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� (9. . .y . L . » . . . � � ,■ . Wild Goose Storage Project Raytheon Engineers &: 77052001 Constructors -� Table of Contents Temporary Compressor Installation Building Permit.Documents - Calculations Temporary Compressor Building Framing Piperack Framing......................................................................................Section 1 Temporary Compressor Building Foundations Pig Launcher Foundations Pig Receiver Foundations Piperack Foundations Pipe Sleeper Foundations........................................................................Section 2 • • INDEX . STRUCTURAL CALCULATIONS WILD,GOOSE PROJECT (77052.001) TEMPORARY COMPRESSOR BUILDING AND PIPERACK FILE NO BOOK NO. DESCRIPTION FINAL PAGES DATE DESIGN CHK'D CALCS :..:.:.:...:.:.:.:.:.::. A. RS.:1...,.:.::.1 98:..::.:.:.:.:.:.:.:.:.:.:.F..:..�.:..:.:..:..:..::..:.:.:.:.:.:.:..:...: .:.:. 0:::::::::;:::: .........................................................................................................................................................'�..��..........M..f�R�lf�.�.1.,..1913...........��T................6R�....... --------:::::.. ;..:.:.:.:... :.:.:.:.:..:.:.:.:. ; ...:.:.:.: WILD GOOSE GAS STORAGE PROJECT STRUCTURAL CALCULATIONS BOOK 1 77052.001 Q��QROfESS/pl,9l .y, Fyc 2 2 L t 3 898 sT Civic 9lF pf CA xi Page 1 • FCRM 5610 REV. 3M Untf, ed C-ngineers CALCULATION SET No. $ construAws CALCULATION SUMMARY 3 4"? D 00 — Z "''""°""'"°'" & CONTROL SHEET PRELIM. FINAL V010 REVISION Page 1 of 2 PROJECT TITLE (1 1 Goose-. 40 V e- �6a c I V%4 DISCIPLINE J le -LA L u, Vi", J.0.'770 -S2, 00 STRUCTURE OR SYSTEM; a ; Ft -awe 11!� DESIGN CLASSIFICATION SUBJECT T,- vv% A Vy (LAO►�-� p V FS SdV' k i (� l Yt ct • COMPLETED BY �►'�b �ri �°Sf DATE 2/2715 5 CHECKED BY ;- P? ,'i -�/�=..c />: : ^�Avzrwovv/'f ATE APPROVED BY BY 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 1n Ok :.. •1 _ ...................... 0 u.s e...�" e.. T e w► o ►�a `,�l .. Cc?w► I��sS o r.S _ _ . ��;e�...._._ .....t-rs�. -�o...��:.��:-.b.e. •cam .L.e.��.� ..�nclb�ec�.. .:-} fie. Tev►1 arQ� �o�-y►. I� sS yrs_ awe.. raw, aveci............. ........................................................................... ............................................................................ ............................................................................ SUMMARY CONCLUSION _ rr . r _ - - - . -Gid' ........................................................... .........................................•---.........................----- ..............................................._................---•--..•--- ............................................................................ .......................................................................---- ............................................................................ ......................................................................._..... ............................................................................ A039W 1111 • • • id1M $eto REV. 3190 CALCULATION SUMMARY & CONTROL SHEET & Page 2 of 2 PROJECT TITLE W I j GO ost ora Fa �� CALCULATION SET NO. 7 6 pb _ 2- PRELIM. FINAL I VOID I REVISION I 4-1 LA ?NE S Z O O °o DESIGN BASIS:. _ ...... _ . d.wz..............•-.._... ............ ..._.. ...........S.IY!.�CP�,q - - - • - ......... ..................................•--------...--•------------.._..---....-- ......_....•-----------............................•--••-----........._..... ............................................................................ UNVERIFIED ASSUMPTIONS/OPEN ITEMS: --------------•-------------•------•-----....--...------.._.._..---......... ......-•-•------------••--------------------------------------------------- ----•-•-•.............•----....•-•-••••••--------•-•------•-•---.........-- -----•...................••-----••-•....._........------..... ..........•-... -- ............................................................................. ........................••--•-••---....._._......--••--........._........... ...............................................•••..........._............_. REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA. FSAR, ETC.) ..........g.¢ .4 6 ..;.:.................................................. .........�...:rs.A.s .. ................................... ..........i �H �rru,N.�c !'�^.�!'� . �!�_ 5 ... ................................. . ............................................................................ .............. .............. ................................................ ........•..............•--•-•-•-----..........----•.....--.................. .................................................0............0............ ............................................................................ COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) S 3 REV. NO. 2 1, 0 REV. DATE PROGRAM TYPE 3-D;._Struc�u►-aI 46,lysis f ms`s►9h UE&C VERIFIED ❑YES ❑NO ANALYSIS DESCRIPTION RUN NO. RESULT TtCOB LDG B 1 . tS 5 a e w h o ov evs nesse m P --16&r The attached computer output has been reviewed. the input data checked. and the results approved for release. INPUT CRITERIA BY7°j'l�j —NOW S e! N DATE � iCHECKED BY.4ruor✓l 7 Wvc-c%E fe RUN SY F CSt DATE 2 APPROVED BY DATE Au,wo,.ri �-V. rev, 3 2/!819$ 7 70 2. a 0) V -Z Ffr \^);IeJ Goose .5400�vaje ley-- 1•�l1I1�i Gvose TG w� v rG l . trvv� C -L4 /o o`' 261-O" G.L, 13 �? /L ---- - 7 WIZ�c4ow C'10x;15,3 W12x4�wLloxl w 61OxIS.3. 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FINAL VOID AT - DA. /. PROJECT ► O bS E SHEET OF DATE DATE. p SUBJECTw 1D. �trw1 fOYess'o JO 7 b�"Zr OO�' y SIAr Z„ �N I � nAll J s L. 3l2µ ;6 _ S 2 .Tt %A f �01s , 73-� B- 0vi ' 1y 4;;1- 1r" 7F a f 419 Cela, • 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION oao -Z FG 5h'c PRELIM. FINAL VOID AT DATE SHEET 3-1-95 PROJECT W ► (� �0 -0S e SHEET f7 OF DATE DATE SUBJECTTeMp 5fa-+-V►10►-PSScV- J.O. 7 //� OS2,6O/ i I . 2-13,o ConkCon 0, -Lot, W/o l / t — LS h o l Sly vw K 1 4 i 4 2—L 9-X.3 z U 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D: BY Constructors COMPUTATION _LDATE SHEET PRELIM. FINAL VOID DATE, PROJECT W I� C�iDOS� SHEET 6 OF_716 DATE DATE SUBJECT I �1D. �aw►� ►�esfor f�j� Gam— J.O. % / �SOZ.U�� 3 W!2 WT S, 3a�� 74- Z _ \4 100 0 PC,kl7 Q-fi(- , .. 4 W ; Ali " / �ry p Tg"S F19 . �4T yP' 4 cs s ec4, o vA ,4-/4 a Nab • • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. REV 009 - L PRELIM. I FINAL I VOID PROJECT W GO 0S +e SHEET OF SUBJECT�C' �6 Y✓1 Y2SC (� J.O. / rJOSZ OO� 28�� —01- 4 �z N IAjIZZZZ e.Ia; t "SH 7 2-io I� fo vi vi. W_I6Web CHK'D. BY DATE DATE I DATE 16 iz 5(I Tt s x 3 fehPa+ baCk of Web 'f"o ISO' 64ove well,'" Form 5007 (Rev. 9/95), Ra Meon Engineers & GENERAL Constrictors COMPUTATION SHEET I Oys CALCULATION SET NO. / 0,06 - L . • REV. COMP. BY FZ-6 CHK'D. BY -==A o PRELIM. FINAL VOID ' I AT 1, Iqf3 DATE PROJECT - SUBJECT�E'V" VI.CO V y, SHEET O OF DATE DATE J.O. Sp1�C-e 17k/P 2 -PIC -S) ' 0 ly M -- M _N 21- lx 1 N / l -Ea, S;�l� a wcb: 48-8 f�325 Bo��s 24 - 4 L D e fa.; / 1 �J U Form 5007 (Rev. 9/95) AaWheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D: BY Constructors COMPUTATION If100 -ZT. - _., PRELIM. FINAL VOID AT DATE SHEET PROJECT `�" (� �eol SHEET OF DATE DATE / l SUBJECT ewv Cc�n VPS.S o J.O. 'J / 0,! Z, 'O� . K cab. 2I FY = , 89 " pl z l J 6 o-�J+ c7 1 F F m 14 o +T4 4f a-4 eYet La 4 M . N t` 4 p�441 . CTyP- • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION 13 700 -1"` SHEET PRELIM. FINAL VOID D b 3 DATE. �. PROJECT Y�' I l_.1 00S'e . SHEET /2 OF ! DATE DATE - Su PT CVA. p- COM -CSS or B J.O. ?'10�G. DCOI 9- 604 conk. C\I M 6"4 3 OCA 51^oWh —Q- bbl+coKh 0 Lj C7 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO., REV. COMP, BYCHK'D. BY Constructors COMPUTATION "" D SHEET PRELIM. FINAL VOID AT o DATE PROJECT VV ` 0-cqft SHEET 2 OF _ SUBJECT76'*v iQ' �Lt-MV eSSOY �B►A�. J.O. %?OS72.00� LASe W Idyc ZZ DATE I DATE /V o ; L oar1 Its e, Sig, C� �� � �o n vLt Or ciel�t �eCl �J1�iLGt 1�►� C Ovt Vt., . W ; �►d Co I , s 2'7 2 3 I .3 Z (W &k 18) o�� �SD p4-91 &L-li I Y m Iz-�I 4" Iii 2 N 0 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY ��:., Constructors COMPUTATION DDD - L F6 _ PRELIM. FINAL VOID AT n DATE SHEET 2 '3 97 PROJECT `�� I .I � SHEET OF DATE DATE SUBJECTTemiO� PYr J-0-7 0 92'. 00/ `I �is SIOe $.i►M.��Ccy 4o -ar.sAe F Cow 'I, s hb� sown 3 1, Tt vW ,i SN 3 WIZ 11 TA :. 4—D6 ►kV1I sec,. i 0-y, � N D 5h0 ul • ;• Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. 7 One ` z REV. COMP. BY CHK'D. BY PRELIM. FINAL VOID AT DATE W; I J Goose PROJECT SUBJECTTBL►� �ovw r. SHEET" OF JS DATE DATE J.O. 77OS2, O© / 4; ;1,? N IZ 7-S 6146 ., ! C 96 Y/s o n a i � 1 Z.�X��X circ) o M .N 00 q-bmlt coffin. I of 3?- • • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET PROJECT►N `� OdS2 CALCULATION SET NO. %DO 0 - Z REV. COMP. BY CHK'D. BY PRELIM. FINAL VOID I DATE 8 GE, SHEET l / � OF ' _ - SUBJECTT&M ,0 (:� OW V"SSOV DATE DATE J.O. 77V.9lo2. 001 Se 1 SrC! s%t I . o d evdopeJ �or - -Ae Vhw,i Ij bl : g, LA;f 1 I a ISO app y (� cryvv.?"S-so Y- $ l -A9 0 talcs, by A i.T +0; %k e T-pM poV-A VY Ref, — i Y' pu r � Ca GS . �l 14cr Q e v- el o D -4 G% 4s �/eya7io.' z 710- 1210 7-o " G -Z G-1 � W/4. . �) _ z4: 6Psi 6 . s(3s�(24. 1-10 ►-� . i 3 S.S�24.6) . 13S K/fit- 7 ou.96 z! �� .96 7'04 �fv.ra►.C� 2,7S ( -24.6)= . 06 �K� t 3s'`/f135 �iF SIX ►�,o x = . 14.1 K ft- ` l -11hill 1068�y{� 111 H 11 26-p Ll 2 �1 K 3Ilt Ifo 11 r� U 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL, CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION ODD - Z r g DATE E SHEET PRELIM. FINAL VOID &6/9gj/�O%g PROJECT WI l C21 o"Bf e SHEET ' OF 7 DATE DATE SUBJECT G►�✓►- G retro J.O. ?7,0197 Ld�+ 2 Ts 1 ¢ zo�,p,� My 9L e.S.5-Kf4 MY 13, 3 z 4f , o7s�'��-K � D7s'Y�t j ,64841 �tII `% L 1 C. L 1. 7�/D 2:2 /y�Dh Z, �N7 w 04 f� 14 A. 6 � r7.29 X 23.Z Z'b (4.9 i) �b � mS� ►z> � /,��ksi �b 27 >Ls 1 Fb X Fb Y %� 4�3 'Z'7 -----;p I,1 se. W/ D x Z Z (J'L 6 .a (v4, /.) z , /4 9 "/4 -'� �/�X /S � qdo� �b ►- /7 OK�f- b Opw use c/oX y 4011"nP4V'is°". %'j-( 3A /9g n u • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET �`� Goose CALCULATION SET NO. REV. COMPP, BY CHK'D. BY PRELIM. FINAL VOID DATE TE PROJECT �• SUBJECT `�%ewtP. �o►+��yesSDr Lc�q. SHEET l 8 OF DATE DATE J.O.• /%DSZ�DOI G -z S + 2 d 7S p My G 8—S"=.I�67s)(0,67)Z= o S%Kit 75 )`/f � L l( l L L L L- L l- LL t V C. 4 6'I Co r rl e Y T o rt c O KTt�v a-{�� ,�,a ,oQa = ►,��C�.S C14,S)(9,$) = 1q3 If 143 S . �b Z. ,vizi t 6 zL �` 5 S7 lr Z� 7. Ks a Eby Z7 K s G ec.�C w l D k l 12��2.1�} - 3. 2OKsc Z,K$�� %., 1, 7 3 + 3. Z� _ ��4 z > — — b use Z [7 0 Form 5007( Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION SHEET 12,41, loo- L r 4�,7- PRELIM. FINAL . VOID I DATE 6 ID�iTa/ 12 PROJECT W `G� O'OS e ► SUBJECT7F&-►'h 1p. CC -VY 9y05S8V' -5(�9. OF SHEE/T7 -I Q J.O. / %.S2.6)01 DATE DATE G-3 2z) p4l �• h� is _ �, (�,Z���q.s�1�.2s� _ 130 p l� M x . 13 O (!aVa = 6 3 Tr W !OXIS , . L 3 (z) 13.E 1,gz'`s` x � r `rbx = /eoo ��(9.zs� = /0,$KSt; 4 bq- �7 Esc /• 4Z t 8.61 e 45 � 1, 3 � b IL z7 u 5 e ►oJ x S' My = , os3��zs)(6.'7S)Z . 48 Kir �. L14A I corner �nrce mw+warn -I BC. ¢'b k Z) 3 , $ - 3,2) K s c Lx Z �3.S(9.zs) - 8.00` 4 .= .-148(►z�/,qs = 3.97Ks j ay = z� aKs� 3? .1 ,+ 3.97 _ . SS e- Y- us.e W f x /s'' • n 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION. SET NO. REV. COMPP, BY, CHK'D. BY Constructors COMPUTATION' Ofl� "l �� 4G?" TE SHEET PRELIM. FINAL PROJECT�''y J IJ G aos a SHEET �� OF ' DATE DATE SUBJECT'' P -"q -p. < oOVl d veS O V' J.o. 77 6S Z. 601. W eS� � ` E' V Gni I / eYl . • • W� ,d lsal = /,190,5)(14.5 -LA-2a Cdrvler 4,0rea 0--..i%AjAn � (2 10yS Tvy W I o x Z z. i q- Zr (J -i 23.Z- 7, 3 4- X Ebx /oeo/z b <4.41j by 1,3r-(lZ-)J3.9? - 4.Lp K j Fey Z7Ks� vp uS e X Z Z r a 3�ii Al • U • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION 1 O • Z SHEET PRELIM. FINAL VOID' , DA 9 S / PROJECT 1N 1 I �T 0 as 2- SHEET 2') _ OF . DATE DATE SUBJECTTe''►'1 �, �cr►'vlrirPSSar, Pu. Pa.e� C)Aj -1-PLA r-1 M S �L s f" 2S %S I f 10 4-d - S (2O'�1,— Rn� S sc- 5l) z zs � l�' C. g y p 2 34 IL 13cbN /3�0" Rm 3 ASS u w. ;,6-9 `f w (1 `0 o ►- . 1 Qti►�l. V O o ln� X11 aX /? is 900 or 3z.5 '` w/ K11 1a�• su.�, W*.K� su�-�� w► _ /.23 (/4, SO 01 lI.SPI load,z !/� ��-�8 1�'_� :4 7 IT.'oL,,Twa.v'd. M� .0 47(26 2 P8 z j.9p8 Kf� c / fcS c r -b X z Loco 6 '7 64) L S.b-3 p K 3iy�y� r� Lj Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D!BY Constructors COMPUTATION '� SHEET PRELIM. FINAL VOID I ��E D/ PROJECT—. `N i ` C� O 05 ^p ' SHEET 22- OF DATE DATE SUBJECT—F—", �O-1 i�v"SsbY Df � J.O: i45S�-.�-,, a BPa-►,., Ta.� es �er'�i col J OQ�S �c1 Ue✓7�, root" IDG_ = 6,5�3��s�) +-6� _ �88.�1� `/erl, 5 1-oc� �oAci=C9;060�i+ 201 8,b'76 1).C19 PO .3cawn M _ 4 2 .q II I ILS LL,tkItI L)j L1. l 1Zx40 Lo ID S;-,3 W I2x 40 9 ood `Fc Y- S7 v- — 4.-2.,q r --H- C 10 X IS, 3 4, axf 9 31 r-'4 0 a • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. Constructors COMPUTATION 12,670ao -1 SHEET PRELIM. I FINAL I VOID PROJECT W1 ( �UUS e SHEET 23 OF - SUBJECT(!-K,tb. CovviprPSsoy- B��a, J.O. 77652. Ddb REV. COMP. BY CHW BY FG DATE T DATE I DATE =H40.J LA0.Q5 foo ,�5 = pops¢ 1sPs� rl;sc, Lcac� t S ps'� Tr b wcc 41, S -O" 921 s� L; es C ;EeacTi'oT L A� z) 63+2;s1 Kl K/fV) L /.SS K 5 i J tSo-5. tcJr--[3,S( 4ps6 q./7ll.ZS)(6 ,?7s��i4)yz - /-01 Faye Sf►75 S d'11�� G► �%s ) 4 psi 206 P 1, - P .4f 1 10Sp - 9=.219.6(.-) _ -- /,03'1 1�F;�d"Col, 0?1 i ,,t ASSume U►�.�� c.a�ls..- lL> A? f 1y 3141 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. _ REV.- COMRBY CHK'D. BY Constructors COMPUTATION -3 74no L D T� SHEET PRELIM. FINAL VOID 3d 8 Z G / PROJECT W+ IJ Go -ore n , 1 SHEET 24 QF DATE DATE SUBJECT�E'm-rp, �QYy1bYPSSOY C��da. J.O. '�7bSZ.D�/ LvIz �K- Pu►-�,'�K' 1, 10' b^ y 2J S (s�(�) o s'4 6- v- P5 ?13 098 r_ 20(3)(S) _ 03nK -2eQ.cTr'v�-► @ Eh c� �ay S = �I 3+ I, (�.Z���,C� 5 • Z4 2 f (4, P 30�09� r< 0 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP, BY CHK'D. BY Constructors COMPUTATION 4(7 DAT SHEET PRELIM. I FIN 11307 'E,, 9A 2 //- 147, PROJECT SHEET ZS OF7 SUBJECT i.o. 4 wl�ujov--,A \.-Jqlls = 13,S-P-Sf, -Poor 22 2's plr W 1, wtA w-4 �,J (Llc LoA.3 Coll Loafs Co 4, 3 1 K-14 z KIA F DATE I DATE O cr 3 /// Aq • • Form 5007 (Rev. 9/95) CALCULATION SET NO. REV. COMP. BY CH Raytheon Engineers & GENERAL 'D. Y Constructors COMPUTATION / 7a�o -Z �G A SHEET PRELIM. FINAL VOID DATE DOE/ ' I 21-1 .Y� PROJECT OSe SHEET OF DATE DATE SUBJECT OVK , CC Y4PSS OY + J.O. ??D SZ. OCJ/ i�► ci W est n I FL -t V-� ►fin 5 Q Y es h s Eh �Y'Giwt cros .675 E,qv� �f1��,f1s E�� �r ►mss = 19:5(4+2���iZ.>> _.7'7 Eave S7 F-K"is -: - �I Carh.ev. Co Cs, B.ZS�13.5{- � +�► d cel . -- � 3 .s(13 ,sp S4� r 6 � g 3 �/fF L�ewaV-A wavi('. D 7S1414f Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET PROJECT 1 1�LJ 6® $ CALCULATION. SET NO. '-,, REV. COMP. BY CHK'D. BY r PRELIM. FINAL VOID AT DATE K(1 `` �"'�' SUBJECT 2 CJw► e5 QY (4 SHEET 217 OF _ DATE DATE J.o: OS Z Vol oL— Use VTC 2-'rr[j,S.S Gw+� SiYiG� w �l8 `�"�►0 es i �pac�� . �2 Sl �►��,Vvi�SS Yct�io " ZO . will L I � y �er�ica� ra�eS 52� SQ C.,, 6. --► u S e 2 -L -S X '1 & 8 3 3 8. ¢« Ver+1' B rAces I`°I e ►►-► 55 �,.,,., ,,� i= .�. SZ�`i3) � 23.46 � ..� = l 3.9 � -->Use 2-1-S4x32X4- Z-8 �cof . $yaCeS S� .. Ca b• 17 . M S9� Pw, 2.3 9. '7 . o s , K .Q /8.7 ' mouse WTEx "l./.,.4 K. 4 p�-Ch.I!). use Y',,/ /: oad for /1.� n U Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID QATFQ _DATE A Go PROJECT–W, OS e- SHEET 2 g OF DATE DATE SUBJECTT(P—WI Q� �C7�M bre55aV (�es J.O. ra c 1 h Sfr u, rS 6 Z (, �-- C` Q,,, l�Se h/IoXZ� 6 e x �/�xZZ Lt5 �J r-1 J Form 5007 (Rev. 9195) I Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET 1_I I -I j � GDt7S e. 21 CALCULATION SET, NO. 7 O - REV. COMP. BY FG CHK'D. BY %o PRELIM. FINAL VOID Z A $ DATES` PROJECT -W i 1 SUBJECT e V!90 (d SHEET , 2 OF DATE DATE .o. J -0- 21 FY 4 4. S1 ' ox c c�,-►-) b Z 5 14 "FY 6. 33 . re a. z /4 -p LAr' Lr3 7 rb . 2 � ----- . U.S e Shear L�c. re LA Ye-� �eY_ W'eX 0weV1I --0L4&,e 1"ll 4" x 0'-7 ►' I�. � r �� �� ds eco �L&O 5+",A 4n v l p . 3-0). -;Use OV--eV•S Ire. -SS �w ten, f 1 i ,i i Q: 0 LA-) a 3/1 A& 6/76 3' fl } Z:)!6 -'EAR - _UCs FOR BA3C PLATE • 3, oeo � s � G�c � e 5MALL SHEAR LUGS BAR LENGTH (REQUIRED MAXIMUM HORIZCNTA SHEAR GROUT - 11' THICKNE55 11/2" 211 5 K1r-,5 3 3 4 ( 10 4 7 7 15 9 10. 10 20 1.2 13 1.4 25 .14 1G 17 jL 3o, 17. 19 20 35 20 22 24 40 23 25 27 -7 25 .8 �O 50 Z8 31 %�1 15A5 - PLATE C.,Fzcut� -, In Z 3/8 lb I a. - H I 1•- �HCAR• LUG 0 POCKET 4" c� SE.'': I©N1 - 5MAL_ SHE,C.R LUG LARGE 51-1EAR LUGS 154R LE-QGTH fZE�iRE•p w4AIMUM 5HEAR GROUT THfC�CNE'S5 lye r 2" 2W 3' p 10 KIP5' 3 3 4 4 20 j 6 G 7 7. i II 30 9• 9 10 10 4o 11 t 1 2 is 14 � 50 14 15 16 17 I 18 19 20 • .23 j 8c 22. -24.. 25 27 a0 Z5 27 28 30 loc 28 29 31 33 3-10 k 5A5I= PLATE CG�JTj . • . i ��_ • � u —SH CAR LUG PACKET � `I J - I -T7 =-- 5" - :.ARG� 5h-IF_AR J� 40 Form 5007 (Rev. 9/95) . Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET PROJECT KV) 1� GOOSe- SUBJECT I e"W0- C,0-w1I0YPSS0' CALCULATION] SET NO. 7V .00 m Z REV. CO/MMP. BY FD- CHK'D. BY PRELIM. I FINAL I VOID ATE r DAT SHEET 7 OF DATE DATE T7 J.O. / 0-19'z, 0 VPrt� �a� 1. �ra��v, �ohh , �� - T. (Mems - sz4 s4) S4 Pj,,,1 a _. 6 .! 4 3 = 9 9, 9 z'�- c csy►, tr , Bra c e Loa -A �1 o Y� , . G owv`�. _ (49 .q Z-) Z- 3 O. S K- 16 ,4 (49.9� p )6 ,4 kDYt: . C a h N �nl 1 = 434 •�� L." S i l�q IZ 9 (Asse+ . . TA --7 ) / 92.h o7 s6k wel� .s 9ooci for ,�i2��s�%S�` 44,1'`ok : N V er+, l q�a -:5 &4 z 30,5 .oghes'G14,4lesi Y, ,Z4''o/ ��CN �� Ilei w ei� cJood oY ,928(3)(24, Yer't i ct ►-a.c w�j CB n n C' �, S 1—/ 2 � (DC -f z!) %Y- (0LQ er � C h0Y}. hnr I ey►7j� ='7" p by _C'vw, �, w� �.� coh v1, vA 5 �v� 9 �2 " s s IIe+ p l aJ-e l� �' . ►11 e wf-kA5�Cia��tci'f t/ = .7ZS(3)(7)hz 'z 3q.0-'`>3o,S Ver�'� I e�5 �-� = . � 6 �. 3 > 39•• 6 0 4- 8�1+ �'r-�.�s ��r � 0 l o w e r �O►-ac -e oY . 4 (q, 3') = 3V2' > 3 o : s og, per Vtt 09 aY+al 161 o1 S� C0r"' b, Z A 3 3 t,:l a -n. ID, S� — 10 7 3. 3 z. 19 Mab. Form 5007 (Rev. 9/95) • Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET 0 o� < CALCULATION SET NO. REV. COMP. BY FS CHK'D. BY PRELIM. FINAL VOID AT DATE PROJECT --W SUBJECTTe►MT, CO►'►'ra1rP$SOV 14a),J.O. SHEET -3-z_ OF r� /rJO5L;60� DATE DATE el `Z v Y ! Gq ►�1 3z,�/'� c�lL 1 use 36 c�,PL� 38`' ►�sse lade 236� L �7,g 4,4o .ale►-�►C.A� Cv��aHe,�►� _ ��%�3Z.9� � �Z.SS�` Force cry watt ZZ.$$K ` .3..051`��ti, l l6Nw3fdS`�� O►� �ucfe+ p1ct4e ZZ.S$ _ 7 63Ks<< 14,4rs E1 '/% weld S ,ear- Force 23-66 = ,9.3%h. /Z,75(z r e.+ wel oJcoc� -�or 3 ? -S') Z'7 14-1 • • • 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION 4111,7494no z — vico DATE SHEET PRELIM. FINAL VOID DAT '<` ) PROJECT W I G> GS e SHEET OF ZL DATE DATE SUBJECT ewe Y, J.O. 7700-z, 061 ' 3 u l e•�, �. 59 pn�ox 31 l 5'3i 9.45" 34- 3,. 41 43,41 I46wt6 S$:coil calwA poN 16.E StI .g 1 . l b) _ . $ 4 16�$ v,Se I.6 F1 Jte7-'w4-0 wtluA 5ussef M � � C� � . C'o� o-vt ev►.� = 9<4S �j 3 ,.5� z 6 , � � �= /8.7¢ ,cl [Ate 4 lZ� US'�n9 36u `Fa �ie�_w�1ds L<gl zf 2 (.gzS):(3� 31 2�� 0 • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. REV. COMP. BY CHK'D. BY .0 PRELIM. FINAL VOID_ PATE DATE PROJECT '7[479 W Y-CSICO Y"' B SUBJECT SHEET OF z I— DATE DATE J.O. UBC: zz I 1.6 2211, 7, F-/exV El WOV5 f w 8A'60, 2—�64 A - S- eezv- y + 6r- tc�2 77 24 C Jz e- 216 K f - for . jcsilyl 2e It, 7, 2, Z 8S 3 f74 14 90 974" 6 3 /� /�g 0 [7 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. I REV. I COMPP, BY PRELIM. FINAL I VOID PROJECT—W IyC9S Q SHEET / OF SUBJECTI&Wl10, �f a-1 SSOy pia-�, J.O. 97SZ• FX,/ i�r� e ✓ Tv ZLv/ a C— ck e c -L t e a tt r 04 ►` +►^ci e v a-►� y 't o rc e 4o O -� ww� rr1 w x-10 , . DATE �l a,►�.� a `ro rc a 21 � 6Z- _ ' / 4'7 , 7 k. (/8,2-4 0S) , C'ol. Web Ske" Stve'sS /47,7 l9•S-F- l9.77'�s �» / 4,4 KS �m�bl *ev- -PI�4cs are re` A CHK'D. BY -2,/?,;? DATE^ DATE Toms; 0.N., Fig , r9-zSc (kI-1) 647,7) - 246-2-'v-. r/� rr + ,�% Z46.Z /.DS" :� �Lk SiTier ye 4" YeSSi cr� t,5. 4/SC ll<l- 8) 4��0 �w� 4100(,4�s)3 36 7,/ 4 /8 P Z96 Z st e-" A :st 3g S f l-lle" e v L `m,; Is fP ?L,•y = 36 (4- 1E) [49r tE(/, 37S)3 1,3 . �ohV\ wb = 4) oO(;4 36 113,4 P, -2`j /S'15 FX, = 6, /08,? K lo -34 -pst Ten s ; pl, vn y) Y, PP b) 3/,t /9's is [7 0 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET PROJECT ' (� ooS CALCULATION SET NO. 'e�QvD a zDT REV. COMP. BY FG CHK'D. BY PRELIM. FINAL VOID 8 DATE tea, <j SHEET 3 OF DATE DATE SUBJECT I �°►`') j�. �o7r1 YQSSOY k7� i, J.O. / 1C)SL. ool �d e �• -� o �o � ww� vt Cc vti vl e �� i �'l C� vn f� �\ st (C pb f -- �, (� (poj Y � ?L,, 244.Z- 3. 46,2-3. S zy St " 3.� D�a:b�Pr �l zfes H s e4(36)(A1E Z9)6,9,zS) /74.6'1->/477K V .b1�- �l weld �o h v►, A 1 SC GR C It + �/ 6�) ►ie J 14-v lam► e .4 k, 15 In✓ tl. also d Z W - p. 2-4647 use /6 %afe Gier�ev- +o wets F-1 9 e; o V s e Iw / I D Q vie ft--, c;JI-r- II b tc ff wdJ§ e� USS 4t' ��et rtti,.e�dS �a 51d e o`t we�j 7,S 8./Z .10 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL. CALCULATION SET NO. REV. COMP. BY CHWD. BY Constructors COMPUTATION 1 � 77a � t G -�� PRELIM. FINAL VOID �I, 9g J `4 J'43 SHEET /DA `11 Z PROJECT � . - I j G ©ds SHEET ' OF DATE DATE SUBJECT e1nK�► YPSto✓ ��� J.O..�'�QSZ.Di�l �ziY�Aer s �►Ce b -C �es,yh ec� -�6 44evejo e �l,e KP - C 5; Z9 -k 1+ 1 VlCil O i Gas _ 34 " �6 l fs 5 i �.3 l e S �, ear _ /� � 8 -..►-o �s �okble 8 , 4- rows rows SSS!% 5 T:t Area v IL 8 - 78'x' ba l fs -Pa 644,k�- e ' C` r� = S.4$�2S,Z'`lbol�� �3�'.�,'C- _ /3 81 Z K > 107 4 dK • • 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. !O40 L REV. COMP. BY FG CHK'D. BY %� 9 PRELIM. FINAL VOID DAT DAT PROJECT iA1 I Gi SUBJECT SHEET OF DATE DATE J -0- .O.P1►A P1 VA, . b e,� d i g ►� cTvi , . Z S Sxre,� _ �s4,3/Zi,� _ /6�4�✓�3 9 5D N e � -Se J" 0-. � Modd 6d 1 a � i — Z" X l Z ". -T w/ 4-1 �.' /SIS 3,78t7' 2114 -4� 1215)-4(1,o�Ys�y3.7B°old -G--o, 5 e SAO I �z 7 s z `lX / Z" 0 LJ rums ouui tnev. wtfo) Ray*heon Engineers & GENERAL Constructors COMPUTATION SHEET �� (� �6©i'� CALCULATION SET NO. 17DDG -L REV. COMP. BY CHK'D. BY f' PRELIM. FINAL VOID 2/AT 99 DATE � - yb PROJECT �1 SUBJECTTf 'V'Wl LCr�'110Y, c GI . SHEET 3 OF DATE DATE �7 J.O.% l D S Z. )( �Er Sw Z- IrYlf� vox, G « W; )� B-CsSL4.re- a� 30-40' ova e p = 1,21 /' 3 2 4 r s� soy 2S7r��F A q, S- (S;, 0) + 6 2, - Loac� Z V-zrIS<�b2T /icy - Soy /��r 5 ,�5 v /5S�-wte Ver , I.aj - /'SK Loa = ?,714 Ye C. = -�')'L /,S'� 4 MY z . /.oZ k ({- 4 Try W $ -)c Z4 M It =42w -f'- X �I�dw e az (j -L) y S63 U sve W 8� z 4 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO.' REV. COMP. BY CHK'D. BY FCr 3i?� Constructors COMPUTATION /.3 ' eve- PRELIM. FINAL VOID. /AT pjIDATE'SHEET p 3-�•/�j PROJECT by �a p SHEET 41 OF711 DATE DATE SUBJECT �►'► C._�m r, D� J.O. - - " 4 ,68 ,b8� • 6 8� M'A al lou•al7l e ` $ • �b 3,z(rz � 6•g��s� 3,0.5" •Z� y z 27. d�csc 38 Z7.a, • C� Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. / %DOD - Z REV. _ . COMP. BY CHK'D. BY .moo PRELIM. FINAL VOID DATF DATE PROJECT! I I la o OS 2A SHEET 4 ( OF )9 DATE -DATE SUBJECT7e ^ Y. J.O. /� 1oSZ. lot .fin ��. �e S�'�eri c e ✓ �rc: ors 'Veljor Q7777q-3 '! �f. = L42�� �ssuwle 1'1�iv)Pv �GtKnS Selo M` _ 1 Lal 1 Crct force p.,,, 5 ut�J�D o �D wtS �D. S�6 ` 1. ?.S �L L- W; Q In -ISS abo 9 vacl e 20 s Load 6 d 2 K— Le ac, o b i • .Form 5007; (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET w GVdS e CALCULATION SET NO. 12, elpDvo - Z REV. COMPP, BY CHK'D..BY & 6 PRELIM. FINAL VOID AT 2-)l DATE O_Q3 PROJECT l SUBJECT�'i!!.. Cw,,,,o 1'.��� SHEETZ OF DATE DATE J.O. PVIl = 8471`<3) /,4I �.o�� s 1 �+. re ve`Yy � :wT<a, I � w, ,h; ►�►�► �.�,,,., t�v � � i�.g K �o m ate► a,�, s a 1^o y. , `I.4Z 7 0'7)1 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET V� `4 �Bfls� CALCULATION SET NO. /J W ee - t REV. COMP. BY lam • C K'D. BY ,:,,20 PRELIM. FINAL VOID /DATE l I 98 DATE PROJECT '�"' SUBJECT -o w a. Cow► py ( J5, SHEET /�� OF DATE DATE J.O. 770 S-2-6 01 2,`I3K�f 2 3.4 S Ks ` o tG lalf - l I I t �9 as -X —�--� s 7-S 6 x 6 k 4 �Y d ea.m �-- - Lc s -e 7'S 4 x 4,x ¢. fa r J sh �ye .0 .,3 )4.12x40,ILAIDx .3_ 1•J17,c4oW CIOx153, 24 k.. W I O KZz I b XZz M (EllW I; X/% . 18 x 17 P --y W/O)( 11 , J8 W /Ox 1 37 9z z 40 w►oxt 10 X 1 nn . Sg LA 59` 6040 J C1 46 3� 7 Z6 ��Xlil 4IZx4ow W 1 Zxgd w�C /OX/S3 `NIOn- WIDXzz� \e�11b�c2Z - All` r 0 21 s //d` 3'42 I Z� O" '7`O" " /2,O.. �" -o X42 �! ro IF s 1 wivxZz w loxzz w�oxiS .SAJ Reeis S S� R ds i • 2-71 . 1 P6 Q - - W 16 Z?- \aJ I D S W I C, ZZ - -� 6 wlo,czzioxZZ . 2 y1io_xt G—! ; w�oxi5 W ib,ciS WtoXrS "n nn W rDxiS. ——— —rte— \. } c .10'otti mI ;411 - rj OL ID PAGE NO. 1 ID6 Raytheon,Eng:. & Const:. •* S T AAD - III * Revision 21.0 * Proprietary Program of * Research Engineers, Inc. * Date= FEB 27, 1998 *. Time= 12:51:21- -USER ID: Raytheon Eng. & Const. *. 1. STAAD SPACE 2. *FILE NAME -,TEMPORARY COMPRESSOR BUILDING (TECOBLDG) 3. *WILD GOOSE COMPRESSOR BUILDING .4.'*REVISION 0 -5. *JAN. 29,198 -6. 7. 9. * DESIGNED BY 10. * CHECKED BY GT 11. 12. 13. UNIT RIP FT •14. 15. •16. JOI COORD 17 18. * COLUMN LINE D 19. 1 0 0 0; 2 0 13 0; 3 0,23 0; 4 0 24.125 13.5; 5 0 23.27; 6, 0 1311,27 ;20..70 0 27; 29 0 0 13.5;-30 0-13 13.5 21. * COLUMN LINE C 22. 8 26 0 0; 9 26 13 0; 10 26 23 0; 11 26 24.125 13.5; 12 26 23 27 23. 13 26 13 27; 14 26 0 27 24. * COLUMN LINE B 25. 15 36 0 0; 16 36 13 0; 17 36 23 0; 18 36.24.125 13.5; 19.36 23 27 " 26. 20 36 1.3 27;,21 36 0 27 27. * COLUMN LINE A 28. 22.62 0 0; 23 62 13 0; 24 62 23 0;-25 62 24.125 13..5; 26 62"_23 27 ' .29. 27 62'13 _27; 28 62 0 27; 31 62 0,13.5; 32 62 13.13.5 30. * ROOF PLANE - 31."33 13 23 0;.34 13 24.125 13.5; 35 13 23'27; 36 49 23 0- 32. 3749 24.125:13.5; 38 49 23 27 34. MEM INCI 35, 36. * COLUMN LINE D 3.7..1 .1 2 6; 25 29 30; 26 30 4; 27 2 30;' 28 30 6 38: * COLUMN LINE C 39. 7 8 9 12 40..* COLUMN LINE B , 41. 13 15 16 18 3%iIfd STAAD SPACE -- PAGE NO. 2 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng.':. & Const. 42. * COLUMN LINE A 43. 19 22 23 24; 29 31 32; 30 32 25; 31 27 32; 32 32 23 •44. * COLUMN LINE 45. * ROOF PLANE 46. 33 3 33; 34 33-10; 35 10 17; 36 17 36; 37 36 24; 38 4'34; 39.34 11 47. 40, 11 18;•41 18 37;'42 37 25; 43 5 35; 44 35 12; 45 12 19; 46 19 38. 48. 4738 26; 48 34 33; 49 35 34; 56 37 36; 51 38 37 49. * ROOF BRACING 50. 56 4 35; 57 35 11; 58'11 19 51. 59 19 37; 60 37 26;, 61 17; 37 52. * VERTICAL BRACING AND STRUTS 53.52 15 9; 53 17 9; 54 13 21; 55 13 19; 62 16 9; 63 6 13; 64 13 20 54. 65 20 27 55. UNIT RIP INCH 56. ********** 57. , MEMB PROP 58. ********** 59. * FRAMES 60. 1 TO 24 TA ST W18%60 61. * WIND COLUMNS 62.,25 26 29 30 TA ST W12B26 63. * STRUTS 64. 27 28 31 32 TA ST W8B18; 48 TO 51 62 64 33 TO 47 TA ST W10B22 65. 63 65 TA ST W10%33 66. * VERTICAL BRACING 67. 52 54 TA LD 1,50355 SP .375 68. 53 55 TA LD L40354 SP .375 69. *.ROOF BRACING •70. 56 TO 61 TA -T W10B22 71. ******** 72. MEM REL 73. ******** 74. * WIND COLUMNS 75. 26 30 END MY MZ F% 76. * STRUTS 77. 27 28 31 32 START MY, MZ; 27 28 31 32.END MY MZ 78. 62 TO 65 START MY MZ; -62 TO`65 END MY MZ 79. 33 35 36 38 40 41 -43 45 46 48 TO 51 START MY MZ 80. 34 35 37 39 40 42 44 45 47 48 TO 51 END MY MZ 81. MEM TRUSS 82. 52 TO 61' 83. ********** 84. ,CONSTANTS 85. ********** 86. E STEEL ALL ,87. POI STEEL ALL 88. DENSITY STEEL ALL 89. BETA 90 MEM 1'2 5 TO 8 11 TO 14.17 TO 20 23 24 62 TO 65 90. ********** 91. SUPPORTS 92. ********** 93. 1 7 8 14 15 21 22 28 29 31 PINNED 94. 95. DRAW ISO JOI MEM SUP PRO I S T A A D -III REV: 21.0 H 0. i K C Sd p C w O I p p.� uR N - Rl z 0 O . p cf _ ` V , • _ 3,y1Bx63 1 STRUCTURE DATA: � 3�{It0x2= 0 4 yttaX27k9 'S z TYPE = SPACE.3d►18X2-'- dIOFL2 1 53;� t®@ zZNNI n l� x tzx eoxe NJ = 39 331118X4` g 301 p� X`rk NM = 65 l x �� �1 LZxg + tBx2- f 4 n 2 OyXe,N 36wta%e�ke X t�/" 0, q}i s kB A�;AIX' 2 X NE = 0 5s 2 ii $; tBx ' A e k0,1 2 m m ZLxe 4 30 rt s e 7 �` m x e' 8 k 7 NL = 0 2 N e% m m UNIT INCH KIP 7fq s 5�,/ ; ss ^ 10X33 ry 2 ;rFS� ;,,IBX`: • x XMAX:= 744.0 e, •k9 m x m 2 N "-a YMAX= 299.5 Ag s CD s et4X33 �2 s I x , ZMA:x= 324.0 x mm 9• k8A 63 ' 5 sq o t m s ..y m , t x m x x CD •25O ... 9 = DATE:FEB 27,1998 TIME: 12:51:21 t USER ID:Raytheon ng. F: Const. DRAW ISO JOI MEM SUP PRO H 0. i K C Sd p C w O I p p.� uR N - Rl z 0 O . p cf _ ` V STAAD SPACE -- PAGE NO. 4 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const.. 96. ************************* 97. UNIT RIP FT ******************* •98. . 99. DEFINE UBC LOAD 100.. ******************* 101. ZONE .3 I 1.0 RWB 8 RWZ 6 S 1.2 102. SELFWEIGHT 103. JOI WEI ' 104. * EAVES STRUT _ 105. * COL. LINES 1 & 2 106. 3 5 24 26 WEI 5.7; 10 12 17 19 WEI 6.73 107.- * PURLINS 108. * COL. LINES A & D 109. MEM WEIGHT - 110. 3 21 CON 2.58 3.5; 3 21 CON 2.58 8.17; 3 21 CON 1.55 12.83 111. 4 22 CON 1.55 .67; 4 22 CON 2.58 5.33; 4 22 CON 2.58 10 112. * COL. LINES B & C 113. 9 15 CON 1.8 3.5; 9 15 CON 1.8 8.17; 9 15 CON.1.8 12.83 114. 10 16 CON 1.8 .67; 10 16 CON 1.8 5.33; 10 16 CON 1.8 10. 115. * GIRT LOADS 116. 1 2 5 6 19 20 23 24 UNI .084;.7 8 11 12 13 14 17 18 UNI .12 117. * HVAC EQUIP. LOADS .118. 15 21 CON'S 9 119. 120. LOAD 1 UBC % DIRECTION (S -N) 121. UBC LOAD % 122. *********************** 123. LOAD 2, UBC Z DIRECTION (W -E) •124. UBC LOAD Z 125. ************************ 126. LOADING 3 -DEAD LOAD (DL) 127. ************************ 128. SELFWEIGHT Y -1.03 129. * PURLINS 130. * COL. LINES A & D 131. MEM LOAD: 132. 3 21 CON GY -2.58 3.5; 3 21 CON GY -2,.58.8.17; 3 21 CON GY -1.55.12.83 133. 4 22 CON GY -1.55, .67; 4 22 .CON GY -2.58 5.33;.4 22 CON GY -2.58.10 134. * COL. LINES B-& C 135. 9 15 CON GY--1.8 3.5; 9 15 CON GY -1.8 8.17; 9 15 CON GY -1.8 12.83 136. 10 16 CON GY -1.8 .67; 10 16 CON GY.-1.8 5.33; 10 16 CON GY -1..8; 10 137. * EAVES STRUT 138. * COL. LINES 1 & 2 139. JOI LOAD 140. 3 5 24 26 FY -5.7; 10 12 17'19 FY -6.73 141. * GIRT LOADS 142. MEM LOAD 143. 1 2 5 6 19 20 23 24 UNI GY -.084; 7 8.11 12 13 14 17 18 UNI GY -.12• 144. * HVAC EQUIP. LOADS 145. MEM LOAD 146. 15 21 CON GY -3 9 147. ***************** 148. LOAD 4 LIVE'LOAD (LL) ***************** •149. 150. * ROOF PURLINS 151. MEM LOAD STAAD SPACE -- PAGE NO. 5 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. 152. 3 21 CON GY -1.5 3.5; 3 21 CON GY -1.5 8.17.; 3 21 CON GY -.90 12.83 153. 4 22 CON GY -.90 .67; 4 22 CON GY -1.5 5.33; 4.'22 CON GY -1.5,10' •154. * COL. LINES B & C 155. 9 15 CON GY -1.8 3.5; 9 15 CON GY -1.8 8.17; 9 15 CON GY -1.08 12.83 156. 10 16 CON GY -1.08 .67;. 10 16 CON GY -1.8 5.33; 10 16 CON GY -1.8 10 157. * EAVE STRUT 158. JOI LOAD 159. 3 5 24 26 FY -1.24; 10 12 17 19 FY -1.53 160. ************************ 161. LOAD 5 CONTINGENCY LOAD (CL) 162. ************************ 163. JOI LOAD 164. 4 11 18 25 FY -2; 3 5 10 12 17 19 24 26 FY +1 165. ************************* 166. LOAD 6 WIND WEST TO EAST (E -W) 167. 168 * OPENING FOR TEMP. COMPRESSORS WILL BE SIDED IN WHEN COMPRESSORS 169. * ARE REMOVED AND BLDG. IS USED AS A WAREHOUSE. 170. MEM LOAD 171. * COL. LOADS 172. 5 6 23 24 UNI GZ -.196; 11 12 17 18 UNI GZ -.243 173. 1 2 19 20 UNI GZ -.131; 7 8 13 14 UNI GZ -.162 174. * ROOF PURLINS 175. * COL. LINES A & D 176. 3 21 CON Y .85 3.5; 3 21 CON Y .85 8.17; 3 21 CON Y .55 12.83 177. 4 22 CON Y .55 .67; 4 22 CON Y .85 5.33; 4 22 CON Y .85 10 178. * COL. LINES B & C •179. 9 15 CON Y 1.05 3.5; 9 15 CON Y 1.05 8.17; 9 15 CON Y .68 12.83 180. 10 16 CON Y .68 .67; 10 16 CONY 1.05 5.33; 10 16 CON Y 1.05 10 181. * EAVE STRUTS 182. * COL. LINES A & D 183. JOI LOAD 184. 3 5 24,26 FY .77 185. *-COL. LINES B & C 186. 10 12 17 19 FY .96 187. 188. LOAD 7 WIND SOUTH TO NORTH (S -N) 189. **************************** 190. * COL. LOADS 191. MEM LOAD 192. 1 2 5 6 UNI G% .11; 25 26 UNI G% .183 193. 19 20 23 24 UNI G% .075; 29 30 UNI G% .122 194. * ROOF PURLINS 195. * COL LINES A'& D- 196. 3 21 CON Y .85 3.5; 3.21 CON Y .85 8.17; 3 21"CON Y .55 12.83 197..4 22 CON Y .55 .67; 4 22 CON Y .85 5.33; 4 22 CON Y .85 10 198. * COL. LINES B & C 199. 9 15 CON Y 1.05 3.5; 9 15 CON Y 1.05 8.17"; 9 15 CON Y..68 12.83 20.0. 10 16 CON Y .68 .67; 10 16 CON Y 1.05 5.33; 10 16 CONY 1.05 10 201. * EAVE STRUTS 202. * COL. LINES A & D 203. JOI LOAD 204. 3 5 24 26 FY .77 .205. * COL. LINES B & C 06. 10 12 17 19 FY .96 207. **********w************** ' STAAD SPACE tI -- PAGENO. 6 _ *FILL E NAME'- •TEMPORARY COMPRESSOR BUILDING•( ID: Raytheon Eng., &' Const. ' Y. 208. LOAD B..WIND NORTH`TO SOUTH'(N-S)• 209. •210. * COL. LOADS r 211. MEM LOAD 4 212. 1 2'5'6 UNI G% -.07.5; 25 26 UNI'G% -.122 > 213. 19 20 23 24 UNI GB -:11;.29 30 UNI.G% -.183 214. * ROOF,PURLINS - 215. * COL LINES A & D 216. 3 21 CON Y :85 3.5; 3~21 CON Y .85,8.17; 3-21 CON Y .55'12.83' a 217. 4 22 CON Y .55 .67; 4 22 -CONY .85 5.33;,4.22 r ,CON Y'.85 10 y } 218. * COL. LINES B & C' •219. 9 15 CON Y 1.05 3.5; 9 15 CON Y 1:05 8.17; s l 9 15 CON Y'.68 .12.83 . 220.10 16 CON Y .68 .67; 10 16 CON Y 1.05 5.33; 10 16 CONY 1.05 "10 t ' 221. * EAVE STRUTS 222. *.COL. LINES A & D. - _223 2i3. JOI LOAD _ 224. 3 5 24,26 FY -:77 ► 225., * COL.' LINES B.•& C - 226. 10 12 17 19 FY .96 Y 227. .'228. *LOAD 8 THERMAL -LOAD (TL) , - 229. x,230. *1 TO 65 TEMP •30'. .231: M. *LOAD COMBINATIONS 233. 234.. LOAD COMB 10 DL+LL+CL 235. 3 1.0 4 1.0.5'1.0 - •,: . 36. LOAD COMB 11 DL+LL+CL+WL(E-W) 0237. t•� 3 :75 4 .75 5 .75 6- ..75 2j8. LOAD COMB -1 2 DL+LL+CL+WL (S -N) r• ; ' y ` • . ' r 239. 3 .75.4 .75 5' .75 7 .75 - _ r 240. LOAD COMB 13 DL+LL+CL+WL(N-S)•,• F 241. 3 .75 4,...75 5 .75 8 .75 �'. _' ,' ;.•..} 242. LOAD COMB 14 DL+LL+CL+SL (W -E) 243. 3 .75 4 .75 .5 .75 2.75 , - 244`. LOAD COMB 15 DL+LL+CL+SL(E-W) .. '245.'3 .75 4 .75 5 .75 2 -.75 246. LOAD COMB 16.' DL+LIi+CL+SL(S-N) 247. -3-'.,75 4 .75 5-.75'1 .75 ' ' 2 4 8 . • LOAD COMB • 17 DL+LL+CL+SL (N- S) - ,• . 249. .3 .75 4•.75 5 .75 1 -.75 w • 250. 251. *LOAD -COMB FOR DEFLECTIONS ti _ : r •` { 252. s : .253. LOAD ,. COMB , 20 DL+LL+CL+WL (E4) _ 254. 3.1.0 4 1.0 '5 1:0 6 1.0 .r 255. LOAD COMB 21•DL+LL+CL+WL(S-N)' - _ �. - • ' 256. 3 1.0 4' 1..0' 5 •'1.0 7 1.0 , 257. LOAD COMB 22 DL+LL+CL+WL(N-S)' ..'258. 3 1.0 .4 1.0 ,..5 1.0. 8 1'.0 • '259:- LOAD COMB - 2 3 DL+LL+CL+SL (W -E )' ` '260. 3 1.0.4 1.0 5-1.0 2 1.0- 6.1.'LOAD COMB 24 DL+LL+CL+SL(E-W). = 62. 3 1.0 .4 •1.0.5 1.0 2 -1.0 �, 263.. LOAD COMB,25 DL+LL+CL+SL(S=N)r >` ; STAAD SPACE -- PAGE'NO. 7 *FILE NAME - TEMPORARY COMPRESSOR -BUILDING ( ID: Raytheon Eng. & Const. 264. 3 1.0 4 1.0 5 1.0 .1 1.0 ' 265. LOAD COMB 26 DL+LL+CL+SL(N-S) •26'6. 3 1.0 4 1.0 5 1.0 1 -1.0 267. ******************************* .268. *LOAD COOMBINATIONS FOR .NET UPLIFT 269. ******************************* 270. * SIDING LOAD DECREASED FROM-10PSF TO 6PSF SO -CHANGE .85DL TO .8DL' 271. * PER REX OWEN 2/16/98 272. LOAD COMB 30 .80DL+WL(E-W) 273. 3 .80 6 1.0 274. LOAD COMB 31 .80DL+WL(S-N) 275. 3-.80 7 1.0 276. LOAD COMB 32 .80DL+WL(N-S) 277. 3 .80 8 1.0 278. LOAD COMB 33 .80DL+SL(S-N) 279. 3_80 1 1.0 .280. LOAD COMB 34 .8ODL+SL(N-S) 281. 3 .80 .1 -1.0 282. LOAD COMB 35 .80DL+SL(W-E) 283. 3 .80 2 1.0 . 284. LOAD COMB 36 .80DL+SL(E-W) 285.` 3 .80 2 -1:0 :286. ******w********** 287. PERFORM ANALYSIS .• 'P' R 0 B-; L E M S TAT I S T I C S • ------------------------- NUMBER OF JOINTS - /MEMBER+ELEMENTS/SUPPORTS -. 38/ 65/ 10 ., ORIGINAL/FINAL BAND -WIDTH = 31/ 8 TOTAL PRIMARY LOAD CASES = 8, TOTAL DEGREES -OF FREEDOM = 19.8 SIZE OF STIFFNESS MATRIX _ .10098 DOUBLE PREC. WORDS REQRD/AVAIL. DISK SPACE = 12.18/ 1631.9 MB, EXMEM = 25.69 MB ++ PROCESSING ELEMENT.STIFFNESS MATRIX. 12:51:22 ++ PROCESSING GLOBAL STIFFNESS MATRIX. 12:51:22 - ++ PROCESSING TRIANGULAR FACTORIZATION. '12:51:22 .++ CALCULATING JOINT DISPLACEMENTS•. 12:51:22 „ * CALC/USED PERIOD FOR X UBC = 0.2583/ 0.2583 SEC * C, C -ALT = 3.6990 , 2.2834, LOAD FACTOR = 1.000 * UBC FACTOR V = 0.1031 X 152.21 = 15.70 RIP *. * * 3 A /M., STAAD SPACE --.PAGE NO. 9 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID:.Raytheon Eng.'& Const. •SUPPORT REACTIONS -UNIT ----------------- RIP FEET STRUCTURE TYPE = SPACE ; JOINT LOAD FORCE-%, FORCE -Y FORCE -Z MOM-% MOM -Y MOM Z 1 1 -0.05 0.13 0.08 0.00 0.00 0.00 2 0.00 -3.57,' -2.10 0.00 0.00 0.00. 3 0.00 17.44 -0.36 0.00 '0.00, 0.00 4 0.00 5.13 "-0.20 0.00 0.00 0.00 5 0.00` 0.00 -0.07 0.00 0.00 0.00 6 0.00 0.61 3.90 0.00 .0.00 0.00. '7 -1.26'.. -2.89 0.19 0.00 0.00 0.00 8 0.86 -3.12 0.05 0.00 0.00' `0.00 10 0.00 212.58 -0.64 0.00 0.00 0.00 11 0.00 17.39 2.45 0.00 0.00 0.00 12 -0.95 14.76 -0.34. 0.00 0.00 0.00 13 0.65 14.59 -0.44 0.00 0.00' .0.00 14 0.00 14.25 -2.05 0.00 0.00 0.00 15 0.00 19.61 1.10 0.00 0.00 0.00 16 -0.04 17.03 .,. =0.42 0.00 0.00 0.00 17 0.04 16.83' -0.54 •0.00 0.00' 0.00 20 0.00 23.19 '3.27 0.00 0.00 0.00 21 -1.26 19.68 -0.45 0.00 0.00 0.00 22; 0.86 19.46 •-0.58 0.00 0.00 0.00 23 0.00 19.01 -2.74 0.00 0.00 0.00 • 24 25 0.00 -0.05 26.15' •22.71 1.46 -0.56 0.00 0.00 0.00 0.00 0.00 .0.00 26 0.05 22.45 -0.71 0.00 _ 0.00 0.00 30, 0.00 14.57 3.62 -0.00 0.00 0.00 31 -1.26 11.06 -0.10 0.00 0.00 32 0.86 10.84. -0.23 0.00 0.00 0.00 33 -0.05 14.09 -0.21 0.00 0.00 0.00 34 0.05' 13.82 -0.36 0.00 0.00 0.00 35 0.00 10.39 -2.39 0.00 0.00 0.00 36 0:00. 17.53 1.81 0.00 0.00 -.0.00 7 1 0.01 -0.14 0.08 0.00 0.00 -0.00 , 2 0.00 3.58. -2.10 0.00 0.00 0.00 3 0.01 17.83 0.44' 0.00 0. 00, 0.00 4• 0.00 5.15 ." 0.19 0.00 0.00 0.00 5 0.00 0.00 0.07 0.00 0.00 0.00 6- 0.00 -6.68 4.0.4 0.00 0.00 0.00 7 -0.58 -3.14 -0.04 0.00 0.00 0.00 8 0.39 -2.90 -0.17 0.00 0.00 0.00 10 0.01 22.98 0.70 0.00 0.00 0:00' 11 0.01 12.23 3.55 0.00 0.00 0.00 12 -0.42 14.87 0.49 0.00 0.00 0.00 13 0.30 15.06 0.40 .0.00 0.00 0.00 14 0.01 19.92 -1.05 0.00 0.00 0.00 15 0.01. 14.55 2•.10 0.00 0.00 0.00 16 0.01 17.13 0.58 0.00 0.00 0.00 17 0.00 .17.34 0.47. 0.00 0.00 0.00 20 0.01 16.30 4.74 0.00 0.00 21 -0.56 19.83 0.66 0.00 0.00 0.00 3 JisApe * 3�//Apw .STAAD SPACE -- PAGE NO. 10 *FILE NAME = TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. .& Const. •SUPPORT REACTIONS -UNIT ----------------- KIP FEET STRUCTURE TYPE = SPACE JOINT LOAD FORCE-% FORCE -Y FORCE -Z MOM-% MOM -Y MOM Z 22 0.40 20.08 0.53. 0.00 0.00 0.00 23 0.01 26.56 -1.40 0.00 0.00 0.00 24 0.01 19.40 2.80 0.00 0.00 0:00 25 0.02 22.83 0.77 0.00 0.00 0.00 26 0.00 23.12 0.62 0.00 0.00 0.00 30 0.00 7.59 4.39 0.00 0.00 0.00 31 -0.57 11.12 0.31 0.00 0.00 0.00 32 0.40 11.37 0.18 0.00 0.00 0.00 33 0.01 14.12 0.42 0.00 0.00 0.00 34 0.00 14.41 0.27 0.00 0. 00 0.00 35 0.01 17.85 -1.75 0.00 0.00 0.00 36 0.01 10.68 2.45 0.00 0.00 0.00 8 1 0.01 -16.84 0.01 0.00 0.00 0.00 2 0.00 -4.48 -2.16 0.00 0.00 0.00 3 0.01 18.7.9 0.93 0.00 0.00 0.00 4 0.00 6.18 0.64 0.00 0.00 0.00 5 0.00 0.00 0.19 0.00 0.00 0.00 6 0.00 -0.30 3.59 0.00 0.00 0.00 7 0.00 -12.20 -0.38 0.00 0.00 0.00 8 -0.01 4.80 -0.38 0.00 0.00 0.00 • 10 11 0.01 0.01 24.97 18.50 1.76 4.02 0.00 0.00 0.00 0.00 0.00 0.00 12 0.01 9.57 1.04 0.00 0.00 0.00 13 0.00 22.33 1.03 0.00. 0.00 0.00 14 0.01 15.37 -0.30 0.00 0.00. 0.00 15 0.01 22.08 2.94 0.00 0.00 0.00 16 0.01 6.10 1.33 0.00 0.00 0.00 17 0.00 31.35 1,.32 0.00 0.00 0.00 20 0.01 24.66 5.35 0.00 0.00 0.00 21 0.01 12.77 -1.38 0.00 0.00 0.00 22 0.01 29.77 1.38 0.00 0.00 0.00 23 0.01 .20.49 -0.40 0.00 0.00 0.00 24 0.01 29.45 .3.92 0.00 0.00 0.00 25 0.02 8.13 1.77 0.00 0.00 0.00 26 0.00 41.80 1.76 0.00 0.00 0.00 30 0.01 14.73 4.34 0.00 0.00 0.00 31 0.01 2.83 0.37 0'.00 0.00 0.00 32 0.`00 19.83 0.36 0.00 0.00 0.00 33 0.01 -1.80 0.75 0.00. 0.00 0.00 34 0.00 31.87 0.74 0.00 0.00 0.00 35 0.00 10.55 -1.41 0.00 0.00 0.00 36 0.01 19.51 2.91 0.00 "' 0.00 0.00 14 1 0.01 -18.03 0.01 0.00 0.00 0.00 2 0.00 4.49 -2.17 0.00' 0.00 0.00 3 0.01 18.47 -0.96 0.00 0.00 0.00 a • 4 5 0.00 0.00 6.24 0.00 -0.63 -01.19 0.00 0.00 0.00 0.00 0.00 0.00 6 0.00 -7.11 5.21 0.00 0.00 0.00 * 3�//Apw ��/of sa 17? STAAD SPACE -- PAGE NO. 11 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. • SUPPORT REACTIONS -UNIT ----------------- RIP FEET STRUCTURE TYPE = SPACE JOINT LOAD FORCE-% FORCE -Y FORCE -Z MOM-% MOM -Y MOM Z 7 -0.01 -13.52 0.38 0.00 0.00 0.00 8 0.00 6.00 0.37 0.00 0.00 0.00 10 0.01 24.71 -1.77 0.00 0.00 0.00 11 0.01 13.20 2.57 0.00 0.00 0.00 12 0.00 8.39 -1.05 0.00 0.00 0.00 13 0.01 .23.03 -1.05 0.00 0.00 0.00 14 0.01 21.90 -2.96 0.00 0.00 0.00 15 0.01 15.16 0.30 0.00 0.00 0.00 16 0.01 5.01 -1.33 0.00 0.00 0.00 17 0.00 32.06 -1.33 0.00 0.00 0.00 20 0.01 17.60 3.43 0.00 0.00. 0.00 21 0.01 11.19 -1.40 0.00 0.00 0.00 22 0.01 30.71 -1.40 0.00 0.00 0.00 23 0.01 29.20 -3.95 0.00 0.00 0..00 24 0.01 - 20.22 0.40 0.00 0.00 0.00 25 0.02 6.68 -1.77. 0.00 0.00 0.00 26 0.00 42.74 -1.78 0.00 0.00 0.00 30 0.00 7.66 4.44 0.00 .0.00 0.00 31 0.00 1.26 -0.39 0.00 0.00 0.00 32 0.01 20.77 -0.39 0.00 0.00 0.00 33 34 0.01 0.00 -3.25 32.81 -0.76 -0.77 0.00 0.00 0.00 0.00 0.00- 0.00 35 0.01 19.27 -2.94 0.00 0.00 0.00 36 0.01 10.28 1.41 0.00 0.00 0.00 15 1 -7.46- 16.72 -0.04 0.00 0.00 0.00 2 -0.38 -2.81 -2.18 0.00 0.00 0.00 3 0.18 20.06 1.21 0.00 0.00 0.00 '4 -0.02 6.26 0.64 0.00 0.00 0.00 5 0.00 0.01 0.19 0.00 0.00 0.00 6 -0.04 -0.11 3.60 0.00 0.00 0.00 7 -3.68 4.63 -0.41 0.00' 0.00 0.00 8 3.72 -12.19 -0.35 0.00 0.00 0.00 10 0.16 26.33 2.04 0.00 0.00 0.00 f 11 0.09 19.67 4.22 0.00 0.00 0.00 12 -2.64 23.22 1.22 0.00, 0.00 0.00 13 2.91 10.61 1.27 0.00 0.00 0.00 14 -0.16 17.64 -0.11 0.00 0.00 0.00 15 0.40, 21.85 3.16 0.00 0.00 0.00 16 -5.47 32.29 1.50 0.00 0.00 0.00 17 5.72 7.21 1.56 0.00 0.00, 0.00 20 0.12 26.22 5.63 0.00 0.00 0.00 21 -3.52 30.96 1.62 0.00 0.00 0.00 22 3-88 14.14 1.69 0.00 0.00 0.00 23 -0.21 23.52 -0.14 0.00 0.'00 0.00 24 0.54 29.14 4.22 0.00 0.00, 0.00 25 -7.30 43.05 2.00 0.00 0.00 0.00_ 26 7.62 9.61 2.08 0.00 0.00 0.00 30 0.10 15.94 4.56 0.00 0.00 0.00 ��/of STAAD SPACE -- PAGE NO. 12 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. .& Const. •SUPPORT REACTIONS -UNIT KIP FEET STRUCTURE TYPE = SPACE ----------------- JOINT LOAD FORCE-% FORCE -Y FORCE -Z MOM -S MOM -Y MOM Z 31 -3.54 20.68 0.55 0.00 0.00 0.00 32 3.87 3.86 0.62 0.00 0.00 0.00 33 -7.31 32.77 0.93 0.00 0.00 0.00 34 7.61 -0.67 1.01 0.00 0.00 0.00 35 -0.23 13.24 -1.21 0.00 0.00 0.00 36 0.52 18.86 3.15 0.00 0.00 0.00 21 1 -8.13 17.98 -0.01 0.00 0.00 0.00 2 0.37 2.76 -2.18 0.00 0.00 0.00 3 =0.22 20.38 -1.17 0.00 0.00 0.00 4 0.01 6.15 -0.63 0.00 0.00 0.00 5 0.00 -0..01 -0.19 0.00 0.00 0.00 6 0.05 -7.31 5.21 0.00 0.00 0.00 7 -5.41 - 6.05 0.37 0.00 0.00 0.00 8 5.38 -13.40 0.38 0.00 0.00 0.00 10 -0.20 26.53 -1.99 0.00 0.00 0.00 11 -0.11 14.41 2.42 0.00 0.00 • 0.00 12 -4.21 24.43 -1.22 0.00 0.00 0.00 13 3.88 9.84 -1.20 0.00 0.00 0.00 14 0.13 21.97 -3.13 0..00 0.00 0.00 15 -0.43 17.83 0.14 0.00 0.00 0.00 • 16 17 -6.25 5.95 33.38 6.41 -1.50 -1.49 0.00 0.00 0.00 0.00 0.00 0.00 20 -0.15 19.22 3.22 0.00 0.00 0.00 21 -5.61 32.58 -1.62 0.00 0.00 0.00 22 5.18 13.13 -1.61 .0.00 0.00- 0.00 23 0.17 29.29 -4.17 0.00 0.00 0.00 24 -0.58 23.77 0.19 0.00 0.00 0.00 25 -8.34 44.51 -2.00 0.00 0.00 0.00 26 7.93 8.55 -1.98. 0.00 0.00' 0.00 30 -0.12 8.99 4.27 0.00 0.00 0.00 31 -5.58 22.35 -0.57 0.00 0.00 0.00 32 5.21 2.90 -0.55 0.00 0.00 0.00 33 -8.30 34.29 -0.94 0.00 0.00 0.00 34 7.96 -1.67 -0.93 0.00 0.00 0.00 35 0.20 19.06 -3.12 0.00 0.00 0.00 36 -0.55 13.55 1.24 0.00 0.00 0.00 22 1 -0.05 -0.02 -0.06 0.00 0.00.. 0.00 2 0.00 -3.71 -2.18 0.00 0.00 0.00 3 0.00 19.31 -0.54 0.00 0.00 0.00 4 0.00 5.15 -0.20 0.00 0.00 0.00 5 0.00 0.00 -0.07 0.00 0.00 0.00 6 0.00 0.64 3.92 0.00 0.00 '0.00 7 -0.86 -3.04 0.06 0.00 0.00 0.00 8 1.26 -3.00 0.17 0.00 0.00 0.00 10 0.00 24.46 -0.81 0.00 0.00 0.00 11 0.00 18.83 2.33. 0.00 0.00 0.00 12 -0.65 16.07 -0.57 0.00 0.00 0.00 13 0.95 16.10 -0.49 0.00 0.00 0.00 sXy/to STAAD SPACE -- PAGE NO. 13 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. • SUPPORT REACTIONS -UNIT ----------------- KIP FEET STRUCTURE TYPE = SPACE JOINT LOAD , FORCE-% FORCE -Y FORCE -Z MOM-% MOM -Y MOM Z . 14 0,.00._ 15.56 -2.25 0.00 0.00. 0.00 15 0.00 21.13 1.03 0.00 0.00 0.00 16 -0.04 18.34 -0.66 0.00 0.00 0.00 17 0.04 18.36 -0.56 0.00 0.00 0.00 20. 0.00 25.10 3.11 0.00 0.00 0.00 21 -0.86 21.43 -0.75 0.00 0.00 .0.00 22 1.26 21.46 -0.65 0.00 0.00 0.00 23 0.00_ 20.75 -3.00 0.00 0.00 0.00- 24 0.00 28.17 1.37 0.00 0.00 0.00 25 -0.05 24.45 -0.88 0.00. 0.00 01.00 26 0.05 24.48 -0.75 0.00 0.00 0.00 30 0.00 16.09 3.49 0.00 0.00 0.00 31 -0.86 12.42 -0.37 0.00 0.00 `0.00 32 1.26 12.45 -0.27 0.00 0.00 0.00 33 -0.05 15.44 -0.50 0:00 0.00 0.00 34' 0.05 15.47 -0.37 0.00 0.00 0.00 35 0.00 11.74 -2.62 0.00 0.00 0.00 36 0.00 19.16 1.75 0.00 0.00 0.00 28. 1 0.01 0.19 -0.05 0.00 0.00 0:00 2, 0.00 3.73 -2.18 0.00 0.00 0.00 • 3 4 0.0,1 0.00 19.01 5.13 0.45 0.20 0.00 0.00 0.00 0.00 0.:00"°: 0.00 5 0.00 0.00 0.07 0.00 0.00 0.00 6 0.00 -6.71 4.05 0.00 0.00 0.00 7 -0.40 -2.85 -0.16- 0.00 0.00 0.00 8 0.57 -3.16 -0.07 0.00 0.00 0.00 10 0.01 24.14 0.72 0.00 0.00 0.00• 11 0.01 13.08 3.58 0.00 0.00 .0.00 12 -0.29 15.97 0.42 0.00 0.00 0.00 13 0.44 15.73 0.48 0.00 0.00 0.00 14 0.01 20.91 -1.10 0.00 0.00 0.00 15 0.017 15.31 2.18 0.00 0.00 0.00 1 0.01 18.25 0.50 `0.00 0.00 0.00 17 0.00 17.96 0.58 0.00 0.00 0.00 20 0.01 17.44 4.77 .0.00 0.00 0.00 21 -0.38 21.29 0.56 0.00 0.00 0.00 22 0.58 20.98 0.64 0.00 0.00 0.00 23 0.01 27.87 -1.47 0.00 0.00 0.00 24 0.01 .20.41 2.90 0.00 0:00 0.00 25 0.02 24.34 0.67 0.00 0.00 0.00 " 26 0.00 23.95 0.77 0.00 0.00 0.00' 30 0.00 8.50 4.41. 0.00 0.00 0.00 31 -0.39 12.36 0.20 0.00 0.00 0.00 32 0.58 12.04 0.28 0.00 0.00 0.00 33 0.01 15.40 0.31 0.00 0.00 0.00 34 0.00 15.01 0.41 0.00 0.00 0.00 • 35 0.01 18.94 -1.83 0.00 0.00 0.00 36 0.01 11.47 2.54 0.00 0.00 0.00. sXy/to STAAD SPACE -r PAGE NO. 14 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. '& Const. •SUPPORT REACTIONS -UNIT ----------------- RIPFEET' STRUCTURE TYPE = SPACE ,-JOINT LOAD FORCE-% FORCE -Y FORCE -Z MOM-% MOM -Y MOM Z 29 1 -0.02 0.00 0.00 0.00. 0.00 0.00 2 0.00 0:00 -0.06 0.00 0.00 0.00 3 '0.00 0.89 0.00 0.00 0.00, 0.00 4 0.00 0.00 0.00 0.00 0.00 0.00 5 0.00 0.00 0.00 0.00 0.00 0.00 6 0.00 0:00 0.07 0.00 0.00 0.00 7 -2.21 0.00 0.00 0.00 0.00 0.00 8 1.47 0.00 0.00 0,.00 0.00 0.00 10 0.00 0.89 0.00 0.00 0.00- 0.00 11 0.00 0.67 0.06 0.00' 0.00 0.00 12 -1.66 0.67 0.00 0.00 0.00 0.00 13 1.10 0.67 0.00 0.00 0.00 0.00 14 0.00 0.67• -0.04 0.00 0.00 '0.00 .15 0.00. 0.67 0.04 0.00 - 0.00 0.00 16 -0.01 0.67 0.00 0.00 0.00' 0:00 17 0.01 0.67, 0.00 0.00 0.00 0.00 20 0;00' 0.89 0.08 0.00 0.00 0.00 •21 -2.21 0.89 0.00 0.00 0.00 0.00 22 1.47 0.89 0.00: 0.00 0.00 0.00 23 0.00 0.89 -0.05 0.00 0.00 0.00 • 24 25 0.00 -0.02 0.89 0.89 0.06 0.00 0.00 0.00 0.00 0.00 0.00 0.00 26 0.02 0.89 0.00 0.00 0.00 0.00. 30 .0.00 0.72 0.08 0.00 0.00 0.00 31 -2.21 0.72 0.00 0.00 0.00 0.00 32, 1.47 0.72 0.00 0.00 0..00 0.00 33 -.0.02 0.72 0.00 0.00 0.00_ 0.00 34 0.02 0.72 0.00 0.00 0.00 0.00• 35 0.00 0.72 -0.05 0.00 0.00 0.00 36 0..00 0.72 .0.06 0.00 0.00 0.00 31 1' -0.02 0.00 0.00 0.00 0.00 0.00 2 0.00 0.00 -0.06. 0.00 0.00• 0.00 3 0.00 0.89 0.00 0.00 0.00 0.00 4 0.00 0.00 0.00 0.00 0.00. 0.00 5 0.00 0.00 0.00 0.00 0.0.0 0.00 6 0.00 0.00 0.07 0:00 0.00 0.'00: 7 -1.47 0.00 0.00 0.00 0.00 0.00 8 2.21 0.00 0.00 0.00 0.00 0.00 10 0.00 0.89 0.00. 0.00 0.00 0.00 11 '0.00 0.67 0.06 0.00 0.00 0.00 12 -1.10 0.67 0.00 0.00 0.00 0.00 13 1.66 0.67 0.00 0.00 0.00 0.00 14 0.00 0.67 -0.04 0.00 0.00 - 0.00 15 0.00 0.67 0.04, 0.00 0.00 0.00 16 -0.01 0.67 0.00 0.00 0.00 0._00 17 0.01 0.67 0.00 0.00 0.00 0.00 • 20 0.00 0.89' 0.07 0.00 0.00 0._00 21 -1'.47 0.89 ,0.00 '0.00 0.00 0.00 STAAD SPACE -- PAGE NO. 15 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. - •SUPPORT REACTIONS ----------------- -UNIT RIP FEET STRUCTURE TYPE = SPACE w JOINT LOAD FORCE-% FORCE -Y FORCE -Z MOM-% MOM -Y MOM Z 22 2.21 0.89 0.00 0•.00 0.00 0.00 23 0.00 0.89 -0.06 0.00 0.00 0.00 24 0.00 0.89 0.06 0.00 0.00 0.00 25 -0.02 0.89 0.00 0.00 0.00 0.00 26 0.02 0.89 0:00 0.00 0.00 0.00 30 0.00 0.72 0.07 0.00 0.00 0.00 • 31 -1.47 0.72 0.00 0.00 0.00 0.00 ; 32 2.21 0.72 0.00 0.00 0.00' 0.00 s 33 -0.02 0.72 0.00 0•.00 0.00 0.00 34 0.02 0.72 0.00 0.00 0.00 0.00 ' 35 0.00 0.72 -0.06 0.00 0.00 0.00 36 0.00 0.72• 0.06 0.00 0.00 0.00 ************** END OF LATEST ANALYSIS RESULT ************** 291. LOAD LIST 1 TO 8 20 TO 26 292. PRINT-JOI DIS LIST 3 4 10 11 17 18 24 25 STAAD SPACE -- PAGE NO. 16 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. • JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE ------------------- = SPACE JOINT LOAD %-TRANS Y -TRANS Z -TRANS S-ROTAN Y-ROTAN Z-ROTAN 3 1 0.06890 -0.00007 -0.03060 -0.00004 0.00015 0.00013 2 0.00394 0.00193 0.83013 0.00113 0.00000 -0.00002 3 -0.00394 -0.00850 -0.02226 0.00045 0.00011 0.00001 4 -0.00087 -0.00278 -0.00047 0.00024 -0.00001 0.00000 5. 0.00002 0.00000 -0.00093 0.00008 0.00000 0.00000 6 0.00041 -0.00033 -0.96140 -0.00131 -0.00002 0.00000 7 0.03645 0.00156 -0.02724 -0.00018 0.00063 0.00535 8 -0.03460 0.00169 ' 0.02577 -0.00010 -0.00045 -0.00361 20 -0.00437. -0.01160 -0.98506 -0.00054 0.00008 0.00001 21 0.03167 -0.00971 -0.05091 0.00060 0.00072 0.00536 22 -0.03938 -0.00959 0.00210 0.00067 -0.00035 -0.00360 23 -0.00084 -0.00934 0.80646 0.00191 0.00010 0.00000 24 -0..00872 -0.01320 -0.85379 -0.00036 0.00010 0.00003 25 0.06412 -0.01134 -0.05426" 0.00073 0.00025 0.00014 26 -0.07368 -0.01120 0.00694 0.00082 -0.00006 -0.00012 4 1 0.08850 0.00013 -0.03064 0.00002 0.00001 -0.00075 2 0.00333 -0.00014 0.83065 -0.00049 -0.00003 -0.00015 3 0.01050 •-0.10548 -0.01542 0.00001 0.00001 -0.00054 4 -0.00195 -0.05047 0.00290 0.00000 0.00000 0.00003 5 -0.00017 -0.02021 .0.00054 0.00000 0.00000 0.00001 • 6 7 -0.00149 .0.05435 0.03037 0.02938 .-0.96381 -0.02921 "0.00050 0.00002 0.00001 0.00001 .0.00012 0.00052 8 -0.04993 0.02915 0.02388 -0.00001 -0.00001 -0.00022 20 0.00689 -0.14580 -0.97580 0.00051 0.00001 -0.00039 21 0.06273 -0.14679 -0.04120 0.00002 0.00002 •0.00002 22 -0.04156 -0.14702 0.01188 -0.00001 0.00000 -0.00072 23 0.01170 -0.17631 0.81866 -0.00048 -0.00002 -0.00065 24 0.00504 -0.17602 -0.84264 0.00049 0.00003 -0.00036 25 0.09687 .-0.17603 -0.04264 0.00003 0.00002 -0.00125" 26 -0.08013 -0.17630 0.01865. -0.00001 -0.00001 0.00025 10 1 0.06684 0.00514 -0.00258 0.00000 0.00012 -0.00030 2 0.00393 0.00222 .0.84588 0.00115 0.00000 0.00000 3 -0.00395 -0.00885 -0.00576 0.00082 0.00010 -0.00005 4 -0.00087 -0.00335 -0.00761 0.00055 -0.00001 -0.00002 5 0.00002 0.00000 -0.00247 0.00016 0.00000 0.00000 6 0.00041 0.00014 -0.96803 -0.00153 -0.00001 0.00000 7 0.03431 0.00461 0.00319 -0.00033 0.00011 -0.00014 8 -0.03314 -0.00059 0.00622 -0.00032 -0.00009 0.00016 20 -0.00438 -0.01206 -0.98387 .0.00000 0.00008 -0.00007 21 0.02952 -0.00759 -0.01265 0.00120 0.00020 -0.00021 22 -0.03793 -0.01279 -0.00962 0.00121 0.00000 0.00009 23 -0.00086 -0.00998 0.83004 0.00268 .0.00009 -0.00007 24 -0.00872 -0.01442 -0.86172 0.00038 0.00009 -0.00006 25 0.06205 -0.00705 -0.01842 0.00153 '0.00021 -0.00036 26 -0.07163 -0•.01734 -0.01326 0.00153 -0.00003 0.00023 11 1 0.08696 0.00534 -0.00260- 0.00000 0.00001 -0.00087 • 2 0.00293 '-0.00037 0.84643 -0.00049 -0.00002 -0.00012 3 0.01063 -0.13228 0.00412 0.00000 0.00001 -0.00057 I STAAD SPACE -- PAGE NO. ' 17 *FILE NAME - TEMPORARY COMPRESSOR BUILDING '( ID: Raytheon Eng. & Const. 0 JOINT DISPLACEMENT (INCH RADIANS) JOINT_ LOAD 17 C 24 • 4 5 6 7 8 20 21 22 23 24 25 26 1 2 3 4 5 6 7 8 20 21 22 23 24 25 26 1 2 3. 4 5 6 7 20 21 22 23 24 25 26 1 2 3 4 5 6z STRUCTURE TYPE = SPACE %-TRANS Y -TRANS Z -TRANS %-ROTAN Y-ROTAN Z-ROTAN -0.00197 -0.08383 -0:00117 0.00000 0.00000 0.00003 -0.00018 0.02716, -0.00029 0.00000 0.00000 0.00001 -0.00070 0.05573 -0.97264 0.00049 0:00000 0.00007 0.05101 0.05276 -0.00063 0.00000 0.00001 -0.00067 -0.04774 0.04717 0.00244 .0.00000 -0.00001 0.00060 0.00778 -0.18754 -0.96999 0.00049. 0.00001 0.00046 0.05949 -0.19051 0.00202 0.00000 0.00002 -0.00120 -0.03927 -0.19611 0.00509 0.00000 0.00000 0.00008. 0.01141 -0.24365 0.84908 -0.00049 -0.00002 -0.00065 0.00554 -0.24290 -0.84378 '0.00049 0.00003 -0.00040 0.09544 -0.23793 0.00005 0.00000 0.00002 -0.00139 -0.07849 -0.24861 0.00525. 0.00000 -0.00001 0.00034 0.06526 0.00379 0.01049 `0.00000 0.00012 -0.00028 0.00393. 0.00178 0.85294 0.00116 -0.00001 0'.00000 -0.00395 -0.00974 -0.00210 0.00108 0.00010 -0.00005 -0.00086 -0.00337 0.00788 0.00055 -0.00001 -0.00002 0.00002 0.00000 -0.00249 0.00016 0.00000 0.00000 0.00041 0.00009 -0.96924 -0.00154 0.00000 0.00000 0.03348 0.00009 0.01362 -0.00032 0.00011 -0.00013 -0.03257 0.00397 -0.00341 -0.00033 -0.00009 0.00016 0.00438 -0.01302 -0.98170 0.00026 0.00009 -0.00007 0.02869 -0.01302 0.00115 0.00147 0.00020 -0.00020 -0.03736 -0.00914 -0.01588 0.00147 0.00000 0.00009 -0.00086 -0.01133 0.84047 0.00295 0.00009 -0.00007 -0.00872 -0.01489 0.86541 0.00064 0.00010 -0.00006 0.06048 -0.01690 -0.00198 0.00179 0.00022 -0.00035 -0.07005 -0.00931 -0..02296 0.00179 -0.00003 0.00021 0.08593 -0.00183 6.00969 -0.00001 0.00001 0.00088 0.00260 0.00063 .0.85322 0.00050 •-0.00002 -0.00011. 0.01076 -0.16566 `•0.01045 -0.00008 0.00001 -0.00057 -0.00200 -0.08380 -0.00145 0.00000 0.00000 0.00003 -0.00018 -0.02715 -0.00031 . 0.00000 0.00000 0.00001 -0.00010 0.45580 -0.97387 0.00049 0.00000 0.00003 0.04989 0.04983 0.00919 -0.00001 0.00001 -0.00065 -0.04704 0.05004 -0.00656 0.00001 -0.00001' 0.00059 0.00848 -0.22082 0.96519 0.00041 0.00001 -0.00050 0.05848 -0.22679 0.01786 -0.00009 0.00002 0.00118 0.03845 -0.22658 0.00212 -0.00008 0.00000 0.00005 0.01119 -0.21599 0:86189 -0.00058 -0.00002 -0.00064 0.00599 -0.27725 -0.84454 0.00042 0.00003 -0.00043 0.09452. -0.27845 .0.01837 -0.00009 0.00002 -0.00142 -0.07734 -0.27479 -0.00101 -0.00008 0.00001 0.00035 0.06752 0.00001 0.02322 0.00004 0.00014 0.00013 0.00393 0.00.201 0.86365 0.00118 0.00001 -0'.00001 -0.00394 -0.00951 0.02946 0.00068 0.00011 0.00001 -0.00086 0.00278' -0.00343 0.00024 -0.00001 0.00000 , 0.00002 0.00000 -0.00139 0.00008 0.00000 0.00000 0.00041 -0.00035 -0.96849 -0.00132 0.00000 0.00000 3l# Afif STAAD SPACE -- PAGE NO. 18 *FILE NAME - TEMPORARY COMPRESSOR BUILDING( ID: Raytheon.Eng. & Const. •JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE ------------------ JOINT LOAD %-TRANS Y -TRANS Z -TRANS B-ROTAN_ Y-ROTAN Z-ROTAN 7 0.03494 0.00164 0.02153 0.00010 0.00044 0.00361 8 -0.03471 0.00162 -0.01704 -0.00017 -0.00059 -0.00536 20 -0.00437 -0.01264 -0.94386 -0.00033 0.00010 0.00001 21 0.03017 -0.01065 0.04617 0.00089 0.00054 0.00362 22 -0.03949 -0.01067 0.00759 0.00083 -0.00049 -0.00534 23 -0.00085 -0.01029 0.88829 0.00218 0.00009 0.00000 24 -0.00871 -0.01430 -0.83901 -0.00018 0.00011 0.00003 25 0.06274 -0.01229 0.04786 0.00104 0.00024 0.00015 26 -0.07230 -0.01230 0.00142 0.00096 -0.00004 -0.00012 25 1 0.08469 0.00184 0.02338 -0.00001 0.00001 -0.00065 2 0.00217 -0.00016 0.86418 -0.00051 -0.00002 -0.00009 3 0.01094 0.13062 0.03805 -0.00010 0.00001 -0.00056 4 -0.00203 -0.05047 0.00007 0.00000 0.00000 0.00004 5° -0.00019 -0.02021 0.00007 0.00000 0.00000 0.00001 6 0.00067 0.03030 0.97090 0.00051 0.00000 -0.00001 7 0.04964 0.02783 0.01973 -0.00001 0.00001 0.00027 8 -0.04793 0.03070 0.01909 0.00001 0.00001 -0.00071 20 0.00940 -0.17101 -0.93284 0.00041 0.00001 -0.00053 21 0.05837 -0.17348 0.05779 0.00011 0.00002 -0.00025 22 0.03920 -0.17061 0.01897 -0.00009 0.00000 -0.00122 23 0.01090 -0.20147 0.90224 -0.00061 -0.00002 -0.00061 • 24 0.00656 -0.20115 -0.82612 0.00041 0.00003 0.00043 25 0.09343 -0.20316 . 0.06143 -0.00011 0.00002 -0.00117 26 -0:07596 -0.19947 .0.01468 -0.00009 -0.00001 0.00014 ************** END OF LATEST ANALYSIS RESULT ************** 293. LOAD LIST 1 TO 8 10 TO 17 20 TO 26 30 TO 36 294. *PRINT MEM FOR ALL 295. LOAD LIST 1 TO 8 10 TO 17 296. SECTION 0.0 .25 .5 .75 1.0 MEM 1 TO 26 29 30 297. *PRINT MEM SEC FOR 298. PARAMETERS 299. KZ 1.75 MEM 1 2 5 TO 8 11 TO 14 17 TO 20 23.24 300. SSY 1.0 MEM 1 2 5 TO 8 11 TO 14 17 TO 20 23 24 301. LZ 22.8 MEM 7 8 11 TO 14 17 18 302. LY 22.8 MEM 1 2 19,20 303. LZ 26 MEM 33 34 36 TO 39 41 TO 44 46 47 304. LZ 27 MEM 3 4 9 10 15 16 21 22 305. UNI, 22.67 MEM 1 2 7 8 13 14 19 20 306. LZ 24.1 MEM 25 26 29 30 307. NSF .85 308. RATIO .9 ALL [7 STAAD SPACE -- PAGE NO. 20 *FILE NAME -TEMPORARY COMPRESSOR BUILDING (; ID: Raytheon Eng. & Const. • STAAD-III CODE CHECKING - (AISC) ALL UNITS ARE -KIP FEET (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 1 ST W18 X60, PASS AISC- H1-3 0.362 14 12.84 C 0.00 -26.71 13.00 2 ST W18 X60 PASS AISC- H1-3 0.744 11 14.79 C 0.00 .68.02 10.00 3 ST, W18 X60 PASS AISC-21-3 0.409 15 6.01 C 0.00 73.32 0.00 4 ST W18'%60 PASS AISC- H1-3 0.404 14 .. 5.96 C 0.00 -72.31 13.55 5 ST W18 X60 PASS AISC--Hl-3 0.432 14 16.98-C -0.01 72.31 0.00 6 ST W18'X60 PASS AISC- Hl 3' 0.221 11 10.81 C -0.08 -33:76 0.00 25 ST W12 X26 PASS AISC- H1-3 .0.216 12 0.41 C -0.03 9.93 13.00 26 ST W12 X26 PASS AISC- H1-3 0.193 12 • 27 ST W8X 18 0.22 C PASS 0.03 AISC-.H2-1 -9.92- 0.067 0.00 10 6.51 T 0.00 0.00 0.00 28 ST W8X 18 PASS AISC- H2-1 0.'067 10. 6.51 T 0.00 0.00 0.00 7 ST W18 X60 PASS AISC- H1-3 0.439 11 16.73 C -0.10 41.93 13.00 8 ST -.W18 X60 PASS AISC- H1-3 0.644 15 17.74 C 0.00 66.40 10.00 9 ST W18 X60 PASS AISC- H1-3 0.360 15 2.86 C 0.00 66.41 0.00 10 ST W18 X60 PASS AISC- H1-3 0.361 14 2.87 C .0.00 -66.65 13.55 11 ST W18 X60 PASS AISC- H1-3 6.405 14,' 17.83 C -0.01 66.65 0.00 12 ST W18 X60 PASS AISC- H1-3 0.284` 14 20.13 C -0.11 38.48 •0.00 13 ST W18 X60 PASS AISC- H1-3 0.468 11 17.89 C -0.10 44.65 13.00 14 ST W18 X6.0 PASS AISC- H1-3 0.694 15 19.04 C 0.00 71.66 10.00 15 ST W18 X60 PASS AISC- H1-3 0.386 15 2.68 C 0.00 71.66 0..00 16 ST W18 X60 PASS AISC- H1-3 0.383 14 3.31 C 0.00 -70.58 13.55 17 ST W18 X60 PASS AISC- H1-3 0.428 14 • 18.46 C -0.01 70.58 0.00 I . J4/ ���. STAAD SPACE -- PAGE NO. 21 *FILE NAME..- TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. UNITS ARE - RIP FEET (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/. FX MY M2 LOCATION 18 ST W18 X60 PASS AISC- H1-3 0.296 14 20.24 C -0.11 40.64 0.00 19 ST W18 X60 PASS AISC- H1-3 0.398 14 14.14 C 0.00 -29.22 13.00 20 ST W18 X60 PASS AISC- Hl -1 0.775 15 18.52 C 0.00 78.68 10.00 21 ST W18 X60 PASS AISC- H1-3 0.440 15 6.67 C 0.00 78.68 0.00 22 ST W18 X60 PASS AISC- H1-3 0.449 14 6.70 C 0.00 -80.42• 13.55 23 ST W18 X60 PASS AISC- H1-3 0.477 14 17.97 C -0.01 80.42 0.00 24 ST W18 X60 PASS AISC- H1-3 0.225 11, 11.66 C -0.07 -34.10 0.00 29 ST W12 X26 PASS AISC- H1-3 0.214 13 0.41.0 0.00. -9.93 13.00 30 ST W12 X26 PASS AISC- H1-3 0.191 13 0.22 C 0.00 9.92 0.00 31 ST W8B 18 PASS AISC- H2-1 0.077 10 • 32 ST WSX 18 7.43 T PASS 0.00 AISC- H2-1 0.00 0.077 .0.00 10, 1.43 T 0.00 0.00 0.00 33 ST W10 X22 PASS AISC- H1-3 0.102 10 0.01 C -0.05 2.92 13.00 34 -'ST W10 X22 PASS AISC- H1-3 0.102 10 0.01 C 0.05 -2.92 0.00 35 ST W10 X22. PASS AISC- H1-3 0.020 16 1.85 C 0.00 0.00 0.00 36 ST W10 X22 PASS AISC- H2-1 0.106 10 0.01 T -0.08 2.92 13.00 37 ST W10 X22 "PASS AISC- H2-1 0.106 10, 0.01 T 0.08 -2.92 0.00 38 ST W10 X22 PASS AISC- H2-1 0.133 10 0.06'.T -0.04 3.91 13.00 -39 ST W10 X22 PASS AISC- H2-1 0.133 10 0.06 T 0.04 -3.91 0.00 40 ST W10 X22 PASS AISC- H1-3 0.013 12 1.19 C 0.00 0.00 0.00 41 ST W10 X22 PASS AISC- H1-3 0.232 16 1.93 C -0.06 5.96 13.00 42 ST W10 X22 PASS AISC- H2-1 0:.204 16 0.94 T 0.06 -5.96 0.00 43 ST W10 X22 PASS. AISC- H2-1 0.146 -10 0.01 T -0.03 4.30 13.00 44 ST W10 X22 PASS AISC- H1-3 0.147 10 i • 0.11 C 0.03 -4.30 0.00 STAAD SPACE *FILE NAME - TEMPORARY COMPRESSOR BUILDING -- PAGE NO. 22 ID: Raytheon Eng: & Const. wUNITS ARE - RIP FEET (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 45 ST W10 X22 PASS AISC- H1-3 0.023 16 2.11 C 0.00 0.00 0.00 46 ST W10 X22 PASS AISC- H2-1 0.099 10 0.10 T -0.03 2.92 13.00 47 ST W10. X22 PASS AISC- H2-1 0.099 10 0.10 T 0.03 -2.92 0.00 48 ST W10 X22 PASS SHEAR -Y 0.004 10 0.01 T 0.00 0.00 0.00 49 ST W10 X22 PASS SHEAR -Y 0.004 10 0.03 C 0.00 0.00 0.00 50 ST W10 X22 PASS SHEAR -Y 0.004 10 0.00 0.00 0.00 0.00 51 ST W10 X22 PASS SHEAR -Y 0.004 10 0.01 C 0.00 0.00 0.00 56 T W10 X22 PASS COMPRESSION 0.034 11 0.57 C 0.00 0.00 0.00 57 T W10 X22 PASS TENSION 0.010 11 0.59 T 0.00 0:00 0.00 58 T W10 X22 PASS COMPRESSION 0.017 15 C 0.00 0.00 0.00 •0.35 59 T W10 X22 PASS COMPRESSION 0.141 17 2.36 C 0.00 0.00 0.00 60 T W10 X22 PASS COMPRESSION 0.014 16 0.24 C 0.00 0.00 0.00 61 T W10 X22 PASS COMPRESSION 0.139 17 2.33 C 0.00 0.00 0.00 52 LD L50 355 PASS COMPRESSION 0.218 16 9.08 C 0.00 0.00 0.00 53 LD L40 354 PASS COMPRESSION 0.256 17 7.74 C 0.00 0.00 0.00 54 LD L50 355 PASS COMPRESSION 0.244 16 10.18 C 0.00 0.00 •0.00 55 LD L40 354 PASS COMPRESSION 0.259 17 7.82 C 0.00 0.00 0.00 62 ST W10 X22 PASS SHEAR -Z 0.003 10 0.02 T 0.00 0.00 0.00 63 ST W10 X33 PASS AISC- H1-3 .0.022 12 1.21 C 0.00 0.00 0'.00 64 ST W10 X22 PASS AISC- H1-3 0.013 13 1.15 C 0.00 0.00 •0.00 65. ST W10 X33 PASS AISC- H1-3 0.021 13 1.17 C 0.00 0.00 0.00 311. STEEL TARE OFF 3 /ff lyw �o171 STAAD SPACE -- PAGE NO. 23,E *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng.. & Const. .STEEL TARE-OFF ------------ PROFILE LENGTH(FEET) WEIGHT(RIP ) ST 'W18 %60 292.37 17.475 ; ST W12 %26 48.25 1.254 • ST W8% 18 - 54.00 0.965 ST W10 822 '260.19 5.735 T •W10 %22 110.71 1.220 LD L50 355, 32.80 0.571 LD L40 354 28.28 0.348 • ST W10 %33 52.00 1.7.15 ---------------- TOTAL = 29.28 END OF'DATA FROM INTERNAL STORAGE ************ 312. FINISH- END OF STAAD-III *************** • **** DATE= FEB 27,1998 TIME=. 12:51:23 **** * For, questions on STAAD-III, contact: * Research Engineers, Inc at * Ph.: (714) 974-2500,: Fax: (714) 921-2543 3./� Ae 0 PAGE NO. 1 ID: Raytheon Eng. & Const. * S T A A D- III * Revision 21.0 * Proprietary Program of * Research Engineers, Inc. * Date= FEB 27, 1998 " * ` Time= 13:16:31 * * . * USER ID: Raytheon Eng. & Const. 1. STAAD SPACE 2. *FILE. NAME - TEMPORARY COMPRESSOR BUILDING (TECOMPDA) 3. *SEISMIC DESIGN FILE FOR PDELTA ANALYSIS 4. *WILD GOOSE COMPRESSOR BUILDING 5. *REVISION 0 6. *JAN. 29,198 7. 8. 9. 10. * DESIGNED BY FG 3 y g 11. * CHECKED BY 9� 12. 13. •15. 14. UNIT KIP FT 16. ********** 17. JOI COORD 18. ********** 19. * COLUMN LINE D 20. 1 0 0 0; 2 0 13 0; 3 0 23 0; 4 0 24.125 13.5; 5 0 23 27; 6 0 13 27 21. 7 0 0 27; 29 0 0 13.5; 30 0 13 13.5 22. * COLUMN LINE C 23. 8 26 0 0; 9 26 13 0; 10 26"23.0; 11 26 24.125 13.5; 12 26 23 27 24. 13 26 13 27; 14 26 0 27 25. * COLUMN LINE B 26. 15 36 0 0; 16 36 13 0; 17 36 23 0; 18 36 24.125 13.5; 19-36 23 27 ' 27. 20 36 13 27; 21 36 0 27 28. * COLUMN LINE A 29. 22 62 0 0; 23 62 13 0; 24 62 23 0; 25 62 24.125 13.5; 26 62 23 27' 30. 27 62 13 27; 28 62 0 27; 31 62 0 13.5; 32 62 13 13.5 31. * ROOF PLANE 32. 33 13 23 0; 34 13 24.125 13.5; 35 13 23 27; 36 49 23 0 33. 37 49 24.125.13.5; 38 49 23 27' 34. ********* 35. MEM.INCI 36. ********* 37. * COLUMN LINE D 38. 1 1 2 6; 25 29 30; 26 30 4; 27 2 30; 28 30 6 39. * COLUMN LINE C •40. 7 8 9"12 41. * COLUMN.LINE B 0 ri STAAD SPACE -- PAGE NO. 2 - *FILE.NAME - TEMP ORARY'COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. ` 42. 13 15 16 18 43. * COLUMN LINE A •44. 19 22 23 24; 29 31 32; 30 32 25; 31 2.7 32,;,32 32 23 45. * COLUMN LINE 46. * ROOF PLANE. 47. 33 3 33; 34 33 10; 35 10 17; 36 17 36;"` 37 36 24;38 4 34; 39 34 11 48. 40 11 18; 4118 37;42 37 25; 43 5 35; 44 35 12; 45 12 19; 46 19,38 49. 47 38 26; 48 34 33; 49 35 34; 50 37 36;.51 38.37 50. * ROOF BRACING 51. 56 5 34; 57 34 12; 58 12 18 52. 59 18 38; 60 38. 25;.61 10 18 53. * VERTICAL BRACING AND STRUTS 54.. 52 15 9; 53 17 9; 54 13 21; 55 13 19; 62 16 9; 63 6 13; 64 13 20 ' 55. 65 20 27 56. UNIT•KIP INCH 57. ********** 58. MEMB PROP . 59. ********** 60. * FRAMES 61. 1 TO 24 TA ST W18%60 62. * WIND COLUMNS - OLUMNS63.' 63.' 25 25 26 29 30 TA ST W12S26 64." * STRUTS 65. 27 28'•31 32 48 TO 51 62,64 TA ST,W8B18; 33 TO 47 TA ST W10B22 66. 63 65 TA ST W10%33 - 67. * VERTICAL BRACING 68. 52 54 TA LD L50355 SP .375 •69. 70. 53 55 TA LD L40354 SP .375 * ROOF BRACING 71. 56 TO 61 TA T W10B22 72. ******** 73. MEM REL 74. ******** 75.'* WIND COLUMNS 76. 26 30 END MY MZ -F% 77. * STRUTS 78. 27 28 31.32 START MY MZ; 27 28 31 32 END MY -MZ' 19. 62 TO 65-.'START.MY MZ; 62'TO 65 END MY MZ - 80. 3335.36 38 40 41 43 45"46-48 TO 51 START,MY MZ 8.1. 34 35 37 39 40 42 44 45 47 48* TO 5.1 END MY MZ 82. MEM TRUSS 83.52 T0. 61 84. *********« 85. CONSTANTS 86. ********** 87. E STEEL ALL 88..'POI.STEEL ALL 89. DENSITY STEEL ALL 90. BETA'90'MEM 1 2:5 TO 8 11 TO 14 1.7 TO 20 23 24.62 TO 65 91. ********** 92. SUPPORTS " 93, 94. 1 7 8 14 15 21 22 28 29 31 PINNED ***********,►************* •95. 96. UNIT RIP FT 97. "13 7y STAAD SPACE -- PAGE NO. 3 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. 98. DEFINE UBC LOAD •99. •100. ZONE .3 I 1.0 RW% 8 RWZ 6 S 1.2 101•. SELFWEIGHT y 102. JOI WEI 103. * EAVES STRUT 104. * COL. LINES 1 & 2 105. 3 5 24 26 WEI 5.7; 10,12'17 19 WEI 6.73 106. * PURLINS i 107. * COL. LINES A & D 108'. MEM WEIGHT 109. 311 CON 2.58 3.5; 3 21 CON 2.58 8.17; 3'21 CON 1.55 12.83 110. 4 22 CON 1.55 .67; 4 22 CON 2.58 5.33; 4 22 CON 2.58 10 111. * COL. LINES B & C 112. 9 15 CON 1.8 3.5; 9 15'CON 1.8 8.17; 9 15 CON 1.8 12.83 113. 10 16 CON 1.8 .67; 10 16 CON 1.8 5.33; 10 16 CON 1.8 10 114. * GIRT LOADS 115. 1 2 5 6 19 20 23 24 UNI .084; 7 8 11 12 13 14 17 18 UNI .12 116. * HVAC EQUIP. LOADS 117. 15 21 CON 3 9 118. ***************,►******* 119. LOAD 2 UBC Z DIRECTION (W -E) 120. UBC LOAD Z .75 122. *LOADING 3 DEAD LOAD (DL) 123. ****w******************* 124. SELFWEIGHT Y -.77' •125. * PURLINS ' 126. * COL. LINES A & D 127. MEM LOAD 128. 3 21 CON GY -1.99 3.5; 3 21 CON GY-1.99*, 8.17; 3 21 CON GY -1.19,12.83 129. 4 22 CON GY -1.19 .67; 4 22 CON GY -1.99 5.33; 4 22 CON GY -1:99,10 130. * COL. LINES B & C 131. 9 15 CON GY -1.39 3.5; 9 15'CON GY -1.39 8.17; 9 15 CON GY -1.39'12.83 132. 10 16 CON GY -1.39 .67; 10 16 CON GY -1.39 5.33; 10 16 CON GY -1.39 10 133. * EAVES STRUT 134. * COL. LINES 1 & 2 135. JOI LOAD 136. 3 5 24 26 FY -4.39; 10,12 17 19 FY -5.18 137.'* GIRT LOADS , 138. MEM LOAD 139. 1 2 5 6 19 20.23 24 UNI GY -.063; 7.8 11 12 13 14 17 18 UNI GY -.09 140. * HVAC EQUIP. LOADS 141. MEM LOAD 142. 15 21,CON GY -2.25 9 143. ***************** 144.. PDELTA ANALYSIS ?41.;7 f STAAD SPACE --.PAGE NO. 4 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon'Eng._& Const. P R O B"L E M S T A T I S T I C.S . • ----------------------------------- 'NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS =- 38/ 65/: 10 ORIGINAL/FINAL BAND=WIDTH = 30/ 8,. TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM 19.8 SIZE•OF STIFFNESS MATRIX = 10098 DOUBLE PREC. WORDS REQRD/AVAIL. DISK SPACE _ 12.14/ 1632.2 MB, EXMEM = 25.69 MB '++PROCESSING ELEMENT' STIFFNESS MATRIX. 13:16:32 ++ PROCESSING GLOBAL" STIFFNESS MATRIX. 13:16:32 ++ PROCESSING TRIANGULAR FACTORIZATION. 13:16:32 ++.CALCULATING JOINT'DISPLACEMENTS. 13:16:32.' * * - * CALC/USED PERIOD FOR Z UBC = 0.8236/ 0.8236 "SEC * ;C, C -ALT = 1.7072,, 2.2834; LOAD FACTOR = 0.750 * UBC FACTOR V =,.0.1142 X 151.88 17.34 KIP * * ++ ADJUSTING "DISPLACEMENTS 13:16:32 ++ CALCULATING MEMBER FORCES. 13:16:32 145. 146. 'LOAD LIST 2 • 147..PRINT JOI DIS LIST .3 10 17 24 • STAAD SPACE -- PAGE NO. 5 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( IDs Raytheon Eng. &.Const.• JOINT DISPLACEMENT (INCH'RADIANS) STRUCTURE TYPE = SPACE - 'JOINT LOAD V --TRANS Y -TRANS Z -TRANS %-ROTAN Y-ROTAN Z-ROTAN 3 2 0.00178 -0.00496 0.63798 0.00125 0.00002 0:00001 10 2 0.00178 -0.00492 0.65216 0.00151 ...0.00001 -0.00005 17 2. 0.00158 -0.006'15 0.65292 0.00173 0.00001 0.00005 24 2 0.00159 -0.00570 0.67664 0.00142 0.00002 0:00001 . END OF LATEST ANALYSIS RESULT.************** 149. PARAMETERS 150. ************** 151. KZ 1.75 MEM 1 2 5 TO 8 11 TO;14 17 TO 20,23 24 152. .SSY 1.,0 MEM 1 2 5: TO 8 11 TO 14 17 TO 20 23 24 ' 153. LZ 22.8 MEM.7 8.11 TO 14 17 18 154: LY 22..8 MEM 1 2 19 20 155. LZ 26 MEM 33 34 36 TO 39 41 TO 44 46 47 156. LZ 27 MEM 3 4 9 10 15 16 21 22 157. UNL 22.67 MEM 1 2 7 8 13 14 19 20 158. LZ 24.1 MEM 25 26 29 30 159. NSF .85 0161. 60. RATIO .9 ALL CHECK CODE ALL STAAD SPACE -- PAGE NO. 6 *FILE NAME- TEMPORARY COMPRESSOR BUILDING (, ID: Raytheon Eng. & Const. • 'STAAD-III CODE CHECKING - (AISC) ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 1 ST W18 X60 PASS AISC- H1-3 0.308 2 9.05 C 0.00 -24.78 13.00 2 ST W18 X60 PASS AISC-.H1-3 0.307 2 8.96 C 0.00 24.78 0.00 3 ST` W18 X60 PASS AISC- H1-3 0.11.1 2 1.75 C -0.03 19.64 13.55 4 ST W18 X60 PASS AISC- H1-3 0.329 2 3.90 C 0.00 -59.72 13.55 5 ST W18 X60 PASS AISC- H1-3 0.355 2 13.51 C 0.00 59.72 0.00 6 ST W18 X60 PASS AISC- H1-3 0.151 2 15.03 C -0.08 16.85 .0.00 25 ST W12 X26 PASS AISC- H1-3 0.051- 2 •0.41 C 0.55 -0.01 13.00 ,26 ST W12 X26 PASS AISC- H1-3 0.048 2 • 27 3T W8X 18 0.22 C PASS -0.55 AISC- H2-1 0.01 0.030 0.00 2 2.86 T 0.00 0.00 0.00 28 ST Wax 18 PASS AISC- H2-1 0.032 2 3.12 T 0.00_ 0.00 0.00 7 ST W18 X60 PASS AISC- H1-3 0.149 .2 8.67 C -0.07 -12.66 13.00 8 ST W18 X60 PASS AISC- H1-3 0.212 2 7.80 C 0.00 -21.07 10.00 9 ST W18 X60 PASS AISC- H1-3 0.128 2 0.32"C -0.03 24.00 13.55 10 ST W18 X60 PASS AISC- H1-3 0.290 2' 2.04 C 0.00 -53.76 13.55 11 ST W18 X60 PASS AISC- H1-3 0.324 2 13.50 C 0.00 53.76 0.00 12 ST W18 X60 PASS AISC- H1-3 0.230 2 16.16 C -0.09 31.35 0.00 . 13 ST W18 X60 PASS AISC- H1-3 0.132 2 11.20 C -0.07 -9".57 13.00 14 ST W18 X60 PASS AISC- H1-3 0.172' 2 9.77 C 0.00 -15.73 10.00 15 ST W18 X60 PASS AISC- H1-3 0.162 2 0.17 C -0.03 30:69 13.55' 16 ST W18 X60 PASS AISC- H1-3 0.313 2 2.18 C 0.00 -58.03 13.55- 17 ST W18 X60 PASS AISC- H1-3 0.348 2 • 13.97 C 0.00 58.03 0.00 STAAD SPACE --.PAGE NO. 7 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng.'& Const. UNITS -ARE - RIP FEET (UNLESS OTHERWISE NOTED) MEMBER TABLE. RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 18' ST W18 X60 PASS AISC- H1-3 0.241 `2 15.73 C -0.09 33.71 0.00 19 ST W18 X60 PASS AISC-'H1-3 0.336 2 10.42 C 0.00 -26.40 13.00 20 ST W18 X60 PASS AISC- H1-3 0.335 2 10.33 C 0.00 26.40 ".0.00 21 ST W18 X60 PASS AISC- H1-3 0.135 2 2.28 C -0..03 23.77 13.55 22 ST W18 X66 PASS AISC- H1-3. 0.368 2 4:84 C 0.00' -66.43 13.55 23 ST W18 X60 PASS- AISC-`H1-3. 0.392 2 14.37 C 0.00 66.44 0.00 24 ST W18 X60 PASS AISC- H1-3 0.154 2 15.89 C -0.09 16.67 0.00 29 ST W12 X26 PASS AISC- H1-3 0.053 2 *ST. 0.41 C '0.58 -0.01 13.00 30 W12 X26 PASS AISC- H1-3 0.050 2 0.22 C -0.58- 0.01 0:00 31 ST .W8X 18 PASS _AISC- H2-1 0.040 2 • 32 ST W8X 18 3.83 T PASS 0.00 AISC= H2-1 0.00 0.036 0.00 2 3.50 T 0.00 0.00 0.00 33 ST W10 X22 PASS AISC- H1-3 0.073' 2. 0.00 C -0.05 2.06 13.00- 34 ST W10 X22 PASS AISC- H1-3 0.073' 2 0.00 C 0.05 -2.06 0,.00 35 ST W10 X22 PASS. AISC- H1-3 0.003 2. 0.31 C 0.000.00 0.00 36 ST W10 X22 PASS AISC- H2-1 0.071 2 0.00 T -0.03. 2.06 .'13.00 , 37 ST W10 X22 PASS AISC- H2-1 0.071 2 0.00 T •-0.03 --2.06 0.00 38 ST W10 X22 PASS AISC- H2-1 0.122 2 0.00 T -0.03 3.59 13:00 39 ST W10 X22 PASS AISC- H1-3 0.125 2 0.18 C 0.03 -3.59* 0.00 40 ST W10 X22 PASS. SHEAR' -Y 0.002 2 0.17 C 0.00 0.00 0.00 41 ST, W10 X22 • PASS, AISC- H2--1 0.087. 2 0.03 T -0.02 2.57 13.00 , 42 ST W10 X22 PASS AISC- H2-1. 0.087 2 0.03 T 0.02 -2.57 0'.00 43 ST W10 X22 PASS AISC- H2-1 0.069 2 0.18 T -0.02 2.02 - 13.00 `44 ST WlO X22 PASS AISC- H2-1 0.069 2, • 0.18 T 0.02 -2.02 .0.00, STAAD SPACE -- PAGE NO. 8 *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. •.L UNITS ARE - RIP FEET (UNLESS OTHERWISE NOTED) MEMBER- TABLE. RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 45- ST W10 X22 PASS SHEAR -Y 0.002 2 0.10 T 0.00 0.00 0.00 46 ST W10 X22. PASS AISC- H1-3 0.107 2 0.24'C. -0.02 3.04 13.00, 47 ST W10 X22 PASS AISC- H1-3 0.103 2 0.01 C 0.02 -3:04 0.00 48 ST W8X 18 PASS SHEAR -Y 0.003 2 0.04 C 0.00 0.00 0.00 . 49 ST W8X 18 PASS SHEAR -Y 0.003 2 0.03 T 0.00 0.00 0.00 50 ST W8X 18 PASS SHEAR -Y 0.003 2 0.03 C 0.00 0.00 0.00 51 ST W8X 18 PASS SHEAR -Y 0.003 2 0.11 C 0.00 0.00 0.00 56 T W10 X22 PASS COMPRESSION 0.015. •2 0.25 C 0.00 0.00 0.00 57 T W10 X22 PASS TENSION 0.000 2- 0.01 T 0.00 0.00 0.00 58 T W10 X22 PASS TENSION 0.002 2 • 59 T W10 X22 0.15 T PASS 0.00 TENSION 0.00 0.005 0.00 2^ 0.29 T 0.00 0.00 0.00 60 T W10 X22 PASS COMPRESSION 0.004 2 0.06 C 0.00 0.00 0.00 61 T W10 X22 PASS TENSION, 0.009 2 0.51 T 0.00 0.00 0.00` 52 LD L50 355 PASS COMPRESSION 0.015 .2 0.62 C 0.00 0.00 0.00- 53 LD L40 354 PASS TENSION 0.007 2. 0.48` T 0.00 0.00 0.00 54 LD L50 355 PASS TENSION 0.006 .2 0.57 T 0.00 0.00. 0.00 55 LD L40 354 PASS COMPRESSION 0.018 2 0.54 C 0.00 0.00 0.00 62 ST W8X 18 PASS SHEAR -Z 0.002 2 0.01 T 0.00 0.00 0.00 63 ST W10 X33 PASS SHEAR -Z 0.005. 2 0.01 C 0.00 0.00 0.00 64 ST W8X 18 PASS SHEAR -Z 0.002 2 0.03 T 0.00 0.00 0.00• 65 ST W10 X33 PASS SHEAR -Z 0.005. 2 0.01 T 0.00 0.00 0.00 162 -FINISH • *************** END OF STAAD-III *************** **** DATE= FEB 27,1998 TIME= 13:16:32 **** 91/79 * For questions.on STAAD-III, contact: • * 'Research Engineers, Inc at r *- Ph: (714) 974-2500 Fax:. (714) 921-2543 f • a F- r� • • Raytheon Engineers & CALCULATION SET NO, Constructors CALCULATION SUMMARY / , opo - PRELIM. FINAL VOID REVISION & CONTROL SHEET Page 1 of 2 I DISCIPLINE J.O. PROJECT TITLE �.�;f STRUCTURE OR SYSTEM- e.- DESIGN CLASSIFICATION - - SUBJECT Al COMPLETED BY iii✓Tyav ✓ DATE a'�a��!sE CHECKED BY , DATEr CL APPROVED BY DATE DE OR MGR OF STAFF GROUP DISTRIBUTION REASON FOR REVISION: TOTAL NUMBER OF SHEETS IN THIS .......................................................................................................................................................................................................................... ISSUE ...................................................................................................:....................................................................................................................... ' SHEETS REVISED, ADDED OR ............................................:.................................................................................. .....:...................................................................................... ........................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... ........:.................................................................................................................................................................................................................. DELETED PROBLEM STATEMENT: ....................................................................................................................................................................................................................................................................................... ................... S./G.!✓.................... .......�T�ee,./ ' '�........F.. f��' ii✓ .......: S. ��..T.. M......................................................... ..... jv^ii'......... ... 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SUMMARY CONCLUSIONS: ....................................................................................................................................................................................................................................................................................... ST.'vcTl .^........./..45 ........... 7....-�.I...........' . .a......X.............................................................r ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... .................................................................................................................................................................................................................................................:.................:................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... � ' t%Ole .......................... A:\CALC-SUM.DOT • • Raytheon Engineers & Constructors CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2 PROJECT TITLE CALCULATION SET NO. ,5;-, C e �—• --/ PRELIM. FINAL VOID JREVISION DISCIPLINE Z -2,7Z., vo DESIGN BASIS: ........................................... ..L/13G.......f./Q. ............................................................................................................................................................................................... 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UNVERIFIED ASSUMPTIONS/OPEN ITEMS: ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................:.................................................................................................................................................................. REFERENCES: (SPECIFICATIONS; DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) ................................................................................................................................................................................................•---................................................................................... ............................................................................................................................................................................................... .....................................Ll 13G...........1. ��` �.. 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COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) TTn ' REV. NO. 2`,�� REV. DATE PROGRAM TYPE ST•CJvG rEio_�=� RE&C VERIFIED � NO ANALYSIS DESCRIPTION RUN NO. RESULT T.0 /f•/ Gc The attached computer output has been reviewed, the input data checked, and the results approved for release. INPUT CRITERIA L DATE 1 �G CHECKED BY \�'� ; �A'i E _4- a$ RUN BY ,r�.�, �� DATE 1 /� f' APPROVED BY ��- DATE A:\CALC-SUM.DOT �i�CcE //Z' 2 AR le ;c/1s1789' 9 "- - - i EGI379Z-�.3 / ;•.,c °v ......................—G . .............._...... :'i ::i .:'—; -.........................................._......:.....4- . 119X Z1 i 01 D L►//oXze,� w,o�: zz J �............ � � DETi�/c / • �� • � 3 4��� , � �3gti �... El ! r VE7-A1 L 3 . ✓14 �� I F' V ACI ' - Form 5007 (Rev. 9/95) • Rayfhe0e. Engineers & GENERAL" CALCULATION SET NO. e REV. COMP. BY G� CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID %AT•D' ATE PROJECT I/1//l- /j SHEET OF2L57 DATE DATE SUBJECT ry//PG /?l7C1C J.O. 770,�t oa / ry r' , e IAC �G y V - L 3bl l m Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. REV- CO P. BY CHK'D BY 76ATE PRELIM. FINAL VOID DTE -3 /,SGC �f PROJECT I/v/Lli SHEET OF 3 DATE DATE SUBJECT PIPZ' 11/el- /l J.O. 77oSL; ao/ ln/8 Form 5007 (Rev. 9/95) • 0- .10 Form 5007 (Rev. 9/95) " Raytheon Engineers & GENERAL Constructors COMPUTATION CALCULATION SET NO. a -v - REV. COMP. BY CHK'D. BY ,SGT SHEET TE n ATE PRELIM. FINAL VOID PROJECT �A /L /) COO <-e DATE DATE SHEET . 67- OF Z J O 7%OSZ do/ SUBJECT /)//`�� .CTC /c DZWO wr' 9 'SFr ,ewe* s LA/ed 43.PR 11,1 Form 5007 (Rev.9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'q. BY Constructors COMPUTATION 000—/ SHEET PRELIM. FINAL VOID ATE , DATE PROJECT SHEET 6 OF DATE DATE SUBJECT J.O. OD w/,civ SAIIZZoI,✓� o� ,01,Oe USr kw = 4 , o No/,/i31WLvI.eG = .21 �Ey�si w.y .ST'C'�ocT�k� l�rS/��c/�O f�S ,�ONL3�//Gpi,�/G ST•E'r/4TU.C�G-;S 3/oily$ . R41 7 2 5 44' _............................_.......................... ...... _'.-..... .............. ........................ _ _................................................................ 24 •: 2/1Y, i nu nei12 S o , ` 0 d I sl 9Z 52 �3 � �% ` �` � S I �.., �- i J.i �._'_ 17 10 24 21 IDIN •. A �. ildt- Lit. .��". ;' � 1 �i - ... - :�•„ . Z� 9 CLCVI,. iG- Ni User ID: Research Engineers, Inc. PAGE NO. .I 101,26 * S T .A AD I I I *, Revision 22-3a * Proprietary Program"of *. • *. Research Engineers; Inc: * Date= FEB 5, 1998 " Time= 7:25:19 USER ID: Research Engineers, In.c.< . ` * * tF * * * • * * k * * *Ir * *.A * * ** * "* * A it *'* *:* * * * * * ** * * * * * * • * * * * * * - I. STAAD SPACE 2. ' PROJECT WILD GOOSE. 3.- ' FILE PIPE .R 4. ' PIPERACK 5. ' REVISION 0 6. • JANUARY 30, 1998 7. ' REVISION FEB, 5 1998 CHANGE COLUMNS TO W10X22 9. ' NO.IMPACT ON DESIGN 1.0 11 ' DESIGNED BY�� DATE 12: '------------•-- 1.3 1 4 ' CHECKED' BY-. DATE S' 7� IS..s --/----------------- 16. ' 17. UNIT KIP FT 18. JOINT COORD 19. 1 00.00 00.00 00.00 2 24.0 00.00 00.00 3 4.4.0 00.00"00.00 20. 4 00 00 00.00 7.5 5 24.0 00.00 7.5 6 44.0 00.0 7.5 21 7 00.00 15.0 00.00 8 8.0 15.0 0:0 9 16.0 15.0 0.0 22...10 24.0 15.0 0.0- 11 34.•0 15:0 0.,0 12.44.0 1.5.0 0.0 23. 13 00.-00 15.,0 7.5 14 8•.0 "15.0 7.5 15 16.0 15.0 7.5, 24. 16 24.•0 15.0 7.5 17 34.0 15.0 .7 .5 18 44.0 15.0 7.5 25. 20 0.00 7.5 0.00 2.1,0'.00 7._5 7.5 22 24.0 7.5 0.00 26. 23 24.0.7.5 7.5 24 44.0 7.5 .0.00 25 44.0 7.5. 7.5 27. MEMB INC_I 28. 1 1- 2;0 2 20 7 3' 2.22 4 22 10 5 3 24 ; 6 24 12 29. 7 4 2.1 8 21 13 9 5 23' 10 23 16 11 6 25 30. 12 25 18 31 20 7 8 24 25 13 14 29 32. 40 7 13 41 8 14 42, 9 15 43 10 16' 44 11 17 45 1'2 18 33•. 50 13 8 51 8 l5 52 15 1.0 53 10 17 54, 17 12 34. 60.20 21 61 22 23 ; 62 =24 25.; 70 1 10 71.2 7 35..72.4 16 73 5 13 74 4 20 ; 75 20 13 76 5 22. 36. 77 22 16 78 6 24 79 2.4 18, 37. UNIT KIP INCH 38. MEMB PROP 39. ' COLUMNS 40: 1 TO A2 TA ST WIOX22 41 .' BEAMS STAAD SPACE User ID: Research Engineers, Inc: -- PAGE NO. 2 12(! * PROJECT WILD GOOSE 42. 20 TO 29 TA ST WIOX22 43. 40 TO -45 TA ST W8X18 44. * BRACES 45. 50 "TO 54 TA T W8X18 46. 70 TO 73 TA LD L35304 SP .375 • 47. 74 TO 79 TA LD L30304 SP .375 48. 60 TO 62 TA LD L30304"SP .375 49. MEMB RELE 50. 2"0 23 25 28 40 TO 45 START MZ MY 51 22 .24 27 29 40 TO 45 END MZ MY 52. MEMB TRUSS 53. 50 TO 54 70 TO 79 60 61 62 54. CONSTANTS 55. E STEEL ALL 56. POI STEEL ALL 57. DENSITY STEEL ALL 58. SUPPORTS 59. 1 TO 6.FIXED BUT MZ MX 60. UNIT KIP FT 61. LOAD 1 DEAD LOAD 62. SELFWEIGHT Y -1.03 63. * PIPE LOADS 64. MEMB LOAD 65. * MEMB 40 TRIB LENGTH 15' VERTICAL AND 12' HORZ. 66. 40 CON GY -2.64 1.75 67. 40 CON GY -2.64 5.75 " 68. * MEMB 43 TRIB LENGTH 22' HORZ 69. 43 CON GY -2.16 1.75 70. 43 CON GY -2.16 '5.75 71 * MEMB 45 TRIB'LENGTH 15' VERTICAL AND 10' HORZ 72.'45 CON GY -2.45 1.75 73. 45 CON GY -2.45 5.75 74. * ADDITIONAL SMALL BORE PIPE FUTURE 75. 40 TO 45 CON GY -.15 76. LOAD 2 HYDRO LOAD 77. * PIPE LOADS •78. 79. MEMB LOAD • MEMB 40 TRIB LENGTH 15' VERTICAL AND 12' HORZ 80. 40 CON GY -3.37 1.75 81. 40 CON GY -3.37 5.75' 82. * MEMB 43 TRIB LENGTH 22' HORZ 83. 43 CON GY -2•.75 1.75 84. 43 CON GY -2.75 5.75 85. * MEMB 45 TRIB LENGTH 15' VERTICAL AND 10' HORZ 86. 45 CON GY'''-3.13 1 . 75 87. 45 CON GY -3.1315.75 88. LOAD 3 WIND LONG 89. MEMB LOAD 90. * WIND ON COLUMNS 91. 1 TO 12 UNI GX .03 92. * BEAMS. 93.'40 TO 45 UNI GX .046 94. * BRACING 95. 70 TO 79 UNI GX .023 96. * WIND ON PIPES 97. * WIND LOAD 20.9PSF TRIB LENGTH 15FT PIPE DIA 20 INCHES 12(! User 1D; Research Engineers, Inc. STAAD SPACE PAGE NO. 3 • PROJECT WILD GOOSE 98."40 45 CON GX .525 1.75 //�� "40 45 CON GX .525 5.75 100. LOAD 4 WIND LATERAL 101. MEMB LOAD * WIND ON"COLUMNS •102. 103. 1 TO 12 UNI GZ .046. 104. * BEAMS 105. 20 TO 29 UNI GZ .046 106. * BRACING " 107. 70 TO 73 UNI GZ ".023 108". * WIND ON PIPES 109. • WIND ON PIPES 34.9 PLF 110. JOINT LOAD. 111. • JOINTS 7'13 TRIB LENGTH 27FT 112. 7 13 FZ .471 113..* JOINTS 10 16 TRIB LENGTH 22FT 114. 10 16 FZ .384 115. '"JOINTS 12 18 TRIB LENGHT 25FT ` 116. 12 1.8 FZ .436" 117. LOAD 5,SEISMIC LONG X 118. SELFWEIGHT X .21- 21'119. 1 19. * PIPE LOADS 120. MEMB LOAD 121. ' MEMB 40 TRIB LENGTH 15 VERTICAL AND 12' HORZ 122. 40 -CON GX .55 1.75 123. 40 CON GX .55 5.75 124. * MEMB 43 TRIB LENGTH 22' HORZ 125. 43 CON GX .45 1.75 126. 43 CON GX .45 5.75 127. • MEMB 45 TRIB LENGTH 15' VERTICAL AND 10' HORZ 128. 45 CON GX .5Y 1.75 129. 45 CON GX .51 5.75 130. * ADDITIONAL SMALL BORE PIPE FUTURE 131. 40 TO 45 CON GX .031 13.2. LOAD 6 SEISMIC LATERAL Z 133. SELFWEIGHT Z .21 134. • PIPE LOADS •135. MEMB LOAD 136. • MEMB 40 TRIB LENGTH. 1'5' VERTICAL AND 12' HORZ 137. 40 CON GZ .55 1.75 13.8. 40 CON GZ .55 5.75 139. ' MEMB 43 TRIB LENGTH 22' HORZ 140. 43 CON GZ .45 1.75 141. 43 CON GZ .45 5.75 142. • MEMB 45 TRIB LENGTH 15' VERTICAL AND 10' HORZ 143•. 45 CON GZ .51 1.75 144. 45 CON GZ .51 5.75 145. * ADDITIONAL SMALL BORE PIPE FUTURE 146. 40 TO 45 CON GZ .031 147. • LOAD 1 DEAD LOAD 148. • LOAD 2 HYDRO LOAD 149. • LOAD 3 WIND LONG" 150. * LOAD 4 WIND LATERAL 151. * LOAD 5 SEISMIC LONG 152. * LOAD'6 SEISMIC LATERAL - 153". LOAD COMB 10 DL + HDRO User ID: Research Engineers, Inc. STAAD SPACE PAGE NO. 4 s PROJECT WILD GOOSE 1.54: 1 1.0 2 1.0 / 155. LOAD COMB 11 DL + WIND LONG: 156. 1 .75 3 .75 157. LOAD COMB 12 DL + WINFD LATERAL l 75 4 75 •158. 159. LOAD COMB 13 DL + SEISMIC X 160, 1 .75 5 .75 161. LOAD COMB 14 DL + SEISMIC Z 162. 1 .75 6 .75 163. s LOAD COMB FOR DEFLECTION 164. LOAD COMB 15 DL + WIND LONG 165. 1 1.0 3 1.0 166. LOAD COMB 16 DL + WINFD LATERAL 167. l 1.0 4 1:0 168. LOAD COMB 17 DL + SEISMIC X 169. 1 1:0 5 1.0 170. LOAD COMB 18 DL + SEISMIC Z 171. 1 1..0 6 1..0 172. • UPLIFT LOAD COMB 173. LOAD COMB 19.DL + WIND LONG 174. 1 .9 3 1.0 175. LOAD COMB 20 DL + WTND LATERAL 176.'1 .9 4 1.0 177. LOAD COMB 21 DL + SEISMIC X, 1 78.' 1 .9 5 1.0 179. LOAD COMB 22 DL'+ SEISM.,IC Z 180. 1 :9 6 1.0 181. PERFORM ANALYSIS P R O- B L E M S T A T I S T C S ------------------------------------ NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 24/ 46/ 6 ORIGINAL/FINAL BAND -WIDTH = 20/ 7 TOTAL PRIMARY LOAD CASES = 6, TOTAL DEGREES OF FREEDOM 120 • SIZE OF STIFFNESS MATRIX = 4560 DOUBLE PREC. WORDS D REQR/AVAIL. DISK SPACE .= 12:11/ 1593.0 MB, EXMEM = 1960.4 MB ++ Processing Element Stiffness Matrix. 7:25:20 ++ Processing Global Stiffness Matrix°." 7:25:20 ++ Processing Triangular Factorization: 7:25:20 +.+ Calculating Joint Displacements. 7:25:20 ++ Calculating Member" Forces. 7:25;20•. 182. PARAMETERS 183. *COLUMNS 184. LZ 15.0 MEMB 1 TO 12 185. UNL 15.0 MEMB 1 TO 12 186. • BEAMS 187. LZ 24.0 MEMB 20.21 22 25 26"27 188. LZ 20.0 MEMB 23 24 28 29. 189. • BRACES - 190. KZ : 5 MEMB 70, TO 73 191. KY .67-.MEMB 70 'TO 73 192. RATIO .9 ALL User ID: Research Engineers, Inc. STAAD SPACE PAGE NO. 5 ' PROJECT WILD GOOSE - 2 / 916 '193. NSF ..85 MEMB 50 TO 54 70 TO 79 .1, / 194. LOAD.LIST 10 TO 14 195. CHECK CODE ALL / STAAD SPACE ' PROJECT WILD GOOSE .STAAD-III CODE CHECKING - (AISC) User ID: Research Engineers, Inc. PAGE NO. 6 *ALL UNITS ARE - KIP FEET, (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 1 ST WIO X22 PASS AISC-'H1-3 .068 11 1.79 C .01 -1.32 7.50 2 ST W10 X22 PASS AISC- H1-3. 067 11 1.67 C .01 -1.32 .00• 3 ST WIO X22 PASS AISC- HI -3 .084 11 3.45 C ..02 -1.32 7.50 4 ST W10 X22 - PASS AISC- H1-3 .083 11 3.36 C .02 -1.32 .00 5 ST W10 X22 PASS, AISC- H1-3 .074 11, 2.46 C .01 -1.32 7.50 6 ST W10 X22 PASS AISC- H1-3 .073 I1 2.34 C .01 -1.32 .00 7 ST WIO X22 PASS AISC- H1-3 073 12 4.88 C 25 00 7.50 8 ST WIO X22 PASS AISC- H1-3 073 12 4.85 C .25 00 00 9 ST W10 X22 PASS AISC- HI -3 074 12 4.89 C .25 .00 7.50 10 ST WIO X22 PASS AISC- H1-3 073 12 4.86 C 25 00 .00 11 ST W10 X22 PASS AISC- H1-3 066 12 4.10 C 25 .00 7.50 12 ST W10 X22 PASS AISC- HI -3 .066 12 4.08 C 25 .00 .00 • 20 ST WIO X22 .08 PASS T AISC- .21 H2-1 -2.36 081 8.00 12 21 ST WI0 X22 PASS' AISC- H1-3 .088 12 .86 C .21 -2.36 .00. 22 ST W 1 0 X22 PASS AISC- H1-3 083 12 .86 C .21 -2.16 .00 23 ST W10 X22 PASS AISC- H1-3 090 12 .78 C .41 -1.39 10.00 24 ST W10 X22 PASS AISC- H1-3 .090 12 .78 C .41 -I.39 00 25 ST W10 X22 PASS AISC- H2 -I .083 12 1.19 T .21 -2.16 8.00 26 ST W10 X22 PASS AISC- 1-12-1 .088 12 1.19 T .21 -2.36 8.00 27 ST WIO X22 PASS AISC- 1-12-1 .085 12 83 T 21 2.36 .00 28 ST W10 X22 PASS AISC- 1-12-1 092 12" .42 T .41 -1.82. 10.00 0 • User ID: Research Engineers, Inc. STAAD SPACE PAGE NO. 7 " PROJECT WILD GOOSE ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 29 ST W10 X22 PASS AISC- H1-3 .092 12- .00 C .41 -1.82 .00 40 ST W8X 18 PASS SHEAR --Y .228 10 .00 T .00 .00 .00 41 ST W8X 18 PASS SHEAR -Y .005 10 00 C 00 "-.00 00 42 ST W8X 18 PASS SHEAR -Y 065 10 .00 C .00 .00 .00• 43 ST W8X 18 PASS SHEAR -Y .187 10 .00 C .00 .00 .00 44 ST W8X 18 PASS SHEAR -Y .005 10 00 C 00 00 00 45 ST W8X 18 PASS SHEAR -Y 212 f0 01 T 00 .00 00 50 T W8X 18 PASS COMPRESSION .038 12 1.08 C 00 .00 .00 51 T W8X 18 PASS TENSION 004 12 20 T 00 .00 .00 52 T W8X 18 PASS TENSION .014 12 68 T 00 00 .00 53 T W8X 18 PASS TENSION .009 12 45 T 00 00 00 54 T W8X 18 PASS TENSION 020 12 .98 T .00 .00 .00 60 LD L30 304 PASS TENSION .005 12 .33 T. 00 .00 .00 61 LD L30 304 PASS TENSION .005 12 .33 T .00 .00 .00 • 62 LD L30 304 PASS .32 T TENSION .00 .005 .00 12 .00 70 LD L 3 5 304 PASS COMPRESSION 054 10 .83 C .00 00 00. 71 LD L35 304 PASS COMPRESSION .143 11 2.20 C .00 00 .00 72 LD L35 304 PASS COMPRESSION .053 10 .82 C .00 .00 .00 73 LD L 3 5 304 . PASS COMPRESSION 143 ll 2.21 C 00 00 00 74- LD L 3 0 304 PASS. COMPRESSION 186 12 4..28 C 00 00 00 75 LD L30 304 PASS TENSION .062 12 3.29 T 00 00 00 76 LD L30 304 PASS COMPRESSION .194 12 4.46 C .00 00 00 77' LD L30 304 PASS TENSION .0.66 12 3.48 T 00 00 00 • • User ID:-Research Engineers, Inc. STAAD SPACE r-- PAGE NO. 8 • PROJECT WILD GOOSE / Js-` 2s- ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE NOTED) •MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/• LOADING/ ' FX MY MZ LOCATION 78 LD L 3 0 304 PASS COMPRESSION .146, 12 3.35 C .00 00 00 79 LD L30 304 PASS TENSION .045 12 2.•37 T. 00 00 0.0 . 196. SECTION. .25 .5 .7 MEMB I' TO 12 20 TO 29 40 TO 45 197. CHECK CODE ALL ' • User ID`. Research Engineers, Inc. STAAD SPACE PAGE NO. 9 ' PROJECT WILD GOOSE STAAD-III CODE-CHECKING - (AISC) *ALL UNITS ARE - KIP` FEET (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/. 'CRITICAL COND/ RATIO/ LOADING/ FX. 'MY MZ LOCATION r 1 ST W10 X22 PASS AISC- H1-3 066 10 6.90 C 02 00. 5.25 2 ST WIO X22 PASS AISC- H1-3 06.4 10 6.57 C 02 00 1.88• 3 ST W10 X22 PASS AISC- H1-3 075 •11 3.58 C .O1 -1.06 <5.25 4 ST W10 X22 PASS AISC- H1-3 075 11 3.•36 C .01 1.11' 1.88 5 ST W10 X22 PASS AISC- H1-3 065 11 2.58 C .01 -1.06 5.25 - 6 ST W10 X22 PASS AISC- H1-3 .065 11 2.34 C 01 1.11 1.88 7 ST W1:0 X22 PASS AISC- Hl-3 066 10 6.83 C .02 00 5.25 8 ST WIO X22 PASS AISC- H1-3 064 10 ' 6.62 C 02 00 1.88 9 ST W10 X22 PASS AISC- HI-3 060 12 5.02 C -.12, .00 1.88 10 ST W10 X22 PASS AISC-. H1-3 059 12 4.86 C -.13 00 5.2-5 11 ST W10 X22 PASS AISC- H1-3 - 063" 10 6.50 C 02 00 5.25 12 ST W10 X22 PASS AISC- 1-11-3-. .061 10 • 6.29 C .02 .00 1.88 • 20 ST W10 X22 PASS 62 T AISC- H2-1 00 ;.061 2.35 5.60 10 21 ST W10 X22 PAS.S' AISC- H2-1 082 10 63 T 00 -3.21 2.00" 22 ST W10 X22 PASS AISC- H2-1 060 10 63 T 00 -2.29 2.00' 2.3 ST W10 X22 PASS AISC- H1-3 057 12 .78 C -.23 -.91 5.00 24 ST W10 X22 PASS AISC-,HI-3 057 1'2 .78 C -.23 -.91 5.00 25 ST W10 X22. PASS AISC-_H2-1 057..' 12 1.19 T- 09 1.62 5.60 26 ST W10 X22 PASS AISC- H2-1 08.2 10 .63 T .00 -3.21 5.60 27 ST W10 X22 PASS, AISC- H2-1 064 10 62 T 00 -2:49. 2.00 28 ST W 1 0 X22., PASS AISC- H2-1 055 12 ' 42 T 23 -1.12 5.00 STAAD SPACE * PROJECT WILD GOOSE User ID: Research Engineers, Inc. PAGE NO. 10 / ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE NOTED) EMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 29 ST W10 X22 PASS AISC- H1-3 .054 12 .00 C -.23 -1.12 5.00 40 ST W8X 18 PASS AISC- 1-12-1 .399 10 .00 T .00 -10.93 3..75 41 ST W8X 18 PASS AISC- H1-3 .047 11' .00 C .24 -.31 3.75 42 ST W8X 18 PASS AISC- H1-3 .047 11 .00 C .24 -.31 3.75• 43 ST W8X 18 PASS AISC- H1"-3 .329 10 00 C 00 9.00 3.75 44 ST W8X 18 PASS AISC- H1-3 .047 11 .00 C .24 -.31 3.75 45 ST W8X 18 PASS AISC- H2 -l' 372 10 .01 T .00 -10.18 3.75 50 T W8X 18 PASS COMPRESSION' 038 12 1.08 C .00 .00 00 51 T W8X 18 PASS TENSION 004. 12 20 T . .00 00 00 52 T W8X 18 PASS TENSION 014 12 .68 T .00 .00 .00 53 T W8X 18 PASS TENSION, 009 12 .45 T .00 .00 .00 54 T W8X 18 PASS TENSION .020 12 98 T 00 00 00 60 LD L30 304 PASS TENSION .005 12 33 T .00 .00 .00 61 LD L30 304 PASS TENSION .005 12- 233 3 3T 00 00 00 62 LD L30 304 PASS TENSION. .005 12 • .32 T .00 .00 .00 70 LD L 3 5 304 PASS' COMPRESSION 054 10 .83 C .00 .00 .00 71 LD L35 304 PASS COMPRESSION .143 11 2.20 C .00 00 .00 72 LD L35 304 PASS COMPRESSION 053 10 .82 C .00 .00 .00 73 LD L35 304 - PASS COMPRESSION .143 11 2.21 C .00 .00 .00 74 LD' L30 304 PASS COMPRESSION .186 12 4.28 C .00 .00 .00 75 LD L30 304 PASS TENSION .062 12 3.29 T .00 .00 .00 76 LD L30 304 PASS COMPRESSION .194 12 4.46 C .00 .00 .00 77 LD L30 304 PASS TENSION .066 12 3.48 T .00 .00 .00 ul � Ger% User ID: Research Engineers, Inc STAAD.SPACE PAGE NO. 11 PROJECT" WILD GOOSE ALL UNITS ARE KIP FEET (UNLESS OTHERWISE NOTED) EMBER TABLE RESULT/' CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION 78 LD L 3 0 304 PASS COM,PR£SS:ION 146 12 3.35 C .00 .00. 00 7.9 LD L30 304 PASS TENSION .045 12 . 2:37 T 00 00 00' 198. LOAD LIST .15 TO 18 1 199. .PRINT J'O.INT DISPLACEMENTS LIST 7 10 -12 /ir �'Pie • - V User ID: Research Engineers, Inc. STAAD SPACE PAGE NO. 12 ' PROJECT WILD GOOSE 1125- 11125- JOINT DISPLACEMENT (INCH RADIANS). STRUCTURE TYPE = SPACE ----------------- •JOINT LOAD X -TRANS Y -TRANS Z -TRANS X-ROTAN Y-ROTAN Z-ROTAN 7 15 .00999 -.00221 -.00020 .00002 .00000 .00027 16 .00052 -.00003 .03185 .00003 .00000 .00000 17 .00548 -.00269 -.00020 .00002 .00000 .00001 18 -.00012 -.00193 .01365 .00010 00000 .00000 10 15 .01098 -.00434 -.00006 .00004 .00000 .00026 16 -.00060 .00023 .03396 .00005 .00000 .00000 17 .00644 -.00386 -.00008 .00003 .00000 .00001 18 .00003 -.0018-7 .01332 .00009 :0000.0 ..00000 .12 15. .01243 -.00306 -.00020 .00002 .00000 .000.25 16 -.0019.2 -.00048 .02451 -.00001 .00000 .00001 17 .00729 -.00306 -.00019 .00002 .00000 .00.000 18 -.00014 -.0017.9 .01206 00008 .00000 .00000 END OF LATEST ANALYSIS RESULT 200. LOAD LIST 1 TO 6 15 TO 22 201. PRINT SUPPORT REACTIONS • - V STAAD SPACE User ID: Research Engineers, Inc. PAGE NO. 13 ' PROJECT WILD "GOOSE SUPPORT REACTIONS - UNIT:.KIP FEET `STRUCTURE TYPE"- SPACE - O I NT LOAD - FORCE•- X -FORCE-Y' FORCE - Z MOM - X MOM - Y. MOM Z . 1 1 34 4:07 00 00 QO 00 2 29 3.38. 00 00 .-0'0 00 3 -2.60 -2.35 00 00 00 00 4 26 -7.16 :45 .00 00 00 5 1.20 -1'.34 0.0 00 00 00 6 12 3.04 04 00 00 00 . 15 -2.26 1-.72 00 00 0-0 00 l6 .0.9 3.08 45 •.00 00 .. 00 17 85 2.73 00 00 00 00 . P8 22 1 . 03 04 00 00 0.0 19 2.29 1.31 IL 00 00 00 00 2.0 ..05 -3.49_" 45 00 00 00 21 -,.89 2.32 �.00 00 00 00 22 1 8 62 pl)�1, - . 04 00 .'00 00 2 DG 1 NYDPO 2 34 3 94 �aApt- ::"00--" `. 00 00 00• w �G`A - 2 . 29 2 . 74 . 1�1 ti . 00 00 00 00 00 00 00 v .23 7 . 4� �/1�G� - . 4.5 00 00" 00 S L01V,5 -"1 . 12 1 .34 00 00 00 00' 6 13 -2.94 04 :00 00 00 15 2.85 6.29: 00. 00 00 00 16 10 -_3.51. -.45- .00 00 00 17 1.46 5.28: 00 00 :,00 00 18 21 1.01 04 00 00 00 19 -2.82 5'. 89. 00 00 00 00 20 -.07 3.91:. 45 00 00 00 21 -1.42 4.89 00 00 00 00 22 - . 47 61 0.4 00 00 00 3 1 00 3.44 00 0.0 00 00 •• 2 3 00 35 3.13 01. 00 00 00 00 00 00, 00 00. 4 00 -5.39 13 00 .00' 00 . 5 -.05 .00 00 00 00 00 6 .00 -2.65 -.01 .00 00 00 15 35 3.45 00 00 00 00 16 00 =1.95• -.13 00 00 00 17 05 3.44 00 00 00 00 18 00 .79 01 00 00 00 19 -.35 3.]0 00. 00 00 00 20 00 -2.30 13 00 00 00, 21 05 3.10 00 00 00 00 22 00 44' -.01 00 00 00 r. 4 1 34 4.07 00 .00 00 00 2 .29 3.36., 00 00 00 00` 3 2-.60 -2.37 00 .00 00 00 4 21 7.16 -4.46 .00 00 00 . 5 1".20 1.35 00 00 00 00 6- 12 3.04 1.64 00 00 00.. User, ID: Research Engineers, Inc. STAAD SPACE PAGE NO. 14' • PROJECT WI -LD GOOSE SUPPORT REACTIONS' -UNIT KIP FEET STRUCTURE TYPE = SPACE"' ----------------- •JOINT LOAD FORCE -X FORCE -Y FORCE -Z MOM -X MOM -Y MOM Z IS -2.27 .1.7.0 .00 .00 .00 .00 16 54 11.23 -4.46 00 00 00 17 86 2.71 00 00 00 00 18 46 7.11 -i.64 00 00 00 19 -2.30 1.29 00 00 00 00 20 51 10.82 4.46 .00 00 00 21 -.89 2.31 .'00 .00 .00 .00 22 42 6.70 1.64 .00 00 .00 5 l 34 3.95 01 00 00 00 2 -.29 2.76 .00 .00 .00 .00 3. -2.52 2.37 -.01 .00 .00 .00 4 -.19 7.46 -4.62 .00 .00 .00 5 -1.12 1.36 -.01 .00 00. 00 6 - . 1 2 2.94 -1.58 00 00 00 15 -2.86 6.33 -:01 .00 .00. .00 16 - . 5 3 11.41 -4.63 .00 00 .00 17 -1.47 5.31 -.01 .00 .00 .00' 18 -'.47 6.89 -1 .59 .,00 00 00 19 '-2.83 5..93 -.01 00 .00 00 20 -.49 -11.01 -4.63 .00 00 .00 21 =1.43 4.92- - . 0 1 .00 00 .00 22 -.43 6.49• -1.59 .00 .00 .00 6 I .00 3.43 00 00 00 00 2 00 3.13 00 00 00 00 3 -'.35 - . 0 1 00 .00 0,0 .00 4 00 5.39 -3.26 .00. 00 00 5 -.05 .,00 .00 .00 .00 .00 6 .00 2.65 -1.41 00 .00 00 15 35 3.43 00 .00 00. 00 • 16 00 8.82 17 -.OS 3.43 3.26 .00 00 .00 00 .00 00 .00 18 00 6.06 1.41 00 00.. 00 19 35 3.06 .00 .00 00 00 20 00 8.48 -3.26 00 00 00 21 05 3.08 :00 00. 00 00 22 00 5.74 - I . 4 1 00 00 00 **************-END OF LATEST ANALYSIS RESULT ••**•►ss►rrr+r 202. SAVE TEMP3 TEMP4 203. FINISH s►►wrr►►rss++ss END,OF STAAD-III ••+srwr►s►rrrr+ *••' DATE= FEB 5,1998. TIME= 7:25:20 •.*" • rrwr►as►rr►*+rrs►►rrrwwwrrr►►s►rs►r►s►r►rrrsssr+►ssrsss►► *^ For questions on STAAD-I1I, 'contact: Research Engineers, Inc at • West Coast: Ph- (714) 974-2500 Fax- (714) 921-2543 • * East Coast: Ph- (508) 688-3626 Fax- (508) 685-7230 sss*+►wrrrs►•►r►assrsrss►swr+►►�ss►rrrrsar►wr►►r+�rrrss►.♦ Form 5007. (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET CALCULATION SET NO. � -e g "/ REV. COMP. BY GT CHK'D BY 60- DATE PRELIM. FINAL VOID ATE PROJECT SHEET OFw!' DATE :DATE SUBJECT. J.O. . ,77o5Z, do/ /�l�G /%/G Cor✓N�= G Tio.e /. �(jG , 1 ZAl /zw = o .X 13,C�.4Cc S �o To 7.3 j</9T� • " L 0.9 0S .�7.C�E V'G K � .� i'9�L G U � S /G .c/ G-01V1l /4LT/Oi✓ 9')/ L'qr6 e1-?G 21eec=.5 74 ro 7? M,4x Wi.� o Logy 5.. 9S/r t o a'Os "7'er ve rz S/`>AL G >G-s1G.✓ /' • • is User ID: Research Engineers, Inc. PAGE NO. 1 ..*........***..:*...*******...**.*....*..*.*..... 2315 * S T A A D- I I I - * Revision 22.3a * Proprietary"Program of * Research Engineers, Inc. * Date= FEB 4, 19.98 * Time= 12: 9:21 * * USER. ID: Research Engineers, Inc. * 1. STAAD SPACE 2. RESTORE TEMP3 TEMP4 3. * PIPE RACK 4. * STATIC MAX END REACTIONS FOR BRACES 5. * JAN 30, 1998 6. *LOAD COMB 15 DL + WIND LONG 7. *1 l.0 3 1.0 8. *LOAD•COMB 16 DL + WIND LATERAL 9. *1 1.0 4 1.0 10. *LOAD COMB 17 DL + SEISMIC X 11. *1 1.0 5.1.0 12. *LOAD COMB 18 DL + SEISMIC -Z 13. *1 1.0 6 1.0 14. LOAD LIST 15 TO 18 15. PRINT MEMB FORCES LIST `70 TO 79 • is - User ID' Research Engineers, Inc. STAAD SPACE` PAGE NO. 2 . MEMBER END FORCES STRUCTURE TYPE _ SPACE ---------------- ALL UNIT'S ARE -- KIP FEET MEMBER LOAD JT AXIAL SHEAR -Y SHEAR -Z TORSION MOM -Y MOM -Z 70 i5 l.. _-2.12 .30 00 00 00. 00 10 1 7.3 • 30 00 00 00 00 16 1 1.9 13 33 0'0 00 00 10 02 13- 33 00 00 .00 17 1 92 15 00 .00 00 00 10 1.03 IS 00, 00. 00 00 18 1 31' 13 03 00 00 00 10 14 13 03 00 00 00 71 15- 2 2.88 04 00 00, 00 00 7 -2..16 04 00 00 00 00 16 2 21 l3 33 .. 00 00 00 7 04 l3 33 00 00 00 17 2 1:69 1L 00 00' 00 00 7 1...47 11 00 - 00 00 00 18 2 30 13 63 00 00 00 7. 13 13 03 00 00 00 72 15 4 -2.13- 30 00 00 00 00 16 1.74 30 00 00 00 00 16 4 62 13 33 00 00 00 16 46 13 33 00 00 00 17 4, -.93 .15 .00 .00 .00 .00 16 1.04 15 .00 00 00 00 18 4- 54 13 03 00 00 00 16 38 1.3 03 .00 00 00 73 15 5 l3 2.89 -2.17 04 04 00 .00 00 00 00 00 00' 00 16 5 60 13 33 00 .00 .00 1.3 - . 44 1 3 33 00 00 00 17 5 1.70 11 00 00 00 00, 13 l .48 11 00' 00 00 - 0.0 18 5 56 13 03 00 00 00 13 30 13 03 00 00 .00 74_ 15 4 03 04 12 00 00 00. 20 04 04 1'2 00 00 00. 16 4 5.70 04 00 00 00 00 20 -5.62 .04 .00 .00 00 .00 . 17 4 04 04 01 00 00 00 20 04 .04 -.01 .00, :00 .00 18 •4 2.32 03 00 00' .•00 00 20 - -2..23 03 00 00- 0.0 00 STAAD SPACE s User ID: Research Engineers, Inc. PAGE NO. 3 2r MOM -Y MOM -Z 00 MEMBER END FORCES STRUCTURE TYPE = SPACE 00 00 ----------------- ALL UNITS ARE KIP FEET 00 00 00 00 MEMBER LOAD JT AXIAL SHEAR -Y SHEAR -Z TORSION 00 75, 15 20 .05' .04 .12 .00 00 00 00 13 .02 .04 .12 .0'0 00 .00 16 20 4.39 .04 .00 .00 00 .00 00 13 4.47 04 00 00 00 .00 17 20 .05 .04 01 .00 00 00 00 13 .02 .04 .01 .00 00 .00 1.8 20 -2.03 .05 .00 .00 13 2.09 05 .00 .00 76 .15 5 .06 .04 -.12 .00 22 .01 .04 -.12 00 16 5 5.95 .04 .00 .00 22 -5.87 .04 .00 .00 17 5 06. 04 -.01 .00 22 02 .04 01 .00 18 5 2.25 03 .00 00 22 -2.16 .03 .00 .00 77 15 22 .03 04 12 00 _ 16 .04 .04 12 00 16 22 -4.64 .04 .00 .00 16 4.72 .04' .00 .00 17 22 .03 .04 .01 .00 16 04 .04 01 00 18 22 -1.96 .05 .00 .00 16 2.02 .05 .00 .00 78 15 6 24 .04- 04 .04 .04 -.12 12 .00 00 16 6 4.46 .04 .00 .00 24 -4.38 .04 .00 .00 17 6 04 04 01 00 24 .04 .04 -.01 .00 18 6 2.04 .03 .00 .00 24 -1.95 03 00 00 79 15 24 .05 .04 .12 .00 18 02 04. 12 00 16 24 -3.15 .04 .00 .00 18 3.23 04 00 .00 17 24 .05 04 01 .00 18 03 04 .01 00 s User ID: Research Engineers, Inc. PAGE NO. 3 2r MOM -Y MOM -Z 00 .00 00 00 00 00 00 00 00 .00' 00 00 00 00 00 .00 00 00 00 00' 00 .00 00 .00 00 .00 00 .00 00 00 00 00 00 .00 00 00 00 00 00 .00 00 .00 00 00 00 00 00 .00 00 00 00 00 00 00 00 .00 00 00 00 00 00 .00 00 00 00 00 00 00 00 00 00 .00 00 00 3 A %9e a FINAL . CHK'D FILE NO BOOK NO. DESCRIPTION PAGES DATE DESIGN CALCS .. 3.-�........� .............T�MP4�F.�1`:.�01�1PR1*����"J.R.��!!.L<[�INC.�. 9398Q4Q- .......... ..............IVIG..IAU 1 I R. t�I NCATIt�N.......:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.::.:.:.:.:h.: .:.:.:.::.:.MARF A.1:����;�::::::::::::::�G::::::::::::::::�A . X43- .....................ILIO..IIt�>~F.QIfCA'IIJI,...........:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:.:..:.:.:.:.1:.:3:.:.:.:..:.:M1�I�CI�: .........P I tAOK Q J VI A'>`IC�f� ........................................................................................h..�3.:.:.:.::.:.MA2- C':.:.:.:.::::iii A��::::::: :13 1' .......� :::::::::::::::::::::::.::..:.::.: ....... .... E. R.: r-.- PIPS.PI= .. :I :. R.CiIIaAT.O��....................................:.:.:.:.:.:.:.:.:.:.:.:.:...::.:.:.::.4:.:.:.::.:.IV1A :...:.:.:.: • r U 0 RaVlheon Engineers & CALCULATION SET NO. Constructors CALCULATION SUMMARY — T & CONTROL SHEET PRELIM. FINAL VOID REVISION Page I of 2 DISCIPLINE J•o• PROJECT TITLE yV%L,/� G �^� STRUCTURE OR SYSTEM DESIGN CLASSIFICATION SUBJECT.7e COMPLETED BY DATE CHECKED BY �r Ir es DATE APPROVED BY DATE • SDE OR MGR OF STAFF GROUP ` DISTRIBUTION REASON FOR REVISION• TOTAL NUMBER OF SREETS IN THIS ............... ............................................................................................................................................................................................................ ISSUE ........................................................................................................................................................................................................................... • :.......................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... .......................................................................................................................................................................................................................... ........................................................................................................................................................................................................................... SHEETS REVISED, ADDED OR DELETED PROBLEM STATEMENT: .........................................................................................._........................................................................................................................................................................................... .................I...........>TUU..N...J1.fQ..............>co...........7..f-1...........................................: ..................G.4..�!!I,t'R... u SQA............. 64 /.. /.ZV ........ /L/Gc............ 4 o. ..A j...................................................................... `- !1� � i.........P.,........ r ........... e.:lG�r.........4�..........7. .94 .............................................. 4. e1.r.�.........A1............No.......---...C7.. ..................... ........7f ...........% .................................................... ),V .?..AA ...........7�/G.......... ice. ......%:................................................................................................................................................ ....................................................................................................................................................................................................................................................................................... ...........................................................................................................................................................................................................................:........................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... SUMMARY CONCLUSIONS: :........................................................................................ .............................................................................................._............................................................................................... ............ ........... ..............r....'0.....x.....7�.." ~ .... .. . 0 (i�/GS........��`� '............1%A:�N..... � N%tip................... �A/ ....-........(�lJ ...........!'."o"..X.....a�.�.` ��...�`...../.=. ..`......... ........ t .4 ............................... T.!-Jug..........W..... 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AACALC-SUM.DOT • • • Raytheon Engineers & Constructors CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2 PROJECT TITLE CALCULATION SET NO. /3/rv:JJJ — PRELIM. FINAL ✓ VOID REVISION DISCIPLINE DESIGN BASIS: �% G ................................................9................................................................................................................................................................ ..................... :........................................... veI.J Izj................... 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UNVERIFIED ASSUMPTIONS/OPEN ITEMS: ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... .......................................................................................... _........................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) .................................................................................................................................................................................................................................. .................................................L../...�/.�./............... /4�y9�://[.,y.................................................................................................................................................................................... ................................................I..:..v! ...........":�./ V.......L..f................................................................................................................................................................................... .............................................. of e �c� .......- �'�po,'z.................................................................................................................................................................... ..................................... c1'.1.5.7...7.................................................................... ....................................................................................................................................................................................................................................................................................... ..............................................................................................._...................................................................................................................................................................................... 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 RUN BY DATE APPROVED BY DATE A:\CALC•SUM.DOT r Form 5007 (Rev.9/95) ' Ll LJ Raytheon Engineers & GENERAL, CALCULATION SET NO. REV. COMP. Y CHK'D. BY Constructors ..COMPUTATION SHEET PRELIM. FINAL VOID ` ATE DATE PROJECT yy/&Z) 600.5e SHEET C OF -71 DATE DATE SUBJECT ��i%f� C0�7� �L,CL-, ' �f''✓ J.O. 112'M•4i�/ CkNI� 'valini�. DSS/�.� • f. /3- 22 Wi^//� GaC.. ��1in/� DEsi��/ COO Go�I�o2�J'J'o�P 24AIV W?) C6- GCo7 60? ctij'7�4AO S�•rr��oieT ,2�.4cyio�v.r r, .... ...... IA j I.J. .0 7 Ito ILI N-1 7.N • �� i I �rl I i I ! i I I i j I (' � ! x I ! i ! ��I I i. I i i I -X ' I I i I I I. l i I .I. i i t I�. � oI S! ! NA ri ' V I I i ( i I` I I ...I I I I _ i I I �� i �I � i i I I ! I I ( 1 I `� j- • 1� ! Im I� i i � ' ( I I � r i ' i �� �j I �I j i I p' I I I �l L ' I I -71 I i ( 't I I � � I I. .I I � I. .I .. I 0 -q 9 - (. ! '2 :/l, /V T '211 s.6 19 Form 5007 (Rev. 9/95) h Raytheon Engineers & GENERAL CALCULATION SET NO. REV. C j P. CHK'D. BY Constructors COMPUTATION /��/Co OJL� "FG SHEET PRELIM. FINAL VOID ATE DTE PROJECT SHEET / OF �� DATE DATE SUBJECT_7E/1//f� Gotilf? GUSOr(lar J.O. - �EM/�oi<'.�.�' CO,Mf�.�'� S� �`' j3C1xr • oG�i�i.�,�$-�/yr� = ILI 03 Ecc. 3x(07 _ D. 6a-o G ' x y N, _ • R/Gid G�24M� � I IN\ - Gyr o� 6—A X-1 (2eo, 4 /v 4 -50) W /N!9 -E3 Y _ GQo.�! CECT wivr, COLUMn/ ` _, (�.'�'D3 WEA a ci-A>_ VI • �/ h _ x/3.79) C�)� (/5 � f a/ 3.79 _ 66p 3111 795 RAYTHEON FILE:BLDGFT2.MCD PROJECT: WILD GOOSE ENGINEERS & PROJECT NO. 77052.001 CONSTRUCTORS SUBJECT: TEMPORARY BY: 9—'0 DATE: • 3 3 9g COMPRESSOR BUILDING CK: FG DATE: 3�S�g8 PAGE - MAIN BUILDING COLUMNS FOOTING DESIGN D Footing: D1 ;D2,D3, D4- B:= 5.0 -ft D:= 7.0 -ft ! i D 1 :- 1.833 -ft _— I, I D2:= 1.0 -ft D 3:= 2.167 •ft m D4:=D-D1-D2-D3 a, m! , ---..-.._._. D 4 = 2.00 -ft CN_.__. m ; Fththk = 1.5•ft 1 E mb := 5.5 -ft PIER • •P roj ;_ .5,ft \-- GRADE BEAM h'= Emb+Proj P h = 6.00 -ft v P edh = h - Fth thk - ----t- -------................. _...__.._... - ............ _I_. -- °j GRADE m ----- -- ---------- P edh = 4.50 -ft f c := 3.0•ksi REBAR —,.CL ' f y := 60.0•ksi w� y c:= 150•pcf -01 1---- y110•pcf soil �_ � �— F soil := 4000-psf t E mb'y soil - A B F soil = 4605.00 -psf F soil wind F soil1.33 F soil wind = 6124.65 -psf RAYTHEON PROJECT: FILE:BLDGFT2.MCD WILD GOOSE ENGINEERS & PROJECT N0,,77052.001 CONSTRUCTORS BY: X�'e' r _ DATE: . � : 3.. 5a SUBJECT: TEMPORARY COMPRESSOR BUILDING / CK: FG,DATE: 3 /:Fj 78PAGE:. 71 LOADS: ; LOADS FROM STAAD RUN 2/9/98 LOAD COMBINATION 1: MAXIMUM VERTICAL LOAD WIND ✓� Z DOWN NO P 1.:= 26.53•k V 1 := 2.0•k LOAD COMBINATION 2: VERTICALDOWN LOAD WITH SEISMIC P 2:= 44.51 •k V 2':= 2.0•k LOAD COMBINATION 3: VERTICAL DOWN LOAD WITH MAXIMUM SHEAR (wind) ✓T P 3:= 26.22•k V 3:= -5.63•k LOAD COMBINATION 4: MINUMUM VERTICAL DOWN LOAD WITH MAXIMUM SHEAR (wind) , ✓� / �� LG `��� 4 P 4:= 7.66•k t V4 :_ -4.44•k LOAD COMBINATION 5: VERTICL UPLIFT WITH SHEAR (seismic) P5:= -3.25k' V 5:= .76•k WEIGHT OF GRADE BEAM, REFERENCE GRADE BEAM CLACULATIONS W gb := 12.87•k RAYTHEON RA i , n EON FILE:BLDGFT2:MCD. PROJECT: WILD GOOSE ENGINEERS & PROJECT NO. 77052.001 CONSTRUCTORS BY: /.'W ' 9 ' DATE. SUBJECT: TEMPORARY COMPRESSOR BUILDING CK: EG -DATE: ?Z5'195 PAGE: 17/ FOOTING WEIGHT - W cf = B•D•Fth thk•Y c w cf = 7.88 -k ' PIER WEIGHT w pi: B ped•D 3•P edh'1' c w pi = 2.93 -k SOIL WEIGHT s 1 - B • D 1 • CP edh ,- P roj) •Y soil s 1 = 4.03 -k s2:= D3 (B - B .ped' CP edh .- P roj1' soil s 2 = 2.86 -k " s 3:= D"4'0 CP edh - P roj)'Y soil s 3 = 4.40-k. TOTAL DEAD LOAD SOIL CONCRETE Pd =wgb+wcf+wpi+s1+s.2+sg P. d = 34.96 o k RESISTING MOMENTS SOIL, FOOTING, PIER AND GRADE BEAM MOMENTS ABOUT POINT A D4 l Msoil_A:=s1'D1+s2• D1+D2+ 2 +s3'(D- 2 2) 2 M =41.3 �k soil A 0 ft Mconc_A:=wgb D1+D-2 +wcf•p+wpi• D1+D2+D3 M =69.0 k conc A 5 ft RESISTING MOMENTS ABOUT POINT B �11 l Msoil B'=s1.' D- +s2 D4+D3's3'D4 Msoil 6=37.75-kft - 2) 2 2 - Mconc_B:=wgb• D4+D3+"D2 +wcf'D+wpi' D4+D3 2 2 2 Mconc B = 96.65 -k -ft FILE:BLDGFT2.MCD RAYTHEON-'PROJECT: WILD GOOSE PROJECT NO: 7705,2.001 ' ENGINEERS & ,CONSTRUCTORS BY: %911'?a DATE: 3' 9 SUBJECT: TEMPORARY j COMPRESSOR BUILDING CK•C-t DATE 3/5J99 PAGE- ! / 1/ SOIL PRESSURES 2 S x B•D fix 40.83•ft3 6 LOAD COMBINATION 1: t Mott V1•h Mott=12.00-kft note: .66 is the ecc. of the load on the pedestial ' M rl P'1 •[ D 1 + (D 2 + D 3) •.66, + M Soil -A + M conc_A M rl =,214.43 -k-ft D Mrl-Mot1 emax:= —- emax:= emaxl 2 P 1 + P d emax=2.50-in D e excess if (e max ` 2 1 O I e excess = 1.00 OK if eexcess = 1 f :=if e D Pd+P16emax 2 P d + P 1 maxi max�+ sB D D D 3•B ��� - e max) f maxl = 2.07 -ksf D P d + P 1 ( 6•e max f mint if e mar s B .D 11i - D , 0 f min = 1.44 -ksf D 1 ll L B := if�f minl �0, 3'(2 - e max1 ,DJ LB=7.00•ft OK pressure if �f.maxl <F soil 1 �) OK pressure ='1.00 OK if 1.0 fs : = M r1 fs = .17.87 OK if > 2.0 M ot1 A FILE:BLDGFT2.MCD RAYTHEON PROJECT: WILD GOOSE ENGINEERS &PROJECT NO. 77052.001 CONSTRUCTORS BY: )9K'o DATE: f3� SUBJECT:, TEMPORARY I COMPRESSOR BUILDING CK: FG DATE: 3/��9� PAGE' / 71 SOIL PRESSURES LOAD COMBINATION 2: M ot2 := V 2•h M ot2 = 12.00 -k -ft' M r2 :- P 2`[ D 1 + (D2+ D3)-.66] + M soil_A + M conc_A M r2 = 284.97 -k-ft D M r2 - M ot2 e max = e max := a max l 2 P 2 + P d emax =0.78, -in D e excess = if (e max15 2 1,0) a excess = 1.00 OK if eexcess = 1 f if e D Pd+P2 1+6•emax 2 P d + P 2 max2 max 6 B D D D 3•B•(2 - e max) f max2 = 2.40 -ksf D Pd+P2 6'e max f mint if a max -`6 ; B D 1- D )'01 f min2 = 2.14 -ksf _ LB:=if[fmin2:50°3•(2 Demax),D L B = 7.00 -ft OK pressure = if (f max2 <F soil—wind, 1 0) OK pressure = 1.00 OK if 1.0 M fs :_ r2 fs = 23.75 OK if > 2.0 • M ot2 p FILE:BLDGFT2.MCD - RAYTHEON - PROJECT: WILD GOOSE PROJECT NO. 77052.001 ENGINEERS 8 CONSTRUCTORS E BY: /_19ev DATE SUBJECT: TEMPORARY ;COMPRESSOR BUILDING • CK: FCx DATE: 3 f �I S PAGE' 7 SOIL PRESSURES LOAD COMBINATION 3: - j , Mot3 = V 3 • h M ot3 = 33.78 -k -ft Mr3 P 3 [ D 4 + �D 2 + D 3) •.34] + M soil -13+ M conc_B M r3 = 215.07 -k-ft .. D M r3 - M ot3 emax = — - emax a max 2 P 3 + P d emax 6.44 -in e excess = if (e max < D 1 ; 0 e excess- 1.04 \\ / OK if. eexcess - 1 f if D Pd+P3 (1, +.6-emax 2 Pd+P3 maxi e max 5• B D D" 3•B•p (2 - e max) fmaxi = 2.55 -ksf D'Pd+P36•e f`min3 if a maxi_, 1 1 max -I0 6 BD D f min3 = 0.94 -ksf L B if f min350,3•.\D - e max),D.l L `2 / J LB=7.00oft x OK pressure 'if (f max3 <F soil wind, 1'0 OK = 1.00 OK if 1.0 .pressure - . fs:="Mr3 fs=6.37 O.Kif>2.0 M ot3 • A FILE:BLDGFT2.MCD RAYTHEON PROJECT: WILD GOOSE PROJECT NO. 77052.001 ENGINEERS & CONSTRUCTORS BY: 01,21P DATE: SUBJECT: TEMPORARY COMPRESSOR BUILDING CK: F& DATE:3�tt PAGE: SOIL PRESSURES LOAD COMBINATION 4:.. M ot4 1 V4 •h M ot4 = 26.64 -k•ft M r4 := P 4'[ D 4 + (D 2 + D 3) •.34] + M soil_B + M conc_B M r4 = 157.97 ok•ft D M r4 - M ot4 e max = 2- P 4+ P.d a max := e max l e max - 5.03 -in D e excess if (e max `- 2 1 , 0) a excess = 1.00 OK ife.... =1 f if e D P d + P 4. 1+6•emax 2 Pd+P4 max4 max15 6 B D D D 3-B. (2 - e max) • f max4 = 1.66 -ksf D Pd+P4 6•e max f min4 if a max � 6, B D • 1- D f 0 f min4 = 0.78 -ksf L B := iff f min4:50, 3'(2D - e max), D l `) J LB=7.00•ft OK pressure if (f max4 5 F soil_wind ,1 , 0) OK pressure = 1.00 OK if 1.0 fs := M r4 fs = 5.93 OKI > 2.0 M ot4 U RAYTHEON' HEON PROJECT: FILE:BLDGFT2.MCD WILD GOOSE' ENGINEERS & PROJECT NO. 77052.001 CONSTRUCTORS SUBJECT: TEMPORARY BY:. r :, DATE COMPRESSOR BUILDING CK: FG DATE: 3�S19S PAGE: .'1171. SOIL PRESSURES LOAD COMBINATION 5: M.ot5 :: 1 V5 "+ P 5 1.[D 1 + (D 2 + D 3) •.66] M ot5 = 17.31 -k-ft M r5 = M soil A + M conc A M r5 = 110.34 ok•ft D Mr5-Mot5 e max- - e max := a max - 2 p 5+ P d e max = 6.80 -in D e excess = if (e max `2 11,0 a excess _ 1.00 OK if eexcess = 1 k D Pd+PS max 1;2 pd+,PS f if max5 e max � 1+6e 1 • '- 6 . B _ D D / 3' B.(D2- e max) f max5 _ 1.35 -ksf D Pd +'P 5 6'e max f min5 = if 1- 0 a max!5,6' B D D f mins = 0.47 -ksf LB := iff f.min5:50,3. - emaxl,Dl L \ / J LB = 7.00•ft. OK pressure = if (f max5 SF soil _wind, 1, 0) OK pressure = 1.00 OK if 1:0 fs := M r5 fs = 6.37 OK if > 2.0. M ot5 RAYTHEON RAY 1T HEON PROJECT: WILD GOOSE FILE: BLDGFT2.MCD ENGINEERS & " PROJECT NO. 77052.001 CONSTRUCTORS5 SUBJECT: TEMPORARY BY: %jiCS DATE: 3 COMPRESSOR BUILDING CK: F_& DATE•3%S/98PAGE• /0/,7/ ` MAXIMUM BEARING PRESSURE AT POINT A f max, Al = if (f maxl � f max2 , f max2 , f maxl) f max -Al = 2.40 -ksf f max_A = if (f max -Al f max5 f max5 , f max-Al� f max- 'A = 2.40 -ksf REINFORCEMENT FOR MAXIMUM PRESSURE AT A For concrete design use load factor of 1.6 f A:= 1.6.•f max A f A= 3.84 -ksf Moment at face of grade beam D 2 M uA := f A.B.- M uA = 32.23 -k -ft 2 Flexure M uA = 32.23-ft•k d:= Fth thk.- 3.0 -in - 1.0 -in d = 14.00 -in b:= B :=_0.9 guess a:= 0.3 -in Given MuA=� 0.85•f c•b.a•(d - a 2 a:= Find(a) a = 0.20 -in .85•f c •a•b A s . A s..= 0.52 -in As int (total for width) fy: A _ b d 200•(psi) , A 2.80 -int s_min1 �- s_min1 = As int total forwidth ( ) f y 3• f c•(Ib) 2 .. . As min2 _ f in -bd A s _min2 = 2.30 -in y As int (total for width) A s_min3 = if (A s mint > As min2, A's -minl, A s_min2) - 2.80 -in2 A s min3 - A - 4 As A 0.69 -int s_min4 •- • s_min4 = As inz (total for width) 3 A s_regA := if (A s>A s_min3,A s) if CA s_min3<A s_min4,A s_min3,As min4 A s_regA = 0.69 -int As inz (total for width) • 3/ii X98 RAYTHEON HEON FILE: BLDGFT2.MCD PROJECT: WILD GOOSE ENGINEERS & PROJECT N0.77052.001 CONSTRUCTORSBY: SUBJECT: TEMPORARY /gODATE: COMPRESSOR BUILDING CK• FG DATE 3/,S%qg PAGE: AY • REINFORCEMENT FOR MAXIMUM PRESSURE AT B f max -B1 = if (f max3 < f max4 , f max4 , f max3), ; f max 61 = 2.55 -ksf For concrete design use load factor of 1.6 " f B:= 1.6•f max_131 f B = 4.08 -ksf Moment at -face of grade beam CD 3 t D4�2 M uB,'= f B•B• M>uB = 177.29 -k -ft' - 2 Flexure M uB = 177.29 -ft•k d := Fth thk - 3.0 -in - 1.0 -in d =14.00 oin b:= B := 0.9 guess a:= 0.3 -in Given M ue= •0.85 f c•b•a•(d - a `` 2/ a :=' Find(a) a = 1.15 -in .85•f c•a•b A s _ A s = 2.93 oin2 As inz°(total, for width) ' fY 200 • ( Psi)2 A s_minl := b d• A s_minl. = 2.80 -in As inz (total for width) f Y _. 3.4f c•(Ib) . A s_min2 '- f Yin •b•d A s_min2 = 2.30 -int As int (total for width) A s_min3 = if (A s_minl > A s_min2 , A s -min 1 A s_min2) A s_min3 = 2.80 -int A s_mird4 = 3'A s A s_min4 = 3.91 -int As inz (total for width) A s_regB := if(A s>A s min3,A sif (A '�s_min3<A.s min4 A s_min3,A s_min4)) A s_reg6 = 2.93 -int As inz (total for width) A sREQ_TOTAL : = if (A s_regA> A s_regB , A s_regA, A s_regB) A sREQ TOTAL =..2.93 -int As inz (total for width) AsREQ _TOTAL A sREQ= 12 in B A sREQ = 0.59 -int As REQ PER FOOT Fth thk t A s_temp = •0018.1 -ft, A s_temp = 0.19 -in As inz (total for width) 2 - RAYTHFILE:BLDGFT2.MCDEON PROJECT: WILD GOOSE ENGINEERS & PROJECT N0.77052.001 CONSTRUCTORS BY:. �'�� DATE: 3- -39� SUBJECT: TEMPORARY COMPRESSOR BUILDING CK: DATE: 3 PAGE: • • SHEAR CHECK' V uA : = f A.B. (D 1 - d) V uA = 12.78 -k VuB:=fB•B•(D3t-D4-d) VuB=61.27-k V umax := if (V uA> V uB, V uA, V uB) V umax = 61.27 -k �V C : _ .85.2f C • Ib"B d �V C = 78.21 -k in V ok if (V umax< �V C 1 1, 0) . PUNCHING SHEAR V ok = 1.00 OK IF Vok = 1.0 P maxi := if (P 1> P 2,P 1 , P 2) P maxl = 44.51 -k P max2 = if (P 3> P 4, P 3, P 4) P max2 = 26.22 -k P max := if (P maxi >.P max2 P maxi , P max2) P max = 44.51 -k P umax 1.6•P max P umax = 71.22 -k bo:=2•(D2+D3+d)+2•(Bped +d) bo=15.00•ft jfT �V C :_ .85.4 b o•d �V C =469.31 -k in Vok := if (P umax<�V C)1 ,0) Vok'= 1.00 OK IF Vok = 1.0 • r � ' FILE:BLDGFT2.MCD RAYTHEON PROJECT: WILD GOOSE ENGINEERS 8 PROJECT NO. 77052.001 . CONSTRUCTORS SUBJECT: TEMPORARY BY: JgQO DATE: 0. 3. 9 � / COMPRESSOR BUILDING CK: FCG DATE•,3/S�" PAGE 1V71 WIND COLUMNS FOOTING DESIGN Footing: B:= 4.0 -ft D:= 5.0 -ft D 1 := 1.33 -ft D2:= 1.0•ft D 3:= 1.67 -ft D4:= D- D1 - D2- D3 D4 = 1 -00 -ft Fth thk 1.5 -ft B ped := 1.5 -ft E mb := 5.5 -ft Proj:=.5•ft h:=Emb+Proj h = 6.00 -ft P edh h - Fth thk P edh = 4.50 -ft f c := 3.0•ksi f y 60.0•ksi Y c := 150•pcf Y soil 110•pcf F soil 4000•psf+ E mb'Y soil F soil = 4605.00 -psf F soil wind F soil' 1.33 F soil wind = 6124.65 -psf e no m AM -_............ __._........ .�.. 'FILE: BLDGFT2.MCD RAYTHEON' PROJECT: WILD GOOSE PROJECT NO. 77052.001 'ENGINEERS 8� CONSTRUCTORS SUBJECT: TEMPORARY BY: %3�0 DATE: COMPRESSOR BUILDING CK: FG DATE•3/S/?S PAGE: • , LOADS: LOADS FROM STAAD RUN 2/9198 LOAD COMBINATION 1: MAXIMUM VERTICAL DOWN LOAD NO WIND P 1 :=.89-k V 1 := .01 •k E LOAD COMBINATION 2: VERTICAL DOWN LOAD WITH SEISMIC`. P 2 := .89•k. V2:=.01•k • LOAD COMBINATION 3: ' VERTICAL DOWN LOAD WITH MAXIMUM SHEAR (wind) P 3 :_ .89•k ' V 3:= 1.47•k LOAD COMBINATION 4: WINUMUM VERTICAL DOWN LOAD WITH MAXIMUM SHEAR (wind) P 4 := .9•k V4 :_ -2.2•k LOAD COMBINATION 5: VERTICL UPLIFT WITH SHEAR (wind) P 5 := 0•k V 5 0-k LOAD COMBINATION NOT USED FOR WIND COLUMNS • WEIGHT OF GRADE BEAM, REFERENCE GRADE BEAM CLACULATIONS W gb := 9.86•k w � T ,RAYTHEON HEON PROJECT: fILE:BLDGFT2.MCD , WILD GOOSE ENGINEERS & PROJECT NO. 77052.001 CONSTRUCTORS SUBJECT: TEMPORARY BY: PJ�>'� DATE: COMPRESSOR BUILDING CK: Fif-x DATE: 3 9'/1?6 PAGE• 6 FOOTING WEIGHT w cf = B•D•Fth thk•Y c w cf = 4.50 -k PIER WEIGHT w pi . B ped•D 3•P edh'Y c w pi = 1.69 -k SOIL WEIGHT s 1 := B•D 1 (p edh - P roj)•Y soil s 1 = 2.34-k s 2 := D 3•.(B ` B ped)- (P edh - P roj) •Y soil s 2 = 1.84 -k s 3 _ D 4-B (P edh - P roj) •Y soil s 3 = 1.76 �k TOTAL DEAD LOAD SOIL CONCRETE Pd:=wgb+wcf+wpi+s 1 +s2+s3 P.d=21.99-k RESISTING MOMENTS SOIL; FOOTING, PIER AND GRADE BEAM MOMENTS ABOUT POINT A 3 D- D4 ') Msoil_A:=s1•D1 2 +s2.(D1+D2+D2 +s3 \ / � 2 M soil A =15.29-k•ft -Wgb• D1+D2 +wbf•-+wpi• D1+D2+D3 M.conc_A 2 2 .. 2) M 34.165 -ft conc A RESISTING MOMENTS ABOUT POINT B D D33 44 M soilB = s 1 ' D - + s 2' D 4 + + s.3-- M soil- B = 14.40 -k'ft - 2 2 2 D+w M _w D +D +D2 +w D +D-3 conc gb ( 4 3 cf pi • 4 2 2. 2 M conc B 45.61 -k•ft • t Y FILE:BLDGFT2.MCD RAYTHEON PROJECT: WILD GOOSE ENGINEERS & PROJECT N0.77052.001 , CONSTRUCTORS BY: 9,00 DATE:Tb� SUBJECT: TEMPORARY COMPRESSOR BUILDING CK: F-6 DATE:3ZF & PAGE:. /V 171. SOIL PRESSURES S B•D Sx=16.67•ft3 6 LOAD COMBINATION 1: M otl V 1'h M ot1 = 0.06.6k -ft note: .69 is the ecc. of the load on the pedestial M rl :_ P 1 [ D 1 + (D 2 + D 3).•.69]'+ M toil_A + M conc A M rl = 52.76 -k -ft D M rl -. M ot1 e max = 2 e max := a max ) 2. P1+Pd emax =.2.36 -in e' excess = if (e max < D �.1'0 a excess = 1.00 / OK if eexcess = 1 if e D Pd+P1 1+6•emax 2 P d + P 1 f maxi max' B D ( D D 3•B'(2 - e max) f maxi = 1.41 -ksf P + P 6•e f mint = if: emax � D , d 1 1 - max ; FILE:BLDGFT2.MCD RAYTHEON NEON PROJECT: WILD GOOSE ENGINEERS &PROJECT N0.77052:001 CONSTRUCTORS SUBJECT: TEMPORARY BY: h3RO DATE: 3 -3 - 9$ / COMPRESSOR BUILDING CK: DATE: 3h �9BPAGE. �� / 7/ SOIL PRESSURES LOAD COMBINATION 2: M ot2 = V 2•h M of = 0.06 -k -ft M r2 := P 2•1 D 1 + (D 2 + D 3).- 69 1 + M soil A'+ M conc_A M r2 = 52.76 -k -ft D M r2 - M ot2 e max := - - e max := a max 2 P,2+Pd emax =2.36 -in D e excess = if (e max < 2 a excess = 1.00 OK if eexcess ' 1 f:=D Pd+P26•emax P.d+P2 max2' if e + max15- B D ( D l 2 D 3-B. (2 - e maxi1 f max2 = 1.41 -ksf A f mint if emax 6 � B D ' \1,- D 0 f min2 = 0.87 -ksf L B if f f min2 0' 3(� emax) , DI L / L B=.5.00•ft OK pressure = if (f max2 <F soil-wind,.1,0) OK pressure = 1.00 OK if 1.0 fs := M - fs = 879.33 OK if> 2.0 • M ot2 3/�i As RAYTHEON PROJECT: WILD GOOSE FILE:BLDGFT2.MCD ENGINEERS &PROJECT NO. 77052.001 CONSTRUCTORS BY: ��'� DATE: SUBJECT: TEMPORARY COMPRESSOR BUILDING CK: DATE:2�S�9�J PAGE-.- �/�� SOIL PRESSURES LOAD COMBINATION 3: M ot3 V 3'h M ot3 = 8.82 -k -ft M r3 := P 3•1 D 1 + (D 2 + D 3) •.69, + M soil -A + M conc_A M r3 = 52.76 -k•ft D M r3 - M ot3. e max — - e max := a max 2 P3+Pd emax =6.95 -in D e excess = if (e max - 2 1'0 a excess = 1.00 OK if eexcess - 1 f if e D Pd+P3 1+.( 6'emax .,2 Pd+P3 max3 max 6' B• D D D 3'B'(2 - e max) f max3 = 1.94 -ksf D Pd+P3 6'e max f mina if a max � 6 B D (1 - D )'01 f min3 = 0.35 -ksf D ll L B:= iff f min3�0,3'(2 - e max), DI LB=5.00•ft OK pressure = if (f max3 <F soil wind, l , 0) OK pressure = 1.00' OK if 1.0 fs := M r3 fs = 5.98 OK if > 2.0 • M ot3 • • [7 RAYTHEON FILE:BLDGFT2:MCD R/`1 i THEO1�111���� PROJECT: WILD GOOSE PROJECT NO. 77052.001 ENGINEERS & CONSTRUCTORS SUBJECT: TEMPORARY BY: B� DATE: COMPRESSOR BUILDING CK: Fra DATE•�ZSf95PAGE• /117� SOIL PRESSURES LOAD COMBINATION 4: M ot4 :_ V 4 I•h M ot4 = 13.20 -k -ft Mr4:=P4.[D1•+(D2+D3)•.31]+Msoil_B+Mconc_B Mr4=61.95-k•ft D M r4 - M ot4 emax:= 2 - P4+Pd emax:= emaxl emax =4.44 -in D e excess : = if (e max < 2 1'0 a excess = 1.00 OK if eexcess = 1 D Pd+P4 6•e max P d + P 4 f max4 : = if a max �— 1 + , 2 6 B D . D 3•B• /D _ e 1 I\ 2 max) f max4 = 1.65 -ksf D P d+ P 4 6•e.max f min4 := if a maxi 6 B D 1- D , 0 f min4 = 0.64 -ksf LB:=iff fmin4!�0,3•(�-emax),DJ LB=5.00•ft OK pressure = if (f max4 <F soil -Wind, 1 , 0) OK pressure = 1.00 OK if 1.0 fs := M r4 fs = 4.69 OK if> 2.0 M ot4 RAYTHEON PROJECT: WILD GOOSE FILE:BLDGFT2.MCD ENGINEERS 8& PROJECT N0: 77052.001 CONSTRUCTORS SUBJECT: TEMPORARY BY: '� DATE: COMPRESSOR BUILDING CK: DATE:45/1$ PAGE: MAXIMUM BEARING .PRESSURE AT POINT A f max Al = if (f maxl f max2 , f max2 > f maxl) f max_Al = 1.41 -ksf f mak A : = if (f max Al f max3 , f max3 , f max_A1� f max_A = 1.94 -ksf REINFORCEMENT FOR MAXIMUM PRESSURE AT A For concrete design use load factor of 1.6 fA:= 1.6-f max A fA=3.10oksf Moment at face of grade beam D 2 1 M uA := f A•B• M uA = 10.98-k•ft 2, Flexure M.uA = 10:98 -ft•k d := Fth thk - 3.0 -in - 1.0 -in d=14.00 -in a \ b,:= B := 0.9 guess a:= 0.3 -in Given M uA=�.0.85•f C..b a•(d - — I 2 a:= Find(a) a,= 0.09 -in .85.f C.a.b 2 A s :_ A s = 0.171 -in As inz (total for width) fi Y A s_minl = b•d,200f( psi) A, s_minl = 2.24 -int As inz (total for. width) Y 3, f c•(lb) 2 As min2 := b•d A s min2 = 1.84 -in — f Y' in — As int total for width ( ) A s min3 = if (A s_min1' A s_min2 , A s_minl , A s min2) 2 A s mina = 2.24 -in , As min4:= s A s_min4 = 0.23 -int As inz (total for width) 3'A A s_regA = if (A s>A s_min3,A s, if (A s_min3�A s_min4>A s_min3,A s_min4)) • t A 0.23 -in s_regA = As inz (total for width) 0 • • RAYTHEON PROJECT: WILD GOOSE FILE:BLDGFT2.MCD 1 ENGINEERS & PROJECT NO. 77052.001 CONSTRUCTORS' BY: Ns'� DATE: ' 3 g SUBJECT: TEMPORARY COMPRESSOR BUILDING CK: > DATE: J5 '?g PAGE: REINFORCEMENT FOR MAXIMUM PRESSURE AT B For concrete design use load factor of 1.6 f B = .1.6 •f max4 ' f B = 2.64 -ksf Moment at face of grade beam CD3 -t -D4)2 Mug:=fB•B; MSB=37:70-k•ft 2 Flexure M iJB = 37.70 -ft•k d:= Fth thk'- 3.0 -in - 1.0 -in d = 14.00 oin b := B := 0.9 guess a:= 0.3 -in Given M uB=�•0.854 c•b•a•(d - a) 2 a:= Find(a) a= 0.30 -in . .85•f c•a•b A s := 2 A s = 0.60 -in As inz (total for width) f y. A s_minl = b•d• 200.( psi) A s_min1 = 2.24' -int As inz (total for width) Y 3 fc•(Ib)2 A s_min2- b•d -- f in . Y A s_min2 = 1.84 -in As.in2 (total for width) A s_min3 _ if (A s_min1 > A s_min2', A s_minl , A s_min2) A s min3 = 2.24 -int A s_min4 - 4 A '- s A 0.81 -int s_min4 _ As int (total for width) 3' As_regB _ if (A s'A s_min3)A s,if(A s_min3<A s_min4,A s_min3,A s_min4)) A s_regB = 0.81 -int As inz (total for width) A sREQ_TOTAL = if (A s_regA> A s_regB A s_regA, A s_regB) A sREQ_TOTAL =.0.81 -int_ As inz (total for width) A sREQ_TOTAL A sREQ := -12-in B A sREQ = 0.20 -int As REQ PER FOOT - '°` s_temp Fth thk _ 0018.1 •ft"• 2 A s_temp = 0.19 yin ' As in z (total for width) 2 - 3/// /98. ' "YTHEON PROJECT: WILD GOOSE FILE:BLDGFT2.MCD ENGINEERS & PROJECT NO. 77052.001 CONSTRUCTORSBY: SUBJECT: TEMPORARY . &R-0 DATE:. `9t� COMPRESSOR BUILDING CK: DATE3��96 PAGE: ?2I7/ SHEAR CHECK VuA:=fA•B•(D1-d) VuA=2.03-k VuB:=fB•B.(D'3+D4-d) VuB=15,90-k V umax = if (V uA> V uB , V uA, V uB) V umax = 15.90 -k �V C:=,85 -2 f c•Ib. d �V c = 62.57-k in V ok := if (V umax< We 1, 0) V ok = 1..00 OK IF Vok =:1.0 PUNCHING SHEAR P maxi : = if P l > P 2 , P 1, P 2) P maxl = 0.89 -k Pmax2 -, if (P 3> P 4, P 3, P 4) P max2 = 0.90 -k P max : = if (P maxl > P max2, P maxl , P max2) P max = 0.90 -k P.umax �= 1.6•P max P umax = 1.44 -k bo.=2D2+D3�d)+2 CB ped +d) b0=1.3.01 -ft If c•Ib • �V C:= .85.4 •b o•d -�V c = 406.93 -k in Vok := if (P umax< �V C' 1 , 0) Vok = 1.00 OK IF Vok = 1 o p a0- 2 RAY HEON FILE:GRADEBM.MCD 1T PROJECT: WILD GOOSE ENGINEERS 8 PROJECT NO. 77052.001 CONSTRUCTORS SUBJECT: TEMPORARY BY: %� DATE: COMPRESSOR BLDG-71CK: FG DATE:3 •5 ?'b PAGE: 2 b GRADE BEAM b:= 12-in i d:=. 4.5-ft TOP BARS_ GRADE BEAM WEIGHT PER FOOT W b:= b-d•.15• s w b= 0.67 -kif i ft MID BARS ADDITIONAL DEAD LOAD PER FOOTN I TIES -o j QI _- w d:= .05•klf • siding and framing �� w MID BARS TOTAL LOAD PER FOOT wt:=wdtwb wt=.0.72-kIf GRADE BEAM SPAN I .._..__..._ BOTTOM BARS VOID FORM 1:= 26-ft GRADE BEAM REACTION wtI V.- V=9.42-k 2 VU:=1.4•V VU=13.19-k GRADE BEAM MOMENTS positive moment mid span 1.4•w t-I MU:= Mu=85.77-k•ft 8 negative moment at support say 2 span condition reference positive moment CONCRETE f c = 3000 • psi STEEL f y : = 60000-psi RFILE:GRADEBM.MCDAYTHEON PROJECT: WILD GOOSE ENGINEERS &PROJECT N0.77052.001 CONSTRUCTORS SUBJECT: TEMPORARY BY:Sll DATE: COMPRESSOR BLDG CK•. �� DATE: 3/5/ $PAGE: REINFORCEMENT Mu=85.77-k-ft dc:=d-3•in dc=51.00-in b=1.00•ft .9 guess a :_ .3 -in given ' M a g g u=�•.85•f �•b•a�(d � - 21 a:= find (a) a = 0.7381 -in ` / .85•f •a•b CA s :` A s = 0.38 -in 2 f 200 • ( psi ) A` s_min1 �= b•d c• f Y 3• f�•(Ib) A s_min2 f. Y* in -bd c A s min1 = 2.04 -int A s mint = 1.68 -int A s_min3 = if (A s_min1' A s_min2 , A s_min, , A s_min2) A s_min3 - 2.04, -int A s4_min4 3 •A s A soi _min4 = 0.50 n 2 A s_req if (A s' A s_min3 , A S' if (A s min3< A s_min4 , A s_min3 , A s_min4)) A s_req = 0.50 -int USE 246 TOP AND BOTTOM CHECK WEAK AXIS BENDING DUE TO LATERAL EARTH PRESSURE LATERAL ACTIVE EARTH PRESSURE P a:= -o'.k LATERAL EARTH PRESSURE IS O PSF SOIL BALANCED ON EACH 3 SIDE OF THE GRADE WALL d2 W a:= P a w a= 0.00 -kif 2 1.7•wa•I Vul'= 2 Vu1=0.00ok • ' 1.7•wa 12 M ul := 8 M ul = 0.00 -k-ft ` pp�T RA i ` 1 H EON PROJECT: s FILE:GRADEBM.MCD - ' . WILD GOOSE ENGINEERS 8. PROJECT NO. 77052.001. ' CONSTRUCTORS SUBJECT: TEMPORARY BY:: DATE: J COMPRESSOR BLDG CK: FG DATE: 3/S-R•S PAGE ..2 f7 i l �� • REINFORCEMENT FOR LATERAL EARTH PRESSURE M ul = 0.00-k•ft d cl := 10 -in d cl = 10.00 -in b l := d b 1 = 54.00 -in :=.9 guess. a := .3 -in given ; M ul=� •.85•f c•b 1•a• d c1 - a 2) a:= find(a) a = 0.0000 -in .85•f c•a•b 1 2 AS:= As=0.00-in . f- Y As minl b I'd cf 200f( psi) As minl = 1.80 -int Y 3.4f c•(Ib) 2 As min2 = f in .b I"d cl A s_min2 - 1.48 -in Y As min3 if (A s_minl :> A s_min2 ,tA s_minl , A s_min2) - A s min3 = 1.80 -int - 4 2 As min4 - s A s_min4 = 0.00 -in . 3'A As_req _ if (A s' A s_min3 , A s , if (A s_min3� A s_min4 As min3 A s_min4)) , A s_req = if (A i s_req!50•in2,A s_min3,As min3) A s_req = 1.80 -int CHECK LATERAL REINFORCEMENT AT MID SPAN INCLUDE TOP REINF. A sl -req = A s_req - .44•in2 A sl -req = 1.36 -int TRY'247 TOP REINF. = 1.21N2 • 2 t A sl -req = A s_req - -60-in i A sl_req - 1.20-in i RAYTHEON PROJECT: WILD GOOSE ENGINEERS & CONSTRUCTORS SUBJECT: TEMPORARY COMPRESSOR BLDG FILE:GRADEBM.MCD PROJECT NO. 77052.001 , BY: DATE: CK: FCi DATE: .3 S9S PAGE: -/ • SHEAR CHECK V U = 13.19 -k Vii=0.00-k �V C:= 2 -.85 -Vic 1b.d C• b in f = 3.00 -ksi d c = 51.00 -in b =,l 2.00 -in �V c = 56.99 -k .5 •�V c — 28.49 -k �i.�. No t -r yE -Z 9d; -V . i2E,�Ui`2 , USS Vow CHECK TIE SPACING PER ACI CHAPTER 21. • f gl;l /�,8 r� u • • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET W/Lp �a,!fOLS�� = CALCULATION SET NO. �3/�0 '" c: REV. COMP. Y , CHK'D. BY FC' PRELIM. FINAL VOID ATE A E PROJECT SUBJECT,Z6 t [? ��,d!'i�" RL�'f �%,P SHEET27 OF DATE DATE j. 0. k IL if K/NCs r — f C'. 0,oIXC2- J-, 2�0. ' C f. 2 0 Vc 2 ets T32ix (US^ - o IVAL cYN Form 5007 (Rev. 9/95) - Raytheon Engineers & GENERAL CALCULATION SET NO. REV. C MP Y CHK'D. BY Constructors COMPUTATION 2 SHEET PRELIM. FINAL VOID DATE • 2•x•9 s �� PROJECT NZ LQ C?GLLr� SHEET 2�7 OF 7 DATE DATE SUBJECT �L�%/� C��%� %3c-,G2'r w J.O. 770-52.60f • Form 5007 (Rev. 9/95) Raytheon Engineers & , GENERAL. CALCULATION SET NO. REV. COMP. Y CHK'D. BY Constructors COMPUTATION Po�- 2 D I SHEET PRELIM.. FINAL VOID`./g. D T E PROJECT %/� �abSE ( SHEET. lL67 OF -71 DATE' DATE JO SUBJECT %E �f? C °"� f.3L1-k5% . />i� !I .. '�% "� c, • CZ7� ' QiQo� Cr�i4,LL� ''P-�`�I. �t1�1'� '� 7�E C o/�ft.'.•.�c � `:'�' {--rO ,�? s �jvo� 7o C12�.4a��� /.4 �. v /00,-^w/,r �/J.vG� �� / fin o���• %� �i. / �o� V �� oG/G�/yG, Pil- I 1ZPr -3 �CONS�Q1/ W7 qC 72�-.vif? Com'^��s'soQ kZ,--/D = / �40 C� /s A-PP,ev,�. @ ,✓I/i.�J�.4-�s/ ,�.� cl,�.i� -- co�vsir.��,Q JL �- Zq.S,� �5. oX/: 5Y /2. 53 k.- t . Ait, S k F Form 5007 (Rev. 9/95) Raytheon EnglneeIs &. GENERAL CALCULATION SENO. �3 60 C>20 REV. COMP. BY CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID , DATE 2 •/ 0 DATE W/ 1-0 �?aO�S� SHEET�7 30 OF DATE DATE. PROJECT SUBJECT 7F��%� ��yi/� �GZx� %�/� J.O. r 2 4 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP Y CHK'D. BY Constructors COMPUTATION DATE SHEET PRELIM. FINAL VOID' . 2•1o•S is PROJECT—W/4,2 C7422S� / SHEET OF'/ DATE DATE ° SUBJECT 74E?Y, C21� J.O. / fol 75 vz • RE�p� Re DSO?L/ = a 01/ VX /�•-rax = 7�. 5 k . VZ "aX = Scok AOR ,d6o.t'/frit/ CiIS� • � _ ¢S k VX. toy YZ=vA: • 0 • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP.pY CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID DATE 3.-z _'7 DTE a s 9a PROJECT W/ -/,o SHEET 32 OF DATE DATE SUBJECT 7�/j CrJ�'%d J.O. 77O62. 00 C -JR// -?S r C: 9/2 9 y . 7k- -4 45 -51 cH�=�.�. � <�� - � g Foy 13�.��i�_✓� h - 3� 38 X 3 > l2 oR V0 IVVIV 37 1 J Np mss /9�/ r, S c .4G� / / J S/Gn/. � 5' .*vv ------------ ooa Z71 - ----�---,-,- ---„---- - - .. - - -- -- -----. .... �-�� --� -- a -- _.-------- ._ - - - ,r.------�--------- 2 Cp 2 7oG EL Ci8 =0 ., -CO 2-Co 2,- h NTS7o0O0CGP.O �� O�• 0,. /-0,/- O'l N>S 70L -- ---- - — — ------- — -�do� -G _•'- 7OG EG NtS i 7.O . 1 N � I • � -� �- - — -- - - �40-'_. tz -3 5 i --- 44, 0' 11,11C 151,1014-0 -1-- i nl 5- 3 Z of <7cy�2 ,poo�L >.o.c. Equi 6 -- - - /�Ty�_ ¢�S, 6� GS o" — - g - — �� ,_ S ,� — -- 7oc EL (�' -o :-- ---- - - --- - - -• -- t .. - ��G/NO,c���on� _ �L�� ^� 7�iVi�o�_4�F�/ Cor�jP,�c SSo,� _ _ f 3�=�r _. _• � - -._ -- - -- - • Form 5007 (Rev. 9/95) Raytheon Engineers.& GENERAL CALCULATION SET No: REV. COMP, Y CH . BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID ATE DATE PROJECT— IVIC-Q C�O� SHEET�. F / DATE DATE SUBJECT 764/-2 CDl--1%% J.O. 40 J Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. Y CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID DATE 2•�7�98 R 3 s�S • PROJECT /G1;) E' SHEET 5f,,�,37 OF -71 DATE DATE SUBJECTZ'--'4/% - J.o. X7052. Lb/ A D Al J ' J Q1 I 5" 5 5 n -\-�4) 24 -caCUA1) - 1ABRC!9�4 • Gum 5c7 _- I 4 ---------------- ]07 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION*' SHEET PROJECT�DL7/�� CALCULATION SET NO. REV. „ COMP Y ATE z •//• 8.3 CHK'D. BY PRELIM. FINAL VOID DTE 's 8 SHEET 3(p OF ' / • SUBJECT %�i�-O: �-�i1 Lam, J"� ' DATE DATE J.O. 770�;.' •/ Form 5007 (Rev. 9/95) 0 v /L- o -?/ leon • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. MI Y CHK'D. BY Con_ structors COMPUTATION ilrG SHEET PRELIM. FINAL.,+ VOID DATE DA E 2 -� /•q� 3 s 98 PROJECT f�V�Go S 3q DATE DATE SUBJECT %vim ��� �L%�G•U� JO .HEET O -710- G. 7 Pow 7lyp UN/J • • f j • Y . . 3 //i �i8 ' r • O • _ oS�7/off/ �- . � ���/off ,�? ,t�- 71 cri THESE SECTS. n �'S APPLY TO a 0 n TOP 2 LAYERS _ /-2-#4 TIE SETS 0 Q N v m OF TIES a / 0 TOP ' a H G F E� µ _ T.O.CONC. EL. 68'-0" - -- ----- ---- It r 4 ' 2-#-, TOP X 0 L i w o 3- 6 EF ' w 0 CLEAN AND CLEAN AND ROUGHEN SURFACE i c° ROUGHEN SURFACE ° (1/4" AMPLITVDE) - ! (1/4" AMPLITUDE) 2-#7 BOT. 1 I Lo kc) • F3lJTc �G .._FL6?'._.l, _ _ ......._._.A ..-----..... I I •1'• t 1 I 6-♦6 fBtN . i • 0 orm 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET PROJECT W IG b G? DOSS CALCULATION SET NO. /3/o Quo - 2 REV. COMP. BY CHK•D. BY DAT 51q S PRELIM. FINAL VOID DATE 3 Z 9e SHEET OF 'J DATE DATE SUBJECT %!iylP. CeomP. &00 E1 -'h J.O. 7o�j Aj 3 PIMP �_ G n'maol,�'.ec/ by cVe��'1 3//,(/98 1� u r� 'orm 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION 3 SHEET PRELIM. I FINAL VOID 3 DATE7� 3 PATE PROJECT SUBJECT W I 7cM �' ��h�!!� Pl Gl�r� GOA ! SHEET OF %/ DATE DATE J.O.%CJ'. ::)C)/ I .. Aj -Y rp � o n � , N,, n Q. :. . . . . . . ..... F- ,. i Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. 3 REV. CODAF>BY CHK'DBY Constructors COMPUTATION 2 SHEET PRELIM. FINAL VOID: DATE 3..2,98 PAJE 5 9 SHEET 3 OF 7/ DATE DATE PROJECT SUBJECT_ZEMP. Gc7!✓IP. fCJ�rs. ©r�./ J:O.'-7 O7 1-9 )011 Tl m 3E�M .C?Ei.V� • • • Form 5007 (Rev. 9/95) Raytheon Engineers & Constructors GENERAL CALCULATION SET NO. COMPUTATION O O U 2 SHEET I PRELIM. I FINAL I VOID REV. COMP. Y CHK'D. BY l- G DATEi of DAzZE ?-- - _ • %1 by psi PROJECT \1214-2 �� SHEET44 OF -7 DATE DATE J.O. 7 7 05 e .'00 SUBJECT7�/��• rz DA' 0 /3%/.. t''-%.- V' 00 'I f.,9 I ') OF 0CKOu7 O • • i Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET O. REV. P. Ba' CHK'D. BY Constructors COMPUTATION PRELIM. FINAL VOID DATE ^ PATE I SHEET w/Lo <i005 • PROJECT SHEET z� OF -71 DATE DATE SUBJECT7� J.O. %p•:�= 7J Al 8f7A �IJ1—'�a �" • � J � I, v 3 AtAp's L` Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION SHEET PROJECT WILD Ca Q- CALCULATION SET N`O. -3 REV. COMP Y CHcK�D°BY PRELIM. FINAL VOID 2 %98� jDATE�� / SUBJECTCD/✓%i? OF 71 DATE DATE �J-O- .ry,p iP6�/�6�21� Form 5007 (Rev. 9/95) r Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. BY CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID DATE DATE PROJECT in� I Ln CODS SHEET �. OF 7 SUBJECT 7�,/-✓,' CGN%f2 .DATE`. , DATE J.O. 7705Z�I 9O r , , i ^ZZ (1o)- ' 7l Form 5007 (Rev. 9/95) Raytheon"Engineers & GENERAL CALCULATION SET NO: ' REV. COMP Y CHK'D. BY Constructors COMPUTATION ����� '! ' ,1 FCx SHEET PRELIM. FINAL VOID DATE DA E PROJECT SHEET 8. OF DATE DATE SUBJECT J.O. 7 � ! rA -16-IVS W/7i/ • /��.�1 i3E yo.�o � 01 Volo F-a!?i✓I 3A(Ifg .10 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP/ Y CHK'D. BY Constructors COMPUTATION �3/� �` + ` ATED- A T SHEET PRELIM. _ FINAL, VOID PROJECT Fo 4i`/;�J "� SHEET 9 OF �� DATE DATE SUBJECT 7GJt%? . �rJ�%%. %Jl. ���•l�V. J.O. i� #t O / Z, O V Fill n ' � y Form 5007 (Rev. 9/95)' Raytheon Engineers & GENERAL CALCULATION SET NO. REV.` COMP - BY CHK'D. BY Constructors COMPUTATION4)ATE DATE SHEET . PRELIM. FINAL VOID PROJECT YV/U� Gc� SLS SHEET OF,7� DATE DATE SUBJECT 7G�%/� CLWI!^� �J`Lli%%/�I J.O. 4 WNW a a i, rc Form 5007 (Rev. 9/95) Raytheon'Engineers & GENERAL CALCULATION SET NO. REV. )MP - -Y CHK'D. BY Constructors COMPUTATION �37,fa,000 - 2 �� ' SHEEI PRELIM. FINAL VOID DATE DATE PROJECT `o'/ 7" SHEET !) OF / DATE- DATE SUBJECT J.O. 7�Q� . col 70c &7 ! �, f t� rv1 ! y 7o N' g -7 ' ' Form 5007 (Rev. 9/95) n �J • n U Form 5007 (Rev. 9/95) Raiyfheon Engineers & GENERAL CALCULATION SET NO. 2 REV. WY, CHK'D. BY 1=6 Constructors COMPUTATION �3 ��— PRELIM. FINAL VOID DATE s � SHEET DATE �•�•7f3 PROJECT tNILD GLi7SEb SHEET 53 OF, DATE BATE . SUBJECT 7��lP. r'OkIf? FLOG. ji;QA/. J.O. 8 (4)_ 7 �. -70,0 � " N Form 5007 (Rev. 9/95) 3 Are • CONTINUOUS CLOSURE STRIP ROOF CLAOOING CONTINUOUS CLOSURE FLASHING )P OF EAVE _EV. 92.-6- � •Mvun tlN(HItH - z SECTION A06 SCALE 3-.1'-O" iTYPICAL EAS BUILDING GIRT BY OTHERS I I CONTINUOUS GASKET • CONTINUOUS RIDGE FiASHIP, . CONTINUOUS CLOSURE STRII 2 . I - CONT. STEEL • . /ANGLE BY OTHERS I CONTINUOUS CLOSU JRE STRIP 4 e • CONT. RAKE ANOX TOP OF CURB _ _ . ELEV. 68'-0- ;n BUILDING GIRT BY 0' 2 1/2 - TOP OF FLOOR ' ELEV 67'-7-r CONTINUOUS INTERIOR CONCRETE, FOUNDATION 11 3/8- 1•-0- BY OTHERS • VAPOUR TYPICAL BASF 3 SECTION A06 SCALE 3-.1'-0- ,jo��- TOLL -S� — - 15'-6'- P:^ 1/2" ' N SHOP TO -S f 1/4" R7 -AL__ -- NCHOR BOL TS - t 1/16" ROLL R. V. 2 J00/ RF CUSTOMER 4'1500/ RTJ--- . 6'150/ RF 4"900/ RTJ 12 20'-D• 19 OUTLET -� ®, — — �l ELEv. ®_ I4'-4- 118 5/8 ^ ELEV. 0 4.1500/ Rrr 1 1/8. I j -n J18 ti ca H ^ j 19'-3" I ¢ £LEV. 0 22 . I I I 1'-11 9/16" IS' -6" 11 I "NPT £JW LOW POINT ORA IN I Q ELEV. 0 I •2'-01/16- VPT STARTER INLET I 10 34NPT COMPRESSOR OlC MAK£-UP j I ?' j 5 ,r -o' 14 J NPT DISTANCE PIECE DRAIN 1 j I .ELEV. 1PT FUEL GAS INLET 15 1 NPT PACK/NG DRAW 1? I NPI FOR CUSL SUPPLIED HEA MR ------------------------- ' 4.900/Rrr TOLL -S� — 6'. 5" RED P:^ 1/2" ' N \ I I,` -I-' -S f 1/4" R7 -AL__ -- NCHOR BOL TS - t 1/16" .0 CUSTOMER CONNEC77ONS Y2 : fM{ OOOJ1[Mf oo.1`4 PRolwfMf —.TOR .w IT 90AL No' R � on V P.1 Q COT RNR obiQOYi O M ma IMF ■rwri ...of irifp comm/L\ y ■4 K 16 9'- 7' £LEV. 6 13 , ELEV. 0 16'-J- N �Q, r-9 1/8- 0 p, 'K .I THROW /1 j I 4 900/ R y jj 4—SCJ 40 1900 - 1tJOj7 +1 • I I _—'---'— —LLL f l• -IO' Q I 00 11000 I 6'. 5" RED I 4 / r 4-1300 RTJ \ I I,` -I-' 1001 I CUSTOMER CONNEC77ONS ALL CONN£CnONS ARE 1'-4 J/16" B.O.P. ELEV. UNLESS UIHERWfSLr NOffO ------- 5001 RF CUSTOMER INLET 1500 RTJ CUSTOMER OURET 9 1' NPT COMPRESSOR WAFER FILL k DRAIN " 17 / NPf COMPRESSOR OIL DRAIN IPT 1st STAGE SCRUBBER DRAIN 10 1 NPT TAW LOW POINT DRAIN!B 11' 1" NPT SURGE TANK FILL & ORA/N 1 ! I, 1 NPT ENGINE OIL ORAIN !PT 2nd STAG£ SCRUBBER ORA/N 11 I "NPT £JW LOW POINT ORA IN I 19 J 4 NPT ENGINE OIL MAKE-UP VPT STARTER INLET 13 !-NPT DISTANCE PIECE V£Nf 10 34NPT COMPRESSOR OlC MAK£-UP VPT FUEL GAS RfU£F VALVE OU 2£T 14 J NPT DISTANCE PIECE DRAIN 1 21 1 NPT SKID INSTRUMENT AIR SUPPLY 1PT FUEL GAS INLET 15 1 NPT PACK/NG DRAW 1? I NPI FOR CUSL SUPPLIED HEA MR In FUEL CAS FILTER DRAIN 16 J NPT PACK/NG VENT 16 9'- 7' £LEV. 6 13 , ELEV. 0 16'-J- N �Q, r-9 1/8- 0 p, 'K .I THROW /1 j I 4 900/ R y jj 4—SCJ 40 1900 - 1tJOj7 +1 • I I _—'---'— —LLL f l• -IO' Q I 00 11000 I 6'. 5" RED I 4 / r 4-1300 RTJ \ I I,` -I-' 1001 I •A t !> �- * L 3 Eu RI— RtJ 3"1500 m { RT9oo/ i 5 A£ROOVIP 0506' • 1001 I 6'-0 J !6" 100 `; SSR ELL J OJOJ - --- - -' - (� I :Gi $ a I � _z m N SHOP t0 REMOVE EAtSRNC STUB O4 PUMP /NLEr S R£PLA(� W 5•STD CAUCE = - OS PAN JOOJ i J'15O0 Q' (Yr 8 � I Z ' w --r---r-------------------------- 0304 ra'-1. 4100 Q ra'-' �♦ I / RTJ W ?? i FOI I a 2 - g L1 21 • r f K I.S ' Op (�,,, Z - C (p eZ p > O -- -- - .x'501 - - --- .. -- e• v 7/16--•� I r h a CAT PANEL ecG a£N4:coMa,caaeR---- —iisaiia((iso) - - --`'i- -_ _ --- --_-/ENavE r r• r _-�---�-------------------------' L 5AEROWIP G. 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I ALLOT�ED DIMENSIONS ARE F'70M j CL OF DRA W PIPE OR CL OF 8'-0" COOLER BASE 11'-0 9 !6" UNIT ALL ELEVA77ONS ARE FRo?d TO. COOLER I BOTTOM OF SKID. j BASE 29'-10- SKID LENGTH K K REV CERTIFIED Fq c RELEASE FOR FABRICATION rya Dedra .r+a „p Dare art R.R a..eu. e.a wR b e+rt avaw aom u.o a..... .rt - �[ a e.4 A R1AN 2 �, KCI, ' I• NC. v1 4 Dram.. R 6105 W. 681h ST. TULSAOK 14131 o -c ni r W r -Mir 918-446-1801 07771706 0 ✓ie A R O b RYANR£V. SCRUBBER CONTROLS TO EXTERNAL ec r, N CAT£RP/ PLAN KC -0777A 4ZLiUAR 03516 r AR/EL ,XX( -2 7-1-98 FLOAT k ANALOG CHANCES "°°" "0 �', n R,u Ka-LPIWLD GOOSE STORAGE J7-9Vr--06 0 { STAAD SPACE F .*FILE NAME - TEMPORARY COMPRESSOR BUILDING A ! -- PAGE NO. -A! ID:`Raytheon Eng. & Const. SUPPORT REACTIONS -UNIT RIP FEET STRUCTURE TYPE = SPACE ----------------- i • j JOINT LOAD FORCE-% FORCE -Y FORCE -Z MOM-% MOM -Y 1 1 -0.05 0.13. 'r 0.08 2 0.00 -3.57 -2.10 3 0.00 17.44 -0.36 4• 0.00 5.13 j -0.20 5 0.00 0.00 i -0.07- 6 0.00 0.61 3.90 7 -1.26 -2.89 0.19 8 0.86 -3.12 0.05. 10 0.00 22.58 1 -0.64 11 0.00 17.39.;. 2.45 12 -0.95 14.76 -0.34 '13 0.65 14.59 i• -0.44 14. 0.00 14.25 t -2.05 15 0.00 19.61 1.10' 16 -0.04 17.03 -0.42 17 0.04 16.83 --0.54 20 0.00 23.191 3.27 21 -1.26 19.681 -0.45 22 0.86 19.46' -0.58 23 0.00 19.01! -2.74 24 0.00 26.15] 1.46 • 25 -0.05 22.71; -0.56 26 0.05 22.451 -0.71 30 0.00 14.571 3.62 31 -1.26 11.061 -0.10 32 0.86 10.84 -0.23 33 -0.05 14.091 -0.21 34, 0.05 13.821• -0.36 .35 0.00 10:391 -2.39 36 0.00 17.531 -1.81 7 1 0.01 '-0.141 0.08 2 0.00 3.581 -2.10 3 0.01 17.83' 0.44 4 0.00 5.15' 0.19 5 0.00 0.00: 0.07 6 .0.00 -6.68 4.04 7 -0.58 -3.14 --0.04 8 0.39 -2.90 -0.17 10 0.01 22.98 0.70 11 0.01 12.23 3.55 12 -0.42 i 14.87 0.49 13 0.30 15.06 0.40 14 0.01 19.92 -1.05 15 0.01 14.55 2.10 16' 0.01 17.13 0.58 17 0.00 17.34 0.47 20 0.01 16.30 4.74 21 -0.56 19.83 i 0.66 '0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 A. 00 O..00- 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 ., 0.00 0.00 0.00 0.00 _ 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00- 0.00 0.00' 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00. 0.00- 0.00 0.00 0.00' 0.00 0.00 0.00 0.00 0.00 0.00. 0.00 0.00 0.00 0.00 0.00 0.00, 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 '0.00 0.00 0.00 0.00 0.00 0.00 0.00' 0.00 •0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0..00 0.00 0.00 -0.00 0.00 0.00 . 0.00" 0.00 0.00 3/// /o STAAD SPACE -- PAGE NO. JAY, *FILE NAME - TEMPORARY COMPRESSOR BUILDING („ ID: Raytheon Eng.. Const. • SUPPORT -REACTIONS -UNIT RIP FEET. STRUCTURE TYPE = SPACE JOINT LOAD FORCE -B FORCE -Y FORCE -Z MOM-% MOM -Y MOM Z 22 0.40 20.08 0.53 0.00 0.00 0.00' 23 0.01 26.56 ; -1.40 0.00 0.00 0.00 " 24 0.01 19.40 2.80 0.00 0.00 0.00 25 0.02 22.83 0.77 0.00 0.00 0.00 ,26 0.0_0 23.12 0.62_ 0.00 0.00' 0.00 30 0.00 7.59 4.39 0.00 0.00 0.00 31 -0.57 11.12 0.31 0.00 0.00 0.00 32" 0.40 11.37 0.18 0.00, 0.00 0'.00 33 0.01 14.12 0.42. 0.00 0.00 0.00 34 0.00 14.41 0.27 0.00 0.00 0.00 35 0.01 17.85 -1.75 0.00 0.00 0.00 36 0.01 10.68 2.45 0.00 0.00 ' 0.00 8 1 0.01 -16.84 0.01 0.00 0.00 0.00 2 0.00 -4.48 .-2.16 0.00 0.'00 0.00 3 0.01 18.79 0.93 0.00 0.00 0.00 4 0.00 6.18 0.64 0.00 0.00 0.00 5 0.00 0.00 0.19' 0.00 0.00 0.00 6 0.00 -0.30 3.59 0.00 0.00 0.00 7 0.00 -12.20 -0.38 - 0•.00 '0.001 0.00 _ 8 -0.01 4.80 -0.38 0.00 0.00 0.00 10 0.01. 24.97 1.76 0.00 0.00 0.00 • 11 0.01 18.50 4.02 0.00 0.00 .0.00 12 0.01 9.57 1.04 0.00 0.00 0.00 13 0.00 22.33 1.03. 0.00 0.00 0.00 14 0..01 15.37 -0.30 0.00 0.00 0.00, 15 .0.01 .22.08 2,.94 '0.00 0.00 0.00 16° 0.01 6.10 1.33 0.00 0.00 0.00 17 0.00 31.35 1.32 0.00 0.00 0.00 . .20 0.01 24.66 5.35" 0.00'- 0.00 0.00 21 0.01 12.77 1.38 0.00 .0.00- 0.00 22 0.01 29.77 1'.38 0.00 0.00 0.00 23 0.01 20.49 -0.40 0.00 0.00 0.00 24 0.01 29.45 3.92 0.00 0.00 0.00 25. 0.02 8.13 1.77 0.00 0.00 0.00 26 0.00_ 41.80 _ 1.76 _ 0.00 0..00 0.00 30 0.01 14.73 4.34 0.00 0.00 0.00 31 0.01 2.83 0.37 0.00 0.00 0.00 32 0.00 19.83 0.36 0.00 0.00 0.00 " 33 0.01 -1.80 0.75 0.00 0.00 0.00 34 0.00 31.87 0.74 0.00 0.00 0.00 35 0.00 10.55 -1.41 0.00 0.00 0.00 36' 0.01 19.51 2.91 0.00 0.00 0.00 . 14 1 0.01 -18.03 0.01 0.00 0.00 0.00 ' 2 •0.00 4.49 -2.17 0.00 0.00 0.00, 3 0.01 18.47 -0.96 0.00 0.00 0.00 4 0.00 6.24 -0.63 0.00` 0.00 0.00 • 5 0.00 0.00. -0.19 0.00 0.00 0.00 6 0.00 -7.11 5.21 0.00 0.00 0.00 " 31114#8 l° y 03 STAAD SPACE -- PAGE' NO . H *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. SUPPORT REACTIONS -UNIT • - RIP FEET STRUCTURE TYPE = SPACE JOINT LOAD FORCE-%, FORCE -Y FORCE -Z`. MOM-% MOM -Y MOM Z 7 -0.01 -13.52 0.38 0.00 0.00 0.00 8 0.00 6.00 0.37 0.00 0.00 0.00' 10' 0.01 24.71, -1.77 0.00 0.00 0.00 11 0.01 13.20 2.57 0.00 0.00 0.00 12 0.00 8.39 =1.05 0.00 0.00. 0*00 13 0.01 23.03 -1.05 0.00 0.00• 0.00 14 0.01 21.90 -2.96 0.00 0.00 0.00 15 0.01 ' 15.16 0.30 0.00 0.00 0.00 16, 0101 5.01 -1.33 0.00 0.00 0.00 17 0.00 32.06 -1.33 0.00 0.00 0.00 20 0.01 17.60 3.43- 0.00 0.00, 0.00' 21 0.01 11.19 -1.40 0.00 0.00 0.00 22 0.01 30.71 -1.40 0.00. 0.00 0.00 23 0.01 29.20 _ -3.95 0.00 0.00 0.00 24 0.101 20.22 0.400.00 0.00 0.00 25 0:02 .6.68- -1.77 0.00 0.00 0.00 26' 0.00 42.74 -1.78. 0.00 0.00 :0.00 30 0.00 7.66 4.44-- 0.00 0.00 0.00 31 0.00 1.26 -0.39 0.00 0.00 0.00 32 0.01 20.77 -0.39 0'.00, 0.00: 0:00 33 0.01 -3.25 ✓ -0.76 0..00 0.00 0.00 • 34 0.00 32.81 -0.77. 0.00 0.00 0.00 35 0.01 19.27 -2.94 0.00 0.00 0.00 36 0.01 10.28 1.41 0.00 0.00 0.00 15' •1 -7.46 16.72 -0.04 0.00 0.00 0.00 2 -0.38 72.81 -2.18 0.00 0.00 0.00 3 0.18 20.06. 1.21 0.00 0.00 0.00 4 -0.02 6.26 0.64 •0.00 0.00 `" 0.00 5 0.00 0.01 0.19 -0.00 0'.00 0.00 6 -0.04 -0.11 -3.60 0.00 0.00i 0.00 • 7 -3.68 4.63- -0'.41 0.00 0.00 0.00 8 3.72 -12.19 -0.35 0.00 0.00 0.00 10 0.16' 26.33 2.04 0.00 0.00 0.00 11 0.09 19.67 4.22 0.00 0.00' 0.00 12 -2.64 23.22 1.22 •0.00 0.00 '0.00 13 2.91 10.61 1.27, 0.00 0.00-' 0•.00 14 -0.16 17.64 =0.11 0.00 0.00 0.00 15 0.40 21.85 3.16 0.00, 0..00 0.00 16 -5.47' 32.29 1.50 0.00 0.00 0.00 17 5.72 7.21 1.56 '0.00 -0.00 0.00 20 0.12 26.22 5.63-'_0.00 0.00 ,0.00 " 21 -3.52 30.96- 1.62 0.00" 0.00 0.00 " '22 3.8814.14 1.69 0.00. 0.00 0.00 23 -0.21 23.52 -0.14 0.00 0.00 0.00 24 0.54 29.14 4.22 0.00 0.00 0.00 25 -7.30 43.05 2.00 0.00 0.00" 0.00 • 26' 7.62 9.61_ 2.08 0.00 0.00' 0.00 30 0.10 15.94 4.56. 0.00 0.00 0.00 31114#8 i X-71 STAAD SPACE { -- PAGE NO. .12r. " *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. SUPPORT REACTIONS -UNIT • ----------------- RIP FEET" STRUCTURE TYPE = SPACE JOINT, LOAD FORCE-% FORCE-Y."'FORCE-Z MOM -B MOM -Y MOM Z 31 -3.54 20.68 0.55 0.00 0.00 0.00 32 3.87 3.86 0.62 0.00 0.00 0.00 33 -7.31 32.77 0.93 0.00 0.00 0.00 34 7.61 '.-0.67 1 1.01 0.00 0.00 0.00 35 -0.23 13.24 -1.21 0.00 0.00 36 0.52 18.86 3.15 0.00 0.00 0.00 21 '1 -8.13 17.98 -0.01 0.00 0.00 0.00 2 • 0.37 2476 i -2.18 0.00 0.00 0.00 3 -0.22 20.38 -1.17 0.00 0.00 0.00 4 ''0.01 .6.15 -0.63 0.00 0.00 0.00 5 0.00 -0.01 -0.19 0.00 0.00 0.00' 6 0.05 -7.31 5.211- 0.00 0.00 0.00 7 '-5.41 6.05 0.37 0.00 0.00" 0.00 8 5.38 -13.40• 0.38 0.00 0.00 0.00 10 -0.20 26.53"1 -1.99 0.00 0.00 0.00 11 -0.11 14.411 2.41 0.00 0.00 0.00 12 -4.21` 24.431 -1.22- 0.00 0.00" 0.00 13 3.88 9.84 -1.20 0.00 -0.00 0.00 14 0.13 21.971 -3.13 0.00 0.00 0.00 15 -0.43 17.831 0.14 0.00 0.00 0.00 16. -6.25 33.381 -1.50 0.00 0.00 0.00 017 5.95 6.41; -1.49. 0.00 0.00 0.00 20 -0.15 19.22! 3.22. .0.00 0.00 0.00 21 -5.61" 32.58 .-1.62 0.00 0.00 -0.00 22 5.18 13.13E -1.61 0.00 0.00 0.00 23 0.17 29.`291 -4.17 0.00 0.00 0.00 24 -0.58 23.771 0.19 0.00 0.00_ 0.00 25 -8.34 44.51V -2.00 0.00 0.00 0.00 26 -7.93 8.551 -1.98 0.00 01.00 0.0.0 30 -0.12 - 8.991' 4'.27 0.00 0.00 0.00 31 -5.58 22.35+" -0.57 0.00 0.00 •0.00 32 5.21 2.90 -0.55 0.00 0.00 0.00 33 -8.30 34,29 -0.941. 0.00 0.00 -0.00 34 7.96 -1.671 -0.93 0.00 0.00 0.00 35 0.20 19.06 -3.12 0.00 0.00 0.00. 36 -0.55 13.55 1.24 0.00 0.00 0.00 22 1 -0.05 --0.02 -0.06 :0.00 0.00 0.00 2 0..00 -3.71 -2.18 0.00 .0.00 0.00 3 0.00 19.31 -0.54 0.00 0.00• 0.00 4 0.00 5.15 -0.20 0.00 0.00 0.00 5 0.00 0.00 -0.07 0.00 0.00 0.00 6 0.00 0.64 3.92 0.00 0.00 0.00 7 -0.86" -3.04. 0.06 0.00 0.00 0.06 8 1.26 -3.00 0.17 0.00 0.00 0.00`. 10 0.00 24.46 -0.81 0.00 0.00 0.00 . it 0.00 18.83 2.33 0.00 0.00" 0.00 • 12 -0.65 16.07 -0.57 0.00 0.00 0.00 13 0.95 16.10 -0.49_ 0.00 0.00 0.00 _+3�y/'d 3 ��i If 0- ' STAAD SPACE, -- PAGE NO. 13 *FILE NAME -.'TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. &_ Const. SUPPORT REACTIONS -UNIT • - RIP FEET STRUCTURE TYPE =`SPACE JOINT LOAD FORCE -B FORCE -Y FORCE -Z MOM -B MOM -Y MOM Z 14 0.00 15.56 -2.25 0.00 0.00 0.00 15 0.00 21.13 1.03 0.00 0.00 0.00 16 -0.04. 18.34 .-0.66, 0.00 0.00 0.00 17 0.04 18.36 -0.56 0.00 .0.00 0.00 20 0.00` 25.10 3.11 0.00 0.00, 0.00 21 -0.86 .21.43 -0.75 0.00 0.00 0`.00 22 .1.26 21.46 -01.65 0.00 0.00 ' 0.00 23 0.00 20,75 -3.00 0.00 0.00 0.00 24 0.00 28.17 1.37 0.00 0.00 0.00 25 -0.05. 24.45 -0.88 0.00 0.00 0.00 26 ._ 0.05 24.48 _-0,75 0.00 0.00 0.00 30 0.00 16.09 3.49 0.00 0.00 0.00 31- -0.86' 12.42 -0.37 0.00 0.00 0.00 32 1.26 12.45 -0.27 0.00 0.00 .- 0.00 33 -0.05 15.44 -0.50 0.00 0.00 0.'00 34 0:05 15.47' -0.37 0.00 0.00 0.00 35 0.00 11.74 -2.62 0.00 0.00 0.00 36 0.00 19.16 1.75 0.00 0.00 0.00 28 1 0.01. 0.19 -0.05 0.00 0.00 0.00 2 0.00 3.73 -2.18 0..00 0.00 0.00 3 0.01 19.01 0.45 0.00 0.00 0.00 • 4 0.00 5.13 0.20. 0.00 0.00 0.00 5 0.00 0.00 0.07 0.00 0.00 0.00 6 0.00 ,` -6.71 4.05 0.00 0.00 0.00 7 -0.40 -2.85 -0.16 0.00 0.00 0.00 8 0..51 -3.16 -0.07 0.00 0.00 0.00 10 0.01, 24.14 .0.72, 0.00 0.00 0.00 11 0.01. 13.08 3.58 -0.00 0.00 0.00 12 -0.29 15:97 0.42 0.00 0.00 0.00 13 0.44 15.73 0.48 .' 0.00 0.00 0.00 14 0..01 20.91 -1.10 0.00 0.00 0.00 15 0.01 15.31 2.18 0.. 00 0.00 0.00 16 0.01 18.25 0.50 0..00 0.00 0.00, 17 0.00 17.96 0.58 0.00- 0.00 0.00 20 0.01 17.44 4.77 0.00 0.00 0.00 21 -0.38 21.29 0.56 �. 0.00 0.00 0.00 22 0.58 20.98 0.64 0.00 0.00 0.00 23 0.01. 27.87 -1.47 .0.00 0.00 0.00 24 0.01. 20.41 2.90. `0.00 0.00 0.00 25, 0.02 24.34 0.67 0:00 0.00 0.00 26 _ 23.95 _ 0.77 0.00 0.00 0.00 30 _0_.00 0.00 8.50 4.41 0.00• 0.00 0.00 - 31 -0.39 12.36 0.20 0.00 0.00. 0.00 32 0.58 12.04 0.28. 0.00 0.00 0.00 33 0.01 15.40 0.31 0.00 0.00 0.00 34 0.00 15.01 0.41 0.00 0.00 0.00 35 0.01 18.94 -1.83 0.00 0.00 0.00 36 0.01 11.47 2.54 0.00 0.00 -0.00 3 ��i If 0- 3/ii /P,? STAAD SPACE -- PAGE NO. *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. SUPPORT REACTIONS -UNIT - • RIP FEET STRUCTURE TYPE = SPACE JOINT LOAD FORCE-% FORCE -Y FORCE -Z MOM -S MOM -Y MOM Z 29 1 -0.02 0.00 0.00 0.00 0.00 0.00 2 0.00 0.00 -0.06 0.00 0.00 0.00 3 0.00 0.89 0.00 0.00 0.00 0.00 4 0.00 0.00 0.00 0.00 0.00 0.00 5 0.00 0.00 0.00 0.00 0.00 0.00 6 0.00 0.00 0.07 0.00 0.00 0.00• 7 -2.21 0.00 0.00 0.00 0.00 0.00 8 1.47 0.,00 0.00 0.00 0.00 0.00 10 0.00 0.89 0.00 0.00 0.00 0.00 11 0.00 0.67 0.06 0.00 0.00 0.00 12 -1.66 0.67 0.00 0.00 0.00 0.00 13 1.10 0.67 0.00 0.00 0.00 0.00 14 0.00 0.67 -0.04 0.00 0.00 0.00 15 0.00 0.67 0.04 0.00 0.00 0.00 16 -0.01 0.67 0.00 0.00 0.00 0.00' 17 0:01 .0.67 0.00 0.00 0.00 0.00 20 0.00 0.89 0.08 0.00 0.00 0.00 21 -2.21 0.89 0.00 0.00 0.00 0.00 22 1.47 0.89 0.00 0.00 0.00 0.00 23 0.00 0.89 -0.05 .0.00 0.00 0.00 24 0..00 0.89 0.06 0.00 0.00- 0.00 • 25 -0.02 0.89 0.00. 0.00 0.00 - 0.00 26 0.02 0.89 0.00 0.00 0.00 0.00 30 0.00 0.72 0.08 0.00 0.00 0.00 31 -2.21 0.72 0.00 0.00 0.00- 0.00 32- 1.47 0.72 0.00' 0.00 0.00 0.00 33 -0.02 0.72 0.00 0.00 0.00 0.00 34 0.02 0.72 0.00 0.00 0.00 0.00 35 0.00 0:72 -0.05 0.00 0.00 0.00 36 0.00 0.72 0.06 0.00 0.00' 0.00 31 1 -0.02 0.00 0.00 0.00 0.00 0.00 2 0.00 0.00 -0.06 0.00 0.00 0.00 3 0.00 0.89 0.00 0.00 0.00 0.00 4 0.00 0.00 •0.00 0.00 0.00 0.00 5, 0.00 0.00 0.00 0.00 0.00 0.00 6 0.00 0.00 0.07 0.00 0.00 0.00 7 -1.47 0.00 0.00 0.00 0.00 0.00 8 2.21 0.00 0.00 0.00 0.00 0.00 10 0.00 0.89 0.00 0.00 0.00 0.00, •11 0.00 0.67 0.06 0.00 0.00 0.00. 12 -1.10 0.67 0.00 0.00• 0.00 0.00 13 1.66 0.67 0.00 0.00 0.00 0.00 14 0.00 0.67 -0.04 0.00 0.00 0.00 15 0.00 0.67 0.04 0.00 0.00 0.00 16 -0.01 0.67 0.00 0.00 0.00 0.00 17 0.01 0.67 0.00 0.00 0.00 0.00 20 0.00 0.89 0.07 0.00 0.•00 0.00 • 21 -1.47 0.89 0.00 0.00 0.00 0.00 3/ii /P,? STAAD SPACE 41 -- PAGE.NO. *FILE NAME - TEMPORARY COMPRESSOR BUILDING ( ID: Raytheon Eng. & Const. •SUPPORT REACTIONS -UNIT RIP FEET ----------------- STRUCTURE TYPE = SPACE JOINT LOAD FORCE -B FORCE -Y FORCE -Z MOM-% MOM -Y 'MOM Z 22 2.21 0.89 0.00 0.00 0.00 0.00 23 0.00 0.89, -0.06 0.00 0.00 0.00 24 0.00 0.89 0.06 0.00 '0.00 0.00 25 -0.02 0.89- 0.00. 0.00 0.00 0.00 26 0.02 0.89 _ _ 0_._0_0 0.00 0.00 0.00 30 0.00 0.72 0.07 0.00 0.00 0.00' 31 -1.47 0.72 ,0.00 0.00 0.00 0.00 32." 2.21 0..72, 0.00 0.00 0.00 .0.00 33 -0.02 0.72 0.00 '0.00 0.00 0.00 34 0.02 0.72 0.00 0.00 0.00 0.00 35 0.00 0.72 -0.06 0.00 0.00 0.00 36 0.00 0.72 0.06 0.00 0.00 0.00 ************** END OF LATEST ANALYSIS RESULT ************** 291. LOAD LIST 1 TO 8 20 TO 26 292. *PRINT JOI DIS LIST 3 10 17 24 293. LOAD LIST 1 TO 8 10 TO 17 20 TO 26 30 TO 36 294. *PRINT MEM FOR ALL •295. LOAD LIST 1 TO 8 10 TO 17 296. SECTION 0.0 .25 .5 .75 1.0 MEM 1 TO 26 29 30 297. *PRINT HEM SEC FOR 298. PARAMETERS 299. KZ 1.75 MEM 1 2 5 TO 8 11 TO 14 17 TO 20 23 24 300. SSY 1..0 MEM 1 2 5 TO 8 11 TO 14 17 TO 20 23 24 301. LZ 22.8 MEM 78 11 TO 14 17 18 302. LY 22.8 MEM 1 2 19 20 303. LZ 26 MEM 33.34 36 TO 39 41 TO 44 46 47 304. LZ 27 MEM 3.4 9 10'15 16 21 22 305. UNL 22.67 MEM 1 2 7 8 13 14 19 20 306. LZ 24.1 MEM 25 26 29.30 307. NSF .85 308. RATIO .9 ALL 309. LOAD LIST 10 TO 17 310. CHECK CODE ALL r.1 (' � I � N�. �I I � I I i !44i i i ! I I i I i I i i ' . I i .. I i i ... .._.L... _ .. � ---... .....� -- - -- I ; ! i i - • :;;';;.;;!;SII it •� o to } pT ... .... ........ ... .... ........ ' ' t i l I� I I j� i l l; l ( I � I � i I I I I ' I I ( I I i I ( I I j i'' I I i( I i I; ; I! i It i! FORM a/`,+ REV. 813T��� ---------'-�----'-------- 'C' ! ' 6 216 LO IF V. 2-lo x2.L- MOD Lb-A L7 W12 Zic I 21)NO 4p I 13 ~� jK i a �-----�--_--�-----��--------------------- &~ -3//t48 0 Raytheon Engineers & CALCULATION SET NO. Constructors CALCULATION SUMMARY 1 3 - I `t3 0 OO — 1 & CONTROL SHEET PRELIM. FINAL VOID REVISION Page 1 of 2 I PROJECT TITLE (GBp $e DISCIPLINES V Lx _+ IA�Q J.O. 0 S Z• �� STRUCTURE OR SYSTEM PQ L ate vi a e r ir- N , DESIGN CLASSIFICATION 11d SUBJECT i 1.. A-1.+ h� f 1' �d vv, COMPLETED BY DATE CHECKED BYG O/'9 _ DATE APPROVED BY DATE 8" SDE OR MGR OF STAFF GROUP ' DISTRIBUTION REASON FOR REVISION: ........................................................................................................................:.......................................................................................... TOTAL NUMBER OF SHEETS HI IN TS ISSUE Z ....................................... _.................................................................................................................................................................................. ........................................................................................................................................................................................................................... .................................................................................................................................................................................................................... ....... ........................................................................................................................................................................................................................... SHEETS REVISED, ADDED OR DELETED PROBLEM STATEMENT: ................................................................................. ...... . ............ . es �� H �owvi a �: ..............�.........� c r � ��. 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SUMMARY CONCLUSIONS: ............................................... ............... �.................... _............... .. . .. _Tk e.......` o a,:...+ .... .S.s{.-.!..Ne ......w..!..� ..... .......... -Sa. ej.�l.... n- !.s. e.r........................................... ... ....................... a.. �.1....-.. o�J e.... �.o a �.s........ T- V t�wl "�"�e....!.... �..... ...-......................................................................................................................-............. .. ` �St,�•-►�I c.�► a y� ...........................5....k �:�......... ........t. 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PRELIM. FINAL VOID REVISION DISCIPLINES to G urs 1.0. S 2 DESIGN BASIS: ............................................................... ................................................. :....... ..................... .. �..�................v ►^ :... S.K.-...1..6.--..�..-�.............................................. ............................................................................. ...................... .:+.... 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COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) REV. NO. REV. DATE PROGRAM TYPE RE&C VERIFIED 0 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 A:\CALC-SUM.DOT �� Iwc �� o oS� - R_. 'PI'O u N car ---- --- .--------- ---� .------ ---� - ---- ----- — ------ - �0 I — ---- - ca -- _— _—.. -- - — - -- —. _.-- - :�---•'�`�'------�--- - i------ -- - ---- - --- . _ .. _ . __. - ---- _------ • - _. � _. — � `' � �-------•-- - --- U �1- � !-�; i�i _lµllk}__�-�%�S ive n ch orS 14 X.494 _FA �N - - - - ---- --- 'P%a - - - -- - - -- r . _.. - ---- - - -- -- - - To. S ace lnlTd -- /— It rA=i7 �s -- --- -- ---- — -------- — - -- �31 -=- _ - E� Spa c ----------- - - - -cl ----------------- -------- - F=l---- ,1 I � AJ eS r v q�_ , ) -.. _ _ Typ► a��G���� Sm � ;—/� e __..._ . 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TOTAL NUM4§R OF SHEETS IN THIS ISSUE ........................................................................................................................................................................................................................... • ................................................................................................................................................................................ ........................................... ......................................................................................: ..............................................................................:...................: .......................................... _............................................................................................................... :................................................................ .........................................._.................................................................................................................................................................... - ........... 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A:\CALC-SUM.DOT Raytheon Engineers & Constructors CALCULATION SUMMARY CALCULATION SET NO. Fj 0 DO '- 2 PRELIM. FINAL VOID REVISION & CONTROL SHEET Page 2 of 2 PROJECT TITLE '/11 I CJ C D GS -e DISCIPLINE J rK e—j UYjA, J.O. % % D -sZ - DO DESIGN BASIS: _............................................................................................................................._....................................................... ;. ........:........................... ..........................�.;.f....y....j..:.........Vawi .g ........6....-'!.:-3...a........E.1z......,............................................................................................... ............................V .S.!...5AA......... .......... ..e. i'.A......................................................................................................................................................................... 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REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) .........................................................................................................................................................................................................:............................................................................. ................................... . 5.4....... 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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 DATEBY RUN BY DATE APPROVED BY DATE AXALC-SUMMOT i )rm 5007 (Rev. 9/95) Raytheon Engineers & GENERAL ..CALCULATION SET NO. REV: COMP. BY CHK'D. BY Constructors COMPUTATION SHEET PRELIM.. FINAL VOID, DTE DATE PROJECT b'a GL70S C SHEET OF -3 DATE DATE 11 2 SUBJECT?��j ?ece-ever �drl J.O. r% 70 SZ. 0 0 1 . wOTES: ?'70 52, co � o n,�`/'/ / oose � '�'---v�^!/�� ��J)�'���C—In �uu�c"r �-c�^/ . / —����� — [ ���--�------ ��---- �----�------� ' . � � (4~9 / ~J� '—'- '----- ---' 1--�2--- ---- - —' '---------� — ---�-------------- � r---- -- /8 L � /?d ~' 0 0 I Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors \COMPUTATION SHEET. CALCULATION SET NO. REV. COMP. BY p a. CH 'D. BY PRELIM. FINAL VOID LDA �} Z PROJECT16 I SUBJECT RI &CV-ly e✓ /=j101' SHEET OF,? F DATE DATE J.O. / � dS 2. OO' 51<wf� s 9, 3 e -o /.9 <157 (1,33) j 19) L 17 % l.Ssf 64 of (. ls>32- 1 1 24.3 1�,J. �� ski4 + ►-�-�al 6oK+2a3�= 263�'- /ve.f ./s-(/' 33) -Re /-h �0 ra, hc� Ass ,v" e :5' J 'b ea►�r o,I (y IDA p ev l" eA ✓- - Z x:f M,8 1.9 8 f � _ 1.9 6 �b 7) 0/ As r ,DJ �s AC 1 K Tofa.l rea r � oo>�y;;�� 4, al) = .9-6 6S, 14.4 A" u`S e / 7- 44 T10 16 �4 (.44) /4.464�D IL Tota! Aeea reS�� 6a �e-a�lfe� _ .96 (s7) 94-72 TO: BILL STALCUP/RANDYiROBERTS COMPANY: - SAGEBRUSH PIPELINE EQUIPMENT :CO. CITY: SAPULPA, OK FAX NO.: 918-224-8452 i FROM:. MYRON SCHULTZ j COMPANY: RAYTHEON ENGINEERS AND CONSTRUCTORS CITY: Englewood :STATE: CO FAX NO.: (303)-843-2208 `: PHONE: (303)7843-2454 - t TOTAL NUMBER OF PAGES.. 13, (INCLUDING COVER SHEET) i Subject: WILD GOOSE GAS ISTORAGE PROJECT #77052.001 REQN.'# D90.02 PIG LAUNCHER V=202 AND PIG RECEIVER V-203 - SRID:ANCHORS AND WEIGHTS Message: • 1. Please .furnish holes in the bottom flanges of the W8 x 31 skid support beams for the Pig Launcher and Pig Receiver in -accordance with the attached sketch SK -1, dated,1-27-98. 2. Also, please furnish us with the total installed weight for each skid. Phone me with the weights AS SOON AS POSSIBLE so that our structural• group can get started on the design of the concrete support slabs for these units. 3. With regard to actually launching and receiving the pigs, do these operations produce additional loads on the skid in addition to the weight that we should consider in our design ? REGARDS, PER 9•'30 i�M Tt.EcoNC� �ic� •�rn+ccvP - G�JE/��rs f�RE.• • V2o2 I°l < !/NGf/ER � 3000. # L� 4, V2o3, P�� �EcE/vii? _ 6'q/3oo # / rsEIPE i ww- /VO L awOT Tyfi+T yf/YE To %3E cON,T/DEI�ED� !/NGEJ.t THE �/� /.f ALLOGVE.O TO SC-0-fM /"T-0 T75/E 1?ECE1 k19o0 7 /-/C-'i90 Z*HIGfpi Nr/,fM/9z 4AS?V-�9770N CC: C.E.FILE L. LEFHOLZ R.MATHEWS A.THOMSEN J.YOUNG F9 u • Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO: REV. COMP BY ' CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID DATE' DATE 27 PROJECT MLD SHEET OF / DATE DATE SUBJECTIOe-/NG SKIDS -HOLD D?Gtl/VS J.O. %%OS2,GL�� C6) EQ Sp 8.0 48,0„ Y - - _ I^✓8x31 r rP z4 �,� V-1003 2.34�A 0" 13 o b W,6x'31 r j4lA V 202 PSG f f'UNCHE#? 5 ID 2 3,SGAAt ►4 (0) REo o. 934 i 0. •0, 31 Commerce Drive Suit® 100 P-Reville. CA &-6431 • 816. 786.8883 -AX 918. 786.7891 09: AM -91678678.91' �':. t� �' . - �— -• - P. lit .._., ., File No. 4074.2 oma, .,,,,o„ 28 January 1998 FU To 9$ .2— I,A . � Mr. Tony Thompson Fa'# � • Raytheon Engineers and Contractorsfrom P.O- Box 5888 P► I Denver, CO. 80217 Subject: Wild Goose Gas Storage Facility } Gridley, California UPDATED MAT FOUNDATION RECOMMENADITONS t - ' { ; Dear Mr. Thompson: At your request, we reviewed our mat foundation recommendations and calculations for the Wild Goose Gas Storage Facility, and performed analysis,to determine their application to the proposed launcher and receiver pads. 17his letter contains our - findings, conclusions, and recommendations. ' :Findintrs I We included recommendations for mat foundations in our Final Geotechnical Report for the Wild Goose Gas Storage Facility (ACG File No. 4074.1, dated 20 may 1997). Based on our knowledge of the project at that time, we assumed the following: 1) Mat foundations would only beat the Remotc Facility, i .2) Maximum mat width would be 20 feet, and 3) The maximum length /width ratio of the mats would be 2, i Based on our recent, conversations with Mr. Tony Thompson, (with Raytheon Engineers), we,understand that the receiver mat at the Remote Facility will be 50 - feet -long and 13 -feet wide. Therefore the length/width ratio is 3.8, which is greater than our assumed 2. ! Mr. Thomspon also told us that a launcher pad will be constructed at the Well Pad site, and that the dimensions .will be 13 -feet -long and 13 -feet -wide.' Because the launcher pad will be located at the Well Pad site and the length/width ratio -is 2.7 { (which is greater than 2), our assumptionsWere not met. Because our assumptions were not met, additional engineering analysis were necessary. We performed elastic settlement and bearing capacity for the proposed launcher and receiver mats, using the dimensions outlined above, and a maximum uniform load of 500 psf, which was supplied by Mr. Thompson. 'Our conclusions ' ' ;and recommendations are presented below. I • r t • s JAN '30 '98 09:28AM 9167867891 P.2i2 File No. -072.2 28 January 1998 Wild Goose Gas Storage Facility Updated Mat Foundation Recommendations ®Conclusions and Recommendations . Receiver Mat . Based on our analysis, we estimate less than % inch of total settlement .of the receiver mat: The Design parameters presented in Section 5.2.2.1 of our Final Geotechnical Report may be used, for the receiver mat. The -outer outside edge of the mat, should extend at least 12 inches into the pad. Launcher Mat Based on our analysis, we estimate .less than %: inch of settlement of the launcher mat due to elastic compression. Additional movement of the mat may occur.due to shrinkage and expansion of the clayey subgrade soil (see Section 5.2.2.5 of our Final . Geotechnical Report) . For the launcher mat, we recommend the following design parameters: • A modulus of elasticity of 486 kips per square foot, • A Poisson's ratio of 0.3, • A Modulus of Subgrade Reaction of 40 kips per cubic inch, • Dynamic Shear Modulus values from Section 5.2.2.1 of our Final Geotechnical Report, and • An Allowable Bearing Capacity of 3,500 psf. To mitigate detrimental shrink/swell affects of the clayey fill underlying the mat, the outer 12 -inch edge of the mat should extend at.least 24 inches into the clayey subgrade. Pre-soaking the pad prior to concrete, placement could also reduce the risk of movement (see Section 5.2.2.5 of our Final Geotechnical Report). Limitations Sections 6.0, Risk Management ,and ; 7.0 Limitations of our Final Geotechnical - Report apply to this letter. If you have questions; or require additional information, please call: Thank you! AND RSON CONSU Tr GROUP 8� Obert B. Lokteff T omas W.AackbuZrn, G.E. Project Engineer President copy:, Wild Goose Storage Inc. / Attn: Mr. Ian Duthie ANDERSON CONSULTING ,GROUP • Raytheon Engineers & , CALCULATION SET NO. Constructors CALCULATION SUMMARY & CONTROL SKEET PRELIM. FINAL VOID REVISION Page 1 of 2 DISCIPLINE PROJECT TITLE /(,/� �j- �'E J•o. 7 70.5 2 , 00 / STRUCTURE OR SYSTEM DESIGN CLASSIFICATION 147.0 G!A/ DA 7/01V4,r SUBJECT O " COMPLETED BY DATE 2- /j - 7 a CHECKED BY C ' _ DATE APPROVED BY DATE SDE OR MGR OF STAFF GROUP " DISTRIBUTION REASON FOR REVISION: ............................................................... .............................................................. 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FINAL VOID 'LbATE DATE �( SUBJECTRIPe �exlA -z"-- //�A7/Q/V SHEET OF DATE DATE J.O. v�i.slrr� Z-47, 7. 2.6 77 Y� = 1.-7( 4.4-0)(.-7s) oM Sin/GGE �iE,e � , /1-7,L /ha..r /1%n =,94E Aq <d ._ . 5� 32 Cao) . y �` h 9c3x�s� y V ��sx�8� g,5) 2 Vc = /2 •.C� �. 7 Vu. G1f� iVoA,71r41 �- SIA X C'�-r,!?/l�Y� 4 2.5 - . 75 ? /. %5 � _ • , 7?Xl. 7X Z o &sr) = 0. Z Form 5007 (Rev. 9/95) ' 1• 1 5007 (Rev. 9/951 Raytheon Engineers & GENERAL CALCULATION SET NO. 131 eaoo- 3 REV. WMPY Cl By Constructors COMPUTATION y PRELIM. FINAL VOID ATE SHEET - ATE PROJECT WILD C -0D SHEET OF DATE DATE SUBJECT J.O. N .a N 1: �. �N Q - o Q • • 11 Form 5007 (Rev. 9/95) Raytheon Engineers & Constructors GENERAL COMPUTATION CALCULATION SET NO. 3 �/5� g REV. COMP. Y CW CHK'D. BY Ae PRELIM. FINAL VOID DATE 2•�i• g JDATF ,r SHEET iN/L%� GiUSc�` 0 PROJECT SUBJECT PlAe )5Z&,QQ ` ;!�--QUIVO�1� SHEET OF DATE DATE J.O. .O Cd�l1) (xbw�� 0 n � Ila" �. 1. _ N Cd�l1) (xbw�� Ra0heun Engineers & CALCULATION NO. Constructors CALCULATION SUMMARY PRELIM. FINAL VOID REVISION & CONTROL SHEET Page I of 2 DISCIPLINE PROJECT TITLE /L� Cj..�� S� J•O• STRUCTURE OR SYSTEM ��0� GpG�n//��70N DESIGN CLASSIFICATION SUBJECT D6nf GN C-S �df COMPLETED BY DATE 2 • Co • �S CHECKED BY 4. 7-11,9,-ops e x.1 DATE APPROVED BY DATE SDE OR MGR OF STAFF GROUP DISTRIBUTION REASON FOR REVISION: TOTAL NUMBER OF SHEETS DV THIS ...............................................................' .............................. ........................................................................................................................... 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A:\CALC-SUM.DOT , Raytheon Engineers & Constructors CALCULATION SUMMARY & CONTROL SHEET Page 2 of 2 PROJECT TITLE YVI&O Gib CALCULATION SET NO. PRELIM. FINAL I VOID I REVISION DISCIPLINE J.O. -7%0 6*Z . Qp i DESIGN BASIS: (��G 1 Gl`7- .............................................................. ......................... :......................................................... .................................................................................................... ...........................................................(�f' /o!',�/I G.......�,44:7.....3................................................................. ...............................................................W....!T..!o............ ..,2E........ ............................................................................................._...................................................................................................................................................................................--... ............................................................................................._............................................................................................................---......................................................................... ........................................... ................................................. _.................................................................................................................................................... ......................................................................... ........------................................................,..................... ..................................... UNVERIFIED ASSUMPTIONS/OPEN ITEMS: .............................................................................................. ......................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ....................................................................................................................................................................................................................................................................................... ................................................ ............................................................................................................................ :...................... ....................................................................................................................................................................................................................................................................................... .............................................................................................................................................................................................................................................................................. :............................................................. ....................... REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, CALCULATIONS, TEXTS, REPORTS, COMPUTER DATA, FSAR, ETC.) ..............................................................................................................................................................................................................................................................................:........ ................................... _........�iJ .........../..9........................................................................................................................................................................................ ................................... _............ i:. ...... i...-.. ..:..................................... ...................................................................................................... ..................................... ................................_........�'o�� �........ oQ....:............................................................. ..................................................................................................... ................................... _.................................................. ............. ................................................................................................................................................................................... ..................................._................................................... ................................................... ............................................................................................................................................. .................................... ................................................................................................................................................................................................................................... 0.............. 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 BY RUN BY DATE APPROVED BY DATE DATE AXALC-SUM.DOT r� :orm 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. CVY CHK'D. BY Constructors COMPUTATION 3/�0�- SHEET PRELIM. FINAL VOID 04E PATE, PROJECT WILD 6DO� SHEET OF SUBJECT_OR& 6J7�'0 J 5, �� DATE DATE . .O. 54, 6 C-115 S4P/3 700' 2 7 0, -740 7S5 ' 7770," No7 Pr�E St..E��� PLA-.✓ �... ;\ /a l � #ZO '0'v/_ y a - r EL CoZ =0 " o U Form 5007 (Rev. 9/95) RaVMeen Engineers & GENERAL" CALCULATION SET NO. REV.Y CHK'D. BY Constructors COMPUTATION 13/Q5000- w *,, SHEET PRELIM. FINAL VOID ATE !B,, .PROJECT W/LD G�.SC-� SHEET 2 OF 0 DATE DATE SUBJECT/����� J.O. dim/�'�I/G : /Vo�/5>/��rc7'�2�fL /�c�l�/.�,r�l�✓'� . p. 23 YNR 20" � • � = (. 231. 5$� - p. �,r Cs w /ob". " c t Form 5007 (Rev. 9/95) U Raytheon Engineers & GENERAL CALCULATION SET N9. REV.W-tAT CHK'D. BY Constructors COMPUTATION �SHEET PRELIM. FINAL VOID ATE r PROJECT_ SHEET � OF DATE DATE , SUBJECT P�s�� SLE���JP.S J.O. , Pi�� s��,��r • • (,�o� ,4-��y�e�� cam o , .. ReFp'o VA -c.. 2 M/nl Go ✓W,4C& —� coNS/ On/G y -01i sec>,av) -7),(OX /5) - -7 9¢ wr- 3Y3)( /5) - 4: 6o WS Cp� p DL fEtp /e•9�- �� ' <&9 7.75) = 6 4!k e 2t. 9 0.25. (1v7, .;) = 0:60 qua_ F3 • • a rums uuui tntw. wtpo) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP. Y CHWD. BY Constructors COMPUTATION SHEET PRELIM. FINAL VOID Z • 5 • g DAT B , 'PROJECT W16 D Czvosz—,y SHEET 'OF" DATE DATE . SUBJECT 52 5702, C -70S J O �2 -4 2.02 4 /. �58 4 2..,62 -)4 /8.9 ,o 2.a ¢14 A 13.'? =. ZV, ¢ k . = qn 3 C 8) 8 _ . , ," . �• 2� �� Dom. " Form 5007 (Rev. 9/95) Raytheon EnglneerS & GENERAL CALCULATION SET O. REV. MP. Y CHWD. BY Constructors COMPUTATION I3/�ODa- W x.." SHEET PRELIM. FINAL VOID ATE ATE 2.5• 2 9/?s PROJECT W/LLQ 60S�1 SHEET S OF `Q > DATE DATE SUBJECT- 17 UBJECT 0 �- o _._ �lv r NJ w JL4 z wwns ��� 40 • 0 • 5007 (Rev. 9/95) Raytheon Engineers & GENERAL CALCULATION SET NO. REV. COMP Y,, CHK'D. BY Constructors COMPUTATION SHEET PRELIM. FINAL - VOID DATE DTE 2•�0 9,a Z /B/B PROJECT 'WIL10 6004& SHEET OF /O DATE DATE SUBJECT J.O. am IrT 1�¢@ten_ �olv A -A I 3111 198 • is 01 Form 5007 (Rev. 9/95) Raytheon Engineers & GENERAL Constructors COMPUTATION CALCULATION SET NO. 1310ba� - - REV. C P Y CHK'D. BY D� PRELIM. FINAL VOID bATE Z (0 %` _/ f w SHEET PROJECT -1 SHEET 8 OF �O DATE, DATE SUBJECT . AyP� 0466 ��•P Scl1JL/L. le— 1 'Ile,.: -7-0 7o,, 602-0„ 3 � o., 52�- i j t y � _ . r T v > I I � I � 1 . TTT i I t C F 1 1 I +++ I I I t i IE A For V-36" O.D. , _X • .++ H 1/8' Thick X t --� Belting Material' T SLOT DETAIL I Rv l_ 1/8" Thick Belting Material; M. B - I ! 'See Report for Specific Recommendations Rev. Date. .By A 8-31-95 MFiT E'I&AW ll Pipe and Bottle Clamp R - - with Belting Material ` 4" to 36" Pipe f APPROVALS i - DRAIMNG No. AA -111 I .Pipe Size I A B C r F' }} i\•I R T v A Bolts 4.5" 10.750" 8.250'! 3.0" 2.000" 6.000" .6215" 0.375" 2.375" .250" .625"' .250" 1/2" 6.625" 111.375" 11.375" 3.0" 2.93:1" 6.000 7 5" 0.500" 3.438" .375" 313" . 5/8" 8.625" 16.875" 13.375" 3.0" 3.938" 6.000" .875" 0.500" 4.438" .375" .75" .313" '5/81, 10.75" 20.500" 16.5" 3.5" 5.0" 7.000" 1.00011. 0.500" 5.500" .500" 1:000" .375" 3/4" 1_1,75" 22.500" 18.5" 3.5" 6.0" 7.000" LOW'` 0:500" 6.500" .500" 1.000" .375" 3/4" 14" =3.75" 19.75" 3.5" 6.6'_'5`' 7.000" 1.000" 0.500" -7.125" .500" 1.000" .375" 3/4" 16" 25.75" 21.75" 3.5" 7.625" 7.000" 1.000" 0.500" 8.125" .500" 1.000" .375" 3/4" 18" 27.75" ..3.75"• ' 3 .5," ` 3.6_5". ' 7.000" 1.000" 0.500" 9.125" .500" 1.000" .375" 3/4" 20" 32A" 2;,75" 4.0" 9.625" 8.000", 1.125" 0.500" 10.125" .625" 1250" .438" 7/8" 24" 36.0" 31.75" 4.0" 11.625" 8.000" 1.125" 0.500" 12.125" .625", 1.250" .438" 7/8" 26" 38.0" 3.3.75" 4.0" - 12.625" 8.000" 1.125" 0.500" 13.125" .625" 1.250" .438" 7/8" 23" 40.0" 35.75" 4.0" 13.625" 8.000" 1.125" 0.500" 14.125" 625" 1.250" .438" 7/8" 30" 43.75"'- 38.75" 5.0" 14.625" 10.000" 1.250" 0.500" 15.125" .75" 1.250" .500" 1.0" 32" 45.75" 40.75" .. 5.0" 15.625"' 10.000" 1.250" 0.500" 16.125" .75" 1.500" .500" 1.0" 36" 4935" 44.75" 5.0" 17.625" .10.000" 1.250" 0.500" 18.125" .75" �,500-.500" 1.0" 0j 113 � S � o� N Q I N � �O' y N n � N b o� SL �O' y N —75 ' 100-0c-91 N.253100 i �— 14.253000 I �G P N.252900 L-A I� N .n V N 5 ^u N.252800 POWER POLE #8 .4.252695.72 E.613275.80 N.252700 N.252686.97 E.613301,51 SW CORNER OF 698.5':387.5' PARCEL n W I I I 1 I 1 JS' /`�...�_.. ._ gin.• �'!�� LANDSCAPE I BERM 4 •c 15' ACCESS 15' ACCESS - 35' LANDSCAPE BERM -- --- . O� I I i J INJECTION V 16 (TYP. 6 .> (FUTURE) I O x a35' LANDSCAPE 0 BERM 15' ACCESS-!/ I I MONUMENT W.C.-3 N.252685.40 E.613330.08 ELEV. 67.40 I I I I POWER POLE %7 I POWER POLE i9 N.252536.60 .4.252633.44 E.613365.48 E.613009.22 UPDATED WITH LATEST BULOINO 01 ADDED TE11P. COYPNESSORS, TW ADDED IEE K BLADIa. PERNETO RMM POC, METMN0 QDO ! B REVISED PARCEL SIZE - UPDA' UPDATED IN ACCORDANCE WITH RELOCATED COMPRESSOR FACIL MAI POWER DISTRI!50Tr 1>rJr�>�QGgoUt4p___f OYE12IEACcw_ ,a plafV 5 m• ;; .,•- u.L'Q°' I " ,, iso TEMPORARY COMPRESSOR _ N. 50- • L41N J p FN JE 27 1. REGENERATION FUEL -CAS . SHUT-OFF —� .4252796.97 9ggni �I 3 TEMPORARY 1 i •{� .� .. _— COMPRESSOR 7 I 1 I 30' MINI 24 1 _ I )ROP DROP st AREA �: AR --i < I r .I -•j: Ox }- LANDSCAPE C P RESSOR [�UILDING' 3� - -- __ - : V I (L BERM W - � .4 -4/1 In _.4, I 15' ACCESS 7 C I� 1 _ �.'—...�r 1-- N 1 r -ice 11 CIL CL cr - - MAIN CATE _WATE GAS EQUIPMENT DATA - 5011 DLDIVICOORDS. _ 12 FENCE 1 I -..- -- - - II II II - L II �...a..4.vy.� .� _ ._�+- • " -t = :PIPE' SLEEPERS'. /`�...�_.. ._ gin.• �'!�� 4 •c 15' ACCESS - 35' LANDSCAPE BERM -- --- . I I DITCH II W -WELL, PADS: &_SK -16-A=02 (OE CF SITE e r WEST UBER]AF.;ROImt:;T':J ',727'. t I i I :t; POWER POLE /6 N.252636.38 E613896.05 ELEV. 67.40 aa, a ��',.wU • =TT..-+ 2 197wP,mmp_::rc6 = 1 K. par.— . :JO, !GADO ; LE DATA ..a wCWMCRf'^l '.: AUIOCAb %m 13a-. s7pVp. i �woa ..r.s„odmn , po0o ; n aua nioct� , oN.arDioa"� :%i,1?.:.tlXt'�Ifa Vg14 r.\PfIW4\E20�P1PE •^ 'wwca, w1alM , m4 wawa ' 1-. :+.1 .: - ::y:- f•: \. :�IQ<%TTIa01/10/96 d"PM11 1I k I ' FOR REMOTE FACIUTY LAYOUT AND GRADING PLAN SEE DWC. 12-01-008 SPACING DIMENSIONS BASED ON IRI UNLESS OTHERWISE_'NOTEO I — LEGEND 0 COMPRESSOR UNITS (C -IOTA, C-1019) O2 PC&E METERING STATION (METER. INSTRUMENT BUILDING h ODORIZER) OCONTROL ROOM/OFFICE BLOC. O GLYCOL RECENERAT1C14 (U -201A/8) O5 MECHANICAL BUILDING - USED INITIALLY FOR TEMPCRARY COMPRESSORS. OPDC/STAND-BY CENERATCR (U-304)/IA COMPRESSOR SYSTEM (U-JO1) O INECTION WATER PUMP SKID (P -202A/9) - FUTURE IO CCMPRESSOR GAS COOLERS (A-IOIA, A-ICIB) 11 COMPRESSOR JACKET WATER COOLERS (A-JOIA, A-3019; 12 INLET SEPARATOR (V-201) 7'-0'0 X 15'-0' T/T 1J OISCHMGE SCRUBBER (V-103) 4'-6'0 X 8'-0' T/T 14 PIC RECEIVER (V-203) IS PROCESS GAS FILTER (V-204) 16 PRODUCED WATER TANKS (12' OIAMETER)(T-201A-F) OILY WATER DRAIN TANK WITH t7 SECONDARY CONTAINMEYT (T-301) 60'0 X 8'-0' T/T . O19 GLYCOL GRAIN TANK WITH SECONDARY CONTAINMENT (T-303) 84-0 X 15'-0' T/T 21 BLOWOOWN/VENT SILENCER (X-201) 22 ENGINE EXHAUSTS 23 COMBUSTION AIR INTAKES 24 OVERHEAD BRIDGE CRANE (CR -101) 25 TEG CONTACTORS PROCESS DRAIN TANK WITH 27 SECONDARY CONTAINMENT (T-302) 60'0 X 8'-0' T/T 2B GLYCOL CONTACTOR AFTER SCRUBBER (V-205) L E44 EM Q _ 4.1..1: UNr,F2y 2oUNP DUC O\1Elzl- p_Ao GAOL-�— TR/'-, 5 E.614108.65 N.252637.31 POWER POLE y5 STATUS PIPING sr"n'° R� aTE soE PE's PLOT PLAN P. IV3,V ECO EY/R" REMOTE FACILITY SCALL- WILD GOOSE STORAGE INC. L 1'-30'—o WILD GOOSE GAS STORAGE PROJECT rew,m • w+lplm NO. 16-10-001 wi•..w+qm �s urm sr+m a arm. �Cc SItrucSOI•S R N . crnnor ALL S , Cpl art Va Kv. w % % Q J 2.0 0 1 REV 0 7 1