ML20138F980
| ML20138F980 | |
| Person / Time | |
|---|---|
| Site: | Clinton  |
| Issue date: | 09/06/1985 |
| From: | SARGENT & LUNDY, INC. |
| To: | |
| Shared Package | |
| ML20138F958 | List: |
| References | |
| CQD-023726, CQD-023726-R00, CQD-23726, CQD-23726-R, NUDOCS 8510250384 | |
| Download: ML20138F980 (94) | |
Text
- .
ILLINDIS POWER COMPANY CLINTON POWER STATION UNIT 1 Y -
DYNAMIC QUALIFICATIGN OF TIME SELAY RELAYS
%J Compiled by THE COMPONENT QUALIFICATION DIVISION SARGENT & LUNDY ENGINEERS Project No.. 4536-32 CCD No.: CQD-6?d72[
Vo lurne : SQ-CL NA Rev. 00 Date: (([,/gf (I) 8510250384 e51023 PDR ADOCK 05000461 E PDR
TABLE OF CONTENTS Description page/ Tab m1e ease ........................................ I Table of Contents ................................. II t
j
^
QA Sign-Off Sheet (Issue Summary) ................. III Ceneric Checklist ..............'................... A A I ~ A 15
, Required Response Spectra (If Applicable) ........ B jf N jd Test Response Soectra (I f Apolicable) . . . . . . . . . . . . . C Cf v Ch Qualification Document (Reference only, do not film) o
~
Checklist for Supporting Calculation (If Applicable) E E l ~ E3 -
Su= porting Calculations (If Applicable , ,,,,,,,,,,, r; (( % %
Da ta. ( .S.e.f.e. r.e. n c. e. ,. .o.n.Q ,. .d.o. .n.o.t.
Reference & Misc. . ..
4 8
I Prcject No.: 4536-32 CQD No.: CQD- 02J 7df Volume: SQ-CL i . Rev.OO Date: (f t
(II) !
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i; I REV COMMENTS RESPONSIBILITY
- i SECTIONS DATE k e
0Hjinal Iss(to PREPARED 8Y: \, 7 '[ I i _ ,',,.h.p [(y h /f ,g" QQ REVIEWED BY: \,,, )f f g ]sj p / (-
HEVIEWED B Y: ,- , g)$. / j f p APPROVED B Y:
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PREPARED BY; '
H E VIE W E D B Y:
R E VIE WE D BY:
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HEVIEWED BY:
REVIEWED B Y:
APPROVED BY:
PREPARED BY:
j REVIEWED B Y:
i j RE VIE WE D B Y:
APPROVED BY:
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4 PREPARED BY:
- REVIEWED BY
REVIEWED BY:
1 APPHOVED BY:
COMPONENT r .-______.- ^
ISSUE
SUMMARY
ountiric^ Tion PROJ NO 4s36-32 il SARGENU+LUNDYl 0 N;37?4- - - -
- , , nivision ,
.~,..~.....ii con
GENERIC CHECKLIST O
l l
.i 1coject No.: 4536-32 CQD No.: CQC- 02372[
Volurt.o : SO-CL Rev.60 Date: 7[f[fg O^
wM e =9*** ***=e .*
- e , -
PROJECT NAME: (Ljdon FILE NO.: CQD- 0 2 3 785 PROJECT NO.
f 63 h 3 k REVISION N0.: pp SPEC. NO.: [(- 1 8 N ,IX-A 6 CI aeviewed By: M-l - W Date: '#
@ BOP NSSS ro ed By: [ j / /[< Date: / /
( g_1g G 1) ( %-1801) (signature.) '
COMPONENT NAME: m e. e au h d %) i e VENDOR / MANUFACTURER: $ k e W exc h k k e V m E c(N bb/ J '\ C-s v COMPONENT NO./MODEL NO.: s!, c m. . ,. E C r., c / 7 o1 Z PC . .
VENDOR'S REPORT NO. AND DATE: 73 "~
- OO5 ~
' '/ - O ^ S q-3 79 734 ~7 9 . O c S. R - , / . c o ej e # 2 -M-7 9 A. L- .
CONCLUSION OF REVIEW M wn)(i hm s :; Ha !,.s p<n t- s ~y' ,s))
' [ g'3(
"'J.y I.i:.i b 2 <!$ O ki i
@ Accepted ORejected Comments: Y h FeOcr D- Ed P is #'m M E W mu tai ~ M W e cAs o ~
A- re a e M-t m B. CLASSIFICATION AND FUNCTION
- 1. Classification Calc. flo: CQD- MJ131 a
) @ Nuclear Safety-Related, Active Rev: 10 Date:. F685
?i3).73 2 Nuclear Safety-Related, Passive Prol. tlo- t
^ PMe ..0' . A /8 i
, Non-Nuclear Safety-Related c 2. The componert function is 3 o o O .m avs C \,'Occ. 8 6 cm ;1- s usiM,, a L'~.w 'Aob % e ies
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. G\ o f"'-( ~' -
iw i s .
y %
y C* u rat i O O -
c 3.
w Operability Recuirements (Active Components Only) h Ihis ccmponent is required to operate:
ed'
@ During and after postulated dynamic and accident events ee .].
a c. O Only after posculated dynamic and accident events b.
a5 2e This c'ecest s a Sars*'tM tuMy prmTv 8 .
y$ p,y:cu neP .t. u.'se.er. t m:,
O' te uscd Dy ulM3 c.
er tamany m :.r.d. A*y oth*r MECHANTCAL OEPAR W:NT STANDAAD sa sus: ue-t .se or rc:'rew:an ce tns cru.
meat mast t.: so road tv Wct 'a L-*- CHECKLIST FOR DYNAMIC QUALIFICATION OF l MECHANICAL AND ELECTRICAL EQUIPMENT Fua OFFICE USE ONLY - NOT TC BE SENT CUTSIDE OF SARGENT & LUNDY gg W, gy "AS-CQ D-2 . 4
,j page 1 of 9
=..m_ ,, e
, ,-. , ,- ,- - , n ,, ,
r PROJECT NO.
h%-3{ FILE NO.: CQD- O M M [ REV.: CC
^
Location and Mounting
- 1. Locatien
)
Building: )$6$2 b6R. b %s '
A CA . ;e.seiGenecAncRm+.
Elevation: 7N ~~ O
- 2. Field Mounting Condition
@ / Pipe /HVAC' Duct: 4 p Q 1"T"A ,[ 6 (k q3(c)),IE M -icod@
O wall /rloor ca-asod-) ' '
- Other: .
- 3. Mounting Attachment EBolting Number: h , Size: [-N '
Material:
r N'd d. SkO-d Owelding welding Type: . I Leg: , Length: , Pitch:
00ther:
p 3e 9 - n..w w
. c- c - e e , -- c , i-c..-3
- .n s t. # < - . u .s rs-- .
l h METHOD OF QUALIFICATION O Static Analysis O Other:
@ Test Dynamic Analysis (
kN r; q 3 Lc&d VD E. VIBRATICN INPUT f,'$
- 1. Dynamic Loads Ccnsidered COlc. No: CQD -.ER3 73 6 (9,,
E Seismic e: i M Ej f, _ g g O nydrodynamic rage...AA..ct...A.li O Seismic and nydroaynamic g
3 g l *f, Other:
}O 2. Required Frequency Range: I o to H - ( TA E3 - B )
20o
- 3. Required Input e .
% Response Spectra Et
'* a) Requiree response spectra (attach graphs, identify): Ew e.: >)
E\evh1 Runome SwMrw , A H Etf--E LecMons . l cs- u E- e 3 1
1
'OR OFFICE USE ONLY - NOT TO BE l MAS-Coo-2.4 r
aENT OUTSIDE OF SARGENT & LUNDY SMGENT4LUNDY ..
...d i l
page 2 of 9
')
i i
,it I l g 1
PROJECT NO.: g FILE NO.: CQD- O[J73[ W .: M b) Method of combinirig required response s g' ggg O Absolute Sum Rev- 00 Date:E6M5 0 #e Proj. flo- fA36'4d P37e b3 ..Cf .. A.L5
-@ Not applicable
~
c) Damping Upset / Service Level B kO Emergency / Service Level C 3 fo Faulted / Service Level D d) Basis for Damping: k e ct bd P .b SeismicCoefficients(Requiredacc'Ilerationineachdirection) -
Upset / Service Level B H , H 2 V Emergency / Service Level C H H
' 2 .V Faulted / Service Level D
- 4. Is support amplification considered?
@ Yes O No ONotApplicable Comments : T h e, R P 5. , , , n _ ,k o,,,\ p p j_n e mt e k M q Mk es e,r L A Essc,s t.oca c , c., s c . . '
- 5. Is fatigue considered?
@ Yes No , ONotapplicable Coments : B OBEs & 1SSE M MM css: Loc %l .
F. QUALIFICATION BY TESTING -
- 1. Does the Vendor's recort indicate that the component is identical to that to be installed?
@ No - justify similarity: A F. ~ bd h.4D av'lt*5' a h ') %h s "
g . . .
F g o <- S i m. \ $ c A_v 6.VA\ u3.,e l u ~swu a s. n .a a :i ..u J e, S 2. Mounting a) Mounting Method: (' 5 dc ComeCd . . Sec+.I.cnR.)
hO @ Bolting Number: $ , Size: g 3K Material: m',\[ Sh e ek Welding Welding Type: !
S . "*'
he > 1 gj Leg: , Length: , Pitch; l
1 FOR OFFICE USE ONLY - NOT TO BE
- ggggg !%S-CQ D-2. 4 SENT OUTSIDE OF SARGENT & LUNDY 3
- . . ; page of 9 6
O l
PROJECT NO..
{-]{ FILE NO.: CQD- $337M REV.: OO O other: -
i b) Does the Vendor's report indicate that the laboratory mounting simulates the actual service mounting?
Yes
@ No - explain differences: Sa? Chm e
- I N" $C A
- n. oc 4 ;&C w.n c . .
- 3. ~Input Motion Calc. flo: CQD .. fddldh.. '
Single-Axis E8V: 80 Date 7//85
@ Multi-Axis Proj,. flo:
p328 ..d _._.ful: _-J A A. . 0f . A/5 ,
Other:
Comments: Y b ~* d ^ ~~
-O# '
cebil:U e s e T or ra 04 bec-s to-ce s
run .
- 4. Test Method O Sine dwell (single frequency):
a) Frequency range:
c b) Dwells at: (Hz)
.c ,c a c) Number of tests'in each orientation:
Upset / Service Emergency / Service Level C
. D l*V*l B N,!==d Faulted /ServiceLevelD I~.=:2 d) Duration:
GR at W-2 e) Input acceleration in each direction:
k,,, Upset / Service Level B Hi ,H2 V h Emergency / Service Level C Faulted / Service Level D H ,H2 ,V 1
f) How is cross coupling and modal participation accounted for ?
a, < - - _
~t d ,1
$~
gi O Sine beat (single frequency):
~o a) Frequency range: QQ '
a .
b) Number of tests in each orientation: '
o$
'* Upset / Service ,Emergene ervice Level C Level B Faulted Service Level D FOR OFFICE USE ONLY - NOT TO BE SARGENT4LUN0y r:AS-Cg D.-2. 4 SENT OUTSIDE OF SARGENT & LUNDY Page
,,7_-__--.
4 of 9
PROJECT NO.:
3h-)) FILE NO.: CQD- h33 73[ REV. : OO
~
c) Number of beats: , Number of cycles per beat:
d) Beats at: (Hz) e) Input acceleration in each direction:
Upset / Service Level B Hy ,H 'V 2
Emergenc Service Level C Hy H Faulted Service Level D '2 V f) How is cross coupling and modal participation 7.ccounted for?
m m Sh A fch 11 "'m~5 A TM 7 u'u:ay u"wau .6 U n' sA d t 4i
@ Random motion (multi frequency):
{ a) Frequency range: I ho NO NE b) Number of tests in each orientation: -
Upset / Service Level B **#E*" I * * "*
, Faulted / Service Level D c) Duration: O E. b 1 ,~2 O f ?c,. s C,.<,E 1 hOf,ec,
~
d) Does Test Response Spectra (TRS) envelop the Required Response Spectra (RRS)?
@ Yes - Provide RRS and TRS as attachment .
( 5 e c. Comm-enh 2.; 5 Cttic'T N)
O No - Explain:
1
- 5. Dynamic Characteristics
@ Natural frequencies: H y 7 M y,i H '
O Natural frequencies not determined.
2 b34E.V)33NE
%ao
- 6. Additional tr> ads e* Are norr.al operating loads considered?
Calc. too: CQD. ...U.,1712 '
EO @ Not applicable Rev:. 00.. Date f!N.-4 5 Ptol. ti 43.5 b -34 J, 5 0 res Page .jo s_ ... ot ... A.S... . .
Io O No - explain:
0$
s' a _
~
FOR OFFICE USE ONLY - NOT TO BE gg MAS -CQD-2. 4 g3g SENT OUTSIDE OF SARGENT & LUNDY 'assenesseen 5 og o
. Page
, - ~ . _ , . . . . . - - - . . ..
- - - - .,-----,__m---r, _ - , , . , _ - , .-_.m_ --.,._,,,.-y ,, , ,__,4_ , .
PROJECT NO.:
g-3 FILE NO.: CQD- U 23 73[ REV.: CO Q -
J
- 7. Monitoring a) Is the component functionally monitored? ( Sec Commed 3 kgn,)
@Yes O No Not applicable b) Is component's operability verified? (. 5:>t ComeM Seck on H)
~
g 3
@Yes O No Not applicable
~
- 8. Does the test meet the reouirements of IEEE 344 19 1 [ ?
~
@ Yes No-explain:
G. .UALIFICATION BY ANALYSIS 1.hypeofAnalysis
,(5 k
' Static Analysis O S c lified Dynamic Analysis Modal alysis Time Histbry Analysis O Other: \
- 2. Analytical Model Calc. NO:
Finite Element Rev- -
- CQD..ll-d14f-_ D3te:. N
~ p ,
Other: Page. N g Of4..A/5.
,J g-...-
- 3. Method of Analysis Computer-AidedCalculaIion
[
Q a) Programs use J
ei b) Ha
/ N cte programs been validated?
- 5. Oyes O No hf and Calculation
).
gg h' 6 ehN h k u b bQ:]h.a [I'[: il S-BiiKUN w a: '
'O
/ \ ,
FOR OFFICE USE ONLY - NOT TO DE '
SARGENT &LUNDY uAS-CQD-2.4 SENT OUTSIOC OF SARGENT C LUNDY ,m assaasemann Page Of 6 9
- 6 PROJECT NO.:
]{ 3Q FILE NO.: CQD- 033 ((,[ REV. : CO 4 Operating Loads Are the operating loads considered in the analysis?
O Not applicable Yes No - explain:
x /
5 Static Simplified Dynamic Analysis a) Acce tion coefficients:
Upset / Service Level B H ,2 ,V ?
Emergency /ServiceLevelC Faulted / Service Level D 1 -[' 2 ,V N /
b) Are dynamic loads applied in the horizotital and vercical directions simultaneously? Calc. flo: CQD ... M.4146.-.3 Rev: 00 Date .M..M. 80 0 Yes Proj.flo._f5 ~
0 No-explain: Page.d2_.0f._. 15... - - -
N / _
Y
- 6. Modal Analysis a) Identify Response Spectra used:
/ \
b) Damping factor sed: \
c) Number of s ificantmodesconsidered:\
\
d) Natural period / frequency of each: \
/ \
/
, e) Method of combining modal responses: )
u / I c,3 Absolute Sum
-! y Square root of sum of the equares (SRSS) n~
fO In compliance with NRC Regulatory Guide 1.92, g, Rev. . Date a3 0 other:
$o , i Bi oo Q) ' tQltyG h.:=U s~ Q :.'*k '."
l
, w s= bs .d U w, 5 q t r*w = m r. nad d f4 1
a--
[' 'r FOR OFFICE USE ONLY - NOT TO BE (s SARGENTaLUNDY mas-CQD-2.4 SENT OUTSIDE OF SARGENT & LUNDY .. . o page 7 of 9 M S G
- e+6mn a em eee
-,g -- - - - - ,, , -- - , , , -
PROJECT NO.:
qg FILE NO,: CQD- 03373[REV.: 00
- 7. Time History Analysis N /
\ /
\ [
- 8. Results <
a) Stress eval tion at critical locations:
N \ LOAD DYNAMIC TOTAL ALLO'n'ABLE LOCATION NOMBINATION STRESS STRESS STRESS
\ /
t > -
/ s y
yG D3 Q .D .D, "; .~', '.T
\-
n
" .Q ' ?, ,i 6 J3 9;.-.. \. L .:5L J u ...) 3 L' ;
m __ _.
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/
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/
- l. S-
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. Calc. No: CQD .R.AJ.2 6......
Rev: @ . Date:.
3J Proj. No _ J2 la _ Fage .. .L.. 01. 1/5
)
FOR OFFICE USE ONLY - NOT TO DE SARGEilTSL11:3DY ltAS-cad-2.4 SENT OUTSIDE OF SARGENT & LUNDY ,a - ame. Page 8 of 9 5
. . ., . 9 PROJECT NO.: g FILE NO.: CQD- O[n3 7M REV. : OO r -
b)
- Deflection evaluation at critical locations (Active Comnonents only/): .
CALCULATED ALLO'dA'BLE L0 m ION DEFLECTION DEFIECTION
/
e l
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j b d L5 d.li,1 : d [jh/$O..W f '
,, -- = --
Calc. No: CQD ?..U2.36.-
Rev: 00 Date: MM5 Proj. No: f431:Ja_.
I Page..J 1.....Of.. A 1 5 ._.
/
/ H. COMMENTS N
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! ' SARGENT&LUNDY Mas-con-2.4 SENT OUTSIDE OF SARGENT C LUNDY z e - - : _- _ . - Page 9 of 9
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2., An ev4uabien 0% n e TRs Vs RR5 was 3ce her mei anA. documerkedSin S L ?! e.
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Rev. e n Date k[/dY C "'C ^
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? IIE"5' Rev. c o care 9/6/f!
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- X Safety-Related Non-Safety-R elated Page 1 of 2
[ Client CECO, IPC, PSI Prepared by M.DM Date E-2$-83 Project Generic (Agastat Tim Delay Relays) Reviewed by _ O -_ -- -
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SARGENThtUNDY Program ema Nasses. R.v. 00 0.i. 8/23/83 C ** 'C ^
- X Safety-Related Non-Safety-Related Page 2 of 2
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TEST RESPONSE SPECTRA O
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CQD No.: COD- 0 23 7[]
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QUALIFI:ATION DOCUI'ENT ,
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t'o l utne : SO-CL Rev.00 Date: 7/fg O
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REPORT #734-79.002 REVIS IO:' 1
- , hp. 7h , i SEPTEMBEP. 3,.1979 f~2 Y h&k *
- ENVIRONMENTAL QUALIFICATION
{ -
~
~~
OF 'hHE
- r SAFETY RELATED INSTRUMENTF ,
FOR t*
,.m LA SALLE NUCLEAR PONER STATION
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- PC HA3 NOT ret >IEWED THIS REPORT. THIS DOCUMEt4T WILL BE RESTAMPED UP0t1 IPC SUBMITTED BY ret /I EW AND ACCEPTANCE . "
. MCC POWERS -
NUCLEAR SYSTEM OPERATION ,
a s- *
/N
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COPY # 1 MCC POWERC .'. L'ta? OF '.t!. AK CCNTACLS CCAPCAATiCN 5440 Wes: F ar;: A,t:. iw n ,it rEO 77,;3;;; r,;77.ggga
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in,anaa{lnent n enCT REPORT #734-79.002 REVISION 1 SEPTEMBER 3, 1979 . PREPATED BY: 8//'C40 h/dl Date d/3[7S Bernardo S. Arce, NSO QA Engineer APPROVED BY: /9 M M A //u xt V Date 9/6[79 Robert A. Neary, MSO QA Manager // REVID"EO BY: c- Date 9.779
's .
A.'Kanagaraju , Registered PE - q% %' 4~J. i], , ' +N
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W-MCC POWERS 1. UNIT CF MA AK CONTACLS CCDPCRATION 5440 '.Ve:r. For ga A.c . Skc4 c. lL 603 7 7. l3
- 21 G7 7 G500
. I Report #734-79.002 r"'h t , _. , . , .
' \L.J ' INTRODUCTION .
' ~
, * ~
This report presents the results of the environmental ,
. stress program performed on the different instruments (herein called test modules) required for the LaSalle County Nuclear Power Station. This str'ess program -
comprises of the different type tests for the environ- . mental qualification of safety relared instruments required by the IEEE-323-19 74 Standards,- cs i=plemented ,
. by the Regulatory Guide.1.89. Cualification of class
. lr Equipment for Nuclear Power Plants. , /
t Some of the test modules, herein presented, had already
' undergone the stress program under the Wm. H. Zimmer
. , Nuclear' Power Station requirement. However, these test modules were still subjected to further :est since they now varied in the location (=est of these are now inside the secondary containment). The above said modules were only subjected to the loss of coolant accident conditions (LOCA).
For those test modules not listed on the Wm. H. Zimmer Project, they were subjected to successive environments of elevated temperature, radiation, accelerat'ed opera-tional cycling, seismic and vibration exposures, accident radiation and a simulated accident exposure to elevated temperature and relative humidity.
~
-The performance of all the test modules were m< nitored either during or after each type test and then sere co=-
Pared with the baseline data obtained during the initial
.- functional test. '
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e Report #734-79.002 c
,' TABLE OF CONTENTS , ,
s . 2NTRODUCTION i SCOPE 1 . TEST PROGRAM 1 SUBSTITUTION
~
2
~
sumuy , 2 , A. GE TRANSFER SWITCH, SB.4 4 15 , B { GE CONTROL RELAY, HFA51A49 C. GE CONTROL RELAY, HMAllBil 26 D. WEED RTD, 601 . 36 ,. E. LOVE CONTROLLER, MODEL 54 . 47 F. LOVE CONTROLLER, MODEL 56 59 G. LOVE INDICATOR, MODEL 48 71 H. NAMCO-LIMIT SWITCE, EA700 82 I. AGASTAT TIMING DELAY RELAY, 7012AD 93 J. SOLON DP SWITCH, 7PSilAD 104 4 K. W & T CHLORINE DETECTOR, 50-1250 115 L. PYROTRONICS DUCT TYPE ION DETECTOR, CDA-2 126 APPENDICES
, A - CERTIFICATION OF GAMMA RADIATION DOSE 137 B* - LIST OF TEST EQU!PMENT AND CALIBRATIO!, 140 DATA ,
I C - POWERS INSPECTION PROCEDURES. AND TEST 143 - l DATA 1 D - REFERENCES - 197 E - ENVIRONMENTAL QUALIFICATION PLAN - 201 BCC PO;.'ERS QAP 501, REV. C 11 6
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Raport #734-79.002
. Page 93 I. TD1ING DELAY RELAY ,
~
MODEL: Acas tac 7012AD ' .
's_/ '
. s
'1. Ecuiceent Specification The time delay relays function the same way as the control
. relays. The only difference is tha't, before the actuatica of the contacts or switches, a time delay is provided to elapse. Such delays can be manually set if it is of the adjustable type. _
- a. Module Qualified .
Model: Agastat 7012AD ' ' . -Quantity: 1 unit ' b., Operational Specification . Model: , 7000 series ti=ing relay Type: On-delay , Il
Contact:
Double pole double throw (DPDT)
'j Coil voltage: 120 VAC, 60 HZ t'] 'l Nuf Time Range: 5 to 50 secs Ambient temp: -20*F to l65'?
- ' Accuracy of delay
- ! 5% .
l ,
- c. Hardware S=ecification Coll:
1 Type - precision wound potted copper 'J Rated voltage - 120 VAC, 60 EZ - i '1 . Wattage - 8 Watts @ rated voltage i 'i Contacts: , Type - DPDT , Rating - 10 A=p resistive; 1/4 HP 11 Material - Flexible beryllium copper blades &
, silver-cadmium oxide contacts -
R3 port #734-79.002 PCga 94 O
's.<>"
Insulation: Dielectric resistance - 1500 VRMS 60H: between Q ter=inal & cround 1000 V ES 66 EZ between non-connected ter=inals Resist'ance - 500 Megach=s w/500 VAC applied
- d. Insta11atien .
The Agastat 7012AD timing delay relay is nor= ally
. mounted in a vertical position frc= the back of the panel. Four tapped holes are provided in the back plate of the unit.
A panel =ount kit can be provided to modnt the unit in control panels. .
. e. Predicted Desien Life -
10 years - 7,400 cycles
- f. Auxiliary Device Pecuired .
Panci =ount kit (o= tion)
~
I)
%. Auxiliarv switch (octien)
= ~ (
\ .
Screw ter=inals (8 X 32 truss head screws)
- 2. Type Tests Procedure u a. General .
- 1) The test module was =cunted in its vertical and upright position to the instrument panel. Solts 1 and nuts were used to connect the back plate of i the test module. This simulated the typical instal-
-: lation of the instrument. .
NOTE: For the second part of the seismic vibraticn te'st,
- j the test =cdule was rotated 90' frc= its original installatien. *
.i
- 2) Unless otherwise specified'herein, all tests described
- 4 below were performed at atmospheric pressure of i: 29.92 2 2.0 inches of mercury absolute, a temperature of 70130'F and a relative humidity of 50 percent i
1 25 percent.
- 3) Measuring and test equipment utili:ed by EA&T in the
, (~} . performance of the type tests were calibrated by their ,
s/ facility (or another ce=mercial f acility) utili:ing '~ reference scandards (or interi= standards) whose f n , -- - - - e y . - --
R: port #734-79.002
?aga 95 _
?
calibration had been certified by being traceable I" to the Naticnal Bureau of Standards. Appendix.3
\c-)> *
-
- lists the test equipment and corresponding calibra-
. tion data.
- b. Ins =ection and Functional Tests . .
- 1) The test module, its accessories and shipping were
. . visually inspected to insure that there was no .
damage incurred during handling and delivery.
, 2) The test item was then mounted in a panel as described '
in paragraph 2al.
. 3) With no pcwer to the relay, the contactor centinuity was determined using a VOM., ,
.
- 4) .The timing head was set to 1-0 seconds.
5') lWith a voM connected to the contactor, voltage was . applied to the input terminal.
, 6) The time delay before the activation of the switch I was measured using a calibrated stop-watch and com-pared to the setting.
( 7) The data ebtained and the results were documented for comparison purposes with those to be obtained from
. the other type tests.
1 3 . c. Service Ccndition Simulation and Acine Tests a . 1
- 1) The timing relay was subjected to the accelerated operational cycling to bring it to its end-of-life
. usage of 10 years. An oscillater was installed to
. -"---- control the applying and remcving of voltage supply j to the test item. The timing on the oscillator and '
i . relay were set such that before de-energizing the relay, the delay would elapse.
. *This cycling was performed 7,400 times which represents
]j the 10 year life usage. f . 2) For the second phase of this type test, the relay 1 was thermally aged, that is, for a duration of 100
! days inside a test chamber, the temperature was 2 maintained at 160*F and the relative humidity at 5 0 % R.9. Pressure was atmosphericthroughout the duration.
1& -
3 2 CPS) and then the fixture was attached to the exciter shake table. The fixtura was designed to transmit the vibratory inputs without any degradation
'co seismic requirements as well as maintaining the test I
item in its correct attitude. - 3 2) Testing done censisted of subjecting the test fi:cture to vibratisn inputs in one axis, as well as twe axes simultanocusly and independently so that a purely rectilinear motion did not result. Durine the two 7- , axes simultanecus vibration, testing was dcne en the ([ . ' () ,
,follcwing configuration:
l
+
Report #734-79.002 Page 97 Vertical-hori:ontal (lengitudinal) #1 axis Vertical-hcri: ental (lateral) #2 axis ig ,\_ ,
\ /' 3) A continuous. sine wave resonance search was con-ducted in each axis. The rate of change of fre-quency (frc= 1 HZ to 40 HZ) was approximately one (1) . octave per minute or that frequency change necessary to acquire suitable response. The input level was 0.2g peak or 1 inch D.A., whichever is
. greater. Only cne axis at a time had vibration applied. -
I 4) The seismic qualification was performed using a complex randc= motica. Testing was done in two steps with the test =cdule's principal heri ental 1 , axis first positioned parallel with the test table J motion , then rctated 90* in the horicontal plane i , for the second step. .
".ae test ite: was then subjected to 5 OBE's of not
.1
' less than 3C seconde each and 1DSI (SSE) of not less
, than 40 seccnds. .
] , 5} The she:k re:spcase spectrum was plotted for both the axes, and the graphs are shewn on Figures II.0, I1.1, j II. 2 and Il. 3.
1 j () T's m
- 6) During the seismic qualificatica the test =cdule was energi:ed and its perfor=ance was reccrded and docu-mented as per paragraph 2b3 through 2b6. perfor=ance data was then ce= pared with these that were previcusly
., obtained.
- f. Sinulated post Accidenu Cenditions Tests
- 'l) This pertien of the stress program was perfer ed in a
an envireng. ental controlled test cha=ber. Since the
- j test =cdule was censidered to be inside the secondary chanber, it was subjected to both LOCA I and II
. conditions. , , 2) For the first 30 days the test =cdule was subjected to elevated tencerature and relative humidity of 122*F and 90% RS, respectively. This was censidered j ~
the LOCA I cenditien. I ' 1'
- j
- 3) For the next 200 days, the temperature and relative humidity were further elevated to 150 *? and 95 % RH respectively. This cendition represented the LOCA II 2nrameters.
r : ( d
- R port #734-79.002 Paga 98
- 4) The test module was then functionally tested after sCN 7 the exposure using the procedure discussed in ([
(v)) . paragraphs 2b2 through 2b6 on page 95. 5). All the results were documented and then ecmpared to those obtained during the initial functional tests.
- 3. Results and Cenclusien The test module, after being subjected to the different type tests of the stress program, remained fully functional. Based on this, the Agastat 7012AD can therefore be classified as
, Class 1E Equipment for Nuclear Pcwer Plants having identical or less severo operational conditions.
The following st==arizes the conditiens/ parameters to which the Agastat relay was exposed and qualified as a Class 12 equipment: Life Simulation: 7,400 cycles of activating and then de-acuavarang :ne relay coil. Time delay set at 10% of the rating. High Temperature Acine: Long term exposure with a total dur-ation of 100 cays maintaining the temperature and relative bc=idity at 16 0
- F and 5 0 % RE , respectively. Pressure at i . atmospheric value. This expcsure and the above cycling (-
i (sj v represent the device's equivalent 10 year service life. - Nuclear Radiaticn: 1 X 107 rads, total cummu'ative dose of I gamma racia :ca produced by Co-60 source pencils. Seismic vibratien: Prem frequencies between 1 and 40 E:, 1
- input acceleransen up to 12 g's without affecting the device's
- - ~
structural integrity. No chattering of the relay's contacts obtained.
! Eigh Tercerature Accident: Long term exp'osures :
a) First 30 cays a a temperature of 122*F and 90% relative
, humidity; and 1
b) Next 100 days at elevated temperature and relative humidiev
- of 150*F and 95% RH, respectively. Pressure at atmescheric.
- value throughout the exposures. .
; Resonance Frecuencies: NOME detected between 1 H and 40 E:
- during ne acr:: ental and vertical frequency sweeps in both J mounting orientations.
- e s . .
. o -
b)
.c .
~
'g * * " -
~
gh ) TABLE II.0 -
SUMMARY
OF Tile TYPE TESTS' RESULTS FOR TIIB AGASTAT TIMING DELAY REIAY, 7012AD s . . . .
.. y -
w ENGINEERING A Al.YSIS' AND TEST COMPANY, INC. *
! TEST "REQUIREME!!T
_ HEASURED V?,LVC REMARKS I. . Initial Inspection a) When energized (120 VAC) Ia)
& Functional ,
verify that timing relay Verified at set time of 40 sec., switch The Agastat timing activates within 10% of relay remaind func-set time. activated at 38 sec. tional throughout
- Ib)
Verified the Qualification II. b) When activated, verify Program. When set iia) Verified at set time i Post-Cycling that terminals 1 and 5 of 40 sec., switch gtime was 15 - 20 sec., the switch are closed and terminals activated at 38 sec. 3 and 5 are open. activated at the IIbl Verified set time. When set - III. . time was 40 - 50 Post Thermal , IIIa1 V rified at set time 3 [y{tcha tvtd activated at 38 sec. 2 - 3 sec. after th" ""' 'I""*
. IIIb1 Verified IV.
Post-Radiation ' IVal Verified at set time . of 40 sec., switch
- l. EE activated at 38 sec. j 'o V. '
-
- Ivbl Verified
~
, N, Post-Seismic -
e
,- Val . Verified at set time *
, . ; ,, of 40 sec., switch a
. activated at 38 sec.
y ( l Vb) Verified VI. . d Po s t-LOCA
- Vial Verified at set time 'o o
, of 40 sec;, switch "
activate at 38 sec. VIb) Verified e .
O(m
. JD o
L. REC. I10 ' GROUP C . _ .,, . DATE: 4-18-78 100 .-
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- lloRIzot:TAL AXIS (Y-z AXES)
AGASTAT TI!!ItJG DELAY RELAY,.7012AD - I 't ( , h
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Raport #734-79.002
. Paga 140 I
on 1 s 4 3 . 1 4 t APPENDIX B . 1 m am . 1 i A U2 M. .e;am. PM %te**C.U A .a -m.4'm. 9 CALIBRATION DA"A ' e t We 'ge ) i .
, e
- NMN baeg
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+n, ,=w--w'v+
Rsport #734-79.002 Page 141 4 rs - TEST EQUIPMENT CALIBRATION DATA
. ^
~
Wavetek Function Generato:'!!odel 110 Oscillators =* Calibration #820043 Calibration date: 12/17/76 12/17/77 . Wavetek Voltage Controlled Generator
- - Model 111 -
Calibration #202953 Calibration date: 8/4/77 8 .
~
Counters VEEDER - Root
- I.D.
iT120506 . VEEDER - Root
. I.D. 4B120506 .
ss . Temperature Controllers THERMAC Controller -
-' Research, Inc.
Calibration #120743 on 9/26/77
. due 9/26/78 Resistance Meter - LEEDS and Northrup Type S Test Set No. 5300 Calibration i 050993 Calibration date: 3/23/77 3/23/78 ,
l i* -
* - ~ .
Ammeter " General Electric ~ l* A.C. Volt Ammeter Calibration #82004C . . l . . Calibration date: 7/12/7.7 7/12/78
- e
. Page 142 l c
- 1
. ( ..:_: . .
( . w- . -
. inclined Tube ==== Mannometer Catalog 140GD/ONM-4
.Mannometer Calibration #66130
, Calibration date: 10/4/77 *
~ .
, due: 5/24/78 '
recalibration date: 5/24/78 du.e: 1/r9/79 Radiation Dosimeter
- Radiochromatic Reader Model 401 Far West Technology, Inc.
. ' ' I.D. #675009 Calibrated while in USE '
Water Colu=n - MERIkM Instrument Co.' Pressure. Source Calibration #66136 - Calibration date: 5/24/78
, due: 1/17/79 .
Air Pressure Gage - Laboratory Test Gage Calibration #66103 (' -
, Calibration date: 8/1/78 (])
due: 3/23/79 (_ )v .
- Voltage - Oh= mete. FLUKE 8000A Digital Multimeter
.I.D. 5346678 Calibration #25757D
. Calibration date: 11/11/77
- due: 5/13/78 i
recalibration date: 5/10/78
. due: 11/10/78 FLUKE I.D. 4269889 8'000A Digital Multineter, Calibration #257573 Calibration date: 11/8/78 "due: 5/3/79 c)
\ <
(\ V I
. * *8" ' ' ~
%' M $ *#'& * * ' ' * '
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Report s/J4-iv.vuz Page 143
<W - '
en _ .e .
. APPENDIX C P'OWERS INSPEC"' ION PROCEDURES g .
TEST DATA OBTAINED
~
4 I . I i I
- i -
l l l l i . ; i
- a .~. = . = ~ . . :.w .umne., i. . .
. ..- . . . =
- FtMr n*, ft[
neconn b*seccnou f 0ff CO'.w'ANY 73 - m ,.. J W. y,.nOy ! gy#,;y -
- HUCLEAf. e sirM", of'ETTATIOrt ,
y g OHAWING NUMUC H nEv. . L Ari tt#:;f riuvtNT NO. PART NUf.t0E A'
- p v 5 t ti.t i;u st g E n -
d b;'. Cat: Pf aO*8 . . L.A2.I,% t E c outJfY /WaA . d. Farus A4E37. * ' rauct.sua. Powe'.t scaricas @(e Soi D QlA 7012 1.0- PJIA' 5 /W7tE P.O o, M.T.O. til .I f.CilutJ VOttJ T SHCET fauM0ER LOT P Aft I L5ib.Mib*t MS ""C"I"I"9 MA I# 1 or 4 i ! 4 TIMI: C RELAY , Il[f.fJ.M.fl. * 'If;5 P. ElY **O. DAY
. )
/.*.N U; d5[.L il ';PEC. N UM UL il LOCAllOff .
AcASTAT _ t[A J . _ _ . _ _ _ .U . S .O ./CAurc9.OlA 4]A m . _ ______. _ RP 6l lT INSPECTIOtJ PHOCEDURE RESut.TS STEP - CHARACTEnlSTICS
- 1. pACKAGI;;G L. Visually inspect and assu're -
1E 'Is the unit packaged? Timing Relay is in. Etyrofoam [e\ proper packaging and labgl Ye)s no container identified by Agastat s'in sfo rma tion . .
/j' labei having the fol' lowing AcAstAT Timing nelay ,',/ ib. correct?
}/s the label information in formation :
- 7012 An 120V at 60 hz Tining Relay Yes No 7012 t.D 120V at.60 hz \S . to. T .1 C 1' .X.\. J'ho~I'neconds /' .
S t.o 50 seconds
?'
.. /
W 2 VISUAL -
,.... l
'{
fro,h./\JQ-N Agastat timing rol y is to b 2 Unpack unit m..shippingt con 2. Recorbth.e following: , identifiedby-labelwhichstaDes\ :. tainer 'and verify < the folio'n-
/ ing nam'eplate inforsatlon -
2a)ttodel 70M-AT) - Model 7012IAD X 2a) Mod lel 70.12[.AD',g. _f' 2b) Coil l10X/j 40 [/ .2-- Coil 120V At 60 HZ 2b) Cott 120v .6p h=C,/ -/ time 5 - 5 0 's c . 2c) Timb 5-50 2c) Time _.rr,,G - 9 o $c~ C .
? c e e (' ./ '
/
z Unit shall be free of any/a Vi' o.916. 1 e' '?I*
~ f' '%
'7" 9
~
[kl}for' _l I.$.A the .'.Y- <
-following: ,
signs of damage or eviden f - 2d) Chec . 2i ) Are there visible signs of poor workmanship, handling or . '.: damage or de forcities ,w storage. J .._ De formity .in phys ical - . 3,g appearance.. ., Yes tio . oo
- Cracks, voids or other r, visible damtige'to unit 2e) 1 A the proper adjusteen&
This unit should hav . an adjust- / case. \.s N knhbpresept? 3-cenc knob scaled uitt timing / .: . range of ,4 to 50 s'qconds 2c) Verify presence of adjhte, *yIs , no 4
-l s... - nient knob trith vnnga of Z' r . c. n i. .:. .n <ln , o
() f , .. . . . . . . .__ . , .g ,) . y,
POWLit*J llLGOL JII t.Ovewsv l._ -- , , RECORD OF INSPECTIO[. TINUATION SilEET yQ y{') ^~ *
- fJUCLEAR SY!, Aa (11ATIOtt .
* '
- E PAflJtJUMDEn PL At1 ItJ5TRU!.tEt4T P40. Sh! ET .N 3. -
I Ci$0 lit 7Ts0 4 . PAlli DESCfilPTIOr# G uA QuMTY /WM- 4. EiMME!1t. .
- TIMIt10 RELAY -AGASTAT 7012 AD M/A 2et 4-
_NL%t%tt hnci STAmg If JSPEcTIOld Pfl0CEDURE RESULTS f EP CilARACTERISTICS . Y
. 4 2f) Arc eight terninals with Tncre are eight terminals on 2f) Verify presence of eight - screws present? o face side of relay, edch with terminals with fastening ,
/ j' terminal fastening screw. screws. .
~Uo Tes \/ r
. L
~~
- l. FU!!CTIONAL -
3a) Rotate knob to assure free- 3a) knob Will the timing adjuste:ent Suitching time is set by rotat- dom 'of moverrient. . rotate without i ing scaled knob obstrue ion? -
,Yes No .
Terminal Layout m :o .. m <n
* $ = .
' - , va w
In normal state, terminal 3 is gg '
- e
* '."; r V
cl'osed with terminal 5, terminal ,I
- 4 is cl.nse<3 wit.h tnrminal 4 sind . _ , M,,y . ,
+
,8
' s r t, .
nerninals 1 and 2 are open to each other and all other termi-Af ter the set delay i[up f 4 Y- -
'~
d b, r. nals. U81"E.an ohmeter, check the, , c ceriod, terminal 1 uill close " f Llowing by measuring
- resistant et ,
'.eith terminal S and terminal 2 pen 3b) verify that terminals 3&5 3b) Are terminals 3 6 5 close.d?
4 1 e
? 1. n 1 are closed.
to each other and all other '
"I"" "" 3c) Verify that terminals 4 & 6 - -
9 s. are closed. 3c) Are terminals 4 6 6 closes. - c.
\ - ~\ 3d) Verify that terminals 1 & 2 Yes / Mo r. ,
5 are open to each other and all other terminals. ~ 3d) Are terminals 1 & 2 open E
* ' to all terminals? h
~
Yes / ,,o i. I i i
-. . -- ..... . _ . _ _ . y
*i
' l a isvi siJ it. -:.i n iv i b,.. . ,... o -
?- ,
l nECORD OF INSPECTIP* ONTINUATIOf4 SHEET {s3, , NUCLEAR, OPEflATIOff .
/ ,
PLAN INSTRur.t EfdT N3. SHE".T is FART NUMBER PART DESCftlPTIOr#
.ca ciscrurticr4 .,, 7012 AD M[A 3 er-LA 3.e.u.E. cdOMTY[lAIM. N. EIMMM TIMING RELAY - AGASTAT ,
M:.!cLE .i.v PMGil. d'AT* .*JS ' HESULTS CilAll ACTERlSTICS INSI'ECilotJ i'itOCEDURC . 51 E/ 3e) Are the two "M" terminals e 3e) tified The two coil terminals id'n-closed?
~ ~ -
by "M" are to be
, 38 8'ed * [ ,' [1 dt
- closed, as measured by minimal' resistance. Yes / No N OTE ' M o 'i b /s d?d ol...s.
f/g (o ,k e t. p n LA..'.!l.* /" 7 A- A 120 V AC pouer ' supply and - 2 ,, /
- MA. stopuatch is needed to determint- ,
,, * / 3,j, .77, switchi.ng operat,lon,. Connect
?
.t power supply to M terminals with power off. Set timing relay to 15 seconds. ,
3f) Turn on power and record 3f) Time until switching seconds. - time until terminal 1 closec occured: I.f
@ tf sec.. .
I,.f cec.
- with terminal S. Switching p*
- - time must be within 10*/. of - -
@ II 58" set time. ,
.' 3g) Terminal 3 must be open to 3g) Is terminal 3 open to. ,
terminal 5. . . terminal 5 7 *
. Yes / No Turn power off. Reset timing * -
* . relay to 40 seconds. .
3 39 ,,c., 3 //O Sec. 3h) Turn power on and record re- 3h) Time untxi switching lay time until termin'ial 2 occured: 3 F. - secori h, //O sec.. clo'ses with terminal 6. , yy
. in m m g Switching time must be with-i w rt in 10% of set timo. - -a 4 -J :st 3j) Terminal 4 must be open to 3j) Is terminal,4 open to .*o;je- i terminal 6. terminal 6?
Yes f/ No b' RE!40VC POLHIR - I i - - - - Q
.g-)
() ... .
. - ~ -
< gs. *
,. s
'g, ) ,
- POWLHS llE{k nECOnD OF INSPECLj CONTINUATION SI(EET nCOMPAffY .
- h, NUCLCAn 3Ysit.M5 Ol'CilATIOra PAftT fiUtADER PLAtt ItJSTflut.lEt4T P40. SHEETt.C i
PAtlT DL5CittrT10tf b-N'$'..$UMTY/WM 7012 AD Allk b ($t.'.:GL.G2 2. FO M SfNf'10MS
. , n. 28Mn ,'"C " REI.AY - AGASTAT RESULTS CilAAACTEniSTICS itJSPECTIOrl PHOCEDunE ,
STEP , ,,
~4~ 5CCESS0! LIES AND IllSTitUCTIONS 4a) Verify presence of installa- 4a) Is proper bulletin present'.
tion and operacion bulletin.
~
Included in A Castat Timing Relay
- Yes _ No shipping container is an install- .. .
- ation and operation bulletin *
~ *
- Record disposition of
,Acpeptance or Rejection , , Accept Rejdct, -
=* . . .. .
. r ',*
s ,
. s ** ' e e 'o 9
.. v.s o
- e * *
. = , , @D OO
* . .. . tl H tt
'J 8
.' m .n:
-J
*
- us
.e of.
, * . 4 m
. . o o
. . .t - as
, e
= - *
?
l , ,
~
I 1 ,
Ea E I CO., $C, , Report #734-79.002 i- ' Paga 19 0-
%76 603iiiaLTY it'ay
~
E!!)TE 21; . TEST LOG SHEET SRDR DEL REY, CB. 9029L . , .
,g iL: (213) 82 2-G931 PROJECT 110.: /$ o / - d/ PAGE / OF /
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, . QUALITY ASSURACE PROCEDURE 501 REV'. '6 .
ENVIRONMENTAL QUALIFICATION TEST . PROCEDURE FOR SAFETY REL'sTED, O INSTRUMENTS UNDER , SPECIFICATION J-2591 .
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POWERS REGUL ATOR CCT.*PANY . ! QUALITY #C. A .NC: NUCLEA R SYSTE*.*.S OPE R ATION l PRCCC UdC T'rts c,A,p . 0 ,,, l JA ENVIR0 RENTAL QUALIFICATION '* * ~
' L) m 3 -/S-PROJ4 CT aY' t LASALLE COUNTY STATION - UNITS 1 & 2 Aco,v l~Tib 7-s t-1.0 PURPOSE -
To de$cribe the procedure to be utilized for the envirorr. ental qualification testing of safety . l- . related instr =ents for Nucl' ear Power Plant applications. i 2.0 SCOPE 8 I This procedure applies to safety related instr =ents for which project specifications require their cualifi-cation in acccrdance with the. requirements of IEEE-323-1974 Standard, as i= lemented by Regula cry Guide 1.39, Qualification of Class lE &quipment for Nuclear Power
.. . Plants.
3.0 DEFINITIONS - ' 3.1 Safe ty Related Inserments - i Instn:..ents that are essential to eterzencv reactor shutdcwn, containment isolation, reactor c'ere cooling, and centain=ent and reactor heat re=cval, or othentise are essential in preventing sitnificant
=clease of ' radioactive caterial to the environment.
3.2 Tvue Tests - Tests cade n one or core sa=cle instr =ents to verify adequacy of design and'=anufacturing processes. 3.3 RAD (Roentgen - Absorbed - Dose) . Absorption dose of _100 ergs /gm (caterial) . The rad is a measure ot rad:. aced encre. absoretion of g any for (p article or electrccagne' tic) in' any l . material. 3.4 0ctave - The interve.- between two frequencies which have a
. frequency ratio of two.
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W L.J gV s PnORCT [- ' f LASALLE COUNTY STATION - UNITS 1 & 2 Ann,,D Y S-7-77 s 3.5 Occratine Basis Earthauake (OBE) That earthquake which produces the vibratory ground motion for which those features of the Nuclear Power j Plant necessary for continued operation without ' undue risk to the health and safety of the public
, are designed to remain functional (excerpted from i
- IEEE-Std. 344, 1975). !
3'. 6 Desien Basis Earthcuake (DBE) . That earthquake that produces the maximum vibratory
~ '
ground motion for which certain structures, systems, and components are designed to remain functional. j 3.7 Required Input Motion (RIM) '
.The required input motion to the equipment under test is the amplitude of acceleration expressed as a function of frequency that an equipment shall withstand and still perform the required functicas.
fs i bs s 4.0
- PROCEDURE 4.1 General .
4.1.1 This procedure outlines a generic environ-mental plan developed to qualify instruments of the Powers Regulator Company for Nucrear Power Plant installation. The procedure desc:ibes the type tests to be performed
. on the instruments in a specified order.
The sequence used is the one recommended by
.the IEEE-323-1974 Standard and briefly.
, , consists of: -
4.1.. 1 Inspection and Functional Tests
.- 4 .1. .'. 2 Service Condition Simulation and Aging Tests ~
4.1.1.3 Irradiation Tests 4.1.1.4 Seismic' Vibration Tests i
'4.1.1.5 Simulated Post Accident Conditions
- Tests ,
- 4.1.1.6 Final Inspection and Functional Tests 4.1.1.7 Seismic Fragility Tests /
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POWERS REGULATOR CC..tPANY cuAUTY M 5U AI.N E NUCLEAR SYSTEF.tS OPE R ATION PROCIOUAE 501 ?
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ENVIR0h3 ENTAL QUALIFICATION Pare -- e d4 3 W , .cac e, LASALLE COC;TY STATION - UNITS 1~& 2 [ymM-teg e .4 7 7 4.1.2 The type tests shall be applied to one instrument from each different family.
- Design verification does not require that
~
more than one unit be tested. The instrument
.to be tested shall be randonly selected production codel. All of the different
- tests and conditions shall be applied to the sa=e instru=ent. Appendix 3 of this procedure lists all different instru.ents to be subjected (one unit of each) to ,
type tests. .
. 4.1.3 In developing this procedure various docu=ents, NRC regulatory guides, IEEE standards etc., were consulted. Appendix
. A of this procedure lists all references.
4'.l.4 Unless otherwise specified herein, all tests described by this procedure shall be per-forced at an at=osphere pressure of 29.92
+ 2.0 inches of nercu y absolute, a te=per-ature of 70 + 30F and a relative hu=idity
. -of 50 percent i 25 percent., .
4.1.5 Instru=ents shall be counted in a canner
, and. position that best simulates the expected installation. The tests and instru=ent perfor=ance shall be =enitered using equipment that provides resolutich
, for detecting ceaningful changes in the
, measured variables.
4.1.6 Measuring and test equipment utilized in
', ' ' the perfot=ance of the type tests shall be calibrated 'cy the test facility (or
' . ancther ce=ercial facility) utilizing rehrence standards (or interin standards) whose calibration has been certified by bei.ag traceable to the National Bureau of Standards. All reference standards
, ut!.tized in =easuring and test equip =ent cal'.bration shall be supported by certificates,
' reports, or data sheets, attesting to the
. data accuracy, and conditicas under which the r,esults furnished were obtained.
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ENVIRONMENTAL QUALIFICATION. 7:q U enonct uv Ch ;q _ l ~ h LASALLC COUNTY STATION ' UNITS 1 T. 2 AwMI M -' 4.2 ' Inspection. and Functional Tests !! 4.2.1 Instruments shall be subjected to inspection and functional tests to assure that there
. is.no damage due to handling since manu-facture and to verify their perform ance is in accordance with design and project specifications. All inspections and functional tests shall be performed in accordance with written procedures and the results shall be documented. Inspection . .
. . and tests procedures are developed, docu-
. mented and controlled in accordance with Powers Quality Assurance Manual, Sections 5-1 and 6-1. Typical inspection and test procedures for sample instruments are presented in Appendix C of this procedure.
4.2.2 Functional tests performed extend, as a
, minimum, to a simulation of instrument
.~ operation under normal conditions. Results es and data obtained from functional t,esting !._)
() - shall be used as a base for comparison with instrument performance under core
- highly stressed conditions.
4.3 . Service Condition Simulation and Acine Tests
-4.3.1 The objective of aging is to put instru-ments in a condition equivalent to the end-of-lf "e condition and to verify that they shall perform their function after being i subjected to normal environments during their design life.- -
4.3.2 These type tests may be categorized in two phases: The first phase shall consist of
. accelerated operational. cycling of instru-ments to simulate the expegted mechanical wear and electrical contact degradation of the instruments being tested. Table I of Appecdix ' D of this procedure lists all inst:uments, the number and rate of cycles
-f - as well as comments on how cycling is to be ,, accomplished. Operational aging shall be
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performed on parameters, which are directly ,, related to the operation of each instrument. . 2 j(sj
'. The second phase shall consist of thermal
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Table II of Appendix D of this procedure provides a schedule of the temperatures, pressures and humidities under which thermal aging shall be performed. 4.3.3 At the completion of the Service Condition Simulation and Aging Tests each instrument shall be inspected and functional 1) tested
- and results shall be documented ~as described in paragraph 4.2 above. Performance. data shall be co= cared with those that were .
= previously obtained and any deviations shall
- be evaluated.
4.4 I; radiation Tests -
. 4.4.1 - The objective of the irradiation tests is to subject the test instruments to radiation doses anticipated in the design life, and as a minimum, one Design Basis Accident.
The irradiation test dose shall be the total of normal and abnormal doses. 6 '
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. 4.'4.2 Irradiation shall be performed in. a radiation chamber with Co-60 source pencils. The
. exposure shall be of Ga=ma radiation and the total integrated dose shall exceed the total of normal and abnormal condition doses. The
- instruments will be operated at regular intervals to verify their proper performance.
4.4.3 The aceponents shall be arranged in the chamber and then the chamber shall be loaded with Co-60 source pencils. The .. chamber temperatura shall be maintained se approximately 70F and the pressure shall be the atmosoheric. The dose rate shall be
. appraximately 1000 Rads /hr. unless otherwise specified, and shall be che:ked and verified by. optical dosimeters as well. As a minimum the operation of the components shall be checked at 1000, 5000. 10 000, 50,000, 1X1CI, 5X105, 1X106 , 5X105 and 1X107 (as /h applicable,) Rads of integrated dose.
After the irradiation tests are completed,
- the instruments shall be functionally
. tested as described in paragraph 4.2 above.
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'4.4.4 The total integrated service life radiation dose varies with instrument location in the .
Nuclear Power Plant. Instruments are classified as being "Inside the Secondarv Cone.ainment" or "Outside the Secondarv
. , Containment". Tables LII & IV or Appendix
'F of this procedure group the instruments in accordance with the above classification.
- Tables V & VI of Appendix F list the total required test radiation levels for both groups. .-
. 4.4.5 Instru=ents classified as being located "Inside the Secondary Containment" require a much higher test radiation dose than those "Outside the Secondary Containment".
' To facilitate the test comolecion in a reasonable amount of t4-a hhese instruments shall be exposed to radiation at a higher dose rate of approximately 1 Megarad per s-hour (unless otherwise specified) . The
. . higher dose rate shall be attained by
- j Cd. . . increasing the nu=ber and concentration of
. sources. . -
[. 4.4.6 All. ' instruments shall be functionally tested
- after cocolecion of the irradiation tests and as described in paragraph 4.2 above.
~ Performance data shall be compared with those that were previously obtained and any
,evi d tions shall be evaluated.
4.5 Seismic Vibration Tests 4.5 '.1 The objective of the Seismic vibration Tests is to verify that the operation of the test
. instruments shall not be imoaired when
. subj acted to a minimum of five (5) Operating Bas: s Earthquakes (OBE) , followed by one.
Desi.gn Basis Earthquake (DBE).
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- l d.b ' ENVIR6UMENTAL QUALIFICATION ' * -- 7 -- 19~ l i U caosccr LASALLE COUNTY STATION.- UNITS 1 & 2 B y, 4 gojijs $.- 3f# w/e[_ *P' l 4.5.2
. The test items primary mounting point shall be the normal mounting attachment provided
. en the test items which shall simulate the actual in-service counting. The test items shall be attached to a rigid fixture (natural frequency > 33 .cos and then the fixture shall be attached to the) exciter shake table. The fixture shall be designed to transmit the vibratory inputs without any degradation to seismic requirements as well as maint,aining the test item in its correct attitude. .
.$ 4.5.3 Testing shall consist of vibration inputs in one axis, as well as two axes simultaneously and independently such that a purely recti- Cs linear motien does not result. During the
, two axes simultaneous vibratien, testing shall be conducted in the follewing configuratica:
Vertical - Horizontal (lengitudinal) #1 axis Vertical - Horizontal (lateral) #2 axis
- 4. 5'. 4 A continuous sine wave resonance gearch W
- The rate of change shall of -frequency in be cenducted (1 each H: to 4axis. IO H:) shall be approximately one octave per minute, or that frequency change necessary to acquire suitable response. The input level shall be 0.2g peak or 1 inch D.A. whichever is less .
Only one axis at a time shall have vibration appli2d. i 4.5.5 Seismic Qualification shall be performed I using a complex random motion. Testing shall be perforced in two stens with the test itens ' principal horizontal ax's i first positioned ' paral'.ed with the test table motion, then
. rotated 900 in the horizontal plane for the secaid step.
The test items shall be subjected to 5 0.3.E. 's ) of not less than 30 seconds cach and 1 D.B.E. l l . (S.S.E.) of not 1ess than 40 seconds, l e
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' QUAUTY AS';UdAi CO POWERS REGULATCR cot.tPANY NUCLE A R SYSTEf."l C PE R ATION PROCEDURE
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. LA SALLE COUNTY STATION - UNITS 1 & 2 AbadT E N7 /h' 4
.4.5.6 In establishing the required input acceleration the following considerations are given. The test instruments may be panel counted, field rigidly mounted or field flexibly mounted.
. - . Therefore, the required input motion shall - be different for the major.ity of the instru-l e ments. However an overall qualifying required input motion shall be established
, in the following manner:
4.5.6.1 Control panels shall be ' seismically
. qualified through a combined test -
- -- and analysis program.. The Required
. Response Spectrum for all directions
~
/ ,is shown in Fig. 1, 2, & 3 of Appen- A
* , dix E of this procedure. The peak /C\
acceleraticn of the various instru-ment locations shall be obtained l from the analysis. This peak acceleratica shall be used as the
, input (test) acceleration for the
~
seismic test of instruments. /' {} 4.5.6.2 For field rigidly mountei instru-ments the required input motion p
. is provided by the Architect /Engi-near and peak accelerations for
/C\
'various frequencies are shown in Table 1 of Appendix E.
i 4.5.6.3 For field flexibly mounted instru-ments the same input motion shown / \
- . in Table 1 shall be applied.
4.5.6.4 From the above a required input motion shall be established which
, envelopes the required input motions from 4.5.6.1 and yet produces a test -
input motion a which envelops the /C'\ Required Input Motion as shown in Table 1 -of Appendix E. In any case the peak acceleration shall '
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be equal to or grcater t_han the Zero I
! , Period Acceleration except at low ! . frequencies where the value of the
,! Required Responsr; Spectrum decreases below and stays celow PA or the in-Q) Put acceleration is limited by the (,s3,' v . test table capability.
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4.5.7 A control accelerometer shall be counted adjacent to an input. counting point. - Additionally, one vertically oriented accelerc=eter shall be located at the center
. of the table for verification purposes.
4.5.8 During the performance of the'seis=ic testings the control accelerometers and
.' response accelerc=eters shall be per=anently recorded on a galvano-=eter oscillog ytph.
~
. The' control accelero=eters outputs for the complex rando= tests shall be routed through a shock spectr c analycer and the data
. presented as peak response of frequency. .
4.5.9 All instr =ents shall be enerriced (as
'. applicable) during the perfor=ance of seismic tests. Output response (such as pressure, cur ent, posifion, et-c.) shall be monitored throuzhout the test. Switch contacts shall 5e conitored for chattering
. using a chatter detector with a chatter
. gate tica cf 1 =sec.
4.5.10 Upon co=pletien of the seismic vibration tests all inst u=ents shall be functionally tested and results shall be docu=ented as described in paragraph 4.2 above. Performance data shall be co= pared with those that were -
. pre iously obtained and any deviations shall the waluated. -
4.5.11 After co=plet:.cn o: Si=ulated Post Accident Conditions Test (see Paragraph 4.6 below) all instru=ents shall be subiected to a /\ Fragility Testing. Figure 4'of Appendix E 'A sha'.1 be used as a guice for the Required Input Motion. The =axi=un level shall be appcoached incrementally,in steps of 257. of the RIM. . 1 4*.6 Simulated Erst Accident Conditions Test
~
~ 4.6.1 The objective of these tests is to verify the capability of the equipnent to operate under
- a. postulated Design Basis Accident.
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LASALLE COUNTY STATION - UNITS 1 & 2 M Y. Am* # 0 ~ ' -E The Simulated Post Accident Conditions Tests shall consist of exposure to radiation, pressure, temperature and humidity. The post accident exposure.to radiation has been combined with the expected in service radiation exposure as described in paragraph 4.4 Irradiation Tests. . e 4.6.2 The Simulated Post Accident Conditions Tests shall be performed in a controlled envirch- . mental chamber. Table III of Appendix F .
. lists the instruments located "Inside the i .
Secondary Containment" and the cest variables (i.e. , temperature , humidity, pressure) and time profile are shown in Table V of the
.' same Appendix. Toble IV of Appendix F
- lists the instruments. located "Outside the Secondary containment" and the test variables and time profi14 are shown in Table VI of the same appendix. When the h
same instrument is used in both Inside and (~i C/ y' Outside the .%cendary Centai=ent arecs, then it shall be subjected to the Inside the u l
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. Secondary Containment environmental conditions. f
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4.6.3 All instruments shall be monitored during the ' performance of these tests. Upon completion, the test instruments shall be
. .. funct:*onally tested and results shall be
.recor ad as described in paragraph 4.2.
4.7 Failure AnalvsIs 4.7.1 Should a failure occur during the qualia fication test process, this does not . necessarily constitute a failure to qualify.
- In cenjunction with the instrument manufacturer
, it st all be determined if the failure is l randcnn or an end-of-life failure. True
- random failures by definition do not impact I-3: qualified life. All failures shall be p -
reporced to the Architect / Engineer. - - 1 - 4.8 Margin shall be applicd to voltage and frequency only
- since adequate margin on the rest of the environmental factors has been included by the Architect /Cngineer in the specified conditions. Thus, instruments shall
'}'
be tested prior to scismic " fragility test at i lot of - rated voltage value and I Si of rated voltage frequency - (as applicabic). >
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V rnoac1 LASALLE COUNTY STATION - UNITS 1 r. 2 ovffiL*17-. wJIh719 7 7' 4.9 'Accentance. Criteria and Oualification Renort
- 4. 9.1 To meet the provisions set
- forth by IEEE-323-1974, the qualification program must be accompanied by a detailed report document-ing'all the tests, data, etc., and the acceptance criteria.
- 4. 9.2 TheacceptancecrkteriaforServiceCondition Simulation and Agh:g are the success ful
. simulation of the tests. The instruments .
- must perform under the simulated accelerated
' ague process uithout the loss of function
- and structural integrity. ,
- 4. 9.3 The acceptance criteria for Simulated Post Accident Conditions recuire that loss of
. performance or calfunctions shall not occur, 3
loss of input and output shall not occur, structural integrity shall be maintained, and spurious signals shall not be produced.
. 4. 9.4 The, acceptance criteria for Scismic tests
. require that. structurr'_ integrigy shall be !
- maintained, loss of performance or cal-
. function shall not occur during and after i
~
the excitation of one Safe Shutdown Earth- -l quake and five Operating Basis Earthquakes.
- 4. 9.5 A qualification report vill be prepared and cictified by a registerad professional engineer. The report shall contain all the detailed test procedures, measurements, description of test instrumentation, fixtures, calibration' data and interpretations, .
, and data on, and explanation of any malfunc- ,
tion t The following infor=ation as a minimum shall be sitbmitted: .
.. Noticos of Deviation, .
i Sinusoidal Accelerometer Response Data, - I- Zero period accel'eration control data, t . '. . Response shock spectrum X-Y plots, Photogrs.phs for each axis and accelerometer p
,,) -
. configuration, Test equipment description and calibration da_ta,
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- Peak Acceleration Values for Rigid and Flexibly Mounted Instruments In each of the two hori:: ental directions = 3.0g In the vertical direction = 3.0g e
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G.ECKLIST FOR SUPPORTIflC CALCULATI0f! O Project No.: 4536-32 CQD No.: CQD-OU/jj volume: SQ-CL Rav. 00 Date: 7/fgg
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PROJECT _ _ % lN O N.~/. CALC NO C_OD- Od3 73 6 R EVISION'._P O _ PROJECT NO kd3 b ~ N REVIEWED BY - Ud' 1//61 ATE . p (signature) j Ll l A. CONCLUSION OF REVIEW Accepted Rejected Comments: .- B DESIGN INPUT DATA B1. Has the input data been approved for use? (
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g ,Q'q,ee; W c n.'e.,n.- . 7y f Lv.J Yes No , Comments: i
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- 82. Is the input data applicable for this analysis? 1 YYes No Comments-C. DOCUMENTATION C1. Does the analysis include, as applicable, purpose, input data, assumptions, and references?
Lk'.1 Yes No 1 Comments: s {.
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a .: { C2. Is the analysis properly documented,in accordance with Quality Assurance Procedure GO-3.08?
,d b Yes No
, $ Comments:
a N i D. TYPE OF ANALYSIS (Check one or Doth, as applicable) Hand-prepared design calculation.
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Computer-aided design calculation. ei *' E. TECHNICAL ADEQUACY 6 8 E1. Assumptions Are the assumptions used valid? Yes No 6.
<o Comments:
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'i"5 MECHANICAL DEPARTMENT STANDARD o "k c fs' . .f 5!,,,.. . Il u '$[.
t CHECKLIST FOR NONSTANDARO r u.t mast :a :,,. .. : ts - a... i L. ut- NUCLEAR SAFETY-RELATED ANALYSES 1
.i FOR OFFICE USE ONLY - NOT TO DE l SAUSENTALCIDY m - m -2.t 4 SENT OUTSIDE OF SARGENT & 4. UNDY 9
inne eenau Page61 of{3 r
PROJECT NO b3 ~3S _ CALC NO COD-O/3~/dd_ REVISION. OO o\s .
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v E2 Modet is the ar alytical model(s) usec adequate for this application? b Yes O No Comments __ Complete E3 and/or E4. depending on the type of calculation. I E3 Hand-prepared calculat, ion e. 1 [. j
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E31 Method of resiew The review was conducted using. !$ dud Id iC zi _ .?* ~ :.: C '.'
- A detailed review of the original calculation .
O A review by an a!!ernate. simplified or approximate method of calculation. b A review of a representative sample of repetitive calculations b A review of the calculation against a similar calculation previously performed E3 2 Are the hand-prepared calculations technically adequate? b Yes O No Comments: E4 Computer _ aided delgn calculation E41 Program Acronym _ . . _ _ _, ._ Program Number-s E4.2 Run I.D.(s)/Date(s). / E4 3 is (*ie computer program applicable for this calculation ? Yes No E4.4 is the program maintained in Computer Services Division-control d files? Yes No-Has the program been validated in accordance h Appendix H of CSD Standards and Procedures Manual (GOP 4-1)? b No Yes-a) Provide validation doc entation file no.: b) Has it been docum ted that the program used is identical to the one va:idated? O Yes b No - h E4.5 is the computer progra nput correct? 92 Qi Yes No O E4 6 Does the pro m input contain sufficient accuracy to produce results within any numerical 9* m limitation the program?
<? dY No 23 E, E4.7 re the computer results consistent with the input?
oo uc Yes No (, FOR OFFICE USE ONLY - NOT TO BE ' SENT OUTSIDE OF SARGENT & LUNDY [ g- b I e u H l! MAS-CQD-2.1 r- -",se esaal Page{2 of E.3
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PROJECT NO CALC. NO.: COD-8/3 72d REVISION _O_O____ f V E4 8 Are the results correct and within stated assumptions and limitations of the pro r Yes b No W/A E4 9 Are the computer-aided calculatio ally adequate? Yes N Comments-v7 :n e.s
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i 1 O - 1 4 SUPPORTING CALCULATION- , l Pro]ect No.: 4536-32 CQD No.: CQD- 023 73 f Volume: SQ-CL Rev. 00 Date:f i's/g 1 ( F) O' l l l
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O REFERENCES & MISC. DATA O - 4 P r.T 7 p c t No.: 4536-32 CQD No.: COC- 033 73_. Volume: SQ-CL Rev.Of Date: i 'p , 'gg-- (G) O
6 SARGENT & LUNDY , INTEROFFICE MEMORANDUM 1
} 7/
tO V From Y. A. Patel - 30 X-6772 Date Auoust 22, 1983 6771-00
. Project No.
Dept /Div. Mechanical /Ccmnonent Qualification spee No, Fue No. COD-009534 Page No. 1 Of I Client - Ceco, IPC, PST Stn. LaSalle , P/B. Clinton- Unit Marble Hill Subject SeiSPIC 0U41i#inA*in" n# Tid "7 nelny poinye -
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Equip = ant 5 Ann en e in1?nn fernn .T o c: o1 cnv LaSalle ca ) To: N.'El-Sorrogy - 30 CC: S. A. Ahmad - 30 R. D. Raheja/K. L. Adlon ,30 J. Sinnappan - 30 AEM/APD/ YAP - 30 CQD File - 30 t The existing Test Response Spectra (TRS) envelop the new Required ( Response Spectra (RRS) for the subject relays in all frequency zones of intere.st. Hence, the existing seismic qualification reports for the relays are adequate. Attached are the applicable TRS & RRS. It nry further'be noted that the panel frequencies are higher than 10 Hz and the relay frequencies are higher than 40 Hz. YAP /nb Attachment ,. I /* L A, h -
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