ML20203J315
| ML20203J315 | |
| Person / Time | |
|---|---|
| Site: | Crystal River  |
| Issue date: | 12/12/1997 |
| From: | Lenn C FLORIDA POWER CORP. |
| To: | |
| Shared Package | |
| ML20203J289 | List:
|
| References | |
| REF-GTECI-A-46, REF-GTECI-SC, TASK-A-46, TASK-OR S97-0541, S97-0541-R00, S97-541, S97-541-R, NUDOCS 9712190186 | |
| Download: ML20203J315 (184) | |
Text
{{#Wiki_filter:- - - - - - - - - ATTACHMENT A to 3F1297-24 FLORIDA POWER CORPORATION CRYSTAL RIVER UNIT 3 DOCKFT NUMBER 50-302/ LICENSE NUMBER DPR-72 h 4. CALCULATION S97-0541, REV. 0 (Confirmatory Study of Selected Safe Shutdown Equipment Anchorage for USI A-46) t a f 0 0 q, PDR y
~ - Elorida INTEROFFICE CORRESPONDENCE 4 Power A -c -To ~ Nuclear Engineering NT60 1503 s Of fice MAC Telephone
SUBJECT:
Crystal River Unit 3 l Quality Records Transmittal Analysis / Calculation l T O. Records Management NR2A The following analysis / calculation package is suomitted as the OA Record copy: DOCNO 4 PC DocVMENT IDtNisFICATION NUMetR Rtv Sv5 TIM'51 TOTAL PAGES TRANSMiTTfD 8 ). S97-0541 0 MT, ER, AC, DP, ES,AH /7h TrTtt Confirmatory Study of Selected Safe Shutdown Equipment Anchorage for USl A46 j uwDS 110tutiPV ElvwoRDS FoR LAf tR RETRitVAd Seismic, SQUG, USl A46, Anchorage i l DxRtp tREFERENCES OR Pitts LIST PR' MARY FILE FIRST# VEND IVENDOR NAME: vtNDoR DOCUMENT HuMatR IDxREFl l SUPERSEDED DOCUMENTS (DyRIF) l Stevenson & Associates n/a ln/a i MTMC 18 l MTSW 3F cgyE-/A l VBTR 1 A VBil 1E l MTXS-1 l ACDP 51 ER1 Through ER8 l MTSW-2C l DPDP-6A MTMC-12 l ACDP-68-T l ESCC 1 AHCP-4 l DPDP 1B l MTMC-21 c m I \\ COMM(NTS (USAGE RISTRICTIONS. PHOPMitT ARY. (TC 1 This calculation is being issued for reference only as an independent study 'o address anchorage of selected equipment. This calculation is provide a bounding calculation. ""This calculation is not a design basis calculation for any of the above tag numbers.**" 4 NOTE: Use Tag number only for valid tag numbers (i.e., RCV 8, SWV 44, DCH.99), otherwise; use Part number field (i.e. CSC14599, AC1459). If more space is required, write "See Attachment" and list on separate sheet. "FOR RECORDS MANAGEMENT USE ONLY ' Quality Record Transmittal received and information entered into SEEK. Entered by: Date (Return copy of Quality Document Transmittal to NOE Support Specialist.) l De nATt vtminic ArioN ENcinetR DATE DATE d bscNENGR/ n44 fift(&+ Ithlhi kvisc.Nu t[AR Elt l2 ~ G c.cw w mr c www cc: Nuclear Projects (if MAR /CGWR!PEERE Calculation Review form Part lit actions req 6lred Yes @No Return to Service Related) Yes @ No (if Yes. send copy of the form to Nuclear Regulatory urance and a Supervisor. Conhg. Mgt. Info. copy of the Calculatrn to the ResDonsible Organization (s) identified in j Mgr., Nucl. Operations Eng. lOnginoO wlattach Part til on the Calculation Review form.) Mew 12.17 l
-(gN CALCULATION REVIEW _./ cxchevenu Page 1 of 2 - C4CWATON NO /htV. S97 0541, Reviston 0 PART I - DESIGN ASSUMPTION / INPUT REVIEW: APPLICABLE Yes No The following organi;ations have reviewed and concur with the design assumptions and inputs identified for this calculation: Nuclear Plant Technical Support s.ea.ie.,o.= System Engr 1 Nuclear Plant Operations s.oa.w.+.. o,,,,13, s.ea.w.c.. 6.en.w.m.= PART ll - RESULTS REVIEW: APPLICABLE Yes @ No The following organizations have reviewed and concur with the results of this calculation and understand the actions which the organizations mu::t take to implement the results. Nuclear Plant Technical Surport System Engr Nuclear Plant Operations s.ea.w.m.. Nuclear Plant Maintenance s.va.w.<o.= Nuclear Licensed Operator Training s.aa.w.o.. Manager, Site Nuclear Services s.va.w.o.. Sr.' Radiation Protection Engineer son.w.e = OTHERS: s.,a.w..o.. Sga.w.to.i. R.w 817
/ i CALCULATION REVIEW \\ 3x /......... v ~ Page 2 of 2 _ l cuewanow no mev S97 0541, Revision 0 PART lli CONFIGURATION CONTROL: APPLICABLE Yes @ No The following is a list of Plant procedures / lesson plans /other documeMs and Nuclear Engineering calcu!ations which require updating based on calculation results review: Document Date Recuired Resoonsible Oraanization fUp:n completion, forward a copy to the Manager, Nuclear Regulatory Assuranoe Group for tracking of actions if any items are identitled in Part 111. If calculations are listed, a copy shall be sent to the original file and the calculation log updated to reflect this impact. PARTIV - NUCLEAR ENGINEERING DOCUMENTATION REVIEW The responsible Design Engineer must thoroughly review the below listed docurrients to assess if the calculation requires revision to these documents. If "Yes," the change authorizations must be listed below and issued concurrently with the calculation. 'V0"* Ethance.J Design Basis Document ]Yes@No"C* Vendor Quahhcation Package Yes@ No "C" ] Yes @ No "'"*'* Topical Design Basis Doc. ]Yes@ FSAR No "C" improved Tech. Speci#'ation ]Yes x No "*""* E/SOPM ]Yes. No improved Tech. Spec. Bates ] Yes x No *"** Other Documents reviewed: L Conbg. Mgmt, Info. System Yes @ No(com Yes icm acac ann ca Analysis Basis Document O Ya' S No"C" QYes] ww ooc. un=,.co Ossign Basis Document Yes@No"C# Yes] w w.m -n Appendot R Fire Study ] Yes @ No"C" Yes ic-wa occ annu.co nce Firu Hazardous Analysis Yes @ No y,, (cM8ea coC MFEREmeggj aces NFPA Code Conformance Document ] ies @ No y,, m a ooc ann cn PART V - PLANT REVIEWS / APPROVALS FOR INSTRUMENT SETPOINT CHANGE PRC/DNPO approvalis required if a se', point is to be physically changed in the plant through the NEP 213 process. PRC Review Required Yes X No PRC Chairman /Date DNPO Review Required Yes @ No DNPO /Date Ot54GN t GNt17404Tt otS&GN (NGINE(R PRINTEQ NAMg N / $$ f how e17
,x [ / g.......... j CALCULATION VERIFICATION REPORT ( Cryst:1 Riv:r Unit 3
- ~'
CALvtRRP PRM Page 1 of 1 CM. Cut AtON NutiaSt M S97 0541 VaGJS C11tl1Lr Confirmatory Study of Selected Safe Shutdown Equipment Anchorage for USl A46 YtB-NO N/A 1, g Are inputs, including codes, standards, ogulatory requirt.ments, procedures, data, and Eng.neering methodology correctly selected and applied? 2. X Have assumptions been identified? Are they reasonable and justified? (See NEP 101, V.c, for discussion on references).
- 3. @
Are references properly identified, correct, and complete? (See NEP 101, V.c., for discussion on assumptions and justification.) 4. @ Have applicable construction and operating experiences been considered?
- 5. g Was an appropriate Design Analysis / Calculation method used?
6. In cases where computer software was used, has the program been verified or reverified in accordance with NEP 135 for safety related design applications and/or are inputs, formulas, and outputs associated with spreadsheets accurate? (SEE NOTE 1)
- 7. @
] is the output reasonable compared to inputs? 8. @ Has technical design information provided via letter, REA, IOC or telecon by other disciplines or programs been verified by that discipline or program? 9. @ Has technical desigt..aformation provided via letter c telecon from an external Engineering Organization or vendor been confirmed and accepted by FPC?
- 10. @ @
Do the calculation results indicate a non conforming condition exists? If "Yes," immediately notify the responsible Supervisor. 11. Do the results require a change to other Engineering documents 1 If "Yes," have these documents been identified for revision on the Calculation Review Form? I have performed a verification on the subject calculation package and find the results acceptable. vt.#tCATON ENaeettR QATE 5VPf * "50R. NUCLE A '#GINE S AING QATE 8e*# 8AAS4 L THoanPM N It/n/O lt /q D., w i NOTE: This calculation uses computer software that has not been verified to FPC's Procedure NEP 135. This calculation is to provide resolution to USl A46. This caletalation is not to be used for the design basis analysis of any of the listed equipment. Therefore, consider this acceptable for this limited application. i - Re, s 31 +
ay O \\ t ANALYSIS /CA..LCULATION
SUMMARY
x A U, .%/ Ol5CIPUNE CONTROL NO. AtVi$l0N LEVEL DOCUMENT IDENTIFICATION NUMBER S -97 0541 0 Tritt CLAS$2PICATION (CHECK ONt) Safety Related % Non Safety Related C:nfirmatory Study of Selected Safe Shutdown Equipment Anchorage for USl A46 "^^'5 * *'""E"8NUM8E" VirdDOR DOCUMENT NUM9th APPROVAL PRINTED SIG,NATilRES NAME Design Engineer [h (( C. Glenn Pugh D:ts /g/,7ly; Verification Engineer //[/M Mark L. Thompson sp/g [q) D:ta ( h_ C.m., h_ _, Supervisor Dan Jopling y _ Date l t ~ l L,,4 ireua mevmo Original Issue 79%%I
SUMMARY
The purpose of this calculation is to document anchorage calculations done to address USI A46. Mibu(IS
SUMMARY
Specific results and conclusions are shown'in the various attachments to this calculation a 1 n, est l
N . DESIGN ANALYSIS /CALCdLATION ,( y "" * """ Crystal River Unit 3 otsachu Page l of 3 DOCUMENT IDENT*nCAh0N No- - Revision ~ S97 0541 0-SECTION l PURPOSE:- The purpose of this calculation is to place into the CR3 files a copy of the attached evaluation. This anchorage study is to provide additional assu:ance that FPC's USl A46 position on anchorage is a valid position. The P! ant Specific Procedure (PSP) for Resolution of Unresolved Safety issue (USl) A46 states that the judgment and experience of well trained engineers is adequate to d:t:rmine the adequacy of equipment anchorage. This calculation is not meant to be the Design Basis calculation for any of the listed equipment tag numbers. Some of the listed equipment is safety related, others are non safety related. Since this calculation is intended to be more of a " study" than a design basis calculation - unverified software was allowed to be used. This study takes a subset of the equipment contained on the USl A46 SSEL and performs a bounding calculation. The intent of this bounding calculation is to envelope the equipment at CR3 and to ensure equipment anchorage adequacy. This study included the following sc,uipment categories: Equipment Class 1, Motor Control Centers Equipment Class 2, Low Voltage Switchgear Equipment Class 3, Medium Voltage Switchgear Equioment Class 4, Transformers Equipment Class 14, Distribution Panels Equipment Class 16, Battery Chargers and Inverters Equipment Class 20, Instrument and Control panels and cabinets. From this list of equipment categories, a sample list has been prepared. This list is further comprised of three categories. First, the NRC Staff had a specific question on the adequacy of the anchorage for the following tag numbers. The calculation contained in these Attechments are to address specific concuns on the anchorage of these items. MTMC-18, Class -1, Auxiliary Bldg, El. 95, Resolved in Attachment "A" , MTMC-21, Class 1, Auxiliary Bldg, El.119, Resolved in Attachment "O" DPDP-1 B, Class 14, Control Complex, El.108, Resolved in Attachment "N" VBIT-1 E, -Class id, Control Complex, El 108, Resolved in Attachment "B" AHCP-4, Class 20, Control Complex, El.164, Resolved in Attachment "M" S:cond; a sort was madedf the SSEL to determine the highest elevation for each class of cquipment. From this sort a sample of equipment from the above subset of equipment
- Rev C/M RET: Lete si piaat PtsP feucwas Engin**'*ne
,m f )N DESIGN ANALYSIS / CALCULATION (/ " " " " ' " Crystal River Unit 3 Df EA C PRM Page 2 of 3 00CVWNT DENhriCAh0N N0 mtv'SiON - S97 0541 0 categories is chosen The intent of this list is that the equipment category is enveloped. The calculations to be done here will bound, or, envelope, the anchorage for similar equipment. MTSW-3F, Class 2, Control Complex, El.145, Resolved.in Attachment "E" MTXS-1, Class 2, Control Complex, El.145, Resolved in Attachment "F" MTSW 2C, Class 3, Control Complex, El 108,~ Resolved in At' chment "G" ACDP 68 T, Cla,ss 4, Control Complex, El.124, Resolved in Attachment "H" 1 VBTR 1 A, Class 4, Control Complex, El.124, Resolved in Attachment "l" ACDP-51, Class 14, Control Complex. El.145, Resolved in Attachment "J" DPDP 6A, Class 14, Diesel Building, El.119, Resolved in Attachment "K" ~ ESCC-1, Class 20, Control Complex, El.145, Resolved in Attachment "L" Third, the list of equipment that follows has been declared outliers per the PSP. The purpose of these calculations is to verify that this equipment will remain in place without anchorage present. These components have been declared outliers and have been screened to be post-restart oudiers. The intent of these calculations is to show this equipmtnt will remain in place if
- he equipment is lef t unanchored until a modification can be done.
- ER1, Class 20, Control Complex, El.145, Resolved in Attachment "C" MTMC-12, Class 1, Turbine Bldg, EF 119, Resolvad in Attachment "D" (Note: MTMC-12 actually has anchorage that was identified on SEWS as poor)
The results of this anchorage review is attached, SECTl?N 11 RESULTSICONCLUSIONS: The attached reviews show rt.sults and conclusion for each of the listed equipment items. With the exceptions noted above, this selection of equipment is intended to bound, or envelope, equipment in the same USl A46 Equipment Class. 1 DECTION til DESIGN INPUTS: S:e individual Attachments. SECTION IV-ASSUMPTIONS: Since this is intended to be an enveloping, or bounding, type cal' ulation, any assumptions used c are to provide a worst case answer. This implies all assumptions should be conservative. There are no assumptions that require later confirmation. em ana % m u.i m }
x if lD DESIGN ANALYSIS / CALCULATION I' S d 'I " " 7 *[ Crystal River Unit 3 OtSA-C FRM Page h of ) 00CVutNT tDENTF4ATION No. PEVISION S97 0541 0 EECIlON V
REFERENCES:
Sn individual Attachments. SECTION VI DETAILED CALCULATIONS: See individual Attachments. SECTION Vil ATTACHMENTS: Attachment Tag Number Pages A MTMC-18 6 9 VBIT-1 E 6 C ER1 through ER8 12 D MTMC-12 7 E MTSW-3F 14 F MTXS-1 6 G MTSW-2C 6 H ACDP-68-T 7 I VBTR 1 A 6 J ACDP-51 7 K DPDP 6A 7 L ESCC 1 ,5 M AHCP-4 6 N DPDP-1 B 7 .O MTMC-21 4 T CHHE-1 A 3 P "The Behavior of Inverted Pendulum Structures During Earthquakes"- 16 pages Q ATC-10-1, " Critical Aspects of Earthquake Ground Motion and Building Damage Potential"- 11 pages R Stevenson & Associates Letter' dated 11/26/97,
Subject:
" Confirmatory USI A46 Evaluation of Selected Safe Shutdown Equipment at CR3"- 14 pages S'
SSEL ltem sort, by class, building and elevation - 18 pages Rev C/MS MT Lde of mont fESP Nucket 8%erW
N)U DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 ' s osu< *w Page A / of 8 DOCuaAU4T OENTIFl0ATCN NO REvtsiON S97-0541 0 A MTMC-18 l ana. n.m nese.u.o..,E,- m
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I 14.1180 154.M22 1.5119 0.0171 2.2MO f 14.3600 135.6PM 1.5137 0.0169 2.2913 l 19J200 135.62M 1.1173 0.0092 1.2483 19.5500 135.3559 1.1019 0.0090 1.2442 W 133.9262 1.0776 0.0087 1.1612 .0100 130.9896 1.0419 0.0083 1.0855 ANALYSIS / CALCULATION
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M.......... DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 sheet G '2. og 14 awiu,me mca.c ...a atmo. numw uw.wu S 0541 O N /A 1 i i i t 1 i
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i l M DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 gg g3g /4 i XKUWENT 4D(Wf67CAf TON NUWSE A R4 v15 ION REl/WANSP e#VWBEWFILE S -cn - o 5 41 O N /A ,.1 OII M IL Ih. (M L C h !. [*_ .Ol .j i ~1.. _.., i h8 er -ima (e g>w - $ ma g = .Or* .p p W .g 4 Y I bl,l 0 H ,U ti, !?,'. b 11.* . ~.. A ss. A 4.' os t $ 7 F 0
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.M.......... DESIGN AN ALYSIS/ CALCULATION Crystal R;ver Unit 3 Sheet 66d 14
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M DESIGN ANALYSIS / CALCULATION Crystel River Unit 3 33,,, t g,,,,g4,_ m...,,,c m,.... m. ., v.i ~,,a S -9 P c 541 o N/A ANCHOR analysis for MTSW 3F EajhjlitE.g1 k Response Spectrum : User Frequency : User 0.00 Percent Damping : User 0.00 Spectrat Values : praction Acceleration (g's) North South 0 39 East - West 0 38 Vertical 0.25 An0 e (N S Direction makes with the X Axis): 0.00 l Combination Crittna : SRSS Weicht,s_,1 Number of Weights : 3 No Weight X Y Z 1 400.00 9.000 45.000 29.000 2 6675 00 57.000 45 000 29 000 3 5814.00 132 000 45.000 34.500 Forens J Number of External Forces : 0 Momente : Number of External Moments : 0 Allowables : _ Anchor : Number of Anchor types : 2 Tenston Shear Ultimate Ultimate Inter Inter Saf No. Dia Manufact Product Tension Shear Coetf Coeff Fact 1 1/2 Other Unknown 1500.00 6000.00 1.00 0.30 1.00 Expansion Anchor 2 3/4 Other Unknown 2640.00 3900.00 1.00 0.30 1.00 Expansion Anchor QQO.01210 Ultimate Stress : 3000.00 psi. Reduction Factor : 0.85 l t l = -.n l
M DESIGN ANALYSIS / CALCULATION Orystal River Unit 3 sheet E 7 of I4 m voiwi oe.n,.c.r.o. vo.in ....o. nemw .imni s-cn-o s4l o N/s we Allowablo S'ross : 30600 psi. Eltrinces : Number of Surfaces : 1 Surfaco Orientation Direction Direction Direction Comp Comp Comp Ne Nx Ny NZ 1 0 000 1 000 0.000 Anchor Pattern for Surface # 1 (('V5 O!/&f7& t-9-99-99-4 99 S S G G 99 4-09-99-9 X-- Legend for Anchor Patterns Anchor Dolts : {~] Concreto Lines : Concrete Points : ' _ _ _,I m.___ _ J [ ] Weld Lines : Geometry : UKhE Number of Anchors : 20 W 900 871
M DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 ne.i E. S og 14-u-i.o a,ni, w,o ., u .....~,u S 0 5 4l O 'UA
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Y Z Gurf No ld Coord Coord Coord Id 1 1 4 000 0 000 2.000 1 2 1 14.000 0 000 2.000 1 3 1 100 000 0 000 7.000 1 4 1 110 000 0 000 7.000 1 5 1 124.000 0 000 -7.000 1 0 1 140 000 0 000 7.000 1 7 1 148.000 0.000 7.000 1 8 1 164 000 0.000 7.000 1 _0 1 4.000 0.000 56.000 1 10 1 14 000 0.000 56 000 1 11 1 100 000 0 000 56.000 1 12 1 116.000 0.000 56 000 1 , 13 1 124.000 0 000 56.000 1 14 1 140 000 0 000 56 000 1 15 1 148.000 0.000 56.000 1 16 1 164 000 0.000 56 000 1 17 2 36 000 0 000 17.000 1 18.__ 2 78 000 0.000 17.000 1 19 2 30 000 0 000 41.000 1 20 2 78.000 0.000 41.000 1 fLoncrete Lines :
- of elements per line : 4 Number of Concrete Lines : 6 Start Start Start End End End Sf Line No X Coord Y Coord Z-Coord X-Coord Y.Coord Z Coord Id Width 1
0 000 0 000 0 000 18 000 0 000 0 000 1 1.000 2 18 000 0 000 18 000 96000 0 000 18 000 1 1 000 3 D6000 0 000 7 000 108 000 0 000 7 000 1 1.000 4 0 000 0 000 50 000 18 000 ___0 000 56 000 1 1 000 5 18 000 0 000 40 000 96 000 0 000 40 000 1 1.000 0 90 000 0 000 56 000 168 000 0 000 56 000 1 1.000 Concrete PointL; Number of Concrete Points : 0 Weld tingjt;
- of elements per line : 4 Number of Wold Lines : 0 1
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M DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 Sheet b b of I4 u,wi=,notar w no.... ar m.o., ..w ww.mu 5 o g 4i O N /A Determination of Redifglion Factors : Reduction Factor input for Anchor # 1 1 No input. Reduction f ctors needing user input are not used. Reduction Factor input for Anchor # 2 No input. Reduction ' actors needing user input are not used. Reduction Factor input for Anchor # 3 No input - Reduction factors needing user input are not used. Reduction Factor input for Anchor # 4 No input. Reduction factors needing user ir put are not used. Reduction Factor input for Anchor # 5 No input Reduction factors needing user input are not used. Reduction Factor inc;t for Anchor # 6 No input Reduction factors needing user inpt are not used. Reduction Factor Input for Anchor # 7 No input Reduction factors needing user input are not used. Reduction Factor input for Anchor # 8 No input Reduction ' actors needing user input are not used. Reduction Factor input for Anchor # 9 No input Reduction factors needing usnr input are not used. Reduction factor input for Anchor # 10 No input Reduction factors needing user input are not used. Reduction Factor input for Anchor # 11 No input. Reduction factors needing user input are not used. Reduction Factor input for Anchor # 12 No input Reduction factors needing user input are not used, Reduction Factor input for Anchor # 13 . - ~,
M DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 n.i. m g _ M E eutut awtwicatow uvwata navisen atvue avwetwa 5-o-os4i o N /A No input Reduction factors needing user input are not used. Reduction Factor input for Anchor # 14 No input Reduction factors needing user input are not used. R: duction Factor input for Anchor # 15 No input Reduction factors needing user input are not used R: duction Factor input for Anchor # 16 No input Reduction factors needing user input are not used. R: duction Factor input for Anchor # 17 No input - Reduction factors needing user input are not used. R: duction Factor input for Anchor # 18 No Input Reduction factors needing user input are not used. R: duction Factor input for Anchor # 10 No input Reduction factors needing user input are not used. Reduction Factor Input for Anchor # 20 No input Reduction factors needing user input are not used. Reduction Factors Data Current : Yes Anc PalU Paltri No Id Vall Vater RT RN RL RG RS RE RF RC RR RP RB RM i 1 1500 00 N/A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 2 1 1500 00 N/A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 3 1 1500 00 N/A X X X X X X X X X X X X 6000 00 N'A X X X X X X X X X X X X 4 1 1600 00 N/A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 1 1500 00 N/A X X X X X 'X X X X X X X 60o0 00 N/A X X X X X X X X X X X X 6 1 1500 00 N/A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 7 1 1500 00 N/A X X X X X X X X X X X X 6000 00 N/A X X_. X X X X X X X .X X X 8 1 1500 00 N/A X X X X X X X 'X X X X X ~ 6000 00 N/A X X X X X X X X X X X X ~ 9 1 1500 00 N/A X X X X X X X X X X X X N 000 871
M DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 g,g g f; g g mum 1.~,.,w~ ....=.m,u S -cn - 054l o bl/A 6000 00 N/A X X X X X X X X X X X X 10 1 1500 00 N/A X X X X X X X X X X X X S000 00 N/A X X X X X X X X X X X X 11 1 1500 00 N/A X ,X. X X X X X X X X X X 6000 00 N,A X X X X X X X X X X X X 12 1 1500 00 N/A X X X X X X X X X Y X X 6000 00 N/A X X X X X X X X X X X X 13 1 1600 00 N'A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 14 1 1500 00 N/A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 15 1' 1$00 00 N/A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 16 1 1500 00 N/A X X X X X X X X X X X X 6000 00 N/A X X X X X X X X X X X X 17 2 2640 00 N/A X X X X X X X X X X X X 3900 00 N!A X X X X X X X X X X X X 18 2 2640 00 N/A X X X X X X X X X X X X 3900 00 N/A X X v X X X X X X X X X 19 2 2640 00 N/A X X X X X X X X X X X X 3900 00 NA X X X X X X X X X X X X 20 2 2640 00 N/A X X X X X X X X X X X X 3900 00 N rA X X X X X _ X X X X X X X tonend-N/A = Not Applicable Pr!I = Allowable Pull without Reduced Inspection Vril = Allowable Shear without Reduced inspection Prllr = Allowable Pull with Reduced Inspection Vrilr = Allowable Shear with Reduced inspection = Outlier X = Reduction Factor Not Used RT = Reduction Factor for Type of Anchorage RN = Reduction Factor for Installation Adequacy RL = Reduction Factor for Embedment RG = Reduction Factor for Gap at Anchors RS a Reduction Factor for Spacing RE = Reduction Factor for Edge Distance RF = Reduction Factor for Concrete Strength RC = Reduction Fe.ctor for Concrete Cracks RR = Reduction Factor for Essential Relays RP = Reduction Factor for Base Stiffness and Prying Action RB = Reduction Factor for Base Strength and Load Path RM = Reduction Factor for Embed. Steel and Pads Analysis Results : An: lysis Performed : Ye, ou 900 871
M DESIGN ANALYSIS / CALCULATION Crystal River Unit 3 Sheet -$ of I4 I
- CCUWENT IDiestippCAf eces NvWH A A(YtSaON R(WWA%SP NUWBE% PILL s-e r 054l o
N/A Type of Analysis : Regular Spectral Accolorations (G's) No NS E-W Vertical Safety f actor 1 0.380 0.152 0.100 0.944 _2 0.380 0152 0.100 15.768 3 0.380 0.152 0.100 7.533 4 0.380 -0.152 -0.100 10.523 5 0.380 0.152 0.100 18.060 0 -0.380 0.152 -0.100 3.709 7 0.380 0,152 -0.100 4.372 8 0.380 0.152 0.100 18.361 0 0.152 0.380 0.100 4.470 10 0.152 -0380 -0.100 42.433 11 0.152 0.380 0.100 46.907 12 0.152 0.380 -0.100 2.196 13 0.152 0.380 0.100 4.137 14 0.152 -0.380 -0.100 42.624 15 0.152 0.380 -0.100 2.308 16 -0.152 -0.380 0.100 46.907 17 0.152 0.152 0.250 8.258 __18 0.152 -0.152 -0.250 6.064 19 0.152 0.152 0.250 2.558 20 -0.152 -0152 0.250 16.440 21 -0.152 0.152 0 250 8.258 22 0.152 -0.152 -0.250 8.219 23 0.152 -0.152 0.250 16 440 24 -0.152 0.152 0.250 2.421 Minimum Safety Factor : 2.190 The Anchorage Capacityis 2.100 times greater than the Demand
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9""*""" DESIGN AN ALYSIS/ CALCULATION Crystal River Unit 3 sheet OY of Y l)CLUMINT (DE Nf 68 8 CATION NuWDin ktyisaQN mggruaggp Ngugggpigg 577-059'I O k/4 rn nowc n riri scc sy ror se in su e. c // M 'r /# G (, E r r / 9 4, tor /c cRCW JY TPr c21/nie &r t aa mw 7223 r/ / if?' pit Me divisp6 17 / r),)ir fo/rd72~ 774: t 0 Vit'sirsr /t re tc dA c/>Me7) h/t U fi(c C/*7Aff f C soo Sri ~
,- ms () DESIGN ANALYSIS / CALCULATION '_ 2-<. _ Crystal River Unit 3 tet&a C Psw - t Page / of /b DOCtWindt (DINTiflCaf 0N NO m!vi& ION S97 0541 0 P "The Behavior of Inverted Pendulum Structure During Earthquakes l l l M OD Rita Life of meet Rt SP. %cient Engwweewg
I f 4 i I l l ( i i \\ ANALYSIS / CALCULATION I DOC ID # 's-nU54i ATT # 8 I I l REV O SHEET 7-O F @ 1 8 i l i 1 l v...aetn. s..ierce sec...,.# a.m. v.i n. we, 2. n. m-m. 7.wwr. It O I f Tyr. BI:ll.\\Ylolt ol' INVl'.ltTl:1) PI':N Dlfl.t'.\\l S Titt'C Tl*lli:8 DllitlNG 1 l'..\\llTilQL*.\\1<!:8 l liv Gunna; W. llotuut i AllsTit At *T Duong ihe Chibuni cartheinate a of Slav. Inun. a tunnin r n( lall leniter.iruvinn = auitived the ground
- haling u herea. more anihin appearing t rnrture= nere severely d.unmred. An l
i l nnslys b made of ih" rocking snuinni of atructiara ni inwrted penduhnu type, it is shun n I l that there h a cah: cliert u hit h make ull
- lender at rucim"= innn' af abb ag:iin overintninir l
than nught hav" Inen espect ed, and. I bro lere, tio.no viv d of =m h.t rnet mw ihiring rati h. q4e. i. mn m pri.ing. INTuonet rtos i l INring the Chilean cattlupiake of.\\tay, I!W), neveral golf balbon a tee types of elevated water tani,. orvived the gremnl shaking despite the appearance of in. stability, as described in a companion paper by W li Clmul On the other hand, much more stable appearing reinforced concrete, elevated water tanks were e-verely damaged as described in a co.npanion paper by 10 Y. Steinhengge and Ib flores. It is clear that,in thir case, the concepi of sepnweniing the cliert of an carth-quake by a certain tatic lateral force (pment u design) may be spiite misleading. It i* not uncononon for hnibling endes to. pecily that elevated w ater tanks 3honhl be de igned for 10 per cent g and, judged from this point of view, the goH ball tank appeai3 to be in danger ftom eartlupmkes w hercan the strength and proportions of the concrete tank unnld be reasuring n to it.< ability to survive carthipmkes. Other unstable types of atructures have also survived strong earthipmkes. During l the Arvin Tehachapi carthipmke in California (.hdy *.!!,1%.') a tunnher of tall, slender, petroleum cracking towers atretched their anchor bolt and rocked back tmd furth on their loundation.' in onu Indian cities. hee ntanding stone v ohnuns that anpported heavy *taine remained standing ahhnugh at the end of the earth- 'pt they woie surrounded by heap, of debris that had been more stable,struc-l tm.7 Tall, rh.nder tone pillars in graveyard have also -mvived trong ground j tuntion. On the other hand,it ha mnetime, happened that hos like electric poaci transformer.* have rocked and overturned. Some light is t'mnvn on thin anomatons i behavior by an arwly is ni the dj namics cf a ngid bloi k that is resting upon n rigid, horizontal ha. c and i* cxcited into rocking motion. It u ill be cen that the vibrational characterbtics of thi4 type of <tructure are nmikedly ditierent from tho e of a lin-arly cletic structme. e l'ut:n Ylutl \\TioS.- Ilgid hlock ehown in hg I will q.<cillate about the s enters of r'dation 0 and 4 h
- " hen it i.4 *ct to rocking.11 i asumed that the coefheient of frictum is -nth-U"ntly large so that then* nill be no Shding between the block and the hac. The
'36:niheant propertic.< of t he block are ite, weight, li'. its moment of inertia l., about ~ ~ ~ ~ - - - , ' linusn. r. C. W., "1.inut Dr ign of $tt ut tutes in llenist t.' art hquaken." l'rurrohne of fl.. II nd.l 4%nference on f:sselhquqL e Enyisittring, Nor tk unir Engoitru tug is'etevela l u s ts'lu le. 7
? I REV O SHEET 3-OF lb l t 404 st1.tri x or int artsuotoolcat. soc cry of AMtRICA PtHAVH l i the point 0, and the location of the center of gravity a distance A above the base ' tion. The block will falli i j and a distance b from the side of the block, As shown in fig,1, the radial distance equation (2) becomes from the center of rotation 0 to the center of gravity is R = VA* + P. When j l the block is at rest, the line R makes an angle a with the vertical. The tilting of the 3 { l block from the vertical is measured b> the angle P. or I I l b t b n i 5 j hl 6 1 I, I 4 t l 9 i w 3 d [ IWLR h 411 l! 9'W i 2 V \\ l s f, 9 n I i yta.1. A rocktrig block. I l I When the block is rotated through an angle e, the weight of the block will exert l a restoring moment II'R sin (a - 0). The equation of motion is then o.p ; I. = -ll'R sin (a - 0) (1) ric. 2' I For tall, slender blocks having the angle a less than about 20* the sine of the angle i ji may be approximated by the angle and equation (1) may be written < uation (3) expresses il ' ~ ll
- 1. 6 - li'R0 = ~ 11'Ra This equation describes the free vibcation of the block. Setting li'R/1. = p', the equation becomes imph of this equation
{
- - pts
- ps, endent upon the am; ; t, and when P./a is cl. 4 This equation, subject to the conditions a = e. and i = 0 at t = 0 which represent g g g j the block released from rest with initial displacement 0., has the solution: 5 the block impacted l i ! 0 = o-(a - e.) cash pc (2) innerement decreas ehalf cycle would b< ^' Equation (2) describes the rotation of the block about the point 0 as it falls back,- ed to be inelastic (no j into the vertical position. The block will then tilt about the point O': and if there is nd the moment of n j I j f ne'gligible energy loss during impact, the block will rotate through an angle 8 ty during impact h i -8., The bleek will then f all back again to the vertical position and will rise about 4 point 0 until e is again equal to 8.. At this instant, one complete eyele will have been. 4 j completed. The time T, required to complete this cycle is the period of free vibra-i 1 i i i i.
i ANALYSIS / CALCULATION f I Doc 10 # S WoS4l ATT #_ 8 REV_ O SHEET k OF- @ l ) { t i tory or autnicA ~ tirnAvion or txyrnTro PtNort.ru sinvercal.s 405 { ty a distance h above the b
- l tion The block will fall from e = e, to e = 0 in a time t - T/4 and at this instant
( a n in fig.1, the radial distant * } equation (2) becomes j ! city is R = VA' + P. Wher. 4 1, the vertical The tilting of the 1 T 0 a - b - e.) conh p 7 t 4 l or i j 1 coth = i 4 1 - e,/a lf 5 -- ~ i )J j i I l 4 \\ l l i 3 i I pga l-A, I, I V t 2 / i i / \\ / \\ t / g / t F' / \\ weight of the block will exert { f motion is then o/ O 0.2 0.4 0.6 0.8 1.0 k e) (1) b. r t 4 x sbout 20* the sine of the angle "'" E "'" may be written Equation (3) expresses the period T in terms of p and e./a ek. Setting IFR//, - p', the ~ 1 - et/a A graph ni this equation is shown in fig. 2 where it is seen that the period is dependent upon the amplitude ratio e./a. When e /a is close to unity the perio long, and when fo/a is close to zero the period is short. , = 0 at t = 0 which represent
- 8.. has the soh on:
l During the rocking of a re.a.1 block there would be, of course, a dissipation o w ben the block impacted on the base. Thus, once during each half. cycle ther i be an increment decrease in the energy of vibration. Consequently, the perio (2) f 'unied to be inelastic (no bouncing), the rotation cont ch half eye e w a d be longer than that which preceded it. If the impact is as. i it the point 0 as it falls back s y i rot rtte h ottgh an angl l 'O' and the moment of momentum about O' is conserved. The re i' isition and will rise about "rny dunna impact,si
- complete cycle will have been
' ~ [5 '#':/ / [\\5 '#') " [\\)";/ j le is the period of free vibra t )/1 \\ I s:T' I / i I I ..~
I I i ANALYSIS / CALCULATION t DOC ID # S M-oS4L ATT # [ REV O SHEET' I OF M_ i i ,I l 400 st't.Lerix or THE stisisotocicAL sotiriv or AllenlCA i Equating the mrment of momentum about O' immediately before impact to that It is seen that fi immediately n!ter impact gives for small oscillat ! ItIIi"*"! I # - OmRbte sin o = le d i (4) ii tion during the f i This gives for the seduction of energy by the impact l l s l l ,nR' (1 - cos 2a ) r= I le t recording to the i l For slender blocks this relation may be written t first there wi i e!- Vr = 1 2mR'a mplitude decre: ! 8 j l
- an increase it.
ocking block [ ji l t l Using the notation v = #/a; p. = 8./a, the displacement and velocity of the block 'd ;1iding invol ' l l 6 may be written l -f, v = 1 -(1 - v.) cosh pl 1.0 ; l j i ) + = -(1 v.)p sinh pt o,g f k .ll At the instant of the n th impact (p = 0, i - f.) i IN ',N 0.6 3 nl cosh pl. = 1 - p... $n i I l ili ""d 0.4 I I!i sinh' pt. - [\\l - v..i/Y-1 I ei Yt 0% a l* sing this relation, the impact velocity may be written: I d @. = - p V I - (1 - 9..i): (5) ' [ o l J Y ( l I i where v. is the amplitude following the n thimpact. The kinetic energy just after j impact is reduced to r times the energy just before impact. The velocity is therefore l l j reduced to VT times the velocity before impact. This condition'may be written i.. l l -pVI -(1 V.)' = -p s/I s/l -(1 - v..i)8 (0)' conditions t i l- ]l. tat. This equation can be written 4 3 r i [ l - (1 v.): r[I - (1 - v.,. ):] = the block'ir ]. and, as this recurrence relation implies, stlog for a "It"d' OI 8 1 - (1 - v.)' = r [1 - (1 - v,i):] a i ecclerat,on i Solving this for v. gives enter of gr;
- v. = 1 - V I - rall - (1 - v.)')
i i l', j A graph of this equation for r = 03 is presented in fig. 3 where the decrease in - seen from t amplitude for successive n is shown for several values of the initial displacement - a/g > a, w [j I 'll'
ANALYSIS / CALCULATION [ DOC ID # 5%054_.L ATr #_ l REV O SHEG 6' O F llo - a 1 407 DEHAVlon oF INVERTED PENDVtNst STRUCTURES or mitnicA , stely before impact to Jt is seen that for large amplitudes the energy of vibration decreases rapidly but for small oscillations the energy decreases slowly. 4 It follows from equations (3) and (0) that the successive half periods of vibra-tion during the free rocking are given by !y I f=2 /g anh-' v'r li - (1 - v.P) t t f" According to the foregoing analysis the free rocking of a block proceeds as follows. l At first there will be a few oscillations of large amplitude and slow rocking. The implitude decreases marked!y with each impact and corresponding with this therc l 'is an increase in frequency of oscillation to an infinite value. Actually, a freely l . rocking block does not make a truly inelastic impnet, but there is a slight bouncing j nt and velocity of the blor Esnd sliding involved. This is another source of energy absorption and under favor. I t I.0 f ,[ r=0.7 ( ..? 0.8 l il O.6 3 1.0 i 4n e 0'4 \\ ~ g O'2 N \\ 1 1 2 Nb ten: jP (5
- +
oO I 2 3 4 5 ,6 7 0 l The kinetic energy just alte [. NUMBER OF IMPACTS l net, The velocity is therefor g, DC" L Amplitude v. subsequent to n.th impnet. } his condition may be writtet q- -(1 - v..ip (6 j,,sble conditions the block makes only some eight or ten impacts before being brought yf to test. h p) i OvenTunsixo av CoxsTAxT AccEtxamos l g If the block is resting on a base whleh is suddenly given a constant acceleration j g o insting for a time t the block may or may not overturn, depending upon the i l _ e,yj g magnitude of a and the duration of ti. For small angles of oscillation the effect of the accelcration is the same as if a force tra/g were acting horizontally through .i g j .f the center of gravity of the block and thus the epation of motion is: L <l.- **d Is # - IPR 8 = IFRa/g - trRa (7) l y e ! n..g. 3 where the decreau ir J.[ lt in *n from this equation that a necessary condition for motion to be initiated is
- es of the initial displ.nenent g that a/g > a, which specifies the fraction of p acceleration required to begin tilting
{ e l i i
408 artttT:s or Tut ritisuoi.ociest soettiv or.o: Ente.s utny ( the block, The solution of equation (I), subject to the conditions that at t = 0 in this equation the p j both the velocity and displacement are sero is f- -1 (coch pl - 1) { u here a is the amplitu<. i I~i hhis insures that a It is s,een that if a/g>a and if the acceleration nets for a suflicient length of time u n ate roe I the block will overturn. It is not necessary, however, for the base acceleration to " **T I ) I act continuously in order to overturn the block. For each value of a there is a time f lI t during which the n:celeration can generate a velocity sufficient to overturn the ) i block. li The conditio,. for overturning is that the total work done by the inertial force 5-11'a/p is just equal to the difference in potential energy between positions e = a i and # = 0. This condition may be written ~ [4 4 ~~ Rll'(a/p)d di = II'R(1 - cos n) (S) i I l Carrying out the integration and approximating (1 - cos a) by a'/2, er;untion l (8) becomes 3 9 (? o' - a ( cosh pli - l ' r, 9 0 ,s y l If this equation is solved for crsh pli, there is obtained ri=1+ (9)h coshir t
- l,
,, s t3 _ n/ ga \\pa l Figure 4 is a graph of this equation giving the duration, ti, of ground acecteration a
- required to overNrn the block.
O r d l The foregoing analysis is not realistic for carthquake ground motions since it. e LO assumes constant ground accelerations of fmite duration followed by a constant velocity of the ground. This type of ground motion does not occur during earth. - 73, (. Constant ji quakes and hence it is not meaningful to discuss the overturniq; of blocks in, terms : of percent p acceleration. olution of this equn 8
- I Ovtatunxixo my Sixesotort Acccounatiox 1
,, _a, 1 n \\ w a The nacelerograms recorded during earthquakes show ecrtain maximum peaks. 7, 1+ ilj whose shapes can be approximated closely by one loop of a sine wave.The question,y, l j then arites as to the amplitude and period of a half sine. wave acceleration pulse j that will suflice to overturn the block, sin ( If the hue is given a sinusoidal acceleration the equation of motion is a 'ndition for overtu } I.# - -it'R sin (a - e) + 11*R f in (wt + () 'ill reach the vah-3 I g ta,ftrst half. cycle 1 e r l1 f, [ ANALYSIS / CALCULATION DOC ID # ".v9 FOS 4l_ ATT # - ./ i
i i j ANALYSIS / CALCULATION Doc to a *AFoS4l ATT # 8 } REV O SHEET _d OF_lb r, l scnAvion or axvontro resort.ex sinectent.s 400 l 't or.uionier 1 se conditions that at 'In this equation the ground acceleration has been expressed by l 1 { i -a sin (wt + () h e 1) ,here a is the amplitude of th'e neceleration and ( is defmed by the condition f JJ a sin ( = p sin a j ( hhis insures that s *1me i = 0 the base neceleration will have reached the value requiied to initiate rocking of the block. For small angles, and setting li'R//. = r a sufh..eient !cngth of tim ..' the equation may be written: p, for the ban acceleration t . I" +N I .ch value of a there is a tlr i - p's - ap' 1 ty sufficient to overturn't 8iu @ ..t k done by the inertial f$r ',)' 5
- y between positions # '
I 4 l l os a) (8 i i f ,os a) by a'/2, equatlo ), t c t, 3 I t, n' k l
- Ti l
2 ~ ld \\ i 4 (9 b -1) f x \\ . I:, of ground acceleration 01 o 2 e 1.0 t2 1.4 1.6 1.8 2.0 ' ke ground rnot. ions since gp g j ion followed by a constao ga l 2es not occur during carth J yea,4, Constant neceleration a of duration (, required for owrturning. l erturning of blocks in term Tbc,,,httion of this equation, subject to, the conditions e = 0, d = 0 at i = 0, is r 8-". _1 'w sinh pt _ ' g g _ sin (wl + ()* gg) t.curriox I "" d 88" Y , sw certain maximum peak 3 1+ i if a sine wave. The restio ine. wave neceleration pul + J sin + = pa/a; cos4 = VI Oa/a)' tion of motion is The condition for overturning is that # = a at time f = (r - V)/w, This insures that P will reach the value a at the instant that the ground acceleration bas com-i twt + () pittal its first half. cycle and has the value zero. O e a ym*-eM wW e==F _*w w w row -w up v--m-s v-v*
- v =v-+=-=s,me-,
em e n eewww- ,e.- -,-.__.%m.,__
nrHAvio st't.t.rm or int stisuot.ocicAt. tocitTV br Autatc4 410 .r Substituting in equation (10) and rearranging terms gives. tan ( = E tanh E (w - 4) (11)t w ,w and this equation specifies the amplitude and frequency of the sinusoidal Steelera d "" '" ' * ### #"E tion puh.e required to just overturn the block, l*nder the conditions of the problem tanh p/w(w - () may be approximated by unity and hence equation (11) may be I written ta" f " h '11)s, nd hence equation (10) f. 'S 2.2 / ~ \\; i 2.0 7 ll j 1.8 7 / i i I $ l.G / 6ere T,is the period e f ' diagonal,2R, the eqt { ,*4 / l / l i.2 / dre K is a constat... { !l; i 6 v i.o s 1
- l 0 02 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 celeration pulse by it '
l' 4 l o'r'a given R. l w p i Fle. 5. Binusoldnt acceleration pulse a sin ut required for overturnino Or l Making use of equation (10) and rentranging terms, equation (11)n can be put in' pje ed ng para ,ninimum accelerat th' I '* ll{r accelerations t' j (12) I l = j[1 + mg but will not ovi E er accelerations if I i of strong motion f
- T 3
' (I2k train of pulses w 1+ l = where T,is the periN of the ground acceleration 'Ihis relation was first det.ved by is periods of stru Kirkpatrick5 and it expresses the conditions under which a single sine puhe w illowing approxb l purposes of illus-overturn the block. As may be verified, this is a rninimum condition as it insures l liserete step chat j A graph of equation (10) is presented in fig. 5 for small values of w/p. For large Lme 0 < 1 < t. l that i = 0 when # = a. li i 'his representa at i-values of w/p, say w/p > 3, equation (10) can be represented by ks'pectrum (un { 2 l. I t ves is the same ;
- / 4 re uting throti !
E F if, s tiltkpattlek, P.. Seismie hicasurements by the Overthrow of Columns " Or ij Seism. Soc, of A mer., Vol.17. No. 2,190r. [ i f i i ANALYSIS / CALCULATION j l i 1 DOC ID # S-9 FOS 4l ATT # / l l ] i C REV C SHEET l O F llo l t i t e--c.+=r.w-,43e-w-eve %,---wwew,w,~~m.v-,..--.%-.
i l ) ANALYSIS / CALCULATION DOC ID # 'AFoS4l ATT # [ i REV O SHEET 80 OF Ib j I I i
- TY or AMEN!CA h
LEHAvton Or INvCHTI,D PENDUtVM sTnVCTUnEA 4II "ns gives! + 5 cr
- )
I ~ Y ij/II7i T, j '.1 T i f t e pr$, %s an example, a mtangular block such as shown in fig. I has the cor d t n ji hence equation (11) nh [d' 4 RJ .v \\p/ 3p i and hence equation (12)b enn be written j h iW /,, j or f a f h Rt1 i / -= l. / / 0' / =a.2rj[hI?; L where T,is the period of the pulso. If we conskler all blocks that bevo a given length l of diagonal,2R, the equation may be written L l' Tf 7 = Na e 1.4 1.6. 1.0 2.0 .i Shere K is a constant. It is thus seen
- hat the product of the amplitude of the acceleration pulse by its duration must he proportional to the slenderness ang'c j
~ a for a given R. i 3nited for overturning. OventunxlNn ny ErnTHQUAKc h!oTioN ! equation (11)n can be pulj De pieceding paragraphs dealt with the overturning of the block by a square j secelerstion pulse and by a half sine. vare pulse and equations (0) and (12) give ,the minhnum accelerations required to overturn a block by such single pulses. (12 Emaller accelerations than are specified by these equations may set the block to ) rocking but will not overturn it. It is, however, possible to overturn the block with v smaller accelerations if a number of pulses act successively. This would be the a j (12) { case or trong motion carthquake ground acceleration, which may be thought of s i !s relation was tint derived b) '. sa a 1am of pulses which, in general, have periods that are short compared to the c, rocking periods of struetmes. The resulting behavior of the block is indicated by lvhich a single sine pulse wiU ithe following approximate analysis. pimum condition as it insure For purposes of illustration, consider ground acceleration composed of a sequence j of N discrete step changes eae in ground velocity, that are randomly distributed , mall values of w/p. For large .(over time 0 < l < fi, and have equal probability of being positive or negative in resented by sign. This represents an idealized earthquake ground motion whose average velocity l ? '051 muse spectrum (undamped) is a constant. The effect of such ground motion on j O 21 structure, is the same as if the ground were at rest and impulsive inertial forces
- h. tow of columns," to u. of d
{ "" # "E "E I " I' ' I"'""'" '" j ,6. F.at = &Mu (n = 1, 2 N) ( I
ANALYSIS / CALCULATION ooc ~ 7 S 9 fos 4L ATT # P j . REV.) SHEET ll OF _ Ib s 4._- 412 st1.ttTax or int scisuot.ocicat soctcrY or Asignica stn' vion The respora.e of a linearly clutic structure, such as is shown in fig. 6, to the randorn The energy lou per cycle i succenion of forces F. is to be excited into oscillations. The effect of the n th irn. r'setion of criticaldamping puise, T.at,is to produce a change in velocity or, and benee to produce a change in 'f' energy loss is then 4d I, kinetic energy of vibration or the system then is8 aKr. - } 3f(r. + ar)' - } Alr.' = Alt. (Ar) + ) 3/(or)* 'he solution of this equati l ~~~ where v. is the velocity of the structure at the time that F.at acts, If a large num. [ ber of such idealized earthquakes were to act upon the structure, the aKE. would, pi I x The average energy of / c , sever, for each individu: =1, i M ,edding uo,m how the impi l j = 41 be a certain probability i The behavior of a rocki l .tnitar to that of the linen: l 4 o the energy of vibration k ~ dshown in the analysis o' ; sepends upon both the am, nplitude of the block exec ! these differences are brou ; l l If the rocking block is si j l lange in kinetic energy pri I Tao. 6. Simple linear structure, } in general, be different for each of the carthqunkes. Ilowever, the average incre- [ slender bodies, having. nent change in energy, AKE., averaged over all the carthquakes would be y KTG. - 3/ r.(ar) + 13f(or)' and since C, the average velocity is sere, and the average Te is also sero, it follows j that d hence I'RE - {3f(ar)' C
- AKE, On the average, then, the totr.i energy of vibration of undamped structures is l
)
- f. = }3/(arVn (n - 1, 2 - N).
d the ensernble average { This represents e.n average building up of energy with the number of pulres add j l hence the ave: age rate of energy input, P,is ere were no energy lor _P=dAl(Ar)'E the average la .t This constant power input P will cause the average amplitude of vibration to in, t crear.e prop 0rtional to NT. If the structure has viscous damping, the power input, P, will build up thel Juf*on. .gtesgopll' amplitude of vibration until the average rate of energy loss just balances the mput. be,,,w30. ,j j i m . = =
ANALYSIS / CALCULATION Doc to W9'l-oS4l ATT # 8 REV O 5HEET ll OF Ib 'i stuAvion or tuvtnytp trNow:w sinvert ats 413 I[ or wenics l su n in fig. 0, to the rando N. The energy loss per eyele for a linently damped oscillator is 4rkE, where A is the The encet of the n.th im ,1 fraction of critical damping, and E is the energy of vibration.The average time rate
- nee to produce a thange f.' cf energy loss is then 4r A f/T, where Tis the period of vibration. An energy balance
[ for the system then is' 't.( U =P-hB (13) I 't a The solution of this equation is l .t F.at acta. If a large num i 4 structure, the aKE. woul f= 1 exp g l t The average energy of vibration thus increases asymptotleally to PT/4rA; { _. ' bowever, for each individual earthquake the energy may be larger or smaller de- {. pending upon how the impulses happen to strike. For individual earthquakes there l I
- will be a certain probability distribution of E about the mean B.
[ ,( imilar to that of the linearly clastic structure in that the impulses te The behavior of a rocking block subjected to a series of remdom impulses is l s l tup the energy of vibratim. and hence the amplitude of the motion. Ilowever, as was shown in the analysis of the frco vibrations, the er ergy dissipation of the block r i k l / depends upon both the amplitude and frequency (. rocking. In addition, if the I s amplitude of the block cxeceds a limiting value the block will overturn. The clicct cf these dinerences are brought out by the following approximate analysis, j If the rocking block is subjected to the series of random pultes, the increment { change in kinetic energy produced by F.at is i aKE. = {l. (d. -F od.) - { t d.' l v"- Ilowever, the average incre Tor slender bodies, having //I, er 1, we may write approximately arthquakes would be f ,g ~ A'Y 0#* " RF. at RMao 3 rage li is also seto, it (0110' 1, f, nd hence aKE. - MR(ar)d. + k (DIRY zg,ys le l >f undamped structures is .and th" ensemble average is (n = 1, 2
- h cith the number of pubes ari E-(av)'
le i If here were no energy loss during the rocking, the buildup of energy would give j t on the average 8 e amphtude of vibration to i
- f. = AW. = f le (ae)'n
Iufu j >< mput, i,, a. t duild uy ' L' 8,g'.n. D. r>, ".Re,spuiue Spectrum Techn,iques in,Enginee,in : Se , u.,a c,,,,,,,,, t., %..i.,,,,,.,,, c.,,,,e 1, !.gy loss just balances the inP fi. j-V
l etn4vio uct.t.trix or int scisuot.ocicAt. society or wenics. This may be compared w 414 l The mi energy required to overturn the block is , the denominator of th-I
- .pj efs nti.tily the same forn PE 11 R(1 cos a) = y e
On the arcrags the condition for everturning at the end of N pulses is - f I' N ( Ar)'N (14) On the other hand, when $,N J = li'R/?a') the den . ! ?... _.... _ 3 equation (10) may be ne or a ,1[N# ITid ( Av)v/R l. 1 i l Wben the idealind carthquake mntion satisfies equation (15) there. is a 50 per cent this case the block probability that the ground ruotion will overturn the block, Jf a is greater than the .juivalent fraction of i j l quantity on the right side rf equation (15) the probabihty of overturning is'len jf don 50 per cent, and F, is smaller than this quantity the probability of over. 4cking increases, the ta >r'omotes an increased n Ee behavior of the roci ; turning is greater. If tice h an enc %v len Ort.ig the rockira of the block, with a fraction rE of j* j round motion may for ' l the energ W vhcs'e bfcc3 ost at each hnpact on the base as described by equa. lf l round motion and lead tion (5), nr. e.wrpy bbnce would te luire Errn ' .pl'f The stability of a roc : j energy input with the ei i with T, as deftned by equation (4), given by computed from the ! 4 l T=4 cosh iotion the requirement ' 3 6 l P 3 j a -) The potential energy of '.he freely roching block is PE - 11'Ra' #.'.-f and for the forced vibration of the block the average instantaneous amplitude of + l rocking, e., is defined h"v is, seen that this h: as a vake ch j l e l ; 'f s f = II'Rd j L l [ r t-l or ~ is; equation may bt I ( f. 1 , [g, 2a'8 4 ock having an ang l a ll'R 'b" ability of being os i The energy balaner tan then be written length R and no ci l j Is't overturning is ' s,N d,, p.,, Pr8 i10) S,the larger block J l 08 2a8 g e,effect which is ]h 2 M*,} li7i l l! l V t '. t; L I ANA'.YSIS/ CALCULATION l l
- f. '
00C 10 # 5'9F054l ATT # i hEV O SHEET 13 oF flo i
REV O" SHEET __lT_ OF lb i r 415 j l or Autnic4 ' BEHAY1on of INVENTED PENDUt.Uht STI,UCTunts t r g g ) y gnav ix compared with equation (13) for the clastic structure. For very small f!,, .;I h*tbe d'enominator of the right side approaches a value of 2 and equa _ ntially the sarne form as equat on (13): i + I =P- , of N pulses is i d the other hand, when the amplitudo of vibration approaches the unstable point j I J IrR/2a ) the denominator becomes extremely large n.d the last term in t .} dustion (10) may be neglected and the equation written b 62 t bg i (15) there is a t,0 p-4 1 l >ck. If a is greater tha. dthis case the block is effectively undt.mped. It is thus seen that, although the ,ility of overturnih duivalent fraction of critical damping remains constant, as the amplitude of
- y the probability (o" 6 eking increases, the rate of energy dissipation decreases strongly and this in turn h
piomotes an inercased amplitude of vibration. It may, therefore, be expected that lock, with a fractiony. th'e behavior of the rocking block could be quite variable in that relatively small base as described by)" af6cnd motion may fortuitously build up the amplitude at the beginning of the q j?ound motion and lead to overturning the block. m*- Errter or St.csoenstsa oN OvenTUnstso L Nhe stability of a rocking type of structure may be estimated by comparing the Puergy input with the energy required to overturn the structure. If the energy input (computed frcm the velocity response spectrum, S., of the carthquake ground f-Motion the requirement for overturning, equation (14), is 4 j 1rRa' = S.' } or' ' r s 0 (17) a= instantaneous aniplitud, -J e
- i. seen that this has the same form as equation (15). For slender structures g[RWe has a value close to '.mity so that equation (17) can be approxim I
S 4 (17)a l n j This equation rnay be interpated as stating that for a given spectrum value S.. i
- block having an angle a given by equation (17)a will have approximately a 50%
j Probability of being overturned. The dimensions of the structure enter only through { 4e length R and as equation (17)n shows, the larger the value of R the more stable against overturning is the block. That is, comparing two blocks of the same propor-I0hs. the larger block is more stable than the smaller. There is thus an unexpected jP \\ 1 I'"Ic Hiert which is explained by the fact that the ground motion is not scaled i i S j i j
410 svLt.ctix or inc sessuot.ocic41. socitTv or. AutnicA uru4vi with the block. !! equations (17)a, (9), and (12)a are compared. netting AIR',l., This v.nlue of 5, gives SO 1 and a = b/h, there is obtained for small a sult is independent of the tank is completely h 6 = S. jTh Earthquake motion: speriente with earthq 03 ft see represents stront Square pulse: b=I he required S, to give a ~ 1 + <j/1 + A 6o Sine pulse: j1+3 g may be concluded, thi l j/ p ) nk would remain stan,1 Its that stretch and a ; obability that the tant ; i lf ball tanks have tem l tain probability that 4 i WI eg l . tion having S, - 2.0 : For comparison, supp< l t it cannot rock but ei i l 'this case the maximur ' l l l h I g ,s the tank should be. { ~D uld be advantageout r
- ever, a 50 per cent pi l s
i l ry design. At prcSent ified small probabillt) he sloshing water in I Fio. 7. Golf t.all.on.n.tce elevated water tunk, i i lt is seen from %ese equations that the semiwidth b required for stability does not. or of the structuri j l Increase linearly with h as physical intuition indleates, but is affected less strongly. l or in other words, tall slender structures are more stable than might be supposed-firee oscillations o Got.r Brt.t, WAtta TANK ' 't ohh ration, by a s, gle i m i l Let A be the height of the tenter of gravity and D the diameter at the base as ,it is shown that i i shown in fig. 7, and suppose that the structure is rigid and is free to rock (no anchor geometrically simi I l bolts). For a structure of such proportions h may be taken equal to R, and I, may that the stability < I be taken equal to AIR'. Equation (17) then becomes greater than would I ' D S, n the light of then " " sh " 7pl 'ently hignly unsti l Of MA Iwst:Tvts or Ti ) /* A, CAurnsi4 S, = ;1 D,j/ { j 1 eript received April ; ANALYSIS / CALCULATION 00010# S*9 FOS 4l ATT # l l ncy b SHEET I5' OF 10) i a
ANALYSIS / CALCULATION DOC ID # 'NOS% ATT # [ REV O SHEET,__ hp OF LIE _ or monter senavion or tuvtutzo trxoct. tar stacerting 117 .mpared, sett!ng Nh'/le ' This value of S. gives 50 per cent probability of overturning, and it is seen that the result is independent of the mass; that is, the stability is not affected by whether the tank is completely full or completely empty if h may be taken to be a constant. i pperience with earthquakes in ti o United States indicates that a value of S. = l 'J ft'see represents strong ground motion > If the tank has A = 100 ft and D = 10 ft, 2 in the required S, to give a 50 per cent probability of overturning is i / + 94' t /p 4 S. = 3 4/ g = 2.0 ft/sec l 'It m3y be concludet', therefore, that for an S. = 2 f t/sce,it is more likely that the !p 7' . tank would remain standing than that it would overturn. If the tank has anchor ' bolts that stretch and absorb energy during the rocking, there will be even less (probability that the tark will overturn. It is, therefore, not so surprising that some i golf. ball tanks have remained standing during earthquakes. There is, of course, n i l /certain probability that a tank nf these proportions will he overturned by a ground motion having S. ~ 2.0 or even less than 2.0. 2 Tor comparison, cuppose that the tank is tightly anchored to the foundation so i at it cannot rock but can only hend and that the period of vibration is 3 seconds. l th $1n this case the maximum hhcar force generated wnuld bc i f F= MS, j and p l l F 2w S, 2r 2 p = 7 - 7 g = 0.13 s l Thus the tank should be designed for 13 per cent p. It might appear from this that it would be advantageous to design tall slender structures to act as rocking blocks; i l howeser, a 50 per cent probability of survival for a rocking structure is not a satis. j factory design. At present it is not known how to design a rocking structure to have specified small probability of failure. It may also be noted that,if the tank is partly j t tak-i full, the sloshing water introduces another mode of vibration which will affect the behavior of the structure. 2 ired for stability does no i at is affected less strongly ,/ Semuny i than might be suppose- ((The free oscillations of a rocking block are analyzed and the rocking period and l energy lon are set forth. The overturning of a block by a constant, horizontal .seccleration, by a single sine pulse, and by an earthquake type excitation are ex. ie diaructer at the base s { 3 is free to rock (no aneb ,amined, it is shown tha' there is an unex'pected scale e!Teet which makes the larger of two geometrically similar blocks more stable than the smaller block. It is also j en equal to R, and I. ma shown that the stability of a tall slender block subjected to earthquake motion it, inuch j forec. greater than would be inferred from its stability against a constant horizontal ] In the light of these facts, the occasional survival of a slender structure that j is apparently highly unstable is not surprising. S'urohm I.sstnvu or hecoLocr j P^** us,CAUFOR m ? f anu eript received April 12.10G2. s j 1 I
f ~x ( D DESIGN ANALYSIS / CALCULATION h.... ' C.I Crysta River Unit 3 Page j / of /6 DOCiWINT IDtNf fiCAtlON No ngvisioN S97 0541 0 i Q i ATC-10-1 " Critical Aspects of Earthquake Ground Motion and Building Damage Potentisl" RGr M M 0M ut: u.., mm = *. %. %~,,,
t t ATC-10-1 CRmCAL ACPEC11i OF EARTIIQUAKE GROUND M0110N AND DUILDING DAMAGE POTENTIAL ANALYSIS / CALCULATION DOC ID # 97V64l ATT # h 5 REV O SHEET M.OF :lO susar t. erso gude) Funded by NATIONAL SCIENCE FOUNDATION Grant No. CEE-8303552 and UNITED STATES GEOLOGICAL SURVEY Orant No. 14-08-0001-0-797 Prepared by APPLIED TECHNOLOGY COUNCIL 2471 E. Bayshore Road, Suite 512 Palo Alto, California 94303 PROJECT STEERING COMMITTEE Christopher Rojahn, Co-Principal Investigator Eric Elsesser Roland L. Sharpe, Co-Principal Investigator William J. Hall Vitelmo V. Bertero Jon D. Raggett 1984
OVERTURNING Op SLENDER RICID BODIES DURINC EARTHOUAY.ES by ANALYSIS / CALCULATION Roger E. Scroll
- DOC ID #S*O *064l ATT #
O REV O SHEET. 2. OF 10 I NTRODUCTION, The pu.r:*e of this paper is to demonstrate why, in general, buildings do n.it overturn J9 ring earthquakes. Conversely, the article shows that tomb-stones having similar aspect ratios as some buildings can be expected to overtcrn during earthquakes. Tombstones have been observed to commonly overtutu during severe earthquakes. For many decades the structural engineering community has labored the issue of overturning. Simple static analysis, based on force analysis and fol-lowing the logic of the equivalent lateral force analysis procedure, commonly implies carthquake overturning instability for tall slender build-ings. Numerous post-earthquake investigations have failed to reveal a single incident where a building has overturned, however. The commentary to the " Recommended Lateral Force Requirements" provided by the Seismology Committee of the Structural Engineers Association of Cali-fornia (SEAOC, 1980) provides a number of arguments t3 reconcile the apparent overturning instabil1ty condition hat results from the high base shears presently prescribed in the recommendations, but the issue is not yet resolved. Specifically, reduction of overturning moments as a means of reconciliation is att11 being considered and it is therefore important that this issue be resolved. TECHNICAL DISCUSSION Houaner (1963) provided the basic mathematics for evaluating rigid block motion during earthquakes. Although his work is in a sense complete, the mathematical expressions he provided do not yield an easily comprehensible interpretation of the fundamental reason for why some blocks overturn dur-ing earthquakes while others do not. Accordingly, the following is only an
- Technical Director, Earthquake Engineering Research Institute; and Vice President, URS/Blume Engineers, San Trancisco.
10$ 't
. _ _ _ _ _. _ _ _ _ ~~ i i elaboration of Housner's work: and all the_ assumptions in his treatise apply here.- yor " Overturning.by Earthquake Motion" Housner's Equation 17(a) is as follows: ANALYSIS /C ALCULATION i sv Doc to #5 t-oS41 ATT.? O Housner's (17a) REV O SHEET._ $._01 lO .wheret an angle defined in Figure 1 (rad) a = S =- response spectrum velocity of the earthquake y motion (es/sec) the acceleration of gra'rity (cm/ cec ), and 2 g a the radial dimension defined in Figure 1 (cm) R = F From Housner (1963) "This equation may be interpreted as stating that for a given spectrum value. F, a block having an angle a given by Equation (17a) y will have a 50% probability of being overturning." For small angles (less than about 20 degrees), a a b/h and R s h and Housner provided the following expressions for earthquake motion 5, 4Tg' b = (1) wheret b the one-half base dimension of the block as = defined in Figure 1 (cm), and h the one-half height of the block as defined in = Figure 1 (cm) Equation (1), or Housner's Equation (17a), can also be interpreted in terms of kinetic and potential energies. If a slender block, initially upright -and at rest, is'given an initial velocity just sufficient to rock the block to the. point'of static instability, then equating the initial kinetic en-ergy of the block to its-increased potential energy at the point of unsta-
- 106-t
- _ - - _ _ = _ _ _ _ _.. _ _ _. _. _ _ _. _ _ _ _ _. _ _.. - - t l ble equilibrius produces Equation (1), with 5,in-the place of the initial -f velocfty. Further assuming that 8,.approxiiiates the maximum velocity of -j the block when passing through its stable static position produces Equa-i tion (1). -i Rearrangement of terms in Equation-(t)'yleidt the followingt l 4 52 8 abg (2) o. 4 If the maximum portion of the response'is approximately sinusoidal with a l s natural frequency of w(rad /sec), then the following approximations are re.- d sonably accurate 0Jenschke, Clough, and-Penzten, 1965): Y JS (3} = d ANALYSIS / CALCULATION DOC !D # S-91-0541 ATT # O and-REV O SHEET. 4-OF 10 [S (4) S = y 1 where: 1 the angular velocity of the earthquake motion L w = (rad /sec2) d the response spectrum displacement of the S = es 'chquake motion- (cm), and i S, the response spectrum acceleration of the = earthquake motion-(cm/sec2)- i
- l Combining Equations-(3) and (4), yields S2
- SS (5) v-ad ? - Substituting Equation-(5)Jinto Equation (2) yields: abg (6) - S,Sd Ja - '= 107- ,u,,.J,m ~r.-
- 1w..
y. y y e ..e-v, .,,,c,s, e.--+-, <w,,m-.-,, --,-,.e..,%. -w-,r,--,,-.-~,,.,,+wev---
_ _.-__. - _ _ _. ~. I m Tar ccevanience Equation (6) can be exprested alternatively ast 9
- Sd:
ab- = (6a) 1 From Equation (6) we now see'that the' condition for overturning is that the
- product of (S,S ) be equal to or greater than the product of (b g/h).
d 2 To explore the physical interpretation of Equation (6), consHer the case where S, is just sufficient to cauwe overturning in the ek ssical statics analysis sense. From Figure 1, the statical analys.is equation for over-turning.is as follows: WS
- h - Wb IH 0
= = 4 o g (7) ANALYSIS / CALCULATION therefore: DOC ID # S-97-o641 ATT # O S REV O SHEET _.fi OF.10. = T=a ( 7a ). Substituting Equation (7) into Equation (6) yields: Sd b a when S, = (8) i The physical interpretation of Equation (8).is that when S , is just suffi-cient-to cause overturning in 2.statical analysis sense, Sd must be equal to b (one-half the base dimension of the block) to produce a 50% probabil-ity of overturning. If S, is just sufficient to cause static overturning, the block will start to rttate; however, if the block is to overturn, its displacement, as approximated by S, must reach the point of instability, b. d Equation (6) indicates that two dynamic motion parameters must be consid-ered for evaluating overturning;_namely,'the product of force and displac ment. The product of force times displacement is a measure of energy This conclusively demonstrates that using acceleration only as th e indica-tor of earthquake demand is not sufficient e for.eyaluating' overturning dur-108 e a 4 y
h ing carthquakes and that en energy-based cha*acterization of ground motion must be used.- Housner's statement that "There is an unexpected scale-effect which is ex-plained by the fact that the ground motion is~not scaled with the block" is precisery correct. Using Equations (6) and (8) above, one can readily de-termine the scaling effect. In general, Sd is never large enough to:cause a typical building to overturn. Convarsely, Equation (6) c.an be used to evaluate the S, and Sd conditions under which smaller rigid blocks, such as tombstones, will overturn. To provide further elucidation of the issue of overturning, consider the example of a tombstone having a base width of 20 cm and a height of 100 cm and the respont.e spectra curves in Figure 2. (5% damping may be slightly high for a tombstone; but little if any information appears available on damping in connection with rigid block rocking.) For the example tombstone a is C.2. Accordingly, a simple atatics analysis would dictate that the tombstone should tip over at accelerations greater than 0.2g. On r. hat basis alone, tombstones would be expected to overturn for all three of the ~ ground motion demand situations depicted in Figure 2. Using either Equa-tio: (2) or (6) above, S = (S,Sd = 44.3 cm/see for the example tombstone. y It can be readily seen in Figure 2 that the toubstone would not be expected to overturn for the Rulison underground nuclear explosion event, but would be expected to overturn for the El Centro 1940 earthquake spectrum and the Imperial Valley-1979 earthquake spectrum. Lee (1983) confirmed that tomb-stones did not overturn at Grand Valley, Colorado for the Sulison event, Jones (1983) stated that several tombstones overturned durin'g the 1979 Imperial County, California earthquake. For a building having a total base width of 100 ft and a total height of .400 ft, there would be a 50% probability of overturning when S y 611 em/sec. This is a very high response spectrum velocity and whether or not such a high value is possible has not yet been established.
- However,
.for a Newmark, Blume and Kapur (1973) response spectrum shape normalized to 1.0g peak' ground acceleration (and for 0.5%-damping), the maximum S does y approach 500 cm/sec. (Housner and Jennings,-1982.) ANALYSIS / CALCULATION 109 DOC ID # S-9FO541 ATT # O V REV O SHEET : to OF 1O + en
ANALYSIS / CALCULATION 4.i DOC ID # S* WOS41 ATT # 6 -4 REV O SHEET 1 CF 10 . CONCLUSIONS AND RECOMMENDATIONS' ): ~The-technical discussion provided above shows that buildings of common _ practicable-dimension will not overturn during typical earthquake excita-tion. The explanation provided also shows why smaller objects such as tombstones do overturn during earthquakes. The critical parameters are the-earthquake demand acceleration and displacement; and the aspect ratio and base dimension of the rigid block. More specifically, the response spec-trum displacement has to be in the range of one-half the base' dimension of the structure to cause overturning. (The precise spectral displacement required also varies with the spoetral acceleration, the rocking period, and the aspect ratio of the. structure, however.) Although this study has revealed why typical buildings do not overturn, this must not be interpreted as a reason for introducing a lateral force reduction factor for design.- Building members do experience the forces implied by spectral accel'eration and the deformations implied by spectral displacement-(depending on boundary comditions, capacity, and ductility, of course). A detailed discussion of rocking effects on foundation design for rigid rocking blocks is provided by Psycharis and Jennings (1983). Rocking effects on a flexible structures are described by Psycharis (1983). The most important conclusion to be drawn from this evaluation is that con-si;eration of either S, or Sd alone as the earthquake demand is not suffi-cient for evaluating overturning. -Either the product of S, Sd or S must y be considered. These are both energy-related terms, and the necessity of using an energy formulation for evaluating earthquake overturning of struc-tures is demonstrated. Additional research is needed to reveal appropriate values of damping for various rocking structures. ACKNOWLEDCMENT The authr* is grateful to Professor Paul C. Jennings of the California Institute of. Technology for the constructive comments he provided following his review of the draft of this paper. 110
.~..~. ANALYSIS / CALCULATION.' Doc to #117-os4/ATT #- G REFERENCES REV-0- SHEET d OF A 'Housner, C. W. (1963),:The behavior of inverted pendulus structures during? -earthquakes, Bulletin of The Seismological ~ Society of America, Vol. 53, No. 2, pp. 403-417, February. k Housner, G. W. 'and P.C. Jennings, (1982), Earthquake design criteria, Earthquake Engineering;Research institute, Berkeley, California, 140 p. 1 Jenschke,"V. A., R. W. Clough, and J.-Penzien, (1965), Characteristics of strong ground motions, Proceedings of the Third World Conference on Earth-quake Engineering,.New Zealand. i jJones,- D. (1983), Personal communication, Evergreen Cernetary _ Manager, El Centro,' California. Lee,'L. A.' (1983),-Personal communication,'Rulison Underground Explosion Structural Effects Evaluation Mana.ger, URS/Blume Engineers, San Francisco. l: Newmark, N. M., J. A. Blume, and K. K. Kapur, (1973), Seismic' design spec- "'s for nuclear pover plants, Jnl, Power Division, ASCE, 99:P02, November, 287-303. Psycharis, I._N.,_and-P. C. Jennings, (1983), Rocking of-slender rigid bodies allowed'to uplift,: Earthquake Engineering and Structural Dynamics, Vol.-II. pp'. 57-76; Psycharis, I.-N.-(In Press), Dynamics of flexible systems with lift off.
- SEAOC,--(1980), Recommended lateral force requirements and commentary. -
l ' Structural EngineersiAssociation of California, San Francisco. T' 111 [~ .a -- +.
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1 Information copy of:
Stevenson & Associates Letter, dated a/r/97
" Confirmatory USI A46 Evaluation of Selecte Safe Shutdown Equipment at CR3" e
R : Ls'e Of P M RE$P' NucinF IMW A
~
DOC ID # fT/'OJW ATT # _
REV 6
SHEET 2 OF /I uStevenson & Assodates
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.. w ~ au or a ummmo rumme m A structural.meehanical consulting engineeringfinn BOSTON CLEYELAVD December 9,1997 Florida Power Corporation 15760 West Power Line Street Crystal River, Ficrida 34428-6708 Attention: C. Glenn Pugh, P.E. Senior Structural Engineer, Nuclear Engineering Design
Subject:
Confirmatory USl A-46 Evaluation of Selected Safe Shutdown Equipment at Crystal River, Rev.1
Dear Mr. Pugh:
An assessment was petmed to ensure the completeness of the USl A-46 evaluation conducted by Florida Power Corporation (FPC) and its contractor, Programmatic Solutions, Inc. This assessment was prompted by comments offered by the United States Nuclear Regulatory Commission (USNRC) regarding the completeness of the Crystal River Unit 3 (CR3) Plant Specific Procedure (PSP) developed to address the USl A-46 requirements as compared to the Generic Implementation Procedure (GIP) developed by the Seismic Qualification Utility Group (SQUG) and approved by the USNRC via a safety evaluation report. The asseument focused on three specific areas of NRC ccncem: A caveat compliance study to atsure that the GIP caveats not explicitly included in the PSP were in fact considered during the walkdowns. An anchorage study to perform representative and bounding anchorage calculations for each class cl equipment to assure that the PSP ev'aluations based on engineering judgment are sufficient. Addressing anchorage concerns on specific equipment raised during the NRC Audit of the CR3 A-46 program. To assure a degree of independence, Stevenson & Associates (S&A) were contracted to perform these assessments. The results of the assessments are presented in the following sections. 1.0 GIP Caveat Comoliance Studv One of the key differences between the CR3 PSP and the GIP methodology was the exclusion of some of the bounding spectrum GlP caveats. Although a limited number of caveats were not explicitly included in the CR3 PSP, the Seismic Capability Engineers \\
AN AL.YSidNALoutm im DOC ID # - f?7 OfW - ATTe_/N REV O SHEET 3 OF /f (SC6) performing the assessments were experienced SCEs and generally kept the caveats in mind. As stated to the NPC during the USNRC's on-site audit, the SCEs considered that no caveats had actually been overlooked, and that if an important caveat not included in the PSP was not being met that it was (would have been) noted in the Screening Evaluation Work Sheets (SEWS). It is noted that review of the PSP SEWS found several examples of comments which specifically address concerns related to the exc!uded GIP caveats. To respond further to the USNRC concerns regarding GIP caveat compliance, FPC decided to address the aforementioned concerns by selecting a 10% equipment sample of the r~afe shutdown equipment list (SSEL) for a rigorous GIP evaluation. Equipment from each of the twenty equipment classes was randomly selected for this evaluation. Mr. Walter Djordjevic of S&A was retained to perform these walkdowns and performed the assessment in the following manner: Each of the selected SSEL items were walked down using the appropriate GlP caveat SEWS for the class of equipment. Emphasis was placed on caveats not included in the PSP SEWS. After completion of the walkdown, the PSP walkdown SEWS were reviewed versus the GIP walkdown notes to assure that all concerns were identified and properly addressed. Table 1 provides a list of the equipment that was walked down and the results of the GIP caveat compliance walkdowns. The conclusion determined based on the sample walkdown was complete concurrence with the results of the A-46 assessments made using the CR3 PSP; that is, (1) no additional outliers were identified, and (2) all concerns associated with excluded caveats were addressed by the PSP walkdowns. 2.0 Anchorage Assrsment Samole Results in addressing the seismic anchorage adequacy of equipment, the CR3 PSP allows for engineering judgment to be used to assess a great deal of the equipment anchorage. The USNRC requested that anchorage evaluations be performed for some specific equipment and that some bounding calculations be performed to provide a degree of assurance that the expert judgments made during the PSP walkdowns regarding anchorage adequacy were, in fact, correct. To respond to these issues the following anchorage evaluations were performed: A set of bounding anchorage evaluations were generated that are representative of the class of twenty SSEL equipment evaluated by engineering judgment. Anchorage evaluations were performed for four specific equipment items observed during the NRC on-site audit walkdown for which the NRC had specific questions. Two outliers (unanchored electrical cacinets identified during the CR3 PSP A-46 walkdowns) were evaluated to demonstrate no short-term operability concerns since they are scheduled for modification to resolve the unanchored condition after plant restart. \\
i ANALYSIS / CALCULATION DOC 10 #,_.f77 Off/ ATT C ,7 2i Bounding Case AnchoragtEvaluations For the bounding case anchorage evaluations a set of equipment was selected from the equipment classes for which the anchorages might control the seismic adequacy. The evaluations used the generic equipment enaracteristics found in the GIP (estimated weights, frequencies, etc.) and typical methods used in GIP anchorage evaluations, in general, the equipment evaluated included most of the electrical equipment classes and excluded most mechanical equipment since they normally exhibit high seismic margins of safety with respect to the anchorage allowables. An anchorage calculation was performed for a representative item for each of the following equipment classes: Equipment Class 1, Motor Control Centers Equipment Class 2 Low Voltage Switchgear Equipment Class 3, Medium Voltage Switchgear Equipment Class 4, Transformers Equipment Class 14, Distribution Panels Equipment Class 16, Battery Chargers and Inverters Equipment Class 20, Instrument and Control Panel and Cabinets To make the anchorage evaluations bounding and enveloping, the following procedure was used:
- 1) Equipment at the highest elevations for any given equipment class were chosen to clearly bound the seismic demand on each equipment class.
- 2) The representative anchorage pattern was selected for evaluation. There is some uniformity for most of the electrical equipment anchorages within each class which facilitates such an approach.
Table 2 provides a list of equipment for which these representative and bounding anchorage assessments were made and presents the results of those assessments. All bounding case anchorage evaluations demonstrated compliance with the GIP allowables even with the conservative assumptions used. 2.2 Anchorage Evaluations for Soecific Eauipment Four equipment items for which the NRC had specific questions were included in the evaluations to specifically address the NRC concerns. The following paragraphs present a description of the equipment, the results of the evaluation, and a conclusion for each of the four items, m MTMC-18 -- 480V Reactor MCC-3A2 Discussion - This MCC (equipment class 1) has ten units, each 20" wide x 20" deep x 90" high. The irdividual sections are all bolted together, it is located at Elevation 95'-0"in the Auxiliary Building. The anchorage consists of 1/4" fillet welds to embedded steel along the front of each cabinet, and along the outer sides of the two end cabinets. There is no anchorage along the back of any of the cabinets. Results - Results of the evaluation indicate the welds along the sides of the end units are sufficient to resist overturning of the cabinet during SSE earthquake 3
ANALYSIS /OALCULATION DOC ID # SM"OTT/ ATT # f O SHEET E OF 6 REV with a minimurn margin of about 7.2 with deadweight effects neglected. The embedded steel consists of C4x7.25 channels anchored to the concrete with 1/2" diameter Phillips Redhead Self Drilling anchors spaced at 30" on center and does not control the anchorage capacity. No credit was taken for possible resistance to overturning provided by the rigid conduit and cable from the top of the MCC. Conclusions - The calculation shows the anchorage is acceptable. (2) MTMC 480V ES MCC-3A3 Discussion - This MCC (equipment class 1)is located in the Auxiliar/ Building at Elevation 119'. The NRC concern with the anchorage of this MCC was relative to the adequacy of the installation of the bolts attaching the cabinets to the anchorage steel. Results - Detailed anchorage drawings for the cabinet were obtained and reviewed. The cabinet is secured to welded base angles by 64 drilled and tapped 1/2" x 2.5" Gr. 5 bolts. The welded base angles, in turn, are secured to the floor by eighteen 5/8' x 8.5" long Phillips wedge anchors. This anchorage design is clearly an engineered and substantial anchorage and is considered acceptable by engineering judgment. Conclusions - The anchorage is clearly robust and no further calculations were deemed necessary. (3) VBIT-1 E -- Dual Inout Inverter 3E Discussion - VBIT-1E is an inverter (equipment class 16) located in the Control Complex at Elevation 108'. It is contained in a 56' wide x 28" deep x 75" high steel enclosure, supported on four C3x4.1 channels. The two outer support channels a e anchored to the concrete floor by 1/2" diameter expansion anchors. One support channel has two expansion anchors through the flange, and the other has one through the flange and one through a friction clip, f,sults - For the evaluation the friction clip was assumed inactive (i.e., this bolt was completely ignored). The calculation using three active bolts indicates the anchorage to be adequate for an SSE earthquake, with a minimum margin of about 1.06, controlled by shear and tensi6n on the expansion anchors. Weak way bending was checked, assuming only the outer two channels resist, and did, not control the anchorage capacity. Conclusion - The calculation shows the anchorage to be acceptable. (4) AHCP SCR Cabinet for AHHE-4A and AHHE-4B Discussion - AHCP-4 is a control cabinet (equipment class 20) located in the Control Complex at Elevation 164'. Six anchor bolts connect the cabinet base plW to the foundation pad. The concem is with the flexibility of the base due to the base plate. In effect, the base plate strength governs the seismic capacity. 4
ANALYSIS / CALCULATION DOC ID # /f/*OIF -' ATT # [ REV W _ SHEET l_ OF I _ Results - Because this anchorage is poor design practice and because the fix is simple and straightforward (for example, a large washer or small baseplate at each anchor to distri Jte the load into the cabinet base), this cabinet has been declared an outlier and will be modified to improve the anchorage design. Conclusions - Since the anchorage system represented a poor design and a fix to improve the situation is minimal, it was decided to address the concern by a modification. Two electrical cabinets, MTMC-12 and ER1, were found to be poorly anchored or unanchored during the PSP walkdowns. MTMC 12 is a MCC located in the Turbine Building, and ER1 is a control panel located in the Control Room. Note, for the latter no ancherage could be identified during various walkewns, and hence it was declared unanchored. These cabinets were declared outliers due to lack of good anchorage and L are scheduled to be modified post startup. They were evaluated during this assessment ' to demonstrate that no short term operability concems exist. The following paragraphs present a description of these equipment items, the re:ults of the evaluation, and a conclusion for each of the items. (a) MTMC Motor Control Center Description - MTMC-12 is located at Elevation 119' of the Turbine Building. It consists of fourteen units,20" wide x 20" deep x 90" high. Several short runs of large diameter conduit run from the top of the MCC to a cable tray 2' above. Results - There is some anchorage for this cabinet. Calculations show that while the cabinet might rock, it will not rock far enough to tip over when subjected to a SSE level earthquake. The magnitude'of motion also is not anticipated to be very great. The evaluation also does no: take credit for any of the existing anchorage, or the bracing effects existing conduit might. Conclusion - MTMC-12 lack of proper anchorage is scheduled to be corrected by a plant mod after restart. The calculation shows there are no short-operability concerns. ~ (b) ER1 - Events Recorder Cabinet 1 3
- Description - This cabinet is located in the Control Room at Elevation 145' of the Control Complex, it is 198"long x 25.5' deep x 105" high. No structures, cables, etc., exist that provide any type of lateral restraint above the base of the
. cabinet. Results - To evaluate the potential for this cabinet to tip over, it was assumed to behave as a rigid block. The results of the evaluation indicate that while the cabinet would be expected to rock, it will not rock far enough to tip over when ' ~ tubjected to a SSE level earthquake as defined for the Crystal River site. ~ Conclusion - ER1 lack 'of anchorage is scheduled to be corrected by a plant mod after restart. The calculation shows there are no short-term operability concerns. 4 5 ~ -..
ANALYSIS /CALCULATDN DOC ID # N AU # REV F . SHEET 2_ OF6 Conclusion ER1' lack of arichorage~is scheduled to be corrected by a plant - " rnod after restart..The calculation shows there are no short term operability - - Concerns; 3.0 Summary and Conclusions 4 To address NRC concerns regarding GIP caveat compliance, a walkdown of a 10% sample of the SSEL equipment including items from each of the twenty equipment 4 classes was performed using the complete GIP SEWS.- The walkdown focused on the excluded GIP caveats and results of the sample walkdown were compared to the_ PSP walkdown SEWS. No additional outliers were identified and all concems associated with excluded caveats had been addressed by the PSP walkdowns, it was concluded that the evaluation of the equipment in the sample showed complete GIP caveat - compliance without exception. Table 1 summarizes these results.- To address NRC_ questions regarding anchorage and the use of engineering judgment, .a set of bounding anchorage calculations were performed for those classes of equipment for which anchorage is likely to control seismic adequacy. All bounding _ case anchorage evaluations demonstrated compliance with the GIP allowables even with the conservative assumptions used. Table 2 summarizes the results of those assessments. For the four equipment items for which the NRC had specific questions, the - anchorage ~s of MTMC-18 and V81T-1E are demonstrated as acceptable by calculations MTMC 21 anchorage is demonstrated to be robust by detailed drawing review, and AHCP 4 anchorage is to be modified since the fix is straightforward and addresses a poor design. j Calculations for two electrical cabinets, MTMC 12 and ER1, demonstrated that there are no short term operability concerns. The anchorage for these cabinets are scheduled to be modified post-startup. Very truly y/ / 7 ours I? f Waltdr Djordjevic - ! Se'nior Consultant \\ x M 1 6 i -m
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~ TABLE 11 a CA'/ EAT COMPLIANCE GIP ASSESSMENT Equip. . Number Tag Tag Number Description Building. Elev. GIP Walkdown Comments Class 1 MTMC-09 480V ?RESSURi2ER HEATER MCC 38 INTER 110 Mota control center. No issuca. SEWS reviewed and in agreement. 1 MTMC 12 - 480V TURBINE MCC 3A TURBINE 119 Urenchored MCC. Adjacent block wallis seismically evaluated. Overhead cable trays restrained to wall and, thus, do not pose interaction hazard. CRPSP SEWS reviewed and in agreement. 1 M1MC 18 480V REACTOR MCC 3A2 AUXILIARY 095 Mator control center witn welced anchorage. No issues. Meets all GIP caveats.CRPSP SEWS reviewed and in agreement. 1 MTMC 21 480V ES MCC 3A3 AUXILIARY 119 ODviously well engineered anchorage for 8-unit MCC. Meets all GIP caveats. CRPSP SEWS reviewed and in agreement, Ouring this walkdown, it was noted that conduit pipe sections and a + stepladder are stored on each end of the MCC lineup and are an interaction hazard. 2 DPXS 1 MAN XTER SWITCH FOR POWER TO AUXILIARY 095 Robust, wall-mounted MUP 38 AND MVP 58 configurabon. Tug tested by Djordievic, OK. CRPSP SEWS reviewed and in agreement.- 2 MTSW 3A 480V TIJRBINE AUX 1UARY BUS A TURDINE 095 Switchgear All GIP caveats addressed except breaker sidesway restraint caveat, No other issues. CRPSP SEWS feviewed and in agreement. 2 MTSW 3F 480V ES BUS 3A CONTROL 124 Meets att switchgear caveats. Checked side restraint caveat on ABB K-Line, Type K 600S 480V breaker, Secondary connecto(s cannot slide off stabs because of divider" ways *t)etween stabs, Side restraint not needed. Trolley hoist mounted on rails on roof of switchgear and free to roll (unbraked) so that it may pose as an impact hazard to relays. SEWS declared the switchgear an irnpact hazard for this potential interl., bon issue. 2 VBXS-30 EFIC vliAL BUS TRANSFER SWITCH D CONrROL 108 Rooust, wall-mountec configuration.- Tug tested by - Djordjevic. OK, CRPSP SEWS reviewed and in agreement. 3.- MTSW 2C 4160V ES 3A (NORTM) CONTROL 108 All caveats met, Door nut on EFP. 1 cubicle hanging loose: however. Me cubicle circuit is red tagged-oul ~ CRPSP SEWS reviewed and in - agreement. a y + -~ -.=
ANALYSiSiOALCULATON DOC ID # __ f9N)M ATT # REV O SMEET 7 OF ff___ E quip. Tag Tag Number Description Bu iding Elev. GlP Walkoown Comments Class Number 3 MuxS 1 4160V 150LATION SWITCH AUAILIARY 035 Robust, w all-mounted con 6guration. Tug tested by Dlordjevie OK. CRPSP SEWS reviewed and in agreement. 4 ACDP-51 T CONTROL COMPLEA DISTRIBUTION CONTROL 124 Small dry transformer mounted to PANEL A TRANSFORMER foor. Anchored by two bolts on front. Anchorage evaluation demonstrates adequacy Meets G!P caveats including t.ansformer positive mounting. CRPSP SEWS reviewed and in agreement. 4 ACDP ST ES DISTR:BUTiON PANEL 3AB CONTROL 124 Meets au caveats. Ancnorage TRANSFORMER contains *).1/2" and 1 5/B" concrete expansion anchors (CEA). Check for weak way bending. Calculation performed showed 9 ksi Stress due to weak way benuing. CRPSP SEWS reviewed and in agreement 4 MTSW 3J. 4163480V PLANT AUxlLIARY BUS TURB!NE 095 Large step-down transformer. T TRANSFORMER Transformer not positively secured to intemal frame. Declared outher. CRPSP SEWS reviewed and in agreement. 4 VDTR 2E 4SO/120v REDUNDANT POWER CONTROL 108 Dry Transformer mounted to botn SUPPLY TRANSFORMER 3E floor and rear watt. Very robust configuration. Meets GIP caveats including transformer positive mounting CRPSP SEWS reviewed and in acreement. 4 VDTR 3E REDUNDANT POWEH SUPPLY CONTROL 108 Rooust, wall-mounted SOLATRON 3E configuration. Tug tested by Djordjevic. OK. CRPSP SEWS reviewed and in agreement. 5 OFP to DC ORIVEN FUEL OIL TRANSFER AuxlLIARY 119 Small honzontal pump. Meets all PUMP D GIP caveats. No issues. 5 FWP7 AVAILIARY FEEDWATER PUMP 7 TURBINE 095 Feedwater pump. No issues. Well anchored. Nozzle loads not adiudged signincant. CRPSP SEWS reviewed and in agreement. 5 SSP 4D LP MEATER SAMPLE EXTRACTION TURBINE 095 Small pump. No issues. CRPSP PUMP SEWS reviewed and in agreement. o RWP-20 NUCLEAR SERVICE SEA WATER AUXILIARY 095 Large vertical pump. Casing PUMP 3B exceeds 20' rule. Anchored by 16-1" cast in place anchors in 52" bolt circle. Meets all GIP caveats, No issues. CRPSP SEWS reviewed and in agreement. 6 RWPJB DECAY HEAT SERV $E bEA WATER AUXILIARY 095 Large vertical pump. Casing PUMP 30 exceeds 20' rule. Anchored by 16: 1" cast-in-place anchors in 52' bolt circle Meets all GlP caveats. No issues. CRPSP SEWS reviewed and in agreement. 7 CAV 000 BORIC ACID PUMP TO MAKE UP TANA AUXILIARY 121 A,r-operated valve. Off set <45". OK. SEWS reviewed and in agreement. 7 CMV1CO AMMb44 (EFIC ROOMS) CONTROL CONTROL 125 Air operated valve. Oftset<45'. OK. VALVE SEWS reviewed and in agreement. 7 CMV 100-CHV 100 CONTROL CONTROL 124 Ruie-of tne-box on valve CHV-100. POS Meets all caveats. No issues. 7 CMV 113-CHV 113 CONTROL CONTROL 124 Rule-of tne-box on valve CHV 113. POS Meets all caveats. No issues. 7 EGV52 EDG A AIR START 3 WAY VALVE DIESEL 119 Small solcnoid valve. Meets all GIP i caveats. 8
d [ ANALYSIS / CALC.ULATION ooc to n 197 01Y/ ATT e A I REV 6 SHEET $_. OF.lf. l Equip. Tag Ia Number Description Spildmu 2.. vir N5thsown comments 1 I Class Number 7-GWV 196 GWP 1A CONTROL VALVE TURBINE - -095 Air operated vatve. Offset =29445*. OK. SEWS reviewed and in. agreement. 7 MSV411 MAIN STEAM UNE A 2 ISOLATION. .-_ INT ER 419 Main steam ssolation valve. No 1 VALVE issues. SEWS reviewed and in agreement. 7 Stu 015-MUV 16 CONTROL AUXIUARY 095 Rule of the box on MUV-16 POC-t J-7 MUV 243 - PREFILTER MUFL 2A OlSCHARGE AUXiUARY 121 Mounted on 2.5* kne. Mmer r ISOLATION VALVE actuated air operated valve with an offset of 33' which is less than 45*. Meets Figure B 8.1. CRPSP SEWS reviewed and in agreement. 7 SCV 096 IAP 1B & IAHE 1B COOUNG WATER TURBINE 108 Small control valve on 1* kne. No CONTROL VALVE extended operator. No issues. CRPSP SEWS reviewed and in - agreement. 8 ARV 48 VACUUM BREAKER REUEF FOR 1URDINE - 119 Mounted on 6* hne. SMB000 COME4A Limstorque operator with an I extended operator offset of 33*. } Meets Figure B 8.1. CRPSP SEWS reviewed and in agreement. o EFV 01 HOTWELL ISOLATION TO TURBINE INTER 095 Mounted on 6* kne. SMB000 DRIVEN EFP 2 Umstorque operator with an extended operator offset of 36*. Meets Figure B 8.1. CRPSP SEWS reviewed and in agreement. 8 FVW 15 FEEDWATER PUMP B SUCTION TURBINE 121 Mounted on 18' kne. SMB 1 ISOLATION VALVE Umitorque operator with an extended operator offset of 75*. a Meets Figure B 8.1. CRPSP SEWS reviewed and in agreement. 8 FkW-31 OTSG A LOW LOAO BLOCK VALVE INTER 136 Mounted on 10" hne. SMS 1 Umstorque operator with an extended operator offset of 36*. Meets Figure B 8,1. CRPSP SEWS reviewed and in aoreement. 8 MUV 073 BWST TO MVP 1A & MUP 1B AUX 1UARY 095 Valve body and yoke are CF8M ISOLATION VALVE stainless steel. Mounted on 6"line. SMB00 Limitorque operator with an extended operator offset of 38*. i Meets Figure B 8.1. CRPSP SEWS reviewed and in agreement. 8 MOV 194 MUFL 2AIMUFL 28 BYPASS VALVE AUX 1UARY 123 Mounted on 2.5* hne. SMC 04 Umstorque operator witn an extended operator offset of 30*. Meets Figure B 8.1. CRPSP SEWS reviewed and in aq eement. 8.1 - AH 033-AHO 1, AHO 10. AHO 2. & AMD-3 CONTROL 164 Contained with HVAC panel 9AB.
- ASV CONTROL.
No issues, SEWS reviewed and in agreement. 81 AH-306-SV AHO.60 CONTROL. OIESEL 119 Contained with HVAC panet 19, N2 issues. SEWS reviewed and in agreement. 8.1 AH-367 SV . AND 58 CONTROL OIESEL-119-Contained with HVAC panel 19, No i issues. SEWS reviewed and in . 1 agreement. - 8.1.. CHV 101 . NORMAL COOUNG FROM AHM. 44 CONTROL 124 Solenoid valve mounted ad acent to i s ISCLATION VALVE AHHE44. No issues. CRPSP SEWS reviewed and in agree:nent. . 8.1 CHV 113 CMV 113 CONTROL CONTROL. 124 Rule of the-cox on valve CHV 113. SV Meets all caveats. No issues. J i 9 <.,n.m n , - + - ,-,.-e-e e ,,.n v,,., ,w .w w
ANALYSGCALCULAT!ON DOC ID # 19MW ' ATT # 7 REV O SHEET // OF /.f_ E quip. Tag-Tag Numtier Description Building Elev. GIP Walkdown Comments Class Number ~ ~ t 6.1 .EFV45 - l EFP 2 TO OTSG B CONTROL VALVE INTER - 095-Mounted on d' kne. Target Rock scienoid operator with an extended operator offset of 40". Meets offset hmits. CRPSP SEWS revowed - i ~ and in agreement. 6.1-EFV48 EFP 1 TO OTSG A CONTROL VALVE . INTER 119 EFV58 Mounted on d' kne. Target i Rock soienoid operator with an. extended ope *ator offset of 30*. Meets offset hmits. CRPSP SEWS reviewed and in agreement. 8.1 - IAV 189 IAP 1B LOADER / UNLOADER VALVE-TURBINE 095 Soienoid velve mounted en air compressor 1 AP18. No issues. CRPSP SEWS reviewed and ;n agreement. ~ 8,1 - MSV. MSV-413 & MSV 414 CONTROL INTER 119 Rule of tne-box cn MSlV. No 413/414-issues. SEWS reviewed and in - SV5 agreement. 6.1 MU-015 SV MUV 16 AIR FAIL LOCK aux!LIARY 095 Mounted on wall adjacent to MUV.
- 16. No issues. Meets GIP cavents.
-9 AMF 17A CONTROL COMPLEX NORMAL CONTROL _164-Mounted on spnng isolators.. SUPPLY FAN A Declared outliers. SEWS revewed and in agreement. 9 AHF 22A DIESEL GENERATOR ROOM A DIESEL 137 Well supported fan. Meets all GIP - SUPPLY caveats. No isolators. CRPSP. SEWS reviewed and in agreement. 10-AHO-61 - AMF 22A DISCHARGE 0:ESEL 124 Damper r90unted on duct. No issues. CRPSP SEWS reviewed and in agreement. 10 AND 81 AHF 8A DISCHARGE AuxlLIARY 123 Rooust, duct. mounted con."guration. Tug tested ty Diordlevic. Meets GIP caveats. OK. CRPSP SEWS reviewed and in agreement. 10 AMD-84 AHF 68 OISCHARGE aux!LIARY 124 Rouust. duct mounted configuration. Tug tested oy Djord3avic. Meets GIP caveats. OK. CRPSP SEWS reviewer! and in agreement. 10 ANNE-05A COOLING UNIT A FOR CONTROL CONTROL 170 Coohng coil contained within duct COMPLEX housing. Supported on floor. Nn potcntial for differential movement between coohng water piping and housing. Meets GIP caveats. CRPSP SEWS reviewed and in - agreement. - 10 AHnE 44 COOLING UNIT D FOR EFlC ROOMS CONTROL 124 Cochng cost Rule of.tne box with AHF-548. N3 potential for differential movement. SEWS reviewed and in agreement. 11 CHME 1 A CONTROL COMPLEX CHILLER A CONTROL 164 Mounted on spnng isolators with, lateral and vertical stops. OK. Meets all other caveats. SEWS reviewed and in agreement 12 AMP 010 CONTROL COMPLEX HVAC AIR CONTROL 164 Mounted on neoprene pacs. 'COMPRESSORD Evaluated and shown OK.- ~; { Concrete pad 10" high. Anchors 16-j 17'long. SEWS reviewed and in j agreement. j 12 LAP-1B INSTRUMENT AIR COMPRESSOR S TURBINE - 095 Air compressor. No isolators. No 1 issues. CRPSP SEWS reviewed 2nd in agreement. -w. 10 r o- .,2--c,, 4 ~.,, --w-. - ~,
ANALYS!S/ CALCULATION DOC ID # f91-C E ATT0 [ O SHEET./l _, OF //_ REV Equip. lag Tag Number Desenption building
- Liev, GIP Walkdown Comments Class Number 12
' SAP 1A STATION AIR COMPRESSOR 1 A TURBINE 095 Air compressor. No isciators. No issues. CRPSP SEWS reviewed and in agreer:,ent. 12 WDP1A WASTE GAS COMPRESSOR A AUXtLIARY 095 Skd mounted witn 4 E castun-place anchors. Meets all GlP caveat.A. CRPSP SEWS reviewed and in agreement. 14 ACDP 51 CONTROL COMPLEX OtsTRIBUTION CONTROL 145 Frame mounted distncution parel. PANEL A Close to adjacent rack; however, does not contain relays. so OK 14 DPDP 1B 250/125V MAIN PANEL 3B CONTROL 10S Lon0 switchocard. 128"Wx90"Tx20* deep. Meets all GIP caveats. CRPSP SEWS reviewed and in moreement. 14 DPDP 5A 250/125V DC ES PANEL A CONTROL 124 No issues noentified. CRPSP SEWS reviewed and in agreement. 14 DPDP 5B 250/125V DC ES PANEL B CONTROL 124 No issues 6 dent:hed. CRPSP SEWS reviewed and in acreement 14 DPGP-6B 2$0/125V DC ES OtESEL GENERATOR DIESEL 119 Panel welded to base channels. PANELB Base channels anchored to floor by 6 3/4" CEAs. Meets all GIP caveats. CRPSP SEWS reviewed and in agreement. 14 DPDS 1C BATTERY 3C DISCONNECT SMTCH TURBINE 095 Switchboard 90" tall x36%x36'D. Anchored by 4 3/4* CEAs. Meets all GIP caveats. Block wall enclosure in Turbine building not seismically designed. CRPSP SEWS reviewed and in agreement. 15 DPBA.1Al 250/125V BATTERY A CONTROL 108 Side rails are not snug against I battery cells. Weided connections for the itself are marginal. Declared outlier by CRPSP SEWS. to DPdC 1G BATTERY CHARGER G TURblNE 095 Battery cnarger. New installation. Block wall enclosure in Turbine Building is not seismically evaluated No issues. Meets all GIP caveats. 16 VBIT 1E DUAL INPUT INVERTER 3E CONTROL 108 All caveats met. Transformer positively mounted. Four anchors found one of which is a friction chp. CRPSP SEWS reviewed and in agreement. 18 CA 11 LT BORIC ACID STORAGE TANK A AUXILIARY 119 Robust, wall-mounted configuration. Tug tested by Djordjevic. OK CRPSP SEWS reviewed and in agreement. 18 CH 378 PI CMV-68 CONTROL OF CHME 1 A CONTROL 164 Mounted on lignt metal strut trame. No issues. Tug tested. SEWS reviewed and in aoreement. 18 DC-54 A T DC SURGE 1 ANK DCT-1B LEVEL AUX 1LIARY 095 Robust, wall-mounteo conhguration. Tug tested by O ordjevic. OK CRPSP SEWS l reviewed and in agreement. 10 DF 4 Lb DIESEL GENERATOR FUEL Ott DAY DIESEL 119 Mourited on diesel fuel oil tank. No TANK B LEVEL SWITCH issues. SEWS reviewed and in acreement. 10 DM 07 LT BORATED WATER STORAGE TANK BWSI 119 Robust. wall-mounted LEVEL configuration, Tug tested by Djordjevic. OK. CRPSP SEWS reviewed and in noreement 1I
ANALYSIS / CALCULATION-DOC 10 # JY/*OfV/ ATT # ' REV 6 SHEET /I OF /L Equip. -Tag Tag Number Descriptio Bytidmg L vm vramcown Comments - -l Class Number 18-EF 95.LT EMERGENCY FEEDWATER TANK - EFW TANN 119 Large hat bottom tank with 36 i LEVEL anchors. One line may have hmited Dexibility (1* hne contairnng valve EFV.115) deper>fng an calculated uplift Check tank capacity calculation. 18 IA 12-PS - INST RUMENT olR COMPRESSOR TURBINE 095 Wall mounted. Small pressure LOAD / UNLOAD PRESS SWITCH switch. Tug tested. OK. 18 MS-113 PT MAIN STEAM LINE B-1 PRESSURE INTER 119 Wall-mounted. T ug tested. Bolted. TRANSMITTER Nolasues CRPSP SEWS ~ teviewed and in agreement. 19 RW 43-TE SEA WATER OUTLET NUCLEAR AVAILIAR Y 095 Meets al8 GlP caveats. CRPSP SERVICE COOLERS SEWS reviewed and in agreement. 20 - ATCP 1 ANTICIPATED TRANSIENT WITHOUT CONTROL 124 Cabinet 24x24x90* tail No tssues. SCRAM LOGIC CABINET SEWS reviewed and in agreement.- 20 CCST CENTRAL CONTROL BOARD CONTROL. 145 CC8T Frame structure very TERMINATION CABINET robustly anchored. Adjacent and in contact with cabinet TGAR; however, since CCDT contains no relays it is adjudged OK, CRPSP SEWS reviewed and in agreement. 20 EGCP 2A EMERGENCY DIESEL GEN A DIESEL 119-Large noor mounted cabinet. Meets ELECTRICAL EQUIPMENT CABINET all GIP caveats. No issues. 20 ER) EVENTS RECORDER CABINET 1 CONTROL 145-No apparent ancnorage PC boards inside cabmet are tight and secure and adjudged OK. CRPSP SEWS reviewed and in agreement. SEWS declared this cabinet an outlier due to it being unanchored 20 ESCP 4D ENGINEERED SAF EGUARDS CONTROL 145 Meets all caveats for control ACTUATION RELAY CAB: NET ( cabinets. One end bears against sheetrock wal!; however,it is the tong (staff) direction for the cabinet lineup and is adjudged acceptable, CRPSP SEWS reviewed and in agreement including same judgment regarding interaction potential with end wall. SEWS mentioned potential interaction with small cabinet, but this had accarently already been removed 20 HTCP4 EDG 8 EMERGENCY LOAD SHEDDING AUX 1LIARY l Walt-mounted panet. Tug tested. 119 . HEAT TRACING OK. No issues. 20 HVAC 16A MVAC CONTROL CABINET 16A AUXILLARY 095 Robust, wall-mountec configuration. Tug tested by Djord evic. OK CRPSP SEWS i 'eviewed and in agreement 20 - NNI.5 AUXILIARY CONTROL SYSTEM CONTROL 145 No issues. Could not open cabmet CAB! NET 5 for intamalinspection. CRPSP SEWS reviewed and in agreemerit. SEWS confirmed that cabinets are 4 not bolted together and were - declared outfiers. ~ 20 RCTR 2 RCP 10 TRANSFORMER CABINET - INTER 119 Caomet cr ntainmg posmvely mounted (rack mounted) < 750 KVA. No issues. CRPSP SEWS reviewed and in aoreement. 1 H .a
_ _ _ _ -._. ~ _ _ ANALYSIS / CALCULATION DOC ID # Of*CN ATT # I -C TABLE 2 -" REV O SHEET _7 OF # RESULTS OF ANCHORAGE ASSESSMENTS P Equipment 10 Equipment Description and OsVt* of Anchorage EvaMtion Class-lit &W4F. 2 MTSW.3F is the 460V ES Bus 3A, low vrMage s.vitchgear locate 0 at Elevabon 124' of the Control Complex. The switchgear are contairled in thre? unih in 24' wide x 68* deep x 90* high steel endosures (wnici. are bdled together), cnd the transformer is 7 containec in a 96* wide x 58" deep x 90* seei encitsure, bolted to the switchgear cabinets. The switchgear cabinets ano 4 iC. (located at the opposite end of the transformer from the switchgear) ce welded to embedded steel with plug welds. Tt'e end switchgear unit was replaced at some time, and is actually fillet welded, front and bacA. to the embedded steel. These welds were conservahvely talen as the origina' pbg welds for tms evaluabon.- The transformer skid is anchored with two 3/4' bolts '.en one side. and two 3'8",3* Iong fil:et welds on the other. For this evaluation, the two 3/8" fillut welcs +.are conservatively assumed as 3/4" expansion anchorsc The results of the evaluahon indica's the anchorage is adequate for an SSE level earthquake, with a margin of abot.t 2.2. controlled by shear and tension on the plug welds. MTxS 1 2 MTSx.1 is tne ES MCC 3na input Power Transfer Switch, located at Elevatior.124' of the Control Complex. It has a 4 T* wide x 15' deep x 70* high steel endos9re, which is bolted with six (three each side) 1r2" diameter bolts to a 4* high channel base. And.orage of the channel base to the concrete floor could not be determined Cased on observation of most expansion anchored equipment, cabinets, and panels in the plant, there are most likely four 1/2" diameter expansion anchors as a minimum, however, to be conservative, the anchorage was assumed to be equivalent to four 3/8" diameter expansion anchors. The results of the evaluation indicate the anchorage is adequate for an SSE level earthquake, with a margin of 2.27 controlled by combined tension and shear on the anchor bolts. MTSW 2C 3 MTSW 2C as the 4160V ES 3A (North) medium voltage switchgear, located at Elevation 108' of the Control Complex. There are seven units, etch in a 26* wide x $8" deep x 90 steel endosure. All sections are bolted together. On top of the second unit, a small Pansformer in a 2'xh2' steel endosure is mounted aear the front, The switchgear is anchored by 3/4" plug welds to embedded steel. For the cn;;horage evaluation, only those plug weMs venfied by the SRT were 'nduded. This excluded all i assumed plug welds along the back of the switchgear escept for two, located in the second panet. The results of the evaluation indicate the anchorage is adequate for an SSE level earthouaire. with a high maroin controlled by shear ca the pluo weids. ACDP.68 f 4 ' ACDP-68 T is the ES Distnbution Panel 3AB transformer, located at Elevation 124%0 of the Control Complex. It is ;: mall transformer in a 26* wide x 22" deep x 25.5" high sWel endosure, supported by the side plates, which extend below the base 3.75*, and are bent outward at a 90* angle. It is anchored to the concrete floor by three 1/2" deameter expansion anchors and one 5/8" diameter expansion anchor. The anchorage evaluation was performed considenng or e anchor bolt inactive, on the basis of the wa;kdown team observing this situation for another similar transformer. The results indicate the anchorage to be adequate for an SSE level earthquake, with a minimum margin of about 3.9 controlled by waak way bending of the bent plates. % B TR-1 A 4 VBTR 1A is a constant voitage transformer locatnd at Elevation 124%0' of tne Control e Complex, it is a small transformer in a 22.5" wide x 25.5* deep x 37.5* high steel endosure, supported on two 2*x2*x3/16" angles. The angles are anchored to the concrete floor with two 1/2" diameter expansion anchors near the front of t!)e transformer, one in eacn angle. Results of the artchortge evaluation indicate the anchorage is adequate for the SSE level eartnquake, with a margin of about 7.4 controlled by shear on the anchor bolts. Bending of the verticallegs of the angles was checked and found to have high margin capadty without consideration of two existing gusset fstiffeners) per angle. AC7P 51 14 ACDP-51 is the CC Distnbution Panel A, located in tne Control Room (inside the main control board structure) at elevation 145' of the Control Compiex. It is a 32* wide x 9' i deep x 65* high distnbution panel, supported by a C4x5 4 wtMed channel frame on each side. The base of the channel frames are each welded to a 3*x3*x3/8" angle,18* + long, which are anchored to the concrete floor with two 1/2" diameter expansion anchors per angle. ACDP.52, identical to and back to back with ACDP 51, is also supported between the channel frames. The two panels are each attached to the channel frames with four bolts,-er stie. The resu.ts of the evaluation indicate that the frames and anchorage are adequate for an SSE level eanhquake, with a minirwm margin. conservatively determined. of 1.4. controlled by pullout of the anchor bolts. 13
ANALYSIS / CALCULATION 000 ID # ff 2'CEE ATT # REV 6 SHEET,]f__ OF /f Equipmelit ID Equ$ ment Description and Results of Anchorage Evaluation Class DPDP 6A 14 DPDP 6A is the 250V/12SV DC ES DG Panet A, located at EM!vation 119' of tne Diesel Building it is a distnbutiori panel with a 32' wide x 20* deep x 76' high steel enclosure. The enclosure is supported on a 6' high channel frame, to which it is seam welded with tuo 2'long welds on each end. The channel frame is anchored to the concrete with six $4* d:ameter expansion anchors The resuta of the evaluation indicate the anchorage is adequate for an SSE level earthquake, with a Ngh marg!n controlled by shear on the seam welds. ESCC 1 20 E5CC 1 is the ES bystem Channel Test Cabinet 1, located at Elevation 145 cf the Control Complex in the Control Roorn. It is 25.5" deep 200* iong, and 105' high There are nine b?ys, each 23' wide. Tbo cabinet is anchored to embedded steel by four 1/2' diametur bolts per b y, one in each cr;teer, bireated into the embedded sM 31. The results tsf t e evaluation Indicata the anchorage is adequate for an SSE level earthquake, witt, a minnum margin of about 5 3 controlled by tension on the anchot colts. 14
(/ ) Florida DESIGN ANALYSIS / CALCULATION Power \\. / "" * """ Crystal River Unit 3 Of sat FRM Page I of f6 00CVMENT OENTIFIC Af r0N NO RfVISION 4 S97 0541 0 e S Information copy of: l SSEL Data Sort. Sorted by Class, Building and Elevation 1 1 I 1 i , 95 RETJ L fe of Meet RitF. Nucreer Engmneg
SSEL Sorttd by Cttss. CALCULATION S97 0541 Elsv: tion, REV.O, and Building ATTACHMENT *S* Tag Nu.nber l Tag Number description ~' ~ l Building lElev. = 1 { h1't h1C 21 { 4soV ES MCC 3A3 i AUXILIARY I il9 I hlThtC-04 l 440V ES MCC 3A2 j AUXILIARY l 119 I hfTh1C 05 l 440V ES MCC 3BI J AUYILIARY 119 i j h1Th1C 07 i 480V ES MCC 3AB j AUXILIARY 1 119 I l hlThtC-03 l 440V PRESSURIZER HEATER MCC 3A j INTER 119 I hlThtC 09 j 480V PRESSuntztR tiEATER MCC 3B l INTER 119 I htThtC 12 j 480V TURBINE MCC 3 A l TURBINE l 119 1 ) h!ThlC 18 480V RLACTOR MCC-3A2 i AUX 1LIARY l 095 I I h1Th!C 22 l dsoV ES MCC 383 l AUXILIARY l 005 1 hlThtC 03 l 480V ES MCC 3Al l AUXILIARY i 095 1 hlTh1C 06 i 480V ES MCC 383 i AUXILIARY 095 2 i blTSW 3F f 480V ES BUS 3A j CONTROL l 124 2 l h!TSW 3G i 4soV ES BUS JB i CONTROL l 124 2 hlTXS 1 l ES MCC 3AB INPUT POWER TRANSFER SWTTCH l CONTROL j 124 2 i VilXS 1 A } VITAL BUS TRANSTER 5WITCil A l CONTROL i 108 l \\ BXS 1B l VITAL BUS TRANSI ER SWITCH B } CONTROL 108 2 2 ll VBXSlC l VITAL BUS TRANSFER SWITCH C l CONTROL 108 2 VUXS-ID j VtrAL BUS TRANSFER SWITCH D l CONTROL l 108 2 VBXSlE I MANU AL TRANSTER SWITCH CONTROL j 108 2 VDXS 3A j EFIC VITAL BUS TRANSFER SWITCil A CONTROL l 108 2 VBXS 3B ) Er!C VITAL BUS TRANSTER SWITCll B CONTROL 108 2 I VBXS-3C l Eric VrTAL BUS TRANSI-ER SWITCH C l CONTROL 108 2 j VBXS 3D 1 ErtC VITAL BUS TRANSFER SWITC1f D l CONTROL 108 2 l DPXS-1 l M AN XFER SWITCit FOR POWER TO MOP.3B AND MUP-5B i AUXILIARY 095 2 I hlTSW 3A l 480V TURolNE AUXILIARY BUS A TURBINE 095 2 ) htTSW-3C l 480V REACTOR AUXILIARY BUS A TURBINE 095 2 l hlTSW 3D l 4A0V REAC10R AUXILl4RY BUS B j TURBINE 095 2 h!TSW 3) 480V PLANT AUXILIARY BUS l TURBINE l 095 3 l h!TSW-2C 41mv ES 3A (NORTin i CONTROL l 108 3 i hlTSW 2D j 41mv ES 3 A (SouTili l CONTROL 108 3 } htTSW-2E i dimV ES 38 (NORTl!) l CONTROL 108 htTSW 2F } dimv ES 3B (south) l CONTROL 108 3 3 hlVXS 1 i 4160V ISOLATION 5%ITCil j AUXILIARY 095 4 { ACDP-68 T j ES DISTRIBUTION PANEL 3AB TRANSFORMER l CONTROL l 124 4 l ACDP 51 T l CONTROL COMPLEX DISTRIBUTION PANEL A TRANSTORMER I -CONTROL l 124 4 l ACDP-52 T j CONTROL COMPLEX DISTRIBtrflON PANEL B TRANSFORMER j CONTROL 124 4 hlTSW-3F-T 4tt&480V ES BUS 3A TRANSTORMER CONTROL 124 5 4 hlTSW 3G T j 4 tav4sov ES BUS 3B TRANSTORMER l CONTPOL l 124 4 VUTR-I A l CONSTANT VOLTAGE TRANSFORMER A { CONTROL l 124 4 VBTR 1B CONSTANT VOLTAGE TRANSTORMER B CONTROL i 124 4 1 VIITR 4A i REGULATING TRANSFORMER A j CONTROL l 124 4 i VBTR 4B i REGULATM TRANSFORMER B l CONTROL l 124 4 i VBTR-4C REGULATING TRANSIORMER C i CONTROL l 124 4 } VBTR-4D i REGULATING TRANSTORMER D i CONTROL l 124 4 i VBTR 2E l 4%I30V REDUNDANT POWER SUPPLY TRANSFORMER JE l CONTROL l 108 4 l VBTR-3E } REDUNDANT M)WER SUPPLY SOLATRON 3E l CONTROL } 108 4 i hlTSW 31-T j 4M40V PLANT AUXILIARY BUS TRANSFORMER l TURBINE l 095 i 5
- i CilP-I A l
CitiLLED WATER PUM8 A CONTROL i 1 68' l CLASSORT.XLS Page 2 OF 18 12/'11/1997
SSEL Sortsd by Class. CALCULATION S97 0541,
- Elzvmon, REV.O, tnd Buildin0 ATTACHMENT *S" l
Tag Number l Tag Number description ' l Building l Elet. 2 5 1 CIIP lb i CitiLLED WATER PUh1P s l CONTROL IM 5 CAP-1 A t BORIC ACID PUhtP A l AUXILIARY I 119 5 CAP-ill DORIC ACID PUMP B AUX 1LIARY 119 5 Si P I A. SPLNT FUt! COOLANT PUMP A AC 'lLIARY !!9 3 5 SFPill l SPENT TUEL COOLANT PUMP s i AUXILIARY j 119 5 DFPlC e DC MOTOR DRIVEN FUrlOlt TRANSTER PUMP C AUX 1LIARY j 119 5 DFP ID i DC DRIVEN FULL Olt TRANSFER PUMP D j AUXILIARY 119 5 l DFPlA i AS MOTOR DRIVLN FUEL O!L TRANSFER PUMP A DIESEL t 119 5 i DFP lb AC MOTOR DRIVEN TUEL OIL 1stANSIER Pt'MP o l DIESEL l !!9 5 l MUP1A M AKE UP AND PURIFICATION PUMP 3 4 AUXILIARY l 095 5 l MUP-ID M AKE UP AND PURlr! CATION PUMP 38 l AUXILIARY 095 5 MUP-2A MUP IA MAIN 011. PUMP AUXILIARY l 095 5 MUP4A l MUP 1 A GEAR Olt PUMP l AUXILIARY l 095 5 MUP-lC l MAKE.UP AND PURIFICATION PUMP 3C l AUXtLIARY l 095 5 l MUP-2D l MUP ta MAtN OIL PUMP AUXILIARY 095 5 i MUP 2C l MUP lC MAIN OIL PUMP AUXILIARY 095 5 { MUP4D l MUP 1B GEAR OIL PUMP I AUXILIARY 095 5 { MUPAC i MUP IC GEAR Olt PUMP I AUXILIARY 095 5 i SWP 2A l NUCLEAR SERVICE BOOSTER PUMP A AUXILIARY j 095 5 l SWP-2D l NUCLEAR SERVICE BOOSTER PUMP B i AUXILIARY j 095 5 DCP<A j DECAY llEAT CLOSED CYCLE COOLING PUMP A l AUXILIARY l 095 5 DCP-lu DECAY llEAT CLOSED CYCLE COOLING PUMP D l AUXILIARY j 095 5 SWP1A f EMERGENCY NUCEEAR SERVICE CCC PUMP 3A AUXILIARY l 095 5 i SWPlu EMtRGENCY NUCLEAR SERVICE CCC PUMP 30 AUXILIARY l 095 i 5 j sw P.lC l NORMAL NUCLLAR SERVICE CLOSED C1CLE COOLING PUMP } AUXILIARY l 095 5 l EFP 2 I TURBINE DRIVEN EME,1GENCY FEEDWATER PUMP l INTER l 095 5 l EFP-1 { MOTOR DRIVEN EMERGENCY TEEDWATEk PUMP i INTER j 095 5 i SCP 3 _ i SECONDARY SERCIVES CLOSED CYCLE COOLING DOOSTER PUMP 1 TURBINE l 095 _ 5 i SSP 4A i CONDENSER A llOTWTLL SAMPLE EXTRACTION PUMP l TURDINE l 095 5 i SS P-4 D l CONDENSER B llOTWELL SAMPLE LXTRAGION PUMP j TUREINE { 095 5 i SSP-4C f CONDENSER AD HOTWELL CROSSOVER SAMPLE EXTRACTION PUMP l TURBINE j 095 5 } SSP-4D LP HEATLR SAMPLE EXTRACTION PUMP l TURBINE l 095 5 FWP-7 l AUX 1LIARY rEEDWATER PUMP 7 l TURBINE 095 5 GWP-1 A CONDENSATE INJECTION PUMP 3A TURBINE 095 i 5 I G W P-lu l CONDENSATE INJECTION PUMP 3D TURBINE 095 5 DSP 1e REACTOR DUILDING SPRAY PUMP A l AUXILIARY j 075 I 5 DSP lu REACTOR DUILDING SPRAY PUMP D AUXILIARY l 075 5 i DilP 1 A DECAY HEAT PUMP A 4 AUXILIARY j 075 5 j DitP-lu i DECAY HEAT PUMP D i AUXILIARY l 075 6 RWP-2A j NUCLEAR SERVICE SEA W ATER PUMP 3 A i AUXILIARY. j 095 6 RWP-3A 1 DECAY HEAT SERVICE SEA W ATER PUMP 3A I AUXILIARY 095 6 RWP1 NORMAL NUCLEAR SERVICES SEA WATER PUMP MOTOR CGOLER AUXILIARY 095 6 RWP-28 NUCLEAR SCRVICE SLA WATER PUMP 30 t AUXILIARY } 095 6-RWP-3B DECAY llEAT SERVICE SEA WATER PUMP 3D AUXILIARY j 095 6 CDP 1A j CONDLNSATE PUMP A TURBINE l 095 6 CDPlu i CONDENSATE PUMP D TURDINE l 095 7 CllV.068 i SERVICE W ATER TO CHHE I A CONTROL VALVE I CONTROL l 172 7 CllV-Oo9 i SERVICE WATER TO CHHE la CONTROL VALVE i CONTROL l 172 CLASSORT.XLS Page 3 OF 18 12/11/1997
~ - -. SSEL Sorted by Class, CALCULATION $97 0541 Elsvetion. REV,O. and Bwidin9 ATTACHMENT *S* l Tag Number l Tag Number description ~' ~ l Building _ lEles. 5 l CilP ID i ClitLLED WATER PUMP B l CONTROL i 164 5 CAP 1A j DORIC ACID PUMP A t AUX 1LIARY l 119 5 CAP 1B l DORIC ACID PUMP D l AUX 1LIARY l 119 5 SFP 1 A SPENT rUEL COOLANT PUMP A I AUXILIARY i 119 5 SFP !D SPENT FUEL COOLANT PUMP D i AUX 1LIARY l 119 5 DFP lc nC MOTOR DRivtN rOEL OlL TRAN5f ER PUMP C AUXILIARY j 119 ~ l DFPID Dc DRIVEN rUEL OIL TRAN5fER PUMP D I AUXILIARY j 119 5 l DFP l A A$ MOTOR DRIVEN rUEL Ott TRAN5fER PUMP A l DIESEL 119' 5 l DFI' ID j AC MOTOR DRIVEN i UEL OIL TRANSFER PUMP D j DIESEL !!9 MAKE UP AND PURiflCATION PUMP 3A l AUXILIARY 095 5 i AIUP-1 A g 5 l h!UP lu l M Art-UP AND PURiflCATION PUMP 3B AUXILIARY 095 5 l AIUP 2A l MUP-l A M AIN OIL PUMP AUXILIARY 095 5 hlUP4A l MUP 1 A GEAR OIL PUMP l AUXILIARY 095 5 blUP lC l MAKL UP AND PURllMCATION PUMP 3C i AUXILIARY l 095 5 blUP 2D i MUP lu MAIN OIL PUMP AUXILIARY j 095 5 MUP 2C l MUP lC MAIN Olt PUld i AUXILIARY 095 5 hlUP4B l MVP-lo GEAR OIL PUMP l AUXILIARY 095 5 htCP4C l MUP lC GEAR OIL PUMP l AUXILIARY 095 5 SWP-2A j NUCLEAR SERYlCE DoOstER PUMP A i AUXILIARY 095 5 SWP-2B l NUCLEAR SERVICE DOOSTER PUMP D l AUXILIARY 095 5 DCPIA } DECAY llEAT CLOSED CYCLE COOLING PUMP A l AUXILIARY 095 5 DCP1B l DECAY llEAT CLOSED CYCLE COOUNG PUMP 3 l AUXILIARY 095 5 SWPlA l EMERGENCY NUCLEAR SERVICE CCC PUMP 3A l AUXILIARY 095 5 SWP-ID l EMERGENCY NUCLEAR SERVICE CCC PUMP 3D i AUXILIARY 095 5 SWPIC l NORM AL NUCLEAR SERVICE CLOSED CYCL E COOLING PUMP l AUXILIARY 095 5 EFP-2 l TURDINE DRIVEN EMERGENCY rEEDWATlR TUMP i INTER 095 5 [ EFP1 MOTOR DRIVEN EMERGENCY rEEDWATER PUMP INTER 095 4 5 SCP 3 stcONDARY sERCIVLS CLOSED CYCL E COOLING DOOSTER PUMP i TURBINE 095 5 j SSP 4A l CONDENSER A ilOTWELL SAMPLE EXTIO.CTION PUMP l TURBINE l 095 5 l SSP-40 l CONDENSER D llOTWELL SAMPLE EXTRACTh)N PUMP l TURDINE 095 5 i SSP 4C l CONDEN5ER AD 110TWELL CROSSOVER SAMPLE EXTRACTION PUMP l TURBINE 095 ~ l SSP 4D l LP llEATER SAMPLE EXTRACTION PUMP l TURBINE 095 5 l FW P-7 i AUXILIARY f EEDWATER PUMP 7 TURDINE 095 5 ) GWP1A-l CONDENSATE INJECTION PUMP 1A 1 TURBINE 095 5 GWPID l CONDENSATE INJECTION PUMP 3D l TURBINE 095 5 DSP 1A REACTOR DUILDING SPRAY PUMP A . AUXILIARY l 075 5 DSPID REACTOR DUILDING SPRAY PUMP D l AUXILIARY l 075 5 1 DHP-1A DECAY lIEAT PUM? A l AUXILIARY l 075 5 { OllP ID i DECAY llEAT PUMP D [ AUXILIARY 075 l RWP-2A NUCLEAR SERVICE SEA WATER PUMP jA j AUXILIARY 095 6 6 l RWP-3A i DECAY llEAT SERWE SEA WATER PUMP 3A [ AUXILIARY 095 6 i R W P-l NORMAL NUCLEAR SERVICES SEA WATER PUMP MOTOR COOLER j AUXILIARY 095 j ^ RWP2D NUCLEAR SERVICE 5EA WATER PUMP 30 l AUXILIARY 095 I, RWP-3B' AUXILIARY { 095 6 i DECAY llEAT 5ERYlCE 5EA WATER PUMP 3D 6 j CDP 1A { CONDENSATE PUMP A l TURDINE 095 l CDPID } CONDENSATE PUMP B i TURBINE 095 6-7 CilV 068 SERVICE WATER TO CllllE IA CONTROL VALVE l CONTROL 172 ~ 7 i CIIV-069 i SERVICE WATER TO CllllE ID CONTROL V ALVE i CONTROL l 172 CLASSORT XLS Page 3 OF 18 12/11/1997
SSEL Sort:d by Class. CALCULATION $97 0541, E12vation, REV.O, cnd Building ATTACHMFNT *S" l Equip. Tag Numl>cr f Tag Numl>er descripilon " f Building l Elev. 21 ass - 7. CilV 068-POS j Clives CONTROL i CONTROL-164 7 CilV 069-POS j CHVM CONTROL i CONTROL j 1 68 7- '-CilV Il3 i AHHE-43 (rrlC ROOMS) CONT ROL VALVE CONTROL-l 130 7 h1UV 201 l LETDOWN ISOLATION VALVE TO DEMINERALIZER MUDM ID AUXILIARY l 128 7 CilV 100 1 AHHE-44 (ErlC ROOMS) CONTROL VALVE i CONTROL l 125 7 blUV 124 ISOLATION VALVE TO PURil'ICATION DEMINERALIZER ML*DM-l A j AUXILIARY .( 124 7 l h1U V 200 t LtlDOWN ISOLATION VALVE TO DEMINEkAllZER MUDM I A . AUXILIARY i-124 .7-h1UV 133 ISOLATION VALVE TO DEMINERALIZER MUDM 1B AUXILIARY l 124 7 CilV-100 POS i CHV 100 CONTROL CONTROL l 124 7 CllV ll3 POS l CHV It) CONTROL i CONTROL 124 7 h1UV 242 PRLflLTER MUFL 2A INLET ISOLATION VALVE l AUXILIARY 123 7 l~- hlUV 245 PREFILTER MUFL 2B E1LET ISOLATION VALVE j AUXILIARY 123 7 hlUV Il6 i DEMINERALIZER MUDM-I A ISOLATlON VALVE TO LETDOWN FILTER i AUXILIARY 122 7 hlUV 117 l DEMIN ARALIZER MUDSIB ISOLATION VALVE TO LETDOWN FILTER I AUXILIARY 122 7 CAV 060 j BORIC ACID PUMP TO MAKE UP TANK j AUXILIARY 121 7 l htUV.243 l PRErlLTER MUrl 2A DISCllARGE ISOLATION VALVE l AUXILIARY 121 7 h1UV 244 l PRLFILTER MUfL 28 DISCl!ARGE ISOLATION VALVE i AUXILIARY 121 - 7 blU V 090 l LETDOWN FILTER MUFL ID TO MUT 1 ISOLATION VALVE l AUXILIARY 119 7 i htUV 091 l L2TDOWN TILTED MUrt-I A TO MUT 1 ISOLATION VALVE l AUXILIARY 119 7 l MUV 096 4 LETDOWN rILTER MUI L 1 A INLET ISOLATION VALVE l AUXILIARY- !!9 7 I blUV497 l LETDOWN FILTEk MurL IB INLET ISOLATION VALVE AUXILIARY 119 7 hlUV 050 l LET DOWN BLOCK OROFICE ISOLATION VALVE AUXILIARY 119 -7 blUV 051 l LET DOWN FLOW CONTROL VALVE A!.XILIARY 119 7 i CAV-057 i DORIC ACID PUMP TO MAKE.UP TANK l r\\UXILIARY I19 7 l h1U V 103 l DORIC ACID PUMP TO MAKE UPTANK ISOLATION VALVE l AUXILIARY 119 7 j MUV 108 l BORIC ACID PUMP TO MUT l ILOW CONTROL VALVE l AUhlLIARY 119 7 j MUV 253 ) REACTOR COOLANT PUMP SEAL BLEEDOFF ISOLATION VALVE j AUXILIARY 119 7 l SWV-041 j ISOLATlON F ROM OUTLrTS OF AllHE-31 A AND AllHE42A l AUXILIARY 119 7 SWV 012 l SEAL RETURN COOLERS SUPPLY ISOLATION VALVE l AUXILIARY I19 7 blU 012 POC j MUV 108 CONTROL l AUXILIARY 119 7 l MU 003-POC { MUvSiCONTROL l AUXILIARY 119 7 EGV-52 j EDO A AIR START 3 WAY VALVE i DIESEL 119 7 EGV-53 i EDG A AIR START 3 WAY VALVE l ' DIESEL 119 7 EGV-54 l EDO B AIR START 3-WAY VALVE l DIESEL 119 7 EGV 55 l EDO B AIR STAkT FWAY VALVE j DIESEL i19 7 htSV-411 MAIN STEAM LINE A-2 ISOLATION VALVE i INTER l 119 7 MSV-412 i ' MAIN STEAM LINE A 1 ISOLATION VALVE INTER l 119 7 htSV-025 { ATMOSPUERIC DUMP VALVE A } INTER 119 -7 MSV 033 MAIN STEAM !.lNE A 2 SAFETY VALVE INTER !!9 7 MSV 037 - { M AIN STEAM LINE A 2 SAFETY VALVE INTER 119 7 MSVol2 l-M AIN STEAM ;.lNE A 2 sal'ETY VALVE j INTER 119 7-i MSVol6 -t MAIN STEAM uNE A 2 SAFETY VALVE INTER 119 7 MSV 034 I MAIN STEAM LINE A 1 SArETY VALVE INTER !!9 7 1 MSWO38 l MAIN STEAM LINE A I S AFETY VALVE INTER 119 7 MSVol0 l ' MAIN STEAM LINE A i SAFETY VALVE i INTER l 119 7 MSV 043 i MalN STEAM uNE A 1 SAFETY VALVE l INTER l 119 7 .} MSV 035 i MAIN STEAM uNE B-l SArETY VALVE l INTER l 119 7 i MS%039 1 MAIN STEAM LINE B-1 SAFETY YALVE l INTER l 119 CLASSORT XLS - Page 4 OF 18 12/11/1997 a.
-- ~... -,.. SSEL Sort 2d by Class. CALCULATION 397 0541, Elsvation. -REV,0, a J Build #ng ATTACHMENT 'S" r Tag Numlier Tag Numlier description ' ~ l Building lElew 7-1 . MSVW4 l htAIN STEAM LINE B t SATETY VALVE j. INTER l 119. 7 i M 5V 047 MAIN STEAM LINE B s SAFETY VALVE I INTER l 119 7 i MSV 414 MAIN STEAM UNE B-2150LATION VALVL INTER l 119 7 . MSV 026 ATMOSPHERIC DUMP VALVE D INTER l 119 7 MSV-036 M AIN STLAM UNE D-2 5ATETY VALYL INTER l 119 7 MSV 041 i MAIN STE AM UNE B-2 SAFETY VALVE I INTER 119 7 MSV-413 i M AIN STI AM UNE h-1 ISOLATION VALVE t INTER 119 i 7 j MSV 045 ' I M AIN STEAM UNE n-2 SArETY VALYL j INTER l 119 7 MSV@8 l M AIN STIAM LINE D-2 SAI ETY VALVE j INTER 119 7 SCV-095 i IAP ! A & 1AllE 1A COOLING WATER CONTROL VALVE l TURBINE 108 '7 l SCV-096 l 1AP ID & IAllE 1B COOLING WATI.R CONTROL VALVE l TURBINE 108 7 l SWV 152 { IC TO RD RAN COOLERS ISOLATION VALVE AUXILIARY 100 7 -l SWV.151 IC l' ROM RD FAN COOLERS ISOLATION VALVE AUXILIARY 100 ~ 7' MdV 016 Rcr SEAL INRCTION FLOW CONTROL VALVE l AUXILIARY 095 7 MUV-031 l ~ MAKE UP FLOW CONTROL VALVE j AUXILIARY 095 7 MUV 049 l LET DOWN Ft.OW ISOLA 3N VALVE l AUXILIARY 095 7 l SWV 03% l INLET ISOLATION FOR AlHIE 3]A AND AHHE 32A AUXILIARY 095 7 l SWV 037 INLET ISulATION FOR AltllE-31B AND AilllE 328 AUXILIARY 095 7 l SWV-039 INLET ISOLATlON IOR AlHIE-31C AND AllHE 32C l AUXILIARY 095 7 l SWV 043 l OLTTLET ISOLATION fOR AllHE 3tB AND AlHIE-32B AUXILIARY 095 7 l SWV 045 i ouTL ET isoLATlON [OR AllHE-3]C AND AllllE 32C AUXILIARY 095 7 l SWV-047 ISOLATION TO MUHE 1B AND WDilE l l AUXILIARY 095 7 SWV 048 LETtx)WN COOLER 3D INLET ISOLATION VALVE l AUXILIARY 095 7 I SWV@9 l LLTOOWN COOL.ER 30 DISCllARGE ISOLATION ' it.VE AUXILIARY 095 7 SWV 050 l ouTt ET isolation FOR MUHE l A AND WDHE 1 AUXILIARY 095 7 DCV 190 l DCT.l A OVERPRESSURE CONTROL VALVE AUXILIARY 095 7 DCV-191 l tKIT ID OVERPRI:SSURE CONTROL V ALVE j AUXILIARY 095 7 j SWV-354 I SW FROM RD I AN COOLERS ISOLATION V ALVE i AUXILIARY 095 7 j SWV 355 l IC I ROM RD FAN C(x)LER51 sot ATioN VALVI-l AUXILIARY 095 7 i SWV 353 j sw To Ru f AN LOOLERS LSOLATION VALVE l AUXILIARY 095 7 i RWV 150 l RW RECIRCULATION FLOW CONTROL V Al.YE l AUXILIARY 095 7 i DCV 186 } NITROGEN SUPPLY To lX'.T.l A } AUXILIARY 095 7 J DCV 188 l NITROGEN SUPPLY To DCT In AUXILIARY 095 MU 015f0C] 7 MUV 16 CONTRot AUXILIARY 095 7 MU-025 POC MuV 31 CONTRot AUXILIARY 095 I 7 i OWVl% GWP lA C'JNTROL VALVE TURBINE E~ 8 RCV,Il j rRrasORIZlR Block VALVL REACTOR 168 8-l RCV 13 i PRESSURIZER INLtT AUXILIARY SPRAY ISOLATION VALVE l REACTOR 145 8 l RCV 53 i DH TO PRESSURIZER AUXILIARY SPRAY ls0LATION VALVE i REACTOR 145 8 l FWV 29 l 015G u MAIN block VALVE i INTER 142 8 i FWV-32 i OTso a low LOAD DLoCK VALVE l INTER 136 8 i FWV 33 l oisG u sTARTurlaOCK VALVE ~ l INTER 136 j 8 FWV 36 i OTSG A STARTUP BLOCK VALv' i INTER !36 8 l FWV 30 i oiso a MAIN nLock s ALVE l INTER 136 8 i FWV 31 I OTSG A LOW LOAD block VALVE l INTER 136 ) ARV 49 i VACUUM DRLAKER RELIEF FOR CDHr JD l TURBINE 127 8 8 i MUVlW l MUrt 2A/MUrt.:n nyPAss v7LVE l AUXILIARY l 123 8 1 FWV 14 i I El.uwaita RUMP a suction ISOLATION V ALVE l TURBINE I 121 CLASSORT.XLS Page 5 OF 18 12/11/1997
SSEL Sortsd by Class, CALCULATION S97-0541, Elevstion, REV.O, and Building ATTACHMENT 'S' Tag Number - l Tag Number description ' l Building l Elev. 8 FWV 15 { IEEDWATER PUMP B SUCTION ISOLATION VALVE I TURBINE l 121 8 MUV 100 1 MUtbl A'MUrt lo BYPASS VALVE j AUXILIARY j 119 8-l- MUV 112 { LETDOWN TO MUT 1 On wp DIVERTER i AUXILIARY l !!9 8 MUV 018 { RCP SEAL ISOL ATION VALVE i AUXILIARY 119 8 MSV 055 i OT50 A TO F FTB-1 STOP CHECK INTER l 119 8 i MSV-056 l OTSO B TO EFTD I STOP CllECK I INTER l 119 8 CFV 5 l COKE FLOOD TANK A DISCHARGE ISOLAllON l REACTOR I 119 8 CFV 6 f CORE FLOOD TANK B DISCHARGE ISOLATION REACTOR l l19 8-ARV-48 l VACUUM BREAKER REtlEF FOR CDHE-4 A TURBINE I19 8 FWV 28 i rEEDwATER PUMPS DISCll ARGE CROS$ TIE ISOLATION VALVE I TURBINE 109 8 M UV-023 j llP lNJ CONTROL VALVE iO RCS INLET LINES LOOP A j AUXILIARY 095 8-MUV 024 l HP IN1 CONTROL VALVE TO RCX INLET LINES MnOP A l AUXILIARY 095 8 MUV 025 l HP IN1 CONTROL VALVE TO RCS INLET LINES LOOP a l AUXILIARY 095 8 MUV 027 l ifPl CONTROL VALVE TO RCS LOOP A l AUXILIARY 095 8 MUV 026 l HP INJ CONTROL VALVE TO RCS INLET LINES LOOP D l AUX 1LIARY 095 8 MUV 073 I DwST TO MUP la & MUP IB ISOLATION VALVE j AUXILIARY 095 8 MUV-058 l Ill PRESS INJECTION SUCilON F ROM DwST i AUXILIARY 095 8 ASV 2tM i ETTD-1 STEAM ADMISS:ON i INTER 095 8 ASV-005 l ETTD l STEAM ADMtS$10N 1 INTER 095 8 EFV 01 I ilOTWE'.L ISOLATION TO TURBINE DRIVEN ETP 2 l INTER 095 8 EFV 02 l HOTWELL ISOLATION TO MOTOR DRIVEN EFP 1 l INTER 095 8 EFV 03 i CDT 1 AND ETT 2 ISOLATION TO ErP-l l INTER 095 8 EFV44 j CDT 1 AND SrT 2 ISOLATION TO ErP.2 l INTER 095 S j CAV-126 RC LF.TDOWN SAMPLE INSME PLNETRATION ISOLATION V ALVE REACTOR 095 8.1 j RCV 10 PRf3SURIZER POWER WERATED RELIEF VALVE l REAC'IOR 168 8.1 All 196 SV AHD-l. AHD ID. AllD 2 & AllD 3 CONTROL CONTROL 164 8! All 199 SV l / HD-4 & All!15 CONTROL CONTROL 164 8,1 1 All 246-SV j AHD-12 CONTROL l CONTROL 164 8.1 All433 ASV l AHD-1. AllD ID. AHD-2. & AHD-3 CONTROL CONTROL 164 8.1 All 033 SV l AllD-l. AHD-ID, AllD-2, & AUD 3 CONTROL l CONTROL 164 8.1 l All 381 ASV l AHD-l. AHD-ID. AllE AHlk) CONTROL l CONTROL IM 8.1 All-381 SV l AHD 1, AllD-ID. allD4. & AHD-3 CONTROL l CONTROL 164 8.1 All-MS ASV l AHD-l. ^HD-ID. AllD 2. & AllD-3 CONTROL l CONTROL 164 8,1 All 648-SV l AHD l. AHD-lD, AHD-2, & AHD-3 CONTROL l CONTROL 164 8.1 { All 649 ASV l AUD 1 AllD ID. AHD 2. & AHD 3 CONTROL l CONTROL 164 8.1 } All 969-SV k AllD-3 CONTROL i CONTROL IM 8I l All 966-SV l AUD l CON TROL i CONTROL 164 8! l All 517 SV l l CONTROL 164 SJ l All 518-SV } } . CONTROL 164 81 l All 194 SV I AHD-13 & AHD 14 CONTROL i CONTROL IM { AII 195-SV l A!!D 15 & AHD-16 CONTROL j CONTROL IM 8.1 ~ 8.1 l - All 200-SV AHD 6 a Allo 7 CONTROL-l CONTROL IM 8.1 All 968-SV I AUD 2 CONTROL i CONTROL 164 8.1 - All 970-SV l AHDm enNTROL l CONTROL IM [ 8.1 { - All 953 SV AHDM ts4 TROL l-CONTROL IM . 8. I I /.ll 967-SV. AHD-I & AHD-lO CONTROL l AUXILIARY 160 8.1 Cll\\-108 ) NORMAL COOLING TO AHHf 43 tSOLATION VALVE t CONTROL 131 8.1 CilV-097 APPX R COOLING TROM AHHL44 tSOLATION VALvt 1 CONTROL l 125 - CLASSORT.XLS Page 6 OF 18 12/11/1997 ~
SStL Sorted by Class. CALCULATION $97 0641, t bvstion, RtV. O, I cnd Building ATTACHMENT 'S' l Tag Numler l Tag Fumber docri dte 4 ~^ l Ilullding lLiet. l 8.1 CilV.100-SV i CHV.Kx1 CONTROL l CONTROL j 124 8.1 CilV 101 NORM AL COct.ING IROM AllHl44150LAlloN Y ALYL l CONTROL i 124 8.3 City l13.SV Cliv.113 CONTkot i CONTROL l 124 8i CllV4190 NORMAL CooLIN010 AHHt44 tsoLATioN VALYL CONTROL 124 f 8i All 250 SV AllD 1i & AHD-22 lost ACCiutN1 CON 1 Rot l-AUXILIARY i !!9 l 8l All 310-SY ) iib 87 CON 1 Rot AUXILIARY I 119 8.1 All.3tiSV l AHD88 CONTROL AUXILIARY I 119 8.1 i CAV 057.SV l CAV57CONikot i AUXILIARY I 119 8I l CAV 060 SV CAv w CON 1 Rot AUXILIARY l !!9 f AUXILIARY j 119 ~ 81 l MUV-103.SV MUniO3 CONT Rot. 8.1 i SWV 012 SV1 SWV 12 CONT ROL j AUXILIARY 119 i 8.1 SWV 012 SV2 I swv 12 CONTRot j AUXILIARY 119 71 MUAO-SV MUv31AIRfAILloCE I AUXlLIARY 119 8.1 '~ LGV 36 1 DG A AIR START $oLINotD YAlvt DIESEL I 119 8.1 EGV 37 LDO A AIR siART SOLLNotD YALvt DIESEL 119 d ~~ 81 EGV 40 l 1 DO P AIR $T AP.1 SOLLNotD VALvt DIESEL 119 81 LGV41 i Ltx2 D AIR START soLLNolp YALyt DIESEL 119 81 { All.365 SV I AHD (M ONikot DIESEL !!9 8I I All 366.SV AHDe CON 1ROL l DIESEL 119 8I l All 367 SV l AHDas CONTROL DIESEL 119 8.1 l All 368 SV _l AHua9 CONTROL DIESEL 119 8i j All 35$.SV l AHD43 CONTRot DIESEL 119 81 l All 356 SV l AHD-63 CONikol DIESEL 119 ~ 81 i All 357 SV AHD48 CONTROL DIESEL 119 8.1 i All 358.SV AHD42 CONT Rot DIESEL 119 8.1 j I;GV 56 iDG A AIR START val.vt DIESEL 119 8i i !!GV 57 100 A AIR START VALYL DIESEL 119 - 8.1 l'GV 58 LDO D AlR START VALYL 1)lESEL 119 8I EG V 59 l I DG D AIR ST ART VALVL i DIESEL !!9 8.1 l EFV 58 I Lir i To OTSO A CONTROL. V ALVI ' INTER 119 8.1 l MSV 411 SVI MsvallCdNlRat INTER 119 ~ 8.1 j MSV 411.SV2 Msva ti CONikot INTER l 119 8I i MSV-411 SV4 Msv-41 t CONTRot INTER 119 8.1 MSV 411/412 SV5 i Msvall A Msval2 CONikot ih TER 110 8.1 MSV 411/412-SV6 l MIV 4tl A MsV412 CONTROL l'NTER I19 8I l MSV 412 SV1 Msvai2 CONTRot INTER 119 d1 l MSV 412 SV2 l MsV-4:2 CONTRot i IN ER 119 81 [ MSV-412 SV4 } Msvat2 CONTROL i INTER 119 1 8 -_1 l MSV 413 SVI f MsV413 0tw1 Rot INTER 119 8.1 MSV 413.SY2 i Msv.413 CONTROL INTER 119 8.1 I MSV 413-SV4 7 Msv.413 CONTRot i INTER 119 8.1 l MSV 413/414 SV5 { Msv 415 A Msv 444 CONT Rot INTER l 119 8l l MSV 413/414 SV6 i Msval) A Msvat4 CONTROL INTER 119 L 8,1 - i _ _MSV-414 SV) l MSV-414 CONT Rot INTER 119 8~l i MSV-414 SV2 i Msv414 CONTROL 1NTER 119 ~ 81 j MSV-414 SY4 Msvai4CONTRot j INTER 119 8.1 1 M UV-050 SV l AUXILIARY l 108 MUvoo ContRot 8.1 'i All 971 SV AHn 12 CONTRot CONTROL j 108 CLASSORT XLS Page 7 OF 18 12/11/1997
SSEL Sort:d by Class, CALCOLATION $97-0$41, Elsvation. REV.O, end Duilding ATTACHfJi[NT 'S' I
- [* l Tag Numi>er Tsg Numlier description -
f Itullding l Tles. 8I l ScV.100 l I AP-lu AtAlit ir CoouNo w At t R 150LATsoN VALu 1 URlilNE l 107 4 81 l SCV 099 i IAP.I A & IAHL.I A Cm> LING w Alt R 150LATloN YALvt 1 'IURIllNE j 107 8I ( hlU 015-SV { MUv n. AIR I Att LOCK s AUXILIARY l 095 AUX 1LIARY l 095 8l l hlU 025 SV l Mov.): Ain rAtt Lock 8.1 j hlVV 049 SV l MUV-49 CON 1ROL AUX 1LIARY l 095 81 } SWV.151 SY j swv.isi CONTaot AUXILIARY j 095 8I i SWV.152SVi swv 1$2 CONTRot AUX 1LIARY j 095 81 1 SWV.152SV2 i swv t$2 CON 1 Rot AUXILIARY j 095 8l { SWV.333 SV2 j swv 353 CONTRot AUXILIARY i 095 8l l SWV.354 SV1 swv 354 CONT Rot AUXILIARY j 095 8.1 SWV.354 SY2 I swv-)s4 CONTRot i AUX 1LIARY l 095 81 i SWV.355 SV i Swv35$ CONTROL i AUXILIARY l 095 8.1 j SWV.353 $V) j $wV JS) CONT Rol i Al'XILIARY j. 095 8.1 CAV402 j WR AND LITDow N OU1$1DL PLNLTRAlloN $AMPLL isoLAlloN I INTER l 095 8.1 EFv 56 LIP-2100150 A CONTROL VALYL { INTER 095 8.1 El V 55 t iP 210 otsa n CONinot yAlvt j INTER 095 81 7 1;FY 57 Li P l To 0T50 B CONikol V Alvt j INTER 095 ~ 8.1 j IAV.188 j IAP,l A Lo4Dl UUNLOADLR VALvt TURBINE 095 8i j I AE.lli9 14P ID LoADLR'UNLoADLR V ALvt TURillNE 095 i ~9 l AllF.17A l CONTROL COMPLEX NORMAL $UPPLY f AN A CONTROL 164 9 Alli.19A l CON 1ROL COMPLLX kETURN I AN A l CONTROL 164 9 Altl41714 [ CONT ROL CoMPLLX NokM AL SUPPLY rAN D j CONTROL 164 9 l Altr.1911 i CONTROL CoMPL LX RLTURN F AN n l CONTROL 164 ~ 9 AllF 22A tutsi L ctNt RAfoR Room A 5UPPLY j DIESEL 137 9 AllF 22C l[ DIL$t L GlNL RAloR Room D $l'PPLY j DIESEL 137 i 9 i AllF 22:1 l DitsLL OLNtRAton Room A SUPPLY l DIESEL 131 9 i AllF 22D l Dilstl GENLRAtoR Ro0M B SUPPLY i DIESEL 131 ~ i 9 Alli 01A Rt.ACloR Dull. DING AIR HANDLING f AN A REACTOR 126 i 9 j AliF-Ollt i HrAClon nUILDING AIR HANDLING l AN u REACTOR 103 9 l AllF 01C j RL ACloR DUILDIN AIR ll ANDLING rAN C i REACTOR l 103 10 I All!!E45A j CootING UNIT A rok CON 1Rol COMPLLN j CONTROL 170 10 i AllllE 04 A i IILATINa dNIT A roR CONTROL CoMPLLN j CONTROL 170 10 i AllD 07 l Attr 17e DisCHApot j CONTROL 170 10 _AilllE 0511 i CootING UNIT D IOR CONTRot COMPLLX l CONTROL 170 to I AllllE 0413 j HLATIN0 0Nii n l0R CONTROL COMPLEX j CONTROL 170 10 AllD-03 i CONIROL COMPLEX I ANs tNTAKE ~ ! CONTROL 164 10 i AllD 13 l AHF 19A INT AKE i CONTROL 164 ~ 10 l AllD 15 i Aur 19e INT Akt CONTROL 164 10 i AllD-14 AltI-10A DiscilARCL j CONTROL 164 to i AllD 16 i Aur tva DiscilARGL i CONTROL 164 10 l AllD 02 i PN0UM ATIC RELIET To ATMosPHIRt i CONTROL 164 10 i AllD 04 i Aur t1A INTAKr l CONTROL 164 10 l AllD 06 i AHF17alNTAKE j CONTROL 164 10 l AllD 99 VINTittATioN LQuiPMENT Room SUPPLv AIR CONTROL 164 to i AllD--05 j Aur i?A DisCHARc0 } CONTROL 164 10 t AllD-01 CONIRot COMPLLX MAKE UP AIR i CONTROL 164 All 19EIDS) 4 AllD-3 CONTRot i CONTROL l 164 [l 10 AllD OlD l CONikolCOMPLEX M Akt UP AIR i AUXILIARY I 160 10 CLASSORT XLS Page 8 OF 18 12/11/1997 -~]
SSEL Sort:d tw CI:ss. CALCULATION $97 0541, t CI:vitcn. REV.O. cnd Builbng ATTACHMENT'S' Tag Nmber l Tag Number dneription ~* l Building l Elet. 10 All 196 lOS4 AllD-ID CONT ROL AUXILIARY l 160 10 All 196 lOSI AfiD.I CLNTROL j CONTROL l 160 10 AllD.87 Allr-IA DISCllAROL l AUXILIARY l 128 i 10 AltllE 31A i GOLINO UNIT A l-OR ltLAC10R BUILDING REACTOR l 126 10 AilllE 31D I C00usTONIT D IOR RLACTOR BUILDING t REACTOR i 126 10 AllilE 32A MOTOR C00Lrn ioR Allr I A i REACTOR l 126 l 10 AllD.88 Alli so DisCll ARot l AUXILIARY 124 i 10 { AilllE.4) COOUNG UNIT A f OR LIIC ROOMS l CONTROL 124 J 10 l' AllilE-44 l 000UNO UNIT D IOR tilC ROOM 5 CONTROL 124 l Alif $4A tilC R00M5 COOLING A CONTROL 124 ~ 10 10 AllF 54D f DC ROOMS LOOLING s ~ { CONTROL 124 10 AllD41 Allr4:A WsCalA RGE i DlESEL 124 10 AllD42 Allr 22J Di$CllARGl: 1 DIESEL 124 ~ 10 AllD43 t000 tA IN1tR ROOM DIESEL 124 ~ 10 AllD40 topo in IrfI R. ROOM DIESEL 124 10 AllD 58 l Alfr 22C DISClf ARot DIESEL !24 10 AllD-59 I Altr42D DISCHARGE l DIESEL 120 10 AliF48A l iPI NT ROLL COOLANT PUMP A AIR flANDLING l AUXILIARY 119 10 AliF480 l $PLNT FUI.L COOLANT PUMP B AIR llANDLING l AUXILIARY 119 to AilllE 29A COOLING UNIT IOR 51 P I A l AUX 1LIARY 119 10 AilllE 2911 C00 LINO UNIT 00R St P 1B AUXILIARY 119 10 AllD 12 SUPPLY 10 CitLMLAB CONTROL 108 10 All 196-POS2 AllD 2 CONTPOL { CON 1ROL 108 10 } AllD 2? SECON1 ARY PLANT LAR IKOD SUPPLY j CONTROL 104 10 AllD 17 9.v tLEVATION RETURN l CONTROL 103 10 AllilE-3tC { COOLING UNIT C IOR REACTOR BUILDING REACTOR 103 10-AllllE 32D i MOTOR C00Lt R IOR Allr lu REACTOR 103 10 AllllE-32C l MOTOR C00l ta rOR Alfr IC l REACTOR 103 to AllllE 30A C00UN0 0 NIT IOR DCP-l A AUXILIARY 095 10 AilllE 300 COOLING UNIT IOR DCP 18 AUXILIARY 095 10 AllllE 13A COOLING Coll $ (OR REACTOR BUIL DING PENETRATION % A j INTER 095 10 Altlit 130 WO!ING Colla TUR REACTOR BUIDUNG Pl.NETRATION e INTER 095 fl ll CilllE LA CON 1ROL COMPLEX CillLLI R A CONTROL 164 ~ 11 CllllE ill CON 1ROL COMPLtx CallLLER a CONTROL 164 12 AllP41A j CONTROL COMPLLX llVAC AIR COMhti ss0R A } CONTROL 164 12 AllP-Olu l CONTROL COMPLEX liVAC A!k COMPRLssOR n l CONTROL IM 12 l AllP 01C CONTROL COMPLLX livAC AIR COMPRLss0R l CONTROL iM 12 AllP 01D l CONTROL COMPLEX llVAC AIR COMPRLsSOR D j CONTROL 164 12 All 506 PS I AllP I A A Alistin CONTROL l CONTROL 164 12 All.508 PS } AillNIC A AllP ID CON'IROL t CONTROL 164 12 WDP 1 A
- AsTE GAS COMPRLSW1 A j
AUXILIARY 095 12 WDP ill i [Asit cAs COMPRLss0R a l AUXILIARY 095 12 IAP IA. l frisiRUMENT Alk COMPRESSOR A l TURillNE 095 12 IAPID I INSTRUWENT stR COMPRESS 0R D j TURBINE 095 j 12 SAP,1 A k 5iATibIAIR COMPRESSOR IA j TURBINE 095 ' 12 sal lu i 57AtsoN AIR mMPRLss0R 10 l TURBlNE 095 l ACDP-51 l GWTROL COMi' LEX DliTRIDUTION PANLL A l CONTROL 145 14 14 1 ACDP-52 i Covinot Catn Lt Dtstatav1:0N PANLL a i CONTROL 145 CLASSORT.XLS - Page 9 OF 18-12/11/1997 l i,- ,., - -. ~ y p + - - - - - - ~ g,. +. -, ._-y, -,,.
SSEL Sof ted by Clus. CALCULATION S97 0541, 'EI)vauon. REV 0, and Buildin0 ATTACHMENT *S' l Tag Number l Tag Number docription ~ f flullding lI:let. 14 1 VDDP 01 1 R100LAT! D INSTRUMENT bus 3A 1 CONTROL i 145 14 I VilDP 02 l k!6UtATLD INSTRUMLNT BUS Ju l CONTROL l 145 14 VilDPa) i VIT AL DUs A l CONTROL l 145 vt1 AL DUs b j CONTROL l 145 14 VDDPO4 14 VIIDP45 vliAL DUs C l CONTROL l 145 14 VDDP 06 vit AL BL5 D l CONTROL l 145 14 VDDP47 COMPUT ER I:0 VAC DISTRIDUTION PANLL i CONTROL i 145 14 DPDP 4Il CONTROL COMPLEX (C PANLL. 3B i CONTROL j 124 14 l DPDP5A 2*l2SV DC Es PANIL A CONTROL I 124 14 j DPDP51] 2m12sv DC Ls PANIL B CONTROL i 124 14 j DPDP8C7 23~l:5 VOLT tc triC PANLL D CONTROL 124 14 { DPDP8D 2m125 YOLT DC LLic PANEL D CONTRO!, 124 14 ACDP 68 t$ Dl57RIDUllON PANLL 3 AB CONTROL 124 14 VDDP10 I LIIC vl1 AL DUs B CONTROL 124 14 { VilDP 11 i Lile VIT AL BU5 D CONTROL 124 14 VilDP 08 Ilic vriAL Bus A CONTROL 124 14 ' VijDP 09 I ric VITAL Bus C CONTROL 124 14 DPDP 6A 1
- wl:SV DC t$ DILSLL OLNt RATOR PANI L A I
DIESEL 119 DPDP-611 i 2*1:SY DC L5 Dir 5LL GENERATOR PANI L 8 j DIESEL 119 14 14 ACDP-05 j Dit$LL 900M 410 VOLT DISTRIBUTION PANLL 3A l DIESEL 119 14 ACDP 06 I DILSEL ROOM ano YOLT DisiRfDUTION PANLL 3D DIESEL 119 ~ 14 DPDP 3D i 2Dl23V DC TURDNil flulLDING PANLL D 1URIllNE 119 14 DPDP.I A I 2212SV DC MAIN PANI L 3A CONTROL 108 14 DPDPlil
- Wl:3v MAIN PANLL 31 CONTROL 108 14 DPDPBA
- W123Y DC L15LNTIAL SLRVICLS PANLL A CONTROL 108 14 DPDP-811 i
2W123V (C ISSLNTIAL SLRVICES PANLL n CONTROL 108 14 VitDP 12 i 120 VOLT RWULATLD DITTRIBUTION PANFL CONTROL 108 14 VDDP13 120 VOL1 RLOULATLD DISTRIDUTION PANI L CONTROL 108 14 VDDP14 120 VOLT RI,GUL* TI D DIST RIBUTION PANLL CONTROL 108 14 VilDP 15 1 1:o v0LT REGUL ATID DISTRIBUTION PANIL CONTROL 108 14 DPDS1A l BATTERY 3A DISCONNLCT $ WITCH CONTROL 108 14 DPDSID j u4TTtRY 3D DISCONNICT swl1Cli . CONTROL 108 14 DPDP-lC l 1mt2sv DC M AIN PANEL 3C TURDINE 095 ~ 14 DPDP 3A 1 234121V (C1URHINE BUllp!NG PANLL A I TURDINE 095 14 DPDS-IC nATTERY 3C DISCONNLCT SwiTCit i TURDINE 095 14 DPXSIC DPDC 1 lNPUT IVWER TRAN5f'l R SwlTC11 i TURBINE 095 15 DPilA lA
- WilSVIMTTERY A j
CONTROL 108 15 DPDA III
- st:SV BATTERY B l
CONTROL 108 15 f DPDA-lC
- wl:5v B ATTL RY C l
TURBINE 095 16 DPilC.l A 1 LaTTERY CilARGtR A CONTROL 108 le DPDClC i DATTERY Cli AkotR C l CONTROL 108 16 VillT.l A DUAL INPUT INViRif R 3A 1 CONTROL 108 16 DP11C IE p ATTERY CilARGER E j CONTROL 108 ~ 16 DPi1C ID aATTERyCitARGtRa i CONTROL 108 16-DPilC lO DA)TE RY CilARGER D l CONTROL 108 16 DPflC lF nATTt RY CI:ARGLR r l CONTROL 108 ~ to Vil!T l:1 l DUAL INPUT INvt RitR 30 i CONTROL 108 16 VDIT lC i DUAL INPUT INv0RitR 3C l CONTROL 108 CLASSORT.XLS Page 10 OF 18 12/11/1997
SSEL S:rted by Wsa. CAL CUL AT!ON 597 01,41
- Ibution, RC V. O, tnd Owltling ATTACHMENT T YE' f lag Numiner l
Tag Numt cr dntnlRion ~~ Iluilding l Lin. am. 16 l Villi lD DU AL INPUT INVI R11 R 3D { CONT ROL 108 16 Villi IL i DU AL input ins t wit R 31 i CONTROL i 108 16 [~DP!)C lO l it A11t RY rH A RGI R o I 1 URillNE 095 16 i DPliC4 'l D AT1t RY CH ARGE R if T UR111NL i 095 16 DPitC Il i H A111 R Y CH ARGI R I i TURillNE 095 17 i 1.GDG l A Otist t GtNIRAloR A i DIESEL -,i 119 17 ) I GDG-ill i toi st L Gt.Nt R A1oR D { DlL$1:L i 119 18 C11378 PT i CHW ON1Rol of ritul.i A CONTROL 164 18 C11379 PT CHV (McoNTRot of CHHt.in t CONTROL l 164 4 18 ~ SF.911T NPI N11 DL L Cool A Ni iloW ik ANM0111 R AUXILIARY j 143 18 i hlO414-LT[ M Aki-UP T ANK ilVI L TR AN%IIT11 R AUXILIARY } 119 1B { h1U414-LT2 { MA Al UP TANK LLVIL TRANsMirit R I AUX 1LIARY j 119 18 hlU.Ol?.P1 l M Akt -OP T ANK PRLntit 1RANufrtii R l AUXILIARY l 119 18 l CA ll LT Hokic ACIO S10kAGE TANK A AUXILIARY j 119 ~ fiA.13-LT i DokiC Arto slouGL TANK n AUXILIARY l 119 18 1B i ht ti-018-DPT l !!1 D0% N ilL1(R DLL1 A P 1RANsMITTI R AUXILIARY j 119 18 1 blV#4DPTl t t i DoW N iloW 1RAN%itTTI R l AUXILIARY 119 lit hlU481 DP1 i ! I T-Dow N PRL-Illit R DILT A P IRA NullT11 R l AUXILLARY 119 IN httW4DPI i t T DOWN iloW 1RAN%11TTLR i AUXILIARY 119 1 18 Dil47.LTI boRATI D wATI R VroRAGL t ANK LI Vi t i IJWS1 I 119 18 Dil.071.T i jg ~ Hok AllD % All R sTokAGI 1 ANK Lt VI L i 11WS1 i 119 [)F 1.L$ I Dl!siL GINt RAloR 8 UIL oit D AY T ANK A LtVIL swlicit i DIESEL l 119 Jg f pf.2.LS } DilALL OLNIRAfoR IUllolL DAY TAN A A llvil sWITCal I DIESEL l 119 Ill Dji) l.S l Dilst L GI Nt R A lor it'll OIL DO TAN A D LLVt L awliCil DILSEL I 119 j$ DT.4-LS j Dil si L Gt N1 RA tor I Ul L oil DA Y T ANK D LLVI L SWITCH l DILSEL f I19 18 i ! l.98.LT l t ut kGtNCY llLD% Alf R TANK tIVLL I LFW TANK l 119 18 ) LF 99 LT i !MIRGI NCY lilD% All R TANK l LVIL l El-W TANK { 119 18 hts 108-PT j M AIN s1L AM ilNI A 2 PRI Mt'Rl 1RAN%11Ti( R ( INTLR j 119 la hiS.106-PT M AIN sifA M LINL A : PRrssekt 1R ANsMir11 R j INTER j 119 13 blS 107 PT i M MN sil AM L INL A.] PRI %t'R[ T R AN%11111 R l INTER l 119 4 18 1 his.lD9 PT l MMN sit AM LINT A 1 PRLnURL TRANsMITit R ( INTER l 119 18 hts-110-PT M AtN STL AM LINL H 2 PRL%t*RL TRANSMIT 11 R INTER 1 119 18 his.llLPI j M AIN sit AM LINL D 2 PRIMURL TRANutlill R j INTER i 119 18 hlS. I l l.PT M AIN sit AM tINL D l PRLbt'RL TRANuttrit R l INTER i 119 15 hts Il3 PT I LE D1137 LT ~ MalN s1L AM ilNE D I Print RI TR ANutlTit R l INTER I 119 DORATLD wAli R siokAGL T ANk t i si t NAOll TANK 119 i 18 510 031111 EcP MI si AL Riit'RN ilow TRAN%Ill1LR REACTOR 119 18 hlU ORFT2 kcP M2 51 AL klit RN IL 0% 1k ANullrit R j REACTOR ' 119 la + hlV44FT) kcP 3pi sL AL RLTURN ILow ikANsulTil R l REACTOR 119 13 hlV431ST4 RcP 3rt2 s!.Al. R t10kN il.ow 1 RANutt r1 t R I REACTOR I 119 18 hlD407 DPTI Rcr 3 u st At INJ citos it 0% TR ANut!111 R i REACTOR I 119 18 4 klUa17 DPT2 l RI P 3 AJ slat NJictioN it o% 1R ANut31TI R REACTOR 119 18 hlU.007 DPT3 i kcP 301 sLAL isit ciloN IL 0% TRANutitTi R i REAClOR 119 18 i hlUa17-DP14 Rcr 3ti2 srAL IN!!c1los I t oW 1R ANuti rTI R 18 CDodLTl REACTOR I 119 coNDt Malt sloRAGr T ANK LLsi L TUR111NE [ 119 IS AlV423-DPil + in PRLss isitcTioN itoW Loop o : AUXILIARY { 095 1R M U 423.DPI2 i H1 rutn INir clioN riow t our A 2 i AUX 1LIARY 095 IB AlU.023-DPf 3 i lu Priss N>t c11oN itow tooP a 2 i AUXILIARY j 095 Cl. A S SORT.XLS Page 11 OF 18 12/11/1997
~ _ -. 8 SSEL Sort:d by Class. CALCULATION $97 0641. Ehvation. REV,0, cnd Dwidmp ATT ACHMENT 'S' l Tag Number l Tag Number description ~ f Building lElev. 18 l MU 023 DPT4 { ill PRi$s INJLCllON ILow LOOP A 1 AUXILIARY i 095 18 j MU 023 DPT5 l lti PRLis NLCTION FLOW LOOP B i AUXILIARY l 095 18 i MU 023 DPT6 ! 10 PRLss NteTioN iLow Loop A i AUXILIARY l 095 18 MU-023 DPT7 l lil PRLS$ INILCTION Flow LOOP e AUXILIARY 095 AUXILIARY f 095 18 MU 023 DPT8 j Hi Priss INif CTION iLOw LOOP A 18 MU 027 DPT { kCP Tot Al sLAL INJLCTioN I Low TRANsurT1r R AUXILIARY l 095 18 MU 002 PT PRLssURt To RCP SEAL 5 i AUX 1LIARY l 095 ~ 18 MU 024 DPT I M AKt UP l LOW TRANSMIT 1 LR { AUXILIARY l 095 18 MU424 DPr2 i M AKI Ur rtow TRANsMITTta i AUXILIARY l 095 18 ~i DC 05 PT i DCP 1A DisCH AROL i AUXILIARY l 075 18 i DC 50-LT DC svRGE TANK DL*1 IA LivrL AUX 1LIARY 095 ~ 18 DC 06 PT DCP.to DISCHARGE PutisURL j AUXILIARY 095 18 - DC 54 LT t DC sVRat i ANK ocT la LLvt L AUXILIARY 095 18 RW.09.PT DLrAY liLAT stA wAf tR PUMP A DisCHAkct PRI3WRt AUXILIARY 095 ~ 18 7 s w.002 Pr l WCt f.AR si RvlCL CCc PUMPS DiscilARot PRLssURL AUXILIARY 095 18 RW 23 PT NUCLtAR sLRvict stA wATLR PUMPS DistilARGE PRtsSURt AUXILIARY 095 18 RW 08 PT DICAy lit AT stA wAt t R PUMP H DistilARGL PRLsSURE AUXILIARY 095 18 5W.135 PT NUCt TAR stRVICL COOLING w ATtR sVROL TANK PRLisURL AUXILIARY 095 is sW.139 LT NUCLi AR stRVICC COOL.ING wait R sVRGr TANK LEvtL AUXILIARY 095 18 M U.102.DPI kCPit AL INilcil0N TIL1LR DLt.TA.PINDICAToR AUXILIARY 095 18 j r.P 24 IT i LI N To ois0 B ITow INTER 095 7 EF.26-17 LIN To of so A Itow INTER 095 18 l'F-23 IT t t P I To oiso-n i tow INTER 095 18 I EF 251T l I f P.10 01s0 A rLow INTER 095 18 SP 17 LT l 511.AM GENERA 10R A LLv!L j REACTOR 095 18 $P 18 LT j stt AM Gl.NLRA10R A lAvr L REACTOR 095 18 l SP 19.LT 51EAM GEN!RATOR A LtvLL REAC' LOR 065 18 ' l SP-20 LT j s1 RAM cLNIRAfoR A LLvit l REACTOR 095 18 [ SP 21 LT j sTLAu ctNt RATOR D LLvtl. REACTOR 095 18 $P 22 LT i 5, TAM 01flLRATOR D Ll;vtt REACTOR 095 18 SP.23-LT sli AM G1NLRATOR D LtvtL REACTOR 095 IB SP.24 LT siLAM GLNI RATOR D L LYLL l REACTOR 095 is SP.25-LT STIAM 6t NLMTok A l EsiL l REACTOR 095 -. -18 SP 26 LT l STEAM cLNERAToR A ttvil i REACTOR 095 18 SP-27-LT j 51 LAM GINLRATOR A t tv0L j REACTOR 095 18 j SP-28 LT i strAM ctNLRATom A LiYLL l REACTOR 095 18 SP-29 LT sit AM UENLRAloR p LLs LL REACTOR 095 la SP 30-LT l sTI.AM GLNLRA10R R Ltvil REACTOR 095 18 SP 31 LT j sit AM GLNtRATon u LLvt L REACTOR 095 18 SP-32 LT j STLAM cLNERATon a Lts EL j REACTOR 095 18 RC 001.LTI i PRL$sORIZE R Ltvil TRAN%tlTTER i REACTOR 095 I - 18 i RC-00l LT2 i PRLssuutztR Ltvit TRANutitTER l REACTOR 095 18 j RC 001.LT3 PRLssoutrLR ttytL TRANsurT1: R l REACTOR 095 18 j RC.131 PT j RIAC10R Cool ANT sYSTLM PRt$RRE } REACTOR 095 18 RC 131 PTl i ktArtou cootANT sysTIM PRfAsURL l REAUTOR 095 l 18 RC414A DPil } RLACTOR CootANT SYsTLM 610T Ltc A Itow l-REACTOR l 095 18 i RC-014A DPT2 i REACTOR Co0LANT SYSTEM HOT LLO A LLOw i REACTOR l 095 18 i RC 014A DPT3 i Ri ACTOR C00LANT sysTrM Hot Ltc A ILow i REACTOR i 095 - CLASSORT,XLS Page 12 OF 18 12/11/1997
- ~ ~ ~ f SSEL Sort:d by Cim. CALCULATION S97 0541 El:vation. REV.O, and Building ATTACHMENT *S' Tag Numlier l Tag Number description l Huilding l l'in. ~ 18 RC 014A DP14 l REACTOR CootANT 5YSTLM HOT LIG A flow j REACTOR j 095 18 RC 014D DPTl l REAGOR C(X)LANT S)ST[M HOT LEG 8 7 Low REACTOR { 095 18 j RC41411 DPT2 l RLACTOR COOLANT sytTI.M Hot Lia a Flow REACTOR i 095 18 l RC414D DPT3 l FI Actor COOLANT SYs1LM HOT LIO B ILow REACTOR l 095 18 RC4148 DPT4 i RLAct0R COOLANT sysTt M HOT t IG B f Low i REACTOR l 095 j 18 RC-003A PTl l REACTOR COOLANT SYSTEM PRE $sURE TRAN$MITTI R j REACTOR 095 18 RC40A PT2 RLActOR COOLANT 5YSTEM PRL55URE TRAN!iMITTLR l REACTOR l.095 18 j RC 003A PT3 l RfAMOR COOtANT $Y$1LM PRL$$URL TILANiMITTIR REACTOR l 095 18 RC403A PT4 l. RLACTOR COOLANT $Y$TLM PRBSURE TRANsMtTTLR j REACTOR l 095-18 RC4K)3!! PTl l RtACTOR C00tlNT SYS11 M PRE $$URC 1RAN5MITTER i REACTOR I 095 18 RC403D PT2 RIACTOR COOLANT SYSTLM PRI$$URL TRANSMtrif R j REACTOR l 095 18 RC4U3D PT3 l REACTOR C00 TANT $YSTI M PRB50RE TRAN5MITTER l REACTOR 095 18 1A 04 PT~] INSTRUMLNT AIR HEADER PRL55URt f TURBINE 095 18 CD 100 LT l CONDI N$LR CDHE4 A HOTW[LL iLYLL l TURBINE 095 18 CD 101 LT l CONDLh$LR CDHE4n HotwLt.L Ltytt j TURBINE 095 18 l NGV4V9 ADY DACKUP Nf1ROGEN SUPPLY VALVE j TURBINE 095 18 f NGV 308 ADV BACKUP NITROGLN SUPPLY VALVE l TURBINE 095 18 l lA 12 PS INSTRUMLNT AIR COMPRL550k LOAD / UNLOAD PRL$5 Sw!TCH l TURDINE 095 19 RC402 TE! PRLss0Rlzi R TLMPt RATURE REACTOR 139 19 RC-002 TI'2 PRLssVRrz[k itMPt RATURF l REACTOR 139 19 CA 10 TE horTOM DORIC ACID STORAGE TANK CAT 4A AUXILIARY 119 19 i CA 12 TE l bonOM DORIC ACIT STORAGE TANK CAT 4D AUXILIARY 119 19 } MU405 TE l LLTDOWN LINE TEMPERATURE i AUXILIARY 119 19 RC-004D TEl i RLACTOR C00LANT SYsitM hor tra a TLMPrRATURE l REACTOR 319 19 RC-004A TEI RtACTOR COOLANT SYSTEM HOT l.LO A TlMPI RATUPE l REACTOR 119 19 RC-004A TE2 RLACTOR COOLANT SYSTI M HOT LLO A TLMPERATL;kt REACTOR 119 19 RC 004A TE3 i RLACTOR C00 TANT SYSTI M HOT LLG A TEMPERATURE REACTOR 119 19 RC 004A TE4 l RrACTOR COOLANT SYSTEM HOT LLG A TLMPERATURL REACTOR 119 19 i RC-Otull TE2 j REACTOR CootANT sysitM HOT Lro n TEMet R ATURE l REAC10R 119 19 RC404D TE3 i RrACTOR cuotANT sYsTru Hot LLG a TLMPERATURE l REACTOR 119 19 RC4XMll TE4 l RfACTOR COOLANT SYSTEM HOT LLG B TLMPLRATURE I REACTOR 119 19 RC-005A TEl I Rf ACTOR COOLANT SYSTEM CULD LLG A TLMPERATURE l REACTOR 119 19 RC405A TE2 j ktACTOR CootANT sYsTLM Col D I Ia p 1 LMPI RATURL REACTOR 119 19 RC405A TE3 } REACTOR COOLANT SYSitM COLD LLO D TEMPERATURL REACTOR 119 19 RC-005A TE4 l RLAUTOR COOLANT SYStiM COLD LtG A TEMPIRATURL REACTOR 119 19 RC4X)511 TEI i RLAnoR nioLANT sYsi t M CotD t to a it MPt R ATURL REACTOR 119 19~~l, RC-005D-TE2 i krAc10k COOLANT si sTLM COLD Lio o itMPERAToRL i REACTOR l 119 19 i i C40$D TE3 i ur ACTOR Coot. ANT systru COLD t.00 0 TEMPERATURE I REACTOR i 119 19 l RC40$D TE4 j krACTOR CootANT COLD Lt 0 a Tt MPERATURL REACTOR 119 19 RW 32 TE i DICAY HEAT COOLER DOIE ID $tA w ATT R OUTLET l AUXILIARY 095 4 19 RW 33 TE l DECAY HEAT Cooti R DCHr-i A srA WATER OUTLET l AUXILIARY 095 ~ 19 RW 13 TE i DCCAY HEAT SEA WATIR PUMP RWP44 D!sCHARGE fl MPI R ATURL i AUX 1LIARY 095 ~ 19 RW 19,TE i NUCLEAR stRVICE stA w ATER PUMP RwP48 DLSCH ARGE TLMP j AUXILIARY l 095 19 RW 12 TE i DH st RVICL SEA WATER PUMP RwPan DISCHARGE TLMPIRATURL } AUXILIARY j 095 19 { _RW43-TE i MA w AttR OUTLET NUCLtAR stRVICr CoottRs l AUXILIARY 095 -20 l AllCP-4 l sCR CADINET IOR AIDIE4A AND AHHran l CONTROL 164 20 AllPL 1 i PANEL l CONTROL 164 20 'l CCHT CENTRAt cuNTRoL noARD TERMINATION CADINET i CONTROL i 145 CLASSORT.XLS Page 13 OF 18 12/11/1997
SSEL Sorted by CI:St. CALCULATION S27 0541, Elevction, REV,C. cnd Building ATTACHMENT *S* l Tag Numi,er l Tag Number description ~ ~ l Building l Elen 20 ERI ( EVLN1s RLCORDLR CAulNET I CONTROL l 145 20 LR2 LVI.NTs PLCORDt R CABINIT 2 i CONTROL i 145 20 ER3 [Yl.NTs RLCORDt R CABINET ) CONTROL l 145 ~ 20 i LR4 j tYLNTs RICORDI R CABINET 4 CONTROL j 145 i 20 1 ERS l LvtNTs RICORDLR CABINET S CONTROL i 145 20 } ER6 l IVLNTs R[CORDtR CABINLT 6 l CONTROL I45 20 i LR7 LVENTs RICORDLR CAalNET 7 i CONTROL 145 20 i ER8 i LVI Nis RICORDE R CABINET s i CONTROL j 145 20 i ESCC1 1 ts sYsTI M Cil ANNEL TLsT CABINET I CONTROL l 145 CONTROL j 145 20 } ESCC 1 A t I s sYsTLM Cil ANNLL CABINET 1 A i 20 ESCC ID l LS sYSTIM CllANNEL CADINET in CONTROL 145 'g~ 20 ESCC 2 Es sY$1LM Cil ANNEL TEST CADINET 2 j CONTROL I45 Es SYsitM Cll ANNtL CABINET 2A l CONTROL 145 20 ESCC 2A j 20 ESCC 28 l ls SYSTEM CllANNLL CABINET 28 l CONTROL I45 20 LSCC 3 l Is siSTEM CilANNLL TLsT CABINET 3 j CONTROL 145 20 ESCC 3A l ls sYsTLM Cil ANN [LL CADINET 3A l CONTROL l 145 20 ESCP1 l MI Cil ANICAL INTIRLOCK CONTROL DOX l CONTROL 145 20 LSCP-4A l f NGIN(( RLD sAf1. GUARDS ACTUATION R1t.AY CABINET 4 A l CONTROL 145 20 j ESCP-411 i LNGINTLkED sAILGUARDs ACTUATION RLLAY CABINLT 40 t CONTROL 145 20 j LSCP 4C I NGINEERLD sAFLGUARDs ACTUATION RELAY CADINET 4C t CO?TTROL 145 20 j !!SCP-4D t.NGINtLRI.D sArtGUARDs ACTUATION RELAY CABINIT 4D l CONTROL 145 20 i LSCP-5A l LNGINEERLD SAllGUARDs ACTUATION RELAY CABINET SA j CONTROL 145 20 l ESCP 511 l LNGINLIRt.D sAf LGUARDS ACTUATION RELAY CABINET SD j CONTROL 145 20 l ESCP 5C l tNGINrLRLD sArLGUARDS ACTUATION RELAY CABINET SC CONTROL I45 20 I ESCP 5D j LNGINLI RlD SAITGUARDS ACTUATION RELAY CABINET $D CONTROL 145 20 j LSCC 311 i Es SYSTEM CliANNEL CABINET 3B CONTROL I45 20 i FSCP 1 i CONTROt. PANLL wlill e ATTERY RACK AND MoDULLs l CONTROL 145 20 t FSCP 3 i LLAsLD LINE ANNUNCIATOR t CONTROL I45 ~ 20 ICS l MAIN CONTROL HOARD j CONTROL. 145 20 ICS 1 l l Nil GRATLD CONTROL sYsTLM CABINET 1 CONTROL I45 20 j ICS 2 l INTEGILATLD CONTROL sYSTE M CADINET 2 l CONTROL 145 20 l ICS 3 i INitGRATLD CONTROL SYSTEM CABINLT ) l CONTROL 145 20 i ICS 4 l INTIGRATI D CONT ROL sYsTLM CADINET 4 j CONTROL I45 20 I ICS 5 i INTEGRATLD CONTROL sYsTLM CADINET S j CONTROL I45 20 l VHDP 05 SIP l 120 VOLT VITA, bus 3C siATUs INDICA tlON PANLL j CONTROL I45 20 i VDDPMSIP i 120 VOLT v! tat nUs 3D st ATus INDICATION PANtt I CONTROL I45 ~ 20 VliXS 2A l AUTO TR ANsri n sw!TCli rOR NN! CONTROL I45 4 20 i VHXS 211 { AUTO TRANsrER sWITC11 IOR ICs CONTROL 145 20 N11P-Al NIAP SYSTEM sUBAs5LMBLY A CABINLT I CONTROL I45 20 Ni&P-A2 i NIAP$YsitM sVBAssLMDLY A CABINri2 l CONTROL 145 20 i N11P Ill i NIArsYsTI.M $Un AsstuaLY n CAniNET 1 i CONEROL 145 20 l N!AP D2 i NIAP sYs1LM sUHAssLMBLY B CABINET 2 l CONTROL I45 20 i NIAP-Cl { NIAr sYsTLM sonAssLMBLY C CABINET I j CONTROL I45 20 NIAP-C2 Nlar sYsTt M sCB ASSLMBLY C CARIN[T 2 i CONTROL 145 20 i N11P Di Ni&P $YsTLM sVB ASSEMDLY D CADINET I i CONTROL I45 20 i N!AP D2 i NIAP sysitM son AsstunLY D CAntNLT 2 } CONTROL I45 20 NN11 i AUX 1LIARY CONTROL sYsTLM CADINET I i CONTROL I45 20 i NNI 2 1 Aux!LIARY CONTROL sYs1LM CAntNET 2 i CONTROL I 145 CLASSORT.XLS Page 14 OF 18 12/11/1997 =
_ _ _ _ _ _ - ~. SSCL Sortsd t>y CI:st. CALCULATION S97 0541, tievation, REV O. 6.nd Dmithng ATTACHM(NT 'S' I N "'E' l Tag Number l Tag Nurnber description l Ilullding I Elev. ~" 2tas I 20 1 NNI-) l AL'XILIARY WN1ROL snilM CADINLT J j CONTROL j 145 20 NNI 4 i AUXILL ARY CONTnOL 5Y$1LM CAblNI T 4 i CONTROL f 143 20 NNI S I ~ AUXILIARY CONTROL $Y111M CADINI:15 I CONTROL j 14$ I 20 NNI-6 l AUXILIAkY CONTROL sYstLM CADIND 6 CONTROL 5 145 20 NNI 7 AUXILLARY CONTROL S)STL M C ADINIT 7 CONTROL 145 20 NN14L l AUXILIARY CON 1kOL $YiM M CAalNIT s i CONTR0! l 14$ i 20 RTL MPLXR ki L Ml'111PLLXt R IOR p Ky sWi1CHYARI{ j CONTROL I45 20 1 RNR l ktCORDIR NIST RACK CONTROL I45 20 i N11 A3 l l'RolOR110N AL COUNTLR / S$lMDLY REACTOR i 140 20 l NI 2 Il3 j PkOtokilON AL COUN11 R Assi MDLY j REAC10R i 140 20 i N14C3 l CUutt NsATLD ION CH AMDl R!A$$1 MULY l REACTOR 140 20 j NI-4 D3 l COMP [ N$All D lON CH AMbi ktA$M MBLY i REACTOR 140 20 j DPTP 5A I NGINLLRLD $All' GUARDS t:C TLAT PANI L l CONTROL 1 124 20 l DP1P 51) ( NGINil klD $AIIGUARDS DC T[$T PANil. l CONTROL 124 i 20 DRRD 10 CRD AC DRLAKER CABINLT A UNIT lo ] CONTROL 124 20 DRRDIl l ( RD AC DRIAKLR CADINLT D UNIT ll CONTROL 124 20 DRRD42 l CRD Dc butAKLR CAntNLT CONTROL 124 20 i DRRD 21 l CRD DC DRIA ALR CADINLT UNIT I & 2 i CONTROL 124 20 l DRRD42 j CRD Oc ukrAKI N CAlt!NLT UNIT 3 & 4 CONTROL 124 ~ 20 l DRRD43 l CkD tic DRIAKLR CABIN [T 1 RIP Riil T CONTROL 124 20 I tilC A LMI RGINCY ll[DWATI R !N111ATION AND CON!kOL CADINI T A CONTROL 124 20 LIIC Il l l MI RULNCY I t LDWAT LR INiilAllON AND CONT ROL CAnlNLT D l CONTROL 124 20 11IC-C i i Mt RGI NCY III DW All R INiilATION AND CON 1ROL CAhlNL T C g CONIROL 124 20 LFIC D j I Mi kGI NCY i tI DW ATi.R INiilAllON AND CONikOL CADINET D [ CONIROL 124 20 Li'IC l.C A LMIRGLNCY filDWATLR AUXILIARY IQUIPMINT CADINLT A CONTROL 124 ~ 20 11IC LC D i Ml RGl NCY IIl DWAlf R AUXilI ARY l QUIPMI NT CAhlNLT 11 CON 1ROL 124 20 1: llc RC lC l I MI RGI NCY ll! DW AT[ R AUXILI ARY RilAY CABINii le i CONTROL 124 20 1.IIC RC ID l LME RGtNCY illDWA1LR AUXil 4RY RtlAY CAhlNIT ID j CONTROL 124 20 [ A1CP 1 AN1CIPAll D IR ANstl NT WITHOut sCR AM L OGlc CAntNL T CONTROL 124 ( 20 J TPC ikANSM1111 R 10% LR SUPPLY CADINL15 A A D CONTROL 124 20 VHDP 10/14/134!P j \\11 AL Hl's NT ATUS INDICAllON PANI L U f OR VHDP314'll CONTROL 124 20 VilDP ll. SIP J Vli AL, pus sT Atus tNotcAllON PANI L D IOR VHDP il l CONTROL 124 f CONTROL 124 20 j VilDP 0ll/12/13 SIP ~ Vil AL ous s1 A10s INDICA. lON PANI L A IOR VDDP R/12/Il l VilDP 0941P Vil AL DU% 5T ATU51NDICATION PANLL C IOR YHDP 9 l CONTROL 124 20 20 i RCITS A Rf AC10R COOLANT INVLNTORY TRACKING $Ysil M CAltlNLT A j CONTROL 124 _4 20 1 RC11511 R( ACTOR CO)lANT INVI NIORY 1 RACKING 5)STI M CAlHNL T p CONTROL 124 20 RCITS C kl ACTOR COOLANT INVI N10RY TR ACKING $) 51L M CAHINt:1C CONTROL 124 20 RRIIV l AUXIIIART R1(AY RACK lilAllNG AND VIN 1tLAllON CONTROL 124 20 RR PSA ) AUXlLIARY kttAY RACK l CONTROL 124 20 RRI i AUXill ARY RELAY RACK j CONTROL 124 ~ 20 j lulA i LNGINLI Rt D $AllGUARD AUxitlARY RtLAY RACK RRI A CONTROL 124 -, 20 ( RRIAll i 1 NGINI'LRt O SAf tGUARD AUXIll%RY RLLAY R ACK RRI AD l CONTROL 124 20 RRID l.NGINLLRl()SAllGUARD AUXILLARY RILAY RACK RRID j CONTROL 124 20 RR2 j AUXILI ARY R[tAY RACK CONTROL 124 20 RR2A INGINItRID SAfiGUARD AUX 1LIARY RilAY R ACK RR2A CONTROL 124 .RR2AD INGINIiRf D sAtLGUARD AUXILIARY Rt LAY RACK RR2AD CONTROL 124 20 20 RRJin j i NGINLIRLD SAllGUARD AUXILIARY RLL AY RACK RR:n CONTROL 124 20 i RR) l AUXILLARY RL LAY RACK CONTROL 124 CLASSORT.Xt,S Page 15 OF 18 12/11/1997
SStL Sortid t>y CI:ss. CALCULATION S97-0641, ' Davstion. REV.O. cnd Dwiding ATTACHMENT 'S' lag Ntuuber f Tug Numiser deuription ~ l Ilullding l Elet. 20 RR)A _ tNGINI LRID $4f EGUARD AUXILtV4V Rt LAY RACK RR)B CONTROL i 124 INGINil RID EAltGUARD AUXtLIARY RILAY lLACK kR3A I CONTROL l 124 20 RR31} I 20 RR4A i IUST ACCll>LNT MON 110RINO PANLL 44 i CONTROL l 124 20 i RR411 lost. ACatiLNT MaNilokiN" PANIL 49 I CONTROL I 124 20 J RR5111 i LNGINil RLD 5AILOUARD AUXitlAkY Ril AY llACK kR3Bl CONTROL l 124 ll 20 RR$112 t NGINIiklD sAllGUARD At,xtuARY RLLAY RACK RR.<B: CONTROL 124 i ~ 20 Ill CP-) 1 DG H [MI ROLNCY LOAD $HLDDING HLAT 1R ACING AUXILIARY j 119 20 1 IITCP 5 t t Do.A t Mr RGENCY toad sHLDDING HLAi 1R ACING AUXILIARY j l19 jI k llVAC.17A IIV AC CONTROL CADINCI I?A i AUXILIARY l 119 20 livAC.171) HVAC CONT ROL CAblNCT 17h i AUX 1LIARY 119 i 20 RCTRd ~ i RCP.14 TRANSIORMER CABINET AUXILIARY 119 20 DPTP-6A i i NGINil atD sAr toVARDs Dilst L GtNt M1on DC TLsT PANIL DIESEL 119 20 j' Dl"I'P 611 I I.NGINi l ki D $AI LOVARD5 DIEil L GLNi kAT OR DC T LST PANI L i DIESEL l 119 ~ 20 LOCP-l A tM0hGLNCY DililL GLNLkATOR A CONTROL PANLL DIESEL 119 ~ 20 LGCPill i DilROLNCY DIL5LL GLNI RA10R B CONTROL PANLL i DIESEL !!9 20 1GCP 2A i LMt AGt NCY DlL$tL GlN A ILILCTRICAL IQUIPMLNT CABfNETl DIESEL 119 20 EGCP-2il Dtl RGENCY DILSLL GLN D LLLCTFICAL LQUIPMLNT CADINET l DIESEL 119 20 l LGCP 3A i DIL$lL Gl.NIRATOR A CONTROL IV%IR RELA [CABINtt j DIESEL 119 ~ 20 EGCP3D l blL51.L GINLRATOR D 03NTROL POWLR RLLA) CADINET i DIESEL 119 20 I:GCP-4A l DilstL GLNIRA10R A PowLR CIRCUlf BRLAKIR PANtt i DIESEL 119 20 i EGCP-411 DIL$1 L GI N1 RATOR II loWLR CIRCUlf DREAk[R PANT L j DIESEL 119 -20 l lIVAC 19 HVAC CONTROL CADINrf 19 i DIESEL 119 20 llVAC 20 HVAC CONT ROL CADINET 20 l DIESEL 119 ~ 20 RCCP.I 1 PRlisuRI7t R litATOR SCA CONTROL PANEL i INTER 119 20 RCTR1 1 RCP-lC T RANsrORMER CAlHNET l INTER 119 20 RCTR 2 l RCP-ID 1 RAN580RMI R CABINLT I IN1ER 119 ~ 2J RCTR 4 i RCP-lh TR AN5l0RMI R CADIN(:1 i INTER 119 20 { DPIP.8A { I NGINil RI D $4f iGUARDS DC TL51 PANEL l CONTROL 108 20 1 DPTP8!! i ENGINLI RLD SAICGU AR!n DC TL$T PANLL i CONTROL 108 ~ 20 hlTCPIA l UNDERVOLTAGE TLST CADINET A CONTROL 108 __ 20~ _ _ i hi1CP lit i UNDI RVOLTAGE TLst CAnlNET B l CONTROL 108 20 PORVIIEhlP 1 toRV & 11 MPI RATURL 5 ATURATION CADINET l CONTROL 108 20 RCPht 3A i kEAC10R uoLANT PUMP lum E R MONITORING CADINt:TA l CONTROL 108 20 RCPht 3D i REActon COOLANT PUMP foWtk McNrTORING CABINIT H j CONTROL 108 20 RSA } RI M010 5IIVil0% N RLLAY CADINIT A j CONTROL 108 20 RSA1 i RI MOTE SHUTDOWN RLLAY CADINt:T 4.l CONTROL 108 20 I RSACA l REMOil bilOT(0% N AUAlllARY CABINIT A i CONTROL 108 20 RSACil j RLM010 $HUTIOWN AUXILIARY CADINET e i CONTROL 108 20 RSil 1 Rt Mo'rt SHUllO% N RLLAY CADINET B CONTROL 108 70 l RSil 1 I RLMOTE SHUTDOWN RELAY CABINET n 1 CONTROL 108 20 t RSPA i RI MOTE $ HUT ()OW N PAN [ L. $t CTION A i CONTROL IOS 20 l RSPAll i RrMott sutrIDOWN PANLL SECTION AB l CONTROL 108 20 l RSPil RLMolt SHUTDOW N PANELI $fCTION D l CONTROL 108 20 ESPSC-3A4 I NGINtt RLD $AT EGU ARDS PRL55URC 5WITCll CA81 NET 3A4 l AUXILIARY 095 20 l'SCP 2 i LE^sr0 UNE ANNUNCIATOR 7 AUXILIARY 095 }} 20 IITCP-2 i ilGa l MI RGENCY LOAD 5110DDING HEAT TRACING AUXILIARY 095 IITCP 4 i t in A I MLRGLNC) LOAD MILDDING HLAT TuCING 20 AUXILIARY 095 i 20 l llVAC-16A i HVAC CONTROL CADINET MA 1 AUXILIARY t 095 CLASSORT.XLS - Page 16 0F 18 12/11/1997 , _...... ~ _ - - _ _ _ _ _ _ _. _ _. - _
SSEL Sort:d by CI:ss. CALCULATION $97 0041, Elsvatittt REV.O. t,nd Build *ng ATTACHMENT'S' l Tag Number l Tag Number dewription l Ituilding l Eles. ~ 20 llVAC 16D 1 HVAC CONIROL CABINET 16H I AUXILIARY 0?$ 20 NSP l Nuct LAR $4 Mitt PANtt l AUXILIARY [ 095 20 I.SPSC 3Al I t.NGINil kI D 5AIIGUARDs PRI.sSURE SWITCH CABINIT )Al j INTER 1 093 LSPSC 3A2 i NGINI I FI D sAtt GU ARD$ PRL15URI $ WITCH CADINET JA2 i INTER j 095 20 20 ESPSC 3A) I NGIN(( RLD sAILGUARD5 PkliiURE $% ITCH CAhlNET )4) l INTER ~j 095 20 13PSC 301 INGINilRLD kAILGUARDS PRLi$UR[ $ Wilt 11 CADINET Jul l INTER { 093 20 ESPSC 3112 t NGINLtRt D sAILGUARDs PRLssUnt $wl1CH CAplNrT 382 i INTER j 095 20 ESPSC 3113 iNGINti RI D sAllGUARDs PRtssVRt SWITCH CAltiNt.T Jn) j INTER I 095 21 i C111 1 } CHILLI D WATC R EXPANSION T ANK I CONTROL 181 21 l AllDR 1 A _l_ CON 1ROL COMPT.tx ilVACCOMPRL$sID AIR DRYLR A [ CONTROL 1 164 21 AllDR ill 1 CON 1kOL COMPLLx HVAC COMPRLsSED AIR DRYLR D CONTROL 164 21 SI DM 1 $PLNT I Ut L COOLANT DLMINLRAt Izt R AUXILIARY 119 21 MUT.1 M AKt-UP T ANK AUXILIARY I19 21 MUllE 2A RCP SEAL RETURN COOL!R 3A AUXILIARY 119 21 hiUiiii.211 RCP 50AL RETURN COOLI R 3D AUXILIARY 119 ~ 21 CAT 5A Doric ACID sToRAct A AUXILIARY l 119 21 CAT $U DORIC ACID sTORAGL1 ANK D AUXILIARY 119 21 MUDM.lA MAKL-UP AND PURillCAtl0N ()LMINE RATillk 1 A AUXILIARY 119 ~ 21 MUDM Ill M AKL.UP AND PURif ! CATION DLMINI AAllZt R 10 AUXILIAltY 119 21 SWV 012 AR sWV 12 CON 1ROL AUXILIARY 119 ~ - 21 SrilE l A set:NT f ut L Cootta A AUXILIARY 119 21 SEllE lit SPl.NT IULL COOLER n AUXILIARY 119 ~21 DLllE l A tiils!L Gl.NL RATOR LUBE OIL COOLI R i A DIESEL 119 21 DLilE lin Dit st t GLNLRATok LUnt ott Coott R in DIESEL 119 21 DillE-2A DilsEL GLNI RATOR LUDI: OIL COOlt R 2A DIESEL i19 21 DLilE 21) DIESLL GLNERATOR LUDE OIL CVoll R 28 DIESEL 119 21 DIT 3A l D1011 L GLN! RATOR I UI L OIL DAY T ANK A 1 DIESEL 119 21 j DIT 311 Dltsti. GLNERAT OR FULL OIL DAY T ANK 11 DIESEL 119 21-EGT-2tl LDG D AIR RLCLlYLR :n DIESEL i19 21 EGTlA LDG A AIR RfC[lVik lA DIESEL 119 21 EGT ill Itxa A AIR RfCflVLR in DIESEL 119 21 LGT 2A tDG D AIR RICLIVER 2A DIESEL l19 21 l LIT 2 I MIRULNCY T ELDWATLR T ANK EFW TANK 119 ~ 21 MSV 411 ARI MsYall AIR RLstRYoiR 1 INTER 119 21 MSV 4ti AR2 M5Vall AIK RLsLRV0lR 2 INTER 119 21, 1 MSV 411 AR3 MW.4tl AIR RlMRVOIR 3 INTER 119 21 MSV 412 ARI l MsYat2 AIR RESLRvolk i l INTER 119 21 MSV 412-AR2 l_ MSV 412 AIR RLs!RVOIR 2 l INTER 119 21 MSV 412 AR3 l Msval2 AIR RL$!RVolR 3 i INTER j 119 21 1 MSV-414 ARI l Msv 414 AIR Rest RVoiR I l INTER 119 2! MSV414 AR2 l MsVai4 Ain RLstRVolR 2 i INTER 119 21 I MSV-414 AR3 i Mwai4 AIR RLitRVotR 3 l INTER 119 l INTER 119 ' 21 MSV-413 ARI l MSV.4%) AIR R0stRVOIR I 21 f MSV-413 AR2 [ IN1 ER 119 M Aal) AIR Rtst RVotR 2 21 MSV-413 AR3 MsVal) AIR arstRYotR 3 INTER 119 21 Dill 1 DORAT to WATI R STORAGt T ANK SOUTil BERM 119 ~~ 21 CDT-1 CONot Nssit sTonAGt T ANK j WEST DERM 119 21 SWilE 2 l $W SUPPLY TO PASS $ AMPLE COOL LRs j AUX 1LIARY 108 CLASSORT.XLS = Page 17 OF 18 12/11/1997 ~ -
SSEL Soft;d by Cists. CALCULATION $97 0641, f Elsvation. REV.O. end Building ATTACHMENT 'S' l Tag Number l Tag Number destdption f fluiltLng l Eter. 21 1 DI'l lh Dil M L GLNL RA10R I ULL olL 510RAGL 1 ANK A SOUlll DERhl i 105 i i 105~ 21 DFT ID i Isttil L GLNERATOR TUI L 01L K1ORAGE T ANK B l $0UTil DERh! ll i $W V 152 AR i AIR RLst RYotR iok swV-is: I AUXIL!ARY 100 21 $WV l$1 AR j AIR RLSLRVOIR IOR $H V 131 AUXILIARY l 100 21 WDT 3A RC BLrro t ANK 3A 4 AUXILIARY j 095 21 i CAllL l j PRI.ssUklit R SAMPLE COoLi k i AUXILIARY l 095 21 l CAllE 2A sitAM GLNtRAToR A sAMPtt(OOLIR l AUXILIARY j 095 21 j' CAllE 2D i $1 TAM GLNtRAton a SAMPLE Coott R AUXILIARY j 095 21 i DCllE l A i DtCAY HEAT C1OsLD CYCLE COOLING A i AUXILIARY l 095 21 { WDT 3D i RC ut Lt D TANK 30 AUXILIARY j 095 21 g WDT 3C l RC DLt LD TANK 3C 1 AUXILIARY I 095 21 l DCllE lu j ptCAY Ht AT Clost D CYCt L COOLING s l AUXILIARY l 095 } $WV 354 AR l AIR kLsLRVo!R IOR $% V 334 ) AUXILIARY _l 0?$ 21 21 i SWV 355.AR i A!R RLsLRVOIR FOR 5% V 35) i AUXILIARY 095 21 [ SWV 353 AR { AtR RLsl RVoiR foR hwV 353 l AUXlLIARY 095 21 SWT1 NUCLt An St RVICE Ct ostD CYCLE $ URGE TANK f AUXILIARY 095 21 $ Wile 1 A g NUCL1 Al' $1 RVICL CCC HLAT EACHANGL R JA i AUXILIAkY 095 21 $ File lli NUCtrAl stRYlCL CCC HC AT LXCll ANGER 3n l AUXILIARY 095 21 i $ Wile lC NUCLEAR $['RVIC[ CCC HLAT EXCH ANGlR 3C j AUXILIARY 095 21 i SWilE ID i NUCLL AR si RVICL CCC HEAT LXCll ANGLR 3D i AUXILIARY 095 ~21 l CAllE-6 l PAu *M CAY HtAT sAMPLL CooltR l AUXILIARY 095 21 i DCT I A I DLCAY HLAT CCC sURGL TANK A j AUXILIARY 095 21 DCTIll } DtCd HrAT CCC scRGL TANK e AUXILIARY 095 21 RWSI' I A f CYCLONE hlPARATOR A AUXILIARY 095 21 1 RWSP ill l () clone st PARATOR D AUXILIARY 095 --21 l WDTIA I WASTE G As DLCAY T ANK I A AUXILIARY 095 21 i WDT lu i WA51L gas DICAY T ANK in AUXILIARY 095 21 i WDTlC W AsTL G As Ot CAY T ANK IC AUXILIARY I 095 ~ 21 i CAllE5 PAu RC sAMPLL Coot t R I INTER 095 21 l CAllE Il i Pass RC SAMPLE PRE.COotIR i INTER 095 21 i blUllE lA i (UT-DowN COOLI R 34 ~ f REACTOR 095 21 i h!UllE ID tLT oowN Coot t R 3n j REACTOR 095 ~ 21 j h!UllE lC L1 T Dow N Coot 1 R 1C i REACTOR 095 -21 l W DilE l RIACTOR CootANT DRAIN TANK Cool! R I REACTOR 095 l 21 l WDT5 REACloR Coot ANi t)R AIN T ANA I kEACTOR 09E i 21 i IADRl 'Ns1RUMLNT AIR DRit R I t TURDINE 095 21 1 1AllE 1A INSTRUMtNT AIR AITtR Crx>t l R A j TURDINE 095 21 l 1AllE ID } INTTRt'MLNT AtR ATTER-Coot tR H i TURLINE l 095 _ 2. [ IATIA j IN51RUMLNT AIR RLCEtVI R A l TURDINE 095 21 l IAT lu (NSTRUMENT AIR REC 0tVER n { TURDINE 095 21 i NGT XX At>V n ACKt'P NR RoGEN SUPPLY T ANLS OO) j TURDINE 095 21 s SAllE 1 A STATION AIR COMPRf SSoR AITlR CooLLL A i TURDINE 095 21-l SAllE ID si AttoN Aint COMPRLsson Artt R Coot tR o l TURDINE l 095 + 21 CDilE-4A MUN CONDLNsta A TURBINE j 095 21 l ClellE-4D MAIN CONDLNsLR n j TURDINE l 095 21 l DIDIE lA i DLCAY HtAT RLMoVAL HLAT LXCHANGLR A ~[ AUXILIARY l 015 21 i D1111E 1D } DiCAY llLAT RLMOVAL HLAT!XCll ANGLR n i AUX 1LIARY i 075 CLASSORT.XLS Pags 18 OF 18 12/11/1997 -,. _ _ _ - ~
,- m, i / r%rida DESIGN ANALYSIS / CALCULATION Ro ( ver ks Crystal River Unit 3 DESACPW... Pa08 [ of DCsCUMfMT fL4NT#aCaf"JN NQ h!VISUJ S97 0541 0 T CHHE-1 A 9 hv 4 M gg, gg,,, go, g gp, y,,,,, g,9,,,,,9
r,, )U DESIGN ANALYSIS / CALCULATION ' _ bd_ I.'".l Crystal River Unit 3 Casa < Hed. :- Page,,) of 5 t@CWINT,D(N1W 4CATCN f40 AtV@DN S97 0541 O Ryaluation cf-CHHE-1A This is a short calculation to confirm the adequacy of the equipment anchorage. Raferences: 1. Vendor drawing 71-760161-2, Rev. 1 2.- FPC drawing 405-044 Rev. 6 3. Cr-3 Environmental and Seismic Qualification Program Manual (ESQPM), Rev. 9 4. Generic Implementation Procedure (GIP), Rev. 2 Per Reference 1, the chiller weighs 12.375 pounds Per Reference 3, the peak horizontal floor response for the Control Complex Elevation 164, at 5% damping is 0.879 Also' per Reference 3, the vertical acceleration is 2/3 horizontal acceleration. Therefore 2/3(0.87 ) = 0.58g 9 Tha estimated CG for this equipment is assumed to 68.5" above the floor. This is a conservative assumption based on inspection of Reference 1. This is the sum of dimensions "U" and "V" from the drawing. Siaximum Horizontal load 12.375 lb. (0.87 ) = 10,766 lb. 9 Maximum Vertical Uplift = 12.375 lb. (0.58g) = 7,178 lb. Maximum Overturning Moment is assumed to be about axial axis of chiller ' Moment = (10,766 lb. (68.5") ) / (4 bolts)(43.75") = 4.214 lb./ bolt This calculation uses 21.875" from centerline of chiller out to bolts. This dimension is based on inspection of Drawing 405-044 and confirmed by field inspection. Also, neglect deadweight and upl.ft effects (conservative) Maximum Shear = 10,766 lb. / (8 bolts) = 1,346 lb./ bolt Inspection of Reference 2 shows the chiller is anchored with eight (8) 11/4" di$ur.:ter through bolts. The bolts pass through the 7" raised pad the chiller is sitting on, and the 8" thick floor slab. The anchors have a 3/4" backing plate on the underside of the fl oor. For the 1 1/4" diameter bolts, the cross-sectional area = 1.25' (n) / 4 - 1.23 in', The bolt material cannot be readily determined, use the conservative assumption that Fy = 36,000 psi. - Use a tensile allowable of 0.6 (36,000 psi)(1.33) = 28,726 psi (this is more conservative that CIP). Therefore, tensile capacity of bolt is 28,726 psi (1.23 in') = 35,335 lb. >> 4,214 lb,/ bolt i Uso a shear allowable of 0.4 (36,000 psi)(1.33)(2/3) = 12,768 psi Therefore, shear capacity of bolt is (12,768 psi)(1.23 in') = 15,705 lb. >> 1,346 lb./ bolt Concrete shear is acceptable by inspection. The floor slab has #5 bottom bars at 9" both directions. The raised pads are doweled into the base slab.- The total thickness of the concrete under the chiller is 15". Therefore, conclude slab is acceptable by inspection. a., m an m.. a-a m m.,e i
FLORIDA POWER CORPORATION CRYSTAL RIVER UNIT 3 DOCKET NUMBER 50-302/ LICENSE NUMBER DPR-72 ATTACllMENT C Calculation S-96-0013 Rev,1, " Qualification of Tanks per U.S.I. A-46" ATTACHMENT D Calculation S97-0542, Rey, 0, "CR3 Structural Margin Evaluation (Study)" ATTACIIMENT E Screening Evaluation Work Sheets (SEWS) for RCPM-3A and RCPM-3B ATTACHMENT F Design Basis Tank Calculations for: The Pressurizer Quench Tank (Tag Number WDT-5) Reactor Coolant Bleed Tanks (Tag Numbers WDT-3A, 3B, 3C) Dedicated Emergency Feedwater Tank (Tag Number EFT-2) ATTACIIMENT G Letter on Grounding Resistor ATTACHMENT H Memo on " Resolution of Questions Regarding Possible Mis-classification SSEL Equipment" ATTACHMENT I Discussion on Specific Cabinet Internals and Weight Concerns ATTACHMENT J Information Copies of Referenced Drawings 4
l A'ITACHMENT C to 3F1297-24 FLORIDA POWER CORPORATION CRYSTAL RIVER UNIT 3 DOCKET NUMBER 50-302/ LICENSE NUMBER DPR-72 CALCULATION S-96-0013, REV. I " QUALIFICATION OF TANKS PER U.S.I. A-46" l 4 -e, -r -.,v. ,,..----e-
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