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INDEX STRUCTURAL CALCULATIONS WILD GOOSE PROJECT (77052.001) GLYCOL CONTACTOR, PROCESS GAS FILTER _ _ UN ND TAIROUNDATIONS AND STEEL PLATFORM FR�4M�IN_ i , :. �r t a� E �� sFINAL CHK'D DESCM VT V. M PAGES f .,.,aDStf ,ESIGN CALCS.. _ f P2 09 qp D• . � °SIN. �'•.':.: t '�^> ' •1'}:x:1. ' � ':r r'� :��4. . yQy.,�. .yy�qq(( [yt�� .{A�■Y�- �/.y� )�i 1p� `,`sf1 ,��yy�,}w�...•: •: •: .��.yr.... .: •: .��.yy.`w,� �, • .:� - }i.(.' K� .... K ...... I�?F��:•l •:li 9.2 •: •:.: •: .•: ' ��.:; •� :.��IKJV:::::::':::i�.�:::::::: ::::�:;lY/T::: �::. • -: ,1 i= ' W4iIR. 0IF C i GAS STORCF�k�RpAR T : _ - =tSTR'UCTURA�ALCULATIONS # w �t BWK 6 L QRpfESS/py rn 0 n 2 A •strfOflCAIEO��\� INDEXar STR.UC.TURAL CALCULATIONS WILD GOOSE PROJECT (77052.001) PDC FOUNDATION, PILE NO BOOK NO. DESCRIPTION -PAGES DATE FINAL DESIGN CHK'D CALCS -i0A....... . :. .. ....:... .R00f0UX .24,1 c 'WILD GOOSE GAS STORAGE PROJECT STRUCTURAL CALCULATIONS BOOK 6 -4-'77052.001 Raytheon Engineers & Constructors CALCULATION SUMMARY CALCULATION SET NO. /6 OGcv — S PRELIM. I FINAL VOID REVISION & CONTROL SHEET Page I of 2 DISCIPLINE J'o' O Z 4 PROJECT TITLE 1 f= STRUCTURE OR SYSTEM F�UNQ� DESIGN CLASSIFICATION SUBJECT PQ G COMPLETED BY , N�D� DATE S CHECKED BY A, _ DATE 1-7 APPROVED BY DATE SDE OR MGR OF STAFF GROUP ¢ DISTRIBUTION REASON FOR REVISION: ............................................................... ............................................................................................................................................................ TOTAL NUMBER OF SHEETS w THIS ISSUE ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... SHEETS REVISED, ADDED OR DELETED PROBLEM STATEMENT: .................................................................................................................................................................................................................................:..................................................... ...............5 /Gc/......4....��/..lr` .T.../a.a..... T.......,�.1!t`'o'.%-.... MD.. .........................................:......... f'Q.l...�'.......... .......e—;v..r��t.'...................................................................................................................... ....................................................................................................................................................................................................................................................................................... .................................................................................................................................................................................................................................::.................................................... ....................................................................................................................................................................................................................................................................................... ..................................................... .......................................................................................................... :....................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ...................................................................................................................................................................................................................................:................................................... SUMMARY CONCLUSIONS: .................................:........................................................................................................................................................................................................................................1............ ................. .......... .. !,I.��' t'�a .'...... '. T.. . ..........w/ c.. ..........y .... L. ............ ............. ...................T............P.la,.......................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ...........................................................................................:.....................................................:..................................................................................................................................... AICALC-SUM.DOT Raytheon Engineers & Constructors CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2✓/ PROJECT TITLE /L - CALCULATION SET NO. -3 PRELINI. FINAL VOID REVISION. DISCIPLINE ST U 11t'�fL 10. 6Z, 0 DESIGN BASIS: ....................................................................................................................................................................................................................................................................................... ..................... U,/.S/+w? Ca'......R�t C,IJ/l-:-........................................................................:................................................................................................ ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... UNVERIFIED ASSUMPTIONS/OPEN ITEMS: ........................................................................................................................................................................................................................................................................:.............. ....................................................................................................................................................................................................................................................................................... ....................................................... :.......................................................................................... ........................................................................................................................................ ...................................................... :............................................................. .................................................................................................................. :................................................... ..................................................................................................................................................................................................:.................................................................................... ..................................................................................................................................................................................................................:...........................................................:........ ............. ...................................................................................................................................................... ............................................. ............................................................ ............ REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) ................................................................................................................................................:...................................................................................................................................... .............................................................................................................................................................................. .......................:............................................................................................................................................................................................................................. ....................4w...,iT ..........-,i�:l ..:,.a�............ :.................................................................................................................... .......................................................................... .................. !.'s ...... ::.....................................................................................................................................................:.......:...................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) REV. NO. REV. DATE PROGRAM TYPE RE&C VERIFIED ❑ YES 6 NO ANALYSIS DESCRIPTION RUN NO. RESULT The attached computer output has been reviewed, the input data checked, and the results approved for release. INPUT CRITERIA DATE CHECKED BY DATE BY RUN BY DATE APPROVED BY DATE AXALC.SUM.DOT Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. Y Constructors COMPUTATION 4100 --3 Afe Alp SHEET PRELIM. FINAL VOID DA E ST PROJECT W&D ItODSG' SHEET / OF DATE DATE SUBJECTVZ) 7 /O/fs J.O. 7 D oo/ r /1R7, lelNG E5r110-9.9rE.o wC=/4,�rr 771v, . 77X/, / 8sr 71< ..SAY � 3 Q Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. Y Constructors COMPUTATION SHEET PRELIM. FINAL. VOID pA—g �/. f /_ / 9, l PROJECT In/�IGV ZZO0-51! SHEET OF DATE DATE SUBJECT f�UC �(.il/S J -0- .43,>" .O. .43.>" 11-/S/' erio,4-/ G4.</T.Q'oG Vvl/AAS lle;,- OO Z P.PoJ-eel A, -e it O 7XJ6 wr"i4 ,4-"r —4!4e�< //z -7 71< ro rxv e,4 So X /3, 3.3 Uva Godo ra�'�=� GAG, S - �Z, S - 77, B - z7, Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL `Constructors COMPUTATION SHEET CALCULATION SET NO. REV. COMP. BY C�HK' /DY 1214- e5no PRELIM. I FINAI I VOID _D�4TE DpTE�r PROJECT �l%G� LLDOSG SHEET OF DATE DATE SUBJECT �U� /�Ol%�/J�%�DN J.O. O Zi OD /'�R�Y... _ !�'L kT!G �G Loyd CO��L3!/.✓_.�T/oc./ 3312 = 7. Z 9 k /3, 1,7' . 7, Z7/, ULtLLfwL tZ Form 5007 (Rev. 9/95) RaVtheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NOJ REV. COMP, -4� CST' OD - PRELIM. I FINAL I VOID PROJECT_[A//GV GZDG?SG� SHEET OF DATE DATE SUBJECT 1e124::f 14222 tZX91%r/DN J.O. -7 — i V, _ _ - Z,St7f4,z J ZS = 7S,f/��r 47 Yl 7 fi�i�n = 1Z / f � x• �9 7Sks/e" a/� 4 .3 ZS s 2-l(1-fZ,eFr /* = �9, s� Z, s lk"'9X 7�% 3 Is s9, S�,Fr �s = 6-/20(l.fz =1 ¢ o, 1,71 rorm ouut (hev.9/95) Rarytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. REV. COMP. BY CHK'D. BY PRELIM. I FINAL I VOID _ pATq DATE PROJECT �/n✓1440 41-- 420S SHEET OF DATE DATE SUBJECT /- G' �o(//S/��r/O/✓S J O ' _ 7705%, OGS/ z 79ki:r.fT lis MIAI _ . S6 iN Z�f i fps ,--F Form 5007 (Rev. 9/95) Hayrheon Engineers & GENERAL CALCULATION SET NO. REV. COMP BY CH Constructors . COMPUTATION - SHEET PRELIM. FINAL VOID TE PROJECT SHEET OF DATE DATE SUBJECT./y/�� fDU.t/D/�T/Oi✓ J.O. 7o Loo/ MI Fool/�4 i /3GA.t /NG P.C't SvC'% roc S Not3 e -% Dsige=s/4�i/GR;.;. t L3 - r�.. d y..orll4f,@s. /3 f �0.../._._..' NO ' v F/r " ev � vn $-�5@T�l3ca sty I I I7777 — �v1 Al R/�G Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP.BY CHK'D Y Constructors COMPUTATION SHEET PRELIM. FINAL VOID SDAT E //9 S PROJECT �A//L U It Dome SHEET OF 7 DATE DATE _ SUBJECT 1444' /� �l/i✓U�1/D/✓S J.O. 77oS'Z� OD V Af .e l.: <v�-si�,✓ -may � .... . ` _. _ f��:P� PAS✓ /'�AT'��/�+L „ 7 V .e l.: � .... . ` _. _ f��:P� PAS✓ /'�AT'��/�+L 1 0 1.0 Raytheon Engineers &' CALCULATION SET NO. Constructors CALCULATION SUMMARY flpp — PRELIM. FINAL _ � VOID REVISION & CONTROL SHEET Page 1 of 2 DISCIPLINE T z - J•O• L PROJECT TITLE �� - / STRUCTURE OR SYSTEMDESIGN CLASSIFICATION SUBJECT - 3Q 30 ^ 30 COMPLETED BY N �, E DATE CHECKED BY VA r / DATE APPROVED BY DATE 7 ��P • qd SD OR MGR 07 STAFF GROUP DISTRIBUTION REASON FOR REVISION: TOTAL NUMBER OF SHEETS IN TIM .......................................................................................................................................................................................................................... ISSUE ........................................................................................................................................................................................................................... ....................................................................................................................................................................... ..................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... - SHEETS SHEETS REVISED, ADDED OR DELETED . PROBLEM STATEMENT: ...................... U, . f'Q..t1is/C?.�4T..fo.. ...... r ............ T,�..'.iC'A..IAI..... T. AIllC............................................ ............................. .......................................................................................................................................................................................................................................................... ..............................................................................................................................................................................................................................:.......:................................................ .................................................................................................................................................................................................................................:..................................................... ....................................................................................................................................................................................................................................................................................... ..........................................................................................:.............................:........................................................:..................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... SUMMARY CONCLUSIONS: .............................................................................................................................................. ,FD...r/n�� H. . -13.-0.f �...!o.......4 ...................... :........ .................. A4.o, -d. ........ a. ....... 7-2 . c.......saZe........ .N.. D....... �'.. ; !S..T.......: Li r .. !,q .. ....... 0 'c. ,.s................ ...................................................................................................................................................................................................................................................................................... .......................................................................................................................................................................................................:............................................... t.............................. ..............................................................................................................................................................................................................................:........................................................ ..................................................................................................................................................................................................................................................................................:.... ....................................................................................................................................................................................................................................................................................... ................................................................................................................................................................................................................................................. ......... AXALC-SUKDOT • .7 • MOM= Engineers & Constructors CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2 PROJECT TITLE L i CALCULATION SET NO. pfl — PRELIM. VOID REVISION DISCIPLINE 577<,aL 0 7 DESIGN BASIS: ....................................................................................................................................................................................................................................................................................... .... 9 .F...t/`1.....,............................... V.NIO.........fr....A....................................................................... ...................................f'�e. ,r r..........so..4-s....... :-Ar....................................•••.......................................... .............................................................. ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ...............................................................................................••...........................................................•.......................................................................................................................... UNVERIFIED ASSUMPTIONS/OPEN ITEMS: ...................................................................................................................................................................•••................••............................................................................................... ......................................................................................................................................_............•••................................................................................................................................ ..........................•......................................................................................................:..................................................................................................................................................... ............... ....... :................................................................................................................................................................................................................................................................ .........................................................................................................................................•••.....................................................................:..................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) ................................................................................................................................................................................................................................................•••••.................................. .............................. :........................................................................................................................................................................................................................................................ •.4....... iM..G........................................................................................................................................................ ........... .................�z,..... .3.1.e ..... 0.s ............................. ............................................................................................................................................................................. ....................................................................................................................................................................................................................................................................................... ......................................................................................................................................................................................................................................................_............................... ....................................................................................................................................................................................................................................................................................... COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) REV. NO. REV. DATE PROGRAM TYPE RE&C VERIFIED YES ❑ NO ANALYSIS DESCRIPTION RUN NO. RESULT The attached computer output has been reviewed, the input data checked, and the results approved for release. INPUT CRITERIA DATE CHECKED BY DATE BY RUN BY DATE APPROVED BY DATE AXALC•SUMMOT r • 1 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET y✓/�� ��Dfl-S� CALCULATION SET N0. Z Qgew& REV. COMP BY CHK BY PRELIM. FINAL OID eAT% ,ATE ry PROJECT SUBJECT L�iP,�/� T�I�itl/!�0� SHEET OF DATE DATE J.O.%%D.4I00/ Gro yi�it/T Fo,P�t /o, Sir r"sr'i/�Art w�i�f/r o�' v'rssr[ z ' Tom' y SG1-7,L3 //, S X .8, -5' X /. S "C' r�i%gra' dries yi�n/T soi� ou�,e� d veDE.c/ ,yPcily )o�' /Y.4'r l• �- ,(>ti�T,� of .sbia 67h, TOT,4L L3Up�,o►,r/r ��O.c�« 1� ToT,9'� .E'cS/STA'�/T cvT OF So/c � SGA.c3 oi� Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP BY CHK'D.Y Constructors COMPUTATION SHEET PRELIM. FINAL VOID PROJECT SHEET Z OF DATE DATE., SUBJECT r ;o/ J.O.%7OS� DO% WR /A of ar"/t WT 7-�FAl/(: /D, S/c T-4T�L Wr'/drl-oeT Z/ S y • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. C,,��OM..PGG. BY. CHK'D�$Y Constructors COMPUTATION DATE SHEET PRELIM. FINAL VOID 5 PATq mr PROJECT/L !% GODSC SHEET • OF DATE DATE SUBJECT /it/ J.O. w he o� •� a .ST'AGE'D El � Is orm 5007 (Rev. 9/95) Raytheon Engineers,& GENERAL CALCULATION SET NO. Constructors COMPUTATION /-?/Saao - SHEET PRELIM. FINAL VOID PROJECT WIZ -0 SHEET OF SUBJECT Q. A/A/ 724k6t J.O. REV. COMP BY CHK'D.AY - AP j%A'7�fT , ''DATE ' DATE DATE • 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D,.� Y Constructors COMPUTATION - wee V• SHEET PRELIM.FINALS VOID TE AT tr V-17 6y� PROJECT W11- U LtDOSG? SHEET Z OF DATE DATE SUBJECT .�PDLESS D.C�4/.c/ TA.�// T -HOZ J.O. 7705 Z, OD I f/►.O�i DI 7 5Z A122 BE�,�i�/C �',Ptssvrc f'Creoss ' 2D 4ee 8 X ii o) 7Z 72 ""sxr P,vEr = 7Z7, - �G, ZS >s 1io -� 9� 7 /'.S / /yv z Z A 33 z o/S/.l Y'14-7- Oo/g X /SX /Z /Z /e/ ir✓, Z/147T lisp Two /'��Ts SSO /Z 7/B • 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMRBY CFJK` ' Y Vd�� Constructors COMPUTATION SHEET o - PRELIM. FINAL . VOID ATE / AT .o F PROJECT SHEET OF DATE DATE J.O. eel SUBJECT f �OGt_SS Iif.4/AI 7Aii/.�T �Oj gzo i.O'i rit vCIfriaAIS T/Z,,vc role To D/N.4TC �L.4CC`�i�1E h` ' x - WILD GOOSE G,KSSTORAGE PROJ. mitlaw Ord" al FOR INITIAL REVIEW ` �� . u FOR REVIEW OF REVIAO ! J FINAL • NO RETURN REO'D + _ _: !OR INFO -NO RETURN REQ'D .r.!'+ Ml�MMENT ear a am fOR FAB WITH 00 1{ INCORl. FINAL REl1'O • �I NO COMMENT • RUEASED FOR PAD FINAL R6Q�II — WIR E. �f",p , NOT RELEASED FOR FAB • REVISE! RESUBMIT FO %'... _ / REVIEW DOES NO RELIEVE ILTTT FOR mMPL1ANCE WTTN THE CONTRA DOCZJMElRY --V. ------------_--I' ` ------------- P -r-- '2 4 a o ce c o0 0 00 00 0o ao 00 00 0o eo 00 00 00 o 00 00 00 00 00 00 00 00 00 00 0° o0 oe eo 00 00 00 ov .,. °woe oo , o c° coo °o°oo 00 0 'o °oc°oc°oo°oc ^oo 0000°ec "copy - ° >.. ° 6" MIN RECOMMENDED BACK—FILL ee ° ° ° ° °° °° Ace �° °° o °° ee ° eo ° �°.woee o o�i o 00 o0 0 oe oo_ oc eco 00 00 00 oe o 00 0 oo ve ee ° _ r 12" CONCRETE PAD NO METAL TIE—DOWN EQUIPMENT TO COME IN �l CONTACT WITH TANK. TANK TO BE COMPLETELY 5 ! ISOLATED FROM ALL METAL OBJECTS. 7,_011 i I NYLON STRAP (3 x 1/8) w/LOOPED ENDS j 2 TURNBUCKLE 5/g" DIA w/HOOK ENDS .(GALV) "0 WIRE ROPE 1/2' DIA x 7,-0" (GALV) I TWO FIST CLAMPS 1/2" (GALV) 50 TWO ,TIE -DOWN ANCHORS #6 ROD (EMP STD) I. OUANTITES LISTED ARE Pnp nNip QTDAD ')-4C'nn) c. /EMF'/contig/UL.lib) vv� V CUSTOMER- WILD GOOSE GAS STORAGEJOB No 6339—.D01 Eaton Metai ProductsCo. 4800 York Street Denver. Colorado 80216 DESCRIPT. EATON STD TIE—DOWN STRAPS _ (303) 296-4800 also Salt Lake City. Utah BY G B A DATE 11- 21-97 CHK'D TCW DATE 11726 - 9 7SKT No.T D S —1 • I - NZ N3 N4 •� N f _ Ks N6 '= po-AAOMA" 1. GRAD 6 0 so S L .1 jM�IWL+Bf tEMT .1 a 7L-cm ♦ 1 � � �... 1 LTJ � � � f a _ Tia D owAv `I VA: g 3 I UV Y4AIC Y mF 7-,4AZ4 4V17H 6,;e o vND W ATM _M 501L rUIZW-6 8 TgAJK l G 5 6,#Z X B. 3 S< Y6AC Z 2 f 8 a: �s s'' � TAi�L� W1.= y000 11 .. .... �-ASSUA44 • _ _A,40 #&ZP "I 7-Y ..:.moil.. - o✓E TAAI,4,,' CIO OAXZ4 s U Sc .. SLA6 c.,12- i Z X 24 "k. ao . ..GOOAIa26 rL :Lomas::_ 4 FT. Fr X2 X�C /O _ .... *44 C2 /o _.W� 2 �_o s __... . Ig EATON METAL PRODUCTS CO. CUSTOMER K /t 7 // / W (L (J �QUSG CONTRACT NO. & -3'3Z 4800 YORK STREET p. /LOv/ DENVER, COLORADO 80216 JOB-& ( � (303) 296.4800 fn (+� /� ALSO SALT LAKE CITY, UTAH BY DATE CH SKETCH NO. %D J L u .• Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. PRELIM. FINAL VOID REV. COMP. BY CH�K'CLB_ Y AT y PROJECT DATE `DATE SHEET OF 'j-0- 77,0sL, oo/ SUBJECT 0,eqiA/ r-&'7" T- �Q3 x .4 tee /B�P CrL�SS sT.E'UGTU�C"S l3U0 YWAIr 040W e37, 9/c wr/41�r' T,Py 51 -AB 20'ov /Z 0X s� tA�T Q/ r Zo n /Z?1 / S V, �'sTiligrE l3Uoyi9�vT soil o ��,� Bvev�.c/ z ¢ -1S7 f -z, �) 0,i TDTgL ,��s�sr�l'•vr ►ver o� sa�� �s�.9c3 19 Form 5007 (Rev..9/95) RaVMcon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CWY Constructors COMPUTATION ` DATESHEET PRELIM. FINAL VOID DA E PROJECT W11- U 4t 20 --She SHEET Z OF DATE DATE SUBJECT lae,42t/ 1,03 J-0- 770 100 ' f3E.9A Ai.✓ �.c'�ssv,��" of T7WAlle ,37, 9/ef-1, ¢k M/AI,fit ii✓i� , oo /,*X /Z?e /B/Z = . /9 /,,V �T 7- i . ° r • ' ♦Y t A e i Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP BY CHK'D Y Constructors COMPUTATION SHEET PRELIM. FINAL VOID s TEAT,E� PROJECT ►�/ �L L% �?'DOSG� SHEET 3 OF ~ DATE DATE SUBJECT iJiE�i�I/itI Ti9N/� T -3D3• J.O. 77D5L, eel— r- o/ r -3o3 of 1 • .7 • Raytheon Engineers &, CALCULATION SET NO. Constructors CALCULATION SUMMARY / : / Z & CONTROL SHEET PRELIM. FINAL VOID REVISION. Page 1 of 2 DISCIPLINE v L J•o• 5Z,::26 PROJECT TITLE STRUCTURE OR SYSTEM TeUG /e 1-0"WmY4 SCA2ESIGN CLASSIFICATION SUBJECT 774wCk eg.4golulA COMPLETED BY DATE L5" CHECKED BYK,d y i DATE 6/ 2 ��9 S APPROVED BY , fI DATE _ SDE OR MGR OF STAFF GROUP DISTRIBUTION REASON FOR REVISION: TOTAL NUMBER OF SHEETS IN TICS ........................................................................................................................................................................................................................... ISSUE SLEETS REVISED, ADDED OR .......................................................................................................................................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... ...........................:..................... DELETED PROBLEMSTATEMENT....................................................................................... ........................................................................................................................... f. .........T ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... .................................................................................................................................................................................................................................:..................................................... .........................................................................:............................................................................................................................................................................................................. ....................................................................................................................................................................................................................................................................I.................. ............................. :............................................................................................................. .........................................................:.........................................................................................................................:................................................................................................. ....................................................................................................................................................................................................................................................................................... .1 SOE' D.l�/l:S./K........! ? ..........�. ....... ........rL............. :........................................................................................................................................... SUMMARY CONCLUSIONS: ....................................................................................................................................................................................................................................................................................... ......,�r%. Q. (✓ ........ LfiL3........IAr,IGL....., f1/EL.y.....,,Fl,00}....�.a'¢'1.... ..... k.ow?!�............................................ ...................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... .........:............................................................................................................................................................................................................................................................................. ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ........................................................................... ......................................................................................................................................... ................. .... ...... !.......... AACALC-SUM.DOT 0 11 0 Raytheen Engineers & Constructors CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2 PROJECT TITLE 0 G E CALCULATION SET NO. �o PRELINI. FINAL VOID REVISION DISCIPLINE ST%?l>G Tvt�i�FL a.o. Om DESIGN BASIS: ....................................................................................................................................................................................................................................................................................... % / � ..... P. A441(�.L.s 4............................................................................................................................................................................. --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- ....................................................................................................................................................................................................................................................................................... ...................................................................................................................................................................................................................................................................:................... ....................................................................................................................................................................................................................................................................................... UNVERIFIED ASSUMPTIONS/OPEN ITEMS: ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ...........................................................................:.................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) ....................................................................................................................................................................................................................................................................................... ..................f'/ P��✓G Olio �c/1r.. 5................................................... ........ .................................................................................................................................................................................... ..........................Q...........1�..G..................................................................................................................................................................................................................... ... ........ /8......p. ............................................. ...................................................................................................................................................... ................................. c. T'!ra:.........................................................................:.................................................................................................... ..............................SQl..G.,s....... ............................................................................................................................................................................................ ....................................................................................................................................................................................................................................................................................... COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) REV. NO. REV. DATE PROGRAM TYPE ' RE&C VERIFIED C] YES C] NO ANALYSIS DESCRIPTION RUN NO. RESULT The attached computer output has been reviewed, the input data checked, and the results approved for release. INPUT CRITERIA DATE CHECKED BY DATE RUN BY DATE APPROVED BY DATE A:\CALC-SUM.DOT Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. 'REV. COMP PY CHWD. BY Constructors COMPUTATION 121 C6GSD- L SG SHEET PRELIM. FINAL • VOID DATE 62 PROJECT'SHEET / OF DATE DATE SUBJECT/e ZeW^ ✓l 5'G.4, 1 J.O. 77oS4, DO/ CrU.,'.e0el /V zsZ92 ; 9 ij- io SIL/K. OF�\ 0 01 Form 5007 (Rev. 9/95) RaytheOnBnglneerS & GENERAL Constructors COMPUTATION SHEET PROJECT_W&O l-TO0Stf PROJECT W&O CALCULATION SET NO. �" L REV. COMRBY CHK'D.BY PRELIM. FINAL . ✓ VOID TE �� DATE 7 - SHEET Z OF DATE DATE SUBJECT T;-Pa4/C L D, g�//✓L SrLiA.B J.0.77OSL� *,4.. ,4. �c .s13 To lywrc N G rA�/ ANv �S X -Af,W7 AO',^f4 r .E'rr.✓f — � � � � �1- ASS Ge�✓T. D GN Alp A`Sx 'ezov, F�i✓O D//Y, NOT S//OW.� St0" SC"tT,b,✓ � D� SACT/O,c� t3 -L3 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION SHEET ILSZA222 -/"" TE D ATE 6 Z PRELIM. FINAL,,• VOID PROJECTWA(- D elf 40Se DATE DATE SHEET 3 OF J.O. 77D o0 SUBJECT o - aewl c/ L SNC UtS/�Al. 12 �.clsf'tclio�/ CeAele—J /✓v U.,Olr / / r O.eGv 7`0 L3.0 Z3ySe /;9 f G/3S�8=o" �Ovv ver/o�✓ f o.P /'�S � o- � / �Nt t � :S ; F� Ps �c% , f4DZ)1r10A/A1- P/1'E SG 7->`,A � CN -O r foe f'i sj i7c �' /2/,A r 4>R Aj[,vi,✓G -/,/0 -14 - SO9 le , I I .v - - _ - - - - - - - MATN. CHUNE 252960'-0• NO ZTC76'G., .j¢• !r 3�_ ';. - - - - - i u � _ 4• BUNO FLANGE . DRILL FOR 2 PIPE i';- > •. ^j. �:f• - ,) . F3* MANUAL oONNEctaNf'4'G°'° n o I I I m - i - -- I v 0 {'i 3• RED. 0 c f F EL 69'-0' I 1 yz i 1 4•-1500 RF FLG. 0 z 1 W W _ `• W z - - 6'-0 Q d OWO 's I'IOUi ro a Pu"to WI I B SOUPNC FLANGE EL 68''-0-0'* 6' a 14' CONCRETE' it II . SLA& HIGH POINT EL '' 7.0.5. EL 72'-6• N 25292{'-0• 8'-6• I I I B'-0' . Of SLAB 68'-0•; - I I I — - i - I - B.O.P. O INTERSECTION SEE DETAIL A w/ 16• SUMP �� EL QS' -0 5/8' _ /-GUARD POST N 252922_-0-0•_ 2'-O T.O.S. EL r4L-------=�h- 2lotoO-AIG-IH-E/T 12 - - — - - — — 69'-8 5/8' — _-r_ - c 210101 -AIG -N — - — - - — - i - - - - _ = - - -- - r I 2•CGIOO-A1C-N - — — — - n 2LO102-AIG-N " o I ' 3VS389 II a {VTIIB-AI-N I SEE DETAIL B I GOOSENECK I i EL 72'-0• SUPPORT ALL {LANES 6.6• )/{'LP. DRAIN B.O.P. EL 68'-6• I I B.O.P. LE I - f/F EL. 69'-0' AT THIS POINT c 2'_0• (TYP { PlACES) EL ITI1 LETI T.O.S. EL 69'-0 • �' 3/4 H.P. YE14T MATCHLINE N. 252915'-0' FOR CONT. SEE OWG. 16-10-309 1T I ' - - (TyP 4 PLACES) ' o Map ollc REVISIONS I1r oml RENSION APPROVAL RECORD IRIEV P2 �DRAWWO RECORD PRINT OtSTRIBUTION RECORD ORA1MttG STATUS PIPING A .' �, •oom tna oswA[ RVA001 euc ooaa P4A1 04R 6118 i . STATUS REV DATE SDE PEL PIPING PLAN as ww EO a a�aml a BO Ifel FOR M10 I u Amur OSNmII CARO FILE DATA d> UL PI D P2' 16 1 ^ IMC ARL>f/IRIICIL TMDAUTOCJiD 1161 13 oalT 2H 1 C�j, SCALE: WILD (PROJECT ~aL "F' 00mm 1O°p ^m ,v Ix IIL �/e'�1'-�' WILD GOOSE GAS STORAGE N 10cm OMIIOnOIYI Ille'l !\F-1\00\FM MIIM 0o pro, RNm • MrOwO DYIT'NO. ' ' fYy1 - "'a'A' OOL ..LIs w4K.a. 14P 3P a Engi=rs & 16-10-308 ES JORDER i P2 ui{ FOR WtERUI iAIIE-OFF ED Vol.ow Io 4v..�,Ox 0,,.,�;,,�, l,.n.» • Conshvctas NO PI /9! FOR Bb PMY ED 1lCUm6/10/96 M lOOCII Au rlwrs MA�Ip naval Dia[ Iy0• MY in 77052.001. m R 7 d { J iATCNu1 R OR CONT-. SEE OwG. 16-10-308 :MMMT MIMMMM 1 mrr mmmmi mgqmmmmlmmmmmmml A 210101 -AIG -N-\ �• \ / ( 2'CG100-A1C-N-\ !, -) V 210102 -AIG -N-\ FOR UTO �fMR I1m O��a 0cow ALL pmn V-1�' fG102- FG106- B.O.P. 69'-0' 8 EL 70 l• M., PIPING • A °E1 PIPING PLAN SCALL' WILD GOOSE STORAGE INC. 3/8' -i' -o' WILD GOOSE GAS STORAGE PROJECT owc. N0. ]Engineers & 16-10-309 Constructors 77052.001 REV 1a O 7 • 0 C, FCRIA 5010 REV 3M Untied Eng111eer: CALCULATION SET NO. & ConastrCALCULATION SUMMARY 13 & CONTROL SHEET Page i of 2 PRELIM. 1, FlN_WC �/ .VOID REVISION _ D PROJECTTITLE W i (� Goose 3+d"L- �e-i 1;'�-�/ DISCIPLINE 1-" L LA GC i.o. 7D SZ.Oc STRUCTURE OR SYSTEM F;:' Io J A i 0-111.1 DESIGN CLASSIFICATION SUBJECT �IyC.e ��"r4tG40ys COQ-IP,Sc�hc) FL i�r f:�Dw,tJ4_4i" 11 COMPLETED BY G M'I erT DATE CHECKED BY �AA1r/-1O /V V 7W4e*4CeA1 DATE APPROVED BY ��/� _ _ DATE SDE OR MGR OF STAFF GROUP DISTRIBUTION REASON FOR REVISION:TOTAL - - - - .... _ ...... - - • - ... _ .. - - ..... - ...................................................... NUMBER OF SHEETS It� Is ISSUE 1 SHEETS REVISED. ADDED OR .......................................................... ....................... ... ..-----.....__....-----•......--- DELETED .................................................--------- PROBLEM STATEM t .... �eS ic�.'►10 u: n c� a, : d . s !,� ............................••----•-..................._.......•--.......... ........................•-----•....----..................................... ................................••--•-......._...._......................--- -•----••...............................•-----.............---............... SUMMARY CONCLUSIOaS: od�..._..a-.,-�o r_ ......:.. ...`1 e w GQ�Ig��,�.►�+9..� I+�.r .... ex�•�ed1� y . i'�e .all owab�� .so. iQE'ar:11n7 . ve�sc�t .............. ..........•--..............•..............•--..._.....--•---•.........._...... .........................................................•-••....-••-•-..... -•...................•---•-•••---•-.........----••.......................... ............................................•-.................•-•-......... -•...................................................._.........._........... .................•--....................---........---------................. ......................................................................-••-- AO7W01711 • 0- 0 FORM $610 REV. 3M3 CALCULATION SUMMARY & CONTROL 9 Of Z SHEET PROJECT TITLE GQ°S e 5� ov' e ae i i CALCULATION SET NO. 1327 ba0 — I PRELIM. FlN�L VOID REVISION DISCIPLINE S lrwc r .SZ o 0 DESIGN BASIS:_ .... ._...��t►9..5....................................................... ------- 5______________ ____-__-----------------_______--_-- -------------------------------------•-.....-•----=--------__.._..._........ ---------------------------------------------------------------------------- ---------------------------------------------------------------------------- _ . _ . UNVERIFIEDASSUMPTIONS/OPEN ITEMS: .__..... ---•..... .... ........ ................. ......... ....__.._•............ ........ ....... ...... ..... ... ... ---------------------------------------------------•----------------------- -•---••••.......................................•-----...__........------... ....:...........'.... -.................... --.... ....... ..------••--••.......................•---.....------.._.._.._............... ........ ............... ... ..... .. ............. . .... ..... _.............. REFERENCES:SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, --pp COMPUTEiiRDATA, FSAR, ETC.) ........T.!� ... ...................................................... - �l�✓IDD✓.'.!'tx�.S..................................................... -•---_C�.$.=5 ..-....._-•----------------••-_...-------• .....................••----........ ---e5i�•yL• �rit-+�iG ---... ............................................................................. ............................................................................ ....................................................... ........ _............. COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) REV. NO. REV. DATE PROGRAM TYPE UE&C VERIFIED a YES ❑ NO ANALYSIS DESCRIPTION RUN NO. RESULT The attached computer output hes been reviewed. the input data checked. and the results approved for release. INPUT CRITERIA BY DATE CHECKED BY RUN BY DATE APPROVED BY DATE DATE A{jwul /R 1327O�p_1 i i 770S2. vol z4/ 9 8 W1.18 Goose- [Y e[y co I c-+a J o r F7ou of oA o v� J 47-�' '7'9" /6_vu /'7-O" �! U- 2ol,4-V -0/8 G, 2z ZJ 22z co IK NIN �► N, zsz7s7-o N ; O.. , P - _' Af N 8 8 /rABRS44--4�tiN)-Z ' I x Pl h 3 ly Col- Cotilfae- r ICo t.l kj11 a`�io 2'9i 2=9i %X30L D`' 3-Ea, Sir S aced z er -splices. -- — s FJV4- ` x3o'-o� is-T /. -B, �SPa3b ;'�,%x2 Lo I To 1 =3 *7, r--11=Z" 7 CZ 1: +b vv,atc� (o n7 bars 10�G " f E$, S�a, 3 #7 r---� �! M 7 (--'j 2 (3" � 4' T; ; ��:' - � � E' , � ac ed i I ix �3t�q,S)d� /4-'7 +o 0 . rorm ouut tmuv. u/vo) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET `' I- IJ Gm:6e- CALCULATION SET NO. REV. COMPLY C PRELIM. FINAL VOID - AT 6 89a TE Qm.8 PROJECT—W SUBJECT G'y Coi C_9m L�Ir ►�1 SHEET ,Q OF , DATE DATE J.O. / QSZ� DQ� bar • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors ' COMPUTATION SHEET / PROJECT w f l a COOS e SUBJECT C.-tIV COI `O►�+�iL�OV V�� CALCULATION SET NO. ` S2 0-00 —1 REV. COMP. BY FG CHK'D�D.,,BY D . PRELIM. FINAL G/ VOID F� _ SHEET ' OFQ DATE DATE J.O. /,70-'2, 1)0 2=334` S k, r� � D°`"v` � Vessel Faase � AhcV►or er _ AV%elk bv '90 C.1�4►r r A D_ 0 •) 6e, Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET OOS e- CALCULATION SET NO. t;-2 .600— REV. COMPP, BY FG CHK'D. BY � DTE PRELIM. FINAL VOID AT Q PROJECT SUBJECT o � Q A0 SHEET _ OF DATE 6�ll�g DATE 1�/%8 J.O. 770 Z.bc.�/ Lo- U-ZD1 A-V .t U -7-01$-V (DAle Peifap'lece- \x -7-M) DL = 43,3 opevoANj +- pac-L4,,5 = 48.7'- - Test � �sK -rof�,l C��era,,l-►9 < <}�,3..-t-;Socal"/1arl,)- 47.6"- Sei Sw, i L :base Skeczv _.3(1,25) (,MS)�48- 7) a 12.6 k SPiSK-%44-- is wLi C - base ' rKcm ekt 1 Z.28y- W � v%d base s�ear = 9,3 r_- base r»ome►�, V - ZoSipG,,.e. KAYVA. -DL= 26" 'Tcst _ 3484.5 Of 27 q s`7 � say 2 a 1L SeiSwti C-7 ats� .SLieekr = 3.(I..ZS��Z.?5)`Z8� `7.2Z-� .. S e is wt ► 4 C. G. = 6 04.2-- 1.7/G 43'7.4 - 9,3? 1-5& IS "I c base M0 .?•Zz"7.77><�f W ti►� base Skea►- = W ,�� base wi ow,ewl = 13.S4K�t' 7>. �ZDa .31"�.34►� � . 65'� �e iSr,n i G Govervi s Sei's K C- Goverr►s t:>L= :ZSf,�lf.3't::l4t.7*..19-t,9z�Z �.93K • 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET O os a CALCULATION SET NO. [S2f7000 - REV. COMP. BY ' DAT DZAT Q CHK'D. BY PRELIM. FINAL, VOID "D �� pgTE L►� 6//l 9Q PROJECTx W 1' SUBJECTL;IYCCbl C�bv► GiL�BY' rG SHEET OF DATE� G 11AR J.O.'??P)�Z, 60/ - -0,0j�( Pf 3 pf, 4 K f'�ZD _ (2,���. Z3`� f .14 Kf �3 3'`'�-� 4�� z 1• $ 8� Z Z r-�-�27"-f /4'`t.13� Z9 y -t :2gKt2.93 7- 7 8 - i 4 H- p % 3 3K�-; 4z') -t-, Z W, 0 Form 5007 (Rev. 9/95) Raytheon Engineers & ' GENERAL Constructors COMPUTATION SHEET ��i` S PROJECT V�[II� I e1. SUBJECT �\UCOl LaIrl �C.'tor �h CALCULATION SET NO. l3Z ? 0-0 REV. COMP. BY CHK'D. BY PRELIM. FINAL VOID D �Z rl � SHEET 5 OF DATE 6/ l,19g DATE ee714 J.O. /?QSz•001 s e�Swli c Lo �5 .Ver• n yr tio. Sei wc-'% c 6,3a 44,*,7. �'iS= 12.3 Base Merle, -►f' _ :3.4�(iz•..5�)=g3.s3K is 44-K � F�-n,,,.► V -Zo S �ra�l pf • Z Verf• fer �ia►-�, seISPv4L ,g2K-�.19.I`t,S3 �.t.ql�` t s0K+,47-'-+.7" = 4-03r 4.28 r-(Zb) /•20"` 3 as e M 6f _t - l.2 n(S� Lo �s Taste sh �r =L 3.4 = -4.4 "*,,7.2ZKf l,20�_ /1,a�"sa,�, K. jas e , j�l o;M al , -�- 67, 8 + /0 121.8' 9*f ,Ay / Zz� 1/ 11 u Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION !3z %0 00-1 p SHEET PRELIM. FINAL VOID Z SAT PROJECT W/ 1 I Q C �Se SHEET 6 OF // \ I 1 r� :yam DATE �D,TE SUBJECT ' Go l aGTo J.O. / QSZ. OO� 611 f/1 S e 15-KIVi Z.. Z-6 GAS va Lqy v-zd/Z- v �►�� 7�f: � 8 V er .. or o►-�, S42 SPP-PIC- = ,ZZ Kt. SZKtL2l IC -V. + _.....__... .. - /8,4 . �rr�-. Seisr•N-i �° _ , 2$20 .q\ = S. %� �c. Tose Mower = 3.7Z'�(/9•/9� 2.109.8 KFs4� )Vo�'R. SeiSwi;C. %Z. 6 y `]34s e M ovn &J L V -C'- , or �or�. Sell S&'%4 K4- 3 6K+. 39 �+.54K' s. a s2. M eIM d(7, l 7) SAY .I 3 , t- base sAeav I 5.?Z"+ 4-/, 2 U-Zo/A-V .;s see a -s' O-ZoPy—U 0 .0 yr � � ^ ���� } ~-k8 � / ��� » � ~~ / popMvc /,^A � REV. ^»^ � ----------------T--�' .001 � 41 �'- �---/� ~~~ x �� ��--'----------------------------�� �� --- CUSTOMER ` SUBJECT 47 14 .0 PTLO 2.0 | � 16 Az 77 1.0 / / -�--'- - _ L - - '------�--�- ----�-�--'--`---- � �-� '----- - ' - �-' --------'-------- -- ------''---�-'�------'-----------'--- - -'---'` - -'� - '' --'--�--------r--r-----���r��--� -�-- -'� ' - ' ----� - ' - ' ' —��- -,-� '�� '�--�--- '-----�� - - - ' ----- '- -! '-- --'--'-----�-------------- -�--��-' ---^'---'-- / / `- ---�--L--��--L-�4------�- - �� '-�--' -'- � -� ' - '-----'--�--�-'�-----'------�--- � r--��--' ------''-' -' - --'---�---| . -� [--�--�--� ----�--�---�- --�-- ----- - - ^ ` ' U Form 5007 (Rev. 9/95) Ra been Engineers & GENERAL Constructors COMPUTATION SHEET `_) . "`� ; fj Goose CALCULATION SET NO. 132'7oo0— REV. COMP. BY CHK'D. BY 14At PRELIM. FINAL VOID DAO AT 2 PROJECT SUBJECT!GIYC61 �Qyti+GAG b►r k^, SHEET8 OF DATE D ATE Fi.o.77052. &0/ 47.5•/ ��2.75��IS�+261.+ S4"+?•Sv`�+3%.K+6.4 9r �`�loY►1, =7.6122.5>+-54(!�� +rI•S�/),?�>+;2.6/66z-) .3ZOr.3 �• Ifs . 2-0 14(2) + + S2.3 j�l a,.,,► x _ - + :,S'2,'?�::`2.?5� + 35 �2, -1-122- = + 9.83: 8 xf� • M Y. 17.0 7) f12o,9K�t Inert,, Y = 3 81-...2 A, :=� .4s0 '916-3116 1028. B'kff o r� , -f •�2.3 K M Soe < Press wry�s e :e.. - P X ` 3Z�.3 L -47.s, _14) K 2•?,°... 9 S., .z 2.2- M So; l Pretr ve Z- 2., -7 f • is Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. ' Constructors COMPUTATION 13 217 0 SHEET PRELIM. FINAL VOID PROJECT V� 1 4j CCPS' Q SHEET9 OF SUBJECT `Y CQI G�L�OY �'I i J.O. 770sz, W F, ,,A D Presses► -e Lie REV, ICOMPBY IC KD. BY QDATE DATE v, B ` '7.58 vvn' L 24..s� j Y) ; 6 5.9� V" , G1 = B i i —yhw L it t� [ I —[� , 689\ z 16,'Z'6 3 9.24' Al of 1-9-essu ve = : /. 93 K'S F Z.-ZS(�. / S J ` 1. S� Ks F M /.Ip '7, o z' (i , ?S.C�, �� _l, 2 , w - 58 �'�/,33' DA•+ N' C he9�c �tJl r►., a c. , h as a M u .bee `i'1� eo.s. f-. h/�s.f d �r. e:c.�-j ._ {'r Ffi M =23_.24-t(.7)�I.1�.= 83.46 qb� _3:2,7z.+ 6 39'.. -1:41" 93.46 L. Z.SJK f"� :► :I.k C:A, l ', ! LA ---- -- a s -e 13,3 ll.'�0 1„. 13A3 H .. .. ..». .. .__..ter.. 4-....._. �. _... _.. .�....... ._ -.. .... _� -�.... Form 5007 (Rev. 9/95) Raytheon Engineers & - GENERAL Constructors CALCULATION SET NO. 3Z % 6 OO REV. COMP. BY CHK'D. BY COMPUTATION — E� SHEET PRELIM. FINAL VOID �� PROJECT r�nl I d C� eose -— SHEET OF l,.D � DATE DATE 1 SUBJECT I..TIV �` O� �bYL10l C O1� i1 ►' J.O. '/ �%05Z� BB 601 '� e � �oVC►� y �C cr~v� �ci� " = 3 esu (1 Z) 2 -BZ .3/.3 K> )4.17 K b k 4 � • 1.s I.T5 ' 2 Z.5 t - W Q 5.3 O 5 t O Q 10 L IL 71 v4L"S MAXIMUM UNIT PRESSURE 1 = K A e CASE I 1 CASE II 1 I 1I 1.0 c = 38(1-n) i r !-q+m'q 4m -1)q -4(3m -1)q q s +6( 1 ?-m-')20 CASE III s ' A. T .e m .1 1 ("ZI, . P ■ 252 kips M = 70.8 ft -kips M' = 18.4 ft -kips 981 0.031 L L = 9'- 0" f _ 0.073 • ' r e1 _ 'e - 7 P 0 O of K = 1.25 FROM CURVE, m FACTOR OF SAFETY X10 PAGE I lo f = K A = 1.25 632 = 5.0 kips/ft? , e= 0.281' CASE I P = 55.0 kips ° 2 M' = 110 ft -kips = 0.2 L 10 M' = 27.5 tt- kips 855 - 0,1 L lot on / K-- / FACTOR OF SAFETY = 2.50 FROM CURVE, ' P X. = 0,41 PAGE 0 Y = 0..6 1 _ e= 0.5 is t. m m f = K A = 3.0 50 = 3,3 kips/ ft2 XL 4 - e=2.01 y8 = 4'-0,. CAS E II P = 220.5 kips M = 331 ft -kips a__ 1.5 e' 2-86 L 14 ° 0.107 6 = 10 =0.286 f1 = 631 ft- kips K = 4.3YFRoCURVE. I FACTOR OF SAFETY = 1.FROMPAGE'I s'=2.86' P 0 f ° K A = 4.3 21405 = 6.70 kips/ft? - _ o � n$=7.86 mL=8.50 n=0.786 e =1,5' m = 0.607 q = 0.50 FROM CURVE WLSE M 1 38(1-n) 14'-0- .I c1 +q =8.0 c(t-q)=4.0 fl = f(f-q) = 3.35 kips/ft2 CASES �11 Tower..Seismic and Wind Analysis —Technical Research Services, Inc. 54x25--598 INPUT DATA: PAGE 1 Diameter of Shell 1 with Insulation (FT) DC1 4.792 Outside Diameter of Shell.(FT) DSHL 4.792 Height of Cylinder 1 (FT) HCl 28.830 .Height of Skirt (FT) HT 1.250 Outside Radius of Skirt (IN) RSR, 28.700 Shell Thickness (IN) T 1.750 Skirt Thickness (IN) TSKT. 0:500 Corrosion Allowance (IN) CA 0.125 Weight of Vessel -Full (LB) WF 68,092 Weight of Vessel -Empty (LB) WE 43,279 Internal Pressure (PSI) PR 1,000 Efficiency of Girth Seam EG 100.000 'Efficiency of Longitudinal Seam EL 100.000 Allowable Stress Shell (PSI) SSH 17,500 Allowable Stress of Skirt (PSI) SSK 17,5.00 Specific Gravity -'of Liguid (Water = 1.0) SPGR 1.250 Height of Liquid Column Above Base IFT) HLH 6.500 WIND FACTORS , end Pressure at 30 Feet(PSF), ,QS 15.000 Height Exposure and Gust Factor CE 1.300 Shape Factor for Round Shapes CQ 0.800 Correction Factor for Rectangular,Shapes CF 0.800 Wind Speed (MPH) MPH 75.000 Wind Pressure before Correction Factors are applied PSF 19.500 Wind Pressure for Cylindrical Surfaces(PSF) PSR 15.600 Wind Pressure for Flat Surfaces(PSF) PSC 15.600 Exposure Code (2 or 3) EXA 3.000 ' SEISMIC FACTORS, Zone Factor (1-4) Z 0.300 .Occupancy Importance Factor I 1.000 RW Factor RW 4.000 Coefficient C C 2.750 Coefficient Site Structure Resonance S 3.000 Period of Vibration (SECONDS) TP 0.144 P.O. M C62031 Raytheon Project #: 77052.001 Item #: U-201 A/B-V Sheet 9 of 12 Date: 4/22/98 PLATFORMS — WIND �A (Sq Ft) C.G. HEIGHT;(Ft) l AP( 1 ) 6:4 LPW( 1 ) 22.0,00 PLATFORMS — SEISMIC WEIGHT (LBS) C.G. HEIGHT (Ft) WP( 1 ) 600 LPS('l ) 22.000 LADDER — WIND HEIGHT (Ft) 23.5 AREA PER FOOT (Sq Ft),'1 C.G. HEIGHT (Ft) 12.75 LADDER — SEISMIC WEIGHT -(LBS) 500 P.O. #: C62031 Raytheon Project #: 77052.001 Item * U-201 A/&V Sheet 10 of 12 Date: 4122/98 MOMENTS - WIND at Base (FT -LB) MWB 37,563 18oment oment at Top of Skirt (FT -LB) MWS 34,357 Moment at Point P (FT -LB) MWP 32,501 MOMENTS - SEISMIC Moment at Base (FT -LB) MSB 273,963 Moment at Top of ,Skirt (FT -LB) MSS 262,035 Moment at Point P (FT -LB) MSP 254,878 THICKNESSES REQUIRED Thks Reqd-Long Press Stress Bottom of Shell (IN) TRPG 0.008 Thks Reqd-Hoop Stress (IN) TRPL 0.016 Thks Reqd in Skirt -Wind (IN) TWSK 0.000 Thks Reqd in Skirt -Seismic (IN) TSSK 0.001 Thks Reqd in Shell, above Skirt-Wind+Pres (IN) TWSH 0.008 Thks Reqd in Shell above Skirt-Seis+Pres (IN) TSSH 0.008 Thks Reqd in Shell above P-Wind+Pres (IN)" TWX 0.008 Thks Reqd in Shell above P-Seis+Pres (IN) TSX 0.008 STRESSES Pressure Plus Liquid Head at Bottom of Shell (PSI) PT 1,003- Stress -Pressure in Shell above Skirt (PSI) SPSH 81.699 -Pressure in Shell at P (PSI) SPP _ 81.699 4stress tress-Wind in Skirt (PSI) SWSK -419.617 Stress -Seismic in Skirt (PSI) SSSK 1,812 .Stress -Wind in Shell above Skirt (PSI) SWSH -128.580 Stress -Seismic in Shell above Skirt (PSI) SSSH 557 Stress=Wind in Shell above P (PSI). SWX -127.858 Stress -Seismic in Shell above P (PSI) SSX 542 Stress -Max in Shell above Skirt incl pres (PSI) SMXS 639 Stress -Max in Shell at P incl.pres (PSI) SMXP. 623 Moment of Inertia (Shell)(IN-4) IZ 111,342 BUCKLING AND DEFLECTION Yield Stress for Shell.(PSI) YSH 38,000 Yield Stress for Skirt (PSI) YSK 38,000 Modulus of Elasticity - Shell EMOD 29,000,000 Allowable Compressive Stress for Shell(PSI) SAC 12,667 Allowable Compressive Stress for Skirt(PSI) SACS 12,667 Maximum Compressive.Stress (Shell)(PSI) SCSH -939.374 Maximum Compressive. Stress (Skirt)(PSI) SMXS -3,359.899 . • P.O. #: C62031 Raytheon Project #: 77052.001 . Item #: U-201 A/B-V Sheet 11 of 12 Date: 4/22/98 SHEAR'" FORCE . Shear due to Wind(LB) VWTO 2,621 �tal otal Rhear due to Seismic(LB) VSTO 14,271 DEFLECTION Note: Based on constant moment of inertia for full height Total Deflection-Seis (IN) DST 0.032 Total Deflection -Wind (IN) DWT 0.004 Allowable Deflection(IN) DAL 1.730 BOLTING AND BASEPLATE " Diameter of Bolt Circle (FT) DBC 5.283 Number of Bolts NB 8:000 Ratio of Mod of Elasticity (Steel/Concrete) N 10.000 Allowable Compressive Stress of Concrete (PSI) FC 3,000 Allowable Stress of Base Ring (PSI) SBR 17,500 Allowable Tensile Stress of Bolts (,PSI) SA 19,000 'Base Ring Width (IN)" LB 7.000 Moment at Base (FT -LB) MZ 273,963 " Total Area of Bolts (Sq -In) BTOT" 5.791. Bolt Root Area Required per Bolt(Sq-In) RTA 0.724 Bolt Nominal Diameter(IN) BD 1.500 Dim from Skirt to Bolt Hole(IN) L2 3.000 im'from Bolt Hole to edge of Base Plate(IN) L3 3.000 ensile Load on Anchor Bolt(LB) FT 24,315 Comp Stress in Concrete Outer edge(PSI) FCON 751 Thickness required for Base Plate'(IN) TBR 2.037 Number of Gussets.at Base Plate NG 8.000 Distance between Gussets(IN) DG 24.897- Bending.Moment in Base Plate(MX OR MY)(IN-LB) MMAX 12,103 Constant used for K CC 0.844 Constant used _for ,K CT 2.891 Constant used for K JT 0.766 Constant used for R Z1 0.480 4 ` (�) �/— ��� / r 3 Fes• S-,= 22, b N n � (Si 2,9 T�.s� e S��-dSC, =- 2z, 12,9 14-s (7!9Y � P.O. #. C62031 Raytheon Project #: 77052.001 Item #: U-201A/B-V Sheet 12 of 12 Date: 4/22/98 ® l q,4 PERRY EQUIPMENT CORPORATjON P.O. Box 640 Fr. Wohm InduSTniAt PARk MiNE7RAI WEJ[ , TOm 760681 FAX: (940) 325-4622 C�NOV. • TEL: (940) 325.2575" 7DLLoLv Sent By:157AUf Date: !lQ From:_L�O' 3o3 / 8�3- 3622 avS� C f. SIO FOZ% 5 • �f izo �E { LJ T- qrO 090 # 20 q O U sE� �ecJ��E ST2ucrv2�. W r N 1'. l s.S C,41-45 0 3¢$¢S*' 7g5? 4 COMPRESS 5.60 I:\COMPRESS\STAPER\27665-2.VSL Mar. 4, 1998 Wind Calculations v- Z fl of wind analysis: OBft1994JC Elevation of base above grade: 1E,Method Increase effective outer diameter: 2 ft SE R Wind force coefficient Cq: 0.7 P CA Basic wind speed, V: . p �� N 5 m Importance factor, Iw: 1 5 Exposure category: /` • sign Wind Pressure find stagnation pressure qs 16.4 Ifttresses due to Wind + pressure, OoeratinQ & Corroded Elevation Type Minimum Heigght. Ce P = Ce*Cq*qs*Iw (Psf ) (ft) above base com ressive 15.0 1.06 12.16 20.0 1.13 12.97 25.0 1.19 13.66 30.0 1.23, 14.12 40.0 1.31 15.03 60.0 1.43 16.41 80.0 1.53 17.56 . 100.0 1.61 18.48 120.0 1.67 '19.17 160.0 1.79 20.54 200.0 1.87 21.46 300.0 2.05 23.53 400.0 2.19 25.14 Ifttresses due to Wind + pressure, OoeratinQ & Corroded Elevation Type Minimum Circ Required Overhead Bending above base com ressive thickness joint thickness weight moment (in.) (psi) corroded eff. (in.) (lbs) (lb -ft) 17500.0*1.2 125.2 (in.) E -193.1c 17500.0*1.2 232.9 33.00 cy1 . 1.5000 1.00. 0.5925 21280.,6 8375.9 0.00 skirt 1.0000 0.55 0.0112 '24936 7„- 11773.7. Table Continues Maximum Allowable-, -Maximum Allowable Total wind tensile tensile compress com ressive Pressure stress/E stress stress stress (psi) (psi) .(psi) E=1 (psi) (psi) & other) •8169.2 17500.0*1.2 125.2 17340.1*1.2 1048.9 -193.1c 17500.0*1.2 232.9 17188.8*1.2' 28.6 40' /J Elevation Elastic Inertia Platform Total wind Bending Deflection start Modulus wind & other (platform section top above base shear shear & other) (in.) psi x10^6 (I, ft^4) (lbs) (lbs) (lb -ft) (in.) 33.00 28.6 3.501 0.0 1131.5 0.0 0.0008 0..00 28.6 2.315 0.0 1339.6 0.0 0.0000 6.16..1997 Page 2 COMPRESS.5.60 I:\COMPRESS\STAPER\27665-2.VSL -Wind Calculations Stresses due to Wind. Empty & Corroded Mar. 4, 1998 Elevation T Maximum Allowable Total wind & other shear '(lbs) tensile tensile compress compressive Pressure stress/E stress stress stress (psi) (psi) (psi) E=1 (psi) (psi) (lbs) -56.3c 17500.0*1.2 125.2 17340.1*1.2 0.0 -193.1c 17500.0*1.2 232.9. 17188.8*1.2 cy1 1.6250 1.00 22280.8 2766.2 0.00 skirt 1.0000 0.55 0.013`0 38080.9 3888.4 Table Continues Maximum Allowable Maximum Allowable Total wind & other shear '(lbs) tensile tensile compress compressive Pressure stress/E stress stress stress (psi) (psi) (psi) E=1 (psi) (psi) (lbs) -56.3c 17500.0*1.2 125.2 17340.1*1.2 0.0 -193.1c 17500.0*1.2 232.9. 17188.8*1.2 cy1 Wind deflection report, empty & corroded Elevation start above base' (in.) Elastic Modulus,. psi x10^6 Inertia (I, ft^4) Platform -wind shear (lbs) Total wind & other shear '(lbs) Bending (platform & other) (lb -ft) Deflection section top (in.) 33.00 0.00 29.0 29..0 3.501 2.315 0.0 0.0 1131.5- 1339.6 0.0 0.0 0.0008 0.0000 (in.) Stresses due to Wind + Hydrotest pressure, New Elevation Type Minimum Circ Required Overhead Bending above base comressive thickness joint thickness weight moment (in.) (psi) (psi) eff. (in.) (lbs) (lb -ft) 38000.0*0.9 98.5 (in.) E -489.1c 17500.0*1.2. 268.3 33.00 cy1 1.6250 1.00 22280.8 2766.2 0.00 skirt 1.0000 0.55 0.013`0 38080.9 3888.4 Table Continues Maximum Allowable Maximum Allowable Hydro .tensile, tensile compress' comressive Pressure stress/"E stress stress s ress (psi) (psi) (psi) E=1 (psi) (psi) 92.3 38000.0*0.9 98.5 17369.7*1.2 6.4 -489.1c 17500.0*1.2. 268.3 17188.8*1.2 4 -COMPRESS 5.60•., I:\COMPRESS\STAPER\27665-2.VSL SKIRT BAS -9 PLATE s Mar. 4, 1998 2 Z Base configuration: External Chairs •Foundation allowable stress: Sc= 1350 psi Concrete ult..28-day strength: fc'= 3000 psi Anchor bolt material:'• SA -36 'Anchor bolt allowable stress: Sb=.19100 psi Bolt -circle: BC= 56.625 in Anchor bolt corrosion allowance: 0 in Anchor bolt clearance: -0.125 in Base plate material: SA -516=70 -Baseplate allowable stress: Sp= 17500 psi Base plate inner diameter:. 'Di= 46.625 in Base plate outer diameter: Do= 61.625 in Base -plate thickness: tb= 2 in Gusset separation: w = 8 in Gusset height: h = 8 in Gusset thickness: tg=0.75 in Compression plate width: .5.5 in , Compression plate thickness: tc= 2 in Estimated base ring weight: Wr= 721.8 lb .Initial bolt -preload:.- 50 A, (9550 psi) Number of bols:N = 8. Bolt size & type: 1.75 inch series 8 threads Diameter of anchor bolt.holes:. db-- 1.875 in Pipe sleeve inner diameter: 2.624:in f Pipe sleeve wall thickness: 0.438 in Calculate the load per anchor bolt Governing vessel weight: W = 24936.7 lb • 'Bolt overturning moment: M = 48308.43 lb -ft' Bolt root area (corroded'):. Ab= 1. 98, in^2 P=-W/N+48 *M/.(N*BC)' = -24936.7 8 +48 * 48308.43 / (8*56.625) = 2001.687.4b Required area per bolt = P /.Sb•= 0.1048604'in^2 The anchor bolts are satisfactory.. Foundation bearing stress (Operating) Ac= pi* Do^2 - Di^2)/4 N* 1*db^2/4' = pi* 61.625^2 - 46.625^2)/4 -.8*pi*11.875^2/4 1253.201 in^2 16=pi* Do^4 Di^4)/64 = pi* 61.625^4 - 46.625^4)/64 475964.8-in^4 � fc= N*Ab*PreLoad/Ac +JW/Ac + 6*M*Do/Ic = 8*1.98*9550/1253.201 + 24936.7/1253.201 + 6*48308.43*61.625/475964.8 - = 178.135 psi As fc <= Sc the base plate width is satisfactory. j Foundation bearing stress. hydro test condition ` fc= N*Ab*PreLoad/Ac + W/Ac +'6*M*Do/Ic • 8*1.98*9550/1253.201 + 38080.98/1253.201.+ 6*3888.491*61.625/475964.8 154.1162 psi 6.16.1997 Page 4, COMS 5.60 Z:\COMPRESS\$TAPER\27665-2.VSL liar. 4, 1998 23. PRES SKIRT• BASE 'PLATE As fc <= Sc,the base plate width is satisfactory. AftCheck'the base plate for foundationa From Brownell.& Young, Table 10.3:, 1/b =,.432 Mx = .0201*17S.135*12.73659^2 =:580..8331` My --.366*178.135*5.5^2 =-1972.221 tr= Sgr(6*Morax / Sp) = Sqr(6*1972.221 /.17500) = .8223 in .The base plate thickness is satisfactory. Check the compression plates for bolt load (Jawad &'.Farr -eq. 12.13) tcr- Sqr(3.91*F/(Sy*(2*b/w+w/(2*j) - d *(j/w+1/(2*1)j))-) /(2 ))))) = Sgr( 3.91*18909/( 38000* 2*5 5 *3 —1.875* ( *3 1.004802 in The compression plates thickness is satisfactory. Check gusset plate thickness (Bednar chapter 4.31 Radius. of gyration .of gusset r .289*t . g 2,89*0.75 .21675 in Cross sectional area of one gusset •Ag=.tg*(b -.25), = 0.75*(5.5•- .25) _ 3.9315 in ^2 -Gusset allowable stress (steel) Sa= 17000 .485* h /-r) ^ 2 17000 .485*�8 / 0.21675) ^ 2 = .16339.3 psi Gusset axial stress due to bolt load Sg= 189092/*(2g* 3.9375) 2401.143 psi The gusset plate thickness is satisfactory. Check skirt for bolt _reaction (Brownell & Young ea, 10.591 't = 1.76* F*1/(Mb*hc*Ss )^ 2/3) * (ODs/2 ^(1/3 1.76* 2001.687*3/(20*12*26250)) ^ (2/3; * (U.625/2 )A( 1/3 ) 5.005055E-02 in The skirt thickness is satisfactory. 6.'16.1997 COMPRESS 5.60 24 I:\COMPRESS\STAPER\27665-2.VSL Mar. 4, 1998 -Seismic Calculations Method of seismic analysis: UBC '1994 1 Seismic zone: 1.25 Importance factor, 1: _� N IE Soil profile: 5 L�gsE X `S Site coefficient, S: 4.5 P SM`C CALC Coefficient Rw: SEI Period of vibration calculation The fundamental period of vibration is calculated using the Rayleigh method of approximation by�the numerical integration. --of the following formulae: T = 2*Pi*Sqr[ Sum W*y^2 / g(Sum W*y) ] -- • �- l%-` ?�-- - 1+ D T o eratin = .027 seconds T�empty) g) = .027 seconds N° c Seismic zone factor, table 16-I: Z 0.3 C = lesser of 2.75 or..the following: (2.75) 1.25*(S/T^(2/3)) = 1.25*1.5/0.027^(2/3),= 20.833• Ratio C/Rw: use larger of 0.4 or.2.75/4 (0.688) V - Z*I*(C/Rw)*W 0.3*1*(0.688)*24936:7 .5146.935 lb T <= 0.7 seconds so Ft = 0 AmhBase shear distribution Fx (V-Ft)*Wx*hx/(Sum wi*hi) wi hi wi*hi. Fi Vx V(other) (lbm) (ft) (lb -ft) ( lbf ) ( lbf ) ( lbf ) 21280.6 9.58 203939.1 5023.1 5023.1 0.0 3656.1 .1.37 5027.1 123.8 5146.9 0:0 . 24936.7 310.5 208966.2 459.6 33.00 cy1 Stresses due to Earthquake + pressure. Operating & Corroded Elevation Type .:Minimum Maximum Circ Required Overhead Bending. above base comressive thickness joint thickness w i h s?ress in. (psi) corroded eff. (psi) (meet ) 17500.0*1.2 232.0 (in.) E 310.5 17500.0*1.2 459.6 33.00 cy1 .1.5000. 1.00 0.6001 21280.6 34324.6 0.00 skirt 1.0000 0.55 0.0222 24936.7 48.1308.4 Table ' Continues , • Maximum Allowable Maximum Allowable tensile tensile compress comressive Pressure stress/.E stress stress s?ress (psi) (psi) (psi) E=1 (psi) (psi) 8276.0 17500.0*1.2 232.0 17340.1*1.2 1048.9 310.5 17500.0*1.2 459.6 17188.'8*1.2 6.16.1997 Page,6 45'A`f4, COIiPRESS 5.60 'I:\COMPRESS\STAPER\27665-2.VSL Kar. 4, 1998 Seismic Calculations - A1111Seismic shear'reRgrt,•operating & corroded,' - Elevation I Elastic Inertia. Seismic Bending-- start Modulus (in.). &:other (platform above base (in.) (lbs) shear & other) (in.) psi x10^6 (I, ft^4) (lbs) (lb -ft) 33.00 28:6 3.501 5023.1 0.0 of 0.4 or.2.75/4. 21280.6 `(0.688) V = Z*I*(C/Rw)*W skirt -� 0.00 28.6 Circ joint 2.315 Overhead weight 5146.9• (in.). 0.0 corroded eff.. (in.) (lbs) (lb=ft) Seismic zone factor, table 16-I: Z = 0.3 C = lesser of 2.75 or the following: (2.75) 1.25*(S/T^•(2/3)) = 1.25*1.5/0.027^(2/3) cyl 20.833 Ratio C/Rw: use larger of 0.4 or.2.75/4. 21280.6 `(0.688) V = Z*I*(C/Rw)*W skirt 1.0000 0.55 = 0.3*1*(0.688)*24936.7 24936.7 48308.4 = 5146.935 lb . T-<= 0.7 .seconds so Ft = 0 Base shear distribution Fx=•(V-Ft)*Wx*hx/(Sum wi*hi) • w1 hi wi*hi Fi Vx V(other) (lbm) (ft) ( lb -ft.) - ( lbf ) ( lbf ) ( lbf ) 21280.6 9.58 203939.1 5023.1 5023.1 0.0 3656.1 1.37 5027.1 123.8 .5146.9 0.0 24936.7, 208966.2 Stresses due to Earthquake, Empty & Corroded Elevation above base Type 'Minimum thickness Circ joint Require thickness Overhead weight Bending moment (in.). corroded eff.. (in.) (lbs) (lb=ft) •(in.) 50.4 17500.0*1.2 E 17340.1*1.2 0.0 310.5 . 33.00 cyl 1.5000 1.00. 0.0167 21280.6 34324.6 0.00 skirt 1.0000 0.55 0.0222 24936.7 48308.4 Table Continues Maximum Allowable Maximum Allowable tensile stress/E tensile stress compress stress comressive s ress Pressure (psi) (psi). .. (psi) E=1 (psi) (Psi) 50.4 17500.0*1.2 232.0 17340.1*1.2 0.0 310.5 17500.0*1.2 459.6 17188.8*1.2 &ismic shear report, empty & corroded 6.16.1997 , COMPRESS -5.60 I:\COMPRE9S\STAPER\27665-2.VSL Kar. 4, 1998 .. Seismic Calculations Elevation Elastic Inertia Seismic Ben ing start Modulus & other (tlatform above base , shear other) (in.) psi x10^6 (I, ft^4) (lbs) (lb -ft) 33.00 29.0 3.501 -5023.1 0.0 0.00 29.0 2.315 5146.9 0.0 A rl Fd1M 5010 REV. 3M3 United Engineers CALCULATION SET NO. &Consh'uclOts CALCULATION SUMMARY 13270_0 — Z - - A''r" wuC0 W & CONTROL SHEET PRELIM. Fl VOID Page 1 of 2 IREVISION " ' (Q �OGSe �TOV e�I 1 .� PROJECT TITLE vel � 010 lPUNE rw L k IrGv '% D S Z, 6 O I STRUCTURE OR SYSTEM FoL,4, 4Li Oh DESIGN CLASSIFICATION SUBJECT ?✓CCCSS GaS �71 +cr V-2-04 mow+-tleA 1 ovi COMPLETED BY �1'�'� G� 1 S DATE -- Sf' 8 CHECKED BY S` DATE APPROVED BY DATE SDE OR MGR OF STAFF GROUP Y DISTRIBUTION REASON FOR REVISION'TOTAL .......... ............... .._....... - .......................................................... NUMBER OF SHEETS IN THIS ISSUE SHEETS REVISED. ADDED OR DELETED ..... - . . ...... . ...... . ... - - - - ........................................................... .......................................................... - PROBLEM STATEM��: 11 - - -�_1 r- ; _ _ _ _ _ . _ - e�v `5D _.._. o4. ............................................................. -•...............•-----......-•----.._.._................__._.............._ ...........................................................................-- ............................................................................ ............................................................................ SUMMARY CONCLUSIONS: i r . _ .... � e _ .-�s-w.�i � aT•1 O Vt � JV1�d . w. ; � _.�Gc�e:� �/..�q-✓t:s�e r ........ _ . . ...... �l. _ Dads .�j- ►�► -� .The. ..... �C G-2 ............................................................................. •......................................................................... •.............................._.........................._................. ............................................................................. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . l - - - - - - - - - - . . . . A03=1711 • • FCRm Salo REY 3m3 ' CALCULATION SET NO. CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2 (3 2 7,B-_ -� PRELIM. FIN VOID I REVISION 11� � PROJECT TITLE w GoeX� S4vv � rote-, l" DISCIPLINE �.o- O 2. 30 7 DESIGN BASIS: _______________________________ .._...�1101� 7 . I-!�:� 5�.............. ..................................... --- V4.— --- ..... .................... =-------. ---------------------------------------------------------------------------- ---------------------------------------------------------------------------- --------------------------------------------------------------------------- _.._ .._. --------- ---- UNVERIFIED ASSUMPTIONS/OPEN ITEMS: --------------------------------------------------------------------------- --------------------------------------•----------------..._....__.._...._._.. --------------------------------------------------------------------------- ............................................................................ ......................................................................:.... ........................................................................... ........................................................................... REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) ..................................................... --._..._-s`�. U.b �........................................ - ................... ...........I--- ............................................................................ ............................................................................ ............................................................................. ..................... COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) REV. NO. REV. DATE PROGRAM TYPE UE&C VERIFIED - ❑ YES ❑ NO ANALYSIS DESCRIPTION RUN NO. RESULT The attached computer output has been reviewed. the input data checked, and the results approved for rekww. INPUT CRITERIA BY DATE CHECKED BY DATE RUN BY DATE APPROVED BY DATE AO=0017R • 6,; rm 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. �3 Z 7000 _2 REV. COMP. BY 6DATE CHK'D. BY �— Constructors COMPUTATION SHEET PRELIM. FINAL VOID DATE,/t Q A S7 19 14 1 (GL Goos C r01 SHEET ! OF DATE DATE PROJECT YV SUBJECT-R Jo ??05Z Wl W -- f �g.spq 07. LlN ---.. V-204• �. 613 SSS=o" 1718 n �Mk � - 3 -77 216 8—/ 2 A B RS'414- 6 (ON) • o zLL 0. V Q Q A 14 /8-47 �----two 4-7- 9—B E ► S , r01 N W -- f �g.spq 07. LlN ---.. -- --.. - -- - - - ---- -- . . 3— 7 1718 n �Mk � - 3 -77 216 ,S�a,l7-T' V Form 5007 (Rev. 9/95) Raytheon Engineers & ' GENERAL CALCULATION SET NO. 13, ?-176 REV. COMP. BY CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID O �Q GDOse PROJECT .SHEET Z OF DATE DATE / 1 SUBJECT /�iC�OGe=SS lt� '^ l ��►- g, J.o. /770-S7,06/ Sic �oryl • I[] Form 5007 (Rev. 9/95) Ra0been Engineers & GENERAL CALCULATION SET NO. REV. COMP.BY CHK'D. BY Constructors COMPUTATION l 27 6-6 O - z - LU DA T SHEET PRELIM. FINAL_ VOID PROJECT &0C:6 e SHEET OF DATE. DATE SUBJECT /iC�OLC_SS �.�5 �i Py�'�+ J.O. Lo �S y -204- 1)L= 31K- Te s = 3qo o ,lls,y -40 K C) f ev-.aA ��� L 3 Z 2 'b9 sa- 3 3'� Sei svwiL :�oase sheat a , 3 �,ZS' �z.71� (3 3) Se, svr, c CC -r. 52-949/ 6:18� `` g, C,7 . .(3 lift 5e %'%.wv wovtA %as e 5�eav- !•/4" 1�/ � �► � base vY► �► e►-✓+ = 9• o k� DL.43-,3SK-/-./3k+,79K+6r/�4t.7?4 SK + 74K = 973K S-zy /dam Pt z 2)L.., 717 2SK+boz"` , 2S k-+ 6-1 X+ ?9" Form 5007 (Rev. 9/95) Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION 13 Z7 6-D0 — Z PRELIM. -FINAL VOID PATE 7 9 DTE /o SHEET. 1_t ] /�' (G PROJECT-YV 1 � oos e- J t SUBJECT SHEET OF DATE DAT E J.O. 770- 114 1• . .�1�i2 " CO Gil P $ G I ►'� 4 ' . �i / %�'� r �o t.� H d GL �1 O v�, - �� 3.3 /0 (9)'(2 M, l06.864) L gZ7.2 .�+- F,s,= 7-7, Z_ 2,57 So 0IL r. :7 • Form 5007 (Rev. 9/95) Rayfhean-Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION 132'7 Oa —Z SHEET PRELIM. FINAL VOID oa QAT 0 Ta PROJECT vv II A Go e SHEET OF DATE DATE SUBJECTJWCGSj'.�.if 6-J1LL �J-O- 555 j Toe jFveSs-aw = 2 0106 18)1 /� 8S KSS O1L .3 (ZA b) /.4.4KSF �eih DrG�9 _ Ma•{ �� = I�44�6•S�Z 1172S 5,47) (��.�� A4 S z 28" AS 176,31,1j I I I II " 194 Ks SZ) o,t Ar 17g 47"Af- i COMPRESS 5.60 I:\COIPRESS\STAPER\27665-1.VSL Kar. 2,1998 ` Wind Calculations ~ O4 -MeV- 2 -c)4 - Method thod of wind analysis: UBC 1994 •Elevation of base above grade: 0 -ft Increase" effective outer diameter: 2 ft Wind force coefficient Cq: 0.7 Basic wind speed,,V: 75 mph Importance 'factor, .Iw: 5 Exposure category: C ` Design Wind -Pressure •, . -Wind stagnation pressure qs = 16.4 f _ Hei ht Ce P = Ce*C *qs*Iw . P[•� ' (fit) (Psf� w i N D- c�►�c'S. 15.0 1.06 12.16 USING; x•15 ✓ 20.0 1.13 12,.97 25.0 1.19 13.66 30.0• 1.23 14.12 40.0 1.31 15.03 -60.0 1.43 16.41 .80.0 1.53 '17.56 .100.0 1.61 18.48 ;. 120.0 1.67' 19.17 v, 1160.0 - 1.79 20.54 - 200.0 1.87 21.46 300:.0 2.05 23.53 400.0 2.19 25.14 &tresses due. to Wind + pressure, Operating & Corroded ° Elevation Type Minimum Circ Reguired Overhead Bending above base compressive thickness joint thickness weight' moment (in.,) (psi) corroded eff . (in '(1 S) (lb -ft) 17500.0*1.2 87:2, (in.) E 1 17500.0*1.2 281.4 33.00 c 2.6250 .'1.00 0:9921 25736.4 6114.5 -0.00 skirt 1.0000 0:55" 0.0136 29949:4 8971.3 Kai, is - - Table Continues ,Continues Maximum Allowable' *Maximum Allowable Total wind tensile tensile .compress compressive Pressure stress/E• '.stress -stress,,, stress (psi). (psi) (psi) E=1 (psi) (psi) & other) .7686:2. 17500.0*1.2 87:2, 17500.0*1:2 2023.6 -321.2c 17500.0*1.2 281.4 17232.6*1.2 28.6 Wind def lection'.r"eport, operating & corroded Elevation Elastic Inertia Platform Total wind Deflection start Modulus wind & other (platform} section top above base ,shear. shear & other) (in..) psi x10^6 (T, ft^4) -(lbs) ►(lbs) (lb -ft) (in.) 33.00 28.6 4.507', 0.0 r 941.6 0.0 0.0006 0.00 28.6' 1.697 0.0.- 1136.0, 0.0 0.0000 COMPRESS 5.60 t I:\COMPRESS\STAPER\27665-1:VSL Wind Calculations Mar. 2, 1998' Elevation Type Minimum Circ Required Overhead Bending above base com ressive thickness joint thickness weight moment (in.) (psi) coded eff. (in�. ) (lbs) -ft) 17500.0*1.2 87.2 17500.0*1.2 0.0 -321.2c 17500.0*1.2 .(lb j3.00 cy1 2.6250 1.00 0.0109 25736.4 6114.5 .0.00 skirt• 1.0000 0.55 0.0136 299.49.4 8971.3 Table Continues Maximum Allowable Maximum Allowable Total wind tensile tensile compress com ressive Pressure stress/E stress stress s ress (psi) (psi) (psi) E=1 (psi) (psi) & other) -51.8c 17500.0*1.2 87.2 17500.0*1.2 0.0 -321.2c 17500.0*1.2 281.4 17232.6*1.2 29.0 Wind deflection report, empty corroded Elevation Elastic Inertia Platform Total wind Bending Deflection start Modulus thickness wind & other (platform section top above base . (psi) shear shear & other) (lb -ft) (in.) psi x10^6 (I, ft"4) (lbs) (lbs) (lb -ft) (in.) 33.00 29.0 4.507' 0.0 941.6 0.0 0.0005 0.00 29.0 1.697 0.0 1136.0 0.0 0.0000 Stresses due to Wind + Hydrotest pressure, New Elevation Type Minimum Circ Required Overhead Bending above base comressive thickness joint thickness weight moment (in.) (psi) (psi) eff. (in.) (lbs) (lb -ft) 38000.0*0.9 74.1 (in.) E -565.3c 17500:0*1.2 299.5 33.00 cy1 2.7500 1.00 26517.4 2019.4 0.00 skirt 1.0000 0.55 0.0144 38941.2 2962.9 Table Continues • 6.16.1997 Maximum Allowable Maximum Allowable Hydro tensile tensile compress comressive Pressure_ stress/E stress stress stress (psi) (psi) (psi) E=1 (psi) (psi) 40.8 38000.0*0.9 74.1 17500.0*1.2 .5.6 -565.3c 17500:0*1.2 299.5 17232.6*1.2 Page 10 COMPRESS 5..60 I:\COMPRESS\STAPER\27665-1.VSL Mar. 2, 1998 SKIRT BASE PLATE , Base configuration: External Chairs • Foundation stress: Sc= -1350 allowable psi Concrete ult..28 day strength: fc'= 3000 psi Anchor bolt material: SA -36 Anchor bolt.allowable stress: Sb-- 19100 psi Bolt circle: BC= 51.7.5 in Anchor bolt corrosion allowance: , 0.in Anchor bolt clearance: 0.125 in Base plate material: SA -516-70.., -Base plate allowable stress: Sp= 17500 psi 'Base plate inner. diameter: Di= 41..75 in Base -plate outer diameter: Do= 56.75 in Base plate thickness: tb= 2 in Gusset separation: w= 8 in Gusset height: h = 8 in Gusset thickness: tg= 0.75 in , Compression plate width: 5.5 in Compression plate thickness: tc= 2 in Estimated base ring weight: Wr= 656.8 lb Initial bolt. reload: 50 $ (9550 psi) Number of bolts: N, = 8_ .Boltsize & type: -1:7.5. -inch series 8 threads' Diameter of anchor bolt holes: db-- 1.875 in Pipe sleeve inner diameter: 2.624 in .Pipe—sleeve wall thickness: 0.438 in Calculate the load per anchor bolt •Governing vessel weight: W = 29949.4lb Governingoverturning moment: M = 52945.3.lb-ft Bolt rooarea (corroded): Ab-- 1.98 in^2 P=-W/N+4.8 *'M/ (N*BC) = -29949.4 8 + 48 * 52945.3 / (8*51.75) =•2394.911 b 1 Required area per.bolt = P / Sb 0.125388 `in^2 The anchor bolts are satisfactory. Foundation bearing stress (gMratingl Ac= pi*(DOA 2 - Di^2)/4 - N*pi*db^2/4 ' = pi*(56.75^2 —41.75^2)/4 - 8*pi*1.875^2/4 = 1138.337 in^2 Ic=:pi* Do^4 - Di^4 /64 = i* 56.75^4 - 41.75^4)/64 = 59994.9 in^4 - fc='N*Ab*PreLoad/Ac + W/Ac + 6*M*Do/Ic = 8*1.98*9550/1138.33 + 29949.4/1138.337 + 6*52945.3*56.75/359994.9 = 209.2766 psi As fc <= Sc.the base plate width is satisfactory. Foundation bearing stress, hydro test condition fc= N*Ab*PreLoad/Ac + W/Ac = 8*1.98*9550/1138.337 +38941.21/1138.337 + 6*2962.927*56.75/359994.9 • = 169.9 psi 6.16..1997 Page 11, COMPRESS 5.60 I:\COMPRESS\STAPER\27665-1.VSL Mar."2, 1998 SKIRT BASE PLATE ` As fc'<= Sc the baseplate width is satisfactory. Check the base plate for foundation bearing -load From Brownell- & Young, Table 10.3., 1/b .508 _ Mx'= .0312*209.2766*10.82218^2 = 764.724 ; My,=-.317*209.2766*5.5^2 ==2006.805 tr_= Sqr(6*Morax / Sp) Sgr(6*2006.805 / 17500) .8295 in The lase plate thickness is satisfactory. Check the compression plates for bolt load (Jawad & Farr eq 12.13) tcr= Sqr(3.91*F/(Sy*(2*b/w`w/(2*1)+8/�2*(2/w+1/(2*l) m ) / = Sgr(3.91*18909/(38000* 2*5.5 $ *3 - 1.875* 2,8+1 (2 3))))) = 1.004802 in The compression plates thickness is satisfactory. Check gusset plate thickness (Bednar chapter 4.3) Radius of gyration of gusset' , r = .289*tg. ' _ ..289*0.75 .21675 in Cross sectional area of one gusset • Ag= ' tg* (b - 25 ) 0.75*(5;5 - .25) =•3.9375 in^2 ' Gusset allowable stress (steel) Sa= 17000 -:485* h / r) ^ 2 =.17000 - .485*�8 / 0.21675) ^_2 = 16339.3 psi Y Gusset axial stress due to.bolt load:'r } Sg= 189092/*(2g* 3.9375) , 2401.143, psi The gusset plate thickness is satisfactory. Check skirt for bolt reaction (Brownell &Young eg. 10.591 t = 1.76* F*1/(Mb*hc*Ss))^(2/3) * (ODs/2 (1/3) 1.76*2394.911*3/(20*12*26250))^(2/3JA * (45.75/2)^(1/3) .5.453555E-02 in The skirt thickness is satisfactory. Y Page 12 2 - COMPRESS 5..60 I:.\COMPRESS\STAPER\27665-1:VSL Mar. -2, 1998 . Seismic Calculations Method of .seismic analysis: UBC 1994SSE TZE-RUN •Seismic zone: Importance factor, I: �.2 5 E `S M 0, G 1 � S Soil profile: • $ Site coefficient, St, •5 S2 Coefficient• Rw: 4 Period of vibration calculation The fundamental period of vibration is calculated using the Rayleigh method of approximation by the numerical integration .of the following. formulae: T. = 2*Pi*Sqr[ Sum W*y^2 / g(Sum W*y) ] 2 (I, = . �• D T operating) = .029 seconds Tfempty) = .028 seconds Seismic zone factor, table 16-I: ,Z = 0.3 C = lesser of 2.75 or the following: (2,75) 1.25*(S/T^(2/3)) = 1.25*1.5/0.029^(2/3) = 19.864 Ratio C/Rw: use larger of 0.4 or 2.75/4 (0.688) .,V = Z*I*(C/Rw)*W ' = 0.3*1*(0.688)*29949.4 6181.557 lb T <= 0.7 seconds so Ft 0 0, �2 2 ase shear distribution Fx (V-Ft)*Wx*hx/(Sum wi*hi) Elevation. Type above base (in.) w1 (lbm) . hi (ft) w3*h1 ( lb -ft) F1 (lbf ) Vx V(other) (lbf ) ( lbf ) 33.00 Cyt 0.00 skirt 25736.4 4213.0 8.75 1.37 225193.5 5792.8 6026.5 155.0 6026.5 0.0 6181.5 0.0 E=1 (psi) 29949.4 230986.4 17500.0*1.2 17500.0*1.2 174.0 Stresses due to Earthquake + pressure Operating Corroded 17232.6*1.2 Elevation. Type above base (in.) Minimum thickness corroded (in.) Circ joint eff. E Reguire thickness (in.) Overhead weight (lbs) Bending moment (lb -ft) 33.00 Cyt 0.00 skirt 2.6250 1.0000 1.00 0.55 1.0029 0.0298 25736.4 29949.4 36159.1 52945.3 E=1 (psi) Table Continues is Maximum tensile Allowable tensile Maximum Allowable stress/E stress compress stress compressive stress Pressure (psi) (Psi) (Psi) E=1 (psi) (Psi) •7773.1 424.2 17500.0*1.2 17500.0*1.2 174.0 17500.0*1.2. 2023.6 616.9 17232.6*1.2 6.16.1997 Page 13 COMPRESS�5.60I:\COMPRESS\STAPER\27665-1.VSL Kar. 2,'1998 Seismic Calculations WeiI I ( I I I sm'c shear re rt gjnrajinct& corroded Elevation Elastic Inertia Seismic Bending start Modulus above base & other. (platform above base thickness 'Ratio C/Rw: use larger of --0.4 or shear & other) (in.) • psi x10^6 (I, ft^4) (lbs) (lb -ft) 33.00 28.6 4.507 6026.5 0.0 0.00 .-28.6 1.697 6181.5 0.0 6,.2' -- Seismic zone factor, table 16-I: 'Z = 0.3 Circ 'Reguired C = lesser of 2.75 or the following: Overhead (2:75) above base .1.25*(S/T^(2/3)) = 1.25*1.5/0.028"(2/3) =.20.334 joint thickness 'Ratio C/Rw: use larger of --0.4 or 2.75/4 (0.688) (psi) V = Z*I*(C/Rw)*W , eff. (in.)." (lbs) k = 0.3*1*(0.688)*29949.4 17500.0*1.2 174..0: 17500.0*1..2 = 6181.557 lb 424.2 17500.0*1.2 616.9 T <= 0.7 seconds so Ft = 0 cy1' 2.6250 - Base shear distribution 25736.4` 36159.1 0.00 Fx = (V-Ft)*Wx*hx/(Sum wi*hi) 1.0000 0.55 0.0298- • wi i w1*hi: 52945.3 other . Fi Vx V (lbm) (ft) (lb -ft) (lbf).- (lbf) (lbf) 25736.4 8.75 225193.5 6026.5 0.0 4213.0 1:37 5792.8 155.0 1.6026.5 6181.5.. 0.0 29949.4 230986.4 Stresses due to Earthquake. Empty & Corroded Elevation Type Minimum Circ 'Reguired Overhead Bending above base com ressive thickness joint thickness weight moment (in.) (psi) corroded eff. (in.)." (lbs) (lb -ft) 17500.0*1.2 174..0: 17500.0*1..2 0..0 424.2 17500.0*1.2 616.9 '33.00 cy1' 2.6250 1.00 0.0217 25736.4` 36159.1 0.00 skirt 1.0000 0.55 0.0298- 29949.4 52945.3 Table Continues aWispic shear report, empty & corroded Maximum Allowable, Maximum Allowable tensile tensile compress com ressive Pressure stress/E' -stress stress sr -press, (psi) (psi) (psi) E=1 (psi) (psi) 34.9. 17500.0*1.2 174..0: 17500.0*1..2 0..0 424.2 17500.0*1.2 616.9 17232.6*1.2 6.16.1997 Page 14 Kf-t- Elevation Elastic Inertia Seismic Bending start Modulus & other (platform above base shear , & other) (in.) psi x10^6 (I, ft^4) (lbs). (lb -ft). 33.00 29.0 4.507 6026.5 0.0 0.00 29.0 1.697 6181.5 .0.0 6.2'- 66Kfl� N25Z�7S7 �O'�. 1-3 IZf�� /67Y -LL „ 1!38 N2 Z -7C-2 alp MZc (tiJ�Clor�, -Z 4 77A/rJ 4CO-7 oil . "F L1,lJC— i i ' Irv - I 14E 3 ;�jrLL Vy Et. f,q=o" T,D. �I cl y ' .� 1 pv :/33 - �1✓G3 � ly f�-t, — - pIT- ,cam 01 F( 2—� H (Gl 'ii Pe Sloe j � orl I ) Zo1VC4., i 20 . V 2 ® PERRy EQUIPMENT CORPORATION P_O. Box 640 R. Wo4m IndwniAl PARk MiNMAJ WIEUS, Toys 76068 FAX (940) 325-4622 C�C� TEL: (940) 325.2575 TO Sent By:C ��2y Date: To:.�e/f-.3%.813-3622 t{-rykasi wit- I 60 S c From:_ Edo' M tu_- HJT 3 2 2g q 0� ¢S. p (7 2 7 5 7 W I )v l' i S t,; 10, Fa1M 5010 REV 3M3 Unifed Eng1neers CALCULATION SET NO. CConsirCALCULATION SUMMARY f 348 &o 0-4- A11111'"""mC-P" & CONTROL SHEET Page 1 of 2 PRELIM. FINAL„ � VOID REVISION PROJECT TITLE W ; 14 Goose S+o i -a a -Fa DISCIPLINE J.o. STRUCTURE OR SYSTEM -51�e Fr4.w,. -e DESIGN CLASSIFICATION ' SUBJECT A-cCeSS t� I4t.r—s 4 v, V - V -26 - COMPLETED BY fS DATE CHECKED BY DATE APPROVED BY 1/�� - DATE SOE OR MGR OF STAFF GROUP DISTRIBUTION REASON FOR REVISION: • • . _ _ .... - - .......................................................... TOTAL NUMBER OF SHEETS IN THIS ISSUE SHEETS REVISED. ADDED OR DELETED ............................................... ..---" .......................................................... ........................................................... PROBLEM STATEMENT r t 11 F ..... '�e5� " fP.�.Gt.,1,�g1" ppip + f .. b braceci..S a.4�._rgr,+�5.•"....."-"-"--""-------""---"--"--- .......-"""-...----""-""""-........""---...." ............................... -""-"-------"-..""........."-""............................................. ............................................................................ ........."..."............."-""--......"..."................................ _ SUMMARY CONCLUSIONS: 1 GG�L ..... Q.. P.�.�} ror'►s ..� �s'� ..e .1.... r � .5,=�. l l�?a v► s` �r - - TO. . ........-"--".................................................... ...... ................................................ .............."......."..................................................... ............................................................................ .................................................................... ............................................................................ ........... ......... ,1WY0017/t • • • FORM 5610 REV. 3100 CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2 11 PROJECT TITLE i ��. �.o-oSc +Or FGZ4. 1, CALCULATION SET NO. PRELIM. I FINAL I VOID REVISION DISCIPLINE rK L u 2.0.E.Z. DD DESIGN BASIS: ..' -�'?1,.t ...:11rran.!'N_.+r►:. .dwSS ----•---- -------------.........--------- ....._....r�ra-'1..��5...C'r�rv�.4-------------------........... --------------------------------.--------............--------------........... ............................................................................ ............................................................................. UNVERIFIED ASSUMPTIONS/OPEN ITEMS: ---------------------------------------------------------------------------- ------------------------------------------------------------------------•-- ............................................................................ ............................................................................ ............................................................................. ................................. -............................................. ..........................................•--........---•--.................. REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) ...........j C.......: ...-'........................................ ............ ..... LSC_ ... _ t ..................................... ............ ; !Y► _Gtrt!._ e.k►'......---•-•............... ............................................................................ ............................................................................. ...........................•----.............................------......... ..................................:............................:............ COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) REV. NO. REV. DATE PROGRAM TYPE UE&C VERIFIED ❑ YES ❑ NO ANALYSIS DESCRIPTION RUN NO. RESULT The attached computer output has been reviewed. the input data checked, and the results approved for release. INPUT CRITERIA BY DATE CHECKED BY RUN BY DATE APPROVED BY DATE DATE Form 5007 (Rev. 9/95) Raytheon Engineers & GENERALS CALCULATION SET NO. REV. COMP. BY C D BY Constructors COMPUTATION 13 S��—'¢ F SHEET PRELIM. FINAL VOID DA E DTE •4 � 2-1 X18 /o PROJECT +,f SHEET OF DATE DATE SUBJECT 1V —ZQ4 AC"fSS PI G,` -Fo�►vl J.O. '70S0, 60/ Sid, N,Tz.K► ,5 BN' 41 0IiVK + Ln s ao V1 Cj,I;Iol �, V Sfd, Ladder AS/, 68-C)14 TO. C, _� �b�. a � 5�►-,�,9 .. r bare .. a 4" a10" r� 1-z3'A.1 -_ lq- loe x 111 v � FA-/ v V Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION /-? aw 7,0( FG, X PRELIM. FINAL VOID 6 ATE DATE SHEET 8 � PROJECT \ (` a Goose SHEETl OF DATE DATE SUBJECT V _ i4 Arzes:� I14�+fd" J.O. ! 704-2, 001 / L ,n u r� • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. Constructors COMPUTATION 1,348 ©60 le - SHEET PRELIM. FINAL. VOID PROJECT 1�l l' acs 4e -SHEET OF SUBJECT )!L_?� 4 -AO -'e -S3 �l fiov"A J.O. 7705 Ze 00/ REV.CQ�Q� BY CHK'D. BY ATE TE DATE -DATE La a -A P'":r e L4x4x3s 300d -fov Is,2" w/Xb z 15.2" plat -coca -Bea w%M�, = . x(z• s)<12>Z�sKft- --+'i'usc C8x1/�,5-"500 �vr 12.gSK4 �L��era.l Scitly{iL • ' 74. DL L S?D . //!/ SOS 76+10,1 Loa,� = 132.8 24 7$ seisvt��C ZS)( W z Z6 1/�l • 0 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET W i lJ GB�---, CALCULATION SET NO. Zlf8 O - REV. COMP. BY CHK'D. BY PRELIM. FINAL,. VOID 1,T Qo O/ PROJECT /��—JO- SUBJECT V -Zo4 ess P[4 T4'" SHEET !f OF DATE DATE, r7 Mei iy>h (Ge, -told ) A►�Q ; -PI a1 t o w..� = 2+ (/, 33) 33/0)o� 33-24 t Og'S-V --- 28. 3 S ° 8 6.4,2 a' W -nA Loyd = 12..3 pJ A6)(86Ar) _ 1, 9y Q-hckvv 5alLoa4= % (1oI) z l•9 x7- b s ear 3 K s%eQ ►- D k,.. .� Q9�,r,a.� brace load t- /-o 2 �s) —mouse .l.—L 3 x3x4 bpac e 9 co oy �. % K 4 �t//A /4Z < /�� L. /6% .45K UBC 2Zl I.9, Z. I. p 1T 4 I), 1411 6 K 7,75(r2.) //7 < A7 oK • 0 - 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. Constructors COMPUTATION SHEET. PRELIM. FINAL VOID REV. I COMP. BYCHS PROJECTyN i �d G�BSe. y f SHEET `5 OF DATE SUBJECT V —,z04 -p1 4 ToV�vI � �J_O? 70EZ&0/ Fq P4 I.yu, TES 07 P1T 1 S S36064) 46 3a, Load = IZ�3 1-D4' sa� �•!K �kl,�►a U�(�¢-t = l.i �t� � . SI K Sl��a�L P55'� DATE ,v--S�- o �- Fo I- O�T, M, • M , =%/..3,5 + .28�, 6$ ; sl)(l•s) In a F, S, 2.54 > !. S a tc �. S8 2.6�$ S of 1 pressure KS. 4,IL reSs%.Ve- "IS Very 6K-40 use *�S@ /Z" o p i -e v -LAS C 4- jt S' V Ld� "� 4 Raytheon Engineers & - GENERAL CALCULATION SET NO. e:�04V . REV. COMP. BY CHK'D. BY Constructors COMPUTATION ATE DATE SHEET PRELIM. FINIAL VOID /4¢ 98 w' I DDS e �// PROJECT `' T-� �^ -Zb4 Cil 4A Tor tit E4J SHEET OF DATE DATE -7 SUBJECT' Y !1 J.O. / 0-5;2- 00/ rl f / N b } 4 -Ats 1.ev -4 7-1'e- q) Q JAS yI Np S" O - • Form 5007 (Rev. 9/95) Ravibe®n Engineers & GENERAL CALCULATION SET NO. 4700 "¢ . REV. COMP. BY FJ' CHK'D. BY 44-' Constructors COMPUTATION SHEET PRELIM. FINAL VOID S -DATE QQ �TE 17OF PROJECT SUBJECT V ^ ZO S SHEET J -0 -770 -CZ -001 DATE DATE N y Ll IMP FSI.! 03 L c,,vri,s I J1 'o — LaAAer J►l +o BnT�- oT 8�r�ti,. er 9 ba.r e of � ca ca tK L v A �i a • • Form 5007 (Rev. 9/95) Ra*heo 1 Engineers & GENERAL Constructors COMPUTATION SHEET Willa G 0OS e CALCULATION SET NO. o" REV. COMP" BY � CHK'D. BY 4.6 PRELIM. FINAL, VOID / D ATE G PROJECT SUBJECT -)1-2-0.9 SHEET 8 OF DATE DATE J -O. 770Sz«001 V— ZD S -PtaL�r►.,, ;. OL = +e e-1 2SrPic .5 V11 - S j2s psf iso,Ps�' -P6St Low /sem (6).�4)�4 = 0 9 K L 4x4x3f, 6 _ 14. �6 s a bt�1�4 . Pl at 'OV --A2 &4111I`�,,,, c . is �) i6%�S =- 1, 3 S eft Cols. b VA e -►`-5 La.�e� Se►sr,•►-i c = . ZSr�.OZS�iZ4� -f 1. l:K� _ . 4.8 4:`�,sw�a:t� Nis, �0,��4 �. ►2.3 S,¢!(►.�� a.1 Wyk,:1 ee- .1�► _ (�. iso/4 _.., q. 14J4e-. bo ��- Load = ,1.��z� 4t'.z l,S''.7} .s'`shPAr --r U S e 3f 3 6 bO o 0 ,SI0 r L1�13, aat y LAS C L 3x3x 4 bv'uc-p- g and �o 1r 4. o "� C, A-IJ1 Q = $' 86 -z)/, = l6 z 4 16 - d K UBC .7L/1�9,2, j ZL" $ase