ML20140B375
| ML20140B375 | |
| Person / Time | |
|---|---|
| Site: | Fermi |
| Issue date: | 09/04/1981 |
| From: | Colbert W DETROIT EDISON CO. |
| To: | Kintner L Office of Nuclear Reactor Regulation |
| References | |
| EF2-54-625, NUDOCS 8109140164 | |
| Download: ML20140B375 (167) | |
Text
{{#Wiki_filter:.- 9 l -V-e 7 v. s e 1 + Edison =000 Second Avenuer-2 4 2 September 4, 1981-i EF2 - 54,625- \\ di h ye[g y\\ Mr. L. L. Kintner fN g ') ~ U.S. Nuclear Regulatory Commission l'] 2 Office of Nuclear Reactor Regulation O [8g7A i Division of Licensing ,d Washington, DC 20555 ys
Reference:
Enrico Fermi Atomic Power Plant - Unit 2 { NRC Docket No. 50-341 4
Subject:
Seismic Qualification Review Team (SORT) Audit Response to Open Items 4 l
Dear Mr. Kintner:
l l As stated in our letter (EF2-54,390) of August 31, 1981, we attach-j herewith, additional information in connection with Open Item #3a. We have prepared ground response spectra for 5% and 7% structural (site) damping for 5% and 7% (equipment)' damping for N-S direction, and E-W i direction reproduced from synthetic time histories - Figures 1 to 4. An overlay of ground responst spectra for 5% and 7% structural (site) j damping shows an excel;ent match - See Figures 5 & 6. 1 We have also prepared oserlays of floor cesponse spectra for 5% and 7% structural damping. Both sets of' spectra have been dcveloped for 5% equipment damping. These are presented as Attachment I. 1 An inspection of the overlays shows that the 5% structurally damped ( spectra pretty well match the 7% structurally damped spectra both in shape and in acceleration magnitudes. The 5% structurally damped curves do show a slightly higher response in the high frequency range. Con-sidering the state of the art developments in this field, the compari-son shows no significant differences. l l Further, an independent analysis was made to project the responso due to 5% structural damping from the 7% structurally damped spectra values as the reference data using a rational analytical approach. The spectra development is presented in Attachment II. This method is somewhat more j j - conservative than the use of the actual floor response spectra. It shows that the 5% structural damped spectra are at most 20% larger than the 7% l structural damped spectra, with generally no significant' increase over 0 /8 8 l most of the frequency range. S / SO ( 0109140164 810904 'PDR ADOCK 05000341 A PDR
..e 7 Mr. L. L. Kintner September 4, 1981 - EF2-54,625 Page 2 The results, as presented in Attachment III, show that no additional requalification of equipment is required. Three items: RPV Top Guide, HVAC Dampers and the Plenum for the multizone unit have calculated stresses in the range of up to 20% over yield. This overstress cal-culation does not consider the positive effects of higher equipment damping and mobilization of ductility that would accompany such stresses. Yours very truly, /Y ll W. F. Colbert Technical Director Enrico Fermi 2 WFC/YNA/jlj Attachments cc: B. Little Dr. Morris Reich Department of Nuclear Energ',' Building 129 Brookhaven National Laboratory Upton, NY 11973 l
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1 cRtc NB. 33E/sz 4. 77. Danc stTE 3rECTRR SRRGENT 4 LUNDY PR8 JECT TERN!-E REV W O!A'EER3 PROJECT N3. 6139-38 PERM 3 WIDENED BY 107. SN EROH s!DE 28 RUG S1 DANPINC 0.050 224DL rnet TRED'.JENCY IN Cf 3 50.0 20.0 10.0 5.0 Z.0 1.0 0.5 I, ,I f f I*t I f, 1,Qt .f I,_t t I t t t t t,f,f ,t ,f f, t ,t J,,
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CALC N3. 330/CZ 4 77. Can.' 21TC Or:0TKR LUNDY raucci runt-e ncy SARGENT c c:Sti:::.-s rne.scer go. cir.a..sc 'C"" "* ""'" ** *** ** E"C" # C 28 RUG 61 Danr1NG 0.000 224DL rnat rntaucuct In ces 50.0 E0.0 10.0 30 2.0 1.0 03 ' ' t'f r # u U I 1 W [ i.- l ,tc.cW'y 3 i i r M '.LI '.'i i i n-P E hl,*'..~ ~'N2 M'/1 f iis s i ti i -: 1:.o 1s.t - - FROM 50 DMiP. SITE SPECTRA I!!PUT 10.0_ FROM 7% DMIP. SITE SPECTRA INPUT --31' ' ~ I l l I d.t.: s s.ct-s.U~ ~ c.e H l 3. t ". 5.E 4.Ct~ , 4.00 3.C0~ ~ !.M ~ 2.00 't.70 x / g
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CRLC H9. 33C/5% f. 7% ORNr ::ITC 3rECTKn S A R C-E N._ 4, ,t_ U N D Y rn3 acct rcnni-t acy i CG * :r.'.3 TROJECT N3. 5133 *3S e PEAK 3 WICENED BY 10% eM ERCH 31DE 28 RUG 81 DANTING 0.050 224DL ract TREQUENCY IN CP3 50.0 10.3 ' 10.0 5.0 f.0 1.0 0.3 _f __f*g, i ..f f f f f f f f f f f f f f_1_j f fff f f f f f f f 1 f, ...0 ) _ _,f f I f 8 '_ i,9fmi siisiiii iii .iii i vri in g _.. _ r_,ii., i i ~ 15.r ~ 1s.c FROM 5% DMIP. SITE SPECTRA INPUT 2 10 4 10.c FROM 7% DMIP. SITE SPECTRA INPUT 3.0: . 03-O ~ ~ G.C; g,c d. g,go 4*L 4.00 ~ 3,g ~ "" 3.0: 2 2 f to z.c ~ + e e,- e x g // \\ = ~
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1101'I'liR ANI).\\M>Uua i1.3 Et.G:t.E t hs /* ATTACTIMENT II EF2 - 54,265 ~ ENRICO FER'M ATOMIC PO'1ER PLANT UNIT 2 Constructed Equipment Responso Spectra for 5% and 7~ Structural Camping and 2% Equipment Damping 4 Prepared for: Detroit Edison Company 2000 Second Avenue Detroit, Michigan 48226 Prepared by: llopper and Associates 1840 S. Elena Avenue, Suite 208 Redondo Beach, CA 90277 l l k s August 27, 1931 9 v.
HOPPER AND AS50 MATES ENGtNE E ES
1.0 INTRODUCTION
Equipment design spectra exist for the Fermi Design project based on the' reassess-ment earthquake evaluation. These spectra have been generated assuming the structural damping to be 7%. This structural damping was rationally selected based upon anticipated structural response level to the newly postulated earthquake excitation. Subsequently, it was observed that anticipated structural response levels were not achieved and the justification for such high structural damping was questionabla. ho concern exists relative to the structural adequacy of the critical Fermi building structures. Hv: ver, internally housed equipment may experience load:ng more severe than that indicated by the existing internal equipment spectra generated from 7% structural damping phenomena. To eliminate such concern, it was considered necessary to dctermine the influence of 5% structural damping on the existing internal equipment spectra generated for 7% structural damping. The normal approach to this problem would be to simply reanalize the existing structure subjected to a given time history with 5% as opposed to 7% damping and generate the attendant internal equipment response spectra. However, basic problems apparently exists in synthisizing one time history that will appropriately envelope both 5% and 7% ground motion input response spectra. Independent of any time history information we have developed internal equipment respons: spectra assuming 5% structural damping for conparison with spectra existing for 7% structural damping. This was accomplished by assuming that the response of the building structure could be approximated by a summation of damped sinusoidal accel. ration tire histories corresponding in frequencies to the primary structural response frequencies of the building structure. The following sections of this report address the methodology by which comparative spectra were developed, a justification for the synthesization technique empioyed, a development of response phenomena to decaying sinusoid excitation, details of the technique employed for equipment spectra generation and a summary of results followed by representative equipment response spectra plots for representative building locations.
IlOPPEl(.\\ND ASSWINTES E NGWE ERS 2.0 METHODOLOGY 2.1 Existing 7% structural damping equipment spectra were reproduced for detailed evaluation purposes. Concurrently, structural response phencmena ar the primary Fermi safety related structures were excerpted from references I and 2. This information was used to establish the baseline upon which spectral synthesi:ation activities were undertaken. 2.2 ' The response of internal equipment to decaying sinusoid excitation was established as a function of the sinusoidal decay ratio which is assumed as representative of the extent structural damping mobilized. 2.3 Spectra were synthesized for 7s sinusoidal damping assuning the total response at a given frequency could be represented by a su cation of decaying sinusoidal excitations at frequencies equivalent to those associated with the primary structural response mo?es. Amplification factors for each of the decaying sinusoides were computed in such a way that the 7L excitation response spectra would be equivalent to the synthesized spectra at all predominant builoing response fre-quencies. Resulting amplification factors were then used to generate spectral acceleration values intermediate to structural response frequencies. 2.4 Five percent sper.tra were s:qthesized with equivalent sumation factors and amplification ratios employed for the 7~ response situation. Higher basic arplifi-cation responte stjDS associated with less severe sinusoidal decay caused amplifi-cation to occur in the 5% spectra relative to the 7% spectra in zones in proximity to primary building response frequencies. 2.5 Comparative response spectra were plottec.,er critical building locations to compare 5% structural dar. ping equipment response spectra with 7% damped structural equipment response spectra. These ccmparative spectra were then used to establish maximum amplification ratios anticipated at various structural locations for equipment acceptability verification purposes. 3.0 SYNTHESIZATION TECHNIQUE JUSTIFICATION 3.1 The damped sinusoidal response suonation approach was selected for internal equipment spectra generations purposes for several reasons. First, censistent and unquestionable basic timc history ground metion time histories are unavailable
_ - = _. HOPPElt AN!) ASSOCIATE 5 E AG*E E RS at this tire. Second, we believe this damped sinusoidal model combination approach will yield amplificatio,n ratios between the 5'; and 7'; structural damping spectra that are definitely conservative. Furthermore, this first approximation simplified approach avoids dangers associated with over sophistication whereby analytical complexities may obscure true structural response characteristics and introduce undetectable unrealistic compu-tational phenomena. 3.2 Dur spectral synthesization technique herein basically corresponds to an approach presented by J. M. Biggs and J. M. Rosette entitled " Seismic Analysis of Equipment Mounted on a Massive Structure". This approach was documented in a three day ser.inar at MIT on Seismic Design for Nuclear Power Plants held in the Spring of 1969. Although the accuracy of this approach is nct precise our experience has shown it to yield conservative internal equipment response spectra and the simplicity of the technique seems appropriate for our specific application. The basic approach is su:marized following: The acceleration for a given spectral frequency may be calculat.1 as 1/2 n" i 2-n' [ l' A"een jl Aem = { (Aemn)2 sn sne [ lsn 4 L ( sne P P d Thefirstsummaticnincludesthosemodesforwhichf9 < l.2h = t c I the numerator of the second term includes the remaining modes while the denomiater includes all modes. Aemn = Asne A where Asne = ..n l'sn +sne and Ae n amped sinusoid amplificatien = l e Ae$n= A ^* '~ 3 A g whe re Aems = f.m dueAdirect elround motion
HOPPER.tND ASSUMATES LNGINE ens and ^ = Ground motion amplification .Ae also Aon = Ground acceleration at period Tsn Isn=Modenparticipationfactor $sne = Mode n eigenvector In our spectra simulation approach we neglect ground motion factors, combine the modal input by direct sum, and compute necessary participation factors to r.atch the baseline spectra. 3.3 The approach taken shouTd also yield conservative spectral amplification ratios between various structural damping input excitation. A major criticism of the technique for general analytical purposes rests upon the argument that modal amplifi-cation factors obtained thereby due not account for lengthy earthquake excitations in which total responses may remain at a constant level for several excitation cycles prior to there ultimate damped sinusoidal characteristic response. This phenomena would yield higher amplification ratios for a given piece of equipment but would make the ratio of amplification factors between the various structural damping ratios diminish. This makes results obtained employing this technique conservative. l 3.4The unproven nature of more advanced techniques for internal equip:nent spectra generation coupled with our ability to check the adequacy of this approach l relative to a known 7" response spectrum makes it justifiable to employ the simple approach for spectral synthesization comparative purposes. 4.0 RESPONSE TO DECAYING SINUSOID EXCITATION j 4.1 The decaying sinusoid used as a representation of the building modal response was represented by the following acceleration time history. - f' g 1 - (.z r i a(t) Sin "d t *
- P
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n n Y *"n-1+hi-1+ n-? n n n and y )-1 y*~((I+"2g26+2o 2/ n h2 2/ y -1 + hy,,) + 7 y -1 an + o n n + 20{ h -1 + E -1 n n The time history output for each frequency is searched for the maximum value of y. The associated absolute acceleration amplification or spectral acceleration 2 amplification is then computed as a y. 4.3 Spectral amplification summaries associated with the above calculation sequence are shown on the following figure. The maximum ratio between (' =.07 and (' =.05 is 1.208. This represents a maximum 21% increase in peak acceleration going from {' =.07 to (' =.05.
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IloPPER.\\xn AS 4:1.\\TES ENG4NEf AS 5.0 EQUIPMENT SPECTRA GENERATION 5.1 It is assumed that a given response spectrum may be constructed from a m summation of accelerations associated with the responce of dgped sinusoids at primary structural response frequencies. [A] (X) = (b) where {A] = Influence matrix (X) = Modal amplification vector (b) = Spectrum accelerations Amn corresponds to the sinusoidal amplification at frequency n associated with maximum amplification at frequency m. An expanded influence matrix [C] may similiarly be constructed to encompess as many n frequencies as desired with a constant number m frequencies dependent of significant structural response modes. [C](X)=(d) where (d) would encompass spectrum accelerations at as nany frequencies as desired. In our situation, we have selected (b) to match a given 7% spectrum. (X) was then computed to give the relative amplification for each mode. [C] (X) = (d) a full spectrum matching the existing 7% curve. [C] is then modified for 5% structural damping and (d) is recomputed yielding a full spectrum simulating the 5% curve to be anticipated from equivalent ground excitation. 5.2 Building analysis data was taken from SL-2682 and SL-3147 and is su=rarized in the following tabular format:
HOPI'ER AND ASS ('CIATES E NGiN E E R S t CR!ilCAL BUILDING MODES PERIO3S N.S. Reactor / Auxiliary Building 7 .2221,.2011,.1994,.1877, .1845,.1548, and.0662 E.W. Reactor / Auxiliary Building 6 .2219,.2011,.1994,.1877, .1845 and.0634 Vert. Reactor / Auxiliary Building 3 .0814, 10656 and.0587 Horizontal RHR Complex 5 .1283,.1034,.0917, .0552 and.0419 Vertical RHR Complex 6 .0655,.0549,.04S0, .0440,.0402 and.0321 5.3 Seven 55 structural damping excitation spectra were develeped associated with 4 critical locations and directions in each of the category 1 structures delineated in the preceeding section of this report. Based on those results and the consistency of the effect on spectral shape considerations, other representative spectra have been constructed and are included with this report. t 6.0
SUMMARY
OF RESULTS Evaluation of comparative equipment response spectra for 7; structural dar. ping and 5% structural damping reveals the maximum amplification the 50 to the 7% curves to be 21%. This maximum amplification varies as a function of building and location and at its minimum range equals 13%. The observed amplification is apparent only in regions adjacent to significant structural response frequencies and is nonexistent at both the high and low frequency ends of the spe:tra. Enclosed following are references and an assembly of representative internal equipment response spectra for the Fermi facilities. The 7% building damping excitstion spectra c.. respond identically to tnose in the reassessment analysis and the 5% building damping excitation spect a correspond to those generated by the synthesization technique described in this report. l m =wswum*,. _c. _ _ _.m.ar e _ _ m e e== e - _e--
HOPPER AND ASSOCIATES ENGIN EE AS REFEPENCES 1. Seismic Analysis of the Reactor Auxiliary Building Complex Enrico Fermi Atom.ic Power Plant Unit 2, Report SL-2682, Sargent and Lundy Engineers, September 27, 1974. 2. Seismic Analysis of RHR Complex Enrico Fermi Atomic Power Plant Unit 2 Report SL-3147, Sargent and Lundy Engineers, July 15, 1980. 3. Seismic Re-Analysis for 7% Damping Site Spectra Reactor - Auxiliary Building, Report SDD-DECO-003, Sargent and Lundy Engineers, April 18, 1981. 4. Seismic Re-analysis of RHR Complex, Report SDD-DECO-001, Sargent and Lundy Engineers, April 18, 1981. 1 w. I O
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]!O1'181:11.\\NI) ASST iCI.\\T!5 tsGN!!' ATTI.Cli!*E!;T III EF2 - 54,625 ENRICO TEP.MI ATC':IC PU,lER PLA'; UNIT 2 Re-eveluction of Ecuic.ent Ouslificd to the 71 Structural Da:pir.g Renssessr.cnt Earthauate when Subjected to a 5'4 Structurci Drpir.g P,eassess-cent Er.rthque.Le Prepared for: Detroit Edisco Co par.y 2000 Second Avcnue Detroit, Michigan 4C226 Prepared by: Hopper and Associates 1840 S. Elena Avenue, Suite 208 Redondo Beach, CA 90277 August 27, 1951 n
HOPPER AND ASSOCIATES EN7.NEta$ i a
1.0 INTRODUCTION
An exhaustive seismic reassessment evaluation was undertaken by the Detroit Edison Fermi Design Team to evaluate the acceptability of critical equipnent relative to a newly postulated carthquake larger than that established as the design l basis for the Fermi site. In this reassessment, it was assumed that structural and mechanical items would be experiencing cycles of relatively large stress re-versals and appropriate famping values were selected for analytical purposes based t i upon this assunption. In this regard it was assumed that the primary structures would respond at the 7% damping level, t Upon completion of the seismic reassessr.ent activities and evaluation of the structural analysis results it was observed that anticipated stress levels were not achieved and the structural response was shown to be quite acceptable relative to the reassessment earthquake input excitation. Howevt, internal equiprent design spectra generated fror the afore described building analysis response data are not necessarily conservative in nature. If l the building responds with a lower effective damping then it would be anticipated l that internal equipment response spectra would be greater than those associated with higher values of structural damping. For this reason, equipmmt response i i spectra were also generated assuming that the structure would respond at the 5'; i l damping level. These 5% structural darping spectra were plotted along with the 7% structural damping spectra for comparative purposes. At the completion of the SQRT audit the Nuclear Regulatory % 'sion requested that Detroit Edison provide to them a sun-ary of the results of the equipment seismic qualification reassessnent based on the use of E% structural damping instead of 77. structural dt.mpir.g. Additional items identified as critical in this evaluation were to be sumari:ed in a table similar to tabic 5.4-1 existing in the current seismic reassessr.ent report for components requiring requalification l or replacement. In addition, Edison was requested to provide the Comission with l floor response spectra associated with 5% structural damping. 4 l ? -,, + - +, .. n
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l l HOPPElt AND ASM CI ATES t u ottas 1 I l This report addresses the re-evaluation of equipmen previously qualified to a 75 j structural da. ping reassessment carthquake when now subjected to a 55 structural f l damping reassessment earthquake. This report is structared to described the methodology by which this re-evaluation i was undertaken and to present a su=ary of the results Obtained from the evaluation. Detailed evaluation information is included as a part of this report. 3 The detailed evaluation is su rarized on the equipment ev31uation su : ary sheets l taken from the original supplementary seismic evaluation report EF2-53332 dated July 15,1981. i s 2.0 METHODOLOGY 1 l 2.1 Five percent structural damping response spectra were generated by an approxi-mate method and are included as part of the reference I report. These spectra indicate a maximum amplification in the rescnate frequency region of 21:. over the 70 values. This raximum resonate ar.plification changes as a function of building location and ranges to a low peak value of 13:'. Amplification is nc. observed in regions of the spectra away from building resonate frequencies. Both' the zero period acceleraticrs and the low frequency accelerations duplicate the 7% curves. l 2.2 Existing reassessment results are included as a part of reference 2. This aport thus establishes a baseline of equipment adequacy for the 7% structural j da r: ping input excitation. As an integ al part of the calculation sumary tabu-j lation, safety margins existing relative to the 7% excitation have been established l for r;ost items. Safety margins existing for other items exist in calculation form i in earlier revisions of the reference 2 report. i l 2.3 The evaluation approach for 50 structural damping input excitation was straight forward. Results of this evaluation have been included on a copy of the t 7% damping damping equipment su mary report in existence and are inc.uded as a l part of this basic report. All items with a safety margin greater than 21t were imediately considered te be acceptable relative to the 5% earthquake excitation input. The actual safety i
HOPPER Axn.iss(K1: s ENGNEC% margin for these items right be larger in light of the fact tnat the 211 amplifi-cation occurs only in narrow frequency regions en the design spectra but need for further refinerent seems unnecessary at this time. If the safety margin for a given item of equipment was less thar 21S than the spectra for the actual equipment location were evaluated to determine if a lower peak amplification value would be in order. If so, the item was considered acceptable. If not, further investigation ensued considering the actual item frequency response and the Dortion of the total stress assignable to seismic excitation phencmena. Anticipated maximun stress levels have been deternined for all critical equipment items. These stress levels have been compared with yield point stresses for ultimate ac:eptability justificaticn purposes. 4 2.4 Ductility was established as allowable in considera;ien of the evaluatien of any Fermi equipment items. The limited pieces of equiprent postulated to exceed yield point stress limits have been evaluatec re!ative to an artificial stress bound established 20:; above the yield point limit to correspend to an arbitrary but smail ar.ount of allcwable ductile response in the inelastic regi n during the reassessment earthquake excitation. Equiprent itens that may exhibit dectility phenomena have been specifically delineated on the detailed evaluation sheets with this report. 3.0 SUM. MARY OF RESULTS The detailed evaluation of the Fermi Seismic Reassessment items to 5'.: rather than 7% structural damping identified no additional items requiring re-evaluation or replacerent. With the exception of those items identified as requiring further evaluatita for 71 structural excitation and three items identified v.ith a potential ine17-tic response, all Fermi reassessment equipment items remain below yield point stress levels when subjected to a 5: structural damping excitation. The three items ider.tified as having a potential for inelastic response due to the higher reassessment earthquake are the P.PV top guide, HVAC PD 300 fire damper, and the Plenum for HVAC multi-zone unit. A reference tabulation and our detailed evaluation summary information are included as the following items in this report.
llOPPER AND ASSOCIATES t w stta: REFEREriCES 1. Enrico Fermi Atomic Pcwer Plant, Unit 2, Constructed Equipment Response Spectra for 5% and 7% Structural Damping and 2^: Equipment Damping, Hopper and Associates, Aug. 27, 1931 2. Enrico Fermi Atomic Power Plant, Unit 2, Supple entary Seismic Evaluation Report, EF2-53332 Rev. O and Rev. 1, Detroit Edisen Company, July 15, 1951. .. ~.. -....... -..... - - - - - - - - - - - - ~ -.,
TADLE 5.3-1 LOADS FOR CERTAIti RPV AtID ItJTERilAL COMPOtIEt4TS !!orizon ta l Vertical Allowable Top Guide (Shear) 350 31.7 687 kip (1) ~ rore Plate (Shear) 347 361 687 kip (1) S t.obil i ze r (Load) 513 0 2,765,.igi (2) ItPV Support (Moment) 221,000 ti/A 1,152,000 in-kip (1) IIPV Support (Shear) 67') 1,191 2,600 kip (1) C RI) liousing (Moment) '507 ti/A 10,070 in-kip (2) CitD Ilousing (Shear) 14 frgligible 4,400 kip (1) CRD Restraint Beam (Load) 14 ti/A 266 kip (2) Shroud Support (l' omen t) 276,000 o ti/A 347,900 in-kip (2) U Shroud Support (Shear) 1,176_ 1,031 1,434 kip (2) . ~ _ _ =_ n_ Fuel Assembly (Momen t ) 12,024 See Section 32,200 in-kip 5.3.1 Fuel Assembly (Shear) 250 See Section 687 kip 5.3.1 (1) I' rom Ferml 2 mathematical model 761E774, Revision 4 (2) From equipment design spec. or analysis 5 kf*M Yf/* /Wfbl
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i 8 TABLE 5.3-1 (Continued) LOADS FOR CERTAIti RPV Atin It1TEntJAL COMPO?!EtiTS Vertical iforizontal i Load Force Force l Plant Combination (kipn) (kips) J Core Plate LaSalle 1 El 423 471 If Permi 2 !!cw Seismic 361 347 1 LaSalle 1 D2 40.8 332 Top Guide _ Permi 2 tiew Seismic 31.7 Y I.oad Combinations 4 13 L & (U - Delta P) & SRV + SSE El = D2 = tiL & (A - Delta P) + Chg. + SRV - 1 + SSE 'l p rih n:i m n.ra/dy p,am;,,,k fy put4 ns~<ta' h = hs. A ,4/ ac e/ d orlenk19se e2hddi4 rw x;mbu -Atyaes,cy l / ) af c,oc qsr. A v /e P V r % y a e,cy n n ii> u.,,, A o,; w h / cre~,sh?ceAdn -fn ", 7 90 h Go c lo s y n 'j 7 = ? 6 8 - i.i z
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TAfut 5.3-2 I!YDitAUI.!C COrlTPOt. UtilT SEI SM IC Im-t:V Af.tfATIOte St[M Aft,Y, TAfif j 3 j Hothod of original sy s t e:me, Steuetute, Comeposien t (bsa l i f I ca t t ori Re-Evaluation !!nnultas tw.:n i t ion t conclualon and Pomarka t Spectra - t Analysis Margin To t. t Analyuls Report i Spectra 8 Comparison Ha r es in Regior t I <> f I' l g. 6 Safety Itydsaulle Control Unit, X Dier 147-11 5 C16 dated ji,n,4 par 147 t non The new gmsak responso 0 N t t. Cl l tinU I CllD004-11 6 4/18/72 Ts n a - CllD005-ii. son-spectra curvos wete H*$-5 1929 Ve r t i c.n l s osi t.a l, 74*5-5A t.e l
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wo 14 9 as y g test 500t martain, e e thistufore t f*u ItCUm are fi-// Ta;s[y D:n*f/ks freq t[ accep t ats t e ' er' ac/ 9xpCAxNm T. l .t-Aan e.wsaswn o t
m TAfs. % 3-) e Dfilt l'lf*4P Attrif 0ft'i SriSPf f C l'P-f:VAf.t:AT f et' EN.* IIA.E[. T.NI'.E tiethod of Orlqinal sy st ene, Structure, temponent Quallfjcation Ik wo1 tion Re-tvaluation Results 3 conclusten and Pemarks t 5:ie' c t r a Analysin P'angin Test Analysets !!epos t I Spectra I Corng a r l son Ha rati n Ptport 8 of r i es. 8 Safety pttrt Pn4: A ncluir fiol t a X 'd t non .15 9 S& 1. 1415% 1/A The Anchor holt wtrennem 3 ' :*s ign borr. report WW ware recalc ilat e t by r elcu- .in 9 Shu.DCCo on applying the new site-ation vart. -nn) y lcl.1
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4 Tnfl e.e: 3.3-3D ItCIC l'UMt* A?4CllOft itO f.TS S F:I SM !(* M:- f:V AI.UAT I OP8 StJWt A tt y T A f tl.t: _ ^ Method of Orjginal ry st (m. Structure, Component QualltAcation Fe-Ev.sluation Results Desca let lose Conclusion anel Pemar k s t Spe:ctra 1 Analysis Parqin Test Asialysis Report i Spectra i com>.inison, H.seqin hepost I of rig. I Safety 5 HCIC l'umgs anchor bol t s X Edison .15 C S s. 1. 609% ti/A The anchor bolt stressos Design horiz. rc3=sr t T.T71P s ecalculateel tJy sure caleu- .10 C S oti-ut'Co us ap3.lyi ng t he new atte-1.stion vos t. -001 yield specific s oimmte loads, t K:- 3 f.9 figures thn eq u i gw.c si t siozzlu loseis 4 ltem 2 3 from the a t t aclie.1 pi ping. C-Il . inst the eq is t g m.cu t.lo. nil / [ / wetyht t o. Is. Tleu shnar L85 $ y* gh[f[f/A9 /fgg/ 8/* -[";,,8fff/ d "'I ten 41un atreasea we:e I w u c.smt,1ned an.) showei to be
- f. (.n-cw/on
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s /.... m TAhe.E 5.3-4 ItCIC Tff fttt f MP. ANCff0R T108.TS SE! P'HJRFY? t^L""' Sttp*ptany Thnt.C Method of Orlylnal System, St s uc t u r e, Crseget.en t Qualifleation Pe-Evd14:atfon l'e sul t e D. weis>tlon Concluslon and itemarks t Spectra t Analysta Pargin Test Analysta iteg*or t I Spectra 8 Comparison f ts t e:I n ficport I of rio. I Safety PC it: Tuttelne ancient toits X t'dinnn
- 1. 5 et If or t S & 1.
25.6% N/A Tise new stresses were f i le Pro. .14 9 resort conservatively estimated l>C-369 vort. !; Do-tirco by nultiplying the oil-ttem 2 -001 ginal stremacg t>y the Pl<r 's Insgent accelaratIon jn-3 crease comparing all i C-11 three directions. These / new strennem are below the new a l l ow al.I n valuen g gj7 n', Q 2.7 / j%d/~!OfM ff9N lN' C?,G itnl,i ',"l"tl R 68 ,j nite-npecifle eartheguake. GI] W /.G'G;PI?Q#1 /H Q /M&ffy s O O e e I
.~ Tant. 5.1-9 ITCIC ItrMP SttcTinn STnAINER St I!;H!c pf*-f:VAI.tlAT10P8 rdtyttAPY, TAf t r Method of Original Sy s t e.m, Structure. Cteponent Quelltjcation Re-Evaluntion Penults ti.scription Conclusion and fremar n a 1 Spectra Analynis Maroln Tent Analynin Tre por t i Spectra I Comparts.on Marnin Hepor t. I of I' i ci. I Safety PCic Pump suction strainers X Edinon 5 g hort. S & t. H/A l W/A The new site-speelfte gg,33go) File tro. 1 9 vert. Deport p t e, 3 g5;ntgiol3 PI-2416 S Ofh f1ECO earthquake accelerationn are lean nevere than the -003 acteleration Inn d i n<g g t h at. I' l q ' n. were unet in the m iginni 3 gni cale qua li f icat arin s C-Il therefore, thin b3utraent in r e< pin i l f l eil. ' lyf'/ ?$s4&gS:1 [dQ l# Y S ue,;-%, seczykfo%. 7-es earyk is - n =epy G - 47/r A /oa ai~,;.vfy?c.v%.y d e ;nigh 5v m n e h i
A w TAfil.!!
- s. 3-6 Itllit SEftVICit WATT:It St:Istlic fit -l: val.ttATIOt' 1
I SUFttAllif TAft!.t M.thod of Original System. Ss r uc t ita t:, Comptenent Quelliicatson lic-l'va l ua t J on Results Desesjetson Conclu s f ore a nd itema t tt a i Spectra L' Adalysis Pargin Test Analyals Report f Spectra I Comparison Haroin Report 8 of I' i q. I Sa f as ty totn couting Towns X Marley Co. S & l. lit Ileams were foun<1 to lae l'.gu a p. No. E l l 5te ll0 01 A, d a t oil EMt)- LIT 7NY"* f lenitale and t lin resul-ti, 2A, is 2-8-74 029950 un tant oneceloration l es t or nadt.s t eov e Z l' A. The pigeing I4sc.n l i on lettit Eluvation 617 3& !. I oails was tourut to tse clone EMD-to rigid. I'l l ! s t ra s seu ' 0117e5 are very low. I:l lmi s ~ .stor stresneu are vesy low. t'l l t actaincts & vi u l l se i n.s t o r r e t.a l n e r :s y/ 'I9 [,./ / Ysir/e'4 43 97.% wy bdar 1 ( a.. l o..ne.ncan n y a.e / tornado loails (li t yte c t ,/ f. r,. / ioad,i. /g / O h 4.N[dM /.b /n I 8 Streunce on the follow-Ing niettia n ica l equ i pmest, a nil p.i s t as ae Hotor Support h a antin As si l'i pe Support Anclust Itul t s 1: nib ueleme n t Tornale loads are go-verrknq lo sd as. S t t ** m a re a t u v*' t ra i n a l lowata le s. litt M Se r v i r er W.s t e r X HeDona t el S & l. g St re.ssue a re teolow l I* imp.snd Motor E.gul p. No. ting. EMD-y e r I. ling I l m i t es. Water Ell 5tCOulA. C& f) Analysim 029950 Imip an.1 => tor qua l i f t em t lasca t i ori ettl H dented to new s csponsiu spectea, a:l ev.s t lun 5 pr. ' 2-4-74 r:ou l.la l tump loc. l al.it nJ l 9-21-75 l (motos) l'un 8 l... 9o Inauu.l oes yletl. fr.1.
TAnf.E 3.3-7 til ESCL CEM".ftATott COMPONENT *t SEISM IC fit-l' VAT.ltAT IoM 5"r"^"L T^ns;r Net 1*od of Original syr t t e.. Structure. Comsnment Onatification ri.: Se r i g t t on Pe-Evaluatlon Pesults Conclus!on an<1 Pemarks t spectra t Analysla Margin Test Analysis Report I spectra I Coesorison Hanoin Report I of Fiq. 8 Safety tilcael Generat, X Colt inel. S a t. Fmri-Sit
- Streance are well withlh sk l.1 A no = tit y Report 021150 a l lowa tsl e s. Sk t.1 a g gern.
rqii l p, no, tilnn150nt-4 .l a t est tily epiall f les to new t.oc.e t t on Pit ti 4-4-75 rearwinae spectra. Elevatlon 590' f: lev.at i nn 590* S L t. THD-003651 Iteat Enchan. gen X Colt i nel. 1&L EHf>- 71001 *' The e<pa l pmen t equ a l l f l e g Stack Assemtsly Hngert 021950 to new reaponge apectra. 2n E. pi i p. No, n10015001-4 ela t c<l I Stregnes very low. 1.ocation ptt ti 4-4-75 m t' lev.etinn 510' SLt. E Mi> - 001659 '/ / }q - fy/ Fw}7/r frq/*Y 'GQ 8 r gpq:aN.cvn f0(? GPy$'/qcy;'N -7 y, '
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SI'ISMIC Hl:-l'VAI.UATION SteFMAltY TA ft t.E ~ Muthod of Original System. Structuse. Component Qualification tee s.c i i p t i on. Re-Evaluation itesults Conclusion and kemarks t Spectra t Analysis Mangin Test Analysle Re g.or t I spectra i Comparison Nasqin stepo r t I of F l as. I Safety f.uti:n u l l r i t t e r X Colt ind. S & t. 7100%
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- <----- ~ *- -- * = = -~ F T Aul.h.,.3-14 EMEPGENCY 1:QUll'HENT C00f.lfHi WATEft' SF'ISHIC Nt'-t val tlAtlorJ Stf >.HAfs f TA ul.t: Hethod of Original Systta., Structure. Cornponent Qualification ~ LAseeiptton ste-l;va l u a t ion itesults Concluslos,and Iwanarks i 4 Spectra t Analysis tiargin Test Analysis Itegio r t f Spectra l Con.pa r i son Harqin liepos t I of I'! q. 4 Safety 1:f:0# Hake-up L.s e A X Edluon S & t. S & f. D]Id" M N/A The original melumic t i ncl ud i n.) anett.r bolts! File tio. Report fleport strenses wer e sepJe atht! Pts IP4400A001 S20-24 S t.- 2 6 8 2 SinD-DICCo un yiel. out ut the onIginal t'lquaes -003 agua l i f ica t ion, increasdd + H-31 rigures for the siew site-speelfic i ll-32 tl- ) ] uarthgunke, and tii.n adJul H-16 n-32 to the orlytnal nonseal C-16 oper at i n<; a.id.leailwn ! ht 9 l o.a d s. Thu new stseensom vi / are i.alow the siew allow- [ e,j g/[9AT$ 76Jjf df,/ a ts t e vatuous thunerosa, time eq u i pinen t in segtal- / (fle] to the now a l t er-GCc g,r.Qyyj / yt/ ar" W ie "a r t'"lua ka-k. k e f r i i 4 l f i t 1 4 e
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^ .m TAtst 5.3-20 CONTHOt. AIR SCIstt!C Nt -tVAI.ttATIOta St!MMAl*Y TAnly Peethod of Original i synta, Structus, cosaponent Qualification Pe-Evaluation Results 4 tu be s jpt ions Conclusion and pesnarks Spoetra t Analyela P4: q i ri Test Analysis Report 8 Spectra 8 Compa r i more Haroln Repost 8 of Fig. 8 Safety Control Air teocelwer 1 Lilson S k t. S&L N/A N/A The new alte-specific l*l Sil'5002 Au u t Film No. Neport Heport e.o r tlutuake accelea at ions S t.-2 6 8 2 htID-tit:Co-are leen severe than F19utes 00) the acceleration loadtryje D-5 F19ures that wese used in the n-6 u-29 original scia.mic <3u I t ti-15 - 2 9 h-10 catioins thesesoro, t t.t e h-30 C-11 equi ment is re.guantiled. t C-6 C-16 N C7/~[/ 5 b kit (;g $ [ 7 O /-/cyf.3 3* h
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5.3-23 9 SSEt4T R Af. IIVAC DAH1't;ItS seisnic pe-tvni.uATim suy_ttAl Y TAltlE j Nethod of Original Syntca, Structuse, cc n.ponent Quailficatlon Re-Evaluation Results Mes ipt ioes Conclusion and Hemarks Spectra t Analysis Pa s q in Test Aealysis Heport 8 Spectra I Comipas A mun. M. stein Heport 8 of Flas. 8 Safety S&L S&L facport Report SDD-Dt.Co-EJlson S L-26 8 2 00) Pfle No. F l yt_a r em riquses w# PU 300 Fire Dampor X D9-2575 13 - 3 7 tt-17 7% W/A The ort <j!nal seismic. C-19 C-19 1M stresses were sel*asated on out of the original yield qua l l t ic.s t f ori, increamerd {[$r u.ackdrafL t >a mt.o r X 59-2175 B-17 U-37 ' gi n for the site-specitle (P.scific Air Psoducts N/A SSE, and added to the C-19 C-19 b anest u, Coare. :ny l poemat opeanting loads t on ort-lin cases where utscenes ut ginal wene low, the combined 04 allowa-nus se.e l ope s.s t i ng a n.1 ble sulamic mtsemmen were A i r Da*=per ., 3 i nes e.n ood t> y thu worst X 89-2175 B-37 n-37 tot 14 N/A .necclesation r a t last. (Pacific Air Products Co*panyt C-19 C-19 '#W t'a l cu t.i t e.t s t r e s s.e n are on ort-. below ttee new a l l ow.s t,l e vi n.n l v.a l ue n t thesefose the on l l ow.a-e* gia l eme n t is s oqu.a l t f l ed ble to tt u mite-specitte sse:. Plemitslo nome X 89-2175 n-37 p-37 lanya -d4 n/A C-19 C-19 -.. Ig h ( k e D \\t? I I *"'4 l M 'fL ~ A_& )Acosjklg-u saAVy nn.,, ym - _6 e y d 'c, A k s. 8 mm6n oa
r. r" olik Inuet h 1;Sht.NTI At. IIVAC DAMlag:RS SE t hMIC Pf:-LVA!.t'ATint* St frattA IO TAlif.0: Nethod of On-iqinal Ey s t es. 5 t a uct ut e,. Cosrponerit Qualliic st lose he-Evaluation Resiu t t s IMse s i p". i ore Conclusion and Itcenar ks t Socctra t Analysis P.s e q iri Test Ariel ys i s Repost i Spectra f Con.parison N.argin lieepor t i of rig. I S.a f.: t y riso is.sn. pes s.i.ed Ai r Cont rol X 09-2131 Test in-D-)) 28% C N/A The original test is a-g.er (Air palance Inc.) or put. ac-C-19 response spects.s enve lopes 89-2175 ce l e t.a-the new si te-speel tic tau tv tlun of reponse spectsas theru-5 y saint-ture, thl m engu t en.en t l as
- a. usa r equ.n ll f led.
Da* leer Hutor Houestings for X till sori S&l. Report S&l Report 46t__P* H/A The new stresses were. T4100Fl'e7A & h Vlle No.
- it.- 2 6 6 2 SbH-l)CCo-o.w c a con mu a v.a t i ve l y c u t l an.s t ed al to Fl6 )A & D us h9-2174 flyures 001 by emisltipl ying the un g
p-17 rigures yleid onl9eri.s! mtsemmes lay the to C-19 p-17 1.a r ge s t necelet.atlun in-8 C-19 ca ua Je ca** pas i n9.s ! ! t breo all s ect aesns. Themo new utsesses see below the new.s t laswals t e v.a l ue s s (l.csetune, the cyut ment le sc<tu. stifled to the eiew s i t e-asa.ec il L e e.a s 119 de. tLee per thatus tbsusa t i sig s for X E:dlann Sk t. Itepor t S&t. Iteport 4.It ~*f ' e$ N/A Tlee new staesses were 74100t ulo tier u F07) Filo 14o. St.-2682 S Dib - DI.Co - na se.1 conwe a v.a t i ve l y c a t t o.s t uel b9-2350 rigures 00) ost by seultiplyin9 the 1 -)? Flyures yle t al ,d usiginal staemmen by the 11.1 11 p-67 i l.n a y ca t acce l e r.s t ioni in-C-9 [ 23-J ts esca o com.p.a s I ng.e l l c-19 T, gn a[y on+ 7,n]er 4 thsee d i s eac t i use s. Tteese j mu, h a a ~,, mfn= su w s t r es sem asu be. ls ew s....,,-.h,. -..e.. ( ( t her e t ess e, thu cegiange.utit 4
i ss s e.gu.a l l f leel t u the new tw y v. n w h
<.sce l.t ices l Concluulon and Fess stlim t Spectra t Analysis Pargin Test Analysis Neport i Spectra I Con.pa ra t,on H.stgtn Heport i of rig. 8 Safety .s.$ rieu Damt.crs X Edison S&L Heport S tl. ficpor t _ T4100t049 L Fl02 File tio. S t.- 2 6 8 2 Sun-Dt.co- ' f214 N/A Tfie new meresses were i... s ed ' conservatively cutimated 74800 rill & l'i l 2 D9-2154 rigures 00) ori tay s=ul tiplying tieu T 4100 r o tih h-17 P19urce y1ald urlyinal stressem lay tree C-9 h-17 i 1.o r 9e s t acceler.stlun in-D-38 l crease casage.s r i n J 411 C-19 tierce di rect ios.m. Tliene 4 l new ntacuses use 1.cluw ~ t l.c new allowatste v.a l uc u s t iiv r e t on e, L t.e c.pa s saesit in r e.gualli ard to tieu tcw n, mi t e-upec t t ic c.s a L t paaku. I v..) in uutterfly Dampers (V.e l ve s ) X Edison 5g (N-5) 561, llegw>r t
- 11. 2 % _7 < VA N/A l.n o al.uv e l W
Type 4J40 D.smpet rite No. $q ( E-nd) SDD-DI:Co- 'uahCJ Sises 0*, 10", 14*, I tl *, 09-1819 ) 9 (Vert) 00) on a tu" rigures yield D-37 B-30 C-IS' . s it.snua l A i r ts.nepu r se X Edleon S6L Heport S61.Ir port 16 6 b e H/A Tle original outsmic Staus Pi le too. S t. 2 6 H 2 SDD-[>ECo-i%.P stressus were acp.srated Hm to h9-21~/6 Figuree 001 osa out of ttee or igin.n l qu.a ll-ll 'J G x 24 H-37 rigestes yield f l ea t ioni, increased for J 45 m 48 Il-13 b-37 l 16 m JG t lies new site-speeltle C-19 n-18 c.s t t leg u.s h e, and tteen. edited q QMo/.1 icq g*cq, uve.t i,e. n 4 fahg /*+c #pr/*s f o rcp ",o-4et s w.P.untw: /M j C-i y to orlui.. I n...m i ein.s an.n aesa-cno t u 1 / [, !* / l oails. The eiew en t e e s s.c a Tr[N,b ', [ l / .e r e leelow t isu siew N .e l low.its l o v.a l ue m : t ree s e-Jg8* g ff y
- A
'T i zs.r6. ru ) c 3 o /l K l" c /Ce/ fone, t t.e e.pa l g eeni t is -l- " " ra * ~ ' '~ -- y
- .e l t e-u pec a l i c ca s t laq u.s k e.
&")/ f5 M u 4 1 i l i l j = ~. TAllLE 3.. -2 3 (Continued) 1:3SLHTI A1. IIVAC DAMI't;itS _S t: 1 '.M.l e. _H_l:- t.'V. A.._l.t ' A_T.i o..t.* l >3 fly _TAtief Hettiod of Orlyinal [ Sy s t eem, Structuso. Con. pone sit Qualliic.ation lic-1;valuatjon Results Duscrig. tion t 'r Conclusion and Periaaks Spesc t r a t Analysis taargin ^ Test Analysis HeposL i Spectra 4 Comparison. Haroin stepost i of r13 8 Safety e l Tyg.o Cull llamg ca's X t:dimon S & t. SE1. l<egu>r t 45% N/A Tlio new stressen were 7 *2 " x 'e 2
- t is s u File tio.
Itepot t St sD-O t:Co-DJ ccuservatively chtim.ated 16" x 16" t19 -7 61 SL-2682 00) sen by multiplytn.3 the rigures r19us ee .a l l ow.n-os ly s s..i t utremnem tay the D-)7 b-17 tale
- 1. sagest
.s eco l e s.i t i on ts-38 is- ) s 4.uc k - ! sic a eano s:bhep.e s $ ng alI ,j C-19 C-19 ti9 t hs ee til s cet ions. Tleceo .] n. a.1 view u t s e e s.c u are t>ulow i L lie new.n l low.itale v luens { t i.e re f u s u, the clut e.ent t 1:n r e.go.il i f l ed to t l.e new l e 6 t u-ug.eck t le ca a t ti gu.nh e. I I un lit" a 3)* Cues t rul Itoons X t:d i most 1 L9 (N-S) S&L Heport 162% N/A (.is.it.uvel O D.in.g.e s a F1 le tio, Q.g (E.W) SDD-bt:Co= 11 @ 119-761 1 (Vert 6003 on l Flyuses ytold 1 D-37 n-)B C-19 i
- g riso p.a peru X
t:.11 son Q9 (NS) S&t. Mcguer t N/A N/A Tleo now e t te speci f ic l'I SIT 41:su r rlle No. 'Q 9 (t w) Stus-l)LCo-e.a r ti.qu.ake acce le s.s t ions g 189-2090 g9 (Vugt 001 .n s o less severe t ii.a u t i.e Flyures accelesation t o.ed a siy a n-)I t i..i t were used 1si t ree ti-l es ussyle..it meimmie egu Itta- .l C-l's c.it s on s t i.e s e l o s e, t ie t s /[frj 97d[ 'T NNh Ob 'NN NI g { { l gdhcck' M ) guy c O S. i4 s*- TAftt. 3-24 IIVAC fuittitN AIR FANS _Sf'I. SM I C. _ f.*I.: IV. Al tlA.T. in, te Stft'MAftY T Ah!.f' Method of Original Sy s t cia, St r ort ur e, Cwrenent OualifIcatlon Re-Evaluatlon Results th;se r let Itm Concitssion and Pemarks t Spectre t Analyste Pargin Test Analynle Report I Spectra f Cmpar1snn Margin Report B of rig. I safety peturn Air l',isi X Edison SLt. Peport S & t. Pe[m r t weakest N/A The new stresses wern (loctudines Ancteur Dolta) Pile Nn. 51.-2(.92 SDD-litTo- .:mgg - _ renservatively estim.ited PISIT11nnCO si D9-364 Figures 003 nent by multiplying the it-3 7 rigures has a original attesges by the B-39 D-37 'I t largent acceleration in-C-19 ti- ) G marytn cre.ine comp.irin; all three C-19 isa scit directions. Tliene new on st renses are l>clow the new ylcld allowable valuena there-fore, the eqinf racent lg p [r((O @ kh e s equ.e l I f I cet in t he new / N8 b7/
- l t e-apacI I Ic ca r t h'lu,ek e, Q(
r u, I(n O /' // E,sr,w,,.+e ,- un G $ $ '- C ' ' ' .[~~~r. f/r ds/.llC i. ( [- / t se ~ </< & cp 3 e. / //.s r. ? l 6 C/ " 7 w c: 7 '/. c~. -l //3 : 7 g/ e,'g ,[3 / E'A 9 *i. r,a '3 .62 i 64 <l.~ /, 5 : j ': ,4 7 ,. 9 t_ ,i / r ( C/ l f/' / j /. l b, e./ C ~
- u3
,/ u g... - 4.'s./ i~ s 7 ?T I l s i l l l l l m ~ TA.: 5.)-25 livAC Cf:MTntiticAt. Cittit.tHG trHITs St'.lSMIC pr-1: Uni.itAttop S!??ti"Y_ Tf D.! E .Hethod of Original sy s t r a., Structute, ca.mt.on e n t 0.salifscation Pe-rvaluation Pesults sw celetion. Concluglon and Pemar k s t Spectra t Analysis Pargin Test Analysis Peport 8 Spectra f Comparigon Haroln Herg.or t i of I' l es. 8 Safety Cent e l f ug.el Clel tlin9 Ifni t s X P.dison SLt,Palert SLt. Peeort ' M1 N/A The new stressen were I t nc l e..te s As.cho r n ) File No. S t.- 2 6 ft 2 SDD-Diefo-I.. iesU conservatively estimated p l S I T i l nn tirit:R 4 9 ft 9 -6 % l l'l ap s r e n 00) ein ort-by smieltl ilyi n<} the l 1 n-37 rigureg t9 nal or1 9 nal stregnes by alie t 11 - 3 9 H-37 allow-l a r <;c as t acceleration in-C-19 ft - ) R .ible es cape repar t nq.n l l t it ree j C-19 et t rect lonn. T'. = n e new i stresseg are below the new allowable valuegg there-tp fore, the equi eent le t 8 r equa l i f Icel to the new ,] si t e-npect Ile c.it t f pvike. l leuptune pleie for x blinon In 9 inpu' S&L Pelmrt. 21001 N/A The original quellficatinn ,l re s. eifua.el ChiIllnq tinita File No. SDn-Dt:Co-Indicates that t he stlne
- l n9-604 00) w.. g muls icct eel t o a,10 <3 f'lyurcs input.
Thlee arcel et a t f ore n-37 l =e wel l.sl.ove the no w D-3R s i tc-sper-l f le re etmnge C-19 [ apectras tiierefore, the /.t-> ff ~n,le cnt i,. r e,i,,a i i r i e,1 f g ,$2Q'i sw?M/xf f,n,bk9k0t '3 e:m t y gf,. t.. tue n~.IIe-npecific ea r i h<p.. c. l,C@ G /^ f< W,
- ,m gy<dowy
TAtJ B,.!; S. 3-2,6 s llVAC EMI!ItGmen HNAC-UP HOTOtts Sl;t SH IC f<f'-!~ val tf ATIOt* l StJPdHAltY TAllt.E Hethod of Original Sy h t enie, Strasetune Component Qualific.stlon Fe-l' valuation Ne6ults tb hica lpt ion Conclusion and le marks e t Spectra Analysis t'a r g in Test Analyale Hoport i Spectra 4 Compa r i son
- Hargin Neport 9 of flg. I Safety 1
i thes ycucy H. eke-up Hutor z X Edison S& f. S& !. H/A 14/A Tiso new alto-specific ca t tlutuske esecc les t.a-f us-F.e ss es wit ti PIS 3*e rile Blo. Heport Report T43000041 6 16 D9-1196 UL-2682 StJt)-ht:Co-L iones are tems severo Fly's 003 tii.an t isa acce l e s.s t ions b-37 Fly's lo.id i sig d t ia.s t were used u-38 u-37 in t ime original me i m.n ic C-19 u-31 . pea l i f ic.at t un g L t.c s e t or e, 3 C-19 tiil m e.liallm.cnt i ns acqual-stied. 7 3 s 0*0] (f / f '*/ $C [6l' D l /AfNM/ M / / / p-ce?re[e / Y i ey,,:#ce.g/an. .m% 4 c1 yisrixm in I l O h T A n t.t* ' 3-27 iltfRC f:Hf ltCENf!Y MAQM-tfl* Afe. ef f'CIleCUf.ATIOff Altt Fif.TCDS IfMITS Sl;t SPile ftt:-INAt.t?AT ree StfMMADY Tant.E Method of original Syo t t a., Stauctune, Component Qualifleation Re-t' valuation Resulto tw seeIptione Conclusion and Permarks 1 Spectra t Analysta Parain Test Analysis Report f Spectra 8 Comparison fiaroin ferport I of Vin. E safety Emesqency Hake-up P. ins X Pdison S& l. S& l. 214% N/A The f.ew strenees were Pts I T4 ton 0017 L 16 File No. Peport Peport T. ne.I ~ conner *atively cotimated D9-1387 St.-26R2 S lit e - fif'Co - on by entat tiplying the orly-rig's 003 Y l e t el Inal stremnas by the n-17 riq*n largast acceleration in-D-36 n-37 creann comparinq all three C-19 D-39 directions. thane new C-19 strennes are i.elow the riew allow.thle valuems t ha'. e-fore, t he equlgeene is r eq:-ali fIcat ta the new a t t e-s pec t f i c ea r t h. n d e, e ,g,, n,
- p...f.......,;.,s.
to f:n.er.p.ncy H.ske-up Pl l t e r s X rd f rion Piq's Fiq'M M. sl N/A 1he new strenn.=a were. Pts t 7110n101i File No. n-13 n-37 It a e connervatively ngtlaate.1 n9-762 ' n-l'I ' '11-M " I on l>y mu' t i pl y i n.: the or(q-C-9 C-19~ Y i e l et inal at renses by t he of " '" ol' largest acceleration in-S 6 f. S& f. crease comparinq nll three Pegert fiepor t. directtous. These riew St.-?fi t 2 I f S DD-Df'r'O-nteegnes are 1.clow the ""[ ,,f,I l no j new allowable v.ilnes; p ' t he r ar f or e, the equipment h< ? /Jf&d Q//.fj ) $Yi k Yl
- '"U alte-apecific carthy.eake.
bRc. $f.5/ U'fftbryf, Gyy /Ytt, $p;u/M / O I !(
- i{;'
e e w e e e s dy tsh n h eg nh e k nh f - r t d - - r n-e se l d k ee e ei h h ici nel ine r tl it we e t . ti I t wernwa ot a ear eh ; l I e mer ear eh eieu hf m r ms enl ct g lh o. rmoenI nt h nq t nih at I P wt etiol el t e ei h ol t t aunt u I e p i f aewna wt eti aew r et l rf t q,a sh t ss i < oc nh t m o;eh r eet t e ct q s i s eu d net yaqel aeti set yaqel a wt a el sl n e brnh ev f e br nh et e peen i oe a myg et Tb e I. i syg eiTbe l o scrI i ml nl t e ml nnl r eh e c. sl na l r l i t c r e cac i n eeieea el tl eeieoa eaq i eavnel r w io rvyn a p.rb f l rvyscp.rvedf t eoin a eI til ncmsaa ,l n til scmnn et t eni sh s nt peaon wel - st p e i. o i e e. l c ek t e t t u air cosor ae air cosl t t e anarl n wvtt t i el out wvt t t t l e b. t i p us nreag e c erl ssnt nl f o nml g i. ee rr k nml gaceneue t et gl i N p qi. erl n neu encg aeese ne.i aset 9 emeas w ,l n<eewnn e s a - nhl l i op C en arerr wm wa en ar ca rl r qt erncai taq e. h oynarit et sei h oynaet tl oei har chr e p e Tcbil cl nnLi ne Tcl il c I. naf rs Tcaat oce 1 n y i t gf e t rof A A A a a / / / s N N s M S t t l l-u s8 n l ee pt r yr l o n ap o nc t h D j AI t l.( \\ n J til n t n ]3 u n eOi 1 d na id d l i a a k - c ge k - e ge l l r at mng rnne at mna v % r n r sno A etioonaaoi t t o. o t e s o <i a 1
- o. tani
/ M WeCpl MI Y W e C ph 0 M I V M-f D f e C R n N 8t ao Rf 0 rsI o O O C C C i f C ti t: tr tI T cr. l R A 1 rn s T f eag l rD i s T rD s 2 l t. ppi o-749 & gD1'y 1 31 & lw p-1 'q 3 M l e- 'q 3 l 7 7 R 9 Smr eD0l - - - en0i - - - lad 0i - - - t & gD) 1 3 R l ^ o . H AV T C sis 0FnnC Sf S 0 r n 'n C Sf S0rHHC t i 'y 5 T. O L f C I' ?" _ f H; R 2 a 2 2 1 P C r r .t8 t t6 s . t0 t9 T O l P' t r6 s I r6 n E t t o2 789 c & r. 'q 31 o2 78 g o2* 78 p. 'g 1 t 1 1 g & p. q1 I S e et i - - - eti - t p SRSrnnC 1 9 et i - - - tT. I l p SPS PnnC SPSrHi 0 P a S f S n fM igo f n // C iJ o o3 o2 't nN4 4 ni0 nN0 R t V oa r o 47 o 2 n 2 S t If c o se56 ne2 ae2 eR N fi p t l il - ll of e dt 99 di9 di9 i R i
- nn EFn rFD f
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- 8 h
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- "/ C77 ' G
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' s,,.,,[u,f;...-f.cp c,: e s e, / c,. - u <... M y ~ ffccci-kllC i f/I*nem e d~/ G 2 9 '- 6' A'. 6 1
- +,p/r
- 7
- -/rc M. 2 t i i
fh'-f.th.',r-- W+j* f/o ' (Q i f i.-~ b/$ i i l /l w s e o l / c,f Occ cy'r ep/ j' /wip.- // p. 3,,' ~ / C ",,, t ~ 11 /
- f,2yc,.' &,n-=n..=_t /$, //.
1 k i s l 1 l I t T- --*wt +-aS -f --=-yaawT---m+1 g-p-W9-ta--M NF-M-wg y--gv*g--y&WD--day 7*,.y wy%--ammyyy 3 y . g g-v 91.y mw-yy-wywe g ww-e - 7 e+ e-9-gi---1y9is r'9y y ^ TAD"* 5.3-29 ItVAC Cit ? t.t.TD WATr.R PlotP f.ND HOTOR S'i Sarc sc-yvAirATirwe Pl?!^ EL.T.^."'M Hethod of Original System, Structure, Coa. pone n t QuallfJeation Pc-I:va l ua t i on Resulta TAseslptlon Conclusion and p,cmarks Spectra n Analysis Pargin Test Analysts Peport I spectra e comparir.on Harain Report i of rio. 8 Safety i clill ic.t Wat er pump X bilmon Pump ~s S& f. N/A a n.) notor File Ho. Eg H-S lie por t ^ N/A The new site-specific 1 t i r. 3 t e l one n g o a 41 n9-651 3 g c-W S Dit-firco-earthquake accelerations are less nevere than t lie D9-IR75 2 9 vert 001 acc.,loration lo s.Il nq s Fig's that. were useil in the 4 MTn's D-37 nrsginal solsm!c qualifi-3.6 7 H-S fi-38 cations tb-retnge, this 4.25 9 r-4 C-19 e egisigeent is requalific.f. 3.6 9 vez r. j &f ? ? l o fm /MA w
- v; y,y bm, Y/s *9 /M Om
.G,wN t 2 c / t e 4 l 1, 1 e TAtli .3-31 IIVAC COOL.l:ltS SI:I SHIC lit:-l. val.liATION SUP.*t A ft Y T A ltl. l* Hethod of Orjg in.a 1 Syn.e s m, Structisse, Cong.anent Cuallfleation He-Evaluation Pesults f 4:sce l 't ion
- Conclusion and humarks l
t Spectra t Analysis P.s r y i si Test Analysis perx>r t i Spectra f Comlia r i son - H4:qin Hegort 8 of I'l y. 8 Saluty Gw a t cli jes s' tuose Coolere X Edison 13 1 ), B14, 15 3 ), D)4, H/A The original scimmic S.trW 1 u is hu.ua coulete I'l l u No. CIS C-19 .a u e stressen wutu urge.a r.a t ed Co.it s is t Ast
- oe=te s a s so r Coules 139-64J S t.- 2 6 3 2 S L 1,
un out of t hu os ig t s..e l agu.1-(741-00u001 & 3 (Ve r t i c.n l Heg ort Yield a f ie.s tion, inese. sued for T4 5-Utah 0 84 T1sso u 2.D i St at e-Dt.Co-the si t u-ag=.ci t a s: SS t:, and T41 - uof10 4 9 00) .sJdeel to t lio no s sn.e l ope r a-Iteug=:ct a vel y) e ting l o. nil m. Csiculatet steessus esa below.stlow- / .sbless thunuture, ti e 1 (Q - 7 M d t / e.iui..ent
- i. r....u.. i i r i ca J
s to (lau site speettle SSt'. autzhs. uur, can <ma n a?7 e / /. q;~ g/is & CQ~ tW/1 h k h i e r e' - ~. - - ~ ~ - - -., - - - ~ ~ - - - - - ~ ~ ~ ~ - - - - - ~ =~ - - - - - ~ ~ ~ - - ~~~ ~~~ * * ~ ~ ~ 6 TA.4 5.3-32 Illlft NOOH COOLI:ltS Sl'I!.MIC* HC-INAl llATIOP8 SUP*HARY TAlif.E Matthod of Orjginal Sy s t ese, St e tee t u s v. Creit <>ne n t Qual ! ! Ic.at lor. Re-t valuat ios. Hesul t a t> eses in.t los. Conclusion and hem. arks Spectra An.n l y a l s Pasqin Test Ariml yss l e Raqo r t i Sg ect ra 8 Comp.srlson H.argin beg >on t I of Fig. I safety 5tsin lei.um Coolet-X Edison S&t. Hensor t S&L Hegert N/A N/A The new site-ugwci fic t iencluillies Ancleon' hul ts) l'ilo No. S t.-2 ti tl2 sop-ljt:Co-coa s tle.guaker acceles.stions P8 SIT 410Gu0lts b9-%4 F19utes 00) ase less acwe ce t ha re the l D-29 Fl yta r e s .iccc l es t.e t t ini t o.sd a r:9 m t ia.s t 18 - 3 0 0-29 wete used in t lie u s l y i n.s 1 C-14 h-10 se l e.ea t e agu.a t i f ic t t un s C-14 tsau t e f or e, tie a u e.gulpaent s' e s ceg u.s t i f i c.f. [ h f h up, sx4, Wacs 4m Oa G" ' ' ' C9/7#". 1 s J* t' e t s.. ,g.1 e; I e r Tr~ t 5.3-33 IIVAC Dgui =nent Huom l'an-Coll (Init t St. I *ittic PI:-t. val ttATION SUt*MA f t Y TAlit.E Mothod of Original Sy ei t e m. Stru.:turo, Com.ponent Quali f icat ion Re-Lvaluation Hesults f(seaiptlon Conclusioen and Neveaaks Spectra t Analyula Pergan Test Analyals Peger t 8 Spectra 4 Con.p.e s i mon Masain Heport i of l'i q. I Safety bgulgeocit Hot me X Edison S6t. Hogert SSL Heg.or t _$113 _. ti/A The new stressues were F.an-Osel1 1Jn6L rito No. S t.-26 0 2 SDD-lit:Co-kaapud conservativuly cht in..st ed t 8S17410011028 b9-554 Figures 00) on by multitifyinq ttic ur191-ti-3 7 Flyusca yletd n.nl ent s em ecu t,y t lie 1s-16 11 - 3 ) 1.s t yein t acceleration I si-C-t9 ti-J e cae su comp.st1:nj.s11 thaoo C-19 d t r ce. t tons. 1ticue new p / s t re:smen.sao t,elow t ree i.e w l lowatit e v.s t uos. / (k Y /Zff L//h hp? ] ~@f M&$f t teen a tun e, s tie ena n n.osnt e ,/ / / .. qu i u lea to i i.e .i t. p ci,ic . ti - v. ),Lqjf,k ,ie. b & A X t m '? M .0ctc n"" Qs3,1 i 6 4 e m .w TADI 3.1-34 IIVAC itCic l't!Mt* ROtM4 0001.1:M St I!. HIC Hl'-LVAl etATIOte St_8P'PtA34Y _TAtsf.t: ttathod of Original Sy0 t t,sm, Structais+, Component Qualification He Evaluatlon Results Desesjptton Conclusion and Hurearks Spectra t Analysis Pasq1n Test Analyste Regust t i Spectra 8 comparimon kargin Ha geor t 8 of Fig. 8 Safety Hetc t*ua.p stoueta Couler X IMimon SI.I. Itepor t S&!. Report 21.44 N/A The new atsesmes teese l'I S 8 T 41006102 4 Filu No. St.-2 f,8 2 SDD-1*Co-u.s a ctr consutvatively estim.sted b9-554 t: sta t tel t 2 003 ur 12y multiplying the or1 1 9-a el Fi9ures yield nal utsemmen tsy the Fag. C-11 15-29 1 r9est.a cce l e s.s t l un I se- !!- 10 ese.sse coep.saing.al; trarue 4 C-Il directions. These new streamum are t,ulow tiie new .al la w.stsla v.sIuum a clieru-t urer, the cyisigaent la e rugu.s11fAud to tties new a s> tows" ?/-s e e w w i " " ~ ~ " ~ " ' ~ ' " " ' - ggf y/skif.h; 4Q $* h <N/ N. ? 4 e i t t I e i t f ~ -s. TAus. 5.3-JS IIVAC CAtSt.E THAY COO! !HG l'AN S_SIPJK_!'E-W^LL'^2M? SimMAltY Taut.E 1 1 Hothod of origani t sy h t is an, Structuso, Campsiese n t Qual i f ica t loss Re-Evaluat ion flasults tws.ca i.t lose t Conclusion ar.d Hema Le t Spectra t Analysis Nasgin Test Arealy s t s Heport i Spectra i Cornp.a r l son H.s s g i n licport 4 of S*' *r _l 2.<th?hHf /-ec<dli qbc b~*cc'""'* inl"<T;LtT""" "" fhm 0 *r c / ) e ts' I ~.2 1 W t i \\ 1 .a h 1 1 4 4 i i e G t 9 TA L 3-35A IIVAC 1:QulPHt;tJT A*JClioits E'i3 !*U IU Id!"I.Y.A.I;b'.A.IE!! S t >PPtA fe V TAftt r ~ / Method of Original Systees. Structune, Congene n t Qualiffiation ac-Evaluation Results Debca ir.t ioes Conclusion and Itevaankm t Spectra t Arialy si s Pargin Test Analysis Itupon t i Spectra 8 Con.pa r i mon
- H.seqin 14epor t i of Fig. 4 Safety Aaictios isolto for Llio followist. 1 Edison S&t. Itupor t S 61. Ite po r t wegu n g ecen t :
Pilo flo. S t.- 2 b 8 2 S DD-tat.Co-rigures Gul Figores 11 3# t* ump Itina. Coolur X DC-575 u-31 15 - 3 1 . h 71__ N/A The anchor lault attuseum ti-32 u-32 r,a :J w were recalculated tsy C-lb C-lb on eg.plyin9 the new site- ) 2 yield specifle mutamic lo.ida. { The resulting 6 hear s tenuton strenaeu are 12elow the siew allowable 1 y s t re m anas p therefuse, the g q .a nc ho s e will n.stely hum-l FJ Lain the effect of tho f new s i t e-anace t t ic e.a r tla-1 quake. Coastrol Air Cenprosasor Cooler X DC-577 u-29 11-29 H/A. Samo as alsovu h-30 19-30 a mes C-18 C-10 on yield 1*qu ignent fiosme Fats-co!! Uni t X DC-582 11 - 3 7 ti-37 33M _ N/A Same as alsove 4 tt-3 0 13 - 3 8 12a med C-19 C-19 on I orig-i n.a t 4 I I ttw
- atil a Clail lod W.stus punt an.d Motor X
t>C-585 u-13 n-37 l l aq _ N/A Samo as aliovo 19 - 1 4 u-38 1.a :s cE C-9 C-I9 on o. 9-ina1 aitow- = abte A h P j [$ l 1 o<.z .gn h kannt e TAtst i.3-35A (cont.) ^ ilVAC 1:Ottil' MENT ANCif0RS ee St'l SHIC til:-t'VAf.lf ATIOt8 StitartA tty TAltf 1: P Method of Origirial systeen. St s uc t ure. Coengeonen t Qualification fic-t valuation stomults Descriptioes Conclusion and i<ema r k s t spectra t Analyste Pas 91n Tust Analysis Report i Spectr.a 8 Comparison H.iagin Itcport 8 of l' l q. 8 Safety u csguncy Kaku-nye Pltter Unit X DC-593 0-13 n-17 9' 3% H/A Same an etsovo 119-762 11-14 11 - 3 8 "Ih C-9 C-19 on yield His t t i-resino Cl jia.s to CisJnge r X DC-589 11 - 3 7 Il-37 ?!t. H/A Same as aleove 11 - 3 0 h-38 7..ased C-19 C-19 on ytutd 4 #9 3 ~J sa sw i t u fiy e.i t Itvom Cooleau X DC-572 12 - 3 ) B-33 N/A N/A The new site-speeltic u-34 u-J4 earttiquako accelera-C-19 C-19 tions are less severe' tie.sn tino acceler.a t ion te adings t in.a t were used ^ in tric ori9 nal meli.mic i .anclear but t e.ilcu l.i t s on s ti.ca ct os o, t iie.n i c f. r u aae e equ.e I i t t eil. s4CIC s'. p leoine coolor X DC-579 ti-29 t1-29 H/A N/A S. amu.a d, alsovo 16 - 3 0 h-30 C-lu C-10 i G Aya//h7hk /$4 <?M,r/ /ih q /d+7 T. TADP
- i. 3-35ft DisYWEt.f. CtK)f.ING SYSTrH sa:s_y3sc us -t vigt!AT)39 Stitat4Al<Y TAlst.f:
Hethod of Original Srstem, Structute, cc.saporien t QualifIcatlon He-l'valua: lon Itosul t s lac 6calption tanclu s ion and Scmarks t Spectra t Analysis Margin T sst Analysis Report i Spectra I Comparisoss H.trqln Iteg.os t I of Fig. 8 Sa f es t y . - _ _... ~. _. ys psywull n=eling runu X Edison S L I. S & l. N/A so N/A Tho new ulte-speelfic n P I S IT 4100(.001 L 2 rito No. Iseport Hepost N e.s r t hqu.s h e act.C l e t e - ns-1106 S t.- 2 6 ft 2 50D-01.C0-tausis are l e ss e i. eve n e u9-1107 Plyuses 00) t h.e n tteo acculus.s tion 1-4) Flyutes l o.ed i ny m t h.s t wuru ts-4 4 h-59 used l as the utlyinal u-62 h-57 ne l umi c qu.n l 11 s c.a t t un g h-62 tiie r e t u r a, t h i as equip-ment 1:s a equ.s I i t i ed. un Dr ywell t'uolors 6 As.cl.orm X D9-637 18 4 3, ts 4 4, n '4 9, 057, -)s 8 I T47000001 L 2 Tries couler snount in9 li f. 2 186 2 feet utsow conn ade - atele so.s t yi sm wi t h s e-9.e s d to yleid stteus. T h e. coolluy coll f a osmiu.nsul.a nchus taal t m aae aImu.sdequ.s t e s.nd aao considese.1 e e.gu.s 1 - liied. d $~- Y N 0$ nul/A1 as+n ~ t / / } & $ 0Qt** d.! U [A.C ~ hNo 9t O WbeA .oc2ar.gnteffime7$ 4v /S f'29 ~ /s w a. ,ea potraw m, /*rn @y. n n / cc tau..t: 5.3-36 14t!R COttPt.!!X sfVAC SI: t f.H I C' IT-l.V Al.tf AT I ops i>'??l^H.Y I.Af 3:E Method of Original Systow, Structuse, Component Quall t scatioes Ite-Evaluation scesults bemeslption Conclu s j on a nd Heena r t s t' spectra t Analysia. Pargin Test Analysle Report i Spectra 8 Cump.s r l a.un M.s s as t se Hepost 8 of flg. 4 Safety IttlH Ce==pl us l'u-p House Vent il-20s
- k Itcovaluat ion was tea med x
S & l. S & f. etion, Switeljear cal.aust Ettt)- t ms-
- T,N on a dyr.asile.an.nlys i n ventet.ation A, u, Isiemut Gesi-029010 cr.atua ven t i l.a t ion 029950 a s..s l u of linear clautte utsuc-6 a t t aci.c. tural modut utilizin.J Hav. I t II 8.ne.a t ion tillit l'Hin-to batst ttic metinual of soapunse Elev.stionu $90' - 617' 029830 pl.a t e s pec t e unia a ri.a l y u e.s. A continuous, uninteruptud oper.s t ion and :.t s ue t u t a t inte.Jrity of tino mute lec t s y n t a mm dsa t i n.) anel ful-l ow i nig a n c.a r t ie.g u.a t u w.s :s dcea.m t s.s t...I in the sn alsov at saen t i on.ed
.se..e l y m i s. y ut s cuacas a s u w a t taisi AISs* tn allowablem. (*unt rol llan.pu rd, type CDil-Pts K Ituskin S &I. 1.27t* Stressus are wittiin it c and ou luola t ives II.impuru, Mf.g. Co. FMts-allowatale limit s. L)pu CD b2-92 CDitt-92 029950 Cont t ul al.smeer:s alua t s t y fe.stion tttttt 1/J9/79 tu siew responnu unwetsa. S L E. EMI)- 017492 3/20/79 I:MO-0171 t87 2/14/79 2/27/29 QQ /s4 Qff,1,4M Y [. fo9 t'f j/g /4 Q },o } t%r top tel.sde t,.amed use Q fjgj d#Qf g d.1, a 1 iuw t.Ic:a E / b / h WG $ e& $ & $[G? YY e h%&( n}d u%.r swa), , a nu-s, j r m 7% h S?o ni ynu", t ~ M TAtst t: S.3-36 (cont.) Intit ('tWl't PE flVM' SC ISet!C HP-t'VAI.1f AT ION StitattA ft Y TAtit l' Method of Original S r i.t s si., steuctuee, Cosalmonen t Cualifleation Mc-rvaluation stenulte Ih.a.es i.t lue t Conclusion and Reasar As 4 Spectra l Analysis t*,e r g is Test Analysis Heg or t i Spectra f Ccsmpa r i son Margin leensor t 8 c, f Fig. t Sa f e e p -g 4 e tuiu Cos o,' r.s u s X Dutf.nlo )N D D I D* S k t. 15.8
- Stressem asa beluw I'qu i s.
X-4I-03-C01, 02, rurge Co. [ f.gg, g. n'.M n - yleiding on founl.etion gyggg h 01, 15, 06, 07, ou 17 K-IS$0 tt 029950 teot t a and wi ttiin allow-fIII f.e ,on alttis 23:9/78 'O. .(, *,. y .nblem sui the other lC N I ""* e.ation 617* J";3, M-fG[lxba G3 id-S k t. seetloan. This equigwent itillt Complum l'.a n u X Duffalo g g S & ?. -13.7W e it.a med on a snore soplais-Equip. fl.a. X 0 3-Ut)21, 22, rurgo Co. p t'MO-tL ic.a t ed ana l y a n a. L t.c 77E-25526 y. g g. g 4- % fg,o tg,[g (* 029950"* tena should aluality-23, 24 1.uc.i t lion Pitu 31s 9/78 G Heanalysis as inndotway. 4;t uv.e t toes blJ' S tl. Sue Sere t i ons 5.4 END-016338
- 1. ' $e.,.(
g,9 a r W htste Co plen P.s aa n X Duffalo L 3 ' % C,4 W @.*glH
- f s t.
>100b a
- tea mt oss a very cani '
l'.gu l p. No. X-41-03-017, 018, rut 9e Co. i
- %%%4 Il:" {.lett it:1950 I:Mti-
= = = - = turvative avalu.ition, 019, 010 77K Mt 7"" A the attemmes in the f.oc.n'L ion HilH $24-273 g Elev.it isen S90
- 9/78 e
lgg,g Q4pf[ (*CQ 'gCM, name componesita ese b l.s hu a than allowablem. S t l. l LMD-tioweve r, wtien an.nlysed l es af e t a i l, the fans may 016338 qu.311ty with little ut na n.odi t ica tives. 8: a - analysnia is undesway. See Section 5.4 e us found.etion 1,olts based wi yield
- r< s jnlet stand luamed use yielst
- t ur a.t..i t t over yleid
- r< s jnlet stand luamed use yielst
TAlti.c 5. 16 Icont.) tttift COMt'f.EX ltVAC SE f !.ttic as t:- t_ vat.ttATlot* stietarty TArit.t: M Method of Original sy n t ese, Staucture. Conw nent Qualifseatton re-Evaluation mesules taus.ee is.t ion Concluston and kaananka t Spectra Analysis PariIn Test Analyela Deport i Sgiectra i Comparison, Margin Reg.o r t, f of Fiss. 8 Safety h [ Heest complex rans X suffalo S&L 16.lt e Stresses are 12elow ytol.1-L*listp. Mu. X-44-03, C009, 010, rurgo Co.
- p 7 'g q q t'MD-ina; limita p
4 011, 012, UI J, Ott, 015, 016 77 K-25516 / / 029950 w f.oestion Ittilt t;t en t 1..n 637 y g*g g [og f 23 s & t. I gl;,, a:yj/Mem n <tl skis t em% 655h G en 4 4 = f g = == a for intet stand liased on . yluid 4 n m TADI.E 5.3-37 Iti3T!ttfMF.f4TATf 0N AND Coif 7!tOI.--Pitf NCIPAT. SY37 EMS StiSMic PE-EVAT.ttATIOt8 Stf?attAt<Y TADI.E Method of Originst System, Structure. Cunponent Quallficatton Re-Evalustion Pesulto iktscription . Conclusion and Pemarks Spectra t Analyste Pargin Test Analysis Iteport i Spectra l Cornparleon Ma r<ti n Report. I of P l at. I Safety oua cru te<ot. Hoo,4 PAtitf.s y til l - P t.u l X X 20% Panel pents selsmic re-quirements by comparison with till-P602 Lest till-P602 X SPE Hemo 48% Panel meets seismic re-107 -- elutaements leased on 110 ortelinal test Itl l-P40 3 X X SPE Mt:MO 26% P.snel mente seismic re-994 epil s ement e by compar i son 1 10 wit h 1111-P60 2 test til l-P612
- X 262A7242 21%
Panel rect s selsmic re-epit rerw?rit u lis hed on or l<tinal test til l-P613
- SPC Memo 7.5%
Panel c.cets seismic re-994 e. epairement s t;y coepar ison 131 with Illl-Phl2 test stil-t 617/P618
- 28%
Panel meets acismic re-qtsi re nent s liy corap.ir i son e wi t ti Itl l-I'612 test til l-I 621
- 15%
Panel meets notamic re-e apsis ement s by cor parison with lill-P612 test til l-t*622 /6 2 3
- SPE MEMO 37%
Panel meets seismic re-ap:I r emcot s ba seil on t est s 994.- 132 of similar panels for Ilp.rie r.nsi i 1.aipina Ve s do til l - s*6 / 8
- 20%
P.enel meets se l t.m i c re-e ops t r ep=?nt s I.y i +r p.a r l son witte 1111-P612 teut @ ema*% d J Le P a w A ge m w l, s 40 s % q s p ya l p g. p h e e.gpd M m t . w l. u w c. .~ m TAf1LC 5.3-37 (Continued) INSTfttfMt'.NTAT!Ott AND CONTPOf.--PftfMCIPAL SYSTEMS S E I SM IC_ RI'-EVAT.tf ATION StfPHA14Y Tant.E Stethod of Original System, Structure, Component Qualification De-Evaluation Results Description Conclusion and Persarks t rpectra t Analysts Fargin Test Analysis Report i Spectra f Comparison Margin Iteport i of Fig. I Safety ill i-P 80 9 SPE MEMO 12% Panel Mets selsr11e 994 ^ requirements liased on 118 original test 1111 - P8 07 Panel meets seismic requirements by comparl-son with Illi-P009 test til l-Ph u S Panel meets selsmic requirement s lay comparl-eten wi t h Illi-P009 test I til l-PBl 7 49 Panel meets selsnic regis t rerent s by comparl-son with origin.nl Itll-PB09 test local hocks s Panels If21-P004 X DRP 40% This equipment is requa11-P005 X A00794-ficJ to the new site l'o n 6 X 22 specific carthquake l'O l ? X 1021 X P022 X i I!21- 037 DRP 74% Tliis equipment is requall-l A00794-e fled to the new site-22 specific carttuguake fif t -rneo X OPE DRP 681 (as at<2 vel { IOst X 1078 A00794-I082 X 22 ( l08) X l'f t S 4 X l085 X l flH6 X t007 X [ ,t; ,!4'
- +!!.
!t i la s u k q r ee a rt e m ik e ssa ^ R i uwq d t eh n nnt a e r mea n ph e ) o i t i u c e s qoi v u etf e i t lc soc a n ice s o hip c Tf s a ( n y i t gf e grof g a a e P S t lu ei s t e st P yr l o n ap o ne i AR S t M au n f T l i S a o Y v % r S E a H I e A R ) d P n e I N ao u C O rsI n l I ti f i i T cr. t R A E. eaq n P t ppi t. o h SnnP T C A A o V T C ( f 0 E ~ P Y nT E R O N R A O t a i . C C P r 5 I U t D M S c E. N S e t A I l p D E a S t A t S n T O i n D I go 8 T - A i i 1 R A rt t 0 0 - T On r 0A - 0 N e o 6 00 E fi p 19 399 M of e 22 - - 0 U i p R 1 P HSc dl t T oa S hu o N tQ l I e s M y l X X I: a !I g }* i nA t s I i i I e T t nen op moC n .o ei rt up ti D F cr uc E rs t e A E SD G H. ^ 9 J 2 m P P e t 1 1 s 2 2 y S H I <1 l l,1'i i'
- 1
,iijJ m 'IR..a 5.3-38 INSTitUMCHTATIOtt At4D cot 4TitOL--EECW SCI SPt!C PC-tVA1.tlAT109 Siff *Mr.RY TAft!.C Method of Original Syst(m, Structure. Component Qualification Re-tvaluat!'an Feaults Description Conclusion and Femarks t a-1 St>e c t r a Analysla Pargin Test Analysta Report i Spectra $ ComParlson Haroin Neport 8 of V i <t. 8 Safety ,$ o '[g[*,U" ~ Ill i-P 8 57 (relay cab) X 262A7245 D!t r ett j A00794-22 l l 1 specific carthquake N' See Section 5.4-1 Ill!-P860 (termination cab) l !!!!-P891 (termination cab), c1 j* See Section 5.4-1 til l-P601 (insert tis 14) Q.",4' See Table 5.3-37 til l-PS O S (insert A5001 h$,')[,que Table 5.3-37 &O ?l % D 0$*C'Y / DQ q } D XE k,f lH $0.?/11d (;f 'i?7 /C10 0 'l 017 ,/ e ff & fiGin O t7 6%77/,/'! '77 CGYdto M,J/,} f*$ bM A'^ .d'ih / 2/:6 24, ?dWCM G2 f/NO3
- h
%: z.. f l ..1 3 1 a It t t 1 i; I n tADt.7: 5.3-37 INSTiiUMENTATIOil AND COtITitOf.--CONTPOt. Allt ST:ISHIC PC-I:VgtJATtors StFFHAftY TADff : Hethod of Original Systers. Structure, component Qualifleaticn Descrlption Re-Evaluatlon Pesults Conclusion and Pemarks t Spectra 4 Analyste Pargir. Test Analysis Report 8 Spectra f Comp.srison Harrain Iteport i of Fig. I Safety P50 - North control Air Conig,russer Control Parel 9N Seo Section 5.4 5 P50-P001 including PSM-P50-fl021 A and 1:/V-t'50-P000 A .p S.a Section 5.4 PS t:-l'50 -N 0 20 A see Section 5.4 flor t h fiehydr.s t lon Uni t - X Bil-436 P50 02000). 5, 7 ef 6 See Section 5.4 JI it!I-P914 (relay rei cab.) X Nuclear er it!!-P985 4t N '*The 44 margin le based S t risc-f upon the minimum yield tures c) strength. This compon-ent la rectualified. Ill i - PU 'J O A (r. clay rm cab.) Of t Sen Section 5.4 ,g 1111-l'601 (!:514 ) yf[ U See Table 5.3-37 Ittt-PU60 (teamination cab.) s,
- See Section 5.4 t'
/ N Oh f0f f h f me.ysp;hanggy,j,, /,,,,ag;,, ,, u s, e -r w n .~ t TADt.E 5.3-40 l It!STfJdtMTATION mfd CONTitOt.--1:SSI'HTIAT. IIVAC SEISMIC RE-EVAT.tfATIOF4 StfMMARY TABt.P a Method of Original System, Structure, Component Qualificatlon Re-Evaluation Resulta Description Conclusion and Remarks e t Spectra t Analysis tsar <lin , Test Analyals Report i Spectra 8 Comparison Haroin Report 8 of 4 Piq. I Safety I it21-P296A Div i IIVAC control York g, Selsmic Test Report p..ne t wi t ti.s t l internal coa-77113-2
- Edison Pfle No. D9-1838" 7
trolse solenolds, relays submitted to H. Street $th floor aus. 1.ullding si,,,
7 A (local) i h TSE-T41-N374A, 18 3710, 14 3 7 4 E, g See Section 5.4 i til? 4 r:, NJ75A, fl375C, H375E, i ti l ? $C, it)27A. t1222A TE-T4 3 -tal 19 A, it)34A Pini-T 41 - t#4 5 ') tt f 21 A, till4A),'(- gL, 'y! //bng asy. n w m M ' r. V'o es m.t. I .Wcnce no - a'c o, I
- A See Section 5.4 GsWIr'A
.wa s l g/ 0TY ^.~" siq; $ h .$ p s 3.rc. k Y ?O A*. cd'scx n N ne,=K8.&8c n ,. ~., tau!.E 5.3-40 (Continutd) Itt3TRt!MCt4 TAT 10tt Afin Cor:Tnot.- ESSEt3TT At, ITVAC SEISMIC P! -EVAI.tf AT109 SttPtt APY TADI.t' Method of original System, Structure, Component Quellfication Re-Evaluation Results tvscription Conclusion and Pemarks t Spoetre t Analysis Parotn Test Analysts Itcport i Spectra f Coteparison Margin Peport I of I'i q. I safety
- m,r p a ~ s o c
- gra/w.
T41-00-C-43% t'luor Report RICO-8901-2 for livAC duct mtd. Jaatru-9 0 0 -I.u-e (Dt.Co f i le tio. 1811). ments: pressuno sw & temp. 010 D9-tiargin based upon yleid sensing elements 1811 strens. Tliis corrponent is re qua lif icit. vs T41 components Damper Motor Fluor 89% (Same as Above) 1 Mountisiys for T-4800 Ploncer ~ [ t-157 A L H thru l'l63 A & D Rico 8901-4 119-2174 This equipment is requali-l'ower s Motor wi tti imsitioning X T41-00 fled to the new site relay 132-2799 t ArtCu r.lmi t. 000-0x-epecific earthquake Switcle EA-700 016 Ill i-l'8 8 8 (t ermin.it Ion cats.) Sco Section 5.4 1t 11 -8 t19 (termination cab.) Sco Section 5.4 See Table 5.3-37 }'/ til l -P508 t:5 t l ^ n tat 2.C 5.3-41 INST!ttfMENTAT10?3 AND CONTROI.--DRYWEf.f. COO!.1NG SE1SMIC PE-fNAf.tf ATION SttPMARY TAnf.E Method of Original System, Structure, Cocponent Qualification Re-Evaluation Results twacription . Conclusion and Femarks i Spectra Analysis Parryln Test Analysis' Peport i Spectra f Corap r ison Har< tin Report I of F i el. I Safety I p. This equipment is requali-II21-PJ28% ta al Panet EA67 V fled to the new site 1001-12-7 opecific earttquake D9-1933 k' See Tat:10 5.3-37 Itl l-P8 0 8 insert A502 g ;r - re tim 5.4 n i i -i. 8., i t-m in. io,.
- Y sco Section 5.4 I DS-T41-t
- 060 A, t4325A l'SI:-T 41 -t 3 26 A See Section 5.4 Scismic Design Calculations X
N See Sectim 5.4 w N ff$f' / $N$ &J ./ m;fTCl=?/7729~OOf f g%gfe:n$ am est,nT.& i i i1 ? M P TA. ; 5.3-42 INSTptJMrHTATION AND CONTR0f.--RftR COMPT.EX
- c. i. i.... o til I-P S9 8 A (relay room cab.)
!% se r I pt lon Re-Evaluation Pesults Conclusion and Remarks t Socctra t Analysis Pargin Test Analysis Report i Spectra f Copiparison Maroln Report I of rig. I Safety CV)t* f etSENTS till-t'601 A50! itten SW 74 34 See Table 5.3-37 Ifl 1 -l*6 0 8 0514 EESW (* See Table 5.3-J7 Is t l-P8 0 711510 RifR SW l' See Table 5.3-37 til 1 -P tt 09 A'.01 Diesul ruel & Itl l-1 tf 0'J A50 2 f.u',e og See Table 5.3-37 fr See Talile 5.3-37 til l-t*6 0 2 H 510 EDGSW See Table 5.3-37 i Tt:t*MitaA'rlOH CAttitit'TS !!1 1 -l'!! 2 3 ftfitt SW is t i-l*H 68 Ittift SW EESW It l l -l'8 (i1 Islesel ruel & f.tabe [1 See Section 5.4 4:21-I 350 II.ocal llVAC Control I'.in e l l - talesel Gener.itor Vent 11ation p8 Seo Section 5.4 1821-l*351 (l.oea l IIVAC Control P.in e l l - Diesel Gener.stor Ventilation 34[A See Section 5.4 $ Lid Terminal and Pelay Dox X ITE S&L >100t* Quallfles to the new r.gu l p. tio. R30015001-4 Inporin! EMD- -~
- f:!SMIC DF-EVAf.tIATION S t n'MA ft Y TADf.C Pethod of Original Sy s t tera. Staucture, Component Qualification
- 3...ca t inn niin dated response spectra. TRS 029950 envelopes the new pris.
I2-19-72 S L t. I f1D-0091971 t.M D - t' /, g / h 7
- 1 ev.s t li,n 593*
qq, f y I.. se a d,. .e r t, ca l.i n.,....,, r o,m a, Af/ f(:p s c o.....
- ,i g
A* '~ 'TADt.E 5. ! (Continued 1 t J INSTRt?MCitTATIO!? AND CottTPot.--Rtift COMP!.EX Sl:1 SP1:C Pl> TVAt.t'ATIOli StiettArv Tant.n Hethod of Original System, structure, Comtonent Qualific.ition Re-Evaluation Pepstts Descriptione ) Conclusion and Pemarke 1 Spectra 1 Analysis Pargin Test Analyste Report I spectra 8 Comparison Ptaroin tecport I of Piq. I Safety En9 no t'anol In s t riemen ta t ion X (fyle t. abs S t!. >100t* Instruments qualify to 1 I.oca t t ori litt tt dated EttD-new response spectra. Elevation 590' 5/1/70 029950 T!ts envelopes the new S g t. U"U* I:HD-013060 Etto-001659 g titcual Cencrator Control X Colt Ind. S g t. t#/A See Section 5.4 Console R10-Do-EttD-
- gcf.c wy R7M U7 x4. 'McT"7=W,R py '/S/
& 007 DA-022 1.e.ca t lon pitit (205961) Clacvatlun 617' 7/2/75 hy It21-P517 Auto Temp Cont rol [1# Sco Section 5.4 l'.i nu t - t)(i Ventllation a a, fa tatt f.oa.1 Se prencer X M A/ Sen Section 5.4 Engine overspecil Governor X Colt Ind, StL p "lant Quallfles to the new . I:.in p. No, it 3 0015 n 01 - 4 Report Et!D-fu lOl responso spectra. f.ocatton liitti d.sted 029950 1:l e v.a t i on '290' 1/24/73 S L t. Lt:0-001659 i e For vertic.sl 4 lussirontal il l r ec t l un i l r. n TAULE
- c. gu l p. tso. 10 00S002, 004, 005, S-900-029950
INSTitUMCMTATIOil AND CONTROL--DI!R COMP!,CX SEISH!c let-EVAI.t!Attots E'_.I."!!_N_P_y,lA IH.E 1 Method of Original System, Structure, Comg.opent QualjfJc.stion Re-Evaluation Results TNsceIptibn Conclusion and Pemarks t Spectra 1 Analysis Pargin Test Analysis Report i Spectra 4 Comparison Haroin leegnor t i of Fig. 8 Safety TIM-x 41 -H 056 A (f:DG 811) [t If See Section $.4 i 7tH -X41-If0561: (1:DG 812) Sw i tet:9ea r suoi 1VAC h [# Ttv-x 41-ta 057 A See Section 5.4 TIM-X41-tt057C I:lX Itoom flVAC Jf-See Section 5.4 TIN-x41-t1058A Pun.g. Homa IIVAC (n operatorn (11 r) M N/ S'o Section 5.4 / g Fo r me:.k i n p..n.pe r s /I # c) O t ( 4 e I j TADT.C 5.3-45 i 400 v AC & 260 V oc POTon cor:Tnor,cimT:" t Y Tv.) t SET S*11C DF'-rvA1.trATiry Simrinny TAnr.g Method of Or191nni syeten, Structure, Component Qualification Re-Evalunt.lon Results 1%:neription Conclusion and Pomarks 1 s Spectra t Analynis Parqin Test Analysis Report i Spectra O Comparlson Pfarqin Heport I of I' l y. 4 Safety i Supp1cmois t Selum!c witti X R16003- .h Sco Sectim 5.4 St.snd.st,111 t y Test Itepor t 900-RA-MCC-IA: vices Oct. 8, 1973 003 (1:4 - H - STS - t r> Supp l en. n t 463) Sc i sm i c H i t lis t.....* a '. t t t t y Tent X fil 600 S- )?/ See Section 5.4 ) twt.or t o.: t. 1 73 4"'t r+-STS-16 '3 0 0 - H A-
- 42 (Continusd)
Ity l e I.te it.:pos t i434?2-t 003 iC5-460) i f/ Sci smic Sipiu l.it lun Tout X R16005-See section 5.4 R..por t to Ou.elity the Streic-900-el ture Wolds,.fuly 31, 1979 RA-010 f t-STS - 70 lle v. 1 ( f;5-59 4 ) i lly l e I. f e. Itepos t 8 4 3 tt 01 - 2 6 It l 600 S- { 900-RA-012 (L5-6 607) This component is requali- .4 fled to the new site Seish:lc navnet in9 for HCC X Rl6005-N/A
- )
j Solsmic Mountin<3 of Relays in .X New ff/A i tlio MCC t Y g y $$ &pk /0 !'?.- r. z etAb2/hby,-cy&, O ft A fk /es m u sea m 1 ',-nt< -We suadetim ce!a9<, :- (&&,& m f ogg l i a o i Tant.c 5.3-46 460 V SWITCilGfmit (TTE) SelSHtC nt-tVAt.tfATro!8 StfMM nY TAHf.E Mothod of original sy s t e sa, Structure, Conapone n t Oualification ite-Evaluation Pesul ts Conclusion and Bemarks Descriptton t Spectra 1 Analysis Fargin To t Analysis Report i Spectra 8 Comparinon Margin Dep(3r t I of Fjq. I Safety hO Okt TRS envelopes the Scis.elo Certilleation Report X It14 0 0S- ==- ""
- f. Vv 3pecific carthquake n!nces 900-fiA-9 rcass qualif 007 i
Okt TRS envelopes the p{ C 7.T*I) X Rl400S-Te s t lieg wir t Seismic Stiock It ttS, 600 V Hetal Enclosed Switch-900-01.- tasard aml compement A.D. 001 g3 tr.< p e r t tio. R-8792 .l. Seo Section 5.4 Seismic Certifleatlon Test X R1400S-ag Peport for 750 EV A Voltage 0 3 0 - t' A-001 lacqulators Wyle lat, liciais t 41169-1 i Okt TRS envelopes the Selsnile Simulat ion Test X D14005-gj .= ], Q FtRS. Report Voltage Itequlators 9 0 0- OI.- Wyle f.le fiqan t tio. 42949-1 031 (C5-l 429) Seismic certification ~~y * % (f }.. Sc l emic Cut t l f t. at ion Vol tage-X R1400S-only. rio attachments. 9 0 0 - l.n-Hequ la t o r :s ITE
- Itns, for Class 11: Swy t' Electrical 900-RA-010 (n5-t P, realpment ITE Hepott H-09322 439)
-a-r [ Ok t TRS envelopes the I' tullemen t Clais I X R1400S-Electrical Selsmic Stuack Certification - 9 0 0 -Of.- 1** + 9 W %c4 'b# J Itp 3. s t 027 (C5-150n KVA Transf ue rrwsr Wf e Its 142: L tio. 14-09402 427) D1400S-A.I.leentum to Test tr..iner t it -n9 4 N 9 p ft - RA-007 Ill 4 00$- 0 0 0 -l.ti-0 10 r& S y/ !e qpm y{ %3P i cqzs e nns on awg m. tc c hf/g7%a-7eg!k?f Ac@y.dvs yv~cfN> yA $ /I sn a n m s,, m <;+,whlqh., l i a l l l l s a a u u .kr g q q ee ee e g g rt e rt e e lk lk P y naa aaa l u l, i u d 9 wq wq n t eh t el i a nnt nnt e r e r n mea mea o ph c ph c i l t l t s u c u e u qoi jol a l 9 etf ctf c i t n sdc sdc o s i ee iee .C k hl p hl p 4 O Tf s Tf s n y [ j(a %.( i t ( gf e 1 rof [i .uh a a e s P S 7,, t lu aI f, n l te at I yr l o n ap { o ne i AD Q t a T u n Q l i e a g 1 v 4 r { "g 4 t a i f e ) g R d 1 n e ) f u E f ao 7 n T O rnf I t! i T cr. n t fA E. eat
- a 096
C A T D SmF S e o f t. t ppl ( A A o g t C V T C 6 i E t t 4 C - Y r. T f' R l I D A b 3 3 S C Ff a W r l c t A A S e a I 5_ I C. V l S c / / P f i tn 0 I l p t y A C C a S T 4 S n y-I in t m.i S go f ii rt t sA SA 3A Oa r nH 0H 0f 0 c o 0 - 0 - 0 - [l c fi p 409 4 404 t of e 100 1 l01 Y i R R90 H p90 dloa & %n-[% O hu e tQ l e e M y l X X t + a n l A 3 l Me t
- g t
t e X / e T l y e p-n i W aq,.* ' }s 1> t 4 i n e g gn (q n dy j o nT t t C p a n n z y e y u u e nr o o f C oD M M y 5.O n i l c ,o t9 e i d ei a*f 1 qnR m m rt e! V :s u s h up l tl f 7 l. i W e1 e cr i uc t p1 S S rs t y r o ru h tu uT Sf C m al al { S a n e - e ~ ic1 o gf i t e p i .f m $f ti e mys cl t:i f t t sI n t C itC Y s l J a i y ons wy wy S SAT Sb Sb /I' i t l j 3 a ,e ~ m TAtst.ft 5.. .7 4160 li SWITCllCt:AR (ITC fitPEftIAL) f t!SPt]C !< t:- 1;V AI.t f AT T OS' SI ?>'P % H Y T A fit.E Method of O . tnol Syctsm, Structure, Component Qualificat' - Re-tvaluation Results t>c s e r i pt i on Conclusion and Remarks Spectra t Analysis tdargin Test Analysts Fte po r t I Spectra 4 Cornpa r i son tt.i r a i n Iteport I of riq. I Safety Saisreic Curti fication for X 1t14000-j*d See section 5.4 Class I t: E!cetric.s1 rquip-000-SC- 'S nent ( f'v es e s 6 4 tt, 64C, 6512, 009-E4-6 '. V, 64T, 65T, 11 FA, 12 f:0, 333 I T t; i13-4'!961 [g( Test, itepo r t Seismic Stiock X R14000-See Section 5.4 %V tie t a l C l..it Sw i t elil>oa r d 000-RA- .s n.1 C4,. pone n t s. Wyle I.a ! > 003 R-O's 121 h# See Section 5.4 m Sei smic Wi tins tan t.alal l i t y X R1400S-I Aux i l l.o r y Itc l a y Gl; 0 0 0 -Itn - H 121 rA51 A4 2t* 011 rep.n t tt- 0 9161 -lin This equipment in requall- [_ Se s umic Wi t tistan latilli t y X 7 g fica to tiie new site Ove r - tintle r Vo l t...je Ite l a y specific earttiquake Gt; I 21 AV5 Jt.l A 4 f r. t.< s a t it- 0 9161t V Se l um l e Wi t titt t a ns!,.ts l l i t y X See Section 5.4 Ovescurrent Irelay CR 1 AC51ril 0 4 A ( l'e s IT!; T11-7629 l'r oce.lo r e ) fret => t 1<-09161-AT
- 4 su s
R14000-See Section 5.4 overensrent fiel.sy CE 000-RA-12P.lellAVIA (t cr 1T t: 006 Tl'- 7 t. 2 9 P s e,<..'. ! n r c ) I?. g a s e t it - O'l l (31 - tiK ) "I D ~ L%s O% GG CO-yWL g as ap+,s s, a msa,, .n e TAtst.t 5. 3. s (Continued) 4160 V SWITCt!CT'AR (ITE fitt'Ettt Att ~ SE T *.M IC Pf:-LVAf.tl AT TOP St!Pt1ADY TAfit.E Method of Original System, St<ucture, Component Coalification Re-Evaluetion Results Description Concltision and Renarks Spectra n Analysis t'argin Test Analysis Report I Spectra f Comparison Harqin f(epor t i of I'J g. 8 Safety i S<atselc Withs tandat:111ty X nl4000- { This equipment is requali-2( fled to the new site .Inckout Irelay Elect..) Sultch 000-DA-Type toit Cat. 73030 (l'e r ITE 007
- el se. ele ul ttis t andalilli ty X
R14000- =[ See Section 5.4 ove r c o r r etit Hel.sy GC 000-HA-12IACb6 CIA (l'e r ITE 008 TD-7619 t* oet.f us e) Heport flo. It-0 9161 - AV (13 X ftl4000-see section 3,4 I Scie,mic Wi th at.initatellity J10 H L JII Itelay I TI:-STin 15/ 3 6/ 000-DA- \\ O 11 002 (E4-402) f% .I This equipment is requa'l- @"' '$U.}Qhj 7 fled to the new site .h E g switch ear Mountir9 Seismic X n14005-9 itelwa r t lay Giffels 9 0 0-It A-speci fic earthquake 013 3d {g h ..,l4 M This equipment la requali-i . Swi t et.jua r Sei smi-
- {g g specific carthquake TD-7629 t'rocedos el Report tio. H-09161-tsc Scismie Withstandatellity X
R1400S e. p fica to the new site 1,y Gitfels "A" go specifle earthquake e ~ n Tats. 5.J-48 DATTEftY MA!!4 DC PtJS!! CAUIN!"t*S VDP tlO. EP2-39, 120n SET SHIC hr..!:VAf.tIATIOt* StJP*ttt ftY TA!'t.f: Method of Origina! evatea, Structure, CoePonent Qualification Re-Evaluatjon Pesults tic se r 'I pt ion Conclusion and Pemarks i I Spectra t Analysjs Fargin Test Analysis Ite po r t I Spectra i Comp.irlson Har< tin Itepo r t i of rig. 8 Safety j Main tx' t'une C.ibinet Selsmic X R3200S-t#/A ) Q ~J~ g IMalf ;to 20.9% 0.K. A mathernatical 1 N analysis has been made Itepo r t 900-DA-g 4 011 lLZ a %' * '".- A $ 6 based on naterial and /[ (fabrication as per Dw). V.tG,Y!/*tff ':gsOC,- &l)<*lfiQ h,~,*, ~
- m t i ng X
la requalified to ttm revised responso upectra. 1 IW s OW j T .I J 1 5 1 e i e es P ~ i Tan:.c 9. 3-4 9 ITATTCRIES & IIA 7"T!"ftY RACKS & TflCIft f10tfNT!ttG (C&D) SE T SMIC ft!'- F:V AI.It ATION I SttPMAltY TAftf.M e t l ><nthod of Original System, Structure. Covationen t Quallfication Ito-Evaluation Pesul'.s f Conclusion and Iemarks N se r l pt i ori 1 Spectra E Analysis Pargin Test Analysis Itepo r t. I Spectra l Comparison th Hepor t. I of Fig. I Safety [8 ok. ,, 7 4.% 9 < 9 24 V DC Dattery--Report of X ft3200S-raans quallf selsmic test on 2 ( 3 Deti-9 ) 900-DA-h e a' t critical p l a ts is 1,a t t e r ie s for C&D. 000 lEll-g gW s li.h 15 b!dy, aux. i INI. Report 84807 and report. 84) 0.665 9
- u}',' '
for melsmic test on two 1 ( l.DCit. 3 ) leatteries and one Altit 114 AC 3 t.harger for j C.D. ,zri. n..re. < 152s3 i 130 V tic tlat t ery--Sel smic X ft 3 2003-( Ok. Test response spec-sleulat tosi tout pro. ..m on 9 00 -It a- [ . gTOh hf }g$ " le y tra envelopes tlie re-two YC-Il 1,.ittery cells & 004 (!;11-quired response spectra g l g 4 e one Altit 130 HK100 1.attery 00) (aux, bidq. 643*-6) l M cenar ter wyler tiepos t O I42954-1 i b q ok* fla t t er y racks for 24 V DC X R12005-N/A g C k'2I).g reass quallt l 1,a t t e r i e u -- se l :.m i c a na l y s i s 900-DA-(3rd Floor aux. !>1 dg. ) r f o f C& D l'a t t e r y suppos t. racks 007 (tll- ' (f O i for L lier C & D 18u. 3 OctJ-7 DS) t.atteny fla t t e r y racks for 130 V TX' X 1t 3 200 3-N/A t .Nf ok. 9 g reass gustif w h li' -C;,Sj'T] [
- 1. 5 g.
.,? l.attorles--ueltmic analyols 900-PA-m e. p s e t of KctJ-17 slugle tier 003 (811-I,attory rack 01) CCf. Itcpor t iA-l19-77 I This equipment is requal.".- S.:! r,mic feeport of 24/48 Y X R32-06S-il/A 46 63 17.311 fled to the new alte i g f'. q, ,pgeggge e,trtliquake teatteey ..c k u nin t l e.g 9 0 0-11 A- _.r. ea t.nn t -tr2 -l',9-15 6 011 1 %. p n32-005-N/A M'. fl3-cat-0164) h.,, l 900-i.C- .t (. 182 h! Jh D!$Wl .- Q Q / *y / 2C0/s W / /?'lh f0k-t ,-* [y m TRnfE 5.3-90 ISATTEnY CllAftCf'!tS At3D ?!!Ein MOUNT!?tG (CtD DATT5ft2ES) i Sf: t SMIC_ RE-MVAF.IlAT tot
- ~
Analysis Pargin l Test Analysin Report i Spectra i Correa rl srin Marq1n Hoport i of l' l q. I Safety d 130 V de teat tery charger X R32-00S-report of t.e l snele test on 900-RA-ok two ( 3 - pet t-3 ) t,..tteries and 005 9 9 reass qualif cne At's<i3AC) etsarger and Can (Ell-84) e, j tut ter les ETf. I its trepo t t 93 p
- j StfMMAftY TADf.lj Mothod of Original System, :it ructu re, Component Qualification Pe-Evaluation Ronults Description Conclusion and periarks Spectra t
This equipment is requali-130 V de 1*a t t e r y clea rqo r X R1200S-reismic simulation test pro-900 f tA-fled to the new alte gram on two FC-13 t,attery 006 specific earthquake 7 cell a.id une At*H1 )!!K100 (E11-80) [ 1.tteny ch ruos j t<y l e t.al. t<epos t 342954-1 This equipment is requali- { Id M Setsn.le Clans t ttachment X R3200s-N/A 482 tied to the new alte og,ccific earthquake for 110,V hattery ch.irger 900!!.5 013 e.a==== i 24 V t,.ittery charger and vo l o ne t e r -t:A l - 0 016 ) R32005 9 0 0 !.C-i l 075 ( t'11 - 10 51 '7b 4 /*gij'.%;C& Mg if.t.4 b by ~j 4 Fq 12] / qty ? ' S y 3 % ? *7 y / } L 9 1 j i m Tant.P. >. 3-51 DC l'tJSED DISTntDttflO'8 CAult8ETS (SOUANt: D) VDP 110. EF2-30,121C Sc tSMic 14r-EVAt.t'Atrop St FMAnY Tant.n 9 Method of Original System, Structure, Component QualliJention Pe-Evaluation Itesul t s Descrittlon conclusion and Pemarks t Spectra Analysis Pargin Test Analysle Report i Spectra i Comparison Haroin Itcport i of Fig. I Safety M See Section 5.4 Seinale Ouallrication for a x n32005-Ik 4 250 V f4: OMf1 l'.i n e l noard 900-RA-015 S.ps a r e D D 9 9 8-l o- 09-!.l f,R (17,- 8 7 ) This equlprnent la requall-ficd to the new site Setsmic class I DC D i s t ri tiu-X T51000000-ti/A 52n ,,7 tita P.snel Installation at RA-001 opecific earthquake the..s e t o r tio l l at i ng (E11-128) -D This equipfnent in requall-Scise tc Class ! DC Distrit>u-X R320nS-N/A 43g ===*"" fica to the ne.s alta tjun Panel Inst.illation at 063
- 3 %84I L 15261 a dd[
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