ML20204H182

Rev 0 to C-PENG-CALC-021, Determination of Waterford 3 Hot Leg Seismic Response Spectra & Accelerations for Use in Analyses of Mnsas

ML20204H182
Person / Time
Site:	Waterford
Issue date:	03/10/1999
From:	Doney R, Haslinger K, Colleen Schmidt ABB COMBUSTION ENGINEERING NUCLEAR FUEL (FORMERLY
To:
Shared Package
ML20204H122	List: ML20204H118 ML20204H123 ML20204H140 ML20204H146 ML20204H171 ML20204H182 ML20204H214 ML20204H245 ML20204H251 ML20204H259
References
C-PENG-CALC-021, C-PENG-CALC-021-R0, C-PENG-CALC-21, C-PENG-CALC-21-R, NUDOCS 9903290027
Download: ML20204H182 (17)

Text

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Deenrudandom of Waterfor.13 Bet Lag Sounde Resposee Spectra &

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ABB C-PENG-CALC-021 Rev. 00 Page 2 of 10 RECORD OF REVISIONS Rev Date Pages c h*" # Pmpared By Revirued By Appevd By 00 ' 03/11/99 Original K.H. Haslinger CA Schmidt R.O. Doney l

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ABB C-PENG-CALC-021 Rev. 00 Page 3 of 10 TABLEOF CONTENTS i Section Pane No.

i 1 INTRODUCTION _- .-

__ __4 1.1 Oasenvt .... .. .

1.2 Asstagneprr oFla4 PACT or PLANT DzsacN CHANGES

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.. . . . . . ...... . .4 2 METEODOLOGY a s

3 ANALYSIS .

.6 3.1 ArrucAauRzstoNasSescr A rom WSES-3 Hof Lto..

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.' 3.3 W3ES-3 PIArt Srscanc Arrar ==avuwe poa Her Lao.. ..

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3.4 SaLacTION Of LOcALHoanowrAL ANo YzancAI. Arc =' =a*Tums rom MNSAs . . . . . . . . . . . . .......7 4 RESULT 5 s

j 5 REFERENCES i se

)

j LISTOF FTGURES

E1EEE DESCRIPTION F. AGE 1

, Colhae of WSES-3 Hot Leg Envelope Global OBE Response Spectra 13 t ,

1 j LIST OF APPENDIfTR No. Pages j APPENDIX A-EXCERPTS FROM ABB CENP CORRESPONDENCE PSE-76-153 NOVEMBER 4,1976, RCS ENVELOPE PIPING SPECTRA,

] (REFERENCE $.1 . . . . . . . . . . . . . . ............. .A1-A7

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! APPENDIXB: QUAIlTY ASSURANCE FORMS.

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ABB C-PENG-CALC-021 Rev 00 Page 4 of 10 1 INTRODUCTION i

1.1 06 fee #wr The objective of this calculation is to determine applicable Seismic Response Spectra and Max Acceleration values for use in the analyses of Mechanical Nor21e Seal Assemblies (MNSA) to instaDed on the Hot Leg PDT, RTD and Sampling nozzles at the Waterford Unit 3.

The MNSA is a wh+=1 device that acts as a complete replacement of the "J" weki bem; , an hconel 600 instrument nozzle and the Hot Leg pipe. Its function is to prevent leakage and restrain i

the nozzle from ejectmg in the event of a through-wall crack or weld failure of a nozzle. The

• potential for these events exists due to Primary Water Stress Corrosion Cracking.

This e*hdeion will be incorporated inte a Design Suess Report for the RCS Pipmg.

f.2 Asamneent ofinpoet ofMen Design Changes This report is based on the seismic data from the original RCS analysis which am unaffecte changes in the tributary lines as a result of snubber reduction or any phe support changes RCS analyses typically do not model the tributary lines and, therefore, the RCS piping serves as th of anchor for these tributar; Nnes. Thus there is no impact on the RCS motions due to any ,

modecation to the branch th.u This calcuistion is in sapport of analytical work for the three WSES-3 het leg MNSA designs m

- a =iin wcs.ce with the requirements of the ABB CENP Quahty Procedures Manual QPM-101 (Reference 5.2).

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ABB C-PENG CALC-021 Rev. 00 Page 5 of 10 1-

[ 2 METHODOthGY The objective of this calculation is to document applicable response spectra and acceleration level for the locations of the MNS As to be installed on three types of Waterford Unit 3 Hot Leg nozzles. For this purpose the response spectra for the hot its from the original saamic analysis were retneved.

Rduence 5.11 pis#,,,d nina (9) response spectra for cold les und nine (9) response spectra for hot leg locations for several ABB CENP plass Cross axis spectra ofnegligible amplitude were omitted from the reference Also included were a set of"Overali Envelope" spectra for all pkms A,e A contains copies of the pertinent reference pages, comprised ofcover page and WSES-3 Hot Leg ard Cold Leg spectra.

As stated in the reference, all spectra apply for the OBE event level and are based on 1% ofcntical damping, which is considered conservative for the MNSA design. DBE event level spectra can be obtained by tr.ultiplying the OBE spectra by a factor of 2. . The spectra peaks are unbroadened winch, dependmg upon the specific plant may be either 10% or 15%. However, based on the type of evaluation perforrned herein, broadening of the peaks was not required it is to be noted that the WSES-3 MNSA analyses address the MNSA denga with an intact nozzle J.

weld and after the nozzle has ejected. When the nozzle is still intact, both nossle and MNSA are dynamically independent sad, therefore, there is no change regured to the original nozzle caladmaan Or.ce the nozzle actually ejects, and is restramed by the MNSA retention plate, the two components tend to pair up id r e.icdf. However, since both contribute in erW- , there is no

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reduction in :ritian natural frequencies. I.1 order to d===*rste the functional perfonnance of the j MNSAs (si=%n of full 180 degree crack), the seismic testing of Referer. e 5.10 was perfonned  !

for the SONGS contract. The testag derrexistrated seal leek tightness under very extreme dynanac  !

and interne: pressure conditions (i.e. the pressure boundary was maintanned). The testing also I included a Hot IAg Temperature R'ID MNSA that is quite samlar to that for WSES-3.

The MNSAs prior to nozzle ejectios are evaluated analytically for Nonnal Operstmg and Seismic loads. In addmon to the analyses, the testag serven to demonstrate full compliance of the MNSA as  !

paired with the manima, in that the nozzles saually provide support to the MNSA retention plate and tie rods, and besset from the addirian=1 std!hess.

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ABB C-PENG-CALC-021 Rev. 00 Page 6 of 10 i

3 ANALYSIS l

J.1 4piiceNe Rayense Speconfer FSESJ Net Leg Since the piping speedication of Reference 5.8 does not contain any design G-levels for the piping, the response spectra of Reference 5.11 were retrieved (see Appendix A). Review of the Hot Lag spectra demonstrates that cros axis motions are relatively small and are thus neglected from

' further considerstbn. This leaves only the orthogonal axis spectra in response to "in-axis" excitation. The three axis spectra am summarized in Figure 1, with Y repreocuting the vertical ax '

X representing the tctwie.1 axis paraRet to the hot leg, and Z the horizontal axis perpendzular to the hotleg.

32 LeuentNaasntFrupreney ofhDVSAs in order to establish the applicable acceleration levels one needs to consider the natural frequen the MNSA design and also the profile of the response spectra curves. As to the latter, the WSES-3 3

site speedic Hot-Leg spectra show strong peaks at a relatively low frequency of approxunately 1 Hertz. At higher frequencies the Z and Y spectra level offrapidly to values ranging between 0.1 and

! 0.2 Gs. The X-eals spectnan largely follows a similar t, ed, but does have a narrow,0.55 G peak around 13 Hertz Review of the !! wee MNSA desi i pi features of Reference 5.4 allows the conclusion that the MNSA retention plate, in E-

--9 with the relatively long tic rods, for the Sampling Nozzle design has the lowest natural frequency. It is calculated according to Reference 5.7, Table 8.8, Case No. 2 for a Ch.hwW Mass (Top Plate) with Beam Mass (Tie Rods) contribution, that f = l/ 2r *(L'(M + 0.24M.)]

Where E = 26.8 x 10'pai(at 35&F)- Youngs Moddun I= 0.0025 in*- area momes, afinertaa of(4) tie ro:is L= 13.675 in - length between upper flange and CL top plate V= 2 n/4 x 5.5 x 0.75 = 17.82 in' - vokune of the top plate based on dunensions of Reference 5.4.

W= p V = 0.290 x 17.82 = 5.17 lbs - weight of top plate M= W/g = 0.0134 (Ib sec' Fin- mass of top plate ABB Combustion Engineering Nuclear Power

1 ABB C-PENG-CALC-021 Rev. 00 Page 7 of 10 t4= 4ALvg = 0.0036(Ib sec yan- 2 mass of tie rods p= 0.290 lb/tn' - densi:y for stain! css steel A= 3 ,

0.0878 in , cross sectaonal area of the tie rod. based on basic pitch diameter of 0 3344 in

, g- Gravitational Constant of 386.4 in/sec 3 Substitution of above values yields a ibndamental frequency of 11.82 Hertz. 1 3.3 WSES-3 Piant.%pecyic Aw'- '

- forHetLeg 1

Considering the lowest natural MNSA frequency of 11.82 Hertz in combination with the ici.ponse ,

spectra of Figure 1, the applicable maximum OBE accelegation levels for the 3 global axes are

! determmed conservatively as follows:

HonzontalZ-Axis 0.18 Gs Horizontal X-Axis 0,55 Gs

} Vertical Y-Axis 0.11 Gs I

l Using the RSS Method, the Maximum Spatial Acceleration is3 (0.13 8+ 0.552+0.11 )

which equals 0.589 Gs.

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j Since the three MNSA designs have different circumferential positions on the hot leg pipe, on would have to consider each MNSA location and orientation with respect to the global axes. A

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relatively sunple approach is to assume that the resultant spatial M Mon actually applies t the sam level (use 0.6 Gs) in both local vertical and horizontal axes of each MNSA. Based on past experi j the MNSA designs can tolerate signdicantly larger G-levels, and it is up to the analyst to select appropriately large acceleration values, provided they meet the 0.6 G criterion in both axes (lateral an longitudinal with respect to MNSA nozzle axis).

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4' RESULTS Based on original plant data the subject evaluation demonstratas minimum acceptable OBE event accelerations of 0.6 Gs in both the lateral and the longitudinal axes of all three WSES-3 Hot Leg MNS A

, designs. SSE event accelerations are twice as large as the OBE values.

i For compuison, the seismic qualification program of Reference ',!0 produced Zero Period Acceleration (ZPA) levels of 2.8 and 5.2 Os for the respective OBE and SSE test levels. It is also important to note that the SONGS PZR Nozzle /MNSA tested in Reference 5.10 had a resonance frequency near 28 Hertz, which coincided with an oil column resonance of the seismic simulation fixture C&qWh the response of both the Nozzle and the MNSA retenuon/ tie rod configurations was mut:h lugher than any of the expected WSES-3 seismic responses (Referince 5.9). This fact easily

] offsets any minor differences in MNSA design betw. the SONGS and WSES-3.

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] ' mere are no assumotions la this document that reunire instification.

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ABB C-PENG-CALC-02I Rev. 00 Page 9 of 10 FIGURE 1 Collage ofWSES-3 Het .

'avelope Gobal OBE Response Spectra (1% Damping)

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. '1 C-PENG-CALC-021 Rev. 00 Page 10 of 10 l

5 REFERENCES 5.1. ABB Propect Plan No. C-NOME-IPQP-0263, Rev 00. Waterford Mechamcal Nonle Seal Assembbes (MNSA). l 5.2. ABB Cand=mian EP= ing Nuclear Operations Quahty Procedures Manual QPM-101, Revision 03.

5.3. Drawing D 74470-772-001, Revision 04, "Instnunent Nonles Waterford III Pipmg" 54 MNSA Drawings 5.4.1. E-MNSAWFD-228-001, Revision 02, " Hot 14g RTD Mechancal Nozzle Seal Assembly" 5.4.2. E-MNSAWFD-228-002, Revisen 02, " Hot IAg PDT Machanir=1 Noszie Seal Assenddy "

5.4.3. E-MNSAWFD-228-003, Revision 03, " Hot IAg Sampinig Mechanical Nonis Seal Assembly" 5.5 Not Used.

5.6. Assurican Socnety of Machanir=1 h=i- s Boiler and Pressure Vessel Code,Section III,1989 Rdirinn(No Addenda).

5.7. "Foriaulas for Natural Frequency and Mode Shape," R. D. Blevins, Krieger,1984.

5.8. sp-ar=ian No. 09270-PE 140, Revison 07,"Pmisa Gesel Speedication for Reador Coolant Pips and Pitmags for Esengr Operanons, Inc Waterford Unit 3", December 1993.

5.9. "Noszie Imeds for winch SONGS Bottom Mourned PZR MNSA was Quakied." Mh Number S- l PENGCALC-008, Revision 00.

5.10. " Seismic Q-rd,*ia= cfthe San Onofra Units 2 & 3 MNSA Clamps for Pressuriser heen=nant Nossles and R'ID Hot IAg Nozzles" Test Report No.1R-PENG443, Rev. 00, July 3,1997 (originety was issued as TR PENso33, Rev. 00).

5.11. ABB CENP Co.. ,--' - - --- PSE-76 1f3, "RCS Envelope PM Spama," Novunbar 4,1976.

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C-PENG-CALC-021 Rev. 00

. Page Al of A7 APPENDIX A  ;

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' EXCERPTS FROM ABB CENP CORRESPONDENCE PSE-76-153, NOVEMBER 4,1976, RCS ENVELOPE PIPING SPECTRA, REFERENCE 5.11.

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Intero.. ice Correspondence I TU:

" bD ND$ f T. A. MacNair RCS Envelope Piping Spectre R. P. Kassausra  !

PSE-76 153 cc: D. A. Pect w/o enc 1. Novemer 4,1976

Reference:

(1) IOC T. A. MacNair to D. A. Peck. Seismic Environment of Inlim Equipuent, dated 9-23-76 '

(2) IRC Regulatory Guide 1.122, issued for comments

Enclosure:

(1) 89 Response Spectrum Curws with $wmary Table The purpose of this mens is to transmit to you the sehoic resgense spectre roguested in Reference (1). In general for each plant. g spectra fbr cold leg and 9 for het leg are ymyided except for these spectra whose ordinates are considend negligible as indicated it. Table 1 of Enclosure (1). An "everall ennlope set of spectra is also incleted. The Jersgr Central RC5 seisefe analysis is being redone. The envelopes for Jersey Central are based on estientes from presently available analyses and will be confimed when the twanalysis is completed. The data in Enclosum (1) includes all plants for which such spectra am presently avellable. As additions) data becomes available it will be transmitted to you in similar fom.

!BE spectra can be obtained by multiplying the 00E ordinates by a facter of

2. The enciesed spectra are as calculated and do not include the broadened peak referred to in Ihrference (2). If further questions arise, please I contact me.

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l TR PENG-033 ABB/COMBCSTION ENGINEERING Contract No. 200T.41, Rev.00 Total of Text 47 Pages Ref. T.R. Ns. T5071 A PRIMARY SYSTEMS Appendices 89 Pages Design-Related Testing Checklist Section 3 - TEST REPORT l

Test Report Seismic Qualification of the San Onofre MNSA Clamps for Document

Title:

Pressurizer instrument Noules and RTD Hot Leg Noules I Document Number: TR PENG-033 Revision: 00 Yes N/A 1 Is the test putpose stated? F 2 Are the test prt,h listed! [

3 Are the test results listed? Y 4 Is the test request document number included on the test report cover page? 7 .

5 Has the test report been signed and dated by the authot'l 2 -- -

j 6 Has provision been made for approval by the manager of the resung orgamzanon? @

7 Has provision been made for a statement of aarptanz by the Cogmzant Fagiw! I Comments / Remarks:

==

v Revzwed by.

y Frank V. Rossano f7[,i/,.7 sisuse-

/ Da i% e mm.

Page 2 of 47

TR-PENG-033 ABB/ COMBUSTION ENGINEERING Contract No. 2007:41 Rev.00 Totaicf Text 47 Pages l Ref. T.R. Nr. TS071 A PRIMARY SYSTEMS Appe: dices 89 Pages RECORD OF REVISIONS l

NO. DATE PAGES INVOLVED PREPARED BY APPROVALS 0 07/ 03/97 All K. H. Haslinger F. V. Rossano P. Leombruni K. Margotta

/

l I

I Page 3 of 47 l

,i, TR PENG-033 ABB/ COMBUSTION EhGINEERING Contract Ns. 20en41 Rev.00 Total cf Text 47 Pages Ref. T.R. No. TS07t A PRIMARY SYSTEMS Appendices 89 Pages i

l l l

l I

The information contained in this Report No. TR-PENG433, Rev. 00 has been reviewed and approved as documented herein.

i i Approved By: h/bheN  % PL Date: 7 b/17 '

V Manager, Primary Systems I

• l l

I I

The tests described in this report are accepted as meeting the objectives and instrucuons described in the referenced test request / test procedures.

Accepted By: MNMMMM a M -

Date: 7/M[7 Cognizant Enginee- **

4 I

l l

4 Page 4 of 47 i

l l

' TR PENG-033 Contract No. 2007241 1-ABB/ COMBUSTION ENGINEERING Rev.00 Totatof Text 47 Pages Ref. T.R. NA TS071 A PRIMARY SYSTEMS Apperdices 89 Pages TABLE OF CONTENTS l

Section Description Page No.

TABLE OF CONTENTS S LIST OF TABLES 6 i LIST OF FIGURES 6 1

LIST OF APPENDICES 8 )

1.0 INTRODUCTION

9 2.0 OBJECTIVE 9 3.0

SUMMARY

9 4.0 TEST DESCRIPTION 11 ,

4.1 Test Specimens and Mounting 11 - -

4.2 Equipment and Instrumentation 12

]

l 4.3 Calibrations 13 l 4.4 Sine Sweep Test Procedure 13 4.5 Simulation of Seismic Environment 13 5.0 DISCJSSION 14 5.1 General 14 5.2 Sine Sweep Testing 15 5.3 Seismic Qualification Testing A* 15

1. 17 6.0 RECORD RETENTION

7.0 REFERENCES

17 l

l Page 5 of 47

TR PENG-033 ABT/COMBL'STION ENGINEERINb Contract No. 2007241 Rev.00 Total of Text 47 Pages R:f. T.R. Ns. TS071 A PRIMARY SYSTEMS Appendices 89 Pages

~

LIST OF TABLES Table No. Description Page No.

1 EQUIPMENT AND INSTRUMENTATION 19 2 TEST M ATRIX. OFF-LINE AN ALYSIS 20 AND DATA FILE IDENTIFICATION 3 REQUIRED RESPONSE SPECTRUM LEVELS 21 AT 1/6th OCTAVE ANALYSIS FREQUENCIES LIST OF FIGURES Figure No. Description Paac No. ~ ~

i REQUIRED RESPONSE SPECTRA 22 2 REPRESENTATIVE MNSA CLAMP DETAILS 23 3 REPRESENTATIVE TEST FIXTURE AND MOUNTING 24 DETAILS 4 HYDRAULIC VIBRATION TEST FACILITY 25 5 HOT LEG RTD AND PZR SIDE MOUNTED NOZZLES 26 WITH MNSAs DURING SEISMIC TEST Aw 6 PZR SIDE MOUNTED NOZZLE SEISMIC TEST SET-UP, 27 7 VIEW OF PRESSURE GAUGES AND HAND PUMP 27 8 HOT LEG RTD NOZZLE WITH MNSA, 28 SEISMIC TEST SET-UP 9 HOT LEG RTD NOZZLE WITH MNSA, VERTICAL & 28 HORIZONTAL RESPONSE ACCELEROMETER 10- BOTTOM MOUNTED INSTRUMENTED NOZZLE WITH 29 MNSA, FREE STANDING 11 BOITOM MOUNTED INSTRUMENTED NOZZLE WITH 29 MNSA, SUPPORTED Page 6 of 47

TR-PENG 433 ABB/ COMBUSTION ENGINEERING Contract No. 2007241 (

Rev.00 TotaLcf Text 47 Pages R:f. T.R. Ns. TS071 A PRIMARY SYSTEMS Appendices 89 Pages LIST OF FIGURES Figure No. Description Page No.

12 BOTTOM MOUNTED INSTRUMENTED NOZZLE WITH 30 MNSA RESPONSE ACCELEROMETER MOUNTING BLOCK AT VALVE MASS TOP 13 BOTTOM MOUNTED INSTRUMENTED NOZZLE WITH 30 MNSA, RESPONSE ACCELEROMETER AT NOZZLE TOP AND TOP MNSA PLATE 14 DVCS INPUT PARAMETERS FOR SINE SWEEP 31 RESONANCE SURVEYS USING SN21T VERSION 04 15 TRANSFER FUNCTION PLOTS, PRESSURIZER- 32 TEMPERATURE NOZZLE, TEST ORIENTATION A 16 TRANSFER FUNCTION PLOTS, PRESSURIZER 33 -

LOWER LEVEL INSTRUMENTATION NOZZLE, , ,

TEST ORIENTATION A, FREE STANDING 17 TRANSFER FUNCTION PLOTS, PRESSURIZER 34 ,

LOWER LEVEL INSTRUMENTATION NOZZLE, TEST ORIENTATION D, FREE STANDING 18 TRANSFER FUNCTION PLOTS, PRESSURIZER 35 LOWER LEVEL INSTRUMENTATION NOZZLE, TEST ORIENTATION A, SUPPORTED 19 TRANSFER FUNCTION PLOTS, PRESSURIZER 36 LOWER LEVEL INSTRUMENTATION NOZZLE, TEST ORIENTATION D, SUPPORTED 20 TRANSFER FUNCTION PLOTS, HOT LEG 37 i TEMPERATURE RTD NOZZLE, TEST ORIENTATION A #

21 DVCS INPUT PARAMETERS FOR OBE AND 38 l SSE TEST EVENTS 22 TEST ORIENTATIONS FOR SEISMIC QUALIFICATION 39 TEST i i

23 HORIZONTAL CONTROL ACCELEROMETER TIME 40 HISTORY, TEST ORIENTATION A, OBE EVENT NO. 5 VERTICAL CONTROL ACCELEROMETER TIME 41 l 24

' HISTORY, TEST ORIENTATION A, OBE EVENT NO. 5

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TR-PENG-033 Contre,ct No. 27241 i ABB/ COMBUSTION ENGINEERING Rev.06 Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages

~ ~

LIST OF FIGURES Figure No. Description Page No.

25 HORIZONTAL CONTROL ACCELEROMETER TRS & RRS, 42 1

TEST ORIENTATION A. OBE EVENT NO. 5 i 26 VERTICAL CONTROL ACCELEROMETER TRS & RRS, 43 i TEST ORIENTATION A. OBE EVENT NO. 5 27 -

HORIZONTAL CONTROL ACCELEROMETER TIME 44 HISTORY, TEST ORIENTATION A, SSE EVENT j

28 VERTICAL CONTROL ACCELEROMETER TIME 45 HISTORY, TEST ORIENTATION A, SSE EVENT

< 29 HORIZONTAL CONTROL ACCELEROMETER TRS 46

& RRS TEST ORIENTATION A, SSE EVENT 30 VERTICAL CONTROL ACCELEROMETER TRS 47

& RRS TEST ORIENTATION A. SSE EVENT LIST OF APPENDICES Appendix Description Prze No.

A DATA SHEETS AND LOG SHEETS Al- All B 1 VOLT PEAK SIGNAL CALIBRATION, OFF-LINE S t - B3 ANALYSIS SYSTEM nw C CALIBRATION RECORDS C1 C14 D OFF-LINE ANALYSIS -RESULTS D1 - D61 GRAPHS & TABULATIONS Page 8 of 47

TR-PENG-04 AdB/ COMBUSTION EN6tNEERIkG Contract No. 2007241 }

Rev 00 Tota!.cf Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages 1,0 INTROD CTION The Testing Services Group of the Primary Systems Department of ABB/CENO had been requested to perform a seismic qualification test on three specimens of MNSA Clamps with simulated cracks for the San Onofre Nuclear Power Plant. Reference 1, which incorporates ,

the I:quirements, was the controlling document for the seismic qualification program. Testing was to demonstrate that the components could meet or exceed their specitied performance characteristic when subjected to the stipulated seismic events. This report documents the seismic environments that were generated during this program and reports the leak resistance l performances of the specimens. l l

l These tests were performed in the Dynamic Test Facility at ABB/ Combustion Engineering, i Windsor CT, from June 10,1997 through June 18, 1997.

The Quality Class I subject test program was conducted in compliance with Quality Assurance guidelines of QPM-101, QP 3.6 (Reference 13) as Design Verificcion per requirements of the*

Test Request (Reference 1) and the Project Plan (Reference 211. The t: sting was performed by -- -

personnel qualified for this work per Reference 19.

2.0 OBJECTIVE I

I The cbjective of this seismic test was to demonstrate that the San Onofre Passurizer and Hot Leg MNSA nozzle assemblies, with simulated 180* cracks, can maintain thei; physical and functional integrity during and following exposure to a Safe Shutdown Earthquake (SSE) preceded by five Operating Basis Earthquakes (OBEs).

.w 3.0

SUMMARY

f Represensative samples of the San Onofre MNSA designs, in conjunction with simulations of the Pressurust (PZR) Temperature Nozzle, the Pressurizer Lower Level Instrumentation Nozzle, and the Hot les T-.pe.-e RTD Nozzle, all with simulated 180* cracks, were provided by ABB/FSME for sensimc qualification testmg. These components were tested as mounted in special fixtures that were provided by ABB/FSME and assembled specifically for the seismic test by ABB/CENO.

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contract No. 200724t i i TR.PENG-033 ABB/ COMBUSTION ENGINEERING Rsv. 00 Totascf Text 47 Pages R:f. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages i

Exploratory low level sine sweep tests. conducted prior to seismic qualificanon testmg.

demonstrated that two of the three test assemblies. as mounted on the seismic simulator. were ngid within the seismic frequency range (1 to 33 Hertz). The free-standing Bottom Mounted PZR Instrumentauon Nozzle with MNSA exhibited a nozzle resonance at 33 Hertz and a MNSA structure resonance at 38 Hertz. The sine sweep transfer functions are shown in Figures 16 and 17 To ave" smecessary conservatism due to a seismic table resonance. the Bottom Mounted PZR Instrue m.auon Nozzle was first tested in a supported fashion. With regards to the MNSA qualification. tius was detemuned to be acceptable (Section 51). There were no entical fixture resonances below 50 Hertz with excepuon of the MNSA resonance at 38 Hertz.. The sme sweep transfer funcuons for the supported nozzle test configurauon are shown in Figures 18 and 19.

Biaxial (vertical and horizontal) seismic base excitations were introduced to the test specunens in either one or in four test orientations to ensure the possibility of the test specimens to respond in all of their horizontal, vertical or torsional vibration modes. if any, located within the seismic

, frequency range. Qualification was caadmad usmg modified Genenc Floor Test curves that enveloped both sets of Plant Specific curves.

P Artificial seismic time histones were synthesized with random multifrequency in*=**== that enveloped the stipulated OBE and SSE Required Response Spectra (RRS) curves of Figure 1. 'Ihe.-

leakage gdvsn.iu of all specimens was monitored after each event simulanon There were no observed leaks. Coa.quently, the test specunens provided are -Hhd ot the seismic intensity .,

levels represented by the speci6ed seismic curves. Typical Time Histones and the resulting Test Response Spectra (TRS) are shown in Figures 23 through 30. A more comprehensive set of

results is included in Appendix D. The Bottom Mounted PZR instrumentation Nozzle with MNSA was tested first in the supported configuration and then in the free standing configuranon Because

. . of the seismic table resonance being near the nozzle resonance, the latter configuration was a very conservauve test. Nevertheless the specimen was capable of wi@= ding these strong seisnue responses without damage or loss of pressure.

All horizontal and verucal control and response accelerometer time histones were stored on j j magnenc tape and were sinultaneously acquired by a PC-based Data Acquisition SS The l data were xt 9 analyzed off-line at 1% damping. These results are presentedsmi Appendix l l

D. For the Bee stamhng Bottom Mounted PZR Instrumentauon specimen, hormar=1 Top Nozzle and MNSA Top Plase time lustory and respotsse spectra wert also generated and are prtmded in Appendet D for the four SSE level events. On-line spectrum analysis plots are not included in this report because of the narrower (1 to 50 Hertz) analysis range. 'Ibey are, however, retamed as raw data.

i

'!he physu:al meegnty of the three specimen types was ven6ed throughout the sensemc testag No damage was observed at any time, as uxhcated on the data sheets of App =div A. Leak j Md vE = cvaluanons were performed by ABB/CENO test personnel before and after each

seiseme event.

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TR-PENG 033 ABBlCOMEUST10N ENGINEERING Contract Ns. 2007241 I i Rev.00 Total.cf Text 47 Pags

. Ref. T.R. No. TS071 A . PRIMARY SYSTEMS Appendices 89 Pages J

N 4.0 TEST DESCRIPTION 4.1 Test Speri== and Mounting I

One test specimen each was provided for the three test nozzle configurations with MNSA clamps. The drawings of References 2 through 4 and 14 provide details of the MNSA clamps.

Reference 15 provides details et the test fixtures. Each MNSA clamp was assembled using the appropriate procedure of Reference 16 using cl!brated torque wrenches. Minor adjustments were made to two of the seals which are reflectcJ in the final sets of drawings and assembly procedure. Ohe of these adjustments was the use of a spacer between the comparison collar and grafoil seal of the Bottom Mounted PZR Nozzle scal, nis resulted in a drawing change, but did not affect the validity of the seismic test. The speman were furnished already with l weights that simulated the RTD heads and/or the valve that are present in the field installation.

Each nozzle was inserted into an appropriately sized socket and a 180' crack was simulated by seal welding only a 180' arc rather than the entire 360' circumference. De bore below the nozzle was plugged and the top of each test nozzle was lurnished with appropriam fittags to

< allow for internal pressurization during testing. De simulated piping or pressuriser wall pieces were welded onto 16x16xl inch base plates that accommodated the bolting panern of the. j i

~ '

seismic test table and permitted simple rotating of the test specimen in 90* increments. De

Bottom Mounted PZR Instrumentation Nozzle was supported near its top using a Unistrut/PlateT '

l support structure. This support did not affect the MNSA, which was free to move. His specimen was subsequently also tested without this support. -

Small diameter tubing was connected to a hand pump and to shut-off valves / pressure gauges to permit monitoring of internal pressures. The gauges and hand pump were located off the  !

seismic table, using generous loops in the pressure tubing, in order to accommodate large relative table movements. Specimens were inspected for any physical defects prior to test, I after each seismic event, and following completion of all qualification sequences. No damage l 1

was observed throughout this entire test program.

Ab w Symmetry of the test fixture bolting pattern allowed for simple re-onentation of the test fixture / specimen assemblies in any of the four required test orientations. De lodoon of the test fixate was near the center of the table, in close proximity to the verucal and horizontal control acceleroinesers. Sine sweep testing was performed to determine the rigidity of the test fixareswithin the enembd seismic range of 1-50 Hertz. Photographic documentation of the mer*anW setup is provided in Figures 5 through 13. Several figures show the piarament of the response accelerometers during the sine sweep tesung.

d l '

Page 11 of 47 4

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i TR-PENG433 ABB/ COMBUSTION ENGLNL.ERING contract No. 2007241 l Rev. 00 Total of Ten 47 Pages Ref. T.R. Ns. TS071 A PRIMARY SYSTEMS Appeidices 89 Pages 4.2 Equipment and Instrweentation Seismic testing was performed in the Dynamic Test Facility using the seismic simulation shaker table. Figure 4 shows a block diagram of the general instrumentation hookup of the hydraulic test facility that was used in this test.

The excitation axis of the simulator is inclined at 45 degrees and, therefore, provides pluse coherent motions of equal magnitudes in the vettical axis and in one horizontal axis. Two control accelerometers (Unholtz-Dickie 100 PA), mounted to the seismic table in a mutually perpendicular arrangement adjacent to the test fixture, were used to monitor the excitation levels in the horizontal and vertical axes during all testing. The control accelerometer signals were conditioned by Unholtz Dickie 2216X Signal Conditioners. The horizontal and vertical I

response accelerometers (Unholtz-Dickie 75D21PA) used during sine sweep and seismic testing were mounted on standard aluminum fixtunng blocks that were glued to selected equipment locations. Unholtz-Dickie D22H charge amplifiers were used to condition the response aculerometer signals. l l

For sine sweep testing, the "SN21T Version 04" software package (Reference 7) of the Digital .~ ~

Vibration Control and Analysis System (DVCA) was employed. The input listing fbr this program is shown as Figure 14. For synthesis and on-line analysis of the table motions of the ,

generated seismic environments, the "WAE 3.0 Decade" software package of the DVCA was used. The permanent file identification of this code is WAEOVI.TSL, and the synthesized SRS on-line analysis function has been Q.A. verified by Reference 8. The input listings for this program are shown as Figum 21.

For each seismic event simulation, on-line analysis was performed for the horizontal motion of the table. These data were used to assure envelopment of the Required Response Spactra (RRS) by the achieved Test Response Spectra (TRS). For this qualificanon effort, the event duration was 32 semnds, yielding on-line test response spectra from 1 to 50 Hertz. Time history recordings of the table motions were used to verify adequacy of achieved 1MPhnod Acce!cration (ZPA) levels. p in addition to peribrains on-line response spectrum analyses of the horizontal metrol ameteromener signals (at the specified damping of 1%), horizontal and vertical control accelerometer signals, and fbr selected evens also up to two response accelerometers, were recorded by a magnetic tape recorder (Racal Store 7DS). In addition, a P.C. based computer program was used to acquire table time hisaory records and to perform off-line analyses (1-100 Hertz range) from these recorded motions using the "SRSKHH" program of Reference 11.

The referenced off-line analysis program was used to compum SRS analyses at the specified damping of 1 % and to display the results in both graphical and tabular form (see Appendix D).

Page 12 of 47

L TR-PENG-033 ABB/ COMBUSTION ENGINEERING Connact No. 2007241 j Rev.00 Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages A list of all equipment used during this test program is given in Table 1.

1 4.3 Calibrations  !

Calibrations were required for the accelerometers, the signal conditioners, the charge amplifiers, the multimeter, the pressure gauges, and the torque wrenches. Required calibrations were accomplished in accordance with the guidelines of Reference 11. A signal calibration was' performed on the tape recorder, using the multimeter and a signal source, as well as the full range calibration signals from the charge amplifiers. A colt input signal checit was used to verify the

• Hands +ff" autocalibration of the P.C. based data acquisition system. Time records of these signal calibrations are included in Appendix B. Table I lists accuractes and calibration dates of all equipment. Copies of pertinent calibration records are I included in Appendix C. .

4.4 Sine Sweep Test Procedure Sine sweep resonance surveys were performed in either one or in two test Orientations A and .,

B with response accelerometers mounted near the top of each test sper=aa For the two axis symmetric nozzle specimens testing was limited to Orientanon A only. Orientations are i defined in Figure 22. Additional details are illustrated in the photographic records of Figures (

5 through 13.

l During resonance surveys, the specimens were excited over a frequency range of 1 to 50 Hertz at a sweep rate of 0.83 octaves per minute (0.25 decades per minute). The test intensity ranged between 0.1 and 0.2 Gs (a ramp from 0.1 G at i Hertz to 0.2 G at 2 Hertz and a constant 0.2 G above 2 Hertz). Several test runs were made using a constant 0.1 G excitation level over the same frequency range. Data runs were displayed on the CRT teruftdPth the l form of tm:.h function graphs (borizontal response over horizontal input or vertip response over verdcalinput) and hard copies were made. Results of these surveys are shown in Figures 15 through 20.

4.5  %=dania= etSeismic Environment Seismic qualification was performed in accordance with the documented Modified Generic Response spectra that enveloped the two sets Plant Specific requirements. The test g-i==s were subjected to a minimum of five consecutive OBE level events in either one or in each of l

the fbur orthogonal test orientations, as specified in Reference 18. For the two axis symmetric Page 13 of 47 l

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'l TR-PENG-033 ABB/ COMBUSTION ENGINEERING Contract No. 2007241 Rev.00. Total of Text 41 Pages Ref. T.R. Ns. TS071 A PRIMARY SYSTEMS Appendices 89 Pages l

i l

l nozzle specimens testing was limited to Orientation A only. This was followed by one SSE level event in each test orientation. For each event, on-line monitoring of the horizontal  ;

i control accelerometer was performed and results were evaluated to ensure that clear i envelopment of the Required Response Spectra (RRS) had been achieved. In addition, for each  ;

ew.nt. the outputs from both the horizontal and the vertical control accelerometers were l recorded on magnetic tape and stored via the P.C. based Data Acquisition System.

l During the seismic events, the test specimens were pressurized to 3.175 f 50 psig.  :

Monitoring of the test pressures was performed by ABB/CENO personnel before and after the seismic event. ,

5.0 DISCUSSION l 5.1 General 4

At the time of testing, it was decided to test the Hot Leg RTD Nozzle and the Side Mounted PZR Nozzle together but separate from the Bottom Mounted PZR Instrument Nozzle. This decision ~

was based on the fact that the first two nozzles are symmetnc about the verocal axis, and thus' needed to be tested only in one orientauon on the seismic table. Furthermore, the Bottom Mounted PZR Instrument Nozzle required some special attenoon to deal with the fact the the nozzle ,

resonance of about 33 Hertz coincided with the oil column resonance of the seismic table. Since the Bottom Mounted PZR Instrumentauon Nozzle had already been seisrmcally T-unad by analysis in Reference 20. emphasis was at first placed on removing unansamy conservatism in qualifying the MNSA seal. Whereas the seismic SSE response spectrum miensity level for the pressurizer near the nozzle frequency of 33 Hertz was determmed from Reference 18, Figure A-17 as approxunately 4.8 Gs, the table resonance situanon would have increased this level to approxunately 35 Gs. Since the pnmary objective of this test was to quahfy the MNSA seal, it was jusufiable to suffe' n the nozzle and to shift its natural frequency away from the table resonance peak, as long as it could be demonstrated that the Zero Period Acceleracon (ZPA) level of the actual test monon is greater than the Required Response Spect:nm level at the natural frequency of the nozzle with MNSA. AW to Appendsx A of Reference 18, respective OBEtul SSE requirements at a frequency cf 93 Hertz are 2.4 Gs a'mi 4.6 Gs. As is demonspated by the respones spectra and time hk 4 as enclosed in this repott, aclueved ZPA levels for OBE and SSE eveens typically exceeded respective k.wels of 2.6 and 5.1 Gs, wtuch met the stated i.i.--.; for this task it should be noted here that tnese ZPA levels are obtamed from the time histones and that the spessnan levels shown in the Test Response Spectra actually =rlice higher levels up to 100 Hertz.

Since testag of the Bottom Manarad PZR Instrument Nozzle with support was -_--A>I. it was decided to also test this specimen in the free-standag configuracon- This resulted in a very conservative, second seisnue qualine=ria= test for this span === Maxunen G levels of appr=% 20 Gs were monitored near the nozzle top. However, the test specunen was shown Page 14 of 47

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! TR.PE.NG-033 - AB8/ COMBUSTION ENGINEERING contract No. wivi j j  ! Rev.00 Total of Text 47 Pages Ref. T.R. NA TS071 A . PRIMARY SYSTEMS Appendices 89 Pages l

able to accept even these extremely conservatne input motions without any loss of pressure or l physical integnty.

4 5.2 Sine Sweep Testing i

i The transfer functions from the sine sweep surveys. which are shown in Figures 15 through

20. allow the following conclusions:

i 4 - The Side Mounted PZR Nozzle and the Hot 1.cg RTD Nozzle, both with MNSA seal 4

installed. showed no horizontal or vertical resonances within the frequency sweep range of I-50 Hertz. There was some motion amplification towards 50 Hertz in the i horizonut monitoring directions which would indicate resonances somewhere between j 60 and 80 Hertz.

t 1

i

- The unsupported Bottom Mounted PZR Instrumentation Nozzle with MNSA .

! demonstrated a significant nozzle resonance peak near 33 Hertz and a MNSA structural ,. ,

i resonance near 38 Hertz, as shown in Figures 16 and 17. As discussed above, it was decided to support the top of the nozzle and, thereby, forcing an upwards shift of the natural frequency of the nozzle. 'Ihis was achieved successfully, as seen by the sine sweep plots of Figures 18 and 19. The sine sweep plots included in these figures show the response behavior of the nouje and the MNSA hold-down plate in the horizontal direction and of the asymmetric valve simulation in both horizontal and verocal directions. Due to non-symnictry, sine sweep testing for this specimen was performed in two orientations. Seinnic qualification of the MNSA seal for the Bottom Mounted PZR Instrumentauon Nozzle was performed at first in the supported configuration followed by testing in the free-standing configuration.

s 5.3 Seismic Q- "'% Testing ,,

/

As mentioned previously, OBE and SSE motion syntheses were performed using the Required Respones Spectra (RRS) curves shown in Figure 1. Documentation of the adequacy of the componens fbr these requirements is based in this document on the results from the off-line analyses. On-line analyses were also performed during the course of the testing to assure envelopinent of the RRS curves by the achieved Test Response Spectra (TRS). The on-line analyses results are not included in this report. However, they are being retained as ra'T data.

Figures 23 through 26 show the waveform time histories and the ruulting off-line analysis outputs for a typical OBE event (Orientation A) for the MNSA clamp seismic imensity requirements. Figures 27 through 30 provide the same complement of results, however this Page 15 of 47

1 TR PENG433 ' ABB COMBL STK)N E GINT.ERING Contract . 20er i i Rev.00 Total of Text 47 Pays Ref. T.R. N:. TS071 A PRIMARY SYSTEMS Appendices 89 Pays j l

time for a typical SSE event (Orientation A). as can be observed, the Required Response Spectra are always cleanly enveloped by the control accelerometer Test Response Spectra in both the vertical and horizontal directions.

Appendix D contains all pertinent off-line analyses, performed for the two control accelerometers. For the Hot Leg RTD and the PZR Side Mounted nozzle specimens, all five OBE events and the SSE event are included. For the Bottom Mounted PZR Instrument Nozzle, one OBE and one SSE event analyses are included for each test orientation of both the supported and the free-standing test coralgurations. There were no requirements to analyze any response accelerometer locations, however the horizontal MNSA hold-down plate and nozzle top motions were evaluated for the Bottom Mounted PZR Instrument Nozzle in the free-standing test configuration.

In viewing the previously mentioned time histories, the top portion always represents the "as digitized" signal, sampled at 1,000 Hertz. The bouom portion represent the same trace, however digitally RC low-pass filtered at 100 Hertz. This measure enables visual determination of the signal content within the analysis frequency range of 1 to 100 Hertz. The filtered time histories are the bases for the off-line analysis results. The unfiltered trams are usable for determination of actual Zero Period Acceleration (ZPA) levels. During respective. .

OBE and SSE event simulations, ZPA levels in the horizontal direction were approxunately 2.7 Gs (Figure 23) and 5.5 Gs (Figure 27). In the vertical direction, respective OBE and SSE event ZPA levels were 2.3 Gs (Figure 24) and 5.1 Gs (Figure 28). Specified ZPA levels, per Figure 1, were 1.5 Gs and 3.0 Gs for OBE and SSE events, respectively.

Table 3 identifies the required response spectrum levels for the 1/6th octave spaced off-line analysis frequencies. This information may be helpful in evaluating any of the tabulated spectrum results. Furthermore, Table 2 identifies the test runs and the data analysis file names. This facilitates cross referencing between the log sheets contained in Appendix A, the Table 2 test matrix, and the attached graphical and tabulated spectrum resulu included as Appendias D.

e *-

The spectral data are moody self explanatory and any observed "pealung" phenom /

enaevident in the TRSes are confined to the table resonance peak near 30 Hertz. There are some higher order ftequency peaks, however, with regard to the qualification in general, these am considered irtelevant. The response spectra for the hold-down plate and the top nozzle (Bonomt Moussed PZR Instrument Nozzle) reflect the respective natural frequencies of the MNSA and the test nozzle.

In summary it is stated that the requirements for envelopment of both horizontal and verucal RRSs by the TRSs were mes during all seismic event simulations (20 OBEs and 4 SSEs for Bonom Mounted PZR instrumenemnnn Nozzle each for the supported and the free-standing test Page 16 of 47

TR-PENG-033 ABB/ COMBUSTION ENGbEERING Contract No. 200724 Rev.00 Total,of Text 47 Pages Ref, T.R. Nr. TS071 A PRIMARY SYSTEMS Appendices 89 Pages configurations and 5 OBEs and i SSE for Hot Leg RTD and Side Mounted PZR Nozzles, all with MNSA clamps installed) documented herein for each of the specified sets of seismic requirements.

Since the selected, modified Generic Floor RRS curves completely enveloped those for the specific plant locations, the test specimens have been demonstrated to exceed all stipulated seismic requirements. With regard to the development / justification of the Test Response Spectrum requirements, one is referred to Appendix A of the applicable Test Procedure, Reference 18. Since, in addition, there was no observance of leaks or significant pressure drops in any one of the three test specimens, it is concluded that the seismic qualification test described has demonstrated full compliance with all acceptance criteria for the MNSA clamps, as stipulated in Reference 18.

6.0 RECORD RETENTION Test records, raw data and original data sheets were assembled and transmined to the Prunary*

Systems (Testing Services Group) custodian of original raw data for storage. All perunent test.. .

records are included in the test report. Magnetic tape recordings of test data are stored in the' Seismic Laboratory for a minimum of five (5) years. There is no need to store the digital files "

since they can be regenerated from the analog tape recordings. The calibration records for instruments used to record test data are stored in accordance with the laboratory procedure of Reference 10. Copies of pertinent calibration records are included in Appendix C. Copies of the original test procedure and test report will be stored in the Primary Systems (Testing Services Group) ales for a minimum of five (5) years. Q.A. Record Storage of the subject document is the responsibility of ABB-CENO/FSME.

7.0 REFERENCES

m

1. Test Reques't TS071 A, Supplement 00.

2. ABB C-E Drawing E-MNSA-228-001, Rev 02, " Bottom Pressurizer Mehaiemi Nozzle Seal Assembly *.

3. ABB C-E Drawing E-MNSA-2284r2, Rev. 02, " Side Pressurizer RTD M~haN Nozzle Seal Assembly".

4. ABB C-E Drawing E-MNSA-228-003, Rev. 02, " Hot Leg RTD Mechanical Nozzle Scal Assembly".

5. IEEE Std. 323-1974 & 1983, " General Guide for Qualifying Class IE Equipment for Nuclear Power C-==g Stations."

i

~

Page 17 of 47

TR-PENG-033 ABB/ COMBUSTION ENGINEERING contract No. 2007241 i Rev.00 Total.cf Text 47 Pages Ref T.R. N:. TS071 A PRIMARY SYSTEMS Appezdices 89 Pages

6. IEEE Std. 344-1974 & 1987. -Recommended Practices for Seismic Qualification of Class IE Equipment for Nuclear Power Generating Stations.-

7 C-E Analysis Report No. S669-100, Rev. 01. "Q.A. Verification of Time / Data Sinusoidal Vibration Control Code Version 04". issued April 11,1985.

8. C-E Analysis Report No. S863-113. "Q.A. Verification 3.0 Decade Wave Synthesized SRS Analysis Program. Vibration Control System", issued May 2,1979.

9. C E Analysis Report No. SE90-125. Rev. 02. "Q.A. Verification of C-E SRS Analysis Modification", issued April 11, 1985.

10. MISC-PENG-IPQP-007, Rev. 01, " Quality Program Plan for the Control and Calibration of Measuring and Test Equipment"

11. C-E Analysis Report No. 00000-ESE-76D-224. Rev. 01, "Q.A. Verification of Computer Program SRSKHH used for Shock Response Spectrum Analyses", issued November 2,1993.

12. S-NOME-WTR-0007. Rev. 00, " Test Requirements for the San Onofre MNSA Clamp for Pressurizer Instrument Nozzles and RTD Hot 1.zg Nozzles"

13. QPM-101, Rev. 01. .

14. ABB C-E Drawing E-MNSA-228-004, Rev. 02, " Mechanical Nozzle Seal Assembly Detads". . _

15. ABB C-E Drawing E-MNSA-228-008. Rev. 02, "MNSA Seismic Test Fixtures".

16. MNSA Assembly Procedures. S3-NOME-EP-0124. Rev. 00.

16.1 MNSA - RTD Hot 12g, Section 7.0.

16.2 MNSA - Pressurizer, Bottom Head, Section 6.0.

16.3 MNSA - Pressurizer, Side Nozzle, Section 5.0.

17. Mini-Specification S023-411-57, Rev. 00, "RCS MNSA Assemblies, San Onofre Generating Station, Units 2 and 3"

18. 00000-PENG-037, Rev. 00, " Test Procedure, Seismic Qualification of the Saa Onefre MNSA Clamps for Pressurizer Instrument Nozzles and RTD Hot leg Nozzles", e

19. IOC PENG'96501, Assessment of Test Personnel Cenificates for 1997.

20. Report CENC-1743, " Addendum to Analytical Report for Southern California Edison San Onofre Unit No. 3 Pressurizer," December 1986.

21 PP-2007241, Rev. 00, Project Plan for MNSA Clamp Analysis and Testing.

Page 18 of 47

AC2/COME TION ENGINEERING Contract No. ',007241 TR-PL i-433 Total of Test ,/ Pages Rev.00 i PRIMARY SYSTEMS Appendices 89 Pages Ref. T.R. No. TS071 A TABLE 1 EQUIPMENT AND INSTRUMENTATION _ - _ -

Tigg g " " __rman ^ MODELNO. SliRIALNO/* RANGR fACCURACY CAL DATE - DUE DATE l I

N/A N/A

$ $'$ $ ABB/C-E - - --

N/A I MM gEf$$MF MTS 104.61 412 --

N/A N/A N/A hh  %$$$$$$$ MTS 406.11 1866 --

N/A

_hh,.M!@$($[ 436.II AB 463 -- -

MTS Tinne Data Corp. 2E-073 Unit C-E - --

Q.A. Veritication of Sullware Used

." 492 & 494 I & ICG iS% of Rdg.* *o4/2s/97-1o/28/97 & (M/29/97 Iw29/97

$ Unhokz-Dickic 100-PA 1 & 10G 12% of Rdg.* 04/28/97 - 10/28/97 g g jyh$$ Unholtz-Dickic 2216X 145 & 146 Q l!h Unholtz-Dickie 75D2tPA 109 & lil 10G - 30G 15% of Rdg.* 04/25/97 - N/25/98 D-22tl 2025 & 5482 10G - 30G 12% of Rdg.* M/16/97 - 04/16/98

." .Mfgjf$ Unhokz-Dickie 12% of Rdg. Signal Cal.,05/15/97 - 05/15/98

' M[dhjj$$ Racal Store 7DS 6330 10V Input 2V &I0V 1(0.2% of Rdg.) 12/18/ % - 12/18/97 gh[ Fluke 8050A 6168012 Cc 486DX-33 ABB 01718 N/A N/A N/A S/N 10593 0 - 10V "11% of Rdg. 05/14/97 - 05/14/98 Signal Cal. " l DT2831-G

% Data Translation 6 f$$$ig$$@ Proto 153668 CL-1031 150 ft-lb il% of Rdg. 05/20/97 - 11/20/97 f+

1. 25 250 in-lb 14% of Rdg. M/01/97 - 04/01/98

$$%$@ Proto l

Solfrunt 4%" CL-1041-1043 0 - 5000 psig  %% of full range 05/15/97 - 11/15/97

{_(( [$$!!T ,

• Overall Measurement Accuracy Better TIEn of Reading. ,

• • See Appendix B Reference i1.

. i Page 19 of 47 i i

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\ 1 TR-PENG433 ABB/ COMBUSTION ENGINEERING Contract N2. 2067241 ,

Rev.00 Total of Text 47 Pages l Ref. T.S. Nr. TS071 A PRIMARY SYSTEMS Appendices 89 Pages l

TABLE 3 I REQUIRED RESPONSE SPECTRUM LEVELS i AT 1/6th OCTAVE ANALYSIS FREQUENCIES j l San Onofre MNSA Nozzles 1 I rea:QUENGY- [ - .OBE' SSE..

F F 1.20 2.40 l ..-

1.46 2.92 4

e 1.75 3.50 1 s 2.07 4.14 j l-S +.id+ 1 2.56 5.12 i x 3.20 6.40 l 3.73 7.46 l 4.51 9.02

{ 5.46 10.92 2 6.00 12.00 .

i 6.00 12.00

__ w .

l l RF40E - l 6.00 12.00 ~~ ' ,

l>u**t4We 1 6.00 12.00 l lJ:-~5.0 W '1 6.00 12.00

)

i n - 5.68 h -l 6.00 12.00 ,

ltc 8.N% 1 6.00 12.00 l l2.zh i.113iFars 1 6.00 12.00 i I& 8.0tBW: mI 6.00 12.00 j IfMe8.9mnte 1 6.00 12.00 i I;14rr 0.0Breml 6.00 12.00 NOTE:

-s 6.00 12.00 OCCASIONAL, UNDERTESTING 6.00 12.00 AT ISOLATED FREQUENCIES

! 6.00 12.00 IS PERMIS848LE ACCORDING TO 6.00 12.00 THE IEEE-344 GulOEUNES, l

j 12.00 ESPECIALLY WHEN OCCURING 6.00 12.00 AT LOW (LESS THAN 3 HERTZ)

IJWu.22.6w. a l 5.16 10.32 FREQUENCIEgE NO MR * ' - 4.46 8.96 RESONANCE CONDITl3NS EXIST.

3.89 7.78 #

6.74 j 2.93 5.86

- 2.54 5.06 2.21 4.42

} 1.91 3.82 1 1.66 3.32 1.50 3.00 1.50 3.00

! 1.50 3.00 00'8 W e

. 1.50 ' 3.00 1

1 l

i Page 21 of 47 4

TR PENN ABMCOMBUSTION ENGINEEIUNG Contrae No. 20tn41 Rev.00 Total of Text M Pages Ref. T.D No. TS071 A PRIMARY SYS'11!MS Appeedcas 89 Pages JHOR2ONTAL & VERTEAL TEST RESPONSE SPECTRA SONGS MNSA Ct#FS, OSE MS SSE.1% DAM l 1W to '

7 X '

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I N o ._y t

ai ti i 16 15 Fawser pee

1. oss vomes a-=. . ses veme= -= 1 l i

l nw Note: A less conservative spectra may be used based on the results from the Sine Sweep Tes:,

provided they envelop the Plant. Specific Curve (s) of Appendix A. #

i i

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FIGURE 1: REQUIRED RESPONSE SPECTRA ,

Page 22 of 47 i

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1 TR PENG-033 AB2/COMBUSsION C4GINEERING contract No. 2007241 Rev.00 Total of Text 47 Pages Ref. T.C. No. TS071 A PRIMARY SYSTEMS Appendees 89 Pages 5

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FIGURE 2: REPRESENTATIVE MNEA CLAMP DETAILS Page23 of 47

TR-PENN ABIWCOMBUSTIdN3d'IUihRING Contract No. 200n41 Rev.00 Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages l

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FIGURE 3: REPRESENTATIVE TEST FIXTURE AND MOUNTING DETAILS Page24 of 47

TR EW33 ABB/ COMBUSTION ENGINd5 RING C . 200724 }

Ref. T.R. No. TS07I A PRIMARY SYSTEMS Apperdices 89 Pages ll l

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Page 25 of 47

TR-PENG-033 ABB/COMBUS'ilON ENGINEERLNG Cunn a o. M 41 i Rev.00 Total of Text 47 Pages i

Ref. T.R. No. TS071 A l RDIARY SYSTEMS Appndices 89 Pages I

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FIGURE 5: HOT LEG RTD AND PZR SIDE MOUNTED NOZZLES WITH MNSAs DURING SEISMIC TEST Page 26 of 47 1

1

TR PENG-033  ; ABB/CO.\GCSTION ENGINEERING i contract No. 2007241

, Rev.00  ! Total of Text 47 Pages l Ref. T.R. No. TS071 A l PRDIARY SYSTEMS Appendices 89 Pages il

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l Page 30 of 47 j

i

TR-PENG-033 ABB/ COMBUSTION ENGINEERING Contract N3. 2007241 l Ref.00 Totel cf Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages I

. 1 TEST ids $1NWAS 2 *<ADING: SONGS MNSA CLAMPS SWEEP PudsAMTWIS8 4 ) it)DE ~ 5=LOGCDEC3, i= Loot 0CT), e=LIN8 3 i 4 START, EFD FIIEO, HZs 1.000,54.00 i FREQ MANGE, DEC=1.69e 5 SPECIFICATION 1= RATE, e=DunATION: 1 RATE, DEC/ MINS. 354e SUEEP DURATION - 94ts, MIN, $ ,ECs e,8,47 i TEST LE.NCTH:

6 SPECIFICATION 1=TTNC, e= SWEEP CYCLEss e d

CWLES 1 000 7 TgsY TIME - HRS, MIN. SECS e,8,47 7 Sf4tf-UP TIME, Secs (e.00

< 8 SHwT.Dotat TIM, SEC 5.000 I 8ttfreENCE SPECTRLFis a

S UNIT 9 1=MTRIC, empeos* PETMICs e i 10 $PECTftyM LIMITS:

O!SPLACEFENT, IN(P P): a.500 UCLeCITY, IN/CECs 1s.00 ACCELERATION, Qs .2006 j

11 TYPE, UALLE, FMGs u, .1000,1 10e ALAftM LIMIT +D9, -dss 3.000,-3 000 A90RT LIMIT =DB, -DOS 14.09.-10.09

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A6 cit? LIMIT +DS, -DS: 10.48,-14.00 e ~

13 TYPE, UALLE, FWEGs 3. 3000.90.00 4

AUWIM LI'"If +DS, -dss 10.00,=19 00 ABORT LIMIT +D8, -DRs 40 00,-40 00 14 TEST LEt4L (DS DELOW f4Fis 9.

! 15 CONTitDE. CHAP 9ELS8 1 Pft0 CESS 3=AUG ABS, a=FLpe,1= PEAK, e=frISs a 16 LIMIT CHmpeELS: e 17 ALD(ILIMY CHareELSs 3,3,4

• Pit 0 CESS 3 4u0 Ass, a=FL#e, i=PEAIC, GatWISs a MAXIP4JR EMPECTED Gs 1.5005 18 ACCEL SENS, MU/Gs CH 18 10000.

CH 38 10000.

CH 3: 1000.

CH 4s iete.

19 FILTER 1=Pfl0PORTIONAL BW, 9= FINED SW8 1

' DW, ts: 50.00 i

20 ftEFEMMCE CH4 reels 1 21 MSPONGE CHereEL8 4 4, 1

i 22 MONITOR CHM 9ELs 3

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' 24 LOOP-CSECIC FMGtHE 3, MAN DRIVE (VOLTS 3 s 3.ees, . sees ftEFERENCE LEVELSs MAM DISPutCEPENT, IN(P-P 3 s 1 957 8

PteW UCLOCITY, IN/ SECS 0 158 Ptts ACCELEltpfTICM, 0: .4000 MIM ACCELEltATION, Gs .1000 ACCEtEnAv!On afmaE, Dee s.eee CodWIECT!cMrP t

FIGURE 14: DVCS INPUT PARAMETERS FOR SINE SWEEP RESONANCE l SURVEYS USING SN21T VERSION 04 l

Page31 of 47

TR PEN @33 AB9/ COMBUSTION ENGDEERING Contract No. 20lrn41 Rev.00 Total of Text 47 Pages Ref. T.Ct. No. TS071 A PRIMARY SYSTEMS Appeedces 89 Pages 5' . .

i-CH H Side Mounted PZR Nozzle with MNSA I Orientation A l CH 2 - -

Vertical Norele Top XFER vertical control

~ -

NE LIN 0 - I - I i I > I >

I FPEGUENCYr HZ LIN 5B PUN 2 SINWRE SONGS MNSA Ct. AMPS ..

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50.80 10.40 57.02 64.00 8.47 7.72 1 mm m 100 71.84 7.96 80.63 7.01 90.51 7.54 FIGURE 29: HORIZONTAL CONTROL ACCELEROMETER TRS & RRS, TEST ORIENTATION A, SSE EVENT Page 46 of 47

TR.PENG-033 ABB/COMEUSTION ENGINEERING Contract No. 2007241 ll Rev.00 Total cf Text 47 Pagm  ;

Ref. T.Q. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages I

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Rev.00 Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages DATA SHEET 3 NOZZLE PRESSURE TEST OBSERVATIONS Date: 4-/Y'97 Observation: d' O. L Reviewed By: [' Mbb i Test Nozzle:

rfce: /A.Ker Arw Nonle Test Pressure Prior to Event l Following Event Comment Orientation A OBEl 3 / Ta 3l r* (sifW' dec L 19. CLis92 OBE2 J/ A f 7/ s(

OBE3 i,.. 3'/pe OBE4 7 'j 4, 3 e v.

OBE5 / , r.

1[ / s e SSE1 3, 4 e. 3 . 2, .

Orientation B OBEl

OBE2 OBE3 OBE4 n , , e i OBE5 d./ul Io Axa )rau m1Tiibt

1. .L , V '- ,,

SSE1 lM A as LA 4M UC( IO Old UOL H f 6 ft W Orientation C 1 OBE1 OBE2 OBE3 OBE4 ** ..

OBE5 2 .

lSSE1 Orientanon D OBE1 OBE2 OBE3 OBE4 OBE5 SSE1 Page A-5

! TR-PENG433 ABB/ COMBUSTION ENGINEERING Contract No. d Rev.00 Total cf Text 47 Pages

Ref. T.R. Nr. TSMI A PRIMARY SYSTEMS Appedices 89 Pages l i

DATA SHEET 3

i 4

NOZZLE PRESSURE TEST OBSERVATIONS i

t

! 'Date: 6 -/ Y ' f 7 Observation: d. A W.

Reviewed By: .k ffh,1 bk )# Test Nozzle: Nor Le 6 Arp f

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! Nozzle Test Pressure l , Pnor to Event l Following Event ,

Comment l Orientation A OBEl 32.oo 3.2.*. nscrass Gne t ts c L s c. w l OBE2 1'2., 7 a. .

l OBE3 ii21 ii> s

! OBE4 l' j 7 ( 3nc i i OBES 3 1>r i ; 7.s SSE1 3.2.. 3<9. ~

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. --. .. . . -- - - - . - -- - . ~ . . _ - - - . . _ . . . . . - . .

1 TR-PENG433 ABB/ COMBUSTION ENGINEERING Contract Ns. 2007241 4 Rev.00 Totarof Text 47 Pages

Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages i

DATA SHEET 3 NOZZLE PRESSURE TEST OBSERVATIONS 4

l Date: /, "IY- 7 7 Observation: // A u.

Reviewed By: fl. N . N(/ lbH 6u Test Nozzle: dofrem M c.r~r Arv i (

/,uhumal& h6 l Nozzle Test Pressure Prior to Event l Following Event Comment l

Orientation A _ l OBEl 3 2 ao 3 .2 a s (gScrua lect dL 1. %

i j OBE2 f.t.. J ' a ..

i OBE3 7'a ae i .z. . ,

l OBE4 f .2 e I a. . .

J OBE5 1'/75 i eq <

.I k SSE1 y,nf 3' isa Orientation B OBEl 3 2 2. f J 1 s 5" ,

'4 OBE2 3).. i 2. 4

• j OBE3 i t oo i 2., e l OBE4 i/75 i, le 5

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OBE3 3 . s. e e 2 . a,,, ,

OBE4 3us J see 3'1 t70 #

OBE5 ' 2 see - a SSE1 3.' 2 ee J . 4. *

• Onentanon D-OBEl 3 i?5 3 . / 7 $'

OBE2 / zee 3. 2. *

• OBE3 / a. *

• 5 irs' OBE4 -j t . i i..o OBE5 i i .s i iIW SSE1 3 ref 3 /4f Page A-7

il TR-PENG-033 ABB/ COMBUSTION ENGINEERING Contract No. 1007241 I Rev.00 Total cf Text 47 Pages Ref. T.R. No. T5071 A PRIMARY SYSTEMS Appendices 89 Pages

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Il TR PENG433 ABB/ COMBUSTION ENGINEERING Contract Ns. 20t7241 -l Rev.00 Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendees 89 Pages )

DATA SHEET 3 J

j NOZZLE PRESSURE TEST OBSERVATIONS Date: 4 -/ #- T7 Observation: 6. D. h.w Reviewed By: (Ld k. OA 22r3 Test Nozzle: do rTEm m ars

( '

W W tuffeA1'4 A Nozzle Test Pressure Prior to Event l Following Event Comment Orientation A OBEL 21.o 1 uo (n.S.rs.a o.t GALG e L. o s 4r l OBE2 f e,f 2 ' /15' mask en hse s.o tt.us a OBE3 3 'z u .I a OBE4 2' s,. i se e OBE5 f f 3( 3e7(  !

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A  ;

SSE1 1_ 11e. 2 i ro -

se unto m = so t p a f L.anuin.? l Orientation B  ;

3 OBEl 3 a.o a 3 2.ed I

OBE2 7's y r .2 #91r OBE3 f ie r  ?' M i OBE4 I i ? r' f ,9 f OBE5 319f i i5s Awall lbf an ll.Leive hw m( f< liv 4,?i '

SSE1 3. n.ae 3 IT f' kd(A /1NMUM alla f f& .

Orientation C OBE1 31 1L ( 2 te.

OBE2 3't. 4 i s..

OBE3 fsee i s ..

OBE4 1 zes i le*

OBE5 . I- a. e . Y: 7i #

i

SSE1 .2 2 m .

3. A V r

Orientarme D OBE1 3e.. .2 s . .

OBE2 _r' e J _'wr e OBE3 fs e. 1' a.. o OBE4 J2. J. 2. . .

i see OBE5 3. 3 s.

SSE1 3.19f 3. /fe 4

i Page A-11 a

- L .:: -D _~~~~~~ -~LC~"~ ~ : ':: ~ ~ ~ '

TR-PENN ABB/CO6HMSHON ENGINEERING contract No. 20rT241 )

Rev.00 Total of Text 47 Pages ,

Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendees 89 Pages i

1 APPENDIX B 1 VOLT PEAK SIGNAL CALIBRATION CHECK

OFF-LINE ANALYSIS SYSTEM l

c i;

f l 1 I

1. i Page B2, As recorded by Data Acquisition System for Each of Six (6) Channels,

]

1 l

j Page B3, As Registered by the Off-Line Analysis Program SRSKHH for Single Channel

! n o-l Note: * /

Calibraion Check Consisted of Passing Nominal 100 Hertz Signal (+/- 1 Volt Peak) into PC based Desa Acquisition System. Digitizing at Sample Rate of 5000 (each Channel), Duplay of

Portions ~of Sampled Data by Data Acquisition System, and Fmally Display of Pottions of i Sampled Dass by Time History Display Secnon of Response Spectrum Analysis Code i

SRSKHH.

Calibration Performed May 14,1997.

t 5 Page B-1

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i APPENDIX C 1

CALIBRATION RECORDS l

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TR PENG-033 AB2/ COMBUSTION ENGINEERING Contract N2. AS[

Rev.00 Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages AM

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Range M M ACCURACY l ^"1 Calibration Document:

Mf g. Serial No. S/bD/E [ j Procedure Rev.

C.E 10 No. N!/9 (fl Manuf acturer's Specifications"[hi-/f f f sf ?'[

Test Equipment Used To Perform Calibration:

Test Ecuioment Serial or 10 No. Test Eauipment Serial or f 0 No.

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REMARKS: A M Aur uru Ooh 0uc 1 c r s- rt ?t rY -

cAU8 RATED f a

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O come 1 nid Page C-2 l

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REMARKS: $

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Page C-4

. - - - -. - .. . - - . - . . . . . . - . . - . - . . . . - . . . - .. .-.-... .~. -. -

TRMN AB2/ COMBUSTION ENGINEERING Contract No. 20e7241 \

Re. M Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages a seat - NON-PERMANENT

!- pg soap i 74%r~oT GUALITY RECORD

< usonarcar CERTIFICATE OF CAUBRATION 1'

instrument Type $*-s d b .dt' Calibration Date M 'M-9 2 i f Manufac:urer IL'b b b Calibration Ove Date lo Of-99 l l Fange M D A:: curacy S- Calibration Document: i

" / hl* l l Procedure Rev. ,

Mfg. Serial No.

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4 Test Ecuipm. the To Perform Calibration:

l Serial or iC _ Test fouipment Serial or 10 No.

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i CALIBRATION RESULTS j

t et Out of Standerd As Found As Left Op08.

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i

' Page C-5 1

1 l

j I

l TR PEm33 AB2/COMBUSMON ENGHGERING Contrace Ns. 2er6[

b# Total cf Text 6 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages ABS NON PERMANENT QUALITY RECORD TaEr*8

, CERTIFICATE OF CALIBRATION Instrument Ty3e 5' *#b Calibration Date M-49 -9 7 i Manuf acturer U e N4

• 1 Calibration Ove Date /d 2 9 9')

Fange Mia b Accur CY t

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Mfg. Senal No. /Yb N2

[ l Procedure Rev.

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I IACCEPTED I IEEJECTED g3,,,,,,, ,,, g% s .,,,

TEMPERATURE 70

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Page C-6

N ABB/ COMBUSTION EbbhEERJNG Contract No. 20t7241 I Total of Text 47 Pages

'I Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages i

a se as NON-PERMANENT rsspBD

• 4 1

'iX*E uscAarony CLUALITY RECORD CERTIFICATE OF CAUSAATION Instrument Type lee d d' r b Calibration Date N"E ~

l

• e Calibration Oue Date /O~ 2I* 9 9 i Manuf acturer NM"A 'h d Range N Accurac IJ Calibration Occument:

l y9Y Rev, Mfg. Serial No. /uf l ] Prc:edure

! C.E 10 No. #L*biY ! /N~OY ( l Man.facturer's $0ecifications l 1

Test Eguipment Used To Perform Calibration:

Test Eculoment Serial or 10 No.

Test Ecui0 ment Serial or 10 No.'

1:bb e CL-Jo7'?

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Value No.udes bk M_ J l T rY Yd o r ~

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CAusAATION MAS P1EN ASAP 0AM40 utiu24N6 MEAsumsmeNT Devicts wnsCM STANOA405 WN8AE SucM STAN0AA0s Exist, wMcAE SUCN STANDAA05 00 NOT gxtsT, AN AA8m DOCUMENTto t

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REMARKS:

CAuaRATEO M 8 I +

y1 ACCEPTED 1 1 REJECTED Y dmm ws m.i TEMPERADJRE /0 I ___

Husioin #fo P 3e= a 1 e.f Page C-7

"NG-433 ABB/ COMBUSTION ENGINEERING Contract No. 20tTM l

,g Ref. T.R. No. TS071 A PRIMARY SYSTEMS n 89 Pages A.45 NON-PERMANENT QUALITY RECORD 75.cwo u T4E CERTIFICATE OF CALfBRATION 4/ - n, 9 7 ]

l instrurnent Tvoe O L c A L A v C ,.,,t,on Oat, s Calibration Ove Oate id-/b- S 7 fb U Manuf ac:urer N00bbN1 ~

bI Range Mb Accuracy tM Calibration Occument:

Mfg. Serial No. 4M[ [ ] Procedure , . . Rev.

IL~ 9 N Manufacturer's ' per.t ationsTru 00(

4 I

C.E 10 No.

1 Test Equioment Used To Perform Calibratson:

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b\(t. $~f"O O _ O._L- d O T1~~

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• i QAU8 RATION RESULTS Q

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>M

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l ACCEPTED I I REJECTED TE'9EU.i'JRE 7 I wm wo pnn I o l Page C-8

TR-PENG-433 ABT/ COMBUSTION ENGINEERING Contract Ns. 2007241 Rev.00 Totat cf Text 47 Pages PRIMARY SYSTEMS AppendCes 89 Pages Ref. T.R. No. TS071 A ABB - NON-PERMANENT QUALITY RECORD 75 5 CERTIFICATE OF CAUSRATION Instrument Ty0ebea r NN O tr Cainbration Date Y- i) A l Manufacturer

- (bf Calibration Ove Date id /$ 7 3 b b  !

Accuracy- A Calibration Document: l Fange Mfg. Serial No. Sf N ( l Procedure _ Rev.

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Serial or 10 No. Test Eouipment Serial or 10 No.

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J J CAUBRATION RESULTS.

Standard As Left Out of Standard As Latt Out of As Found Tot.

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CAUBRATED BY:, _

ACCEPTED I IREJECTED e,,, gw sg TEM?EWUREli

^ ,_,I HUM!Dli\ ...- 'l ,

Page C-9

1 TR-PENG-033 ABB/ COMBUSTION ENGINEERING contract No. 20trt241 Rev.00 Total of Teu 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages

~

AM NON-PERMANENT QU ALITY RECORD Ta%G CERTIFICATE OF CAUBRATION I instrument Type- Aofs r11r=M b" Calibration Oate 4 . .?.5497 j Manuf acturer II*J b oO: I- Eb Calibration Due Date Y X- T I i Range Al,/A Accuracy Calibration Document:

/O9 Rev.

Mfg. Serial No. l l Procedure ,,_,

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~

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value r

~

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L ea] X' ras "~b bnk '

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CAueAArso88 MAS S$$N PGApoAMeo UTIU21884 utAsumsutwT DEVICES WMsCM MAvi Epsowes atuf@#sMers to NtST STAwoAAng wwgng SUCH STAssoAmot DIST.WNERE SUCH STANoAAct oo Not Dist. Ass APmovto PmottouRE N

'N AC"oAoANCE mfM fwt uANu8 ACTUAsm S RECouutNoAfioNS MAS SttN ulto Asso fME STAwoA REMARKS; A ( % SL s : M /s~ o O./e @ S O

• uSRATE I ACCEPTED I IREJECTED - ,f # si Ns es m sr =

TEMPES,ATURE 70 t Hi.tMlCl!Y _ 47 7o o ,n. , ..o I Page C-10

TR-MM AB2/ COMBUSTION ENGINEERING Contract No. 200724[ 'l E*'* # Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appeedcas 89 Pagm ABB ~ NON-PERMANENT QUALITY RECORD

'r.aTaar'57 i.Asonarone CERTIFICATE OF Call 8 RATION Instrument Tyos he tktreM ds r* Calibration Date M - M'~~ 9 ) l Manuf acturer kad ad3 b t1 Calibratson Oue Date Y ~ #~ i I l Range M /A Accuracy 1 Calibracon Document: l

_ Rev, Mfg. Serial No. /// ( l Procedure 4

C.E 10 No. N!A l l Manufacturer's Soecifications Test Equioment Used To Perform Calibration:

Serial or 10 No. Test Eouioment Serial or 10 No.

Test Eouioment Mi. , &-407'1 LL tts DJan EL-942

WV t C.L 10 84 r14k C.L .10 73 entT2s (Lla.or m. rst / /~1/ 'maarT7. / 1 ' Ar759.- 4t444#. 84 84r2'/ rf

,QAUSRATION RESULTS S: ndard 4- Ogf S ard As Found As Left , ' Ogot As Found l oh L srh3 7' h 7A L

/ 5 1 D-10a ~7 2'YC ,

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'w acconoamca wiTu twa uuusacTunam s mecouwewoafious was tesw usso awo Twa REMARKS: A 0 L. (ms_ . v To i I a h'd.@ @ f h CAUSRATED SY:,- -

I ACCEPTED I IREJECTED . si .u m= ss remwne w micm 47 7 * . .. . . . /

Page C-11

TR-PENG-033 ABB/ COMBUSTION ENGemERING Contract No. 2007241 };

Rev. 00 Total of Text 47 Pays Ref. T.R. Ns. TS071 A PRIMARY SYSTEMS Appe: dices 89 Pays i

SIGNAL CHECKS. STORE 7 RECORDER. CHANNm R 17 ieAL.oATu: os.ts of l Ous naru: os.1s e8 l r Tucn a.om. i uNa. x.u.a. i

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ACCEP M -

CERTIFICATION OF ACCURACY DATE///d/

CUSTOWE M Hg 04/01/97 ABB COWIJETION ENGINEERING GAGETVPE: ToegtJEintf.NCH 1000 PROSPECTIIILL110. 3 33 PROTO IWNISOR CT 06096 RERig e25 EA.fi 4471Glar DATE DLE: 04/01/96 f

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1 TR PENG-033 AB2/ COMBUSTION ENGINEERING Contract No. 2087241 Rev.00 Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages

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INSPs m inc. TORQUE CALIBRATION CERTIFICATE REPORT NUMBER: 213012 PO Nember: 45676KP DATE OF CALIBRATION: 5/20/97 CUSTOMER: ABB Combustion Eng:neenns U -iLiBRATION INSTRUMENT: Torque Wrench,150 Mbs. U M N~ # )

S/N:CL-1031 MAKE: Proto 153668 PRECENT OF RANGE 20 % 40 % 60 % 80 % 100 % .

CLOCKWISK l INDICATED '

30'Ibs. 60'Ibs. 90'Ibs. 120'!bs. 150'!bs.

WRENCH TORQUE:

60'Ibs. 90'Ibs. 120'!bs. 149'!bs.

ACTUAL TORQUE: 30'Ibs.

COUNTERCLOCKWISE l

INDICATED WRENCH TORQUE:

ACTUALTORQUE:

PROCEDURE:#32 **

TEMPERATURE / HUMIDITY: 68'/41%

l l

• THIS INSTRUMENT.WAS CALIBRATED USING MASTER CALIBRAMR SERIAL NOrS(17 i

CALIBRATED ON 6/17/96 DUE:6/17/98 TRACEABLE TO THE NIST THROUGE.NIST TEST NO. MMAP 822/LA 0 A1W CALIBRATION TECHNICIAN Ref. ANSI S197.14 Ref.FederalSpee.GGG W des Ms.w-2seyr l Calibreden esaforms to ANSI 19461 l

Esdeseed levelof essersey is 21%

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Page C-14

TR-PENCA33 ABB/ COMBUSTION ENGINEERING Contract No. 20F1241 Rev.00 Tasal of Text 47 Pages Ref. T.R. No. TS&71 A PRIMARY SYSTEMS AppeIdices 89 Pages APPENDIX D l OFF-LINE ANALYSIS - RESULTS GRAPHS & TABULATIONS Hot leg RTD Nozzle and PZR Side Mounted Nozzle Input Test Response Spectra for 5 OBE Events and 1 SSE Event in one Test Orientation (Axis-Symmetric Specimens)

Pages D2 through D11 Horizontal & Vertical OBE Spectra Pages D12 & D13 Horizontal & Vertical SSE Spectra PZR Bonom Mounted PZR Instrument Nozzle. Supported Configurat.on Input Tat Response Spectra for 1 OBE and 1 SSE Events in Each of Four Test Orientations Pages D14 through D17 Orientanon A ,

Pages D18 through D21 Orientation B Pages D22 through D25 Orientation C - -

Pages D26 through D29 Orientation D PZR Bottom Mounted PZR Instrument Nozzle, Free Standing Test Configuranon input Test Response Spectra for 1 OBE and 1 SSE Events in Each of Four Test Orientations Pages D30 through D33 Orientation A Pages D34 through D37 Orientanon B Pages D38 through D41 Orientation C Pages D42 through D45 Orientarian D Time Histories for 4 SSE Events, for Horizontal Nozzle Top and Horizcstal MNSA Top Plate e

Pages D46 and D47 Orientation A Pages D48 and D49 .Orienenrina B Pages D50 and D51 Orienenrinn C Pages D52 and D53 Orienennna D Test Response Spectra for 4 SSE Events, for Horizontal Nozzle Top and Horizontal MNSA Top Plate  ;

Pages D54 and D55 Orienenrinn A Pages D56 and D57 Orienenrina D l Pages D58 and DS9 Orientadon C Pagtv..D60 and D61 Orienation D Note: Graphs can be identiced by File Number in combination with Table 2. l Page D-1

~_

FC-PENG.033 Contract No. 2007241 '

ABB/ COMBUSTION ENGINEERING Rev 00 Total of Text 47 Pages PRIMARY SYSTEMS Appendbs 89 Pages l Ref. T.R. No. TS071 A l l

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TR-PENG433 ABB/ COMBUSTION ENGINEERH4G contract No. 20e7241

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l 1

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DATA FILE c:\gl\mnobualv.khh DAMPING 1.00 (%)

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2.00 3.88 /

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TR-PENG-033 ABB/ COMBUSTION FMGINEERING contract No. 2007241 Rev.00 Total of Text 47 Pages Ref. T.R. No. TS07t A *RIMARY SYSTEMS Appendices 89 Pages Analysis Code: SRSKHH Version 1 DATA FILE c:\gl\mnasuah.khh DAMPING 1.00 [%]

FRE;sUENCY ACCELEimTION (HERTZ] (G) 1.00 2.21 1.12 2.75 1.26 3.64 1.41 3.86 1.59 4.51 1.78 6.45 2.00 7.82 2.24 8.05 .

13.49 3.17

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TR.PENG433 ABB/ COMBUSTION ENGINEERING Contract No. 2007241 ' I Rev.00 Total of Text 47 Pays l Ref. T.R. No. T5071 A PRIMARY SYSTEMS Appendees 89 Pa p s l

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I Page D-33 i

1 I

I

i TR-PENG-433 ABB/ COMBUSTION ENGINEERING Contract No. 2007241 Rev.00 Total of Text 47 Pa8es Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pa8es Analysis Code: SRSKHH Version 1 DATA FILE c:\gl\mnobub1h.khh DAMPING 1.00 [t]

FREQUENCY ACCELERATION (HERTZ] (G) 1.00 0.88 1.12 1.37 1.26 1.74 1.41 2.27 1.59 2.57 1.78 3.35 2.00 4.17 2.24 4.36 3.17 5:

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__ __ ~

TR-PENG-033 ABB/ COMBUSTION ENGINEERING Contract N:. 2007241 Rev.00 Total cf Text 47 Pages Ref. T.O. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages Analysis Code: SRSKHH Version 1 DATA FILE c:\gl\mnobubiv.khh DAMPING 1.00 (%)

FREQUENCY ACCELERATION (HERTZ) (G) 1.00 1.06 1.12 0.98 1.26 1.98 1.41 2.38 1.59 2.71 1.78 3.53 2.00 3.88 2.24 4.47 2.52 2.83 5.43 6.86 8 RESPONSE SPECTRUM 3.17 7.55 - .m 2.... .......... .... .t.+.4 .. + . .. .em rn or.. _.

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l I

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TR.PENG-033 ABB/ COMBUSTION ENGINEERING Contract No, 2007241 Rev.00 Total of Text 47 Pages  ;

Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pa8es  ;

1

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1 l

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TR.PENG-033 ABB/ COMBUSTION ENGINEERING Contract No. 30e7241 Rev.00 Totd of Ten 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages Analysis Code: SRSKHH Version 1 DATA FILE c:\gl\mnobuc1h.khh DAMPING 1.00 (%)

FREQUENCY ACCELERATION

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TR-PENG-033 ABB/ COMBUSTION ENGINEERING Contract No, 2007241 Rev.00 Total of Text 47 Pages Ref. T.T. No. TS071 A PRIMARY SYSTEMS Appeneces 89 Pages 1

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TR.PENCA33 ABB/ COMBUSTION ENGINEERING Contract No. 2007241 Rev.00 Total of Text 47 Pages Ref. T.R. No. TS071 A PRIMARY SYSTEMS Appendices 89 Pages l

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