3.85 -1410.23 38 -19.83 111.98 3.34 -0.44 29.22 559.65 5 38 577.65 58.42 0.44 -45.53 133.75 5122.65 62 -576.65 -58.15 -0.44 45.53 -138.06 -4552.43 6 38 -796.35 107.10 10.44 59.56 -189.07 -3720.60 62 796.95 -106.93 -10.44 -59.56 86.95 4767.64 7 38 -483.53 -217.68 0.10 52.90 -155.66 -5689.60 62 484.12 217.84 -0.10 -52.90 154.71 3559.04 8 38 -181.01 122.10 8.15 11.71 -44.97 917.13 62 182.01 -121.83 -8.15 -11.71 -34.77 276.19 9 38 53.61 -121.48 0.39 6.71 -19.91 -559.62 62 -52.61 121.75 -0.39 -6.71 16.05 -630.26 5 12 645.82 -97.27 0.16 -0.06 0.00 0.00 39 -640.87 97.27 -0.16 0.06 -7.70 -4547.52 6 12 -757.50 45.99 -3.93 0.25 0.00 0.00 39 760.46 -45.99 3.93 -0.25 183.55 2149.83 7 12 -565.16 134.60 -0.26 0.08 0.00 0.00 39 568.12 -134.60 0.26 -0.08 12.31 6292.62 8 12 108.03 -35.91 -2.83 0.15 0.00 0.00 39 112.98 35.91 2.83 -0.15 132.09 -1678.99 9 12 36.22 30.55 -0.08 0.02 0.00 0.00 39 -31.27 -30.55 0.08 -0.02 3.66 1428.11 5 39 620.98 -97.28 -1.83 -0.18 21.28 4547.73 40 -620.17 97.28 1.83 0.18 -7.38 -5286.65 6 39 -773.64 222.22 11.56 0.77 -193.61 -2149.98 40 774.12 -222.22 -11.56 -0.77 105.78 3838.00 7 39 -577.47 -54.92 2.28 0.24 -26.62 -6292.85 40 577.96 54.92 ~2.28 -0.24 9.31 5875.68 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 27 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 28 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 23 24 25 26 B 39 -133.84 96.26 7.35 0.44 -129.80 1679.02 40 134.64 -96.26 -7.35 -0.44 73.99 -947.82 9 39 13.28 -111.60 0.38 0.05 -4.55 -1428.13 40 -12.48 111.60 -0.38 -0.05 1.64 580.44 5 48 615.46 69.12 -0.59 -1.58 18.89 5286.66 69 -614.46 -68.85 0.59 1.58 -13.12 -4611.72 6 40 -821.63 99.29 11.75 29.37 -111.78 -3838.07 69 822.23 -99.13 -11.75 -29.37 -3.19 4808.76 7 40 -527.42 -229.74 0.59 1.58 -21.18 -5875.62 69 528.01 229.91 -0.59 -1.58 15.42 3627.02 8 40 -172.59 124.00 8.39 20.89 -70.16 947.77 69 173.59 -123.73 -8.39 -20.89 -11.89 264.10 9 40 48.07 -122.78 0.01 0.04 -2.21 4580.39 69 -47.07 123.05 -0.01 -0.04 2.06 -622.21 5 14 647.11 -97.26 0.01 0.00 0.00 0.00 41 -642.16 97.26 -0.01 0.00 -0.29 -4547.03 6 14 -759.57 45.99 -3.88 0.23 0.00 0.00 41 762.54 -45.99 3.88 -0.23 181.48 2150.18 7 14 -566.09 134.58 -0.02 0.00 0.00 0.00 41 569.06 -134.58 0.02 0.00 0.75 6291.83 8 14 -108.65 -35.90 -2.91 0.17 0.00 0.00 41 113.60 35.90 2.91 -0.17 135.90 -1678.36 9 14 36.45 30.54 -0.01 0.00 0.00 0.00 41 -31.51 -30.54 0.01 0.00 0.35 1427.87 5 41 621.84 -97.26 -0,03 0.00 0.30 4547.08 42 -621.04 97.26 0.03 0.00 -0.10 -5285.85 6 41 774.12 222.23 10.38 0.68 -181.33 -2150.25 42 774.60 -222.23 -10.38 -0.68 102.45 3838.29 7 41 -578.49 -54.95 0.12 0.00 0.69 -6291.87 42 578.97 54.95 -0.12 0.00 -0.23 5874.48 8 41 -133.58 96.28 7.77 0.51 135.79 1678.36 42 134.38 -96.28 -7.77 -0.51 76.77 -947.02 9 41 13.15 -111.60 0.07 0.00 -0.30 -1427.86 42 -12.34 111.60 -0.07 0.00 -0.25 580.12 5 42 617.91 69.14 -0.01 -0.02 0.11 5285.86 76 -616.91 -68.86 0.01 0.02 -0.03 -4610.77 6 42 -822.81 99.16 11.27 28.37 -99.04 -3838.36 76 823.41 -99.00 -11.27 -28.37 -11.24 4807.77 7 42 -530.39 -229.70 0,03 -0.09 0.18 -5874.42 76 530.99 229.87 -0.03 0.09 -0.51 3626.21 8 42 -171.70 123.91 8.45 21.26 -74.20 946.98 76 172.70 -123.64 -8.45 -21.26 -8.45 264.04 9 42 47.61 -122.74 0.02 -0.09 0.21 -580.07 76 -46.61 123.01 -0.02 0.09 -0.40 -622.13 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 28 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 29 *4GBA WITH RAFTER STIFFENER M~MBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS AP, E -- POUN INCH (LOCAL) M~MBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 27 28 29 30 31 5 5 16 645.81 -97.27 -0.15 0.06 0.00 0.00 43 -640.87 97.27 0.15 -0.06 7.09 -4547.51 6 16 -759.55 46.02 -3.73 0.19 0.00 0.00 43 762.51 -46.02 3.73 -0.19 174.48 2151.22 7 16 -565.01 134.60 0.22 -0.08 0.00 0.00 43 567.98 -134.60 -0.22 0.08 -10.29 6292.49 8 16 -109.58 -35.89 -2.91 0.18 0.00 0.00 43 114.52 35.89 2.91 -0.18 135.99 -1677.94 9 16 36.32 30.55 0.06 -0.02 0.00 0.00 43 -31.38 -30.55 -0.06 0.02 -2.59 1428.01 5 43 620.99 -97.28 1.77 0.18 -20.58 4547.72 44 ~620.18 97.28 -1.77 -0.18 7.13 -5286.64 6 43 -773.52 222.26 9.04 0.57 -165.46 -2151.39 44 774.01 -222.26 -9.04 -0.57 96.83 3839.65 7 43 -577.51 54.92 -1.99 -0.23 24.50 -6292.71 44 577.99 54.92 1.99 0.23 -9.35 5875.51 8 43 -133.75 96.29 8.06 0.55 -139.00 1677.96 44 134.55 -96.29 -8.06 -0.55 77.79 -946.57 9 43 13.26 -111.60 -0.21 -0.05 3.47 -1428.03 44 -12.46 111.60 0.21 0.05 -1.85 580.32 5 44 615.49 69.12 0.57 1.53 -18.56 5286.64 83 -614.49 -68.85 -0.57 -1.53 12.96 -4611.72 6 44 -820.65 99.08 10.80 27.18 -85.48 -3839.71 83 821.25 -98.92 -10.80 -27.18 -20.18 4808.34 7 44 -527.65 -229.72 -0.52 -1.73 20.79 -5875.45 83 528.25 229.89 0.52 1.73 -15.72 3627.04 8 44 -171.84 123.84 8.51 21.49 -77.55 946.53 83 172.83 -123.57 -8.51 -21.49 -5.75 263.78 9 44 47.92 -122.77 0.03 -0.19 2.16 -580.28 83 -46.92 123.04 -0.03 0.19 -2.41 -622.19 5 18 593.74 -94.23 0.76 0.46 0.00 0.00 45 -588.79 94.23 -0.76 -0.46 -35.66 -4405.41 6 18 -722.32 43.72 -4.14 -0.05 0.00 0.00 45 725.29 -43.72 4.14 0.05 193.62 2043.84 7 18 -508.30 131.15 -0.55 -0.61 0.00 0.00 45 511.27 -131.15 0.55 0.61 25.49 6131.13 8 18 -119.35 -35.41 -2.55 0.30 0.00 0.00 45 124.30 35.41 2.55 -0.30 119.39 1655.59 9 18 41.16 30.16 0.14 0,13 0.00 0.00 45 -36.22 -30.16 -0.14 0.13 -6.71 1409,87 45 570.86 -94.32 -26.75 1.80 53,17 4407.02 46 -570,05 94.32 26.75 -1.80 150.06 -5123.45 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 29 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 30 *4GBA WITH RAFTER STIFFENER ME~ER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT AXI;tL SHEAR-Y SHEAR-Z TORSION MOM-Y MO~-Z 32 33 34 35 6 45 -735.74 220.01 29.40 -0.48 214.10 -2044.34 46 736.22 -220.01 -29.40 0.48 -9.23 3715.56 7 45 -519.98 -58.28 30.38 -2.28 -50.43 -6133.59 46 520.46 58.28 -30.38 2.28 -180.33 5690.90 8 45 -141.70 96.75 2.68 0.94 -122.09 1656.38 46 142.51 -96.75 -2.68 -0.94 101.73 -921.49 9 45 20.11 4111.97 3.41 -0.41 0.66 -1410.56 46 -19.31 111.97 -3.41 0.41 -26.60 560.02 5 46 578.01 58.48 -0.49 45.19 -132.15 5123.50 90 -577.01 -58.20 0.49 -45.19 136.98 -4552.70 6 46 -792.86 106.79 13.12 -4.09 -12.56 -3715.63 90 793.46 -106.63 -13.12 4.09 -115.77 4759.69 7 46 -485.45 -217.76 0.09 -52.20 148.50 -5690.91 90 486.05 217.92 -0.09 52.20 149.34 3559.56 8 46 -178.13 121.92 9.48 29.65 -105.10 921.47 90 179.12 -121.64 -9.48 -29.65 12.37 270.03 9 46 52.43 -121.50 -0.30 -6.43 15.69 -559.99 90 -51.43 121.77 0.30 6.43 -12.80 -630.07 5 20 4.68 0.00 0.01 0.01 0.00 0.00 25 4.68 0.00 -0.01 -0.01 -0.57 0.00 6 20 2.81 -0.02 0.03 -0.12 0.00 0.00 25 2.81 0.02 -0.03 0.12 -1.42 -0,75 7 20 2.81 -0.01 0.01 0.12 0.00 0.00 25 2.81 0.01 -0.01 -0.12 -0.28 -0.47 8 20 4.68 -0.01 0.03 -0.09 0.00 0.00 25 4.68 0.01 -0.03 0.09 -1.48 -0.56 9 20 4.68 -0.01 0.01 0.09 0.00 0.00 25 4.68 0.01 -0.01 -0.09 -0.62 -0.35 5 21 474.15 0.03 -0.04 0.02 0.00 0.00 47 -464.79 -0.03 0.04 -0.02 1.80 1.51 47 102.29 -216.52 0.01 0.30 0.60 10122.32 7 21 -104.80 271.06 0.22 0.26 0.00 0.00 47 110.42 -271.06 0.22 -0.26 -10.12 12671.95 8 21 254.45 162.41 -0.04 -0.21 0.00 0.00 47 4245.08 -162.41 0.04 0.21 1.75 7592,84 9 21 248.36 203.32 0.13 0.21 0.00 0.00 47 -238.99 -203.32 -0.13 -0.21 -6.29 9505.06 5 22 427.23 0.03 1.67 0.03 0.00 0.00 48 -417.86 -0.03 1.67 0.03 77.98 1.52 6 22 -102.77 209.50 -2.98 -0.36 0.00 0.00 48 108.40 -209.50 2.98 0.36 139.14 9794.32 7 22 -104.41 225.55 4.10 -0.24 0.00 0.00 48 110.03 -225.55 -4.10 0.24 -191.78 10544.53 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 30 of 89 Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 31 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL ) MEMBER LOAD JT ;~XIAL SHEAR-Y SEEAR-Z TORSION MOM-Y MOM-Z 36 37 39 8 22 218.00 157.15 -3.45 0.25 0.00 0.00 48 -208.63 -157.15 3.45 0.25 161.05 7346.84 9 22 216.77 169.19 1.86 -0.16 0.00 0.00 48 -207.40 -169.19 -1.86 0.16 -87.13 7909.50 5 23 294.65 0.00 -1.28 0.04 0.00 0.00 49 -285.28 0.00 1.28 -0.04 60.02 -0.10 6 23 -11.77 99.06 -2.69 -0.15 0.00 0.00 49 17.39 -99.06 2.69 0.15 125.93 4630.93 7 23 -108.87 116.19 3.61 -0.28 0.00 0.00 49 114.49 -116.19 -3.61 0.28 -168.89 5431.88 8 23 196.86 74.29 -2.95 -0.08 0.00 0.00 49 -187.49 -74.29 2.95 0.08 138.04 3473.13 9 23 124.03 87.14 1.78 -0.18 0.00 0.00 49 -114.66 -87.14 -1.78 0.18 -83.08 4073.84 5 24 166.81 -0.05 1.15 0.39 0.00 0.00 50 -161.87 0.05 -1.15 -0.39 -53.68 -2.40 6 24 57.86 -3.83 -2.83 -0.14 0.00 0.00 50 -54.89 3.83 2.83 0.14 132.12 -179.24 7 24 -60.67 4.47 0.66 -0.64 0.00 0.00 50 63.63 -4.47 -0.66 0.64 -30.84 209.20 8 24 157.44 -2.90 ~1.29 0.18 0.00 0.00 50 -152.50 2.90 1.29 -0.18 60.21 -135.74 9 24 68.55 3.33 1.33 -0.20 0.00 0.00 50 ~63.61 -3.33 -1.33 0,20 -62.02 155.59 5 50 129.15 -37.14 -29.36 1.60 65.26 ~29.76 51 -128.34 37.14 29.36 -1.60 157.72 -252.38 6 50 -105.73 11.62 19.93 -0.79 -136.94 185.42 51 106.21 -11.62 -19.93 0.79 14.46 -97.18 7 50 -67.73 9.65 21.49 -2.30 26.91 -191.62 51 68.21 -9.65 -21.49 2.30 -190.18 264.94 8 50 12.51 -18.27 -6.31 0.57 -55.47 116.96 51 -11.70 18.27 6.31 0.57 103.37 -255.73 9 50 41.01 -19.74 -5.13 -0.57 67.42 -165.82 51 -40.21 19.74 5.13 0.57 -28.42 15.86 5 51 117,86 -2.98 -0.58 45.80 -147.55 252.34 97 -116.86 3.25 0.58 -45.80 153.23 -282.84 6 51 -147.14 22.96 -4.14 -9.92 23.11 97.18 97 147.74 -22.79 4.14 9.92 17.44 126.63 7 51 -52.55 -21.00 -17.57 -57.75 192.82 -264.87 97 53.15 21.16 17.57 57.75 -20.92 58.65 8 51 -26.00 14.70 -3.53 25.72 -89.49 255.70 97 27.00 -14.43 3.53 -25.72 124.06 -113.21 9 51 44.94 -18.26 -13.60 -10.16 37.79 -15.84 97 -43.94 18.54 13.60 10.16 95.28 -164.20 C:lat work\HORTON\6 BAYS\i3GG3ORR.anl Page 31 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 32 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ABE -- POUN INCH (LOCAL ) MEMBER LOAD JT AXIAL SHEAR-Y SHEA~-Z TORSION MOM-Y MOM-Z 43 44 45 46 47 5 5 25 3.45 0.00 0.05 0.03 -1.03 0.00 26 3.45 0.00 0.05 -0.03 -0.57 -0.01 6 25 2.07 -0.01 -0.03 0.35 -0.95 -0.82 26 2.07 0.01 0.03 -0.35 2.05 0.47 7 25 2.07 0.03 -0.03 1.19 0.02 -0.23 26 2.07 -0.03 0.03 -1.19 0.85 1.32 8 25 3.45 -0.01 0.01 0.28 -1.42 -0.62 26 3.45 0.01 -0.01 -0.28 1.20 0.34 9 25 3.45 0.02 0.01 0.92 -0.69 -0.17 26 3.45 -0.02 -0.01 -0.92 0.29 0.98 5 47 423.34 0.03 -0.65 0.07 8.76 -1.51 52 -416.44 -0.03 0.65 -0.07 13.57 2.65 6 47 -127.19 -121.54 -2.10 -0.25 36.86 -10120.81 52 131.34 121.54 2.10 0.25 35.34 5933.76 7 47 -136.17 -125.49 1.13 1.02 -23.51 -12671.19 52 140.31 125.49 -1.13 -1.02 -15.52 8348.14 8 47 203.77 -91.13 -2.04 -0.14 34.00 -7591.71 52 -196.87 91.13 2.04 0.14 36.26 4452.24 9 47 197.04 -94.09 0.38 0.81 -11.28 -9504.49 52 -190.13 94.09 -0.38 -0.81 -1.88 6263.02 5 48 375.58 0.03 4.91 0.09 -91.20 -1.51 54 -368.67 -0.03 -4.91 -0.09 -77.87 2.53 6 48 -133.28 -128.59 10.59 -1.02 -180.03 -9794.24 54 137.42 128.59 -10.59 1.02 -184.72 5364.55 7 48 -135.85 -171.05 -13.22 -0.77 232.40 -10544.45 54 139.99 171.05 13.22 0.77 223.07 4652.07 8 48 166.74 -96.42 11.52 -0.70 -201.40 -7346.78 54 -159.84 96.42 -11.52 0.70 -195.61 4025.25 9 48 164.82 -128.26 -6.33 -0.52 107.92 -7909.43 54 -157.91 128.26 6.33 0.52 110.23 3490.89 5 49 250.78 0.00 2.46 0.12 -84.78 -0.03 100 -243.87 0.00 -2.46 -0.12 0.00 0.00 6 49 -38.80 -134.42 3.18 -0.65 -109.57 -4630.75 100 42.94 134.42 -3.18 0.65 0.00 0.00 7 49 -125.14 -157.68 -5.19 -1.05 178.81 -5432.04 100 129.28 157.68 5.19 1.05 0.00 0.00 8 49 151.80 -100.82 4.17 -0.40 -143.77 -3473.08 100 -144.89 100.82 -4.17 0.40 0.00 0.00 9 49 87.04 -118.26 -2.10 -0.70 72.51 -4074.05 100 -80.14 118.26 2.10 0.70 0.00 0.00 54 257.41 0.58 -12.79 0.14 104.89 4.77 101 -255.77 -0.58 12.79 -0.14 0.00 0.00 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 32 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT~13GG -- PAGE NO. 33 *4GBA WITH RAFTER STIFFENER MEb~ER END FORCES STRUCTURE TYPE = SPACE A~LL UNITS A~E -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SSEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 48 49 5O 6 54 -124.28 -308.04 -20.26 -1.57 166.17 -2525.96 101 125.27 308.04 20.26 1.57 0.00 0.00 7 54 -117.99 -310.84 26.07 -1.39 -213.74 -2548.85 101 118.97 310.84 -26.07 1.39 0.00 0.00 8 54 94.72 -230.61 -24.51 -1.08 200.99 -1891.02 101 -93.08 230.61 24.51 1.08 0.00 0.00 9 54 99.45 -232.71 10.24 -0.94 -83.95 -1908.19 101 -97.80 232.71 -10.24 0.94 0.00 0.00 5 53 164.45 -0.45 16.29 21.58 -267.09 -7.39 102 -161.16 0.45 -16.29 -21.58 0.00 0.00 6 53 -85.94 -25.88 -2.87 -219.61 47.06 -424.45 102 87.91 25.88 2.87 219.61 0.00 0.00 7 53 -88.15 -171.21 -8.26 -243.38 135.54 -2807.85 102 90.12 171.21 8.26 243.38 0.00 0.00 8 53 56.29 -19.74 9.43 -149.08 -154.68 -323.69 102 -53.01 19.74 ~9.43 349.08 0.00 0.00 9 53 54.63 -128.73 5.39 -166.90 -88.32 -2111.24 102 -51.35 128.73 ~5.39 166.90 0.00 0.00 5 52 281.57 -0.10 0.32 0.12 -7.99 -2.48 103 -276.64 0.10 -0.32 -0.12 0.00 0.00 6 52 -115.40 -339.43 1.79 -0.08 -43.96 -8349.99 103 118.36 339.43 -1.79 0.08 0.00 0.00 7 52 -113.96 -310.87 -0.75 1.43 18.46 -7647.30 103 116.92 310.87 0.75 1.43 0.00 0.00 8 52 118.02 -254.65 1.57 0.03 -38.59 -6264.29 103 -113.09 254.65 -1.57 -0.03 0.00 0.00 9 52 119.10 -233.22 -0.33 1.16 8.22 -5737.27 103 -114.17 233.22 0.33 -1.16 0.00 0.00 5 26 3.29 0.00 0.00 0.07 -0.09 -0.01 27 3.29 0.00 0.00 -0.07 0.80 0.00 6 26 1.97 0.02 -0.08 0.88 2.62 0.72 27 1.97 -0.02 0.08 -0.88 0.00 0.00 7 26 1.97 0.04 -0.03 1.97 0.88 1.43 27 1.97 -0.04 0.03 -1.97 0.00 0.00 8 26 3.29 0.02 -0.06 0.71 1.95 0.53 27 3.29 -0.02 0.06 -0.71 0.00 0.00 9 26 3.29 0.03 -0.02 1.53 0.65 1.06 27 3.29 -0.03 0.02 -1.53 0.00 0.00 5 7 -36.89 0.00 -0.55 0.00 0.00 0.00 28 36.89 0.00 -0.55 0.00 0.00 0.00 6 7 -56.73 0.00 -0.33 1.38 0.00 0.00 28 56.73 0.00 -0.33 -1.38 0.00 0.00 7 7 91.79 0.00 -0.33 -0.54 0.00 0.00 28 -91.79 0.00 -0.33 0.54 0.00 0.00 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 33 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 34 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCA~ } MEMBER LOAD JT ~XIAL SHEAR-Y SEF~%R-Z TORSION MOM-Y MOM-Z 52 53 54 55 8 7 -69.39 0.00 -0.55 1.04 0.00 28 69.39 0.00 -0.55 -1.04 0.00 9 7 42.00 0.00 -0.55 -0.40 0.00 28 -42.00 0.00 -0.55 0.40 0.00 5 28 ~38.04 0.00 -0.55 0.00 0.00 29 38.04 0.00 -0.55 0.00 0.00 6 28 -57.46 0.00 -0.33 0.30 0.00 29 57.46 0.00 -0.33 -0.30 0.00 7 28 94.26 0.00 -0.33 0.31 0.00 29 -94.26 0.00 -0.33 -0.31 0.00 8 28 -70.76 0.00 -0.55 0.23 0.00 29 70.76 0.00 -0.55 -0.23 0.00 9 28 43.03 0.00 -0.55 0.23 0.00 29 -43.03 0.00 -0.55 -0.23 0.00 5 29 -39.89 0.08 -0.55 0.00 0.00 30 39.89 0.00 -0.55 0.00 0.00 6 29 -59.48 0.00 -0.33 0.17 0.00 30 59.48 0.00 -0.33 -0.17 0.00 7 29 99.51 0.00 -0.33 0.24 0.00 30 -99.51 0.00 -0.33 -0.24 0.00 8 29 -73.63 0.00 -0.55 0.12 0.00 30 73.63 0.00 -0.55 -0.12 0.00 9 29 45.61 0.00 -0.55 0.18 0.00 30 -45.61 0.00 -0.55 -0.18 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 0.00 0.00 0.00 0.00 0.00 0.00 0.00 5 30 -43.50 0.00 -0.55 0.01 0.00 0.00 31 43,50 0.00 -0.55 -0.01 0.00 0.00 6 30 -61.92 0.00 -0.33 -0.07 0.00 0.00 31 61.92 0.00 -0.33 0.07 0.00 0.00 7 30 109.11 0.00 -0.33 0.14 0.00 0.00 31 -109.11 0.00 ~0.33 -0.14 0.00 0.00 8 30 -78,08 0.00 -0.55 -0.05 0.00 0.00 31 78.08 0.00 -0.55 0.05 0.00 0.00 9 30 80.20 0.00 -0.55 0.11 0.00 0.00 31 -50.20 0.00 -0.55 -0.11 0.00 0.00 5 31 -46.64 0.00 -0.64 -0,10 0.00 32 46.64 0.00 -0,64 0.10 0.00 6 31 -64.04 0.00 -0.38 0.10 0.00 32 64.04 0.00 -0.38 -0.10 0.00 7 31 119.87 0.00 -0.38 -0.20 0.00 32 -119.87 0.00 -0.38 0.20 0.00 8 31 -81.92 0.00 -0.64 0.01 0.00 32 81.92 0.00 -0.64 0.01 0.00 9 31 56.01 0.00 -0.64 -0.22 0.00 32 -56.01 0.00 0.64 0.22 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 34 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG - PAGE NO. 35 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTUR~ TYPE = SPACE ALL UNITS A~E -- POUN INCH (LOCAL) ME~ER LOAD JT AXIAL SHEAR-Y SEEAR-Z TORSION MOM-Y MOM-Z 56 57 58 59 6O 5 5 8 -1.29 0.00 -0.55 0.00 34 1.29 0.00 -0.55 0.00 6 8 -64.65 0.00 -0.33 -1.08 34 64.65 0.00 -0.33 1.08 7 8 -1.39 0.00 -0.33 1.75 34 1.39 0.00 -0.33 -1.75 8 8 -49.50 0.00 -0.55 -0.81 34 49.50 0,00 -0.55 0.81 9 8 -2.06 0.00 -0.55 1.32 34 2.06 0.00 -0.55 -1.32 5 34 -1.27 0.00 -0.55 0.00 35 1.27 0.00 -0.55 0.00 6 34 -62.08 0.00 -0.33 0.84 35 62.08 0.00 -0.33 -0.84 7 34 2.89 0.00 -0.33 -0.20 35 2.89 0.00 -0.33 0.20 8 34 -47.54 0.00 -0.55 0.63 35 47.54 0.00 -0.55 -0.63 9 34 -3.14 0.00 -0.55 -0.15 35 3.14 0.00 -0.55 0.15 5 35 -0.41 0.00 -0.55 0.00 36 0.41 0.00 -0.55 0.00 6 35 -57.13 0.00 -0.33 0.71 36 57.13 0.00 -0.33 -0.71 7 35 -6.55 0.00 -0.33 -0.27 36 6.55 0.00 -0.33 0.27 8 35 -43.18 0.00 -0.55 0.53 36 43.18 0.00 -0.55 -0.53 9 35 -5.24 0.00 -0.55 -0.20 36 5.24 0.00 -0.55 0.20 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 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 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 0.00 0.00 0.00 0.00 0.00 0.00 5 36 3.35 0.00 -0.55 0.24 0.00 0.00 58 -3.35 0.00 -0.55 -0.24 0.00 0.00 6 36 -48.55 0.00 -0.33 0.94 0.00 0.00 58 48.55 0.00 -0.33 -0.94 Q.00 0.00 7 36 -16.53 0.00 -0.33 -1.75 0.00 0.00 58 16.53 0.00 -0.33 1,75 0.00 0.00 8 36 -33.99 0.00 -0.55 0.88 0.00 0.00 58 33.99 0.00 -0.55 -0.88 0.00 0.00 9 36 -9.97 0.00 -0.55 -1.14 0.00 0.00 58 9.97 0.00 -0.55 1.14 0.00 0.00 32 -35.44 0.00 -0.54 1.36 0.00 0.00 37 35.44 0.00 -0.54 -1.36 0.00 0.00 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 35 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG - PAGE NO. 36 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL ) MEMBER LOAD JT AXIltL SHEA~-Y SHEAR-Z TORSION MOM-Y MOM-Z 62 63 64 6 32 154.87 0.00 -0.33 -0.28 0.00 0.00 37 -154.87 0.00 -0.33 0.28 0.00 0.00 7 32 -106.58 0.00 -0.33 -2.18 0.00 0.00 37 106.58 0.00 -0.33 2.18 0.00 0.00 8 32 90.51 0.00 -0.54 0.77 0.00 0.00 37 -90.51 0.00 -0.54 -0.77 0.00 0.00 9 32 -105.58 0.00 -0.54 -0.65 0.00 0.00 37 105.58 0.00 -0.54 0.65 0.00 0.00 5 58 33.56 0.53 -0.13 6.39 0.00 0.00 65 -33.56 0.53 -0.13 -6.39 0.00 0.00 6 58 219.72 0.32 -0.08 -5.49 0.00 0.00 65 -219.72 0.32 -0.08 5.49 0.00 0.00 7 58 -306.66 0.32 -0.08 -6.48 0.00 0.00 65 306.66 0.32 -0.08 6.48 0.00 0.00 8 58 189.09 0.53 -0.13 0.51 0.00 0.00 65 -189.09 0.53 -0.13 -0.51 0.00 0.00 9 58 -205.70 0.53 -0.13 -0.22 0.00 0.00 65 205.70 0.53 ~0.13 0.22 0.00 0.00 5 59 -4.90 0.53 0.13 2.47 0.00 0.00 66 4.90 0.53 -0.13 -2.47 0.00 0.00 6 59 260.43 0.32 -0.08 -2.34 0.00 0.00 66 -260.43 0.32 -0.08 2.34 0.00 0.00 7 59 -277.97 0.32 -0.08 -2.31 0.00 0.00 66 277.97 0.32 -0.08 2.31 0.00 0.00 8 59 191.77 0.53 -0.13 0.04 0.00 0.00 66 -191.77 0.53 -0.13 -0.04 0.00 0.00 9 59 -212.03 0.53 -0.13 0.06 0.00 0.00 66 212.03 0.53 -0.13 -0.06 0.00 0.00 5 60 0.27 0.53 -0.13 -2.46 0.00 0.00 67 -0.27 0.53 -0.13 2.46 0.00 0.00 6 60 293.89 0.32 -0.08 1.95 0.00 0.00 67 -293.89 0.32 -0.08 -1.95 0.00 0.00 7 60 -306.66 0.32 -0.08 2.66 0.00 0.00 67 306.66 0.32 -0.08 -2.66 0.00 0.00 8 60 220.62 0.53 -0.13 -0.32 0.00 0.00 67 -220.62 0.53 -0.13 0.32 0.00 0.00 9 60 229.80 0.53 -0.13 0.21 0.00 0.00 67 229.80 0.53 -0.13 -0.21 0.00 0.00 5 61 -0.17 0.53 -0.13 6.82 0.00 0.00 68 0.17 0.53 -0.13 6.82 0.00 0.00 6 61 303.77 0.32 -0.08 5.75 0.00 0.00 68 -303.77 0.32 0.08 -5.75 0.00 0.00 7 61 -331.34 0.32 -0.08 6.88 0.00 0.00 68 331.34 0.32 -0.08 -6.88 0.00 0.00 C:\at work\HORTON\6 BAYS\13GG3ORR.ani Page 36 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 37 MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCJtL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 65 8 61 227.71 0.53 -0.13 -0.63 68 -227.71 0.53 -0.13 0.63 9 61 -248.63 0.53 -0.13 0.22 68 248.63 0.53 -0.13 -0.22 5 37 -68.47 0.00 -0.54 0.05 39 68.47 0.00 40.54 -0.05 6 37 137.59 0.00 -0.33 -0.04 39 -137.59 0.00 -0.33 0.04 7 37 74.91 0.00 -0.33 -0.06 39 74.91 0.00 -0.33 0.06 8 37 53.64 0.00 -0.54 0.01 39 -53.64 0.00 0.54 -0.01 9 37 -105.74 0.00 -0.54 -0.01 39 105.74 0.00 -0.54 0.01 66 5 65 70.13 0.53 -0.13 0.07 72 -70.13 0.53 -0.13 -0.07 6 65 108.58 0.32 -0,08 -0.05 72 -108.58 0.32 -0,08 0.05 7 65 -354.33 0.32 -0.08 -0,08 72 354.33 0.32 -0.08 0.08 8 65 132.21 0.53 -0.13 0.01 72 -132.21 0.53 -0.13 -0.01 9 65 -214.98 0.53 -0.13 -0.01 72 214.98 0.53 -0.13 0.01 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 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 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 67 5 66 -9.93 0.53 -0.13 0.00 0.00 0.00 73 9.93 0.53 -0.13 0.00 0.00 0.00 6 66 167.07 0.32 -0.08 0.00 0.00 0.00 73 -167.07 0.32 -0.08 0.00 0.00 0.00 7 66 -275.13 0.32 -0.08 0.00 0.00 0.00 73 275.13 0.32 -0.08 0.00 0.00 0.00 B 66 118.11 0.53 -0.13 0.00 0.00 0.00 73 -118.11 0.53 -0.13 0.00 0.00 0.00 9 66 -213.54 0.53 -0.13 0.00 0.00 0,00 73 213.54 0.53 -0.13 0.00 0.00 0.00 68 5 67 0.23 0.53 -0.13 -0.05 74 -0.23 0.53 -0.13 0.05 6 67 217.79 0.32 -0.08 0.04 74 217.79 0.32 -0.08 -0.04 7 67 -298.84 0.32 -0.08 0.06 74 298.84 0.32 -0.08 0.06 8 67 163.51 0.53 -0.13 -0.01 74 -163.51 0.53 -0.13 0.01 9 67 -223.96 0.53 -0.13 0.01 74 223.96 0.53 -0.13 -0.01 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 0.00 0.00 C:\at work\HOBTON\6 BAYS\13GG3ORR.anl Page 37 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 38 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ABE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 69 7O 72 73 5 5 68 -0.23 0.53 -0.13 -0.08 75 0.23 0.53 -0.13 0.08 6 68 179.95 0.32 -0.08 0.06 75 -179.95 0.32 -0.08 -0.06 7 68 -324.65 0,32 -0,08 0.09 75 324.65 0.32 -0.08 -0.09 8 68 134.80 0.53 -0.13 -0.02 75 -134.80 0.53 -0.13 0.02 9 68 -243.65 0.53 -0.13 0.01 75 243.65 0.53 -0.13 -0.01 5 39 -66.30 0.00 -0.54 0.00 41 66.30 0.00 -0.54 0.00 6 39 89.64 0.00 -0.33 0.00 41 -89.64 0.00 -0.33 0.00 7 39 -78.70 0.00 -0.33 0.00 41 78.70 0.00 -0.33 0.00 8 39 19.24 0.00 -0,54 0.00 41 -19.24 0.00 -0.54 0.00 9 39 -107.01 0.00 0.54 0.00 41 107.01 0.00 -0.54 0.00 5 72 71.86 0.53 -0.13 0.00 79 -71.86 0.53 -0.13 0.00 6 72 17.34 0.32 -0.08 0.00 79 -17.34 0.32 -0.08 0.00 7 72 -357.86 0.32 -0.08 0.00 79 357.86 0.32 -0.08 0.00 8 72 65.03 0.53 -0.13 0.00 79 -65.03 0.53 -0.13 0.00 9 72 -216.37 0.53 -0.13 0.00 79 216.37 0.53 0.13 0.00 5 73 -8.43 0.53 -0.13 0.00 80 8.43 0.53 -0.13 0.00 6 73 67.99 0.32 -0.08 0.00 80 -67.99 0.32 -0.08 0.00 7 73 -281.29 0.32 -0.08 0,00 80 281.29 0.32 -0.08 0.00 8 73 44.89 0.53 -0.13 0.00 80 -44.89 0.53 -0.13 0.00 9 73 -217.07 0.53 -0.13 0.00 80 217.07 0.53 -0.13 0.00 74 -0.38 0.53 -0.13 0.00 81 0.38 0.53 -0.13 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 O.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 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 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 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 0.00 c:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 3~ of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 39 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SSEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 74 75 76 77 6 74 143.10 0.32 -0.08 0.00 81 -143.10 0.32 ~0.08 0.00 7 74 -287.66 0.32 -0.08 0.00 81 287.66 0.32 -0.08 0.00 8 74 107.05 0.53 -0.13 0.00 81 -107.05 0.53 -0.13 0.00 9 74 -216.01 0.53 -0.13 0.00 81 216.01 0.53 -0.13 0.00 5 75 0.02 0.53 -0.13 0.00 82 -0.02 0.53 -0.13 0.00 6 75 58.19 0.32 -0.08 0.00 82 -58.19 0.32 -0.08 0.00 7 75 -325.12 0.32 -0.08 0.00 82 325.12 0.32 -0.08 0.00 8 75 43.66 0.53 -0.13 0.00 82 -43.66 0.53 -0.13 0.00 9 75 -243.82 0.53 -0.13 0.00 82 243.82 0.53 -0.13 0.80 5 41 -66.21 0.00 -0.54 0.00 43 66.21 0.00 0.54 0.00 6 41 42.09 0.00 -0.33 0.00 43 -42.09 0.00 -0.33 0.00 7 41 -79.00 0.00 -0.33 0.00 43 79.00 0.00 -0.33 0.00 8 41 -16.36 0.00 -0.54 0.00 43 16.36 0.00 -0.54 0.00 9 41 -107.17 0.00 -0.54 0.00 43 107.17 0.00 -0.54 0.00 5 79 71.80 0.53 -0.13 0.00 86 -71.80 0.53 -0.13 0.00 6 79 -73.01 0.32 -0.08 0.00 86 73.01 0.32 -0.08 0.00 7 79 -358.12 0.32 -0.08 0.00 86 358.12 0.32 -0.08 0.00 8 79 -2.78 0.53 -0.13 0.00 86 2.78 0.53 -0.13 0.00 9 79 -216.61 0.53 -0.13 0.00 86 216.61 0.53 -0.13 0.00 5 80 -8.39 0.53 -0.13 0.00 87 8.39 0.53 -0.13 0.00 6 80 -32.77 0.32 -0.08 0.00 87 32.77 0.32 -0.08 0.00 7 80 -287.09 0.32 -0.08 0.00 87 287.09 0.32 -0.08 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 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 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 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 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 c:\a~ work\HORTON\6 BAYS\13GG3ORR.anl Page 39 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM PAGE NO. 40 MEMBER END FORCES STRUCTUBE TYPE = SPACE ALL UNITS ARE -- POUN INCS (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SSEAR-Z TORSION MOM-Y MOM-Z 8 80 -30.65 0.53 -0.13 0.00 87 30.65 0.53 -0.13 0.00 9 80 -221.39 0.93 -0.13 0.00 87 221.39 0.53 -0.13 0.00 78 5 81 -0.45 0.53 -0.13 0.00 88 0.45 0.53 -0.13 0.00 6 81 72.22 0.32 -0.08 0.00 88 -72.22 0.32 -0.08 0.00 7 81 -273.89 0.32 -0.08 0.00 88 273.89 0.32 -0.08 0.00 8 81 53.84 0.53 -0.13 0.00 88 -53.84 0.53 -0.13 0.00 9 81 -205.74 0.53 -0.13 0.00 88 205.74 0.53 -0.13 0.00 79 5 82 0.05 0.53 -0.13 0.00 89 -0.05 0.53 -0.13 0.00 6 82 -65.04 0.32 -0.08 0.00 89 65.04 0.32 -0.08 0.00 7 82 -332.54 0.32 -0.08 0.00 89 332.54 0.32 -0.08 0.00 8 82 -48.74 0.53 -0.13 0.00 89 48.74 0.53 -0.13 0.00 9 82 -249.36 0.53 -0.13 0.00 89 249.36 0.53 -0.13 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 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 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 80 5 43 -68.19 0.00 -0.54 -0.05 0.00 0.00 45 68.19 0.00 -0.54 0.05 0.00 0.00 6 43 -3.54 0.00 -0.33 0.04 0.00 0.00 45 3.54 0.00 -0.33 -0.04 0.00 0.00 7 43 -75.98 0.00 -0.33 0.06 0.00 0.00 45 75.98 0.00 -0.33 -0.06 0.00 0.00 8 43 -52.01 0,00 -0.54 -0.01 0.00 0.00 45 52.01 0.00 -0.54 0.01 0.00 0.00 9 43 -106.35 0.00 -0.54 0.01 0.00 0.00 45 106.35 0.00 -0.54 0.01 0.00 0.00 81 5 86 69.98 0.53 -0.13 -0.07 0.00 0.00 93 -69.98 0.53 -0.13 0.07 0.00 0.00 6 86 -159.87 0.32 -0.08 0.06 0.00 0,00 93 159.87 0.32 -0.08 -0.06 0.00 0.00 7 86 -355.04 0.32 -0.08 0.08 0.00 0.00 93 355.04 0.32 -0.08 -0.08 0.00 0.00 8 86 -69.23 0.53 -0.13 -0.01 0.00 0.00 93 69.23 0.53 -0.13 0.01 0.00 0.00 9 86 -215.62 0.53 -0.13 0.01 0.00 0.00 93 215.62 0,53 -0.13 -0.01 0.00 0.00 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 40 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG - PAGE NO. 41 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS APE -- POUN INCH (LOCAL } MEMBER LOAD JT AXIAL SHEAR-Y SHF~%R-Z TORSION MOM-Y MOM-Z 82 83 84 85 86 5 5 87 -9.82 0.53 -0.13 0.00 94 9.82 0.53 -0.13 0.00 6 87 -137.43 0.32 -0.08 0.00 94 137.43 0.32 -0.08 0.00 7 87 -293.36 0.32 -0.08 0.00 94 293.36 0.32 -0.08 0.00 8 87 -110.18 0.53 -0.13 0.00 94 110.18 0.53 -0.13 0.00 9 87 -227.13 0.53 -0,13 0.00 94 227.13 0.53 -0.13 0.00 5 88 0.03 0.53 -0.13 0.05 95 -0.03 0.53 -0.13 -0,05 6 88 8.33 0.32 -0.08 -0.04 95 -8.33 0.32 -0.08 0.04 7 88 -256.33 0.32 -0.08 0.06 95 256.33 0.32 -0.08 0.06 8 88 6.26 0.53 -0.13 0.01 95 -6.26 0.53 -0.13 -0.01 9 88 -192.23 0.53 -0.13 -0.01 95 192.23 0.53 -0.13 0.01 5 89 -0.12 0.53 -0,13 0.08 96 0.12 0.53 -0.13 -0.08 6 89 -193.72 0.32 -0.08 -0.06 96 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January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER -- PAGE NO. 42 MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ABE -- FOUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 87 88 89 90 6 93 213.81 0.32 -0.08 5.39 0.00 0.00 100 213.81 0.32 -0.08 -5.39 0.00 0.00 7 93 -308.20 0.32 -0.08 6.52 0.00 0.00 100 308.20 0.32 0.08 -6.52 0.00 0.00 8 93 -136.05 0.53 -0.13 -0.61 0.00 0.00 100 136.05 0.53 -0.13 0.61 0.00 0.00 9 93 -206.85 0.53 0.13 0.23 0.00 0.00 100 206.85 0.53 -0.13 -0.23 0.00 0.00 5 94 -4.68 0.53 -0.13 -2.36 101 4.68 0.53 -0.13 2.36 6 94 -256.13 0,32 -0.08 2.33 101 256.13 0.32 -0.08 -2.33 7 94 -311.99 0.32 -0.08 2.25 101 311.99 0.32 -0.08 -2.25 8 94 -195.49 0.53 -0.13 0.03 101 195.49 0.53 -0.13 -0.03 9 94 -237.38 0.53 -0.13 -0.02 101 237.38 0.53 -0.13 0.02 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 5 95 -0.08 0.53 -0,13 2.46 0.00 102 0.08 0.53 -0.13 -2,46 0.00 6 95 -43.97 0.32 -0.08 -1.95 0.00 102 43.97 0,32 -0.08 1.95 0.00 7 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SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ABE -- POUN INCH (LOC;iL ) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 92 93 94 8 47 -7.51 0.00 -0.55 1.03 0.00 0.00 25 7.51 0.00 -0.55 -1.03 0.00 0.00 9 47 3.58 0.00 -0.55 0.50 0.00 0.00 25 -3.58 0.00 -0.55 -0.50 0.00 0.00 5 49 -20.55 0.00 -0.55 -0.01 0.00 0.00 48 20.55 0.00 -0.55 0.01 0.00 0.00 6 49 -38.60 0.00 -0.33 -0.05 0.00 0.00 48 38.60 0.00 -0.33 0.05 0.00 0.00 7 49 52.49 0.00 -0.33 -0.13 0.00 0.00 48 -52.49 0.00 -0.33 0.13 0.00 0.00 8 49 -43.91 0.00 -0.55 0.04 0.00 0.00 48 43.91 0.00 -0.55 0.04 0.00 0.00 9 49 24.40 0.00 -0.55 -0.10 0.00 0.00 48 -24.40 0.00 -0.55 0.10 0.00 0.00 5 50 -32.69 0.00 -0.64 0.10 0.00 0.00 49 32.69 0.00 -0.64 -0.10 0.00 0.00 6 50 -62.25 0.00 -0.38 -0.13 0.00 0.00 49 62.25 0.00 -0.38 0.13 0.00 0.00 7 50 85.25 0.00 -0.38 0.19 0.00 0.00 49 -85.25 0.00 -0.38 -0.19 0.00 0.00 8 50 -70.45 0.00 -0.64 -0.02 0.00 0.00 49 70.45 0.00 -0.64 0.02 0.00 0.00 9 50 40.17 0.00 -0.64 0.21 0.00 0.00 49 -40.17 0.00 -0.64 -0.21 0.00 0.00 5 52 3.61 0.00 -0.55 0.00 0.00 0.00 26 3.61 0.00 -0.55 0.00 0.00 0.00 6 52 -115.33 0.00 -0.33 -1.01 0.00 0.00 26 115.33 0.00 -0.33 1.01 0.00 0.00 7 52 25.71 0.00 -0.33 -2.44 0.00 0.00 26 -25.71 0.00 -0.33 2.44 0.00 0.00 8 52 89.43 0,00 0.55 -0.76 0.00 0.00 26 89.43 0.00 -0.55 0.76 0.00 0.00 9 52 16.35 0.00 -0.55 -1.83 0.00 0.00 26 -16.35 0.00 -0.55 1.83 0.00 0.00 5 53 -11.75 0.13 88.40 -0.22 -2934.13 3.99 52 11.75 -0.13 -102.44 0.22 0.00 0.00 6 53 -113.58 6.23 -42.07 2415.39 1164.02 191.57 52 113.58 -6.23 33.64 -2415.39 0.00 0.00 7 53 25.09 62.90 -44.35 703.17 1234.42 -1934.26 52 -25.09 62.90 35.93 703.17 0.00 0.00 8 53 -93.87 4.77 32.75 1811.39 -1222.97 146.57 52 93.87 -4.77 -46.79 -1811.39 0.00 0.00 9 53 10.13 -47.08 31.04 -527.53 -1170,17 -1447.80 52 -10.13 47.08 -45.07 527.53 0,00 0.00 C:\a~ work\HORTON\6 BAYS\13GG3ORR.ani Page 43 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 44 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT ;~XIAL SHEAR-Y SEEAR-Z TORSION MOM-Y MOM-Z 95 96 97 98 99 S 5 54 -33.10 0.57 -93.88 7.13 0.00 0.00 53 33.10 -0.57 79.85 -7.13 2671.06 17.56 6 54 -110.20 -13.37 32.22 2840.14 0.00 0.00 53 110.20 13.37 -40.64 -2840.14 -1120.25 -411.06 7 54 36.53 55.00 31.46 2105.23 0.00 0.00 53 -36.53 55.00 -39.88 -2105.23 -1096.76 1691.16 8 54 -106.52 -9.61 -41.78 2135.27 0.00 0.00 53 106.52 9.61 27.74 -2135.27 1068.80 ~295.58 9 54 3.53 41.66 -42.35 1584.09 0.00 0.00 53 -3.53 -41.66 28.31 -1584.09 1086.41 1281.09 5 100 -4.95 0.00 -0.55 -0.20 0.00 0.00 54 4.95 0.00 -0.55 0.20 0.00 0.00 6 100 -76.05 0.00 -0.33 1.72 0.00 0.00 54 76,05 0.00 -0.33 1.72 0.00 0.00 7 100 -13.46 0.00 -0.33 2.35 0.00 0.00 54 13.46 0.00 -0.33 2.35 0.00 0.00 8 100 -60.52 0.00 -0.55 1.15 0.00 0.00 54 60.52 0.00 -0.55 -1.15 0.00 0.00 9 100 -13.58 0.00 -0.55 1.62 0.00 0.00 54 13.58 0.00 -0.55 -1.62 0.00 0.00 5 55 89.55 45.39 -21.93 -121.87 120.10 365.57 56 -88.75 -44.63 21.93 121.87 109.61 105.93 6 55 -152.82 -22.08 33.02 152.27 -179.50 -153.22 56 153.30 22.53 -33.02 -152.27 -166.40 -80.41 7 55 -33.81 -43.47 12.67 100.60 -37.37 -238,76 56 34,29 43.93 -12.67 -100.60 -95.37 -219.00 8 55 -49.34 16.49 8.89 25.97 -47.66 153.26 56 50.14 -15.73 -8.89 -25.97 -45.46 15.53 9 55 39.92 0.45 -6.37 -12.78 58.94 89.10 56 -39.12 0.32 6.37 12.78 7.81 -88.41 5 56 36.62 60.31 -10.55 -84.92 -119.58 -106.09 57 0.99 7.36 10.55 84.92 245.46 421.99 6 56 -99.79 -9.94 7.26 97.70 171.43 80.54 57 100.16 10.60 -7.26 -97.70 -258.05 -203.06 7 56 28.92 -16.34 8.23 68.72 107.47 219.19 57 -28.55 17.00 -8.23 -68.72 205.65 -418.04 8 56 -47.54 37.28 -2.20 11.79 42.02 -15.55 57 75.90 13.75 2.20 -11.79 -15.82 155.94 9 56 48.99 32.48 -1.47 -9.95 5.95 88.44 57 -20.63 18.54 1,47 9.95 23.49 -5.29 57 -19.73 -17.01 26.66 -14.44 265.29 -422.21 58 45.74 118.75 -26.66 14.44 -166.14 -676.28 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 44 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 45 *4GBA WITH P~AFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL } MEMBER LOAD JT AXIAL SHE~-Y SSEAR-Z TORSION MOM-Y MOM-Z 100 102 103 6 57 -46.20 22.88 -43.15 21.48 291.90 203.26 58 46.45 -21.88 43.15 -21.48 406.48 158.95 7 57 48.38 44.50 -26.71 10.67 220.70 418.26 58 -48.13 -43.51 26.71 -10.67 211.57 293.85 8 57 -48.67 5.19 -13.06 5.65 26.85 -155.95 58 68.29 71.53 13.06 -5.65 184.58 ~380.81 9 57 22.26 21.41 -0.73 -2.46 -26.55 5.30 58 -2.65 55.31 0.73 2.46 38.39 -279.63 5 58 0.26 103.45 -5.46 10.46 139.82 624.56 59 52.95 96.10 5.46 10.46 33.90 -507.62 6 58 13.92 -3.86 0.24 13.48 -297.82 -115.68 59 -13.40 5.81 -0.24 -13.48 290.32 -38.09 7 58 42.10 ~7.44 7.46 8.16 -195.60 -205.46 59 -41.58 9.39 -7.46 8.16 -41.90 -62.39 8 58 11.40 74.21 -3.78 2.53 -122.13 376.03 59 28.72 76.26 3.78 -2.53 242.28 -408.62 9 58 32.53 71.52 1.65 -1.46 -45.47 308.70 59 7.59 78.95 -1.65 1.46 -6.89 -426.85 5 59 3.10 99.77 0.59 -6.61 -15.18 514.14 60 50.11 99.77 -0.59 6.61 -3.56 -514.07 6 59 -34.66 2.21 0.94 8.87 -293.91 35.23 60 35.18 -0.26 -0.94 -8.87 264.03 4.09 7 59 3.65 2.94 0.11 5.34 12.79 53.23 60 -3.13 -0.99 -0.11 -5.34 16.40 9.38 8 59 -22.94 76.20 1.13 1,86 -231.42 411.15 60 63.07 74.27 -1.13 -1.86 195.45 -380.45 9 59 5.79 76.75 0.51 -0.79 -1.40 424.64 60 34.34 73.72 -0.51 0.79 -14.87 -376.48 5 60 1.86 95.85 -0.06 -2.76 1.50 505.95 61 51.35 103.69 0.06 2.76 0.33 -630.72 6 60 -178.29 0.34 -1.98 3.76 -259.45 -2.32 61 178.81 1.61 1.98 -3.76 322.46 -18.01 7 60 -29.32 0.20 0.47 2.64 14.27 -6.94 61 29.84 1.75 -0.47 -2.64 -29.13 -17.62 8 60 -131.61 71.79 -1.53 0.82 -193.50 375.66 61 171.73 78.68 1.53 0.82 242.09 -485.41 9 60 -19.88 71,69 0.31 -0.02 11.79 372.20 61 60.01 78.78 -0.31 0.02 -21.61 -485.12 5 61 7.40 120.27 0.01 -0.49 -0.23 652.27 9 45.82 79.27 -0.01 0.49 0.00 0.00 6 61 419.78 1.39 13.30 0.65 -423.22 13.10 9 420.30 0.56 -13.30 -0.65 0.00 0.00 7 61 -53.59 1.34 -1.47 0.68 46.76 11.73 9 54.11 0.61 1.47 -0.68 0.00 0.00 C:\at work\HORTON\6 BAYS\I3GG3ORR.anl Page 45 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER -- PAGE NO. 46 MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH {LOCAL } MEMBER LOAD JT AXIAL SHEAR-y SHEAR-Z TORSION MOM-Y MOM-Z 104 106 108 8 61 -308.50 90.87 9.98 0.13 -317.57 497.75 9 348.63 59.59 -9.98 -0.13 0.00 0.00 9 61 33.86 90.84 -1.10 0.15 34.90 496.73 9 73.99 59.63 1.10 -0.18 0.00 0.00 5 97 75.96 49.22 21.91 118.19 -116.39 345.74 98 -75.15 ~48.46 -21.91 -118.19 -113.13 165.87 6 97 -194.04 10.26 -2.93 -4.15 18.22 -72.39 98 194.53 -9.80 2.93 4.15 48.91 177.45 7 97 1.56 -51.56 -13.58 -63.55 -2.64 -173.53 98 -1.07 52.02 13.58 63.55 144.87 -368.99 8 97 -90.15 43.52 13.66 82.46 -97.94 199.39 98 90.96 -42.76 -13.66 -82.46 -45.19 252.50 9 97 56.55 -2.85 5.68 37.90 -86.26 123.54 98 -55.75 3.61 -5.68 -37.90 26.78 -157.33 5 98 22.65 59.85 10.54 80.13 121.92 -166.03 99 14.96 7.81 -10.54 -80.13 -247.71 476.47 6 98 -224.19 -4.65 -10.26 9.38 -43.87 -177.38 99 224.55 5.31 10.26 -9.38 166.31 117.94 7 98 64.99 -12.95 -8.24 -16.12 -144.19 369.17 99 -64.62 13.61 8.24 16.12 242.45 -527.58 8 98 -151.00 40.90 -0.06 65.05 55.35 252.56 99 179.37 10.12 0.06 -65.05 -54.62 436.16 9 98 65.87 34.68 1.46 45.93 -19.89 157.35 99 -37.51 16.35 -1.46 -45.93 2.49 -47.98 5 99 -33.05 -21.02 426.70 9.08 266.52 -476.69 100 59.06 122,76 26.70 -9.08 165.61 686.75 6 99 -248.51 -15.75 0.35 52.05 -155.59 -117.79 100 248.76 16.74 -0.35 -52.05 149.86 -145.13 7 99 82.88 57.31 28.06 51.31 -246.65 527.80 100 -82.62 -56.32 28.06 -51.31 -207.42 391.64 8 99 -210.10 -26.71 19.07 45.61 76.28 -436.20 100 229.71 103.43 19.07 -45.61 232.30 -616.83 9 99 38.44 28.09 1.71 45.06 7.98 47.99 100 18.83 48.63 1.71 -45.06 -35.67 -214.25 5 100 -10.31 96.57 5.49 5.06 -139.43 600.07 101 63.52 102.97 -5.49 5.06 -35.26 -701.97 6 100 -236.71 6.92 -10.67 50.12 -73.10 101.09 101 237.23 -4.97 10.67 -50.12 412.77 88.12 7 100 83.82 -6.53 -9.31 53.16 198.77 -245.91 101 -83.30 8.49 9.31 -53.16 97.45 6.92 8 100 -184.37 77.40 -4.03 41.26 -155.78 521.33 101 224.50 73.07 4.03 -41.26 284.05 -452.45 9 100 56.03 67.31 -3.01 43.54 48.13 261.09 101 -15.90 83.16 3.01 -43.54 47.56 -513.35 C:\at work\HORTON\6 BAYS\i3GG3ORR.anl Page 46 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 47 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL ) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MO~4-Y MOM-Z 112 114 116 118 319 5 5 101 19.30 119.69 -0.97 1.16 18.21 762.56 102 33.91 79.85 0.97 -1.16 12.66 -128.69 6 101 -229.28 -7.53 11.06 52.15 -419.59 -112.71 102 229.80 9.48 -11.06 -52.15 67.65 -157.99 7 101 23.62 -4.24 8.84 56.01 -98.78 -27.35 102 -23.10 6.19 -8.84 -56.01 -182.63 138.68 8 101 -157.48 83.07 7.59 39.96 -301.51 477.06 102 197.61 67.40 -7.59 -39.96 59.91 -227.66 9 101 32.19 85.54 5.93 42.85 -60.91 541.08 102 7.93 64.93 -5.93 -42.85 -127.81 -213.19 5 102 -17.28 77.21 -0.27 2.81 6.58 143.06 103 70.50 122.33 0.27 -2.81 2.07 -861.01 6 102 -140.49 8.05 -3.85 -1.87 -244.43 147.90 103 141.01 -6.10 3.85 1.87 366.80 77.17 7 102 4.66 7.31 -1.45 -3.45 -12.37 129.85 103 -4.14 -5.36 1.45 3.48 58.45 71.73 8 102 -116.98 64.30 -3.08 0.64 -178.55 230.00 103 157.11 86.17 3.08 -0.64 276.59 -578.07 9 102 -8.12 63.74 -1.28 0.55 -4.50 216.47 103 48.25 86.73 1.28 0.55 45.34 -582.15 5 103 -13.17 126.18 0.03 0.51 -1.00 840.61 27 66.39 73.36 -0.03 -0.51 0.00 0.00 6 103 35.63 -1.15 14.48 -0.44 -460.69 -67.57 27 -35.11 3.10 -14.48 0.44 0.00 0.00 7 103 -22.63 -0.97 2.51 -1.00 -79.78 -61.81 27 23.15 2.92 -2.51 1.00 0.00 0.00 8 103 18.33 93.19 10.88 0.04 -346.24 571.45 27 21.80 57.28 -10.88 -0.04 0.00 0.00 9 103 -25.36 93.33 1.90 -0.38 -60.56 575.78 27 65.49 57.14 -1.90 0.38 0.00 0.00 5 62 508.82 328.18 -20.19 -116.43 112.82 4552.46 63 -508.01 -327.42 20.19 116.43 98.71 -1118.85 6 62 -841.84 ~173.93 18.04 102.52 -58.23 -4767.69 63 842.33 174.38 -18.04 -102.52 -130.79 2943.45 7 62 -332.64 -414.34 23.69 132.39 -127.07 -3559.06 63 333.12 414.80 -23.69 -132.39 -121.08 -783.46 8 62 -263.48 106.73 -1.09 -7.41 38.03 -276.20 63 264.29 -105.97 1.09 7.41 -26.65 1390.17 9 62 118.42 -73.58 3.15 14.99 -13.60 630.27 63 -117.62 74.34 -3.15 -14.99 19.37 -1405.01 63 425.28 465.96 -10.36 -82.56 -129.01 1118.95 64 -386.99 -397.06 10.36 82.56 252.64 4029.20 C:\at work\HORTON\6 BAYS\13GG3ORR.anI Page 47 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 48 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL ) M~MBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 120 121 122 123 6 63 -828.95 -331.45 -2.00 59.61 167.00 -2943.63 64 829.73 332.86 2.00 -59.61 -143.11 -1019.15 7 63 -221.42 -444.92 10.31 90.54 148.70 783.44 64 222.19 446.32 -10.31 -90.54 -271.73 -6099.88 8 63 -313.39 89.56 -9.01 -15.08 31.86 -1390.23 64 342.44 -37.30 9.01 15.08 75.59 2146.96 9 63 142.26 4.46 0.23 8.12 18.14 1405.07 64 -113.21 47.80 -0.23 ~8.12 -20.88 -1663.59 5 64 284.36 476.93 27.37 -15.59 -263.12 -4029.04 65 -257.87 -373.33 -27.37 15.59 ~179.77 10909.05 6 64 -736.13 -437.05 -61.08 24.13 159.20 1019.03 65 736.67 439.16 61.08 -24.13 829.25 -8109.02 7 64 -131.54 -396.07 -32.72 16.30 286.91 6099.72 65 132.08 398.17 32.72 -16.30 242.67 -12526.39 8 64 -345.98 18.55 -25.99 6.80 -71.11 -2146.93 65 366.07 60.03 25.99 -6.80 491.79 1811.33 9 64 107.46 49.29 -4.73 0.93 24.67 1663.58 65 -87.38 29.29 4.73 -0.93 51.85 -1501.70 5 65 255.79 353.74 -6.05 -11.08 165.46 -10902.16 66 -201.61 -150.56 6.05 11.08 27.22 18926.61 6 65 -737.94 -263.17 -2.53 12.40 -678.37 8103.12 66 739.04 267.31 2.53 -12.40 758.93 -16544.29 7 65 -139.54 -228.40 7.46 11.09 -219.28 12519.42 66 140.64 232.53 -7.46 -11.09 -18.25 -19853.89 8 65 -367.74 60.75 -6.28 1.27 -388.99 -1810.76 66 408.84 93.36 6.28 -1.27 588.90 1291.95 9 65 81.06 86.83 1.21 0.29 -44.67 1501.47 66 -39.96 67.28 -1.21 -0.29 6.02 -1190.25 5 66 196.06 128.52 0.33 -7.04 ~10.11 -18923.94 67 141.88 74.66 -0.33 7.04 -0.29 19781.07 6 66 -741.85 43.90 3.14 8.18 -760.28 16541.77 67 742.95 48.03 -3.14 -8.18 660.24 -18004.54 7 66 -144.72 -9.17 2.19 6.97 -10.38 19851.41 67 145.82 13.31 -2.19 -6.97 -59.31 -20209.04 8 66 -413.92 62.13 2.59 1.04 -577.51 -1291.91 67 455.02 91.98 -2.59 -1.04 494.97 817.03 9 66 33.93 88.18 1.88 0.13 15.10 1190.32 67 7.16 65.93 1.88 -0.13 -44.69 -836.34 5 67 135.26 -96.69 0.02 -3.00 0.53 -19783.69 68 -81.08 299.87 -0.02 3.00 -0.23 13473.52 6 67 -745.72 175.38 -4.97 3.90 -655.76 18006.61 68 746.83 -171.24 4.97 -3.90 813.78 -12491.11 7 67 -148.38 210.06 -0.35 2.93 53.33 20211.85 68 149.48 -205.93 0.35 ~2.93 -42.25 -13592.51 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 48 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 49 MF/4BER END FORCES STRUCTURE TYPE = SPACE ALL UNITS APE -- POUN INCH (LOCAL ) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 124 125 126 127 8 67 -460.85 63.51 -3.71 0.75 -492.20 -817.37 68 501.95 90.60 3.71 -0.75 610.17 386.34 9 67 -12.85 89.52 -0.24 0.02 39.62 836.56 68 53.94 64.58 0.24 0.02 -31.85 -439.72 5 68 75.04 -322.00 -0.01 -0.54 0.33 -13480.68 11 -20.85 525.18 0.01 0.54 0.00 0.00 6 68 -748.44 394.75 31.29 0.90 -995.94 12497.15 11 749.54 -390.62 -31.29 -0.90 0.00 0.00 7 68 -154.92 429.40 -1.77 0.51 56.46 13599.73 11 156.02 ~425.26 1.77 -0.51 0.00 0.00 8 68 -506.49 64.89 23,46 0.28 -746.72 -386.99 11 547.59 89.21 23.46 -0.28 0.00 0.00 9 68 -61.35 90.88 -1.34 -0.01 42.58 439.95 11 102.45 63.23 1.34 0.01 0.00 0.00 5 69 505.89 350.55 0~09 -0.98 0.46 4611.63 70 -505.08 -349.79 -0.09 0.98 -1.39 -943.65 6 69 -837.57 -189.66 4.38 20.50 22.07 -4808.73 70 838.05 190.11 -4.38 -20.50 -67.93 2819.72 7 69 -330.67 -439.94 0.05 0.88 -0.58 -3626.88 70 331.15 440.40 0.05 -0.88 1.09 -983.83 8 69 -262.40 111.13 3.35 14.66 16.89 -264.14 70 263.20 -110.37 -3.35 -14.66 -51.96 1424.21 9 69 117.78 -76.58 0.03 -0.05 -0.10 622.25 70 -116.97 77.35 -0.03 0.05 -0.19 -1428.45 5 70 376.22 480.18 -0.51 -1.29 -7.19 943.60 71 -337.92 -411.28 0.51 1.29 13.32 4374.15 6 70 -790.23 -341.40 -10.41 -1.53 78.32 -2819.81 71 791.01 342.80 10.41 1.53 45.83 -1261.62 7 70 -167.86 -461.19 0.43 1.10 7.90 984.00 71 168.64 462.59 -0.43 -1.10 -13.05 -6494.57 8 70 -319.88 92.39 -8.18 2.08 53.53 -1424.32 71 348.92 -40.13 8.18 2.08 44.02 2214.85 9 70 146.90 2.55 -0.05 -0.10 0.72 1428.54 71 -117.85 49.71 0.05 0.10 -0.14 1709.86 5 71 220.39 474.45 0.13 0.00 -8.22 -4374.19 72 -193.91 -370.85 -0.13 0.00 6.14 11213.99 6 71 -690.35 -435.40 -42.72 11.37 -35.29 1261.66 72 690.89 437.51 42.72 -11.37 726.65 -8324.85 7 71 -58.76 -393.15 0.72 0.02 7.43 6494.61 72 59.30 395.26 0.72 -0.02 4.23 -12874.09 8 71 -357.96 17.99 -31.95 8.53 -32.42 -2214.86 72 378.05 60.58 31.95 -8.53 549.43 1870.24 9 71 115.73 49.68 -0.45 0.01 -0.38 1709.86 72 -95.65 28.90 0.45 -0.01 7.62 -1541.69 C:\at work\HORTON\6 BAYS\i3GG3ORR.ani Page 49 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 50 *4GBA WITH R3~FTER STIFFENER ME~ER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ABE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 128 129 130 131 132 5 5 72 195.31 351.72 0.45 -0.06 -1.72 -11213.95 73 -141.13 -148.54 -0.45 0.06 -12.69 19174.16 6 72 -698.21 -261.79 -6.47 2.93 -583.23 8324.84 73 699.31 265.93 6.47 -2.93 789.19 -16722,09 7 72 -68.12 226.05 -0.95 -0.01 -5.96 12874.04 73 69.22 230.19 0.95 0.01 36.10 -20133.89 8 72 -381.74 60.33 -4.53 2.16 -438.67 -1870.22 73 422.83 93.78 4.53 -2.16 582.70 1337.84 9 72 90.83 87.13 -0.38 -0.05 -5.72 1541.68 73 -49.74 66.98 0.38 0.05 17.89 1221.01 5 73 136.79 126.24 0.52 -0.05 11.50 -19174.18 74 -82.61 76.94 0.52 0.05 4.97 19958.59 6 73 -704.16 42.29 4.26 2.11 -780.99 16722.11 74 705.27 46.43 -4.26 -2.11 645.53 -18133.85 7 73 -74.19 -6.55 3.77 0.00 -42.81 20133.91 74 75.29 10.69 -3.77 0.00 -77.22 -20408.21 8 73 -428.57 61.68 2.82 1.55 -577.42 -1337.84 74 469.67 92.43 -2.82 -1.55 487.74 848.58 9 73 43.91 88.49 2.45 -0.04 -23.78 1221.01 74 -2.81 65.62 -2.45 0.04 -54.32 -857.18 5 74 77.01 -99.24 0.15 -0.05 -3.59 -19958.63 75 -22.83 302.42 -0.15 0.05 -1.16 13567.24 6 74 -708.86 177.21 -5.05 1.29 -643.92 18133.88 75 709.97 -173.07 5.05 -1.29 804.53 -12560.08 7 74 -78.88 212.95 -2.32 0.01 72.51 20408.25 75 79.98 -208.82 2.32 -0.01 1.38 -13696.98 8 74 -475.39 63.04 -3.68 0.94 -485.53 -848.59 75 516.48 91.07 3.68 -0.94 602.55 402.47 9 74 -2.90 89.84 -1.63 -0.02 51.79 857.19 75 43.99 64.27 1.63 0.02 0.19 -450.21 5 75 17.22 -324.72 -0.02 0.01 0.72 -13567.24 13 36.97 527.90 0.02 -0.01 0.00 0.00 6 75 -712.34 396.73 30.70 0.40 977.15 12560.06 13 713.44 -392.59 -30.70 0.40 0.00 0.00 7 75 -85.78 432.45 -0.24 -0.02 7.62 13696.99 13 86.89 -428.32 0.24 0.02 0.00 0.00 8 75 -521.29 64.41 23.01 0.31 -732.35 -402.48 13 562.39 89.70 -23.01 -0.31 0.00 0.00 9 75 -51.37 91.20 -0.20 -0.01 6.23 450.22 13 92.47 62.91 0.20 0.01 0.00 0.00 76 506.22 350.34 0.00 -0.03 77 -505.41 -349.58 0.00 0.03 0.01 4610.69 0.01 -944.96 C:\a£ work\HORTON\6 BAYS\13GG3ORR.anl Page 50 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 51 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS AR~ -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 133 134 135 136 6 76 -836.86 -189.57 4.58 20.30 21.67 -4807.76 77 837.34 190.03 -4.58 -20.30 -69.68 2819.66 7 76 -331.36 -439.69 -0.05 -0.39 0.42 -3626.09 77 331.84 440.15 0.05 0.39 0.12 -981.97 8 76 -261.62 111.04 3.44 15.21 16.26 -264.09 77 262.43 -110.28 -3.44 -15.21 -52.25 1423.22 9 76 117.50 -76.55 -0.04 40.31 0.32 622.16 77 -116.70 77.31 0.04 0.31 0.10 -1428.00 5 77 375.49 480.11 -0.01 -0.02 -0.02 944.92 78 -337.20 ~411.21 0.01 0.02 0.10 4372.04 6 77 -788.60 -341.34 410.74 -2.17 73.19 -2819.76 78 789.38 342.74 10.74 2.17 54.95 -1260.99 7 77 -167.38 -461.14 -0.13 -0.37 -0.14 982.13 78 168.16 462.54 0.13 0.37 1.66 -6492.14 8 77 -319.18 92.39 -8.06 -1.64 54.87 -1423.32 78 348.22 -40.13 8.06 1.64 41.28 2213.79 9 77 146.74 2.54 -0.10 -0.29 -0.12 1428.10 78 -117.69 49.72 0.10 0.29 1.32 -1709.56 5 78 219.84 474.45 -0.02 0.01 -0.09 -4372.09 79 -193.36 -370.85 0.02 -0.01 0.41 11211.91 6 78 -689.28 -435.40 -42.81 11.32 -40.47 1261.04 79 689.82 437.51 42.81 -12.32 733.24 -8324.26 7 78 58.10 -393.15 -0.27 0.06 -1.53 6492.18 79 58.64 395.25 0.27 -0.06 5.89 -12871.59 8 78 -357.55 17.99 -32.12 8.49 -30.42 -2213.80 79 377.64 60.58 32.12 -8.49 550.23 1869.18 9 78 115.83 49.68 -0.22 0.05 -1.22 1709.56 79 -95.74 28.89 0.22 0.05 4.72 -1541.33 5 79 193.57 351.74 0.02 0.00 -0.39 -11211.95 80 -139.39 -148.56 -0.02 0.00 -0.19 19172.82 6 79 696.90 261.80 -6.63 2.83 -584.63 8324.30 80 698.01 265.94 6.63 -2.83 795.68 -16721.84 7 79 -65.64 -226.08 -0.81 0.00 -2.54 12871.64 80 66.74 230.21 0.81 0.00 28.28 -20132.25 8 79 -382.01 60.33 -4.96 2.13 -438.76 -1869.17 80 423.11 93.77 4.96 -2.13 596.63 1337.06 9 79 91.44 87.13 -0.59 0.00 -2.19 1541.33 80 -50.34 66.98 0.59 0.00 21.07 -1220.75 5 80 134.33 126.26 -0.02 0.00 0.19 -19172.84 81 -80.15 76.92 0.02 0.00 0.43 19957.85 6 80 -702.51 42.30 5.32 2.03 -791.06 16721.87 81 703.61 46.43 -5.32 -2.03 621.75 -18133.83 7 80 -70.90 -6.57 3.93 0.00 -37.59 20132.27 81 72.00 10.71 -3.93 0.00 -87.63 -20407.26 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 51 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 52 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS A~E -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SEEAR-Z TORSION MOM-Y MOM-Z 137 138 139 140 8 80 -429.11 61.69 3.98 1.52 -593.16 -1337.05 81 470.21 92.42 -3.98 -1.52 466.62 848.06 9 80 44.60 88.48 2.94 0.00 -28.05 1220.75 81 -3.50 65.62 -2.94 0.00 -65.41 -857.01 5 81 74.47 -99.23 0.02 0.00 -0.43 -19957.83 82 -20.29 302.41 -0.02 0.00 -0.24 13566.98 6 81 -707.04 177.20 -6.12 1.23 -619.94 18133.81 82 708.14 -173.07 6.12 -1.23 814.74 -12560.17 7 81 -75.51 212.93 -4.23 0.00 88.50 20407.24 82 76.61 -208.80 4.23 0.00 46.14 -13696.61 8 81 -475.86 63.04 -4.58 0.92 -465.27 -848.06 82 516.96 91.06 4.58 -0.92 610.88 402.21 9 81 -2.21 89.84 ~3.16 0.00 66.06 857.01 82 43.31 64.27 3.16 0.00 34.42 -450.12 5 82 14.57 -324.71 -0.01 0.00 0.22 -13566.96 15 39.62 527.89 0.01 0.00 0.00 0.00 6 82 -710.92 396.73 30.94 0.40 -984.82 12560.16 15 712.02 -392.60 -30.94 -0.40 0.00 0.00 7 82 -82.23 432.44 1.30 0.00 -41.43 13696.60 15 83.33 -428.31 -1.30 0.00 0.00 0.00 8 82 -522.15 64.42 23.20 0.30 -738.46 402.21 15 563.25 89.69 -23.20 -0.30 0.00 0.00 9 82 -50.63 91.20 0.97 0.00 -30.91 450.12 15 91.73 62.91 -0.97 0.00 0.00 0.00 5 83 505.91 350.55 -0.09 0.93 -0.41 4611.63 84 -505.10 -349.79 0.09 -0.93 1.38 -943.67 6 83 -835.86 -189.80 4.63 19.73 21.43 -4808.31 84 836.35 190.26 -4.63 -19.73 -69.91 2817.77 7 83 -330.94 -439.93 -0.03 -1.59 0.88 -3626.90 84 331.42 440.38 0.03 1.59 -0.53 -983.64 8 83 -261.10 111.02 3.40 15.47 15.77 263.82 84 261.90 -110.26 -3.40 -15.47 -51.43 1422.74 9 83 117.60 -76.57 0.09 -0.52 0.36 622.23 84 -116.79 77.34 0.09 0.52 0.61 -1428.32 5 84 376.23 480.18 0.50 1.24 7.14 943.62 85 -337.93 -411.28 -0.50 -1.24 -13.11 4374.13 6 84 -788.22 -341.40 -10.97 -2.84 67.55 -2817.86 85 789.00 342.80 10.97 2.84 63.28 ~1263.60 7 84 -168.01 -461.19 -0.68 -1.81 -8.22 983.81 88 168.79 462.59 0.68 1.81 16.30 -6494.35 8 84 -318.36 92.39 -7.86 -1.23 55.83 1422.84 85 347.41 -40.13 7.86 1.23 37.97 2213.35 9 84 146.79 2.55 -0.15 -0.46 -1.00 1428.42 85 -117.75 49.71 0.15 0.46 2.73 1709.71 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 52 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 53 *4GBA WITH RAFTER STIFFENER MEMBER END FORCES STRUCTUB~ TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHE~-Z TORSION MOM-Y MOM-Z 141 142 143 144 145 5 5 85 220.39 474.45 -0.16 0.01 8.03 -4374.17 86 -193.91 -370.85 0.16 -0.01 -5.43 11213.97 6 85 -689.00 -435.40 -42.17 11.20 -45.16 1263.64 86 689.54 437.50 42.17 -11.20 727.54 -8326.79 7 85 -58.73 -393.15 0.19 0.07 -10.32 6494.40 86 59.27 395.26 -0.19 -0.07 7.18 -12873.86 8 85 -356.94 18.00 -31.74 8.41 -28.06 -2213.35 86 377.03 60.58 31.74 -8.41 541.73 1868.77 9 85 115.76 49.68 0.03 0.06 -1.93 1709.71 86 -95.67 28.90 -0.03 -0.06 1.45 -1541.54 5 86 195.29 351.72 -0.42 0.06 1.04 -11213.93 87 -141.11 -148.54 0.42 -0.06 12.30 19174.14 6 86 -697.89 -261.78 -7.55 2.78 -573.53 8326.77 87 699.00 265.91 7.55 2.78 813.96 -16723.58 7 86 -67.91 -226.05 -0.84 -0.02 1.70 12873.82 87 69.01 230.19 0,84 0.02 25.16 -20133.71 8 86 -381.51 60.34 -5.97 2.13 -429.39 -1868.75 87 422.61 93.77 5.97 -2.13 619.38 1336.71 9 86 90.98 87.13 -0.94 0.03 2.03 1541.53 87 -49.88 66.98 0.94 -0.03 27.78 -1220.89 5 87 136.76 126.24 0.48 0.05 -11.10 -19174.16 88 -82.58 76.94 -0.48 -0.05 -4.06 19958.58 6 87 -704.18 -42.28 7.35 1.98 -813.70 16723.61 88 705.28 46.41 -7.35 -1.98 579.76 -18134.88 7 87 -74.09 -6.55 4.50 -0.02 -37.66 20133.73 88 75.19 10.69 -4.50 0.02 105.61 -20408.08 8 87 -428.61 61.69 5.86 1.53 -618.31 -1336.71 88 469.70 92.42 -5.86 -1.53 431.88 847.81 9 87 43.96 88.49 3.72 0.02 -36.28 1220.88 88 -2.87 65.62 -3.72 -0.02 -82.15 -857.09 5 88 76.98 -99.24 -0.11 0.05 2.71 -19958.62 89 -22.80 302.42 0.11 -0.05 0.64 13567.23 6 88 708.67 177.23 -8.58 1.18 -576.73 18134.91 89 709.77 -173.09 8.58 -1.18 849.63 -12560.60 7 88 -78.78 212.95 -6.54 -0,03 111.72 20408.12 89 79.89 -208.81 6.54 0.03 96.26 13696.90 8 88 -475.26 63.05 -6.51 0.92 -430.59 -847.81 89 516.35 91.06 6.51 -0.92 637.69 402.07 9 88 -2.85 89.84 -4.98 0.01 85.75 857.10 89 43.94 64.27 4.98 -0,01 72.66 -450.15 89 17.19 -324.72 0.01 -0.01 -0.27 -13567.23 17 37.00 527.90 -0.01 0.01 0.00 0.00 C:\at work\HORTON\6 BAYS\I3GG3ORR.anl Page 53 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 54 MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT A~XIAL SSEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 146 147 148 149 6 89 -713.10 396.75 32.01 0.40 -1018.75 12560.59 17 714.20 -392.61 -32.01 -0.40 0.00 0.00 7 89 -85.48 432.45 3.00 0.01 -95.38 13696.91 17 86.59 -428.32 -3.00 -0.01 0.00 0.00 8 89 -521.88 64.42 24.01 0.30 -764.26 -402.07 17 562.98 89.69 -24.01 -0.30 0.00 0.00 9 89 -51.17 91.20 2.25 0.01 -71.73 450.16 17 92.27 62.91 -2.25 -0.01 0.00 0.00 5 90 508.96 328.29 20.07 115.82 -111.82 4552.73 91 508.15 -327.53 -20.07 -115.82 -98.43 -1117.90 6 90 -838.12 -172.66 -11.42 -70.74 104.70 -4759.75 91 838.60 173.12 11.42 70.74 14.96 2948.75 7 90 -334.44 -414.56 -23.35 -131.67 121.03 -3559.58 91 334.92 415.02 23.35 131.67 123.58 -785.26 8 90 -260.59 107.76 5.96 30.80 -2.45 -270.05 91 261.39 -107.00 -5.96 -30.80 -60.01 1394.83 9 90 117.17 ~73.66 -2.98 -14.89 9.80 630.08 91 -116.37 74.42 2.98 14.89 21.45 -1405.67 5 91 425.17 466.03 10.36 82.26 128.53 1118.00 92 -386.87 -397.13 -10.36 -82.26 -252.14 4030.98 6 91 -823.71 -330.27 -19.00 -67.84 -19.73 -2948.95 92 824.49 331.67 19.00 67.84 246.44 -999.66 7 91 -222.46 -445.05 -10.68 -91.00 -150.56 785.23 92 223.24 446.45 10.68 91.00 277.99 -6103.29 8 91 -309.54 90.50 -6.75 8.69 78.24 -1394.91 92 338.59 -38.24 6.75 -8.69 2.27 2162.87 9 91 141.39 4.41 -0.51 -8.68 -19.88 1405.73 92 112.34 47.85 0.51 8.68 25.93 -1664.85 5 92 284.03 476.92 -27.29 15.57 262.27 -4030.82 93 -257.54 -373.32 27.29 -15.57 179.29 10910.57 6 92 -736.99 -437.26 -18.96 2.29 -242.37 999.52 93 737.53 439.37 18.96 2.29 549.27 -8092.85 7 92 -130.95 -396.01 32.02 ~16.59 -289.25 6103.11 93 131.49 398.12 -32.02 16.59 228.97 -12528.94 8 92 -346.87 18.38 -33.98 9.56 8.12 -2162.85 93 366.95 60.19 33.98 -9.56 541.76 1824.55 9 92 107.67 49.32 4.26 -1.17 -27.04 1664.83 93 -87.58 29.26 -4.26 1.17 41.93 -1502.51 5 93 255.30 353.73 6.06 11.06 -165.19 -10903.65 94 -201.12 -150.55 -6.06 -11.06 -27.66 18927.76 6 93 -742.64 -263.30 -15.17 -6.73 -409.68 8087.04 94 743.74 267.43 15.17 6.73 892.38 -16532.13 7 93 137.76 -228.37 -9.76 -11.45 215.49 12521.91 94 138.86 232.50 9.76 11.45 95.21 -19855.40 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 54 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT 13GG -- PAGE NO, 55 *4GBA WITH P. AFTER STIFFENER MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- POUN INCH (LOCAL) MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 150 151 152 8 93 -371.62 60.65 -6.99 2.97 -426.85 ~1823.89 94 412.72 93.46 6.99 -2.97 649.26 1301.90 9 93 82.04 86.85 -2.94 -0.58 42.02 1502.26 94 -40.94 67.26 2.94 0.58 51.39 -1190.55 5 94 195.37 128.51 -0.39 7.02 10.47 -18925.22 95 -141.19 74.67 0.39 -7.02 1.88 19782.00 6 94 -745.71 -44.02 11.94 -4.13 -881.19 16529.61 95 746.82 48.16 -11.94 4.13 501.16 -17996.33 7 94 -142.24 -9.15 7.54 -7.25 -87.26 19852.96 95 143.35 13.28 -7.54 7.25 -152.75 -20209.81 8 94 -417.32 62.03 8.68 1.99 -653.31 -1301.95 95 458.42 92.08 -8.68 -1.99 377.23 823.85 9 94 35.28 88.19 5.38 -0.35 -57.87 1190.56 95 5.82 65.92 -5.38 0.35 -113.20 -836.26 5 95 134.60 -96.70 0.00 3.01 0.20 -19784.61 96 -80.42 299.88 0.00 -3.01 -0.27 13474.05 6 95 -748.54 175.25 -12.65 -1.46 -509.99 17998.40 96 749.64 -171.11 12.65 1.46 912.58 -12486.96 7 95 -146.79 210.08 -9.54 ~3.10 147.61 20212.62 96 147.89 -205.94 9.54 3.10 155.86 -13592.77 8 95 -463.44 63.41 -9.49 1.08 -382.35 -824.19 96 504.54 90.70 9.49 -1.08 684.24 389.83 9 95 -12.13 89.53 -7.15 -0.15 110.86 836.47 96 53.23 64.58 7.15 0.15 116.69 -439.53 5 96 74.25 -322.01 0.00 0.55 -0,03 -13481.08 19 -20.06 525.19 0.00 -0.55 0.00 0.00 6 96 -751.62 394.62 34.00 -0.11 -1081.91 12492.93 19 752.73 -390.49 -34.00 0.11 0.00 0.00 7 96 -152.18 429.40 4.94 -0.57 -157.35 13599.93 19 153.28 -425.27 -4.94 0.57 0.00 0.00 8 96 509.45 64.79 25.50 0.32 -811.45 -390.44 19 550.55 89.32 -25.50 -0.32 0,00 0.00 9 96 -59.87 90.87 3.71 -0.03 -118.03 439.81 19 100.97 63.23 -3.71 0.03 0.00 0.00 ************** END OF LATEST ANALYSIS RESULT ************** 178. PRINT MEMBER STRESSES ALL C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 55 of 89 SYSTEM 4E CLT-13GC *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM PAGE NO. 56 MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-y SHEAR-Z 5 .0 2.3 C 0.0 0.0 2.3 0.0 0.1 1.00 2.3 C 1.0 0.0 3.3 0.0 0.1 6 .0 1.4 C 0.0 0.0 1.4 0.1 0.1 1.00 1.4 C 1.0 0.4 2.8 0.1 0.1 7 .0 1.4 C 0.0 0.0 1.4 0.0 0.0 1.00 1.4 C 0.6 0.2 2.1 0.0 0.0 8 .0 2.3 C 0.0 0.0 2.3 0.1 0.1 1.00 2.3 C 1.5 0.3 4.0 0.1 0.1 9 .0 2.3 C 0.0 0.0 2.3 0.0 0.0 1.00 2.3 C 0.3 0.1 2.7 0.0 0.0 5 .0 156.0 C 0.0 0.0 156.0 0.0 0.4 1.00 151.4 C 4.4 0.0 155.8 0.0 0.4 6 .0 30.9 T 0.0 0.0 30.9 1085.0 0.4 1.00 33.7 T 4.7 4888.1 4926.4 1085.0 0.4 7 .0 31.4 T 0.0 0.0 31.4 1008.9 1.1 1.00 34.1 T 14.1 4545.2 4593.5 1008.9 1.1 8 .0 84.6 C 0.0 0.0 84.6 813.8 0.5 1.00 80.0 C 6.7 3666.0 3752.7 813.8 0.5 9 .0 84.3 C 0.0 0.0 84.3 756.7 0.6 1.00 79.7 C 7.4 3488.9 3496.0 756.7 0.6 5 .0 140.2 C 0.0 0.0 140.2 0.0 0.9 1.00 135.7 C 11.3 0.0 147.0 0.0 0.9 6 .0 34.4 T 0.0 0.0 34.4 934.7 0.8 1.00 37.1 T 9.7 4210.8 4257.7 934.7 0.8 7 .0 35.9 T 0.0 0.0 35.9 869.0 2.4 1.00 38.6 T 30.0 3915.1 3983.7 869.0 2.4 8 .0 70.8 C 0.0 0.0 70.8 701.0 1.3 1.00 66.2 C 15.6 3158.1 3239.9 701.0 1.3 9 .0 69.7 C 0.0 0.0 69.7 651.8 1.1 1.00 65.1 C 14.2 2936.3 3015.7 651.8 1.1 5 .0 136.7 C 0.0 0.0 136.7 0.0 1.00 132.1 C 17.0 0.1 149.2 0.0 6 .0 32.0 T 0.0 0.0 32.0 784.0 1.00 34.7 T 15.1 3531.8 3581.6 784.0 7 .0 31.9 T 0.0 0.0 31.9 728.8 1.00 34.7 T 46.3 3283.3 3364.3 728.8 8 .0 70.8 C 0.0 0.0 70.8 588.0 1.00 66.2 C 23.7 2648.8 2738.6 588.0 9 .0 70.8 C 0.0 0.0 70.8 546.6 1.00 66.2 C 22.3 2462.6 2551.1 546.6 3.7 3,7 5 .0 144.3 C 0.0 0.0 144.3 0.0 0.8 1.00 139.8 C 9.5 0.1 149.3 0.0 0.8 6 .0 32.4 T 0.0 0.0 32.4 655.8 1.8 1.00 35.1 T 22.5 2954.5 3012.1 655.8 1.8 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 56 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM PAGE NO. 57 }{EMBER STRESSES ;iLL UNITS ARE POUN/SQ INCH MEMB LD SECT ;~XIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 7 .0 48.1 T 0.0 0.0 48.1 609.8 3.6 1.00 50.8 T 44.9 2747.2 2842.9 609.8 3.6 8 .0 76.5 C 0.0 0.0 76.8 491.9 1.9 1.00 71.9 C 23.8 2215.9 2311.5 491.9 1.9 9 .0 64.7 C 0.0 0.0 64.7 457.3 2.2 1.00 60.1 C 26.8 2060.3 2147.2 457.3 2.2 5 .0 163.6 C 0.0 0.0 163.6 3.1 3.0 1.00 159.0 C 119.0 112.5 390.6 3.1 3.0 6 .0 346.6 T 0.0 0.0 346.6 2.6 1.2 1.00 349.3 T 48.1 93.1 490.5 2.6 1.2 7 .0 79.8 T 0.0 0.0 79.8 1.2 2.4 1.00 82.5 T 94.3 42.9 219.7 1.2 2.4 8 .0 147.7 T 0.0 0.0 147.7 0.3 3.1 1.00 152.3 T 122.3 12.6 287.1 0.3 3.1 9 .0 52.4 C 0.0 0.0 52.4 3.1 4.0 1.00 47.8 C 156.9 114.6 319.4 3.1 4.0 5 .0 130.1 C 145.6 165.9 441.6 91.9 79.2 1.00 129.4 C 364.6 378.0 871.9 91.9 79.2 6 .0 227.1 T 0.2 118.6 346.0 40.3 58.1 1,00 227.6 T 373.9 120.0 721.5 40.3 58.1 7 .0 89.4 T 82.7 4.2 176.3 64.3 65.8 1.00 89.9 T 506.8 384.8 981.4 64.3 65.8 8 .0 77.7 T 105.2 32.3 215.3 36,5 13.8 1.00 78.4 T 16.4 183.9 278.8 36.5 13.8 9 .0 25.6 C 167.4 124.5 317.5 18.5 8.0 1.00 24.9 C 116.1 14.7 155.6 18.5 8.0 5 .0 121.3 C 340.6 377.9 839.9 16.9 2.0 1.00 120.4 C 356.9 509.2 986.5 17.5 2.0 6 .0 184.6 T 321.3 119.9 625.9 11.0 23.1 1.00 185.2 T 513.1 202.3 900.6 10.6 23.1 7 .0 79.6 T 502.6 384.7 966.9 14.2 40.5 1.00 80.1 T 166.2 275.2 521.4 14.5 40.5 8 .0 51.5 T 5.6 183.9 241.0 4.8 15.9 1.00 52.4 T 126.3 222.5 401.2 5.3 15.9 9 .0 27.3 C 130.4 14.7 172.4 23.7 31.8 1.00 26.4 C 133.9 167.9 328.1 24.2 31.8 5 .0 1.7 C 0.2 0.0 1.9 0.0 0.4 1.00 1.7 C 3.2 0.0 4.9 0.0 0.4 6 .0 1.0 C 1.4 0.4 2.8 0.1 0.2 1.00 1.0 C 0.1 0.3 1.3 0.1 0.2 7 .0 1.0 C 0.0 0.1 1.2 0.1 0.2 1.00 1.0 C 1.7 0.5 3.2 0.1 0.2 8 .0 1.7 C 0.9 0.3 2.9 0.0 0.2 1.00 1.7 C 2.3 0.2 4.2 0.0 0.2 9 .0 1.7 C 0.1 0.1 1.9 0.1 0.1 1.00 1.7 C 1.1 0.4 3.1 0.1 0.1 C: \at work\HORTON\6 HAYS\13GG3ORR.anl Page 57 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 58 MEMBER STRESSES ALL UNITS A~E POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SSEAR-Z 5 .0 137.8 C 4.2 0.0 142.0 0.0 0.2 1.00 134.4 C 2.6 0.0 137.1 0.0 0.2 6 .0 42.0 T 6.4 4887.5 4935.9 407.1 2.2 1.00 44.0 T 14.0 3536.0 3594.0 407.1 2.2 7 .0 42.8 T 14.6 4544.8 4602.1 378.6 2.7 1.00 44.8 T 10.0 3287.9 3342.7 378.6 2.7 8 .0 66.3 C 7.8 3665.6 3739.7 305.3 1.8 1.00 62.9 C 8.6 2652.0 2723.5 305.3 1.8 9 .0 65.8 C 7.9 3408.6 3482.3 283.9 1.9 1.00 62.4 C 9.4 2466.0 2537.8 283.9 1.9 5 .0 121.4 C 11.1 0.0 132.5 0.0 2.0 1.00 118.0 C 7.3 0.1 125.4 0.0 2.0 6 .0 45.4 T 12.0 4210.7 4268.1 557.9 4.2 1.00 47.4 T 26.1 2358.7 2432.2 557.9 4.2 7 .0 47.2 T 29.4 3915.2 3991.8 518.8 5.8 1.00 49.2 T 23.4 2192.9 2265.5 518.8 5.8 8 .0 52.1 C 17.1 3158.0 3227.3 418.4 4.6 1.00 48.8 C 25.0 1769.0 1842.8 418.4 4.6 9 .0 50.8 C 14.0 2936.4 3001.2 389.1 2.8 1.00 47.4 C 12.1 1644.7 1704.2 389.1 2.8 5 .0 117.9 C 19.1 0.1 137.1 0.0 3.6 1.00 114.5 C 14.2 0.2 128.9 0.0 3.6 6 .0 43.1 T 16.8 3531.6 3591.6 708.6 8.6 1.00 45.2 T 34.1 1179.1 1258.4 708.6 5.6 7 .0 43.3 T 48.8 3283.4 3375.5 659.0 10.0 1.00 45.3 T 42.6 1095.6 1183.5 659.0 10.0 8 .0 52.1 C 26.5 2648.6 2727.2 531.5 6.8 1.00 48.7 C 36.0 884.2 968.9 531.5 6.8 9 .0 51.9 C 22.7 2462.6 2537.2 494.3 4.8 1.00 48.6 C 21.5 821.8 891.9 494.3 4.8 5 .0 123.9 C 36.7 0.0 160.6 0.0 4.0 1.00 120.5 C 0.0 0.0 120.5 0.0 4.0 6 .0 42.7 T 1.5 2954.5 2998.7 890.0 0.2 1.00 44.8 T 0.0 0.0 44.8 890.0 0.2 7 .0 57.8 T 67.7 2747.3 2872.8 827.6 7.4 1.00 59.8 T 0.0 0.0 59.8 827.6 7.4 8 .0 57.3 C 27.8 2215.9 2301.0 667.5 3.0 1.00 53.9 C 0.0 0.0 53.9 667.5 3.0 9 .0 46.0 C 24.1 2060.5 2130.6 620.7 2.6 1.00 42.6 C 0.0 0.0 42.6 620.7 2.6 5 .0 106.7 C 13.7 0.1 120.5 0.1 6.3 1.00 105.9 C 0.0 0.0 105.9 0.1 6.3 6 .0 49.6 T 41.3 1179.1 1270.0 1492.2 19.0 1.00 50.1 T 0.0 0.0 50.1 1492.2 19.0 C:\at work\HORTON\6 BAYS\i3GG3ORR.anl Page 58 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 59 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 7 .0 49.4 T 36.2 1096.1 1181.8 3387.1 16.6 1.00 49.9 T 0.0 0.0 49.9 1387,1 16.6 8 .0 41.0 C 41.1 884.3 966.3 1119.0 18.9 1.00 40.2 C 0.0 0.0 40.2 1119.0 18.9 9 .0 41.1 C 17.1 822.1 880.3 1040.4 7.8 1.00 40.3 C 0.0 0.0 40.3 1040.4 7.8 5 .0 108.8 C 2.4 0.1 111.3 0.1 0.6 1.00 107.2 C 0.0 0.0 107.2 0.1 0.6 6 .0 52.7 T 30.4 2358.4 2441.4 1492.3 7.0 1.00 53.7 T 0.0 0.0 53.7 1492.3 7.0 7 .0 54.0 T 19.2 2192.6 2265.9 1387.4 4.4 1.00 55.0 T 0.0 0.0 55.0 1387.4 4.4 8 .0 39.7 C 24.7 1768.7 1833.1 1119.2 5.7 1.00 38.1 C 0.0 0.0 38.1 1119.2 5.7 9 .0 38.8 C 12.5 1644.5 1695.8 1040.6 2.9 1.00 37.1 C 0.0 0.0 37.1 1040.6 2.9 5 .0 124.7 C 0.9 0.1 125.6 0.0 0.1 1.00 122.3 C 0.0 0.0 122.3 0.0 0.1 6 .0 50.2 T 17.4 3536.9 3604.4 1492.0 2.7 1.00 51.6 T 0.0 0.0 51.6 1492.0 2.7 7 .0 50.8 T 7.7 3288.8 3347.4 1387.4 1.2 1.00 52.3 T 0.0 0.0 52.3 1387.4 1.2 8 .0 53.2 C 13.8 2652.6 2719.7 1119.0 2.1 1.00 50.8 C 0.0 0.0 50.8 1119.0 2.1 9 .0 52.7 C 5.0 2466.7 2524.3 1040.5 0.8 1.00 50.3 C 0.0 0.0 50.3 1040.5 0.8 5 .0 1.6 C 3.3 0.0 4.9 0.0 0.4 1.00 1.6 C 0.0 0.0 1.6 0.0 0.4 6 .0 1.0 C 0.6 0.4 1.9 0.1 0.1 7 .0 1.0 C 1.8 0.5 3.3 0.2 0.2 1.00 1.0 C 0.0 0.0 1.0 0.2 0.2 8 .0 1.6 C 2.8 0.3 4.7 0.1 0.3 1.00 1.6 C 0.0 0.0 1.6 0.1 0.3 5 .0 549.7 C 0.0 0.0 549.7 188.4 2.0 1.00 545.2 C 79.4 6866.4 7491.0 188.4 2.0 6 .0 663.9 T 0.0 0.0 663.9 87.6 7.7 1.00 666.7 T 306.2 3193.0 4165.8 87.6 7.7 7 .0 470.7 T 0.0 0.0 470.7 262.2 1.2 1.00 473.5 T 49.1 9555.9 10078.5 262.2 1.2 8 .0 106.8 T 0.0 0.0 106.8 70.7 7.2 1.00 111.4 T 287.1 2574.9 2973.5 70.7 7.2 9 .0 38.0 C 0.0 0.0 38.0 60.3 0.5 1.00 33.4 C 20.7 2197.3 2251.4 60.3 0.5 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 59 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG *4GBA WITH R3%FTER STIFFE~FER PAGE NO. 60 MEMBER STP. ESSES ALL UNITS APsE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 20 22 23 5 .0 528.4 C 118.7 6869.0 7516.2 188.6 71.5 1.00 527.7 C 341.9 7985.7 8855.2 188.6 71.5 6 .0 684.8 T 284.4 3193.7 4162.8 440.2 23.9 1.00 685.3 T 438.0 5800.0 6923.2 440.2 23.9 7 .0 480.7 T 103.0 9559.9 10143.6 116.6 80.8 1.00 481.1 T 417.9 8869.5 9768.6 116.6 80.8 8 .0 134.0 T 299.2 2576.3 3009.4 193.6 33.9 1.00 134.7 T 81.0 1429.8 1645.5 193.6 33.9 9 .0 19.1 C 8.7 2198.4 2226.2 224.0 8.9 1.00 18.4 C 65.9 872.4 956.7 224.0 8.9 5 .0 535.1 C 301.7 7985.7 8822.5 116.8 1.2 1.00 534.1 C 311.5 7096.8 7942.4 116.3 1.2 6 .0 737.6 T 426.5 5800.1 6964.2 214.2 27.8 1.00 738.2 T 196.1 7432.3 8366.6 213.9 27.8 7 .0 447.9 T 351.2 8869.6 9668.6 435.4 0.3 1.00 448.4 T 349.0 5548.2 6345.7 435.7 0.3 8 .0 167.7 T 101.4 1429.7 1698.8 244.2 21.7 1.00 168.6 T 78.4 430.6 677.6 243.7 21.7 9 .0 49.7 C 44.9 872.4 967.0 243.0 1.0 1.00 48.7 C 36.2 982.5 1067.5 243.5 1.0 5 .0 598.2 C 0.0 0.0 598.2 194.5 0.4 1.00 593.6 C 17.4 7089.2 7700.2 194.5 0.4 6 .0 701.6 T 0.0 0.0 701.6 92.0 10.4 1.00 704.4 T 414.1 3351.4 4469.8 92.0 10.4 7 .0 523.5 T 0.0 0.0 523.5 269.2 0.7 1.00 526.2 T 27.8 9809.6 10363.6 269.2 0.7 8 .0 100.1 T 0.0 0.0 100.1 71.8 7.5 1.00 104.7 T 298.0 2617.4 3020.0 71.8 7.5 9 .0 33.5 C 0.0 0.0 33.5 61.1 0.2 1.00 29.0 C 8.2 2226.3 2263.5 61.1 0.2 5 .0 575.2 C 48.0 7089.5 7712.7 194.6 4.9 1.00 574.4 C 16.7 8241.4 8832.5 194.6 4.9 6 .0 716.6 T 436.8 3351.6 4505.0 444.4 30.8 1.00 717.0 T 238.6 5983.1 6938.8 444.4 30.8 7 .0 534.9 T 60.0 9810.0 10404.9 109.8 6.1 1.00 535.3 T 21.0 9159.6 9716.0 109.8 6.1 8 .0 124.0 T 292.8 2617.4 3034.2 192.5 19.5 1.00 124.7 T 166.9 1477.6 1769.2 192.5 19.5 9 .0 12.3 C 10.3 2226.3 2248.9 223.2 1.0 1.00 11.6 C 3.7 904.9 920.1 223.2 1.0 5 .0 570.1 C 42,6 8241,4 8854.1 138,2 1.6 1.00 569.2 C 29.6 7189.2 7788.0 137.7 1.6 6 .0 761.1 T 252.2 5983.2 6996.4 198.6 31.3 1.00 761.6 T 7.2 7496.4 8265.2 198.3 31.3 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 60 of 89 SYSTEM 4E CLT-13GG *4GBA WITH P~AFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM PAGE NO. 61 MEMBER STRESSES ALL UNITS A~E POUN/SQ INCH MEMB LD SECT ;~XI~L BEND-Y BEND-Z 24 25 26 27 7 .0 488.5 T 47.8 9159.5 9695.8 459.5 1.6 1.00 489.1 T 34.8 5654.2 6178.0 459.8 1.6 8 .0 159.9 T 158.3 1477.5 1795.6 248.0 22.3 1.00 160.8 T 26.8 411.7 599.3 247.5 22.3 9 .0 44.5 C 5.0 904.8 954.3 245.6 0.0 1.00 43.6 C 4.7 970.0 1018.2 246.1 0.0 5 .0 599.4 C 0.0 0.0 599.4 194.5 0.0 1.00 594.8 C 0.7 7088.4 7683.9 194.5 0.0 6 .0 703.6 T 0.0 0.0 703.6 92.0 10,3 1.00 706.3 T 409.4 3351.9 4467.7 92.0 10.3 7 .0 524.4 T 0.0 0.0 524.4 269.2 0.0 1.00 527.1 T 1.7 9808.4 10337.2 269.2 0.0 8 .0 100.6 T 0.0 0.0 100.6 71.8 7.7 1.00 105.2 T 306.6 2616.4 3028.2 71.8 7.7 9 .0 33.8 C 0.0 0.0 33.8 61.1 0.0 1.00 29.2 C 0.8 2225.9 2255.9 61.1 0.0 5 .0 576.0 C 0.7 7088.5 7665.1 194.5 0.1 1.00 575.2 C 0.2 8240.2 8815.6 194.5 0.1 6 .0 717.0 T 409.1 3352.0 4478.2 444.5 27.6 1.00 717.5 T 231.1 5983.5 6932.2 444.5 27.6 7 .0 535.8 T 1.5 9808.4 10345.8 109.9 0.3 1.00 536.3 T 0.5 9157.8 9694.6 109.9 0.3 8 .0 123.7 T 306.3 2616.4 3046.5 192.6 20.7 1.00 124.5 T 173.2 1476.3 1774.0 192.6 20.7 9 .0 12.2 C 0.7 2225.9 2238.8 223.2 0.2 1.00 11.4 C 0.6 904.3 916.3 223.2 0.2 5 .0 572.3 C 0.2 8240.2 8812.8 138.3 0.0 1.00 571.4 C 0.1 7187.8 7759.2 137.7 0.0 6 .0 762.1 T 223.4 5983.6 6969.2 198.3 30.0 1.00 762.7 T 25.4 7494.9 8282.9 198.0 30.0 7 .0 491.3 T 0.4 9157.7 9649.4 459.4 0.1 1.00 491.8 T 1.1 5652.9 6145.9 459.7 0.1 8 .0 159.0 T 167.4 1476.2 1802.7 247.8 22.5 1.00 160.0 T 19.1 411.6 590.7 247.3 22.5 9 .0 44.1 C 0.5 904.3 948.8 245.5 0.1 1.00 43.2 C 0.9 969.8 1013.9 246.0 0.1 5 .0 598.2 C 0.0 0.0 598.2 1.00 593.6 C 16.0 7089.1 7698.7 6 .0 703.5 T 0.0 0.0 703.5 1.00 706.3 T 393.6 3353.6 4453.5 7 .0 523.4 T 0.0 0.0 523.4 1.00 526.1 T 23.2 9809.4 10358.7 8 .0 101.5 T 0.0 0.0 101.5 1.00 106.1 T 306.8 2615.7 3028.6 9 .0 33.6 C 0.0 0.0 33.6 1.00 29.1 C 5.8 2226.1 2261.0 194.5 0.4 194.5 0.4 92.0 9.9 92.0 9.9 269.2 0.6 269.2 0.6 71.8 7.7 71.8 7.7 61.1 0.1 61.1 0.1 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 6I of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 62 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SEEAR-Z 28 29 30 32 5 .0 575.2 C 46.4 7089.5 7711.1 194.6 4.7 1.00 574.5 C 16.1 8241.4 8831.9 194.6 4.7 6 .0 716.5 T 373.3 3353.8 4443.6 444.5 24.0 1.00 716.9 T 218.5 5985.6 6921.0 444.5 24.0 7 .0 534.9 T 55.3 9809.7 10399.9 109.8 5.3 1.00 535.4 T 21.1 9159.4 9715.8 109.8 5.3 8 .0 123.9 T 313.6 2615.8 3053.2 192.6 21.4 1.00 124.6 T 175.5 1475.6 1775.7 192.6 21.4 9 .0 12.3 C 7.8 2226.2 2246.3 223.2 0.6 1.00 11.5 C 4.2 904.7 920.4 223.2 0.6 5 .0 570.1 C 41.9 8241.4 8853.4 138.2 1.5 1.00 569.2 C 29.2 7189.2 7787.7 137.7 1.5 6 .0 760.1 T 192.8 8985.7 6938.7 198.2 28.7 1.00 760.7 T 45.5 7495.7 8302.0 197.8 28.7 7 .0 488.7 T 46.9 9159.3 9694.9 459.4 1.4 1.00 489.3 T 35.5 5654.2 6179.0 459.8 1.4 8 .0 159.2 T 174.9 1475.5 1809.7 247.7 22.6 1.00 160.1 T 13.0 411.2 584.3 247.1 22.6 9 .0 44.4 C 4.9 904.6 953.8 245.5 0.1 1.00 43.5 C 5.4 969.9 1018.8 246.1 0.1 5 .0 550.0 C 0.0 1.00 545.4 C 80.4 6 .0 669.1 T 0.0 1.00 671.8 T 436.8 7 .0 470.8 T 0.0 1.00 473.6 T 57.5 8 .0 110.6 T 0.0 1.00 115.1 T 269.3 9 .0 38.1 C 0.0 1.00 33.5 C 15.1 0.0 550.0 188.5 2.0 6867 · 6 7493.4 188 · 5 2 · 0 0.0 669.1 87.4 11.0 3186 · 2 4294 . 8 87.4 11 · 0 0.0 470.8 262.3 1.4 9557.9 10088.9 262.3 1.4 0.0 110.6 70.8 6.8 2580 . 9 2965 .4 70.8 6. 8 0.0 38.1 60.3 0.4 2197.9 2246.6 60.3 0.4 5 .0 528.8 C 119.9 6870.1 7518.8 188.6 71.2 1.00 528.0 C 338.5 7987.0 8853.5 188.6 71.2 6 .0 681.5 T 483.0 3186.9 4351.4 440.0 78.2 1.00 681.9 T 20.8 5792.2 6495.0 440.0 78.2 7 .0 481.6 T 113.8 9561.7 10157.1 116.6 80.8 1.00 482.1 T 406.8 8871.6 9760.5 116.6 80.8 8 .0 331.3 T 275.4 2582.1 2988.8 193.5 7.1 1.00 132.0 T 229.5 1436.5 1798.0 193.5 7.1 9 .0 18.6 C 1.5 2198.9 2219.0 223.9 9.1 1.00 17.9 C 60.0 873.0 950.9 223.9 9.1 5 .0 535.4 C 298.1 7987.1 8820.6 117.0 1.3 1.00 534.5 C 309.0 7097.2 7940.7 116.4 1.3 6 .0 734.4 T 28.3 5792.3 6555.1 213.6 34.9 1.00 735.0 T 261.2 7419.9 8416.0 213.3 34.9 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 62 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG _r PAGE NO. 63 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS APE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND- Z C~INED SHEA/~-Y SHEAR-Z 33 34 35 36 7 .0 449.7 T 335.0 8871.6 9656.3 435.5 0.2 1.00 450.2 T 336.9 5549.0 6336.1 435.8 0.2 8 .0 165.0 T 237.1 1436.5 1838.6 243.8 25.2 1.00 165.9 T 27.9 421.0 614.8 243.3 25.2 9 .0 48.6 C 35.4 873.0 956.9 243.0 0.8 1.00 47.6 C 28.9 982.2 1058.7 243.5 0.8 5 .0 2.3 C 0.0 0.0 2.3 0.0 0.0 1.00 2.3 C 0.5 0.0 2.8 0.0 0.0 6 .0 1.4 C 0.0 0.0 1.4 0.1 0.1 1.00 1.4 C 1.3 0.4 3.1 0.1 0.1 7 .0 1.4 C 0.0 0.0 1.4 0.1 0.0 1.00 1.4 C 0.3 0.2 1.9 0.1 0.0 8 .0 2.3 C 0.0 0.0 2.3 0.1 0.1 1.00 2.3 C 1.4 0.3 4.0 0.1 0.1 9 .0 2.3 C 0.0 0.0 2.3 0.0 0.0 1.00 2.3 C 0.6 0.2 3.0 0.0 0.0 5 .0 231.9 C 0.0 0.0 231.9 0.2 0.1 1.00 227.3 C 1.7 0.8 229.7 0.2 0.1 6 .0 47.3 T 0.0 0.0 47.3 1136.5 0.0 1.00 50.0 T 0.6 5119.8 5170.3 1136.5 0.0 7 .0 51.2 T 0.0 0.0 51.2 1422.7 0.8 1.00 54.0 T 9.5 6409.3 6472.8 1422.7 0.8 8 .0 124.4 C 0.0 0.0 124.4 852.5 0.1 1.00 119.9 C 1.6 3840.4 3961.9 852.5 0.1 9 .0 121.5 C 0.0 0.0 121.5 1067.2 0.5 1.00 116.9 C 5.9 4807.5 4930.3 1067.2 0.5 5 .0 208.9 C 0.0 0.0 208.9 0.2 5.9 1.00 204.3 C 72.9 0.8 278.0 0.2 5.9 6 .0 50.3 T 0.0 0.0 50.3 1099.6 10.5 1.00 53.0 T 130.1 4953.9 5137.0 1099.6 10.5 7 .0 51.1 T 0.0 0.0 51.1 1183.9 14.5 1.0O 53.8 T 179.4 5333.3 5566.5 1183.9 14.5 8 .0 106.6 C 0.0 0.0 106.6 824.8 12.1 1.00 102.0 C 150.6 3715.9 3968.6 824.8 12.1 9 .0 106.0 C 0.0 0.0 106.0 888.0 6.6 1.00 101.4 C 81.5 4000.5 4183.5 888.0 6.6 5 .0 144.1 C O.0 0.0 144.1 0.0 4.5 1.00 139.5 C 56.1 0.0 195.7 0.0 4.5 6 .0 5.8 T 0.0 0.0 5.8 519.9 9.5 1.00 8.5 T 117.8 2342.3 2468.6 519.9 9.5 7 .0 53.2 T 0.0 0.0 53.2 609.8 12.7 1.00 56.0 T 158.0 2747.4 2961.3 609.8 12.7 8 .0 96.3 C 0.0 0.0 96.3 389.9 10.4 1.00 91.7 C 129.1 1756.7 1977.9 389.9 10.4 9 .0 60.7 C 0.0 0.0 60.7 457.4 6.3 1.00 56.1 C 77.7 2060.5 2194.3 457.4 6.3 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 63 of 89 Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 64 SYSTEM 4E CLT-13GG *4GBA WIT~ RAFTER STIFFENER MEMBER STP. ESSES ALL UNITS ABE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 37 39 43 44 5 .0 154.5 C 0.0 0.0 154.5 0.1 3.1 1.00 149.9 C 121.1 3.7 274.8 0.1 3.1 6 .0 53.6 C 0.0 0.0 53.6 7.7 7.5 1.00 50.8 C 298.1 279.4 628.3 7.7 7.5 7 .0 56.2 T 0.0 0.0 56.2 8.9 1.8 1.00 58.9 T 69.6 326.1 454.6 8.9 1.8 8 .0 145.8 C 0.0 0.0 145.8 5.8 3.4 1.00 141.3 C 135.8 211.6 488.7 5.8 3.4 9 .0 63.5 C 0.0 0.0 63.5 6.7 3.5 1.00 58.9 C 139.9 242.5 441.4 6.7 3.5 5 .0 119.6 C 147.2 46.4 313.3 74.3 78.1 1.00 118.9 C 355.8 393.4 868.1 74.3 78.1 6 .0 97.9 T 308.9 289.1 695.9 23.2 53.0 1.00 98.4 T 32.6 151.5 282.5 23.2 53.0 7 .0 62.7 T 60.7 298.7 422.2 19.3 57,2 1.00 63.2 T 429.0 413.0 905.2 19.3 57.2 8 .0 11.6 C 125.1 182.3 319.1 36.5 16.8 1.00 10.8 C 233.2 398.7 642.7 36.5 16.8 9 .0 38.0 C 152.1 258.5 448.6 39.5 13.7 1.00 37.2 C 64.1 24.7 126.1 39.5 13.7 5 .0 109.2 C 332.9 393.4 835.4 6.0 1.5 1.00 108.2 C 345.7 440.9 894.8 6.5 1.5 6 .0 136.3 T 52.1 151.5 339.9 45.9 11.0 1.00 136.8 T 39.3 197.4 373.6 45.6 11.0 7 .0 48.7 T 435.0 412.9 896.6 42.0 46.7 1.00 49.2 T 47.2 91.4 187.9 42.3 46.7 8 .0 24.1 T 201.9 398.6 624.6 29.4 9.4 1.00 25.0 T 279.9 176.5 481.4 28.9 9.4 9 .0 41.6 C 85.3 24.7 151.6 36.5 36.2 1.00 40.7 C 215.0 256.0 511.6 37.1 36.2 5 .0 1.7 C 1.0 0.0 2.7 0.0 0.2 1.00 1.7 C 0.5 0.0 2.2 0.0 0.2 6 .0 1.0 C 0.9 0.4 2.3 0.1 0.1 1.00 1.0 C 1.9 0.2 3.2 0.1 0.1 7 .0 1.0 C 0.0 0.1 1.2 0.2 0.1 1.00 1.0 C 0.8 0.7 2.5 0.2 0.1 8 .0 1.7 C 1.3 0.3 3.3 0.0 0.0 1.00 1.7 C 1.1 0.2 3.0 8.0 0.0 9 .0 1.7 C 0.6 0.1 2.4 0.1 0.0 1.00 1.7 C 0.3 0.5 2.5 0.1 0.0 5 .0 207.0 C 8.2 0.8 216.0 0.2 2.3 1.00 203.6 C 12.7 1.3 217.7 0.2 2.3 6 .0 62.2 T 34.5 5119.0 5215.7 637.9 7.4 1.00 64.2 T 33.1 3001.2 3098.5 637.9 7.4 C: \at work\HORTON\6 BAYS\13GG3ORB.anl Page 64 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 65 *4GBA WITH RAFTER STIFFENER ME~ER STP. ESSES ALL UNITS ARE POUN/SQ INCH 45 46 47 48 7 .0 66.6 T 22.0 6408.9 6497.5 658.7 4.0 1.00 68.6 T 14.5 4222.4 4305.5 658.7 4.0 8 .0 99.6 C 31.8 3839.8 3971.3 478.3 7.2 1.00 96.3 C 33.9 2251.9 2382.1 478.3 7.2 9 .0 96.4 C 10.5 4807.3 4914.2 493.9 1.3 1.00 93.0 C 1.8 3167.8 3262.5 493.9 1.3 5 .0 183.7 C 85.3 0.8 269.7 0.2 17.3 1.00 180.3 C 72.8 1.3 254.4 0.2 17.3 6 .0 65.2 T 168.4 4953.8 5187.4 674.9 37.3 1.00 67.2 T 172.8 2713.3 2953.3 674.9 37.3 7 .0 66.4 T 217.4 5333.3 5617.1 897.8 46.6 1.00 68.5 T 208.6 2353.0 2630.1 897.8 46.6 8 .0 81.5 C 188.4 3715.9 3985.8 506.1 40.6 1.00 78.2 C 183.0 2035.9 2297.0 506.1 40.6 9 .0 80.6 C 100.9 4000.5 4182.0 673.2 22.3 1.00 77.2 C 103.1 1765.7 1946.0 673.2 22.3 5 .0 122.6 C 79.3 0.0 201.9 0.0 8.7 1.00 119.3 C 0.0 0.0 119.3 0.0 8.7 6 .0 19.0 T 102.5 2342.2 2463.6 705.5 11.2 1.00 21.0 T 0.0 0.0 21.0 705.5 11.2 7 .0 61.2 T 167.2 2747.5 2975.9 827.6 18.3 1.00 63.2 T 0.0 0.0 63.2 827.6 18.3 8 .0 74.2 C 134.5 1756.6 1965.4 529.2 14.7 1.00 70.9 C 0.0 0.0 70.9 529.2 14.7 9 .0 42.6 C 67.8 2060.6 2171.0 620.7 7.4 1.00 39.2 C 0.0 0.0 39.2 620.7 7.4 5 .0 125.9 C 98.1 2.4 226.4 3.1 45.1 1.00 125.1 C 0.0 0.0 125.1 3.1 45.1 6 .0 60.8 T 155.4 1277.6 1493.8 1616.8 71.4 1.00 61.3 T 0.0 0.0 61.3 1616.8 71.4 7 .0 57.7 T 199.9 1289.2 1546.8 1631.5 91.8 1.00 58.2 T 0.0 0.0 58.2 1631.5 91.8 8 .0 46.3 C 188.0 956.5 1190.8 1210.4 86.4 1.00 45.5 C 0.0 0.0 45.5 1210.4 86.4 9 .0 48.6 C 78.5 965.1 1092.3 1221.4 36.1 1.00 47.8 C 0.0 0.0 47.8 1221.4 36.1 5 .0 80.4 C 249.8 3.7 334.0 2.4 57.4 1.00 78.8 C 0.0 0.0 78.8 2.4 57.4 6 .0 42.0 T 44.0 214.7 300.7 135.8 10.1 1.00 43.0 T 0.0 0.0 43.0 135.8 10.1 7 .0 43.1 T 126.8 1420.2 1590.1 898.6 29.1 1.00 44.1 T 0.0 0.0 44.1 898.6 29.1 8 .0 27.5 C 144.7 163.7 335.9 103.6 33.2 1.00 25.9 C 0.0 0.0 25.9 103.6 33.2 9 .0 26.7 C 82.6 1067.8 1177.2 675.7 19.0 1.00 25.1 C 0.0 0.0 25.1 675.7 19.0 c:\at work\HORTON\6 BAYS\13GG3ORR.ani Page 65 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER -- PAGE NO. 66 MEMBER STBESSES ~%LL UNITS AR~ POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 49 5O 52 53 5 .0 137.7 C 7.5 1.3 146.4 0.5 1.1 1.00 135.3 C 0.0 0.0 135.3 0.5 1.1 6 .0 56.4 T 41.1 4223.3 4320.9 1781.6 6.3 1.00 57.9 T 0.0 0.0 57.9 1781.6 6.3 7 .0 55.7 T 17.3 3867.9 3940.9 1631.6 2.6 1.00 57.2 T 0.0 0.0 57.2 1631.6 2.6 8 .0 57.7 C 36.1 3168.4 3262.2 1336.6 5.5 1.00 55.3 C 0.0 0.0 55.3 1336.6 5.5 9 .0 58.2 C 7.7 2901.8 2967.8 1224.1 1.2 1.00 55.8 C 0.0 0.0 55.8 1224.1 1.2 5 .0 1.6 C 0.1 0.0 1.7 0.0 0.0 1.00 1.6 C 0.0 0.0 1.6 0.0 0.0 6 .0 1.0 C 2.4 0.4 3.8 0.1 0.3 1.00 1.0 C 0.0 0.0 1.0 0.1 0.3 7 .0 1.0 C 0.8 0.7 2.5 0.2 0.1 1.00 1.0 C 0.0 0.0 1.0 0.2 0.1 8 .0 1.6 C 1.8 0.3 3.7 0.1 0.2 1.00 1.6 C 0.0 0.0 1.6 0.1 0.2 9 .0 1.6 C 0.6 0.5 2.8 0.2 0.1 1.00 1.6 C 0.0 0.0 1.6 0.2 0.1 5 .0 101.9 T 0.0 0.0 101.9 0.0 3.1 1.00 101.9 T 0.0 0.0 101.9 0.0 3.1 6 .0 156.6 T 0.0 0.0 156.6 0.0 1.9 1.00 156.6 T 0.0 0.0 156.6 0.0 1.9 7 .0 253.4 C 0.0 0.0 253.4 0.0 1.9 1.00 253.4 C 0.0 0.0 253.4 0.0 1.9 8 .0 191.6 T 0.0 0.0 191.6 0.0 3.1 1.00 191.6 T 0.0 0.0 191.6 0.0 3.1 9 .0 116.0 C 0.0 0.0 116.0 0.0 3.1 1.00 116.0 C 0.0 0.0 116.0 0.0 3.1 5 .0 105.0 T 0.0 0.0 105.0 0.0 3.1 1.00 105.0 T 0.0 0.0 105.0 0.0 3.1 6 .0 158.7 T 0.0 0.0 158.7 0.0 1.9 1.00 158.7 T 0.0 0.0 158.7 0.0 1.9 7 .0 260.3 C 0.0 0.0 260.3 0.0 1.9 1.00 260.3 C 0.0 0.0 260.3 0.0 1.9 8 .0 195.4 T 0.0 0.0 195.4 0.0 3.1 1.00 195.4 T 0.0 0.0 195.4 0.0 3.1 9 .0 118.8 C 0.0 0.0 118.8 0.0 3.1 1.00 118.8 C 0.0 0.0 118.8 0.0 3.1 6 .0 164.2 T 0.0 0.0 164.2 0.0 1.9 1.00 164.2 T 0.0 0.0 164.2 0.0 1.9 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 66 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 67 *4GBA WITR RAFTER STIFFENER MEMBER STRESSES ALL UNITS APE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z C(~4BINED SHEA~-Y SHEAR-Z 54 55 56 57 7 .0 274.8 C 0.0 0.0 274.8 0.0 1.9 1.00 274.8 C 0.0 0.0 274.8 0.0 1.9 8 .0 203.3 T 0.0 0.0 203.3 0.0 3.1 1.00 203.3 T 0.0 0.0 203.3 0.0 3.1 9 .0 125.9 C 0.0 0.0 125.9 0.0 3.1 1.00 125.9 C 0.0 0.0 125.9 0.0 3.1 5 .0 120.1 T 0.0 0.0 120.1 0.0 3.1 1.00 120.1 T 0.0 0.0 120.1 0.0 3.1 6 .0 171.0 T 0.0 0.0 171.0 0.0 1.9 1.00 171.0 T 0.0 0.0 171.0 0.0 1.9 7 .0 301.3 C 0.0 0.0 301.3 0.0 1.9 1.00 301.3 C 0.0 0.0 301.3 0.0 1.9 8 .0 215.6 T 0.0 0.0 215.6 0.0 3.1 1.00 215.6 T 0.0 0.0 215.6 0.0 3.1 9 .0 138.6 C 0.0 0.0 138.6 0.0 3.1 1.00 138.6 C 0.0 0.0 138.6 0.0 3.1 5 .0 128.8 T 0.0 0.0 128.8 0.0 3.6 1.00 128.8 T 0.0 0.0 128.8 0.0 3.6 6 .0 176.8 T 0.0 0.0 176.8 0.0 2.2 1.00 176.8 T 0.0 0.0 176.8 0.0 2.2 7 .0 331.0 C 0.0 0.0 331.0 0.0 2.2 1.00 331.0 C 0.0 0.0 331.0 0.0 2.2 8 .0 226.2 T 0.0 0.0 226.2 0.0 3.6 1.00 226.2 T 0.0 0.0 226.2 0.0 3.6 9 .0 154.7 C 0.0 0.0 154.7 0.0 3.6 1.00 154.7 C 0.0 0.0 154.7 0.0 3.6 5 .0 3.6 T 0.0 0.0 3.6 0.0 3.1 1.00 3.6 T 0.0 0.0 3.6 0.0 3.1 6 .0 178.8 T 0.0 0.0 178.5 0.0 1.9 1.00 178.5 T 0.0 0.0 178.5 0.0 1.9 7 .0 3.8 T 0.0 0.0 3.8 0.0 1.9 1.00 3.8 T 0.0 0.0 3.8 0.0 1.9 8 .0 136.7 T 0.0 0.0 136.7 0.0 3.1 1.00 136.7 T 0.0 0.0 136.7 0.0 3.1 9 .0 5.7 T 0.0 0.0 5.7 0.0 3.1 1.00 5.7 T 0.0 0.0 5.7 0.0 3.1 5 .0 3.5 T 0.0 0.0 3.5 0.0 3.1 1.00 3.5 T 0.0 0.0 3.5 0.0 3.1 6 .0 171.4 T 0.8 0.0 171.4 0.0 1.9 1.00 171.4 T 0.0 0.0 171.4 0.0 1.9 7 .0 8.0 T 0.0 0.0 8.0 0.0 1.9 1.00 8.0 T 0.0 0.0 8.0 0.0 1.9 8 .0 131.3 T 0.0 0.0 131.3 0.0 3.1 1.00 131.3 T 0.0 0.0 131.3 0.0 3.1 9 .0 8.7 T 0.0 0.0 8.7 0.0 3.1 1.00 8.7 T 0.0 0.0 8.7 0.0 3.1 C:\at work\HORTON\6 BAYS\I3GG3ORR.anl Page 67 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG PAGE NO. 68 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 58 59 6O 62 5 .0 1.1 T 0.0 0.0 1.1 0.0 3.1 1.00 1.1 T 0.0 0.0 1.1 0.0 3.1 6 .0 157.7 T 0.0 0.0 157.7 0.0 1.9 1.00 157.7 T 0.0 0.0 157.7 0.0 1.9 7 .0 18.1 T 0.0 0.0 18.1 0.0 1.9 1.00 18.1 T 0.0 0.0 18.1 0.0 1.9 8 .0 119.2 T 0.0 0.0 119.2 0.0 3.1 1.00 119.2 T 0.0 0.0 119.2 0.0 3.1 9 .0 14.5 T 0.0 0.0 14.5 0.0 3.1 1.00 14.5 T 0.0 0.0 14.5 0.0 3.1 5 ,0 9.3 C 0.0 0.0 9.3 0.0 3.1 1.00 9.3 C 0.0 0.0 9.3 0.0 3.1 6 .0 134.1 T 0.0 0.0 134.1 0.0 1.9 1.00 134.1 T 0.0 0,0 134.1 0.0 1.9 7 .0 45.6 T 0.0 0.0 45.6 0.0 1.9 1.00 45.6 T 0.0 0.0 45.6 0.0 1,9 8 .0 93.9 T 0.0 0.0 93.9 0.0 3.1 1.00 93.9 T 0.0 0.0 93.9 0.0 3.1 9 .0 27.5 T 0.0 0.0 27.5 0.0 3.1 1.00 27.5 T 0.0 0.0 27.5 0.0 3.1 5 .0 97.8 T 0.0 0.0 97.8 0.0 3.1 1.00 97.8 T 0.0 0.0 97.8 0.0 3.1 6 .0 427.6 C 0.0 0.0 427.6 0.0 1.9 1.00 427.6 C 0.0 0.0 427.6 0.0 1.9 7 .0 294.3 T 0.0 0.0 294.3 0.0 1.9 1.00 294.3 T 0.0 0.0 294.3 0.0 1.9 8 .0 249.9 C 0.0 0.0 249.9 0.0 3.1 1.00 249.9 C 0.0 0.0 249.9 0.0 3.1 9 .0 291.5 T 0.0 0.0 291.5 0.0 3.1 1.00 291.5 T 0.0 0.0 291.5 0.0 3.1 5 .0 92.7 C 0.0 0.0 92.7 9.7 0.8 1.00 92.7 C 0.0 0.0 92.7 9.7 0.8 6 .0 606.7 C 0.0 0.0 606.7 5.8 0.5 1.00 606.7 C 0.0 0.0 606.7 5.8 0.5 7 .0 846.7 T 0.0 0.0 846.7 5.8 0.5 1.00 846.7 T 0.0 0.0 846.7 5.8 0.5 8 .0 522.1C 0.0 0.0 522.1 9.7 0.8 1.00 522.1 C 0.0 0.0 522.1 9.7 0.8 9 .0 568.0 T 0.0 0.0 568.0 9.7 0.8 1.00 568.0 T 0.0 0.0 568.0 9.7 0.8 5 .0 13.5 T 0.0 0.0 13.5 9.7 0.8 1.00 13.5 T 0.0 0.0 13.5 9.7 0.8 6 .0 719.1 C 0.0 0.0 719.1 5.8 0.5 1.00 719.1 C 0.0 0.0 719.1 5.8 0.5 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 68 of 89 SYSTEM 4E CLT-13GG *4GBA WITH P~AFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM PAGE NO. 69 MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHF, A/-Z 83 64 65 66 7 .0 767.5 T 0.0 0.0 767.5 5.8 0.5 1.00 767.5 T 0.0 0.0 767.5 5.8 0.5 8 .0 529.5 C 0.0 0.0 529.5 9.7 0.8 1.00 529.5 C 0.0 0.0 529.5 9.7 0.8 9 .0 585.4 T 0.0 0.0 585.4 9.7 0.8 1.00 585.4 T 0.0 0.0 585.4 9.7 0.8 5 .0 0.7 C 0.0 0.0 8.7 9.7 0.8 1.00 0.7 C 0.0 0.0 0.7 9.7 0.8 6 .0 811.5 C 0.0 0.0 811.5 5.8 0.5 1.00 811.5 C 0.0 0.0 811.5 5.8 0.5 7 .0 846.7 T 0,0 0.0 846.7 5.8 0.5 1.00 846.7 T 0.0 0.0 846.7 5.8 0.5 8 .0 609.2 C 0.0 0.0 609.2 9.7 0.8 1.00 609.2 C 0.0 0.0 609.2 9.7 0.8 9 .0 634.5 T 0.0 0.0 634.5 9.7 0.8 1.00 634.5 T 0.0 0.0 634.5 9.7 0.8 5 .0 0.5 T 0.0 0.0 0.5 9.7 0.8 1.00 0.5 T 0.0 0.0 0.5 9.7 0.8 6 .0 838.8 C 0.0 0.0 838.8 5.8 0.5 1.0O 838.8 C O.0 0.0 838.8 5.8 0.5 7 .0 914.9 T 0.0 0.0 914.9 5.8 0.5 1.00 914.9 T 0.0 0.0 914.9 5.8 0.5 8 .0 628.7 C 0.0 0.0 628.7 9.7 0,8 1.00 628.7 C 0.0 0.0 628.7 9.7 0.8 9 .0 686.5 T 0.0 0.0 686.5 9.7 0.8 1.00 686.5 T 0.0 0.0 686.5 9.7 0.8 5 .0 189.0 T 0.0 0.0 189.0 0.0 3.1 1.00 189.0 T 0.0 0.0 189,0 0.0 3.1 6 .0 379.9 C 0.0 0.0 379.9 0.0 1.9 1.00 379.9 C 0.0 0.0 379.9 0.0 1.9 7 .0 206.8 T 0.0 0.0 206.8 0.0 1.9 1.00 206.8 T 0.0 0.0 206.8 0.0 1.9 8 .0 148.1 C 0.0 0.0 148.1 0.0 3.1 1.00 148.1 C 0.0 0.0 148.1 0.0 3.1 9 .0 292.0 T 0.0 0.0 292.0 0.0 3.1 1.00 292.0 T 0.0 0.0 292.0 0.0 3.1 5 .0 193.6 C 0.0 0.0 193.6 9.7 0.8 1.00 193.6 C 0.0 0.0 193.6 9.7 0.8 6 .0 299.8 C 0.0 0.0 299.8 5.8 0.5 1.00 299.8 C 0.0 0.0 299.8 5.8 0.5 7 .0 978.4 T 0.0 0.0 978.4 5.8 0.5 1.00 978.4 T 0.0 0.0 978.4 5.8 0.5 8 .0 365.1 C 0.0 0.0 365.1 9.7 0.8 1.00 365.1 C 0.0 0.0 365.1 9.7 0.8 9 .0 593.6 T 8.0 0.0 593.6 9,7 0.8 1.00 593.6 T 0.0 0.0 593.6 9.7 0.8 C:\at work\HORTON\6 BAYS\i3GG3ORR.ani Page 69 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 70 *4GBA WITH RAFTER STIFFENER ~4BER STBESSES ALL UNITS /~ POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 67 68 69 70 5 .0 27.4 T 0.0 0.0 27.4 9.7 0.8 1.00 27.4 T 0.0 0.0 27.4 9.7 0.8 6 .0 461.3 C 0.0 0.0 461.3 5.8 0.5 1.00 461.3 C 0.0 0.0 461.3 5.8 0.5 7 .0 759.7 T 0.0 0.0 759.7 5.8 0.5 1.00 759.7 T 0.0 0.0 759.7 5.8 0.5 8 .0 326.1 C 0.0 0.0 326.1 9.7 0.8 1.00 326.1 C 8.0 0.0 326.1 9.7 0.8 9 .0 589.6 T 0.0 0.0 589.6 9.7 0.8 1.00 589.6 T 0.0 0.0 589.6 9.7 0.8 5 .0 0.6 C 0.0 0.0 0.6 9.7 0.8 1.00 0.6 C 0.0 0.0 0.6 9.7 0.8 6 .0 601.4 C 0.0 0.0 601.4 5.8 0.5 1.00 601.4 C 0.0 0.0 601.4 5.8 0.5 7 .0 825.2 T 0.0 0.0 825.2 5.8 0.5 1.00 825.2 T 8.0 0.0 825.2 5.8 0.5 8 .0 451.5 C 0.0 0.0 451.5 9.7 0.8 1.00 451.5 C 0.0 0.0 451.5 9.7 0.8 9 .0 618.4 T 0.0 0.0 618.4 9.7 0.8 1.00 618.4 T 0.0 0.0 618.4 9.7 0.8 5 .0 0.6 T 0.0 0.0 0.6 9.7 0.8 1.00 0.6 T 0.0 0.0 0.6 9.7 0.8 6 .0 496.9 C 0.0 0.0 496.9 5.8 0.5 1.00 496.9 C 0.0 0.0 496.9 5.8 0.5 7 .0 896,4 T 0.0 8.0 896.4 5.8 0.5 1.00 896.4 T 0.0 0.0 896.4 5.8 0.5 8 .0 372.2 C 0.0 0.0 372.2 9.7 0.8 1.00 372.2 C 0.0 0.0 372.2 9.7 0.8 9 .0 672.8 T 0.0 0.0 672.8 9.7 0.8 1.00 672.8 T 0.0 0.0 672.8 9.7 0.8 5 .0 183.1 T 0.0 0,0 183.1 0.0 3.1 1.00 183.1 T 0.0 0.0 183.1 0.0 3.1 6 .0 247.5 C 0.0 0.0 247.5 0.0 1.9 1.00 247.5 C 0.0 0.0 247.5 0.0 1.9 7 .0 217.3 T 0.0 0.0 217.3 0.0 1.9 1.00 217.3 T 0.0 0.0 217.3 0.0 1.9 8 .0 53.1 C 0.0 0.0 53.1 0.0 3.1 1.00 53.1 C 0.0 0.0 53.1 0.0 3.1 9 .0 295.5 T 0.0 0.0 295.5 0.0 3.1 1.00 295.5 T 0.0 0.0 295.5 0.0 3.1 5 .0 198.4 C 0.0 0.0 198.4 9.7 0.8 1.00 198.4 C 0.0 0.0 198.4 9.7 0.8 6 .0 47.9 C 0.0 0.0 47.9 5.8 0.5 1.00 47.9 C 0.0 0.0 47.9 5.8 0.5 C: \at work\HORTON\6 BAYS\13GG3ORR.ani Page 70 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 71 *4GBA WITH P. AFTER STIFFENER MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH M~MB LD SECT ~IAL BEND-y BEND-Z COMBINED SHEAR-Y SEEAR-Z 72 73 74 75 7 .0 988.1 T 0.0 0.0 988.1 5.8 0.5 1.00 988.1 T 0.0 0.0 988.1 5.8 0.5 8 .0 179.5 C 0.0 0.0 179.5 9.7 0.8 1.00 179.5 C 0.0 0.0 179.5 9.7 0.8 9 .0 597.4 T 0.0 0.0 597.4 9.7 0.8 1.00 597.4 T 0.0 0.0 597.4 9.7 0.8 5 .0 23.3 T 0.0 0.0 23.3 9.7 0.8 1.00 23.3 T 0.0 0.0 23.3 9.7 0.8 6 .0 187.7 C 0.0 0.0 187.7 5.8 0.5 1.00 187.7 C 0.0 0.0 187.7 5.8 0.5 7 .0 776.7 T 0.0 0.8 776.7 5.8 0.5 1.00 776.7 T 0.0 0.0 776.7 5.8 0.5 8 .0 124.0 C 0.0 0.0 124.0 9.7 0.8 1.00 124.0 C 0.0 0.0 124.0 9.7 0.8 9 .0 599.4 T 0.0 0.0 599.4 9.7 0.8 1.00 599.4 T 0.0 0.0 599.4 9.7 0.8 5 .0 1.0 T 0.0 0.0 1.0 9.7 0.8 1.00 1.0 T 0.0 0.0 1.0 9.7 0.8 6 .0 395.1 C 0.0 0.0 395.1 5.8 0.5 1.00 395.1 C 0.0 0.0 395.1 5.8 0.5 7 .0 794.3 T 0.0 0.0 794.3 5.8 0.5 1.00 794.3 T 0.0 0.0 794.3 5.8 0.5 8 .0 295.6 C 0.0 0.0 295.6 9.7 0.8 1.00 295.6 C 0.0 0.0 295.6 9.7 0.8 9 .0 596.5 T 0.0 0.0 596.5 9.7 0.8 1.00 596.5 T 0.0 0.0 596.5 9.7 0.8 5 .0 0.0 C 0.0 0.0 0.0 9.7 0.8 1.00 0.0 C 0.0 0.0 0.0 9.7 0.8 6 .0 160.7 C 0.0 0.0 160.7 5.8 0.5 1.00 160.7 C 0.0 0.0 160.7 5.8 0.5 7 .0 897.7 T 0.0 0.0 897.7 5.8 0.5 1.00 897.7 T 0.0 0.0 897.7 5.8 0.5 8 .0 120.5 C 0.0 0.0 120.5 9.7 0.8 1.80 120.5 C 0.0 0.0 120.5 9.7 0.8 9 .0 673.2 T 0.0 0.0 673.2 9.7 0.8 1.00 673.2 T 0.0 0.0 673.2 9.7 0.8 5 .0 182.8 T 0,0 0,0 182.8 0.0 3.1 1.00 182.8 T 0.0 0.0 182.8 0.0 3.1 6 .0 116.2 C 0.0 0.0 116.2 0.0 1.9 1.00 116.2 C 0.0 0.0 116.2 0.0 1.9 7 .0 218.1 T 0.0 0.0 218.1 0.0 1.9 1.00 218.1 T 0.0 0.0 218.1 0.0 1.9 8 .0 45.2 T 0.0 0.0 45.2 0.0 3.1 1.00 45.2 T 0.0 0.0 45.2 0.0 3.1 9 .0 295.9 T 0.0 0.0 295.9 0.0 3.1 1.00 295.9 T 0.0 0.0 295.9 0.0 3.1 C:\at work\HORTON\6 BAYS\I3GG3ORR.anl Page 71 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 72 MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH REND-Z COMBINED SHEAR-y SHEA~- Z 76 77 78 79 8O 5 .0 198.3 C 0.0 0.0 198.3 9.7 0.8 1.00 198.3 C 0.0 0.0 198.3 9.7 0.8 6 .0 201.6 T 0.0 0.0 201.6 5.8 0.5 1.00 201.6 T 0.0 0.0 201.6 5.8 0.5 7 .0 988.8 T 0.0 0.0 988.8 5.8 0.5 1.00 988.8 T 0.0 0.0 988.8 5.8 0.5 8 .0 7.7 T 0.0 0.0 7.7 9.7 0.8 1.00 7.7 T 0.0 0.0 7.7 9.7 0.8 9 .0 598.1 T 0.0 0.0 598.1 9.7 0.8 1.00 598.1 T 0.0 0.0 598~1 9.7 0.8 5 .0 23.2 T 0.0 0.0 23.2 9.7 0.8 1.00 23.2 T 0.0 0.0 23.2 9.7 0.8 6 .0 90.5 T 0.0 0.0 90.5 5.8 0.5 1.00 90.5 T 0.0 0.0 90.5 5.8 0.5 7 .0 792.7 T 0.0 0.0 792.7 5.8 0.5 1.00 792.7 T 0.0 0.0 792.7 5.8 0.5 8 .0 84.6 T 0.0 0.0 84.6 9.7 0.8 1.00 84.6 T 0.0 0.0 84.6 9.7 0.8 9 .0 611.3 T 0.0 0.0 611.3 9.7 0.8 1.00 611.3 T 0.0 0.0 611.3 9.7 0.8 5 .0 1.2 T 0.0 0.0 1.2 9.7 0.8 1.00 1.2 T 0.0 0.0 1.2 9.7 0.8 6 .0 199.4 C 0.0 0.0 199.4 5.8 0.5 1.00 199.4 C 0.0 0.0 199.4 5.8 0.5 7 .0 756.2 T 0.0 0.0 756.2 5.8 0.5 1.00 756.2 T 0.0 0.0 756.2 5.8 0.5 8 .0 148.7 C 0.0 0.0 148.7 9.7 0.8 1.00 148.7 C 0.0 0.0 148.7 9.7 0.8 9 .0 568.1 T 0.0 0.0 568.1 9.7 0.8 1.00 568.1 T 0.0 0.0 568.1 9.7 0.8 5 .0 0.2 C 0.0 0.0 0.2 9.7 0.8 1.00 0.2 C 0.0 0.0 0.2 9.7 0.8 6 .0 179.6 T 0.0 0.0 179.6 5.8 0.5 1.00 179.6 T 0.0 0.0 179.6 5.8 0.5 7 .0 918.2 T 0.0 0.0 918.2 5.8 0.5 1.00 918.2 T 0.0 0.0 918.2 5.8 0.5 8 .0 134.6 T 0.0 0.0 134.6 9.7 0.8 1.00 134.6 T 0.0 0.0 134.6 9.7 0.8 9 .0 688.5 T 0.0 0.0 688.5 9.7 0.8 1.00 688.5 T 0.0 0.0 688.5 9.7 0.8 5 .0 188.3 T 0.0 0.0 188.3 0.0 3.1 1.00 188.3 T 0.0 0.0 188.3 0.0 3.1 6 .0 9.8 T 0.0 0.0 9.8 0.0 1.9 1.00 9.8 T 0.0 0.0 9.8 0.0 1.9 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 72 of 89 SYSTEM 4E CLT 13GG *4GBA WITH P~TER STIFFENER Wednesday, January 28, 2009, 02:23 PM PAGE NO. 73 MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND - Z COMBINED SHEAR-Y SHEAR-Z 82 83 84 7 .0 209.8 T 0.0 0.0 209.8 0.0 1.9 1.00 209.8 T 0.0 0.0 209.8 0.0 1.9 8 .0 143.6 T 0.0 0.0 143.6 0.0 3.1 1.00 143.6 T 0.0 0.0 143.6 0.0 3.1 9 .0 293.6 T 0.0 0.0 293.6 0.0 3.1 1.00 293.6 T 0.0 0.0 293.6 0.0 3.1 5 .0 193.2 C 0.0 0.0 193.2 9.7 0.8 1.00 193.2 C 0.0 0.0 193.2 9.7 0.8 6 .0 441.4 T 0.0 0.0 441.4 5.8 0.5 1.00 441.4 T 0.0 0.0 441.4 5.8 0.5 7 .0 980.3 T 0.0 0.0 980.3 5.8 0.5 1.00 980.3 T 0.0 0.0 980.3 5.8 0.5 8 .0 191.2 T 0.0 0.0 191.2 9.7 0.8 1.00 191.2 T 0.0 0.0 191.2 9.7 0.8 9 .0 595.4 T 0.0 0.0 595.4 9.7 0.8 1.00 595.4 T 0.0 0.0 595.4 9.7 0.8 5 .0 27.1 T 0.0 0.0 27.1 9.7 0.8 1.00 27.1 T 0.0 0.0 27.1 9.7 0.8 6 .0 379.5 T 0.0 0.0 379.5 5.8 0.5 1.00 379.5 T 0.0 0.0 379.5 5.8 0.5 7 .0 810.0 T 0.0 0.0 810.0 5.8 0.5 1.00 810.0 T 0.0 0.0 810.0 5.8 0.5 8 .0 304.2 T 0.0 0.0 304.2 9.7 0.8 1.00 304.2 T 0.0 0.0 304.2 9.7 0.8 9 .0 627.2 T 0.0 0.0 627.2 9.7 0.8 1.00 627.2 T 0.0 0.0 627.2 9.7 0.8 5 .0 0.1 C 0.0 0.0 0.1 9.7 0.8 1.00 0.1 C 0.0 0.0 0.1 9.7 0.8 6 .0 23.0 C 0.0 0.0 23.0 5.8 0.5 1.00 23.0 C 0.0 0.0 23.0 5.8 0.5 7 .0 707.8 T 0.0 0.0 707.8 5.8 0.5 1.00 707.8 T 0.0 0.0 707.8 5.8 0.5 8 .0 17.3 C 0.0 0.0 17.3 9.7 0.8 1.00 17.3 C 0.0 0.0 17.3 9.7 0.8 9 .0 530.8 T 0.0 0.0 530.8 9.7 0.8 1.00 530.8 T 0.0 0.0 530.8 9.7 0.8 5 .0 0.3 T 0.0 0.0 0.3 9.7 0.8 1.00 0.3 T 0.0 0.0 0.3 9.7 0.8 6 .0 534.9 T 0.0 0.0 534.9 5.8 0.5 1.00 534.9 T 0.0 0.0 534.9 5.8 0.5 7 .0 960.1 T 0.0 0.0 960.1 5.8 0.5 1.00 960.1 T 0.0 0.0 960.1 5.8 0.5 8 .0 401.4 T 0.0 0.0 401.4 9.7 0.8 1.00 401.4 T 0,0 0.0 401.4 9.7 0.8 9 .0 720.3 T 0.0 0.0 720.3 9.7 0.8 1.00 720.3 T 0.0 0.0 720.3 9.7 0.8 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 73 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT~13GG PAGE NO. 74 *4GBA WITH P~TER STIFFENER MEMBER STP. ESSES kLL UNITS ABE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND- Z COMBINED SHEAR-Y SHEAR-Z 85 86 87 88 89 5 .0 97.0 T 0.0 0.0 97.0 0.0 3.1 1.00 97.0 T 0.0 0.0 97.0 0.0 3.1 6 .0 198.0 T 0.0 0.0 198.0 0.0 1.9 1.00 198.0 T 0.0 0.0 198.0 0.0 1.9 7 .0 300.4 T 0.0 0.0 300.4 0.0 1.9 1.00 300.4 T 0.0 0.0 300.4 0.0 1.9 8 .0 218.6 T 0.0 0.0 218.6 0.0 3.1 1.00 218.6 T 0.0 0.0 218.6 0.0 3.1 9 .0 295.5 T 0.0 0.0 295.5 0.0 3.1 1.00 295.5 T 0.0 0.0 295.5 0.0 3.1 5 .0 92.7 C 0.0 0.0 92.7 9.7 0.8 1.00 92.7 C 0.0 0.0 92.7 9.7 0.8 6 .0 590.4 T 0.0 0.0 590,4 5.8 0.5 1.00 590.4 T 0.0 0.0 590.4 5.8 0.5 7 .0 851.0 T 0.0 0.0 851.0 5.8 0.5 1.00 851.0 T 0.0 0.0 851.0 5.8 0.5 8 .0 375.6 T 0.0 0.0 375.6 9.7 0.8 1.00 375.6 T 0.0 0.0 375.6 9.7 0.8 9 .0 571.1 T 0.0 0.0 571.1 9.7 0.8 1.00 571.1 T 0.0 0.0 571.1 9.7 0.8 5 .0 12.9 T 0.0 0.0 12.9 9.7 0.8 1.00 12.9 T 0.0 0.0 12.9 9.7 0.8 6 .0 707.2 T 0.0 0.0 707.2 5.8 0.5 1.00 707.2 T 0.0 0.0 707.2 5.8 0.5 7 .0 861.5 T 0.0 0.0 861.5 5.8 0.5 1.00 861.5 T 0.0 0.0 861.5 5.8 0.5 8 .0 539.8 T 0.0 0.0 539.8 9.7 0.8 1.00 539.8 T 0.0 0.0 539.8 9.7 0.8 9 .0 655.4 T 0.0 0.0 655.4 9.7 0.8 1.00 655.4 T 0.0 0.0 655.4 9.7 0.8 5 ,0 0.2 T 0.0 0.0 0.2 9.7 0.8 1.00 0.2 T 0.0 0.0 0.2 9.7 0.8 6 .0 121.4 T 0.0 0.0 121.4 5.8 0.5 1.00 121.4 T 0.0 0.0 121.4 5.8 0.5 7 .0 639.8 T 0.0 0.0 639.8 5.8 0.5 1.00 639.8 T 0.0 0.0 639.8 5.8 0.5 8 .0 91.2 T 0.0 0.0 91.2 9.7 0.8 1.00 91.2 T 0.0 0.0 91.2 9.7 0.8 9 .0 480.0 T 0.0 0.0 480,0 9.7 0.8 1.00 480.0 T 0.0 0.0 480.0 9.7 0.8 5 .0 0.1 C 0.0 0.0 0.1 9.7 0.8 1.00 0.1 C 0.0 0.0 0.1 9.7 0.8 6 .0 919.2 T 0.0 0.0 919.2 5.8 0.5 1.00 919.2 T 0.0 0.0 919.2 5.8 0.5 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 74 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 75 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 9O 92 93 7 .0 1026.9 T 0.0 0.0 1026.9 5.8 0.5 1.00 1026.9 T 0.0 0.0 1026.9 5.8 0.5 8 .0 689.4 T 0.0 0.0 689.4 9.7 0.8 1.00 689.4 T 0.0 0.0 689.4 9.7 0.8 9 .0 770.2 T 0.0 0.0 770.2 9.7 0.8 1.00 770.2 T 0.0 0.0 770.2 9.7 0.8 5 .0 5.9 T 0.0 0.0 5.9 0.0 3.1 1.00 5.9 T 0.0 0.0 5.9 0.0 3.1 6 .0 21.9 T 0.0 0.0 21.9 0.0 1.9 1.00 21.9 T 0.0 0.0 21.9 0.0 1.9 7 .0 19.0 C 0.0 0.0 19.0 0.0 1.9 1.00 19.0 C 0.0 0.0 19.0 0.0 1.9 8 .0 20.7 T 0.0 0.0 20.7 0.0 3.1 1.00 20.7 T 0.0 0.0 20.7 0.0 3.1 9 .0 9.9 C 0.0 0.0 9.9 0.0 3.1 1.00 9.9 C 0.0 0.0 9.9 0.0 3.1 5 .0 56.7 T 0.0 0.0 56.7 0.0 3.1 1.00 56.7 T 0.0 0.0 56.7 0.0 3.1 6 .0 106.6 T 0.0 0.0 106.6 0.0 1.9 1.00 106.6 T 0.0 0.0 106.6 0.0 1.9 7 .0 144.9 C 0.0 0.0 144.9 0.0 1.9 1.00 144.9 C 0.0 0.0 144.9 0.0 1.9 8 .0 121.3 T 0.0 0.0 121.3 0.0 3.1 1.00 121.3 T 0.0 0.0 121.3 0.0 3.1 9 .0 67.4 C 0.0 0.0 67.4 0.0 3.1 1.00 67.4 C 0.0 0.0 67.4 0.0 3.1 5 .0 90.3 T 0.0 0.0 90.3 0.0 3.6 1.00 90.3 T 0.0 0.0 90.3 0.0 3.6 6 .0 171.9 T 0.0 0.0 171.9 0.0 2.2 1.00 171.9 T 0.0 0.0 171.9 0.0 2.2 7 .0 235.4C 0.0 0.0 239.4 0.0 2.2 1.00 235.4 C 0.0 0.0 235.4 0.0 2.2 8 .0 194.5 T 0.0 0.0 194.5 0.0 3.6 1.00 194.5 T 0.0 0.0 194.5 0.0 3.6 9 .0 110.9 C 0.0 0.0 110.9 0.0 3.6 1.00 110.9 C 0.0 0.0 110.9 0.0 3.6 5 .0 10.0 T 0.0 0.0 10.0 0.0 3.1 1.00 10.0 T 0.0 0.0 10.0 0.0 3.1 6 .0 318.4 T 0.0 0.0 318.4 0.0 1.9 1.00 318.4 T 0.0 0.0 318.4 0.0 1.9 7 .0 71.0 C 0.0 0.0 71.0 0.0 1.9 1.00 71.0 C 0.0 0.0 71.0 0.0 1.9 8 .0 246.9 T 0.0 0.0 246.9 0.0 3.1 1.00 246.9 T 0.0 0.0 246.9 0.0 3.1 9 .0 45.1 C 0.0 0.0 45.1 0.0 3.1 1.00 45.1 C 0.0 0.0 45.1 0.0 3.1 C: lat work\HORTON\6 BAYS\I3GG3ORR.anl Page 75 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 76 *4GBA WITH P~AFTER STIFFENER M~MBER STRESSES ALL UNITS A~E POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 94 95 96 97 98 5 .0 7.3 T 1781.5 3.3 1792.1 0.1 82.2 1.00 7.3 T 0.0 0.0 7.3 0.1 95.3 6 .0 70.4 T 706.7 159.2 936.4 5.8 39.1 1.00 70.4 T 0.0 0.0 70.4 5.8 31.3 7 .0 15.6 C 749.5 1607.9 2373.0 58,5 41.2 1.00 15.6 C 0.0 0.0 15.6 58.5 33.4 8 .0 58.2 T 742.5 121,8 922.6 4.4 30.5 1.00 58.2 T 0.0 0.0 58.2 4.4 43.5 9 .0 6.3 C 710.5 1203.5 1920.3 43.8 28.9 1.00 6.3 C 0.0 0.0 6.3 43.8 41.9 5 .0 20.5 T 0.0 0.0 20.5 0.5 87.3 1.00 20.5 T 1621.7 14.6 1656.9 0.5 74.3 6 .0 68.3 T 0.0 0.0 68.3 12.4 30.0 1.00 68.3 T 680.2 341.7 1090.2 12.4 37.8 7 .0 22.6 C 0.0 0.0 22.6 51.1 29.3 1.00 22.6 C 665.9 1405.8 2094.4 51.1 37.1 8 .0 66.0 T 0.0 0.0 66.0 8.9 38.8 1.00 66.0 T 648.9 245.7 960.7 8.9 25.8 9 .0 2.2 C 0.0 0.0 2.2 38.7 39.4 1.00 2.2 C 659.6 1065.0 1726.8 38.7 26.3 5 .0 13.7 T 0.0 0.0 13.7 0.0 3.1 1.00 13.7 T 0.0 0.0 13.7 0.0 3.1 6 .0 210.0 T 0.0 0.0 210.0 0.0 1.9 1.00 210.0 T 0.0 0.0 210.0 0.0 1.9 7 .0 37.2 T 0.0 0.0 37.2 0.0 1.9 1.00 37.2 T 0.0 0.0 37.2 0.0 1.9 8 .0 167.1 T 0.0 0.0 167.1 0.0 3.1 1.00 167.1 T 0.0 0.0 167.1 0.0 3.1 9 .0 37.5 T 0.0 0.0 37.5 0.0 3.1 1.00 37.5 T 0.0 0.0 37.5 0.0 3.1 5 .0 82.9 C 270.9 569.9 923.8 90.8 58.3 1.00 82.2 C 247.3 165.1 494.6 89.3 58.3 6 .0 141.6 T 405.0 238.9 785.4 44.2 87.8 1.00 142.0 T 375.4 125.3 642.7 45.1 87.8 7 .0 31.3 T 84.3 372.2 487.8 86.9 33.7 1.00 31.8 T 215.1 341.4 588.3 87.9 33.7 8 .0 45.7 T 107.5 238.9 392.1 33.8 23.6 1.00 46.4 T 102.6 24.2 173.2 31.5 23.6 9 .0 37.0 C 133.0 138.9 308.8 0.9 16.9 1.00 36.2 C 17.6 137.8 191.7 0.6 16.9 5 .0 33.9 C 269.8 165.4 469.1 120.6 28.1 1.00 0.9 C 553.7 657.8 1212.5 14.7 28.1 6 .0 92.4 T 386.7 125.6 604.7 19.9 19,3 1.00 92.8 T 582.1 316.5 991.5 21.2 19.3 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 76 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 77 *4GBA WITH RAFTER STIFFENER NE~4BER STP. ESSES UNITS A/~ POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SH~.R-Y SHEA~-Z 99 100 101 102 7 .0 26.8 C 242.4 1.00 26.4 C 463.9 8 .0 44.0 T 94.8 1.00 70.3 T 35.7 9 .0 45.4 C 13.4 1.00 19.1 C 53.0 5 .0 18.3 T 1.00 42.4 T 6 .0 42.8 T 1.00 43.0 T 7 .0 44.8 C 1.00 44.6 C 8 .0 45.1 T 1.00 63.3 T 9 .0 20.6 C 1.00 2.5 C 341.7 610.9 32.7 21.9 651.7 1142.1 34.0 21.9 24.2 163.1 74.6 5.8 243.1 349.1 27.5 5.8 137.9 196.7 65.0 3.9 8.2 80.3 37.1 3.9 598.5 658.2 1274.9 34.0 70.9 374.8 1054.3 1471.4 237.5 70.9 658.5 316.9 1018.2 45.8 114.8 917.0 247.8 1207.8 43.8 114.8 497.9 652.0 1194.7 89.0 71.0 477.3 458.1 979.9 87.0 71.0 60.6 243.1 348.8 10.4 34.7 416.4 593.6 1073.3 143.1 34.7 59.9 8.3 88.8 42.8 1.9 86.6 435.9 525.0 110.6 1.9 5 .0 0.2 C 315.4 1.00 49.0 C 76.5 6 .0 12.9 C 671.9 1.00 12.4 C 654.9 7 .0 39.0 C 441.3 1.00 38.5 C 94.5 8 .0 10.6 C 275.5 1.00 26.6 C 546.6 9 .0 30.1 C 102.6 1.00 7.0 C 15.5 5 .0 2.9 C 34.2 1.00 46.4 C 8.0 6 .0 32.1 T 663.0 1.00 32.6 T 595.6 7 .0 3.4 C 28.8 1.00 2.9 C 37.0 8 .0 21.3 T 522.1 1.00 58.4 T 440.9 9 .0 5.4 C 3.2 1.00 31.8 C 33.6 5 .0 1.7 C 3.4 1.00 47.6 C 0.8 6 .0 165.1 T 585.3 1.00 165.6 T 727.4 7 .0 27.2 T 32.2 1.00 27.6 T 65.7 8 .0 121.9 T 436.5 1.00 159.1 T 546.1 9 .0 18.4 T 26.6 1.00 55.6 T 48.7 973.6 1289.3 206.9 14.5 791.3 916.8 192.2 14.5 180.3 865.1 7.7 0.6 59.4 726.7 11.6 0.6 320.3 800.5 14.9 19.8 97.3 230.3 18.8 19.8 586.2 872.3 148.4 10.0 637.0 1210.2 152.5 10.0 481.2 613.9 143.0 4.4 665.4 688.0 157.9 4.4 801.5 838.6 199.5 1.6 801.4 855.8 199.5 1.6 54.9 750.1 4.4 2.5 6.4 634.6 0.5 2.5 83.0 115.2 5.9 0.3 14.6 54.5 2.0 0.3 640.9 1184.3 152.4 3.0 593.1 1092.4 148.5 3.0 662.0 670.5 153.5 1.4 586.9 652.3 147.4 1.4 788.7 793.8 191.7 0.2 983.2 1031.5 207.4 0.2 3.6 754.1 0.7 5.3 28.1 921.1 3.2 5.3 10.8 70.2 0.4 1.2 27.5 120.8 3.5 1.2 585.6 1144.0 143.6 4.1 756.7 1461.9 157.4 4.1 580.2 625.2 143.4 0.8 756.3 860.6 157.6 0.8 C:\~t work\HORTON\6 BAYS\13GG3ORR.anl Page 77 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG - PAGE NO. 78 *4GBA WITH P~AFTER STIFFENER MEMBER STRESSES ALL UNITS ABE POUN/SQ INCH MEMB LD SECT AXIltL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 103 104 106 108 5 .0 6.9 C 0.5 1016.8 1024.2 240,5 0.0 1.00 42.4 C 0.0 0.0 42.4 158.5 0.0 6 .0 388.8 T 954.7 20.4 1364.0 2.8 35.4 1.00 389.3 T 0.0 0.0 389.3 1.1 35.4 7 .8 49.6 T 105.5 18.3 173.4 2.7 3.9 1.00 50.1 T 0.0 0.0 50.1 1.2 3.9 8 .0 285.8 T 716.4 775.9 1778.1 181.7 26.5 1.00 322.9 T 0.0 0.0 322.9 119.2 26.5 9 .0 31.4 T 78.7 774.4 884.5 181.7 2.9 1.00 68.5 T 0.0 0.0 68.5 119.3 2.9 5 .0 70.4 C 262.6 539.0 871.9 98.4 58.3 1.00 69.6 C 255.2 258.6 583.4 96.9 58.3 6 .0 179.7 T 41.1 112.8 333.7 20.5 7.8 1.00 180.2 T 110.3 276.6 567.1 19.6 7.8 7 .0 1.4 C 6.0 270.5 277.9 103.1 36.1 1.00 1.0 C 326.8 575.2 903.0 104.0 36.1 8 .0 83.5 T 221.0 310.8 615.3 87.0 36.3 1.00 84.2 T 101.9 393.6 579.8 85.5 36.3 9 .0 52.4 C 194.6 192.6 439.6 5.7 15.1 1.00 51.6 C 60.4 245.3 357.3 7.2 15.1 5 .0 21.0 C 275.0 258.8 554.9 119.7 28.0 1.00 13.9 C 558.8 742.8 1315.4 15.6 28.0 6 .0 207.7 T 99.0 276.5 583.1 9,3 27.3 1.00 208.0 T 375.2 183.9 767.1 10.6 27.3 7 .0 60.2 C 325.3 575.5 961.0 25.9 21.9 1.00 59.9 C 547.0 822.4 1429.3 27.2 21.9 8 .0 139.9 T 124.9 393.7 658.5 81.8 0.2 1.00 166.1 T 123.2 679.9 969.3 20.2 0.2 9 .0 61.0 C 44.9 245.3 351.2 69.4 3.9 1.00 34.7 C 5.6 74.8 115.2 32.7 3.9 5 .0 30.6 T 601.3 743.1 1375.0 42.0 71.0 1.08 54.7 T 373.6 1070.6 1498.9 245.5 71.0 6 .0 230.2 T 351.0 183.6 764.8 31.5 0.9 1.00 230.4 T 338.1 226.2 794.8 33.5 0.9 7 .0 76.8 C 556.4 822.8 1456.0 114.6 74.6 1.00 76.5 C 467.9 610.5 1155.0 112.6 74.6 8 .0 194.6 T 172.1 680.0 1046.7 53.4 50.7 1.00 212.8 T 524.1 961.6 1698.4 206.9 50.7 9 .0 35.6 C 18.0 74.8 128.4 56.2 4.6 1.00 17.4 C 80.5 334.0 431.9 97.3 4.6 5 .0 9.5 T 314.6 935.4 1259.5 193.1 14.6 1.00 58.8 T 79.5 1094.3 1232.7 205.9 14.6 6 .0 219.3 T 164.9 157.6 541.8 13.8 28.4 1.00 219.7 T 931.2 137.4 1288.3 9.9 28.4 C:lat work\HORTON\6 BAYS\13GG3ORR.anl Page 78 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 79 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT A~XIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 112 114 116 118 7 .0 77.6 C 448.4 383.3 909.4 13.1 24.8 1.00 77.2 C 219.8 10.8 307.8 17.0 24.8 8 .0 170.8 T 351.4 812.7 1334.9 154.8 10.7 1.00 207.9 T 640.8 705.3 3554.1 146.1 10.7 9 .0 51.9 C 108.6 407.0 567.5 134.6 8.0 1.00 14.7 C 107.3 800.3 922.3 166.3 8.0 5 ,0 17.9 C 41.1 1188.8 1247.7 239.4 2.6 1.00 31.4 C 28.6 200.6 260.6 159.7 2.6 6 .0 212.4 T 946.6 175.7 1334.7 15.1 29.4 1.00 212.9 T 152.6 246.3 611.8 19.0 29.4 7 .0 21.9 C 222.9 42.6 287.4 8.5 23.5 1.00 21.4 C 412.0 216.2 649.6 12.4 23.5 8 .0 145.9 T 680.2 743.7 1569.8 166.1 20.2 1.00 183.0 T 135.1 354.9 673.1 134.8 20.2 9 .0 29.8 C 137.4 843.5 1010.7 171.1 15.8 1.00 7.3 C 288.3 332.3 628.0 129.9 15.8 5 .0 16.0 T 14.9 223.0 253.9 154.4 0.7 1.00 65.3 T 4.7 1342.2 1412.2 244.7 0.7 6 .0 130.1 T 551.4 230.6 912.1 16.1 10.2 1.00 130.6 T 827.5 120.3 1078.4 12.2 10.2 7 .0 4.3 C 27.9 202.4 234.6 14.6 3.9 1.00 3.8 C 131.9 111.8 247.5 10.7 3.9 8 .0 108.4 T 402.8 358.6 869.7 128.6 8.2 1.00 148.5 T 624.0 901.2 1670.7 172.3 8.2 9 .0 7.5 T 10.2 337.5 355.1 127.5 3.4 1.00 44.7 T 102.3 907.5 1054.5 173.5 3.4 5 .0 12.2 T 2.3 1310.4 1324.9 252.4 0.1 1.00 61.5 T 0.0 0.0 61.5 146.7 0.1 6 .0 33.0 C 1039.3 105.3 1177.6 2.3 38.5 1.00 32.5 C 0.0 0.0 32.5 6.2 38.5 7 .0 21.0 T 180.0 96.4 297.8 1.9 6.7 1.00 21.4 T 0.0 0.0 21.4 5.8 6,7 8 .0 17.0 C 781.1 890.8 1688.9 186.4 28.9 1.00 20.2 C 0.0 0.0 20.2 114.6 28.9 9 .0 23.5 T 136.6 897.6 1057.7 186.7 5.1 1.00 60.7 T 0.0 0.0 60.7 114.3 5.1 5 .0 471.3 C 254.5 7096.9 7822.7 656.4 53.7 1.00 470.6 C 222.7 1744.2 2437.4 654.8 53.7 6 .0 779.8 T 131.4 7432.4 8343.5 347.9 48.0 1.00 780.2 T 295.0 4588.6 5663.8 348.8 48.0 7 .0 308.1 T 286.7 5548.2 6143.0 828.7 63.0 1.00 308.6 T 273.2 1221.3 1803.1 829.6 63.0 8 .0 244.1 T 85.8 430.6 760.4 213.5 2.9 1.00 244.8 T 60.1 2167.2 2472.1 211.9 2.9 9 .0 109.7 C 30.7 982.5 1122.9 147.2 8.4 1.00 108.9 C 43.7 2190.3 2342.9 148.7 8.4 c:\at work\HORTON\6 BAYS\13GG3ORR.ani Page 79 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT 13GG -- PAGE NO. 80 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS APE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SEEAR-Z 119 120 121 122 123 5 .0 185,9 C 114.9 515.6 816.5 364.0 17.6 1.00 169.2 C 224.9 1856.8 2250.9 310.2 17.6 6 .0 362.4 T 148.7 1356.5 1867.6 258.9 3.4 1.00 362.8 T 127.4 469.7 959.8 260.0 3.4 7 .0 96.8 T 132.4 361.0 590.2 347.6 17.5 1.00 97.1 T 241.9 2811.0 3150.1 348.7 17.5 8 .0 137.0 T 28.4 640.7 806.1 70.0 15.3 1.00 149.7 T 67.3 989.4 1206.4 29.1 15.3 9 .0 62.2 C 16.1 647.5 725.8 3.5 0.4 1.00 49.5 C 18.6 766.6 834.7 37.3 0.4 5 .0 124.3 C 234.3 1856.7 2215.3 372.6 46.4 1.00 112.7 C 160.1 5027.2 5300.0 291.7 46.4 6 .0 321.8 T 141.7 469.6 933.2 341.4 103.5 1.00 322.1 T 738.3 3736.9 4797.3 343.1 103.5 7 .8 57.5 T 255.4 2810.9 3123.9 309.4 55.5 1.00 57.7 T 216.1 5772.5 6046.4 311.1 55.5 8 .0 151.3 T 63.3 989.4 1204.0 14.5 44.1 1.00 160.0 T 437.9 834.7 1432.6 46.9 44.1 9 .0 47.0 C 22.0 766.6 835.6 38.5 8.0 1.00 38.2 C 46.2 692.0 776.4 22.9 8.0 5 .0 111.8 C 147.3 5024.1 5283.2 276.4 10.3 1.00 88.1 C 24.2 8722.0 8834.3 117.6 10.3 6 .0 322.6 T 604.0 3734.2 4660.8 205.6 4.3 1.00 323.1 T 675.7 7624.1 8623.0 208.8 4.3 7 .0 61.0 T 195.2 5769.3 6025.6 178.4 12.7 1.00 61.5 T 16.2 9149.3 9227.0 181.7 12.7 8 .0 160.8 T 346.3 834.5 1341.6 47.5 10.6 1.00 178.7 T 524,3 595.4 1298.4 72.9 10.6 9 .0 35.4 C 39.8 691.9 767.1 67.8 2.1 1.00 17.5 C 5.4 548.5 571.3 52.6 2.1 5 .0 85.7 C 9.0 8720.7 8815.5 100.4 0.6 1.00 62.0 C 0.3 9115.7 9178.0 58.3 0.6 6 .0 324.3 T 676.9 7623.0 8624.2 34.3 5.3 1.00 324.8 T 587.8 8297.1 9209.7 37.5 5.3 7 .0 63.3 T 9.2 9148.1 9220.7 7.2 3.7 1.00 63.8 T 52.8 9313.0 9429.5 10.4 3.7 8 .0 181.0 T 514.2 595.4 1290.5 48.5 4.4 1.00 198.9 T 440.7 376.5 1016.1 71.9 4.4 9 .0 14.8 C 13.4 548.5 576.8 68.9 3.2 1.00 3.1 C 39.8 385.4 428.3 51.5 3.2 5 .0 59.1 C 0.5 9116.9 9176.5 75.5 0.0 1.00 35.4 C 0.2 6289.0 6244.7 234.3 0.0 6 .0 326.0 T 583.9 8298.0 9207.9 137.0 8.4 1.00 326.5 T 724.5 5756.3 6807.4 133.8 8.4 C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 80 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG PAGE NO. 81 *4GBA WITH RAFTER STIFFENER MEMBER STBESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 124 125 126 127 7 .0 64.9 T 47.5 9314.3 9426.6 164.1 0.6 1.00 65.4 T 37.6 6263.9 6366.8 160.9 0.6 8 .0 201.5 T 438.2 376.7 1016.4 49.6 6.3 1.00 219.5 T 543.3 178.0 940.8 70.8 6.3 9 .0 5.6 T 35.3 385.5 426.4 69.9 0.4 1.00 23.6 T 28.4 202.6 254.6 50.5 0.4 5 .0 32.8 C 0.3 6212.3 6245.4 251.6 0.0 1.00 9.1 C 0.0 0.0 9.1 410.3 6 .0 327.2 T 886.7 5759.1 6973.0 308.4 53.0 1.00 327.7 T 0.0 0.0 327.7 305.2 53.0 7 .0 67.7 T 50.3 6267.2 6385.2 335.5 3.0 1.00 68.2 T 0.0 0.0 68.2 332.2 3.0 8 .0 221.4 T 664.8 178.3 1064.6 50.7 39.8 1.00 239.4 T 0.0 0.0 239.4 69.7 39.8 9 .0 26.8 T 37.9 202.7 267.5 71.0 2.3 1.00 44.8 T 0.0 0.0 44.8 49.4 2.3 5 .0 468.6 C 1.0 7189.1 7658.7 701.1 0.2 1.00 467.8 C 3.1 1471.1 1942.0 699.6 0.2 6 .0 775.8 T 49.8 7496.4 8322.0 379.3 11.6 1.00 776.3 T 153.3 4395.7 5325.2 380.2 11.6 7 .0 306.3 T 1.3 5654.0 5961.6 879.9 0.1 1.00 306.7 T 2.5 1533.7 1842.9 880.8 0.1 8 .0 243.0 T 38.1 411.8 692.9 222.3 8.9 1.00 243.8 T 117.2 2220.2 2581.2 220.7 8.9 9 .0 109.1 C 0.2 970.0 1079.3 153.2 0.1 1.00 108.3 C 0.4 2226.8 2335.6 154.7 0.1 5 .0 164.5 C 6.4 434.8 605.7 375.1 0.9 1.00 147.7 C 11.9 2015.7 2175.3 321.3 0.9 6 .0 345.5 T 69.7 1299.5 1714.7 266.7 17.6 1.00 345.8 T 40.8 581.4 968.0 267.8 17.6 7 .0 73.4 T 7.0 453.5 533.9 360.3 0.7 1.00 73.7 T 11.6 2992.9 3078.2 361.4 0.7 8 .0 139.9 T 47.7 656.4 843.9 72.2 13.9 1.00 152.6 T 39.2 1020.7 1212.4 31.4 13.9 9 ,0 64.2 C 0.6 658.3 723.2 2.0 0.1 1.00 51.5 C 0.1 788.0 839.6 38.8 0.1 5 .0 96.4 C 7.3 2015.8 2119.4 370.7 0.2 1.00 84.8 C 5.5 5167.8 5258.0 289.7 0.2 6 .0 301.8 T 31.4 581.4 914.7 340.2 72.4 1.00 302.1 T 647.0 3836.3 4785.4 341.8 72.4 7 .0 25.7 T 6.6 2992.9 3025.2 307.1 1.2 1.00 25.9 T 3.8 5932.8 5962.5 308.8 1.2 8 .0 156.5 T 28.9 1020.7 1206.0 14.1 54.1 1.00 165.3 T 489.2 861.9 1516.3 47.3 54.1 9 .0 50.6 C 0.3 788.0 838.9 38.8 0.8 1.00 41.8 C 6.8 710.5 759.1 22.6 0,8 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 81 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG _r PAGE NO. 82 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS A/%E POUN/SQ INCH MBMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 128 129 130 131 132 5 .0 85.4 C 1.5 5167.7 5254.7 274.8 0.8 1.00 61.7 C 11.3 8836.0 8909.1 116.0 0.8 6 .0 305.3 T 519.3 3836.3 4660.9 204.5 11.0 1.00 305.7 T 702.7 7706.1 8714.5 207.8 11.0 7 .0 29.8 T 5.3 5932.8 5967.8 176.6 1.6 1.00 30.3 T 32.1 9278.3 9340.7 179.8 1.6 8 .0 166.9 T 390.6 861.9 1419.3 47.1 7.7 1.00 184.9 T 518.8 616.5 1320.2 73.3 7.7 9 .0 39.7 C 5.1 710.5 755.3 68.1 0.6 1.00 21.7 C 15.9 562.7 600.4 52.3 0.6 5 .0 59.8 C 10.2 8836.1 1.00 36.1 C 4.4 9197.5 6 .0 307.9 T 695.3 7706.1 1.00 308.4 T 574.7 8356.6 7 .0 32.4 T 38.1 9278.3 1.00 32.9 T 68.7 9404.7 8 .0 187.4 T 514.1 616.5 1.00 205.3 T 434.3 391.1 9 .0 19.2 C 21.2 562.7 1.00 1.2 C 48.4 395.0 5 .0 33.7 C 3.2 9197.6 1.00 10.0 C 1.0 6252.2 6 .0 309.9 T 573.3 8356.7 1.00 310.4 T 716.3 8788.1 7 .0 34.5 T 64.6 9404.8 1.00 35.0 T 1.2 6312.0 8 .0 207.8 T 432.3 391.1 1.00 225.8 T 536.5 185.5 9 .0 1.3 T 46.1 395.0 1.00 19.2 T 0.2 207.5 8906.1 98.6 0.9 9238.1 60.1 0.9 8709.3 33.0 7.2 9239.7 36.3 7.2 9348.9 5.1 6.4 9506.4 8.3 6.4 1318.0 48.2 4.8 1030.7 72.2 4.8 603.1 69.1 4.2 444.6 51.3 4.2 9234.4 77.5 0.3 6263.2 236.3 0.3 9239.9 138.4 8.6 6814.8 135.2 8.6 9503.8 166.4 3.9 6348.2 163.1 3.9 1031.2 49.2 6.2 947.8 71.2 6.2 442.4 70.2 2.8 226.9 50.2 2.8 5 .0 7.5 C 0.6 6252.2 6260.4 253.7 0.0 1.00 16.2 C 0.0 0.0 16.2 412.4 0.0 6 .0 311.4 T 870.0 5788.1 6969.5 309.9 52.0 1.00 311.9 T 0.0 0.0 311.9 306.7 52.0 7 .0 37.5 T 6.8 6312.0 6356.3 337.9 0.4 1.00 38.0 T 0.0 0.0 38.0 334.6 0.4 8 .0 227.9 T 652.0 185.5 1065.4 50.3 39.0 1.00 245.9 T 0.0 0.0 245.9 70.1 39.0 9 .0 22.5 T 5.5 207.5 235.5 71.3 0.3 1.00 40.4 T 0.0 0.0 40.4 49.1 0.3 5 .0 468.9 C 0.0 7187.6 7656.6 700.7 0.0 1.00 468.1 C 0.0 1473.1 1941.3 699.2 0.0 6 .0 775.2 T 48.9 7494.8 8318.9 379.1 12.2 1.00 775.6 T 157.2 4395.6 5328.4 380.1 12.2 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 82 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG - PAGE NO. 83 *4GBA WITH RAFTER STIFFENER MEMBER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 133 134 135 136 7 .0 306.9 T 0.9 5652.7 5960.6 879.4 0.1 1.00 307.4 T 0.3 1530.8 1838.4 880.3 0.1 8 .0 242.3 T 36.7 411.7 690.7 222.1 9.1 1.00 243.1 T 117.9 2218.7 2579.6 220.6 9.1 9 .0 108.8 C 0.7 969.9 1079.5 153.1 0.1 1.00 108.1 C 0.2 2226.1 2334.4 154.6 0.1 5 .0 164.2 C 0.0 435.5 599.6 375.1 0.0 1.00 147.4 C 0.1 2014.8 2162.3 321.3 0.0 6 .0 344.8 T 65.2 1299.4 1709.4 266.7 18.2 1.00 345.1 T 48.9 581.1 975.2 267.8 18.2 7 .0 73.2 T 0.1 452.6 525.9 360.3 0.2 1.00 73.5 T 1.8 2991.8 3066.8 361.4 0.2 8 .0 139.5 T 48.9 655.9 844.3 72.2 13.7 1.00 152.2 T 36.8 1020.2 1209.2 31.3 13.7 9 .0 64.2 C 0.1 658.1 722.4 2.0 0.2 1.00 51.5 C 1.2 787.8 840.4 38.8 0.2 5 .0 96.1 C 0.1 2014.8 2111.0 370.7 0.0 1.00 84.5 C 0.4 5166.8 5251.7 289.7 6 .0 301.4 T 36.0 581.1 918.5 340.2 72.6 1.00 301.6 T 652.8 3836.1 4790.5 341.8 72.6 7 .0 25.4 T 1.4 2991.8 3018.6 307.1 0.5 1.00 25.6 T 5.2 5931.6 5962.5 308.8 0.5 8 .0 156.3 T 27.1 1020.2 1203.6 14.1 54.4 1.00 165.1 T 489.9 861.4 1516.4 47.3 54.4 9 .0 50,6 C 1.1 787.8 839.5 38.8 0.4 1.00 41.9 C 4.2 710.3 756.4 22.6 0.4 5 .0 84.6 C 0.3 5166.8 5251.8 274.8 0.0 1.00 60.9 C 0.2 8835.4 8896.5 116.1 0.0 6 .0 304.7 T 520.5 3836.1 4661.3 204.5 11.2 1.00 305.2 T 708.4 7705.9 8719.6 207.8 11.2 7 .0 28.7 T 2.3 5931.7 5962.6 176.6 1.4 1.00 29.2 T 25.2 9277.6 9331.9 179.9 1.4 8 .0 167.0 T 390.6 861.4 1419.0 47.1 8.4 1.00 185.0 T 531.2 616.2 1332.4 73.3 8.4 9 .0 40.0 C 1.9 710.3 752.2 68.1 1.0 1.00 22.0 C 16.8 862.6 603.3 52.3 1.0 5 .0 58.7 C 0.2 8835.4 8894.3 98.6 0.0 1.00 35.0 C 0.4 9197.2 9232.6 60.1 0.0 6 .0 307.1 T 704.3 7706.0 8717.4 33.0 9.0 1.00 307.6 T 553.6 8356.6 9217.8 36.3 9.0 7 .0 31.0 T 33.5 9277.6 9342.0 5.1 6.7 1.00 31.5 T 78.0 9404.3 9513.8 8.4 6.7 8 .0 187.6 T 528.1 616.2 1331.9 48.2 6.7 1.00 205.6 T 415.5 390.8 1011.9 72.2 6.7 9 .0 19.5 C 25.0 562.6 607.0 69.1 5.0 1.00 1.5 C 58.2 394.9 454.7 51.3 5.0 C:\at work\HORTON\6 BAYS\I3GG3ORR.ani Page 83 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 84 *4GBA WITM RAFTER STIFFENER MEMBER STP. ESSES ALL UNITS A~E POUN/SQ INCH MEMB LD SECT AXIAL BEND-¥ BEND - Z COMBINED SHEAR-Y SHEAR-Z 137 138 139 140 141 5 .0 32.6 C 0.4 9197.2 9230.1 77.5 0.0 1.00 8.9 C 0.2 6252.1 6261.2 236.3 0.0 6 .0 309.1 T 552.0 8356.6 9217.7 138.4 10.4 1.00 309.6 T 725.4 5788.1 6823.1 135.2 10.4 7 .0 33.0 T 78.8 9404.3 9516.1 166.4 7.2 1.00 33.5 T 41.1 6311.8 6386.4 163.1 7.2 8 .0 208.1 T 414.2 390.8 1013.1 49.3 7.8 1.00 226.0 T 543.9 185.4 955.3 71,1 7.8 9 .0 1.0 T 58.8 394.9 454.7 70.2 5.4 1.00 18.9 T 30.6 207,4 257.0 50.2 5.4 5 .0 6.4 C 0.2 6252.1 6258.6 253.7 0.0 1.00 17.3 C 0.0 0.0 17.3 412.4 0.0 6 .0 310.8 T 876.8 5788.1 6975.8 309.9 52.4 1.00 311.3 T 0.0 0.0 311.3 306.7 52.4 7 .0 36.0 T 36.9 6311.8 6384.7 337.8 2.2 1.00 36.4 T 0.0 0.0 36.4 334.6 2.2 8 .0 228.3 T 657.5 185.3 1071.1 50.3 39.3 1.00 246.3 T 0.0 0.0 246.3 70.1 39.3 9 .0 22.1 T 27.5 207.4 257.1 71.2 1.6 1.00 40.1 T 0.0 0.0 40.1 49.1 1.6 5 .0 468.6 C 0.9 7189.1 7658.6 701.1 0.2 1.00 467.9 C 3.1 1471.1 1942.1 699.6 0.2 6 .0 774.2 T 48.3 7495.7 8318.3 379.6 12.3 1.00 774.7 T 157.7 4392.6 5325.0 380.5 12.3 7 .0 306.5 T 2.0 5654.0 5962.5 879.9 0.1 1.00 307.0 T 1.2 1533.4 1841.6 880.8 0.1 8 .0 241.8 T 35.6 411.3 688.7 222.0 9.1 1.00 242.6 T 116.0 2217.9 2576.5 220.5 9.1 9 .0 108.9 C 0.8 970.0 1079.7 153.1 0.2 1.00 108.2 C 1.4 2226.6 2336.2 154.7 0.2 5 .0 164.5 C 6.4 434.8 605.7 378.1 0.8 1.00 147.7 C 11.7 2015.7 2175.2 321.3 0.8 6 .0 344.6 T 60.1 1298.6 1703.3 266.7 18.6 1.00 345.0 T 56.3 582.3 983.6 267.8 18.6 7 .0 73.5 T 7.3 453.4 534.1 360.3 1.1 1.00 73.8 T 14.5 2992.8 3081.1 361.4 1.1 8 .0 139.2 T 49.7 655.7 844.6 72.2 13.3 1.00 151.9 T 33.8 1020.0 1205.7 31.4 13.3 9 .0 64.2 C 0.9 658.3 723.3 2.0 0.2 1.00 51.5 C 2.4 787.9 841.8 38.8 0.2 5 .0 96.4 C 7.1 2015.8 2119.3 370.7 0.3 1.00 84.8 C 4.8 5167.7 5257.4 289.7 0.3 6 .0 301.2 T 40.2 582.3 923.8 340.2 71.5 1.00 301.5 T 647.8 3837.2 4786.5 341.8 71.5 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 84 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 85 *4GBA WITH RAFTER STIFFENER ME~ER STRESSES ALL UNITS ARE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEltR-Z 142 143 144 145 7 .0 25.7 T 9.2 2992.8 3027.7 307.1 0.3 1.00 25.9 T 6.4 5932.7 5965.0 308.8 0.3 8 .0 156.1 T 25.0 1020.0 1201.0 14.1 53.8 1.00 164.8 T 482.3 861.2 1508.4 47.3 53.8 9 .0 50.6 C 1.7 787.9 840.2 38.8 0.0 1.00 41.8 C 1.3 710.4 753.5 22.6 0.0 5 .0 85.4 C 0.9 5167.7 5254.0 274.8 0.7 1.00 61.7 C 10.9 8836.0 8908.7 116.0 0.7 6 .0 305.1 T 510.6 3837.2 4653.0 204.5 12.8 1.00 305.6 T 724.7 7706.7 8737.1 207.7 12.8 7 .0 29.7 T 1.5 5932.7 5963.9 176.6 1.4 1.00 30.2 T 28.4 9278.2 9330.8 179.8 1.4 8 .0 166.8 T 382.3 861.2 1410.3 47.1 10.1 1.00 184.8 T 551.5 616.0 1352.2 73.3 10.1 9 .0 39.8 C 1.8 710.4 752.0 68.1 1.6 1.00 21.8 C 24.7 562.6 609.2 52.3 1.6 5 .0 59.8 C 9.9 8836.1 8905.7 98.6 0.8 1.00 36.1 C 3.6 9197.5 9237.3 60.1 8.8 6 .0 307.9 T 724.5 7706.8 8739.1 33.0 12.5 1.00 308.4 T 516.2 8357.1 9181.7 36.3 12.5 7 .0 32.4 T 33.5 9278.2 9344.2 5.1 7.6 1.00 32.9 T 94.0 9404.7 9531.6 8.4 7.6 8 .0 187.4 T 550.5 616.0 1353.9 48.2 9.9 1.00 205.4 T 384.5 390.7 980.6 72.2 9.9 9 .0 19.2 C 32.3 568.6 614.1 69.1 6.3 1.00 1.3 C 73.1 395.0 469.4 51.3 6.3 5 .0 33.7 C 2.4 9197.6 9233.6 77.5 0.2 1.00 10.0 C 0.6 6252.2 6262.7 236.3 0.2 6 .0 309.8 T 513.5 8357.1 9180.5 138.5 14.5 1.00 310.3 T 756.5 5788.3 6855.1 135.2 14.5 7 .0 34.4 T 99.5 9404.7 9538.6 166.4 11.1 1.00 34.9 T 85.7 6312.0 6432.6 163.1 11.1 8 .0 207.8 T 383.4 390.7 981.9 49.3 11.0 1.00 225.8 T 567.8 185.3 978.8 71.1 11.0 9 .0 1.2 T 76.3 395.0 472.6 70.2 8.4 1.00 19.2 T 64.7 207.4 291.3 50.2 8.4 5 .0 7.5 C 0.2 6252.2 6260.0 253.7 0.0 1.00 16.2 C 0.0 0.0 16.2 412.4 0.0 6 .0 311.8 T 907.0 5788.3 7007.1 310.0 54.3 1.00 312.3 T 0.0 0.0 312.3 306.7 54.3 7 .0 37.4 T 84.9 6312.0 6434.3 337.9 5.1 1.00 37.9 T 0.0 0.0 37.9 334.6 5.1 8 .0 228.2 T 680.5 185.3 1093.9 50.3 40.7 1.00 246.1 T 0.0 0.8 246.1 70.1 40.7 9 .0 22.4 T 63.9 207.4 293.7 71.2 3.8 1.00 40.3 T 0.0 0.0 40.3 49.1 3.8 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 85 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 86 *4GEA WITH RJkFTER STIFFENER MEMBER STP. ESSES ALL UNITS ABE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z C(~4BINED SHEAR-Y SHEAR-Z 146 147 148 149 150 5 .0 471.4 C 252.2 7097.3 7821.0 656.6 53.4 1.00 470.7 C 222.0 1742.7 2435.4 655.1 53.4 6 .0 776.3 T 236.2 7420.0 8432.5 345.3 30.4 1.00 776.8 T 33.8 4596.8 5407.3 346.2 30.4 7 .0 309.8 T 273.0 5549.1 6131.9 829.1 62.1 1.00 310.2 T 278.8 1224.1 1813.2 830.0 62.1 8 .0 241.4 T 5.5 421.0 667.9 215.5 15.9 1.00 242.1 T 135.4 2174.4 2551.9 214.0 15.9 9 .0 108.5 C 22.1 982.2 1112.9 147.3 7.9 1.00 107.8 C 48.4 2191.3 2347.5 148.8 7.9 5 .0 185.9 C 114.4 515.2 815.5 364.1 17.6 1.00 169.1 C 224.5 1857.6 2251.2 310.3 17.6 6 .0 360.1 T 17.6 1359.0 1736.7 258.0 32.2 1.00 360.5 T 219.4 460.7 1040.6 259.1 32.2 7 .0 97.3 T 134.0 361.9 593.2 347.7 18.1 1.00 97.6 T 247.5 2812.6 3157.7 348.8 18.1 8 .0 135.3 T 69.7 642.8 847.8 70.7 11.4 1.00 148.0 T 2.0 996.7 1146.8 29.9 11.4 9 .0 61.8 C 17.7 647.8 727.3 3.4 0.9 1.00 49.1 C 23.1 767.2 839.4 37.4 0.9 5 .0 124.2 C 233.5 1857.5 2215.2 372.6 46.2 1.00 112.6 C 159.6 5027.9 5300.2 291.7 46.2 6 .0 322.2 T 215.8 460.6 998.6 341.6 32.1 1.00 322.5 T 489.0 3729.4 4540.9 343.3 32.1 7 .0 57.3 T 257.5 2812.5 3127.3 309.4 54.3 1.00 57.5 T 203.9 5773.7 6035.1 311.0 54.3 8 .0 151.7 T 7.2 996.7 1155.6 14.4 57.6 1.00 160.4 T 482.4 840.8 1483.6 47.0 57.6 9 .0 47.1 C 24.1 767.2 838.4 38.5 7.2 1.00 38.3 C 37.3 692.4 768.0 22.9 7.2 5 .0 111.6 C 147.1 5024.7 5283.4 276.3 10.3 1.00 87.9 C 24.6 8722.5 8835.1 117.6 10.3 6 .0 324.7 T 364.8 3726.8 4416.2 205.7 25.7 1.00 325.2 T 794.5 7618.5 8738.2 208.9 25.7 7 .0 60.2 T 191.9 5770.5 6022.6 178.4 16.5 1.00 60.7 T 84.8 9150.0 9295.5 181.6 16.5 8 .0 162.5 T 380.0 840.5 1383.0 47.4 11.8 1.00 180.4 T 578.1 600.0 1358.5 73.0 11.8 9 .0 35.9 C 37.4 692.3 765.6 67.9 5.0 1.00 17.9 C 45.8 548.6 612.3 52.5 5.0 5 .0 85.4 C 9.3 8721.3 8816.1 100.4 0.7 1.00 61.7 C 1.7 9116.2 9179.6 58.3 0.7 6 .0 326.0 T 784.6 7617.4 8728.0 34.4 20.2 1.00 326.5 T 446.2 8293.3 9066.0 37.6 20.8 C:\at work\HORTON\6 BAYS\13GG3ORR.anl Paqe 86 of 89 Wednesday, January 28, 2009, 02:23 PM -- PAGE NO, 87 SYSTEM 4E CLT-13GG *4GBA WITH P. AFTEE STIFFENER MEMBER STRESSES ALL UNITS APE POUN/SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SSEAR-Y SHEltR-Z 151 152 7 .0 62.2 T 77.7 9148.9 9288.7 7.1 12.8 1.00 62.7 T 136.0 9313.3 9512.0 10.4 12.8 8 .0 182.5 T 581.7 600.0 1364.1 48.5 14.7 1.00 200.4 T 335.9 379.7 915.9 71.9 14.7 9 .0 15.4 C 51.5 548.6 615.6 68.9 9.1 1.00 2.5 C 100.8 385.4 488.7 51.5 9.1 5 .0 58.8 C 0.2 9117.4 9176.4 75,5 0.0 1.00 35.2 C 0.2 6209.3 6244.7 234.3 0.0 6 .0 327.3 T 454.1 8294.2 9075.6 136.9 21.4 1.00 327.8 T 812.5 5754.4 6894.6 133.7 21.4 7 .0 64.2 T 131.4 9314.6 9510.2 164.1 16.2 1.00 64.7 T 138.8 6264.0 6467.4 160.9 16.2 8 .0 202.6 T 340.4 379.8 922.9 49.5 16.1 1.00 220.6 T 609.2 179.6 1009.4 70.9 16.1 9 .0 5.3 T 98.7 385.5 489.5 69.9 12.1 1.00 23.3 T 103.9 202.5 329.7 50.5 12.1 5 .0 32.5 C 0.0 6212.5 6245.0 251.6 0.0 1.00 8.8 C 0.0 0.0 8.8 410.3 0.0 6 .0 328.6 T 963.3 5757.1 7049.0 308.3 57.6 1.00 329.1 T 0.0 0.0 329.1 305.1 57.6 7 .0 66.5 T 140.1 6267.3 6473.9 335.5 8.4 1.00 67.0 T 0.0 0.0 67.0 332.2 8.4 8 .0 222.7 T 722.5 179.9 1125.1 50.6 43.2 1.00 240.7 T 0.0 0.0 240.7 69.8 43.2 9 .0 26.2 T 105.1 202.7 333.9 71.0 6.3 1.00 44.1 T 0.0 0.0 44.1 49.4 6.3 ************** END OF LATEST ANALYSIS P~ESULT ************** 179. FINISH C: \at work\HORTON\6 BAYS\13GG3ORR.anl Page 87 of 89 Wednesday, January 28, 2009, 02:23 PM SYSTEM 4E CLT-13GG -- PAGE NO. 88 *4GBA WITH RAFTER STIFFENER *********** END OF THE STAAD.Pro RUN *********** **** DATE= JA2g 28,2009 TIME= 14: 1: 6 **** For questions on STAAD.Pro, please contact Research Engineers Offices at the following locations Telephone USA: +1 (714)974-2500 CA/g/~DA +1 (905) 632-4771 CANADA +1 (604) 629 6087 UK +44(1454)207-000 FRANCE +33(0)1 64551084 GEP~L~NY +49/931/40468-71 NORWAY +47 67 57 21 30 SINGAPORE +65 6225-6015/16 INDIA JAPAN CHINA THAILAND support@reiusa.com detech@odandetech.com staad@dowco.com support@reel.co.uk support@reel.co.uk info@reig.de staad@edr.no support@relasia.net +91(033)2357-3575 support@calcutta.reiusa.com * +81(03}5952-6500 eng-eye@crc.co.jp +86(411)363-1983 support@reiasia.net +66(0)2645-1018/19 support@thai.reiusa.com * North America support@reiusa.com * Europe support@reel.co.uk * Asia support@reiasia.net c:\at work\HORTON\6 BAYS\13GG3ORR.anl Page 88 of 89 SYSTEM 4E CLT-13GG *4GBA WITH RAFTER STIFFENER Information about the key files in the current distribution Wednesday, January 28, 2009, 02:23 PM -- PAGE NO. 89 Modification Date CRC Size (Bytes) File Name 07/18/2006 0x3881 13000704 07/18/2006 0x100 05738496 09/19/2003 0x2fc0 00081970 05/30/2006 0x3c0 02486272 01/23/2001 0x9b40 00073728 09/25/2003 0x6340 00704512 09/22/2003 0xce00 00069632 12/22/2005 0x4181 00094208 01/03/2006 0x81cl 00493568 06/13/2006 0xd4cl 01204224 01/05/2005 0x79cl 00319488 01/05/2005 0x4bS1 01810432 01/05/2005 0xcacl 03651584 01/27/2005 0xeb01 00552960 01/05/2005 0xcd01 00163840 01/05/2005 0x6a41 00229376 07/08/2005 0xgd41 00434176 06/28/2005 0x8201 00327680 01/05/2005 0xabc0 00262144 05/31/2005 0xges1 00450560 06/09/2006 0xlfS1 00774144 01/05/2005 0xd6c0 00600064 01/05/2005 0xla00 00354304 01/05/2005 0xd301 00202752 01/05/2005 0xllcl 00233472 01/05/2005 0x3c40 00264192 01/05/2005 0xd540 00180224 03/23/2006 Oxa080 00200704 11/08/2005 0x9081 00376832 01/05/2005 0xb740 00174080 02/03/2005 0xda00 00096256 02/07/2005 0xga00 00243712 06/13/2006 0x3501 00421888 02/03/2005 0x9b40 00307200 01/05/2005 0x9081 00206848 01/06/2005 0x9341 00194560 01/04/2006 0x8680 00223232 01/05/2005 0xbac0 00149504 01/20/2006 0xSe40 00159744 SProStaad.exe SProStaadStl.exe CMesh.dll dbSectionInterface.dll LoadGen.dll MeshEngine.dll QuadPlateEngine.dll SurfMesh.dll aiscsections.mdb AISCSectionsRCeco.mdb aiscsections all editions.mdb aiscsteeljoists.mdb aitctimbersections.mdb aluminumsections.mdb australiansections.mdb britishsections.mdb bscoldformedsections.mdb butlercoldformedsections.mdb canadiansections.mdb canadiantimbersections.mdb ChineseSections.mdb dutchsections.mdb europeansections.mdb frenchsections.mdb germansections.mdb indiansections.mdb iscoldformedsections.mdb japanesesections.mdb Kingspancoldformedsections.mdb koreansections.mdb lysaghtcoldformedsections.mdb mexicansteeltables.mdb RCecoColdFormedSections.mdb russiansections.mdb southafricansections.mdb spanishsections.mdb uscoldformedsections.mdb usersectionstemplate.mdb venezuelansections.mdb C: %at work\HORTON\6 BAYS\13GG3ORR.anl Page 89 of 89 STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS SHEET NO: 1 OF: 20 CALCULATED BY: CHECKED BY: ENG NUMSER~ _ Bob Lupo DATE: DATE: 11/01/01 JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 2 OF: 20 CALCULATED BY: BobLupo DATE: 11/01/01 CHECKED BY: DATE: ENG NUMBER: SYSTEM 4 REGULAR BAR W/RAFTER STIFFENER (4GBA+4RSB) ALLOY:6005-TS, 6005-T5 II SPEC 3.4.2 I.= 19000 psi SPEC 3.4.7 I KL/r = 194" / 1.543" = 126 o = 51000 / ( 126 )2 = 3226 psi blt = 1.395 "/0.090" = 15.5 * = 19000 psi SPEC 3.4.16 I blt = .848" ! 0.120" = 7.1 c =21000 psi SPEC 3.4.18 I h/t= 1.395"/0.090" = 15.5 c =28000 psi MAXIMUM ALLOWABLE STRESSES COMPRESSION: = 3226 psi BENDING: = 19000 psi JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 3 OF: 20 CALCULATED BY: Bob LuDo DATE: 11/01/01 CHECKED BY: DATE ENG NUMBER: SYSTEM 4 HEAVY BAR {4HBA) ALLOY:6005-T5 II SPEC 3.4.2 {x= 19000 psi SPEC 3,4.7 I I KL/r = 119 "/.796" = 149.5 ~ = 51000 / ( 149.5 )2 = 2282 psi bit = 1.233 "/0.140" = 9 o-= 19000 psi SPEC 3.4,16 I blt = 1.43" ! 0.257" = 5.5 ~ =21000 psi SPEC 3.4.18 I hit=.1.233"~0.140"=9 ~ =28000 psi MAXIMUM ALLOWABLE STRESSES COMPRESSION: = 2282 p~i BENDING: = 19000 psi JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway HolDrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 4 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01/01 CHECKED BY: DATE: ENG. NUMBER: SYSTEM 4 HEAVY BAR W/RAFTER STIFFENER {4HBA+4RSB) ALLOY: 6005-T5, 6005-T5 II ~PE¢ 3.4.2 lo = 19000 psi SPEC 3.4.7 I KL/r= 194"/1.496" = 130 r = 51000 / ( 130 )2 = 3033 psi bit = 1.233" / 0.140" = 9 ~ = 19000 psi SPEC 3.4.16 blt = 1.43" / 0.257" = 5.5 ~ =21000 psi SPEC 3.4.18 hit = 1.233" / 0.140" = 9 o =28000 psi MAxIMuM ALLOWABLE STRESSES COMPRESSION: = 3033 psi BENDING: = 19000 psi JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Hotbrook, New York 11741 ($16) 563-4000 Fax: (516) 218-9076 SHEET NO: 5 OF: 20 CALCULATED BY: BobLup0 DATE: 11/01/01 CHECKED BY: DATE: ENG. NUMBER: !SYSTEM 4 GABLE MULLION BAR (4GMA) ALLOY:6005-T5 SPFC 3.4.2 Io= 19000 psi SPEC 3.4,7 kL/r = 139" / .863" = 161 (~ = 51000 / ( 161 )2 = 1966 psi blt = 1.905 "/0.080" = 23.8 (~ = 23.1 - 0.25 ( 23.8 ) = 17147 ps~ bit = 1.55" / 0.080" = 19.375 ~ =21000 psi SPEC 3.4.18 I blt = .1.905" / 0.080" = 23.8 ~ =28000 psi MAXIMUM ALLOWABLE STRESSES COMPREsSiON: = 1966 psi BENDING: = 19000 psi JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 6 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01/01 CHECKED BY: DATE ENG. NUMBER: SYSTEM 4 GABLE MULLION BAR W/RAFTER STIFFENER {4GMA+4RSB) ALLOY:6005-T5, 6005-T5 SPEC 3.4.2 I(~ = 19000 psi SPEC3.4.71 I KL/r= 185"/1.555"= 119 c~ = 51000 / ( 119 )2 = 3603 psi blt = 1.905" / 0.080": 23.8 ~= 23.1 -0.25 (23.8)= 17147 psi ~/t = 1.55" / 0.080" = 19.375 r =21000 psi SPEC 3.4.18 I hit: 1.905 "/0.080": 23.8 ~ =28000 psi MAXIMUM ALLOWABLE STRESSES ;OMPRESSION: = 3603 psi ~ENDING: = 19000 psi JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 7 OF: 20 CALCULATED BY: BobLupo DATE: 11~1101 CHECKED BY: DATE: ENG. NUMBER: 118" SILL CLiP ANGLES TO BASE ALLOYS: 6063-T5 SCREWS: 2 - 3/8" LAG BOLTS ( 1 PER CLIP ANGLE CONNECTION BEARING _ _ Phs = 1 / 1.65 ( .375 ")( 0.125 ")( 26 ksi) = 739# ...... Pns= ~ / 2.34 ( .375 ")( 0.125 ")(46 ksi) = 921 # _ . Pas = 2' 739#= 1478# CONNECTION TENSION~ Pnov = ( 0.125 ")( .75" - .375 ")( 22 ksi)/3 = 344 # _ Pat = 2' 344 #= 688# MAXIMUM ALLOWABLE LOADS TENSION: 688 # SHEAR: 1478 # NOTE: THESE CALCULATIONS PERTAIN TO THE CONNECTIONS UP TO, BUT NOT INCLUDING, THE CONNECTIONS TO THE EXISTING STRUCTURE AND/OR ANY NEW CONSTRUCTION. THE CONNECTIONS TO THE EXISTING STRUCTURE AND/OR ANY NEW CONSTRU_CTION _ - _ _MUST B_E ANALYZED ACCORDING TO CONDITIONS SPE_ClFIC TO EACH JOB BY OTHERS--__ JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 8 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01/01 CHECKED BY: ! DATE: ENG NUMBER: SYSTEM 4 REGULAR BAR (4GBA) TO 118" SILL CLIP ANGLES SCREWS: 3-# 10" x 1 1/4"SCREWS CONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0.090 ")( 56 ksi) = 580 # Phs = 1 / 1.65 ( .19 ")( 0.125 ")( 26 ksi) = 374 # Pns= 1 / 2,34 ( .19 ")( 0.090 ")( 80 ksi) = 585 # Phs = 1 / 2.34 ( .19 ")( 0.125 ")( 46 ksi) = 467 # Pas = 3'374#= 1122# MAXIMUM ALLOWABLE LOADS TENSION: 1122 # SHEAR: 1122 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 9 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01/01 CHECKED BY: DATE: ENG. NUMBER SYSTEM 4 HEAVY BAR (4HBA)TO 118" SILL CLIP ANGLES SCREWS: 3-# 10" x 1 1/4" SCREWS CONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0,140 ")( 56 ksi) = 903# Pns= 1 / 1.65 ( .19 ")( 0,125 ")( 26 ksi) = 374 # )ns = 1 / 2,34 ( ,19 ")( 0.140 ")( 80 ksi) = 909 # Phs = 1 / 2.34 ( .19 ")( 0.125 ")( 46 ksi) = 467 # Pas = 3' 374#= 1122# MAXIMUM ALLOWABLE LOADS TENSION: 1122 # ;HEAR: 1122# [ JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS 10 OF: 20 FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: CALCULATED BY: CHECKED BY: ENG NUMBER: Bob Lupo DATE: 11/01/01 DATE: SYSTEM 4 REGULAR BAR (4GBA) TO SPLICE CHANNEL SCREWS: 6 - #10 SCREWS ( 3 EACH SIDE) CONNECTION BEARING Phs = 1 / 1.65 ( .19 ")( 0.120 ")( 56 ksi) = 774# Phs = 1/1.65(.19")(.343")(39ksi)= 1540# Phs = 1 / 2.34 ( .19 ")( 0.120 ")( 80 ksi) = 779 # Pns=l/2.34(.19")(.343")(60ksi)= 1671# Pas =3.774#= 2322# CONNECTION TENSION Pnot = ( 0.85 )( .19 ")( ,343 ")( 32 ksi) = 1773 # / 3 = 591 # Pnov = (0.120")(.361 "-.19")(38 ksi)= 780#/3 = 260# Pat=3*260#= 780# MAXIMUM ALLOWABLE LOADS TENSION: = 780 # SHEAR: = 2322 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 {516) 563-4000 Fax: (516) 218-9076 SHEET NO: 11 Of: 20 CALCULATED BY: BobLupo DATE: 11/01/01 CHECKED BY: DATE: m ENG NUMBER: ISYSTEM 4 HEAVY BAR (4HBA) TO SPLICE CHANNEL SCREWS: 6 -#10 SCREWS ( 3 EACH SIDE) CONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0.257 ")( 56 ksi) = 1657 # Pns=l/1.65(.19")(.343")(39ksi)= 1540#1 Phs = 1 / 2.34 ( .19 ")( 0.257 ")( 80 ksi) = 1669 # Phs = 1 / 2.34 ( .19 ")( .343 ")( 60 ksi) = 1671 # Pas=3*1540#= 4620# ' CONNECTION TENSION Pnot = ( 0.85 )( .19 ")( ,343 ")( 32 ksi) = 1773 # / 3 = 591 # Pnov = ( 0.257 ")( ,361 "- ,19 ")( 38 ksi) = 1670 # / 3 = 557 # Pat= 3*557#= 1671# MAXIMUM ALLOWABLE LOADS TENSION: = 1671 # SHEAR: = 4620 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 12 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01/01 CHECKED BY: DATE: ENG NUMBER SYSTEM 4 REGULAR BAR (4GBA)TO 118" RIDGE CLIP ANGLES SCREWS: 4 - # 10" x 1 1/4" SCREWS CONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0.090 ")( 56 ksi) = 580# Pns= 1 / 1.65 ( .19 ")( 0.125 ")( 26 ksi) = 374 # Phs = 1 / 2.34 ( .19 ")( 0.090 ")( 80 ksi) = 585 # Pns= 1 / 2,34 ( ,19 ")( 0,125 ")( 46 ksi) = 467 # Pas=4*374#= 1496# MAXIMUM ALLOWABLE LOADS TENSION: 1496 # SHEAR: 1496 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Ho[brook, New York 11741 (516) 563-4000 Fax: (516} 218-9076 SHEET NO: 13 OF: 20 CALCULATED BY: BobLupo DATE: 11/01101 CHECKED BY: DATE: ENG. NUMBER: SYSTEM 4 HEAVY BAR (4HBA) TO 118" RIDGE CLIP ANGLES SCREWS: 4-# 10" x 1 1/4" SCREWS CONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0.140 ")( 56 ksi) = 903 # Pns= 1 / 1.65 ( .19 ")( 0.125 ")( 26 ksi) = 374 # Pns= 1 / 2.34 ( .19 ")( 0.140 ")( 80 ksi) = 909 # Phs = 1 /2.34 ( .19")( 0.125")(46 ksi) = 467# Pas =4'374 #= 1496# MAXIMUM ALLOWABLE LOADS TENSION: 1496 # SHEAFS: 1496 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 14 OF: 20 CALCULATED BY: Bob Lupo DATE: 11101/01 CHECKED BY: DATE: ENG. NUMBER: 1/8" RIDGE CLIP ANGLES TO RIDGE LEDGER SCREWS: 2 - # 10 SCREWS (2 PER CLIP ANGLE ) ;ONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0.125 ")( 26 ksi) = 374 # Pns= 1 / 1.65 ( .19 ")( 0.062 ")( 56 ksi) = 400 # Pns= 1 / 2.34 ( .19 ")( 0.125 ")( 46 ksi) = 467 # Phs = 1 / 2,34 ( .19 ")( 0.062 ")( 80 ksi) = 403 # Pas=4*374#= 1496# CONNECTION TENSION Pnot = ( 0.85 )( .19 ")( .062 ")( 38 ksi) = 380 # / 3 = 127 # Pnov = ( 0.125 ")( .361 "- .19 ")( 22 ksi) = 470 # / 3 = 157 # Pat =4' 127#= 508# MAXIMUM ALLOWABLE LOADS TENSION: 508 # SHEAR: 1496 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS 20 FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 {516) 563-4000 Fax: (516) 218-9076 SHEET NO: 15 OF: CALCULATED BY: BobLupo DATE: CHECKED BY: DATE: ENG NUMBER: 11/01101 RIDGE LEDGER TO SUPPORT STRUCTURE {BY OTHERS) SCREWS: 2 - 1/4" LAG BOLTS (W/WASHERS) x 3" MIN. EMBEDMENT @ 16" C.C. (4 PER RAFTER) CONNECTION BEARING Pns= 1 / 1.65 ( .25 ")( 0.062 '3( 56 ksi) = 526 # Phs = 1 / 2.34 ( .25 ")( 0.062 ")( 80 ksi) = 530 # Pas = 4' 526#= 2104# CONNECTION TENSION Pnov = ( 0.062 ")( .625" - .25 ")( 38 ksi) = 884 # / 3 = 295 # Pat = 4'295 #= 1.180# MAXIMUM ALLOWABLE LOADS TENSION: 1180 # SHEAR: 2104 # NOTE: THESE CALCULATIONS PERTAIN TO THE CONNECTIONS UP TO, BUT NOT INCLUDING THE CONNECTIONS TO THE EXISTING STRUCTURE AND/OR ANY NEW CONSTRUCTION. THE CONNECTIONS TO THE EXISTING STRUCTURE AND/OR ANY NEW CONSTRUCTION MUST BE ANALYZED ACCORDING TO CONDITIONS SPECIFIC TO EACH JOB BY OTHERS, I JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 16 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01101 CHECKED BY: DATE: ENG. NUMBER: SYSTEM 4 GABLE MULLION (4GMA) TO 118" SILL CLIP ANGLES SCREWS: 3 - # 10" x 1 1/4" SCREWS CONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0.080 ")( 56 ksi) = 516 #1 Pns= 1 / 1.65 ( .19 ")( 0.125 ")( 26 ksi) = 374 #1 Pns= 1 / 2.34 ( .19 ")( 0.080 ")( 80 ksi) = 520 # Pns= 1 / 2.34 ( .19 ")( 0.125 ")( 46 ksi) = 467 # Pas= 3'374#= 1122# MAXIMUM ALLOWABLE LOADS TENSION: 1122 # SHEAR: 1122 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS 17 OF: 20 FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 {516) 563-4000 Fax: (516) 218-9076 SHEET NO: CALCULATED BY: CHECKED BY: ENG. NUMBERi Bob Lupo DATE: 11/01/01 DATE: 118" STRAP (CN6104) TO GABLE MULLION (4GMA) ALLOYS: 6063-T5, 6005-T5 I I I SCREWS: 2-# 10 x 1 1/4" SCREWS CONNECTION BEARING Phs = 1 / 1.65 ( ,19 ")( 0,080 ")( 56 ksi) = 515 # Phs = 1 / 1,65 ( .19 ")( 0.125 ")( 26 ksi) = 374 # Phs = 1 / 2.34 ( .19 ")( 0.050 ")( 80 ksi) = 520 # Phs = I / 2.34 ( .19 ")( 0.125 ")( 46 ksi) = 467 # Pas=2*374#= 748# 1/8" STRAP (CN6104) SHEAR o = 5500 ps~ A -~ ( .125 ")( .5 ") = .0625 sqin I P = ( 5500 psi)( .0625 sqin) = 345 # /IAXlMUM ALLOWABLE LOADS _ TENSION: =748 # SHEAR: = 345 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Hoibrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 18 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01/01 CHECKED BY: DATE: ENG. NUMBER: 1/8" STRAP (CN6104)TO ROOF REGULAR BAR (4GBA) SCREWS: 2 -# 10 x 1 1/4" SCREWS CONNECTION BEARING Pns= 1 / 1.65 ( .19 ")( 0,090 ")( 56 ksi) = 580 # Phs = 1 / 1.65 ( .19")( 0.125 ")(26 ksi) = 374 # Pns= 1/2.34 (.19")(0.090")(80 ksi)= 585# Phs = 1 /2.34 (. 19 ")( 0.125 ")( 46 ksi) = 467 # Pas = 2* 374 # = 748 # 1/8" STRAP TENSION o = 9500 ps~ A = ( .125 ")( .5 ") = .0625 sqin P = ( 9500 psi)( .0625 sqin) = 594 # MAXIMUM ALLOWABLE LOADS TENSION: = 594 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS 19 OF: 20 FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: CALCULATED BY: CHECKED BY: ENG NUMBER: Bob Lupo DATE: 11/01/01 DATE: 118" STRAP {CN6104) TO SYSTEM 4 HEAVY BAR {4HBA) SCREWS: 2-# 10 x 1 1/4" SCREWS CONNECTION BEARING Pns= 1 / 1.65 ( ,19 ")( 0.140 ")( 56 ksi) = 904# Pns= 1 / 1.65 ( .19")(0.125")(26 ksi) = 374# Pns= 1 / 2,34 ( .19 ")( 0,140 ")( 80 ksi) = 910 # Phs = 1 / 2.34 ( .19 ")( 0,125 ")( 46 ksi) = 467 # Pas = 2* 374# = 748 # 1/8" STRAP TENSION o = 9500 ps~ A= ( .125 ")( .5 ") = .0625 sqin P = ( 9500 psi)( .0625 sqin) = 594 # MAXIMUM ALLOWABLE LOADS TENS Oh[:= 594 # JOB: STANDARD SYSTEM 4E ENGINEERING CALCULATIONS FOUR SEASONS SOLAR PRODUCTS 5005 Veterans Memorial Highway Holbrook, New York 11741 (516) 563-4000 Fax: (516) 218-9076 SHEET NO: 20 OF: 20 CALCULATED BY: Bob Lupo DATE: 11/01/01 CHECKED BY: DATE: ENG NUMBER: GLAZING CAPS TO ALUMINUM RAFTERS AND COLUMNS SCREWS: # 10 x 1-1/2" @ 9" ON CENTER MAXIMUM ALLOYS: 6005-T5, 6005-T5 CONNECTION TENSION Pnot= (0.5)( 0.85 )( 0.19 ")( 0.25 ")( 38 ksi) = 767 # / 3 = 255 # Pnov= ( 0.05 ")( .365" - .19 ")( 38 ksi) = 332.5 # / 3 = 110.8 # Pat= 110.8# *(12"/'/9")= 166.2#/' MAXIMUM ALLOWABLE LOADS TENSION: = 166.2 #/' / 3 ' = 55.4 PSF MAX APPENDIX Table 3 3 I ~' MINIMUM MECHANICAL PROPERTIES FOR ALUMINUM ALLOYS COMPRESSIVE ALLOY 13'IICKNE~S TENSION COMPRESSION SHEAR BEARING MODULUS OF AND pRODUCT' RANGE' I EL~S~CrW¢ TEMPER IN. Fm'~ F~, t Fey F.u F,,V Fbu Fby E ksi Esi ESl ESi ksl ESl ksi ket 1100-H12 /Sheet. Plate ) All 14 11 10 e gL om ,:1~ to1~ -H14 ~ Rolled Rod & Bar All 16 14 13 10 8 32 21 10,100 2014-T6 Sheet 0.040-0.24.9 66 58 59 40 33 125 93 10,900 -T651 Plate 0.250-2.000 67 59 58 40 34 127 94 10,900 -T6, T6510, T6511 Extrusions All 60 53 52 35 31 114 55 10,900 -T6, T651 Cold Finished Rod All 65 55 53 38 32 124 88 10,900 & Sar, Drawn Tube Alclad 10,800 2014-T6 Sheet 0.025-0.039 63 55 56 38 32 120 88 -T6 Sheet 0,040-0.249 64 57 58 39 33 122 91 10,000 -T651 Plala 0.259-0,49g 64 57 56 39 33 122 93 10,800 3003-H12 Sheet & Plate 0.017-2.000 17 12 10 11 7 34 19 10,100 0.009-1.000 20 17 14 12 10 40 25 10,100 0.006-O.162 24 21 18 14 12 46 31 10,100 0,006-0.128 27 24 20 15 14 49 34 10,100 All 17 12 11 11 7 34 19 10,100 All 20 17 16 12 10 40 25 10,100 All 24 21 19 14 12 46 31 10,100 All 27 24 21 15 14 49 34 10,100 -H14 Sheet & Plate -H16 Sheet -H18 Sheet 3003-H 12 Drown Tube -H14 Drown Tube -H16 Drawn Tube -H18 Drawn Tube Alclad 3003-H12 Sheet & Plate -H14 Sheet & Plate -H16 Sheet -H18 Sheet 3003-H14 Drawn Tube -H18 Drawn Tube 0.017-2.000 16 11 9 10 6.5 32 18 10,100 0.009-1.000 19 16 13 12 9 38 24 10,100 0,006-0.162 23 20 17 14 12 44 30' 10,100 0.006-0.128 26 23 19 15 13 47 32 10,100 0.025-0.259 19 16 15 12 9 38 24 10,100 0.010-0.500 26 23 20 15 13 47 32 10,100 3004-H32 Sheet & Plate 0.017-2,000 28 21 18 .H34 Sheet & Plate 0.009-1.000 32 25 * 22 -H36 Sheet 0.006-0.162 35 -28 25 -H38 Sheet 0.006-0.128 38 31 29 3004-H34 Drawn Tube 0,018-0.450 32 25 24 -H36 D~awn Tube 0.018-0.450 35 28 27 17 12 56 36 10,100 19 14 64 40 10,100 20. 16 70 45 10,100 21 18 72 45 10,.100 19 14 64 40 10,100 20 16 70 45 10,100 Aiclad 3004-H32 -H34 -H36 -H38 -H14 -H16 -H131, H241 -H151, H261 -H361 Sheet 0.017-0.249 27 20 17 16 12 54 34 10,100 . Sheet 0.009-0.249 31 24 21 18 ' 14 62 38 10,100 Sheet 0.006-~162 34- 27 24 19 16 68 43 10,100 Sheet 0.006-0.128 37 . 30 28 21 17 70 44 10,100 Shem & Plate 0,009-0.499 32 26 24 19 15 64 39 10,100 Sheet 0.006-0.162 35 30 28 20 17 * 66 45 10,100 Sheet 0,024o0.050 31 26 22 18 15 62 39 10,100 Sheet 0.024-0.0S0 34 30 28 lg 17 66 45 10,100 3005-H25 Sheet 0.013-0.050 26 22 20 15 13 49 35 10,100 -H2B Sheet 0.006,.0.080 31 27 25 17 16 56 38 10,100 3006-H391 Sheet 0.010-0,850 31 27 27 20 16 60 44 10,100 3105-H25 Sheet 0,013-0.080 23 19 17 14 11 44 28 10,100 5005-.H12 Shem&Plate 0.017-2.000 18 14 13 11 8 34 22 10,100 -H14 Sheet& Plate 0.009-1.000 21 17 15 12 10 40 25 10,100 -H16 Sheet 0,006-0.162 24 20 18 14 12 48 30 10,100 *H32 Sheet & Plate 0.017-2.000 17 12 11 11 7 34 20 1 O, 100 -H34 Sheet & Plate 0.009-1.000 20 15 14 12 8.5 40 24 10,100 -H36 Sheet 0.006-0.162 23 18 16 13 11 48 29 10,100 For all footnotes, see last page of this Table October 1994 I-A-17 Table 3.3-1 " MINIMUM MECHANICAL PROPERTIES FOR ALUMINUM ALLOYS COMPRESSIVE TENSION COMPRESSION SHEAR .BEARING MODULUS OF ALLOY THICKNESS ELASTtCITY~: AND PRODUCT' RANGE' TEMPr:R IN, Fro1. Flyt Fei F,u F~y Fbu Fby E bei ksi ksi ksi ksi ksi ksl ksi 5DSO-H32 -H34 -H32 5052-H32 Sheet 0.017-(3.249 22 16 14 14 9 Sheet 0.009-0.249 25 20 18 15 12 50 32 10,10e Cotd Fin. Rod & Bart All 22 16 15 13 9 44 27 10,100 Draw~ Tube Cold Fin. Rod & Bart All 25 20 19 15 12 50 32 10,100 Draw~ Tube · Sh.t 0.OOr,-0.1S~37 2~ ~s ~2 1~ 70 ,~s lO~OO 5083-H 111 Extrusions up thru 0.500 40 24 21 24 14 78 41 10,400 -H111 Extrusions 0.501 and over 40 24 21 23 14 78 38 10,400 -H321, H116 Sheet & plate 0,189-1.500 44 31 26 26 18 84 53 10,400 .H321, H116 Plate 1.501-3.000 41 29 24 24 17 75 49 10,400 -H323 Sheet 0.051-0.249 45 34 32 26 20 88 58 10,400 -H343 Sheet 0.051-0.249 50 39 37 29 23 95 66 10,400 5086-H111 Extrusions up thru 0.500 36 21 18 21 12 70 36 .10,400 -Hlll Extrusions 0.501 and over 36 21 18 21 12 70 34 10,400 -H112 Plate 0.250-0,499 36 18 17 22 10 72 31 10,400: -Hl12 Plate 0.500-1.000 35 16 16 21 9 70 28 10,400' -Hl12 Plate 1.001-2.000 35 14 15 21 8 70 28 10,400 -Hl12 Plate 2.001-3.000 34 14 15 21 8 68 25 10,400~ -El 16, H32 ( Sheet & Plate ) All 40 28 26 24 16 78 48 10,400, -H34 Drawn Tube All 44 34 32 26 20 84 58 10.400 Sheet 0,006-0.125 45 35 33 24 20 81 56 10,300 5154-H38 . 5454-Hlll . Extrusions up thru 0.500 33 19 16 20 11 64 32 10,400 -Hlll Extrusions 0.501 andover 33 19 16 19 11 64 . 30 10,400 -Hl12 Extrusions up thru 5.000 31 12 13 19 7 62 24 10,4D0 -H32 Sheet & Plate 0.020-2.~30 36 26 24 21 15 70 44 10,400 -H34 Sheet & Plate 0.020-1.000 39 29 27 23 17 74 49 10,400 5456-Hlll -H116, H321 -H116, H321 Extrusions up thru 0.500 42 26 * 22 25 15 82 44 10,4~0 Extrusions 0.501 and over 42 26 22 24 15 82 42 10,400 - Extrusions up thru 5.00 41 19 20 24 11 82 38 10,4C0 Sheet&Plate 0~188-1.250 46 33 27 .27 19 87 56 10,400 plate ' ' 1.251.1.500 44 31 25 25 18 84 53 10,400 · Plate 1.501-3.0D0 41 29 25 25 17 ' ~2 49 10,400 24 6005-T5 ExthJsions up thru 1,000 38 · 35 35 20 80 56 10,100 6105-T5 Extrusions up thru 0.500 38 35 35 24 20 80 56 10,100 6061-T6, T651 Sheet & Plate 0.01'0-4.000 42 35 35 27 20 88 58 10,100 -T6, T6510, T6511 Extrusions up thru 1.000 38 35 35 24 20 80 56 I0,100 -T6, T651 Cold Fin. Rod & Bar up thru 8.000 42 35 35 25 20 88 56 10,100 -T6 Drawn Tube 0.025-0.500 42 35 35 27 20 88 56 10,100 -T6 Pipe up thru 0.999 42 35 35 27 20 88 56 10,100 -T6 Pipe over 0.999 38 35 35 24 20 80 56 10,100 6063-T5 Extrusions up thru 0.500 22 16 16 13 9 46 26 10,100 -TS Exlrusions ' over 0,500 21 15 15 12 8.5 44 24 10,100 -T6 Extrusions & Pipe All 30 25 25 19 14 63 40 10,100 6351-T5 Extrusions up thru 1.00 38 35 35 24 20 80 56 10,100 · Most prociuct and thickne~ ~ange~ ars leiden from 'i'ne Aluminum Association 1993 edition of 'Aluminum Standards and Dat~' 1' F~ and F~ are minimum specified values (except F~, for 1100-H12, -H14 Cold Finished Rod and Bar and Drawn Tube, Alclad 3003-H18 Sheet snd 5050-H32, -H34 Cotcl Finished Rod and Bar which are minimum expected values.); other strength prope~es are corresponding minimum expected values. :i: Typical values. For detiection calculations an average modulus of elasticity is used; numerically this is 100 PSi lower than values in this For stress values in MPa mutt[ply the given values in Psi by 6,895, for thic~,:ness in mm multiply the given values by 25.4 I-A-18 October 1994 }:or angles, the gross width shall be the sum of the widths of the legs less the thickness. The gage for holes in opposite legs shall be the sum of the gages from the back of the angles, less the thickness. For splice members, the thickness shall be only that pas'~ of the thicimess of the member that has been developed by Hvets or bolts, beyond the section considered. 5.1.7 Effective Sections of Angles If n discontinuous angle (single or paired) in tension is connected to one side of n gusset pinto, the effective net section shall be the net section of the connected leg plus one-third of the section of the outsumd~g leg unless the outstanding leg is connected by a lug angle. In the latte, r c~c, the effective net section sh~l be thc entire net section of the angle. The lug angle shall be designed to develop at least one-half the total load in the member and shall be connected to the main member by at least two fasteners. For double angles pla~ed back-to-back and connected tn both sides of a guss~ plate, the effective net section shall be the net section of the connected legs plus two-thirds of the section of the outstanding legs. For intormediam joints of continuous angles, the effec- tive net area shall be the gross sectional area less deductions for holes. 5.1.8 Grip of Rivets, Screws and Bolts If the grip (total thickness of meUg being fastened) of rivets, screws or bolts carrying calculated stress exceeds four and one-half times the diameter, the allowable load per rivet, sc'rew or bolt shall be raduced. The ~vxinced allowable load shall be the norm01 allowable load divided by [lf2+G/(gD)] in w]ainh G is the grip and D is the nominal' diameter of the rivet or bolt. If the grip of the rivet exceeds six times the diameter, special care shall be taken to insure that holes will be f-filed completely. 5.1.9 Spacing of Rivets, Screws and Bolts Minimum distance between rivet centers shall be 3 times the nominal rivet diameter, minimum distance of bolt or screw centers shall be 2~ ~mes the nominal diameter. In built-up comp~ssicu members the pitch in the direction of stress shall be such that the allowable stress on the individ- ual outside sheets and shapes, treated as columns having an effective ]angth cqual to one half thc rivet, scrc.w or bolt pitch exceeds the calculated s~css. The gage at right angles to the direction of stress shall be such that the allowable s~ess in the outside sheets, calculated from Section 3.4.9 exceeds the calculated stress. In this case the width b in Section 3.4.9 shall be permitted to be taken as 0.Sg where 'g" is the gage. 5.1.1'0 Spacing of Stitch Rivets, Screws and Bolts in Webs Where two or more web plates are in contact, there shall be stitch rivets, screws or bolts to make them act in unison. In compression members, the pitch and gage of such rivets or bolt~ shall be determined as outlined in Section 5.1.9. In · tension mcrnbers, the maximum pitch or gage of such rivets, scr~vs or bolts shall not exceed a distance, in inches, equal to 3+20t. (in mm 76 + 200 in which t is thc thickness of the outside plates. 5.1.11 Edge Distance of Rivets, Screws or Bolts The miniraum distance from the c~nt~r of rivet, screw or bolt under compu~ad stress to the edge of the sheet or shape toward which thc pressure is directed shall be twice the nominal diameter of the riv~ screw or bolt when using the allowable beaxing stress shown in Tables 5.1.1.3-1 and -2. When a thoner edge distance is used, the allowable bearing stress shall be reduced by the ratio: actual edge dis- tanceJtwice the fastener diameter (See Section 3.4.5). The edge distance shall not be less than 1.5 times the fastener diameter to extruded, sheared, sawed, rolled or planed 5.1.12 Blind Rivets Blind rivets shall not be used unless~he ~rip'tan~hs and ~et-bole tolerances are as recommended by the respective manufacturers. 5.1.13 Hollow-End (Semi-tubular) Rivets If hollow-end rivets with solid cross sections for a portion of the length are u~ed, the strength of these rivets shall not be mkan equal to the strength of solid rivets of the same material, unless thc bottom of thc cavity is at least 25 percent of the rivet diameter from th~ plane of shear, as measurod toward th~.hollow-end, and further provided that they are used in locations where they will not be subjected to appreciable tensile stresses. 5.1.14 Steel Rivets Steel rivets shall not be used in alum~um struc~res unless the aluminum is to be joined to steel or where corrosion resistance of the smacmre is not a reqnlrement, or where the sm~cture isto be protected against corrosion (See Section 6.6.1). 5.1.15 Lockbolts Lockbolts shall be per'milled to be used when installed in conformance with the lockbolt manufactorer% recom- mended practices and provided that the body diameter and bern-lng areas under the head and nut, or their equivalent, are not less than those of a convanfional nut and bolt. October 1994 I-A-59 $.1.16 Steel Bolts Hot-dip galvanized, electro-galvanized and aluminized steel bolts and 300 series stainless steel bolts shall be used as an alternative to aluminum bolts. Plating thickness on stol bolts must be adequate to provide corrosion protection for the anticlpatod environment and service life. Hot-dipped galvanized A490 bolts shall not be used. Coated steel fastenerS shall be installed with a lubricant to eliminate galling and assure adequate preload. 5.2 Metal Stitching Staples Allowable strength values for metal stitches in joints carrying calculated loads shall be established on the basis of tests in accordance with Section 8. 5.3 Self Tapping Screw Connections The following notation applies to this section: F~cI ~ coefficient which depends on screw location nominal screw diameter nominal liole diameter nominal washer diameter larger of the nominal washer diameter and the screw head bearing ultimate strength of member in contact with the screw head bearing ultimate stxength of member not in contact with the screw head bea~-ing yiald strength of member in ctntam with the screw head bearing yield strength of member not in contact with the screw head tensile ultimate strength of member in contact with the screw head tensile ultimate slxength of member not in contact with the screw head factor of safety = 3.0 allowable shear force per screw nominal shear strength per screw allowable tensile force per screw nominal tensile strength per screw pull-out force per screw pull-over force per screw thickness of member in contact with the screw head t~ = 'th~cimess of member not in contact with the screw head Ail the requirements of this section shall apply to self-tapping screws with diameter D = 0.08 in. (2 mm) through 0.25 in. (6.4 mm). The screws shall be thread- forming or thread-cutting, with or without a self-drilling point. Alternatively, design values for a pmiealar appli- cation shall be permitted to be based on tests according to Section 8. Screws shall be instulled and tightened in accordance with the manufacturer's recommendations. The tensile stress on the net section of each member joined by a screw connection shall not exceed the allowable stress from Sections 3.4.1 through 3.4.4. The net section shall be determined according to Section 5.1.6. 5.3.1 Shear The shear force shall not exceed the allowable bearing force for a screw according to Section 3.4.5 nor the allow- ables according to subsections of this section. ~.3.1.1 Connection Shear The shear force per screw shall not exceed P, calculated as follows: p., = P,,/n, (Et~.5.5.l.l-1) where P,, shall be thc lesser of ', (£q ~,e. LI-2) P,, = --DF~yItl . . Y n, DF~,~ q (Eq. 5.3.1.1-4) P" = 1.2n,, ", DF~,:ta (Eq. 5.3.1.1-5) P"' = 1.2n. For t:/t~ ~ 1.0 , P~ shall not also exceed p,, = 4.2(t~D)m ~q. 5.$.1.1~) 5.3.1~. Shear in Screws The ultimate shear capacity of the screw shall be deter- mined by multiplying the allowable shear capacity deter- mined according to Section 5.1.1 by the factor of safety used or by test aneording to Section 8. The ultimate shear capacity of the screw shall not be less than 1.25 P~. l-A-60 October 1994 5.3.2 Tension For screws which carr~ tensile loads, the head of the screw or washer, if a washer is provided, shall have a diameter D. not less than 5/16 inch (8 mm). Washers shall be at least 0.050 ia. (1.3 mm) thick. The tension force shall not exceed P., calcniatM as follows: p,, = P,,/n, (Eq. 5.3.2-1) p., shall be taken as the lesser of P,~ and P,~ determined below in Sections 5.3.2.1 and 5.3.2.2. 53.2.1 hill-Out The pull-out force, P,.,, for pulling out the threaded shank of the screw through the connected plate, shall not P..t = 0'85trO F,.z (E.q. .5.3.2.1-1) where t, is the lesser of thc depth of thc pcnelxation of screw threads ia the rocmber or sheet not in contact with.thc screw head not including the self-drilling point, sad thc thickness 5.3.2.2 Pull-Over Thc pull-over force, P,~, for pulling out thc head of the screw through thc connected plate, shall not exceed: p,~ = Ct, F,~(D,,-D~) (Eq. 5.3.2.2-1) where C is a coefficient that depends on screw location (1.0 for valley fastening and 0.7 for crown fastening), D,,, is thc . larger of the screw head diameter or thc washer diameter, and shall be taken not larger than 1/2 iaeh (13 mm). 5.3.2.3 Tension in Screws The ultimate tensile capacity of the screw shall be determined by multplyiag thc allowable tcnsilc.cap, acity determined according to Section 5.1.1 by the factor of safety used or by tests according to Section 8. The ultimate tensile capacity of the scow shall not be less than 1.25 P.,. 5.4 Laps in Building Sheathing 5.4.1 Endlaps Minimum cndlaps shall be those expressed ia Table 5.4.1 5.4.2 Sidelaps For a sinusoidal corrugated sheet, the minimum sidelap for roofing shall have a width equal to the pitch of the cor- rugations, and the minimum sid¢lap for siding shall have a width equal to half the pimh. For a trapezoidal sheet of a depth greater than 1 ia. (25 mm) thc minimum sidelap for both roofing and siding shall have a developed width eq~ to the width of the narmwest fiat plus 2 in. (50 mm) A trapezoidal sheet with a depdi of 1 in. (25 mm) or less shall have aa overlap of proven design including an antisiphoniag feature. 5.4.3 Fastener~ in Laps Minimum size of#12 screws or 3/16 in. (5..mm) diameter rivets shall be used ia end laps and side laps. Maximum spaning for required sidelap fasteners shall be i2 in. (300 ram). Endlep fasteners added for the ~ of. improving closure shall be located not more than 2 in. (50 mm) from the end of thc ovcrlappiag sheet. 5.5 Flashings and Closures Flashings'shall be formed from aluminu~ alloy sheet of -lpproximately the Same thickness .as thc mating Or siding :heat. Ur~ss engineering computations determine other- wise, use minimum # 12 screws or 3/16 ia. (5 mm) diamcmr rivets to secure flashings to the roofing or siding. Table 5.4.1 MINIMUM END LAPS Minimum End ~ ~na . Depth of section Roofing, slope greater Roofing slope 3 on 12 or Siding than 2 on 12, less than 3 more on 12 1 in, or less 6 in. 4 in. (25 mm or less) (150 mm) (100 mm) Greater than 1 in., less than 2 In. 9 in, 6 in. 4 in. (greater than 25 mm, (230 mm) (150 mm) (100 mm) less than 50 mm) 2 in. or more 9 in. 6 in. 6 in (50 mm ar more) (230 mm) (150 mm) (150 mm) I-A-61 October 1994 Section 6. Fabrication 6.1 Laying Out a. Hole centers shall be center punched and cutoff lines shall be punched or scribed. Center punching and scrib- ing shall not be used where such marks would remain on fabricated material. b. A temperature correction shall be applied where necessary in the layout of critical dimensions. The coefficient of expansion shall be taken as 0.000013 per degree Fahrenheit (0.000023 per degree Centigrade). 6.2 Cutting a. Material shall be permitted to be sheared, sawed, cut with a muter, or arc cut All edges which have been cut by the arc process shall be planed to remove edge cracks. b. Cut edges shall be mae and smooth, and f~e from excessive burrs or ragged breaks. c. Re-entrant cuis shall be avoided wherever possible. If used, they shall be filleted by drilling prior to cutting. d. Oxygen cutting shall not be used on aluminum alloys. 6.3 Heating Smactural material shall not be heated, with the foIlow- lng- exceptions: ~t. Material shall be permitted to be heated to a temperature not exceeding 400°F (200 DC) for a period not exceeding 30 minutes. Such heating shall be done only when proper temporamre controls and supervision are provided to insure that the limitations on temperature and time are carefully observed. If structural material is subjected to elevatr. A temperatures or times in excess of the foregoing, the allowable stresses shall be reduced consistent with mechanical properties specified for the material after the heating process. For 5XXX series alloys with magnesium contents greater than 3 percent, holding within the temperature range from 150 (66 °C) to 450 ~F (230 °C) must be avoided in order to minimize the possibility of sensiri:,atlon to exfoLiation and stress corrosion cra~king~ The length of time at temperature is a c~fical fa~tur in determining the degree of sensitization. Hot forming techniques must include quick heat up to a temperature not to exceed 550DF (290 °C) to minimize loss of mechanical properties. Forming must be completed before the metal cools below 4$0DF (230 °C). The metal shall then be fan cooled, to drop thc metal temperature from 450°F (230 °C) to 150 °F (66 °C) in the r,i,~mum time possible to prevent sensitization. Some elevated temperature processes, such as factory paint curing or fu'ing of porcelain enamel eoarings, can reduce the mechanical properties of the metal. Since the amount of the reduction will vary with the alloy and temper used, as well as with the elevated temperature exposure, the supplier shall be consulted for mechanical property specifications for the processed material. 6.4 Punching, Drilling, and Reaming The following niles for punching, drilli~S, and reaming shall be observed: ~. Rivet or bolt holes shall be permitted to be either punched or drilled. Punching shall not be used if the metal thickness is greater than the diameter of thc hole. The amount by which thc diameter of a sub- punched hole is less than that of the finished hole shall be at least 1/4 the thiclmnss oftbe piece and in no case less than 1/32 in. (0.8 mm). b. The finished diameter of holes for cold-drlvea rivets shall be not more than 4% greater than the nominal diameter of the rivet c. The finished diameter of holes for hot-ciriven rivets.shall be not more than 7 per cent greater than the nominal diameter of the rivet d. The finished diameter of holes for bolts shall be aot more than 1/16 in. (1.6-mm) larger than the nominal holt diameter. e. 'If any holes must be eniarged.to admit the rivets or bolts, they shall be reamed. Poor matching of holes shall be cause for rejection. Holes shall not be drifted in such a mlmner as to 'distort the metal. All chips lodged between contacting surfaces shall be removed before assembly. 6.5 Riveting 6.5.1 Driven Head The driven head of aluminum alloy rivets shall be of the fiat or the cone-point type, with dimensions as follows: ia. Fiat heads shall have a diameter not less than 1.4 times the nominal rivet diameter and a height not less than 0.4 times the nominal tivet diameter. b. Cone-point he~,t~ shall have a diameter not less than 1.4 times the nominal rivet diameter and a height to the apex of the cone not less than 0.65 times the nominal rivet diameter. The included angle at the apex of the cone shall be approximately 127t [-A-62 October 1994 6.5.2 Hole Filling Rivets shall fill the holes completely. Rivet heads shall be concentric with the rivet holes and shall be in proper contact with the surface of the metal. 6.5.3 Defective Rivets Defective rivets shall be removed by drilling. 6.6 Painting Structures of the alloys covered by these specifications are not ordinarily painted (with the exception of 2014-T6 when exposed to corrosive environments). Surfaces shall be pained where: ~. The aluminum alloy parts are in.contact with, or are fastened to, steel members or other dissimilar malerials. b. The sUmctures are to be exposed to extremely corrosive conditions, or for reason of appearance. Painting procedure is covered in the following Sections 6.6.1 and 6.6.2, and methods of cleaning and preparadon are found in Section 6.7. ('Treatment and painting of the structure in accordance with United States Military Specification MIL-T-704 is also acceptable.) 6.6.1 Contact with Dissimilar Materials Where the aluminum alloy partz are in contact with, or are fastened to, stol m~rnb~s or other dissimilar materials, thc aluminum shall be kept from d'trent contact with the steel or other dissimilar material by painting as follows: a Steel surfaces to hc placed in contact with aluminum shall be painted with good quality non lead containing prim/ag palnt~ such as zinc molybdalc, alkyd type primer in accordance w~th Federal Spccificarion Tl'-P-645B, followed by two coats of paint consisting of 2 lb. 0f aluminum paste pigment (ASTM Specification D962-81, Type 2, Class B) per gallon of varnish meeting Federal Specification TT-V-81, Type H, or the equivalent. Where severe corrosion conditions are expected, add/tiona] protection can he obtained by applying a suitable sealant to thc laying surfaces, capable of excluding moisture from the joint during prolonged service in addition to thc zinc molybdate, alkyd type primer. Aluminized, hot-dip galyanizad or electro-galva~.zed steel placed in contact with alumi- num need not bc psintad. Stainless steel (300 series) placed in contact with aluminum need not be palnred cxcopt in high chloride contain/n§ environments. b. Aluminum shall not be placad in direct contact with wood, fiberboard or other porous material that absorbs wa~r and causes corrosion. When such contacts cannot bc avoided, au insulal/ng harrier betwenn thc aluminum and the porous material shall be installed. Aluminum surfaces shall be given a heavy coat of alkal/resistant b~turninons paint or other coating providing equivalent protection before installation. Ainmiunm in contact w~di concrete or masonry shall be sim/larly protected in eases where moisture is present and corrodcots will be entrapped between the surfaces. c. Aluminum surfaces to be embedded in concrete ordinarily need not be painted, unless corrosive components are added to the concrete or unless the assembly is subjected for extended periods to extremely. corrosive conditions. In such cases, aluminum surfaces shall be given one coal of suitable quality paint, such as zinc molybdate primer conforming to Federal Spocl- fication 'IT-P-645B or equivalent, or a heav~ coating of flkali resistant bituminous paint, or shall be wrapped with a suitable plastic tape appli~ in such a manner as to provide adequ~e protection al the overlaps. Alumi- num shall not be embedded in concrete to which cor- rosive components ~uch as chlorides have been added ff the aluminum will be electrically connected to steel. d. Water that comes in contact with aluminum after tint running over a heavy metal such as copper may conUfin trace quantifies of the dissimilar metal or its corrosion produ~ which will cause corrosion of the aluminum. Protection shall be obtained by .painting or plastic coating the dissimilar metal or b~ designing the structure so that the drainage from the.dissimilar metal is divenad away from the -~uminum. ~ e. Prapalnt~l aluminum genenflly does not need additional painting even in contact with other materials such as · wood, concrete or steel. Under extsemaly corrosive conditions, additional protection shall be provided as described.in the preceding paragraphs, 6.6.2 Over-All Painting Strucwa~s of the alloys covered by these specifications are either not orc~adly painted for surface protection (with the exception of '2014-T6 when exposed to corrosive environments) or are made of 10~¢palnted aluminum compo- naars. There may be applications where the structures are to be exposed to exn'emely corrosive conditions. In these cases over-all painting shall be specified. 6.7 Cleaning and Treatment of Metal Surfaces Prior to field painting of structures, all surfaces to be painted shall be cleaned immediately before painting, by a method th.twill remove all dirt, oil grease, chips, and other foreign substances. Exposed metal surfaces ~hall be cleaned with a suitable chemical cleaner such a~ a solution of phosphoric acid and organic solvents meeting United Stat~s Military Specifica- tion MIL-M-10578. Abrasion-blasting shall not be used on aluminum less dian Or equal to 1/8 in. (3 mm) thiclc October 1994 I-A-63 Table Z-zu Spec. Allowable Stress Type of Slress Type ot Member or Component 3,4, Allowable Stresses for BUILDING , and Similar Type Structures TENSION, axial, Any tension member I t9 ~ : 6005--T5 Extrusions net seclion ~,,, , i?, Thicknesses Up Through 1.00 In. Rec!angular tubes, structural 2 t9 TENSION IN shapes bent around strong axis ~ []-'~ ~ ~, 61 05--T5 Extrusions ~ Thicknesses Up Through 0.50 In. BEAMS, Round or oval tubes 4~) 0 (::~ - 3 extreme fiber, ~ [ WHITE BARS ] apply to nonwelded members and to welded ne~ section Shapes bent about weak axis, I- ~ · 4 28r t3J members et locations farther than 1.0 In. from a weld. bars, plates : ~ SHADED BARS ~ apply ~lhln LO In. of a weld. On Hvels and bolts 5 34 ~ !~ ~ Equations that strad~e the ~haded and unshaded a~as apply to both. ? ~ *For tubes with circumferential welds, equations of SecUons 3.4.10, BEARING On ~a, sudaces and pins and on bolts In slotted holes ~ 23 { 3.4.12, and 3.4.16.1 apply for ~ 20. [ Allowable Stress Slenderness Allowable Stress 3.4, Allowable Slenderness Slenderness Limit Type of Stress Type of Member or Component Spec. Stress Limit S~ Baleen ~1 and SI CO M P RESSION I ] 9 k~r = 9.5 ~0.~ - 0. ] 26 (k~r) ~r = 66 ~ [ ,~1(~Ur)a Flat plates suppoded along one 19 b/~ = 5.2 23.1 - 0.79 (blt) b/~ = l0 I54/(bh) edge - columns buckling about a . _ _~. 8 .~' ~" ':~'~" Fiat plates supposed along one 19 blt = 3.2 23. I - 0.79 (~t) b/~ = 12 197~(b~)~ edge- columns not buckling about -~. ] b ~ 19 blt = 16 23. I - 0.25 (b~) b/t = 33 4~(b/t) COMPRESSION Flat plates wllh both OF COLUMNS Flat plates with one edge iross suppoded and other edge with g.1 See Section 3.4.g.1 Flat plales wllh both ~ ~ I edges suppoded and with 9.2 See Section 3.4.9.2 on both edges, walls of 10' · i :;i1~;~' ~;'; :'~ff3~0 ,: . (R/t)(l Type of Stress Allowable Stress Slenderness Allowable Stress Ulowable Slenderness Slenderness LImtt Sz Slenderness Spec. Stress Limit S~ Between $, end $, 103 , ~ - ' - 25 ~dt = 2~ ~9.3 - z.7o~ ~/t = ~ Same as Round or OVal tubes 1 2' ...... -: ' 18.6 - . ' RQ" 1~4 t2 ~t~[,l~ = t3 405 - O,93aa~ g~'~ = Z9 ii .400 __ ~olld reclangular and ~ · 13 =z~ ' 21 ,S / S~2 = 146 23.9 0.24~'~ I,S,/ Sff7 = 17~) 24,000 Rec angular tube. and I 4 .................... ;- -- ~,/ *~ = box sections ' iO,5 -- ~ ~, ,' 10.5 , Flat plales supposed on ~ ~ ~ 1 S ..... ' -- ~ bh = 33 5801(bh) edges supported 133 ' 25 Rjr = 1.6 26.2 - 0.94 ~ Rjr = 141 3 gO0 Cu~ed plates supposed 16.1. , , Rdl=l,~ - ~, t2.4- 0-33~ R/t= 340 on both edges 12 . suppoMed end lhe oiher 1 ~.~ Flat plates wgh both I ~~ See Section 3.4.16.3 edges suppoded and wtlh 1 6.3 -- bh = 8.9 405- 1.41 blt blt = 19 4,9001(b/t)~ )N compression edge free. ~ 17 ...... ...... ' ' ' hit- , , ~ ~ · 13.5 ' ~ ' , ...... - '. ' tension edge supported = hit = 75 Flat plale with both edges 18 , - ~ ..... :' 'j ~ ' t supported 13.J ' ' PRESSION BEAMS, rome fiber IPRESSION V~PONENTS 3F BEAMS, component compression), COMPRESSION COMPONENTS Table 2-22 Spec. Allowable Stress Type of Stress Type of Member or Component 3.4. Allowable Stresses for BUILDING and Similar Type Structures TENSION, axial, Any tension member I ,.5 6.5 aet ~.ogon ,; , 6063-T5 Rectangular lubes, slructural 2 ~.5 i~6,~ Extrusions shapes bent around slrong axis -]' [~'1' ~ ~ ~ (Thickness up thru 0.500 in.) TENSION IN BEAMS, Round or oval lubes O0Q 3 ~15 S.S exlreme fiber, net section Shapes bent about weak axis, I ~ · 4 125 8,5 i WHITE BARS ] apply to nonwelded members and to welded -- members at locations fadher than 1 .O in. from a weld. bars, plates = I SHADED BARe, I apply within 1.0 In. of a weld. On rivets and bolts 5 16 [ 13-~ Equations that straddle the shaded and unshaded areas apply to both. [ 'For tubes with circumferential welds, equations SEARING On fiat sudaces and pins and on bolts In slotted holes 6 t0$ ,, , , 3.4.12, and 3.4,16,1 apply for R// ~ 20. I Spec. Allowable Slendernes~ Allowable Stress Slenderness Allowable Stress Flat plales suppoded along one 8,5 hA = 68 tO - 0.22 (glo blt -- t6 IOll(b/O edge - columns buckling about a _ -~- 8 :, : F~at plates supported along one 8.5 h/t = 6.8 IO- 0.22 (~/t) b/t a symmetry axis b/t-- 16 ~ ~J~ 8.5 blt = 21 10.0 0.071 (hit) h/! = 50 329/(b/t) COMPRESSION Flatplateswlthboth ~ ~ 9 ~ ' 6~ ; 3201(~/t) ~ : COMPONENTS OF COLUMNS Fiat plates with one edge gross stJppoded and olher edge with 9.1 See Section 3,4.9.1 section sllffener _._J edges suppoded and with 9.2 See Section 3.4.92 an Intermediate stllfener Sh]9[e web be~ms bent ab°ut-- 11 .... :.~'- f~'~ ....... COMPRESSION Round of oval tubes 1 2' =' ~' - ' ' -:: t2.s-o.fil~ ~d,2~ ~xtreme fiber , ~ 125 ~'~ = 18 17.2 - 0.26~tt~iJ ~u~,~ = 45 I 1,400  ' blt= t8 one edge ~ 6J - OF SEAMS, Cu~ed plates suppu~ed 16.1' ............. . ' '~,~-0,~ ~;,~ ~to compression). 1 6.2 COMPRESSION compression edge free. ~ 17 : *lt~ )wa plane) stiffener, both edges Z~o, 19 .... , r ~ ~' ' ? ' ' ' - _ , a,h~ll7 ~3,~l(a,lO~ O Type of Stress TENSION, axtai, net section TENSION IN BEAMS, extreme tiber, net section Type of Member or Component Any tension member Rectangular tubes, structural shapes bent around strong axis o0o ~hapes bent about weak axis, bars, plates On rivets and bolts BEARING On rial sudaces and pins and on boils in stetted holes Type of Stress Type of Member or Component COMPRESSION IN COLUMNS, dl columns axial, gross mclion Spec. 3.4. COMPRESSION COMPONENTS OF COLUMNS Flal plales supported along one edge - columns buckl,ng about a -Z- ~-~-~ axis supported along one a symmel~ axis Ib~ Flat p,ates with bolh edges suppoded ~ b ~ Flat plates with one edge ~1 supported and olher edge with stiffener Flat plates wllh both edges suppoded and with n inlermedlate sliffener Curved plates supported on both edges, walls of round of oval tubes Allowable Stress ~s Table 2-23 Allowable Stresses for BUILDIHG and Similar Type Structures 6063-T6 Extrusions, Pipe 20 24 ; 13.5 I [ WHITE BARS I apply to nonwelded members and to welded members at Iocalions fadhor lhan 1.0 In. from a weld· ~ SHADED BARS I apply within 1.0 In. of a weld. Equations that straddle the shaded and unshaded areas apply to both. 'For tubes with circumferential welds, equations of Sections 3.4.10. 3.4.12, and 3.4.16.1 apply for /:~ ~ 20. AUowabie Stress I Slenderness Stenderness I Limit Sz Allowable Stress Slenderness ~ S~ 13.5 kilt =9.5 135 6.5 blt = 5.7 16.1 - 0.46 (b/~) 135 b/t = 5.7 51,000/(klJr)~ blt = 12 1291(blt) ~vf=2.0 ~ 12gl(b/t). 'ii 16. I - d 144 (blt) b/I = 39 410/(blt) : 4 lOt(b/t) See Section 3.4.g.1 See Section 3.4.9.2 15.6 - 0.50~t I R/t = 188 3200 13.5 6.5 o AIIownble Stress Type of Stress Type of Member or Component Spec. Allowable Stress Slenderness Slenderness Slenderness Allowable Stress Single web beams bent about _ 11 18 R~t = 33 27.7- 1.70~ R~t=102 Same as 12' ~NeEAMS, nound or oval tubes 8 :' ad"6= ~: " t3.S~0.61~ R~=2~ SecUon3.4.10 fiber ~t~ = 15 27.9 - B.J3a/t ~ d/t~ = 35 I 1,400 section ,ound section beams -- 8j - aj: ~/,~ a 32 (dlO'(L,Id) :component on both edges 8 R/~ = 0.3 : 7.9'0.]9~ . ~ ".. compression). Fiat plates with one edge gross section supporled and lhe other~ 1 6.2 See Section 34.16.2 COMPRESS,ON compresslon edge free. (component ~upporled 8.5 , ; , SHEAR [Iai webs~ / /~_ TABLE 6. NOMINAL SHEAR AND TENSILE STRESSES FOR STAINLESS STEEL STEEL BOLTS NAMEI TYPE DIAMETER AREA DIA. HEAD F.v F,t P, PI in inz in. ksi ksi lbs lbs # 6 S.S. 0.138 0.015 0.262 33.7 56.0 295 565 # 8 S.S. 0.164 0.021 0.312 33.7 56.0 416 798 # 10 SS. 0.190 0.028 0.361 33.7 56.0 559 1071 # 14 S.S. 0.242 0.046 Q480 33.7 56.0 906 1738 1/4" S.S. 0.250 0.049 0.480 33.7 56.0 967 1855 # 17 S.S. 0.285 0.064 0.500 33.7 56.0 1257 2410 3/8" S.S. 0.375 0.110 0.625 33.7 56.0 2176 4173 1/2" S.S. 0.500 0.196 0.750 33.7 560 3869 7418 3/4" S.S. 0.750 0.442 1.000 33.7 560 8705 16691 REFERENCE: ASCE STANDARD: Specification for the design of Cold-Formed Stainless Steel Structural Members ASCE-8-90 page 29 U U ~_ 2.4400 1.1588 ................ REGIDNS ................ Area: 1.0796 sq ~m Perimeter: ~2.4878 in Bounding box: X: -0.855~ -- 0,8549 in £emtroid: X: 0.0000 in Y: 0,0000 in Moments oF inertia: X: 0.7826 sq in sq in Y: 0,3790 sq in sq ~n Product oF inertia: XY: 0.0000 sq in sq in Rod~i oF gyration: X: 0,8514 in Y: 0.5925 in Principal moments (sq in sq in) and X-Y directions about centroid: I: 0,3790 along [O.OOOO 1,0000] J: 0.7826 along [-10000 0.0000] Section ModuluS: Sx Top: 0.611 Sx Bat: 0675 in3 Sy LeFt: 0443 Sy Right: 0442 in3 ALLOY ~o. REViSiON BY~ FOUR SEASONS SOLAR PRODUCTS CORP. TEUPER 6005--T5 O~ 5005 VETERANS MEMORI^L ~mHWA¥ TYPmAL 0.090 WALL 2 DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS FINISH 3 TITLE SECTION PROPERTIES ~,~ NO. ~4~ ~ SYSTEM 4 REGULAR BAR ~ NO. 4GBA 5 DO NOT SCALE DRAWINGS SCALE1''=~'' DRAWN BY RPLDWO. ~,PPROVED ~ DATE 1~-13-97 4GBA 6 TOLERANCES + ~- -~ 2.579° \ 5.017' 2.438' / 0.840' -- ' 0.870' / / / / ................ REf_i]~N~. .- .......... ~--- Areo~ 2.2872 sq in Perimeter: 38~8855 in Bounding box: X: -0.8595 -- 086D0 in Y; -2.3790 -- 2;6377 in Centroid~ X~ 00000 ~n Y: 0.0000 in I: 0.9603 ~Lon9 [0.0031 1.0000) ALLOY NO. REVISION 8Y FOUR SF, ASONS SOLAR PRODUC?S CORP. TEMPER 6005-TS,6005-T5  __~ 5005 VETERANS MEMORIAL HIGHWAY TYPICAL 0.090, 0.100 Iu~ HOLBROOK, NEW YORK 11741 WALL FINISH 2 c~ ,~,~N~.~ ~N.~ M^NU~^CT,~RES O~ ~OU. SEASO,~S SUN.OOMS .~ TITLE SECTION PROPERTIES o,E No. 5416. 7249A 4 SYSTEM 4 REGULAR BAR WITH RAFTER STIFFENER PART NO.4GBA' 4RSB 5 DO NOT SCALE DRAWINGSscAL£1''=I'' DRAWN BY RPL DWG. APPROVED~ DATE ~-~-97 4GBA-4RSB 6 TOLERANCES + ~- -~" ................ REGIONS ................ Area: 1.6594 sq in Perimeter: 21.5252 in Bounding box: X: -0.8551 -- 0.8549 in Y:-1.1189 -- 1.,3211 in Centroid: X: 0.0000 in 'Y: 0.0000 in Moments of inertia: X: 1.0514 sq in sq in Y: 0.5045 .sq in sq in' Product of inertia: XY: 0.0000 sq in sq in Radii of gyration: X: 0.7960 in Y:' 0.5514 in Principal momen.ts (sq in sq in) and X-Y directions about centroid: · I: 0.5045 along [0.0000 1.0000] J: 1.0514 along [-1.0000 0.0000] Secfion Nlodulus: Sx Top: 0.7959 in^5 Sx Bat: 0.9,396 inA Sy Left: 0.59 in^3 Sy Right: 0.59 REVISION FOUR SEASONS SOLAR PRODUCTS CORP. 5005 VETERANS MEMORIAL HIGHWAY HOLBROOK, NEW YORK 11741 DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS TITLE SECTION PROPERTIES SYSTEM 4 HEAVY BAR ~ NOT SCALE DR~ ~PPROVED ~ DATE 11-1,,]-97 ALLOY TEUPER 6OO5--T5 TYPICAL 0.140 WALL FINISH D-~-NO. 5417 PART NO. 4HBA 4HBA ................ REGIONS ................ Areo: 2.867 sq in Per~meter: 36.723 ~n Bounding box: X: -0.857 -- 0.859 in Y: -2.628 -- 2.386 ~n Centro{d: X: 0.000 in Y: O.0O0 in Moments of inertia: X: 6.4t5 sq in sq in Y: 1.086 sq in sq in Product of inertia: XY: -0.010 sq in sq in Rodl; of gyration: X: 1.496 in Y: 0.615 in Principal moments (sq in sq in) and X-Y direc[ions about centroid: i: 1.086 along [0.002 -1.000] J: 6.41.~ along [1.000 0.002] ALLOY qo.J REVISION BY FOUR SEASONS SOLAR PRODUCTS CORP. TEMPER 6005-TS.6005-T5  5005 VETERANS MEMORIAL HIGHWAY TYPICAL O.140.0.1OO 1 HOLBROOK, NEW YORK 11741 WALL 2 DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS FINISH 5 TITLE SECTION PROPERTIES D,E NO. 3417.7249A 4 SYSTEM 4 HEAVY BAR WITH RAFTER STIFFENER PART NO. 4HBA' 4RSB 5 DO NOT SCALE DRAWINGS $CALE i":i"JDRAWN BY RPL DWG. APPROVED ~ DATE 11-13-97 4HBA-4RSB 6 TOLERANCES + ,'-' - 1.205' I ---- ""~"- 2.440' 1235' //- 0.855' 0.855' 7 / 1.710' / '1 ................ REGIBN§ ................ Area: 0.834 sq in Perimeter: 19.904 in Boundin9 box: X: -0,855 -- 0.855 in Y: -1235 -- 1.205 in Centroid: X: 0.000 in Y: 0.000 in Momen~cs of inertia: X: 0.622 5q in sq in Y: 0.331 sq in. sq in Product oF inertia: XY: 0.000 sq in sq .in Radii o¢ gyration: X: 0.863 in Y: 0.630 in Principal Moments (sq in sq in) and X-Y directions about centroid: 1:0.331 along [0.000 J: 0.622 along [-1.000 0.000] ALLOY TEMPER 6005--T5 NO. REVISION BY ~'OUR SEASONS SOLAR PRODUCTS CORP. E~ 5005 VETERANS MEMORIAL HIGHWAY TYPICAL 0.080 1 HOLBROOK, NEW YORK 11741 WALL 2 ~;~ DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS FINISH 3 TITLE SECTION PROPERTIES o,~- NO. 4 SYSTEM 4 GABLE MULLION BAR PAR'r NO. 5 DO NOT SCALE DRAWINGS SCALE 1 ":1" )RAWN BY RPL DWG. APPROVED ~ DATE 11-13-97 4OMA 6 TOLERANCES + '--' -"~ 2.?6° 5.00' 2.2~° ................ REGIONS ................ ALLOY qO. R[VISION BY~ FOUR SEASONS SOLAR PRODUCTS CORP. TEMPER6005-TS, 6005-T5 Ol~ 5005 VETERANS MEMORIAL HIGHWAY TYPICAL 0.080 HOLBROOK, NEW YORK 1174! WALL 3 TITLE SECTION PROPERTIES DIE NO. 5968 4 SYS 4 GABLE MULLION WITH STIFFENER PART "0-4GMA, 4RSB 5 DO NOT SCALE DRAWlNGSiSCALE3/4''--1'' DRAWN BY RPL DWG. 4OMA-4RSB DATE 6 TOLERANCES + ~ -~ 1,366' 1 8.533' 1.166' ,~--0.855' ~ 0.855'~ 1,710' ................ R[GION$ ................ Area: 1.2075 sq in Perimeter:. 15.3977 in Bou. ndincj box: X: -0.8550 -- D.8550 tn Y: -1.1661 -- 1.3984 in Centroid: X: 0.0000 in Y:' 0.0000 in Moments of inerlio: X: 0.8971 sq in sq in Y: 0.5813 sq in Sq in Product of inertia: XY: 0.0000 sq in sq in Radii of gyration: ×: 0.8619 in Y: 0.6938 in Princlpol moments (sq in sq in) and X-Y directions cenlroid: I; 0.,5813 alan9 [0.0000 -LO000] J: 0.8971 alan§ [1.0000 0.0000] 1,366' I L.166' ~--0.855' ~ 0.855'-~ 1.710' ALLOY NO. REVISION BY FOUR SEASONS SOLAR PRODUCTS CORP. TEMPER 6005--T5  6005 VETERANS MEMORIAL HIGHWAY TYPICAL 0.100 1 HOLRROOK, NEW YORK 11741 WALL 2 DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS FINISH ~ 3 TITLE SECTION PROPERTIES D,E NO. 724gA 4 RAFTER STIFFENER PART NO. 4RSB 5 DO NOT SCALE DRAWINGS SCALE 1"----1" DRAWN BY RPL DWG. ~,PPROVED ~ DATE 11-21-97 4RSB 6 TOLERANCES + ~ -~ 1.862' .538' ? 2.004' x ................ REGIONS ................. Areo: 0.886 sq in Perimeter: 2,5..00,5 in Bounding box: ×: -2.004 -- 2.145 in Centroid: X: 0.000 in Y: 0.000 in Moments of inedio: ×: 0.229 sq in sq in Y: 1.747 sq in sq in Product of inertia: XY: 0.27~ sq in sq in Radii of gyrafion: X: 0.,509 in Y: 1.404 in Principo[ moments (sq in sq in) and X-Y directions about cenfroid: h 0.182 Dion9 [0.98S 0.170] J: 1.793 olong [-0.170 0.98.5] ALLOY NO. REVISION BY ~ ~'OUR S~]~LSOINTS SOLA.[~ !P~O~)UCTS COl~iE), TEMPER 606,3--T5 1 0 ~' 5005 VETERANS MEMORIAL HIGHWAY TYPICAL HOLHROOK, NEW YORK 11741 WALL 0.0'70 2 DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS FINISH 3 TITLE SECTION PROPERTIES D,E No. 4. SYSTEM 4 SILL PART NO. 4GSL 5 DO NOT SCALE DRAWINGS SCALE 1"=1" DRAWN BY RPL OWO. 6 TOLERANCES + '"-' --,,~ APPROVED ~ lO-lO-O'l 4GSL 5,592" ~ ................ R~c~o.s ................ Area: 0.914 sq in Perimeter: 24.198 in Bounding box: X: -1.404 -- 0.505 in Y: -5.002 -- 2.592 in Centroid: X: 0.000 in Moments of inerlio: X: 2.185 sq in sq in Y: 0.241 ' 3.001" Product of inerfio: XY: -0.117 Radii of gyration: X: 1.546 in Y: 0.814 in Principal m~ments. (sq in sq in) and X-Y directions about cenfroid: i: 0.254 along [0.060 -0.998] 'J: 2,191 along [0.998 0.060] -~ -- ,47" ALLOY NO. REWS~ON BY ~1 FOUR SEASONS SOLAR PRODUCTS CORP. TEUPER 6065--T5 , 5005 VETERANS MEMORIAL HIGHWAY TYPICAL ~i~ HOLHROOK, NEW YORK 11741 WALL 0.070 2 DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS FINISH .., 3 TITLE SECTION PROPERTIES 4 SYSTEM 4 RIDGE PART NO. 4OR 5 DO NOT SCALE DRAWINGS SCALE 1":1" DRAWN BY RPL DWG. 6 TOLERANCES -F ~-- --,~ APPROVED ~ DATE ~0-10-0~ 4GR ,1,907 2,625 ,718 ¥ ,? ,4o2 , -- ],483 ..... ........... REGIONS ............. ---- Area: 0.341 sq in Perimeter: 8.099 in Bounding box: X: -'1.081 '-- 0.402 in Y: -0.718 -- 1.907 in Cen'froid: X: 0.000 in Y: 0.000 in -Momenfs of inert[a: X: 0.20.3 sq in s.q in Y:' 0.073 sq in sq in Produc~' of inertia: XY: 0.070 sq in sq in Radii of gyration:' X: 0.77'2 in Y: 0.462 in Principal momenfs (sq in sq in) and X-Y direcflons abouf cen'Jroid: h 0.042 along [0.401 0.916] J: 0.234 along [-0.916 0.401] ALLOY NO. REVISION BY FOUR SEASONS SOLAR PRODUCTS CORP. TEMPER 6063--T5 ~.~_O~ 5005 VETERANS MEMORIAL HIGHWAY TYPICAL ~ HOLBROOK, NEW YORK 11741 WALL 0.125 2 DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS FINISN ~ 5 TITLE SECTION PROPERTIES DIE NO. 9854-B '~ RIDOE LEDOER PA,~T NO. ~LL 5 DO NOT SCALE DRAWINGS SCALE 1 "----'[" ORAWN BY RPL DWG. 6 TOLERANCES -'J- '"-' -- ~,~ ~,PPROVED ~ lo-~o-o~ 4LL / 2.204 / ................ REGIONS ................ Area: 0.321 sq in Perimeter: 8.544 in Bounding box: X: -1.130 -- 1.074 in Y: -0.2g~ -- 0.700 in Centroid: X: 0.000 in Y: 0.000 in Moments of ifiertio: X: 0.039 sq in sq in Y: 0.080 sq in sq in Product-of inedia: XY: 0.002 sq in sq in Radii of gyration: X: 0.~49 in Y: 0.501 in Principal moments (sq in sq in) and X-Y directions about cen~roid: h 0.0~9 along [0.999 0.044] J: 0.081 along [-0.044 0.999] ALLOY ~o. ~EWS,ON eY~ FOUR SEASONS SOLAR PRODUCTS CORP. TEMPER 606~--T5 1 ~ 5005 VETERANS MEMORIAL .IG.WAY TYPICAL 0.062 HOLBROOK, NEW YORK 1~?~ WALL 2~ DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUN~OOMS FINISH TITLE ECTION P OPE TIE5 O,E ,o. 5 DO NOT SCALE D~AWiNGS SCALE i"=~" DRAWN BY RPL DWG. ~PPROVED ~ DATE ~0-~0-0~ 4OMT 6 TOLERANCES + ~ -~ -- ~102 ,~ 2,204 ................ REGIONS ................ .&rea: 0.216 sq in Perimeter: 6.423 in Bounding box: X: -1.102 -- 1.102 in y: -0.$78 -- 0,102 in Cenfroid: X: 0.000 in Y: 0.000 in Moments of inertia: X: 0.003 sq in sq in Y: 0.067 sq in sq in Product of inertia: XY: 0,000 sq in sq in Radii of gyrofion: X: 0.107 in Y: 0,554 in Principal moments (sq in sq in) and X-Y directions about centroid: h 0.00.3 along [1,000 0.000] J: 0.067 along [0,000 1.000] ALLOY TEMPER 6063--T5 NO. REWS~ON BY ['OUR SE^SONS SOLAR PRODUCTS CORP. __. 5005 VETERANS MEMORIAL HIGHWAY TYPICAL 0.050 WALL ] HOLBROOK, NEW YORK 11741 , 2 ~ DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROOMS F{NISH ~ 3 TITLE SECTION PROPERTIES O,E NO. 9860 4 MUNTIN CAP PART "0. 4GMC 5 DO NOT SCALE DRAWINGSscALE1''=1'' DRAWN BY RPL DWG. APPROVED ~ DATE 10-10-01 4OMC 6 TOLERANCES + ~ -~ ,619 x/ 1,119 ~ 1,085 / 2.204 ................ REGIONS ................ Areo: 0.539 sq in Perimeter: ~ 4.967 .in Bounding box: X: -~.~9 -- ~.085 in Y: -0.619 -- 0.582 in Centroid: X: 0.000 in Y: 0.000 in Moments of inerti~: X: 0.~26 sq in sq in Y:-0,148 sq in sq in Product of ~nerti~: XY: -0.00~ sq in sq in Rodii of gyrofion: X: ~.483 in Y: 0,523 in Principol moments (sq in sq in) ond X-Y directions ~bout cenfrold: h 0.126 olong [0.999 -0.05'2] J: 0.148 olong [0.052 0.999] ALLOY ~0.! R~ISION BY~ ~OU~ S~ASONS SOLAB PRODUCTS CORP. TEMPER 6~65-f5, 606~-f5 ~ ~ 5005 VETERANS MEMORIAL HIGHWAY ~PlCAL 0.050 HOLBROOE, NEW YORK 1~74i WALL 3 T~TLE SECTION PROPERTIES DIE NO. 9860, 9853 4 SYSTEM 4 MUNTIN ASSEMBLY 5 DO NOT SCALE DRAWINGSscALE1''=1'' DRAWN BY RPL DWC. ~PPROVED ~ DATE ~0-~0-0~ 4OMC, 4GMT 6 TOLERANCES + ~ -~ {-- ,167' / 1.71' / / ................ REGIONS ................ Area: 0.183 sq in Perimeter: 6.1,37 in Bounding box: X: -0.855 -- 0.855 in Y: -0.193 -- 0.167 in Centroid: X: 0.000 in Y: 0.000 in Moments of inertia: X: 0.002 sq in sq in Y: 0:054 sq in sq in Product of inertia: XY: 0:000 sq in sq in Radii of gyration: X: 0.101 in Y: 0.54,3. in Principal moments (sq in sq in) and X-Y directions about cenfroid: h'0.002 along [1.000 0.000] J: 0.054 alan9 [0.000 1.000] ALLOY NO. REVISION BY~ FOUR SEASONS SOLAR PRODUCTS CORP. TEMPER 6005--T5 1 ~ 5005 VETERANS MEMORIAL HIGHWAY TYPICAL 0,050 HOLBROOK, NEW YORK 11741 WALL } TITLE SECTION PROPERTIES O,E 4 GLAZING CAP PART NO. 40CB 5 DO NOT SCALE DRAWlNGS SCALEI"=I'' )RAWN BY RPL DWG. 6 TOLERANCES + '--- _ ¢., APPROVED ~ DATE ~0-~0-0~ 4GCB 1,285 ,715 ~ .125 .215 ~-,785 -~' ......... - ...... REGIONS ---- ............ Area: 0.359 sq in Perimeter: 6,000 in Bounding box: X: -0.215 -- 0.785 in Y: -0.715 -- 1,285 in Cenfroid: X: O.000 in Y: 0.000 in Moments of inertia: X: 0.150 sq in sq in Y: 0.026 sq in sq in Product of inertia: XY: -0,056 sq in sq in Radii of gyration: X: 0.647 in Y: 0,271 in Principal moments (sq in sq in) and X-Y directions abou~ cenfrold: I: 0.017 along [0.258 -0.966] J: 0.160 along [0,966 0,258] ALLOY ~o. R~V~S~ON BY ~ ~OUR S~ASONS SOLAR PRODUCTS CORP. TEMPER 606~--T5 1 O 5005 VETERANS ~E~ORIAL ~IG~WAY TYPICAL 0.125 ~O~BROOK, NEW YORK 1 ~741 WALL 2 DESIGNERS AND ~ANUFACTUR~S OF FOUR S~kSONS SUNROOMS FINISH ~ TITLE ~ECTION ~0P~TI~ D~E NO. 4 1/~" OUP ~N~ ~AR~ NO. CN~S00 5 DO NOT ~CALE D~AWIN~SSCALEI"=i" D~WN BY RPL DWG. 6 TOLERANCES + ~ --~ APPROVED ~ DATE 01-05-98 CN4600 2.750 '-- 1.150 -- R 2.-750 .125 .062 R TYP 104' ./P/N: H~1006 MATERIAL: ALUMINUM FOUR SEASONS SYSTEM 4 HEAVY GLAZING BAR P/N 4HBA REVISION WAS 1.430 REF -- ~ FOUR SEASONS SOLAR PRODUCTS CORP RC 5005 VETERANS MEMORIAL HIGHWAY ROLBROOK, NEW YORK 11741 '.-----------DESIGNERS AND MANUFACTURES OF FOUR SEASONS SUNROolViS - SYSTEM 4 D~~CE CHANNEL CAST,NO LE DRAWING: = 1:1 DRAWN ElY; RC ___.[TOLERANCES ~ ~ --~ Civ )ATE: .3-7-97 FOUR SEASONS SYSTEM 4 REcuLAR_ -- GLAZING BAR ~ j REF I- P/N 4GBA ~ MPER ~ NO. PART NO. HN1006 DWG NO. 4-~59