Text

Equipment Qualification Sqrt Post-Audit Documentation, Vol 10
	ML20005C127
Person / Time
Site:	LaSalle
Issue date:	11/05/1981
From:	; SARGENT & LUNDY, INC.
To:	;
Shared Package
ML20005C123	List: ML20005C122; ML20005C127;
References
	NUDOCS 8111180427
	Download: ML20005C127 (250)
	v • d • e

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o SARGEN'T & LUNDY INTER OFFICE MEMORANDUM From J. Sinnappan - 30 x6773 Date Nov. 3, 1981 Project No 4266/4267/6093-00 Dept./Div. Mechanical / Component Qualification Spec. No. l File No. COD-000412 Page No. 1 of 1 _

Client CECO Stn. LaSalle County Unit 1&2 Subject SQRT - Post Audit Documentation (Vol. 10)- q a

(Safety-Related) i To: D. C. Haan/G. C. Jones - 31

! J. B. Gouvas - 31 i

n

CC: M. M. Hassaballa - 30 l AEM/JS - 30 .

CQD File - 30 {

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References:

1) Let-er from G. R. Crane dated 10-26-81 h

2) Conference call with NRC dated 10-26-81 i'

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O ^of safety-related equipment.ttachea is our ecaetea status reeort oa seismio sue [1

(,

h The following are attached:

I TAB-A: Status of modifications on HPCS Values and RCIC Turbine TAB-B: SQRT forms for six components for which tests were completed but report not received.

SQRT forms completed based on test witness reports.

l l TAB-C: Justification for Interim Operation for six open items.

These six items are scheduled for test in the near future.

' However, we show with the existing reports that the device

' has been successfully tested to required 'g' levels. We i opted to retest because of lack of proper documentation.

I We also attach a copy of our test program which would furnish complete documentation.

TAB-D: This contains the test program for fatigue testing of two-representative Limitorque operators. These tests were com-i pleted on 11-2-81. We also include the test results for one valve as logged by our S&L engineers who witnessed the test.

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The above documentation should answer and eliminate all the concerns j; raised by NRC SQRT.

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Attachments. -

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! LA SALLE COUNTY NUCLEAR STATION ;

COMMONWEALTH EDISON COMPANY SAFETY-RELATED EQUIPMENT QUALIFICATI0t!

l POST NRC AUDIT DOCUMENTATION !

i !

VOL,10 !

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I BY COMPONENT GUALIFICATI0t! DIVISION +

SARGENT & LUNDY Ef!GINEERS l 11-5-81 l i

O CQD FILE # 000412

. SARGENTQ LUNDY ENOINEERO 4 CMICAGO r'N TABLE OF CONTENTS

1. TAB-A -

Status of modifications on HPCS Valves and RCIC Turbine

2. TAB-B - SQRT forms for components retested but test tuports not received.

a. 'ITT Barton' Level Ind. Trans. Switch (760)

159C4383

b. ' Cutler Hammer' Push Button Switch (10250T)

145C3230

c. 'GE' Log Radiation Monitor #238X660

d. 'GE' Time Delay Relay (CR2820) #145C3035

e. ' Eagle' Signal Timer (HP 5) #145C3043

f. Solenoid Valve #Cll-F009

3. TAB-C - Justification for Interim Operations for components for which retesting planned but not completed. Also f-]

(j . includes test plans.

a. 'GE' Voltage Preamplifier #163Cl263

h. 'GE' WRM/MSV Inter. Range Monitor #368X102AA i c. 'GE' Indicator & Trip Unit #129B2802

d. 'GE' Contactor (CR 105/205) #145C3029 l e. 'GE' Sensor & Converter #194C927

f. 'Hamel Dahl' 2" Globe Valve #Cll-F0ll

4. TAB-D - Test Plan and Preliminary Test Results for representative Limitorque Motor Operators O

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STATUS OF MODIFICATIONS ON HPCS VALVES AND THE RCIC TURBINE EQUIPMENT # MODIFICATIONS STATUS E22-F010 10" Globe Valve; add Completed /

modified yoke legs to per ECN-M513LS.

existing valve yoke legs.

Dwg. #VPF3238-21-6 E22-F0ll 10" Globe Valve; add Completed /

modified yoke legs per ECN-M5132S.

to existing valve yoke legs.

Dwg. #VPF3238-230-3 E22-F023 12" Globe Valve; add Completed /

modified yoke legs to per ECN-M513LS.

existing valve yoke legs.

Dwg. #VPF3238-022-9 E22-F012 4" Valve, add additional Completed /

support for valve. per ECN-M513LS.

Support Dwg.#M09-HP09-1037R 1

C. / E51-C002 RCIC Turbine Completed /

Replace #8 taper pins per tele-con with with #9 pins and pedestal field bolt lock plates.

Verify stiffness of trip latch spring used on S&K valve to be 32.5 #/ inch.

Replace 2 EGM control boxes with Model #8271-236.

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Replace 2 RGSC Modules with i Model #8271-083 and #8271-590.

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CAM MSFER WITCH Device Name:

Model Number:

The seismic qualification testing for this device was done at S'.f3TH WEST RESEARCH INSTITUTE, SAN Alfr0NIO, TEXAS, on 10-26-1981.

One of our engineers representing COMMONWEALTH EDISON COMPANY witnessed the testing and he confirms that the device passed the test without any structural or functional failure. Therefore the SQRT forms were completed based on his reporting and the only items not included were: ,

a) the report number b) the TRS and RRS envelops.

This will provided when the report becomes available.

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Nuclear Saf ety Related Project Nos. 4266/67 LA SALLE NUCLEAR STATIONS.

Q UNITS 1 8 2 NSSS EQUIPMENT QUALIFICATION

SUMMARY

EQUIPMENT NAME: Level Indicating Transmitter Switch EQUIPMENT NO: B21-N026A/D B21-N044A/B LOCATION: Reactor Bldg. El. 761', 710' EQUIPMENT CLASSIFICATION: @ ACTIVE C PASSIVE QUALIFICATION METHOD:

Biaxial Random Motion Test CU ALIFICATION DOCUMEf4T

REFERENCES:

1. SWRI Test Report # g

2. GE Drawing 159C4383

3. Nutech Test Specification: MK2-02-100 Rev. O dated 10-7-81 a I

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. LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

1. Normal Operating Loads + OBE + hRVASY-TO + ALL-Trf ENVELOP

=

B ce 2. Normal Operating Loads + SSE + COLEVY-2+h#ASY-TO+8#ALL-TO ENVELOP Normal Operating Loads + SSE+ Chugging + SRVASY-TO+

3. ALL-TO ENVELOP

~~

4. Normal Operating Loads + SSE + AP en h 5. Normal Operating Loads + SSE + COLEVY-1 j 0

) QUALIFICATION:

. PPF.PIRCD BY: Date 1

REVlHUCD BY: Date SARGENT *2 LUij0Y Il,h Date .mo. ...U g APPROVED BY: c ~.c .oo -

L

Nuclear Safety Related Project Nos. 4266/67 9i SEISMIC QUALIFICATION

SUMMARY

Required Response Spectrum curves were generated from the analysis of the local panels. These spectra were used as input to the instrument for seismic qualification.

Mounting on the test table simulates the actual in-service mounting.

Monitoring for funtionability and operability was done as !

per the referenced test specification. No malfunction was noted.

Proof Testing:

a) Upset. Condition: Biaxial Random Motion test.

Excitation is independently controlled in the horizontal and vertical direction. The frequency range is from 1 to 100 Hz. The duration of the test is 30 seconds per event with 5 OBE events per orientations, b) Emergency Condition:' Same as Upset Condition except that one event of 30 seconds duration in each orientation shall be performed.

Supporting Testing:

^

a) SRV f atigue testing was performed using two independent inputs such taht the TRS envelopes the RRS. Frequency

' range 1 - 200 Hz.

l b) SRV + LOCA testing was also performed based on the same v procedure as above.

C c) Resonance search was also performed in the frequency j range of 1. to 100. Hz. in all three separate axis.

9 7

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{v Ref: CCD File No. CQD-000251

, SARGENT d LUNDY h l

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t Nuclear Saf ety Related Qualification SLmnary of Equip ent Project Nos. 4266/67 T. P1 t m.

LaSalle County g

1. Utility: CECO WR

2. NSSS; GE MR X

3. A-E: S&L Level Indicating Trans. Switch l:

II. Corponent th.e

1. Fbdel tuter 760 Quantity: 6 f

2. Vendor ITT Barton l r

3. If the w@uent is a cabinet or panel, na:ne and nodel !b. of ;

h the devices included;

4. Physical Description a. Appearance Rectancular Shape g

b. Di:nensions 8" x 11" x 5" f

c. Weight 10 lbs. f g

b 5. Iocation: Building: Mounted on Local Panels (See Table 1)

Elevation;

^

6. Field bbunting Conditions [ ] Solt (!b. , Size )

Mounted on local panel per [ ] Weld (Iength ) !

, lI Mrg. standard mounting I I :;

, bracket.

7. i;atural Fregm.ncies in Each Direction:

v hl: h2: V: g o

'b 8. a. Functional

Description:

High and Low water level f a:

Indicating Switch a

y b. Is the equiprent required for[XIlbt Stantrf[X} Cold ]

Shut h m p l }Both v

i f)(l Post LOCA

9. Pertinent Feference Design Specifications:

d 8 GE 225A6634 & 225A6635 a

m SAIIGENT': LUNDY ; y Feference: CCDFile ib. CQD-0002 51 -sNoirsemasct'

~ - - - - - - - -- ___ _ , , . _ _ _ _ _ _ _ _ _ _[*

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7 Nuclear Satety Related Project Nos. 4266/67 III. Is Equigent Available for Inspection in the Plant: [x} Yes [ ] tb Ctnents:

Test: X IV. Equiptent Qualification Method:

Analysis:

Ccebination of Test and Analysis: i

'- khv )

Test and/or Analysis by SWRI Report #

(n3me of Ccqmy or Laboratory & Pcport tb.)

V. Vibration Inout:

1. loads considered 1.[X] Seismic only 2.[ ] Hydrodynamic only 3.[] Explosive only ;

SRV + LOCA 4.[X] Other (Specify) 5.[ ] Oxbination of 164 ;

2. Pequired Pespnse Spectra (attach the graphs):

RRS curves generated from local panel analysis

3. Required Acceleration in Each Direction:

h2 = V= -

hl =

VI. If Qualification by Test, then Corplete:

[ ] Single Frequency JXj M.11ti-Frequency 1.

i

2. [ ] Single Axis [X) Multi-Axis e

3: Frequency Parca: 1 - 100 Hz TRS enveloping RRS using Multi-Frequency Test [X] Yes (Attach TRS graph 4

4. / -1, ; i- )

{ ] tb E

hl = h2 = V=

5. g-level Test at

6. Laboratory Mounting: Simulating the field mounting

1. [ ] Dolt (ib . , Size ) [ ] Weld (Iength )[ ]

7

$ [ ] tb [ ] tbt Applicable

7. Functional cperability verified: [X] Yes 0 8. Other tests perfomed (such as fragility test, including results)

-y 1 SRV Fatigue, SRV + LOCA, Fesonance Search D

SARGENT"LUNDY h5; Peference: CQDFile tb. COD-000251 -enciNusasu s m^.-u a

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Nuclear Safety Related Project Nos. 4266/67 VII. If Otulitication by Analysis or by the Ocr:bination of Test and Analysis, v

Complete the Following Information: N/A

1. Description of Test including Results:

L

2. M3thod of Analysis:

[ ] Static Arulysis [ JEquivalent Static Analysis [ ]Dynanic

[ } Response Spectrum [ ] Tim-History

3. & del 'Pfpe: [] 3D [ ] 2D [ llD

[ l Finite Elem2nt[ JBeam [ ] Closed Fom Solution

4. [ ] Cbrputer Codes:

Frequency Range ard !b. of nodes considered:

( ) Hand Calculations

5. th.minu: , , _ _ _ , , , _ , _ , _ _

6. Support Considerations in the model:

7. Critical Structural Eleents: Governing Seismic 'Ibtal Stress A. Identification Iocation Response Qxbination Stress Stress Allcwable!,

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Effect Upcr. Functional u B. Max. Deflection location Operability [

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eeference: Coo File :n. Coo-ooo2 51 SARGENT LUNDY f I a.~_.. .q _

Final

INSTRUMENT IDENTIFICATION 8 IFICATION REQU! ret 1ENTS ,,

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ID No.: J' '34383

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Name: Lcvel Indic. Trcnd. Switch Quali fica tion 'g ' levels TABLE-1 blanu f acturer: Barton h,= '= V=

Blodel No. : 760 Instrument Required 'g' levels Equipment Numbers Location Class. Remarks hi h2 V B21-N026A/D Region RB-2 1.21 .91 .84 A Ilot Standby, Cold Shutdown and El. 761' on panels, Post LOCA II22-P004,5,26,27 B21-N044A/B Region ' B- 8

. 1.95 1.46 1.04 A El. 710' o panels 112 2-P0 D S ,10 TRS er velopes RRS e

I m A - Active P - Fassive 1E - Class 1E

lh REACTOR VESSEL LEVEL & PRESSURE SYSTEM LEVEL INDICATING TRANSMITTER '

SWITCH B21-N026 A ENVIRONMENTAL QUALIFICATION TABLE B21-7

1. DESCRIPTION The instrument is a Barton Model 760 Level Indicating Transmitter Switch which has four (4) SPDT switches.

2. SAFETT FUNCTION .

The level indicating transmitter senses reactor vessel water level and is designed to trip the Nuclear Steam Supply Shutoff System isolation

' logics (MSIV closure) on low level.

3 SAFETY DESIGN PARAMETERS A. Switching: Low-2 SPDT snap action switches sicultaneous setpoint ,

only for decreasing water level.

High-2 SPDT snap action switches simultaneous setpoint only for decreasing water level.

B. Switch Rating: 5 a=ps at 120 Vae 0.1 amp at 125 Vdc C. Working Pressure: 2000 psig D. Transmitter Output: (A) 10-50 mA into 500 ohms 52.5 Vdc (B) 4-20 mA into 300 ohms 25 Vdc O

W ) 4.

FSAR ENVIRONMENTAL CONDITIONS The Instrument is on the Reactor Vessel LevcL and Pressure Panel (H22-P004) in the reactor building. The ESAR environmental conditions are tabulated below:

Temperature Pressure Humidity Radiation Duration 0-1 hr. 3400F 7 in. WC All steam Operating 0.001 R/hr Accident 6.5x102 R/hr Integrated 6.5x10 2 Rad

5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Temperature Pressure Humidity Radia tion 0-1 hr. 3400F 7 in. WC All steam Operating 0.001_R/hr Accident 6.5x10 d R2 /hr Integrated 6.5x10 Rad

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REACTOR VESSEL LEVEL & PRESSURE SYSTEM LEVEL INDICATING TRANSMITTER SWITCH B21-N026 (Continued)

< ENVIRONMENTAL QUALIFICATION TABLE B21-7 '

6. QUALIFICATION METHOD Type Test The instrument continued to perform all functions (transmitter, indicator and switches) during the a=bient conditions of:

- Time Temperature Humidity Ambient Pressure t

1 hr 400F 205 RH Atmospheric - 1 in. H 2O 1 hr 700F Atmosphere Atmospheric e

1 hr 1000F Atmosphere Atmospheric 1 hr 2120F . 100% RH Atmospheric + 7 in. H2 O

7. RESULTS The instrument continued to perform all functions throughout the tests.

The performance of the test specimen was within the General Electric Speci-fication No. 159C3383 Q

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. nutech San Ase, Calif:rnis N Project .'Zimmer/La Salle SQRT Recualification Procram file No.

p Owner Cincinnati Gas and Electric. Company / Commonwealth Edison Comcany _

Client Cincinnati Gas and Electric comoanv/ commonwealth Edison Comoany TABLE I

. INSTRUMENT DATA 4

INSTRUMENT-NAME: LevelindicationTransmitterSwitch MODEL NO.: 760 .

SERIAL OR ID. NO.: Iff MANUFACTURER: Sar, ton SPECIAL TEATUPIS IF ANY: Ncne FUNCTION: RPV level 2 trip DIMENSIONS: 11.5" E x 8.94" W x 6" D

WEIGHT: -

'REQU7 RED RATGE: -150 (214.69)/0/+60 (64.40)

REQUIPID ACCURACY: !7.5" MONITORINT FIQUIPI2iENTS: Out=ut and differential oressure, contact position and Chatter Detection MOUNTING DETAILS: See Figure 1

! CHATTER TIME: 20 milliseconds when scale readinc is

! +1 % of full scale from setcoint To be completed by SwRI b)

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i REACTOR TESSEL IEVEL & PRESSURE SYSTEM LEVEL INDICATING TRANSMITTER SWITCH B21-N044 EITIRONMENTAL QUALIFICATION TABLE B21-7

1. DESCRIPTION The instrucent is a Barton Model 760 Level Indicating Transmitter Switch which has four (4) SPDT switches.

2. SAFETT FUNCTION The level indicating transmitter senses reactor vessel water level and is designed to trip the Nuclear Steam Supply Shutoff System isolation

- logics (MSIV closure) on low level.

3 SAFETT DESIGN PARAMETERS A. Switching: Low-2 SPDT snap action switches sicultaneous setpoint ,

only for decreasing water level.

High-2 SPDT snap action switches sicultaneous setpoint only for decreasing water level.

B. Switch Rating: 5 a=ps at 120 Vac 0.1 amp at 125 Vdc C. Working Pressure: 2000 psig D. Transmitter Output: (A) 10-50 mA into 500 oh=s 52.5 Vdc (B) 4-20 ci into 300 oh=s 25 Vdc

( 4. FSAR ENVIRONMENTAL CONDITIONS -

The Instru:ent is on the Reactor Vessel Level and Pressure Panel (H22-P004)

) V' - in the reactor building. The FSAR environ = ental conditions are tabulated below:

Duration Tenperature Pressure Humidity Radiation 0-1 hr. 340 F 7 in. WC All steam Operating 0.001,R/hr Accident 6.5x10' 5/hr Integrated 6.5x104 Rad

5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Temperature Pressure Hu=idity Radiatien 1

0-1 br. 340 F 7 in. WC All stea= Operating 0.001 R/hr Accident 6.5x102 R /hr Integrated 6.5x102 Rad l

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i REACTOR VESSEL LEVEL & PRESSURE SYSTEM LEVEL INDICATING TRANSMITTER l7 SWITCH B21-N044 (Continued) p ENVIRONMENTAL QUALIFICATION TABLE B21-7 .

Q 6. QUALIFICATION METHOD Type Test The instru=ent continued to perform all functions (transmitter, indicator and switches) during the a=bient conditions of:

Time Temperature Humidity Ambient Pressure 1 hr 400F 205 RH Atmospheric - 1 in. H 2O 1 hr 700F Atmosphere Atmospheric 1 hr 1000F Atmosphere Atmospheric '

1 hr 2120F 100% RH Atmospheric + 7 in. H 2O

7. RESULTS The instrunent continued to perform all functions throu6hout the tests.

The performance of the test specimen was within the General Electric Speci-fication No. 159C4383 co -

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Device Name: PUSH BUTTON SWITCH # 145C3230 10250T.

Model Number:

The seismic qualification testing for this device was done at WYLE LABORATORIES, NORCO, CALIFORNIA on One of our Engineers representing Connonwealth Edison Company witnessed the testing and he' confirms that the device passed the test without any structural failure or functional failure. Therefore the SQRT forms were completed based on his reporting and the only items not included were:

a) the report number b)'The TRS and RRS envelops.

This will be provided when the report becomes available.

S e

I O .

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LA SALLE NUCLEAR STATIONS'

( > UNIT 18 2 NSSS EQUIPMENT QUALIFICATION

SUMMARY

145C3230 EQUIPMENT NAME : Push Button Switch Model # -

B21C-S32A/B, B21C-S33A/B, B21C-S25A/D, E12A-S61, E21A-SO9, E22A-SO2,

, EQUIPMENT NO:E51A-S41 f

I LOCATION: Aux. Building El.768' on Panels H13-P601 i

~

EQUIPMENT CLASSIFICATION: O ACTIVE ] PASSIVE QUALIFICATION METHOD: Seismic ( See page 2)

I I

QUALIFICATION DOCUMENT

REFERENCES:

l

1. WYLE Test Report # dated l 2. NUTECH Test Spec. # MK-02-031 Rev.2.

e I

3. Drawings & Misc. Data.

t i

4. .

5.

6.

l I 7.

8.

9. .

w.

LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

1. Normal Operating Loads + OBE + _SRVASY-TQ + ALL-TO ENVELOP j 2. Norma 1 Operating Loads + SSE + COLEVY-2+ SRVASY-TQ + SRVALL-TQ -

ENVELOP 1 1

1

3. Normal Operating Loads + SSE+ Chugging + 3RVASY-TQ +- SRVALL-TQ ENVELOP l

4. Normal Operating Loads + SSE + AP

! 5. Normal Operating Loads + SSE & CO LEVY-1 i

QUALIFICATION:

l I Date PREPARED BY: ,

s, I REVIEUCD BY: Date SARGEiJTatu JDY '

i

~" Redo.NSS ASU j APPPOJED 7Y: Date _

c .-. .c a o .;

1 l

QUALIFICATION METITOD The test specimen is attached to a fabricated test fixture.

The monitoring devices are provided for testing.

1. Operational Testing:

First, operational tests are performed which establishes a baseline function.

2. Exploratory Testing:

Test Method: Low Level Sine Sweep Input Motion: Single Axis No. of Tests: 3, One in Each Orthogonal Axis Frequency Range: 1 - 100Hz Sweep Rate: 1. Octave Per Minute Input 'g' Level: .025g Peak

, 3. Proof-Testina: .

I w

(a) OBE Testing (b) DBE Testing Test Method Random Motion Random Motion Input Motion -

Biaxial Biaxial No. of Tests 10 With 5 in Each 4-Armed and Dis-Orientation Armed in Each Orientation Frequency Range 1 - 100Hz 1 - 100Hz Test Duration 30 Secs / Test 30 Secs / Test i

i 4. Required Response Spectrum:-

l Different size control panels were tested to a random multifrequency biaxial testing with the test response spectrum enveloping the floor respouse spectrum. The response spectrum at different instrument locations were obtained during this test. The envelop of these response l

spectrum were obtained and this was the required response spect*um r for the instrument qualification.

i I

I,l I l

Ref: CQD File No. 000271 . -

l SMiGEilT hLU:!DY hj

.~.,~ ~.a

'*]A- . r. ,

i'

,I Qualification Sumnar,f of Equirrent g 7, p ,

LASALLE COUNTY 1&2 g.

1. Utility: CECO IMR GE 54R X

2. NSSS:

3. A-E: SEL il Push Button Switches # 145C3230 j II. C& ponent Na.m

1. bbdel Nu::ber 10250T Quantity: Several i Cutler Ha:=er

2. Vendor f t

3. If the cxrponent is a cabinet or panel, name and hodel tb. of a

the devices included; q Push Sutton type i

4. Physical Description a. Appearance switches

b. Dinensions 1.3S"d x 4.38" long (with 3 blocks) m I lb. j

c. Weight on Panels H13-P601 Aux. Bldg.

5. Iocation: Building:

Elevation: El. 768'

6. Field bbunting Conditions [ ] Bolt (tb. , Size ) i Pane 1 mounted. [ ] Weld (IEngth ) f, l

[ ] i

. i

7. Natural Frequencies in Each Direction:

hl: h2: V:

Functional

Description:

used for remote manual contrcl

8. a.

of various reactor and coolant systems

b. Is the equi; rent required for[ ]!bt Sta.tby[ ] Cold Shutdan

[ ]Doth Other safety function

9. Fertinent Beference Design Sprifications: --

I d

SARGENT 'r LUNDY ,I'i1

Reference:

CQD File No. CQD 000271

ssaineen.L

-_ ._ _- - -_ _ ._ _ _ _._m'J;J

I 3f III. Is Equignent Available for Inspection in the Plant: [x ] Yes [ ] No

(' ,\ "

Carments:

l IV. Equitznent Qualification Method: Test: X

]

Analysis: .

Chibination of Test and Analysis: I*

haby) dated h Test and/or Analysis by WYL:, Project #

(nane of Cortpany or Iaboratory & Report No.)

V. Vibration Input: l 4

1. Ioads considered 1.[X ] Seismic only 2.[ ] Hydrodynamic only 3.[] Explosive i.

only L l 4.[ ] Other (Specify) 5.[ ](bnbination of i a a

2. Required Fespanse Spectra (attach the graphs): See attached.

P Y

l

! 3. Required Acceleration in Each Direction: i l -

hl = h2 = V= ,

L p '

VI. If Qualification by Test, then Comlete:

. I

1. [ ] Single Frequency [X] mlti-Prequency l

2. ,

[ ] Single Axis [X] Multi-Axis

! 3. Frequency Farcp: 1 - 100 Hz 1 l

TRS enveloping RRS using Multi-Prequency Test [X] Yes (Attach TRS graphs l 4.

( Aalaf ) ?

[ ] No

5. g-level Test at h l =_ h2 = V=

l

6. Iabaratory Mounting: ,

l l

1. [X} Bolt (No. , Size ) [ ] Weld (Iength )[ ] I i

7. Functional operability verified: [X] Yes [ ] tb [ ] Not Applicable l

l l 8. Other tests perfonned (such as fragility test, including results) [

l Resonance Search Test

! I i

lh Pcference: CQD File ?b. CQD 000271 _4- SARGENTi LUNDY IF

suoms mas [j i,

. 50

N If Qualification by Analysis or by the Coctination of 'Ibst and Analysis,the ,

Q VII.

Cbnplete: NA

1. Description of Test including Results: ;

2. Method of Analysis:

[ ). Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic .

[ ] Pesponse Spectrum [ ] Time-History

3. Madel Type: [ ] 3D I J 2D [ ]2D l

[ ' Finite Elemnt[ JBeam [ ] Closed Form Solution

4. [ ] Conputer Codes:

Frequency Fange and fb. of Itodes considered:

[ ] Hand Calculations

5. Da:rping: _ , _ _ _

6. Support Considerations in the rmdel:

O 7. Critical Structural Elements: Coverning Seismic Total Stress !

... Identificatien Iocation Perrense @bination Stress Stress A11cuablef Iffect Upon Functional-

8. Max. Deflection Incation _

Operability [

O l

'i SARGENT ' LUNDY l Pcference: COD File No. 000271 2eumunen._a

~^

Jan% M p

V INSTRUMENT IDENTIFICATION 8 ^VALIFICAT10N REQUIREMENTS I D ID No.: -

~ ~

3230 '

~

Name: Purh Button Switch' Qualification 'g' levels Manufacturer: Cutler Hananer h'= h -.,= y=

Model No. : 10250T Instrument Required 'g' levels Equipment Numbers .

Locetion' , Clas s . - Remarks

! h1 h2 V i i B21C-S32A/B (Aux.' Bldg El.768' { A Random multifrequency biaxial i On Panel' P601 .

testing w.i.th TRS enveloping RRS B21C-S33A/B --

A B21C-S25A/D --

A E12A-S61 --

A E12A-SO9 --

A E22A-S02 --

A E51A-S41 A k

A - Active P - Passive 1E - Class 1E

~

- - = = - -

f

$l PUSHBUTTON SWITCH C71A-S---

ENVIRONMENTAL QUALIFICATION TABLE C71-4

1. DESCRIPTION The equip =ent is a pushbutton switch as manufactured by Cutler R1==er.

2. SAFETY FUNCTION Manual initiation of Safety System. (R. G.1.62) 3 SAFETY DESIGN PARAMETERS Type: Ar ed Pushbutton

' Contacts: Mo:entary Collar Positions: 2&3 Contact Ratings: 10 A ps continuous, 6 a:ps at 110 VAC, 2.2 Amps at 120 VDC break, 60 Acps at 110 VAC, 2.2 Acps at '

120 VDC =ake & interrupting ,

4. FSAR ENVIRONMENTAL CONDITIONS The equip:ent is lccated inside the Control Room. The FSAR environment conditions are tabulated below:

Duration Te=perature Pressure Humidity Radiation Min 400F Range 0.10 in. 10% Operating 0.0005 R/hr Normal 60 0

-900F to 1.0 in. 50% Integrated 1.75x102 Rad Max. 1200F water gauge 60% .

static pressure

5. ENVIRONMINTAL QUALIFICATION ENVELOPE (Spec. 22A3087, Rev. 0)

Duration Te=perature Pressure Humidity Radiation Min 400F Range 0.10 in. 10% Operating 0.0005 R/hr Normal . 600-900F to 1.0 in. 50% Integrated 1.75x102 Rad Max. 120 F water gauge 60%

static pressure

6. QUALIFICATICN METHOD Type Test Details of the Test -

First Step - Set temperature at 400F, relative hu=idity 90%. Let stabilisc for 45 minutes and then operate 5 times.

i at rated load.

Second Step - Increase temperature to 50 0 F, relative humidity 90%.

Let stabilize for 45 minutes and then operate at 5 times rated load.

0 Subsequent Steps - Repeat teeperature increases at 10 F intervals up to 120 F, everything else remaining the same.

I e

I

- _,,,,-,-n,= _

0

)

FUSHBUTTON SWITCH C711-S--- (Continued)

BlVIRONMENTAL QUALIFICATION TABLE C71-4 Final Step - Retun. ',o Ambient temperature and humidity. Let stabilize for PS =inutes and then operate at rated ,

load 100 times.

7 RESULTS h

The rotopush 10250T switch have passed the environmental test requirements

~

. of the General Electric Company.

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San J:se California i Project ttt . II . Zimer/La Salle County Nuclear Power Stationsfila No.

Owner Cincinnati Gas and Electric Co. /Cc:rionwealth Edison Co.

Clint Cincinnati Gas and Electric Co. / Corr.onwealth Edison Co.

Too- .

Top m

Lege'd :aining Platu 4 / U Nut i

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g -)i i Hole l 7 Gauge Sneet Steel Mounting Plate Horizontal 7

_., _ _ _ _ _ ._' s _ . _ _ _ ___--- _ _ --

Suggested

Response

{ l Front Legend Accclerometer Top ; Plate --

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Blocks l Mounting Plate (7 Gauge Sheet Steel)

MOUNTING TECHNIQUE FOR TEST SPECIMEN l FIGURE 1 Revision C l l l Page 11 Pre;;ared By/Cate Cre:ked 9f /Cate h .h I < ,-kr.' f.d"M * !.2 ff#[ 'I U!

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5 10 10 10 10 &

R 2 FREQUENCY - HZ .I Figure 4

- ~

I!orizontal DDE Required Response Spectrum 7

'O. *M

g 3 ]

nutech l San Jne, California W. H. i Pr: Ject Zim er/La Salle County Nuclear Power Stations Fdetao. i

,,0wner Cincinnati Gas and Electric Co./Co m onwealth Edison Co. '

)

(dlient Cincinnati Cas and Electric Co./Cc ronwealth Edison Co. ;l I

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{ I COOWJWECHNON N O i

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9' f Page 15 PU0E'b_* ' ff .A '

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Device Name: LOG RADIATION tt0NITOR # 238X660 Model Number: 807E228 1

The se'ismic qualification testing for this device was done at WYLE LABORATORIES, NORCO, CALIFORNIA on 9~7~1901 One of our Engineen representing Commonwealth Edison Company witnessed the testing and he confirms that the device passed the test without any structural failure or functional failure. Therefore the SQRT forms were completed based on his reporting and the only items not included were:

i

,O a) the report nnmber b) The TRS an'd RRS envelops.

! This will be provided when the report becomes available.

e t

l .

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l 1

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47 ,

F i

LA SALLE NUCLEAR STATIONS'

( ) UNIT 182 NSSS EQUIPMENT QUALIFICATION

SUMMARY

EQUIPMENT NAME : LOG. RAD. MONITOR # 238X660

, EQUIPMENT NO: D18-K610A/D LOCATION: Reactor Building CR-1, El. 768' on Panels H13-P635, 36 I

~

EQUIPMENT CLASSIFICATION: Q ACTIVE ] PASSIVE QUALIFICATION METHOD:

i QUALIFICATION DOCUMENT

REFERENCES:

i

l. WYLE Test Report # dated ,

2. NUTECH Test Spec. # MK2-02-034 Rev.O i 3. Drawings & Misc. Data.

4. .

5.

6.

! 7.

8-l 9. .

g I

h LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

1. Normal Operating Loads + OBE + SRVASY-TQ + SRVALL-T ENVELOP h 2. Norma 1 Operating Loads + SSE + COLEVY-2+ _ ASY-TQ+ ALL-TO_ ENVELOP

3. Normal Operating Loads + SSE+ Chugging + SRVASY-TQ + SRVALL-T ENVELOP

4. Normal Operating Loads + SSE + AP

5. Normal Operating Loads + SSE + CO LEVY-1 QUALIFICATION:

PREPARED BY: Date ,

l ..

l REVIEUCD BY: Date SARGEfJTSLU DY )

APPROVED 3Y: Date 72700 3

i ti9 Quslification Method Nutech provides the test laboratory with a drawout shelf assembly upon which the test specimen shall be mounted.

Monitoring devices are provided for cesting the specimen by the test laboratory.

1. Explanatory Testing: -

Test Method: Low level sine sweep Input Motion: Simple axis No. of Tests 3-1 in each orthogonal axis Frequency Range: 1-100 Hz Sweep Rate: < 1 octave per minute Input 'g' Imel: 0.25g peak

2. Proof Testina CBE Testino DBE Testina Test Method Random Motion Random Motion

{ )

Input Motion Biaxial Biaxial No. of Tests 10 with 5 in 2 with 1 in each each orientation orientation Frequency Range 1-100Hz l-100Hz Test Duration 30 sec./ Test 30 sec./ Test

3. Required Response Spectrum:-

Different size control panels were tested to a random multifrequency biaxial testing with the test response spectrum envelopin.; the j floor response spectrur. The response spectrum at different instrumentj locations were obtained during this test. The envelop of these response spectrum were obtained and this was the required response spectrum for the instru.cnt qualification.

l l

l l I Ref CQD File No- -000262 SARGEijT 5 LUi!D f pl

EPeO M f*'re* dj

_- - - - - , ,..o . - - _ . . . . . . . . . , ,

.[. N

1 11 0 Qualification Stw., of Dquiprent

,LASALLE COUNTY l &2 . Type-p ,

CECO WR

1. Utility:

BHR X

2. NSSS: GE

3. A-E: S&L Log Radiation Monitor # 23SX660 f]

II. CcrTrnent Name

1. bbdel Nunter 807E228 Quantity: 4 l

j Vendor G.E. ;

2. 9

[

3. If the ccrponent is a cabaret or panel, name and nodel tb. of >

the devices included: NA s 1

4. Physical Description a, Appearance Instrumentation ,

7"HX19"W

b. Dinensions 35 lbs.

c. Weight

l Region CR-1

5. Iocation: Building:

Elevation; 76S'-0" on panels Hl3-P635, 636

6. Field bbunting Conditions [ ] Bolt (tb. , Size ) !

pane 1 counted [ } Weld (Irngth ) J (see sketch attached) [ ]

j

7. Natural Frequencies in Each Direction:

l hl: h2: V: -

8. a. Functional

Description:

1 (See attached any. Qual. Tables ) I 9

b. Is the equiprent required for[ ]Ibt Stundby[ } Cold jf Shutdown I JBoth :

P

9. Pertinent Reference Design Specifications:

~

2 l

Pcference: CQL File No. CQD 000262 SARGENT': smaisena.o LUNDY h

_ _ _ _ _ _ g.r _ _ _ _ _' G ,.3

. -~ -

i GO

<. >~

,9 Ill. Is Equiprunt Available for Inspection in the Diant: (X) Yes [ ] No LJ Contnents: ,

IV. Equiprnent Onlification bbthod: Test: X Analysis: -- i L

l Oxbinat. ion of 'Ibst and AnaJ , sis: h

deted Test and/or Analysis by WYLE Report #

(na:re of L_cpany or Laboratory & Report !b.) k

(.

I V. Vibration Input: h s

1 i 1. Ioads considered 1.!X] Seismic only 2.( ] Hydrodynamic only 3.[] Explosive if i

only i.

i 4.[ ] Other (Specify)_ 5.[ ] Conbination of f I h, l

2. Pequired Response Spectra (attach the graphs): , p on pp f fs :, 7fs -r, panc i 20celerations--for-panels-n13-F635,_6%

3. Pcquired Acceleration in Each Direction: NA ,

j l h1 = h2 = V= j

.r; i

VI. If Qualification by Test, then Ccrnlete:

1. [ ] Single Frequency IX]bblti-Frequency 1

3 j 2. . [ ] Single Axis [X) Multi-Axis

3. Frequency Para: 1-100Hz

4. TRS enveloping RRS using Multi-Frequency Testt() Yes (Attach TRS graph I NA I 3 ID (Iah1) r I

5. g-level Test at hl = h2 = V=

f I 6. Iaboratory obunting: (See attached sketch )

I l

1. [ ] Dolt (ib . , Size ) [ ] Weld (Icngth )[ ] [<

l

7. Functional operability verified: [ ] Yes [ ] tb [ ] ttt Applicable [

8. Other tests perfomxi (such as fragility test, including results) l I Resonance Search Test f U

d Peference: CQD File ;4.CQD 000262 4- SARGENT ' LUNDY !!flj

enanneenou M l

h

. ~ m .1 .j

,-.2 A L_.

r s -- -

_ - - - .- r_ . =--.,.7 _

-f

(/

VII. If Qualification by Analysis or by the Cabination of Test and Analysis,the :

_Ca plete: NA

1. Description of 'Ibst including Pcsults:

2. Method of Analysis:

[ ] Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic

[ ] Response Spectrun [ ] Time-History

3. Model Type: [ ] 3D [ ] 2D [ ]1D

[ ] Finite Element [ ] Beam [ ] Closed Form Solution

4. [ ] Conputer Codes:

Frequency Pange and No. of nodes considered:

[ } Hand Calculations

5. Damping:_

6. Support Considerations in the model:

{ 7. Critical Structural Elements: Governing Seisfaic Total Stress A. Identification Incation Pesconse Conbination Stress Stress Allcwablei 1

I

(

t Effect Upon Functionali B. Max. Deflection Incation Operability l I

1 1

1 i _

~

1 Peference: COD File Ib- 000262 SARGEi1T' LUTiDY l -5_ .~ o,~....u j l

L

i INSTRUMENT IDENTIFICATION 8 7"ALIFir,ATION REQUIREMENTS O

ID No'.: '2 u l60C007

~

V

' (^s V

ame: Log. Rcd.Moniter-Qualification 'g ' levels Manufacturer: C.E.

h,= h=

2 V*

Model'No.: 807E228 Instrument Required 'g' levels Equipment Numbers Location . Class. Remarks h1 h2 V D18-K610A/D Region CR-1 A Random Multifrequency biaxial El. 768' on Panels testing with TRS enveloping RRS.

lil3-P635, 36 i

A - Active P - Passive 1E - Class 1E

w ;- _ _,__ _

_ _ _ _ __ -.. = . - - -

- - _ _ - _ ;_y _ m - -- - . .= .a g _ , _

53 t

6

-DI.V J RADIATION MONITORING SYSTEM LOG. RAD. MON. D18-K610 j

( ENVIRONMENTAL QUALIFICATION TABLE D18-3 ,

1. DESCRIPTION The instrument is a General Electric Logarithmic Radiation Monitor ,

^

drawing nucber 238X660. All controls and indicators required for

normal operatier. are mouated on the Front Panel.

2. SAFETY FUNCTION

. -The Log Radiation Monitor provides conitoring of gross gacca radiation ;

levels in the =ain stea: lines and provides initiation of a reactor ,

, . scram and closure of the cain steam line isolation valves in case ,

pf significant increases in the gross ga=sa radiation levels. ,

J. SAFETY DESIGN PARAMETERS 115 Vac, 53 to 63 Hz A. Jnput Power:

B. Trip Circuits: Two upscale One downscale One high voltage - inop

4. FSAR ENVIRONMENTAL CONDITIONS

_The instrucent is located in the control room. The FSAR envircntent91 conditions are tabulated below:

l iiuration Temperature Pressure Humidity Radiation N/A 400F Range 0.1 in. 20% Operating 0.0005 N/A 600-900F To 0.25 in, water 40-50% Integrated 1.75x10 2

.N/A 1200F gauge static pressure ,

ji, ENVIRONMENTAL QUALIFICATION ENVELOPE (F,,ce. 22A3008, Rev. 5)

Duration Temperature Pressure Humidity Radiation N/A 400F Range 0.1 in. 20% Operating 0.0005 Integrated 1.75x10 2 l N/A 60 900F To 0.25 in. water 40-50%

N/A 1200F gauge static 60% (1)

! pressure f (1) Puring IIVAC equipment failure conditions, relative humidity may approach 100% for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 120 F uould not occur concurrently.

6, , UALIFICATION Q METHOD l

I Type Test i NO DATA

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nutsch y

. San hs?, California Project Wm. H. Zi=er/La Salle County Nuclear Power Stations File No.

/ '< Owner Cincinnati Gas and Electric Co./Co=onwealth Edison Co.

Chent Cincinnati Gas and Electric Co./Cc=onwealth Edison Co.

NOTE: Test fixture to be supported such that it is rigid below 200 H::. .

f Test Fixture

/

.A

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)

,/

/ s

(&

/ Y' /

/

TN B[ Detail A f O.ccJ

/ 8 C-)

/

Mounting Rails c Detail Rear B h Mounti.^.g Bracket

} c NOTE: Mounting rails attached I r

with 10-32 X .50 flat head screws and 10-32 #

I Front Mounting nuts. ,

Bracket L /

1 i i

O Test Fixture for Test Specir.en Mounting Ficure 2 Revis cn l O l l l l l Pre;;ared Ey/Ca:e ff. g[a $b

- _ ,o2b l eq 32 r r . c- c . m , v e,<- '- ' I i

i nUYGCh %

San J:se, California Project Mm. H. Zi:mer/La Salle County Nuclear Power Station File No.

Owner Cincinnati Gas and Electric Co./Cc=onwealth Edison Co.

Client Cincinnati Gas and Electric Co./Co=onwealth Edison Co.

CAPACITOR PONER SUPPLY , [ UNDER TEST

@ 50 VDC 7 l

/' OSCILLOSCOPE

( v' OHM WITH' POWER

- A'iPLIFIER DIGITAL f VOLT >iETER L

l l TEST SET-UP FOR CAPACITOR TEST 1

(3

!,C/

l\

i FIGURE 3 Revision j d l l l j 25 Page Pre::ared Sy/Cate hMy,[hMjl l of 32

nutech n San hse, California Project Wm. H. Zimmer/La Salle County Nuclear Power Station Fife No.

/ ' Owner Cincinnati Gas and Elecuic Co./ Commonwealth Edison Co.

Client Cincinnati Gas and Electric Co./ Commonwealth Edison Co.

51

% ll5VAC,6OHZ 1

1/100A NEUTRAL FUSE GROUND F2 FUSE HOLDER SEE NOTE 1 SEE NOTE 1 J8 1 2 3 SEE NOTE 2 J4 J1 A CURRENT .

SOURCE LOGARITID1IC B RADIATIO:I MONITOR 238X666 NOTES: 1. FUSE SHALL BE J2 E A B C D

\O f- REMOVED FRCM FUSE HOLDER AND CC::::ECTED AS_SHCWU.

2. SOLDER UIRES TO FUSE HOLDER TERMI:!ALS A::D BROUGHT GUT OF CHASSIS.

( y TO MONITORING CIRCUIT TEST SET-UP FOR LCGARIT~iMIC RADIATION MONITOR 238X666 OPERATIONAL TEST O

FIGURE 4 Rev:scn l O l l l l l Page 26 Prepare:: Sy/Cate lW/;pyjj l l l of 32 r r .c- c vn 96 '

i ! A _I

nutech '

San As , California os* 6 Project Wm. H. Zimmer/La Salle Countv Nuclear Power Stations file No.

Owner Cincinnati Gas and Electric _Co./Co- wealth edinnr rn.

( ) Chent Cincinnati Gas and Elec+-ic co . /c~ wea 1 *h raiwn en-

~

TABLE 2

, INSTRUMENT DATA INSTRUMENT NAME: Logarithmic Radiation Monitor MODEL NO.: 238X6'60 SERIAL OR ID. NO.:

MANUFACTUPIR: General Electric SPECIAL FEATUPIS IF ANY: None O I FUNCTION:

Receive current input proportional to v radiation and provide RPS trip outputs DIMENSIONS: 7"H X 19"W WElGHT: 35 lbs

' REQUIRED RANGE: 1-10 6 mR/hr REQUIRED ACCURACY: 31 MONITORING REQUIREMENTS: Input current and output trips and voltage MOUNTING DETAILS: See Figures 1 and 2 To be completed by test laboratory I I -

l Revision 4 l l Page 32 Prepared By/Cate ffrz/p/4//f /l l Checked By/Cate of 32

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g o

0 10 10 1 2 3 - -

3 m

10 10 e2 FREQUENCY - HZ I E

. Figure 7 .

u o a w IIOrizOntal DDE Required Response Spectrum 3w 5

a E b4 E.U %,s 3 m

8l San Jose. California g

Project _Wm. H. Zim er/La Salle County Muclear Power Stations File No Owner Cincinnati Gas and Electric Co./Cc=cnvealth Edison Co.

'fient Cincinnati Gas and Electric Co. /cc-- Snwealth Edison Co. l

. M p err a . , . - 4 S

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TIME DELAY RELAY # 145C3035 M ica Nm:

- ~

CR2820.

Model Number:

The seismic qualification testing for this device was done at WYLE LABORATORIES, NORCO, CALIFORNIA on One of our Engineen representing Commonwealth Edison j ,

Company witnessed the testing and he confirms that the device passed the test without any structural failure or functional failure. Therefore the SQRT forms were co=pleted based on his reporting and the only ite=s not included were:

O a) the report number b) The TRS and RRS envelops.

This will be provided when the report becomes availsble.

5 e

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Y ,

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l0 .

l V* 4 w e *-evw e v e'w e--w ww,es.~e,+-e<w tvi--o.y-,-y.v-m---w.n.w,-,. .--#-,we,p.-,9.,,, , -,,,_,,_-,,._,n-.,____...,_.m ,_m,,,., _ , , , , , , . , , , . , ~ . , , _ . - . , .

1 P' &

I LA SALLE NUCLEAR STATIONS' i > llNIT 18 2 NSSS EQUIPMENT GUALIFICATION

SUMMARY

EQUIPMENT NAME : Time Delay Relay # 145C3035 .

See Table -l

, EQUIPMENT NO:

l l LOCATION: on Panel til3-P609 Aux. Bldg. El. 768'

~l EQUIPMENT CLASSIFICATION: @ ACTIVE ] PASSIVE QUALIFICATION METHOD: seismic Tests ( see page 2)

I I

QUALIFICATION DOCUMFNT

REFERENCES:

WYLE Test Report dated !

1

2. NUTECH Test Spec. MK2-02-040 Rev.l.

3. Drawings & Misc. Data.

4. -

5.

6.

7. ;

l l I 8- l i

i

9. .

g l U* ,

LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

[

1. Normal Operating Loads + OBE + _SRVASY-TQ + ALL-TQ ENVELOP i

- t ;

2. Normal Operating Loads + SSE + COLEVY-2+ _SRVASY-TQ+ ALL-TQ ENVELOP i

3. Normal Operating Loads + SSE+ Chugging + SRVASY-TQ+ ALL-T ENVELOP

4. Normal Operating Loads + SSE + AP 1

l 1 5. Normal Operating Loads + SSE + COLEVY-1 l

r I

i QUALIFICATION: [

PREPARED BY: Date ,

REVIEUED BY: Date SARGEiJTaLU;jDY lf 5 A P P R O '.'E D 7 Y : Date _ __

TjZ"[

i i

M3 n

U QUALIFICATION METHOD The test specimen is attachec to a fabricated test fixture.

The monitoring devices are provided for testing.

1. Operationa'l Testing:

First, operational tests are performed which establishes a baseline function.

2. Exploratory Testing:

Test Method: Low Level Sine Sweep Input Motion: Single Axis No. of Tests: 3, One in Each Orthogonal Axit Frequency Range: 1 to 100Hz Sweep Rate: 1 Octave / Minute Input 'g' Level: 0.25g Peak

'{ 3. Proof Testing: -

s (a) OBE Testing (b) DBE Testing Test Method Random Motion Random Motion Input Motion Biaxial Biaxial No. of Tests 10-4 de-energized and 4-1 de-energized and 1 energized, in each 1 energized in each orientation orientation Frequency Range 1 - 100Hz 1 - 100Hz Test Duration 30 Secs / Test 30 Secs / Test

4. Required Response Spectrum:-

Different Size control panels were tested to a random multifrequency biaxial testing with the test response spectrum enveloping the floor response spectrum. The response spectrum at different instrument locations were obtained.during this test. The envelop of these r,esponse spectrum were obtained and this was the required response spectrum for the instrument qualification.

l I Ref: CQD File No. 000273 SMGDAT'rLW'!DY )

a r.w n s a,m a d 4* ~ e.. qa,_- .

L~ -m m m

}

f//

Oualification Sterary of a:uipv_nt l l

4

)

Plant. th, e_:

.LASALLE COUNTY 1&2 DTei T. i CECO WR

1. Utility: i GE gqa X *l 2.. NSSS: __

3. - A-E:

S'b \

i Time Delay Relay il 145C3035 j II. Ctroonent ?bme See Table-1 CR2820 Quantity: 24 ,

1.- bbdel Nu:rber t CE/ general purpose control Vendor i !

2.2- ! s 3.: If the ccrponent is a cabinet or panel, nxe and hedel No. of l; ;

the devices incitxied: I -

Instrumentation ,

Physical Description a, Appearance 4 .4 -

b. Dinensions S 75 x 3 7 5 "x 3.G " , .

N

c. Weight 2 lbs .

4)

Iocation: Building: Auxiliary Buildin;;

5.5 Elevation; on Panel H13-P609 El. 768' 10-24) 64 Field bbunting Conditions [ ] Bolt (!b. 4 , Size ,

[ ] Weld (Iength ) l':

y Mounted en Panels

[

h

7. Natural Frequencies in Each Direction: _

h2: V:

hl: i J-8; a. Functional

Description:

l (See attached env. Qual. Table) I Is the equiprent required for[ } Hot Sta:xiby[ } Cold l

b. Shut h n Other safety functio Pertinent Peference Design Specifications: (

9 .2 i i

t-

?

I.

SARGEifT t LU?iDY l ,

Peference: CQD File tb.CQD 000273 -sso;Namas_s

-- - . m _. m, - - ~rv y . z__, _ -lyn

e 6f "A.

Ill. Is Equiprent Available for Inspection in the Plant: [X ] Yes [ ] No J

Comnents:

X IV. Equipnent O.:alification Method: Test: [

Analysis:

Ox:bination of Test and Analysis:

}

'Ibst and/or Analysis by, '4YLE LAB. REPORT # (LRrER )y date (na:Te of Cctpany or laboratory & Report !b.)

l V. Vibration Inout: f

? tt

1. Ioads considered 1.[X] Seistnic only 2.[ ] Hydrulynamic only 3.[] D< plosive

[

only J 4.[ ] Other (Specify) 5.[ ] Cortination of [j

-; 2, Required Pespnse Spectra (attach the gra;fis): See attached. L d

tl 3, Beguired Icceleration in Each Direction: NA .

t h1 a h2 = V=

i i VI. If Qualification by Test, then Ccrolete: i

1. [ ] Single Frequency [X} Wlti-Preque.g ;

'l

2. . [ ] Single Axis [X] mlti-Axis 1

3. Frequency Rar.,0: 1 - 100H2.

4. TFS enveloping RRS using Multi-Frequency Test [X] Yes (Attach TRS graph (

l @ATER) }

[]b

[I h2 = V=

S. g-level Test at h l =_

l I 6. Laboratory .tunting:

1. [XjDolt ( b. 4 , Size 10-33 [ ] Weld (Iangth )[ ]

l l 7 Functional operability verified: [X] Yes [ ] !b [ ] tbt Applicable l k 8. Other tests p2rformi (such as fragility test, including results) j Resonance Search Test. .

l l L

1

Reference:

CQd File tb. CQD 000273 SARGENT -LUNDY li4 l mNGINEERS

. . c < a c. ,;

l ).

y _ ,__ - . . . . . . - _ . - _ _ _ __ _

= _ _ _ ,____;.___ = __

I h

If Qualification by Analysis or by the Canbination of Test and Analysis,the VII.

CotTplete: N.A.

1. Description of Test including Pesults: _

2. Method of Analysis:

[ ] Static Analysis [ ] Equivalent Static Analysis [ JDymmic

[ ] Response Spectrum [ ] Tine-History

3. bbdel Type: [ ] 3D [ ] 2D [ llD

[ ] Finite Element [ ] Beam [ ] Closed Form Solution.

4. [ ] Corputer Codes:

Frequency Pange and bb. of nodes considered:

[ ] Hand Calculations

5. Damping: _ _ _ _

6. Support Considerations in the nodel:

Critical Structural Elements: Governing Seismic Ibtal Stress O' 7.

A. Identification Incation Pescense Conbination Stress Stress Allcwabl l

Effect Upon Functional Iocation Operability B. M u. Deflection SARGENT b LUNDY !

Paference; COD File !b. 000273 -

-n- : E N GIN E E 53 s b -

l

- w -- --- - - - . - - - - -

i e

67 TIME DELAY RELAY B21C-K--

,.,f S ENVIRONMENTAL QUALIFICATION TABLE B21-12 U 1. DESCRIPTION The equipment is a CR2820 time delay relay manufactured by General Electric.

2. SAFETY FUNCTION Time delay relay energi:ation required to permit initiation of the Automatic Depressurization System function and General Safety System application.

3. SAFETY DESICN PARAMETERS The time delay relay est energize and de-energize with a 10% accuracy when required and supply a 120 volt DC,130 MA inductive load.

Maximum environ = ental condition: 1200 F - 90% R/H ,

4. FSAR ENVIRONMENTAL CONDITIONS The equipment is located ', side the Control Room. The FSAR environment conditions are tabulated below.

Duration Temperature Pressure Humdity Radition Minimum 400F Range 10% Operating 0.0005 /hr Normal 600-900F 0.10 in. to 50% Integrated (40 yrs)

Maximum 1200F 1.0 in . wa te r 605 1.75x102 Rads Gauge Static

,,-~ Pressure ,

~#

5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008 Rev. 5)

Duration Temperature Pressure Humdity Radition Minimum 400F Range 10% Operating 0.0005 /hr Normal 600-900F 0.10 in. to 50% Integrated (40 yrs)

Maximum 1200F 1.0 in, water 60% 1.75x102Rs.ds Gauge Static Pressure

6. QUALIFICATION METHOD Operational Oualification Ihe devices were placed in the Environmental Chamber and soaked for 16 hours1.851852e-4 days 0.00444 hours 2.645503e-5 weeks 6.088e-6 months at 600C and 90-95% relative humidity. At the conclusion of the soak period ,

without change of environmental conditions, each device was cycled 50 times at rated load. Each cycle consisted of 1 sec. on and 9 sec. off except for the selector switch shich had 1 sec. right, 1 sec. le ft, 8 sec. off.

7. - RESULTS Contact tests show relay will handle 120 volts DC,130 MA inductive load.

Tests demonstrate that the relay has 10% timing accuracy. Relay will function in environments up to 1200F and 90% R/H.

O U

p INSTRUMENT IDENT.FICATION & p.L.IFICATION REQUIREMENTS l '

1D ' No~. : 14k d35 Name Time Daley Ralsy Qualification 'g' levels Manufacturer: GE i= 2= W Model No.: CR2820 Instrument Required 'g' levels Equipment Numbers Location . Class. Remarks h1 h2 V B21C-K05A/B Aux. Bldg. El.768' A Random Multifrequency Biaxial on Panel til3-P628/631 Testing with the TRS enveloping B21L-K01A/D On Panel lil3-P689/690 A A The RRS.

CllA-K01 On Panel H13-P610 C71A-K16A/D on Panel 1113 .609/611 A C71A-K22A/D On Panel til3-P609 A 673' E12A-K054A/B Reactor 6 ,AB-731' A On Panel til3-P618/629 E12A-K055 Reactor Bldg. El.673' A On Panel ill3-P613 E12A-K070A/B Aux. Bldg. El.731' A 3 On Panel Ill3-P618/629 r

E12A-Ko93A/B --

A E22B-K06 D.G.-l El.710' On Panel ll22-P028 A E51A-K09 'Aeactor Bldg. El.731' A On Panel II13-P621 D

A - Active P - Passive 1E - Class 1E

, 'J.

o i

nutech a San Jose, California ,

Project Uu. H. Zinner/ La Salle County Nuclear Power Stations File No-((,,)' Owner Cincinnati Gas and Electric Co./Conmonwealth Edison Co.

Client cincinnati Gas and Electric Co./Corronwealth Edison Co.

4-P-4006-1024 MOUNTING NUTS AND #10-24 BOLTS

/

'O pp 0' b b UNISTRUT SUGGESTED P-4000 RESPONSE (O O 3

ACCELEROMETER

?

LOCATIONS

- ^s .

C GilO C O C :

< . O OllC O

,- m O

t .

'w/ l l TIME DELAY 0 [B ) 0; EMY ? ,

l l I UNISTRUT Lal O W

{ n-4000 I

k M l TIME DELAY ADJUSTMENT TEST SPECIMEN MOUNTIUG PLATE ,

I (7 GAUGE SHEET STEEL) l l ,y l

\_-) MOUNTING TECHNIOUE FOR TEST SPECIMEN 1 FIGURE 1 Rewsion l, O, I l -

P e 11

.. , Jx, Pre;:ared By/Date lj,cf,ggffg of 16 e -

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% ; D D -

g ,

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_ a a 9 9 t4 g n

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7 ;,S_ A ZPA= 0.81 _ o o a h

q kj ; e C BETA = 0.020 g g c -

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~ o m u E . te+'J_,

E & E m u

r* N'1-. . L .al - m- M r

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E ? , FREQUENCY - HZ Figure 4 w ~

Horizontal DDE Required Response Spectrum M

e -

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=

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- a., 2o-a o a o o s'

? rn "' 'I gO 10 2 s8 '

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ct M P

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BETA = 0.020 ? 9 @

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e a . A;e o o a v.

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e. 2 FREQUENCY - HZ F

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l Figure 5 l w w Vertical DDE Required Response Spectrum i

M

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. 72 Device Name: EAGLE SIGNAL TIMER # 145C3043

' ~

Model Number: HP 5 The seismic qualification testing for this device was done at WLE LABORATORIES, N0hCO, CALIFORNIA on 9-5-1981 One of our Engineers representing Commonwealth Edison Company witnessed the testing and he confirms that the device passed the test without any structural failure or functional failure. Therefore the SQRT forms were completed based on his reporting and the only items not included were:

O a) the report number b)'The TRS and RRS envelops.

This will be provided when the report becomes available.

t 1

e o

I I

i

O . . ,

s 9

4 --n e w- -w-n-- y ~ y, p-ev e w r s- w ,-e - o , e - --p- --s+v-+--- w . w w n w - -s w wags w-w n-,,wwe-a,r-m.,-+~ew- , , - , - ,--,-----een-,ame,--,- -r--w---,-,wwu e

I t 73 I

LA SALLE NUCLEAR STATIONS' I I UNIT 18 2 NSSS EQUIPMENT GUALIFICATION

SUMMARY

Adjustable Timer # 145C3043 EQUIPMENT NAME : E32-N601A,E,J,N, E32-N602A,E, E31-R621A/B, E32-N600A,E,J,N,

, EQUIPMENT NO: E32-N604 I

I LOCATION:

Reactor Building CR1 El.768' on Panels H13-P632, 642 E1.761' on Panels H13-P655, 654

( ] PASSIVE EQUIPMENT CLASSIFICATION: @ ACTIVE QUALIFICATION METHOD: seismic Test f QUALIFICATION DOCUMENT

REFERENCES:

1. WLE Test Report # dated ,

i 2. NUTECH Test Spec. MK2-02-032 Rev.2.

3. Drawings & Misc. Data.

4.

tlf 5.

6.

7.

! 8.

j 9.

10.

l' LOAD COMBINATIONS CONSIDERED IN,0UALIFICATION:

/ >

V

1. Normal Operating Loads + OBE + SRVASY-TQ + ALL-TO, ENVELOP

2. Normal Operating Loads + SSE + CO EVY-2+ SRVASY-TQ + RV ALL-TQ ENVELOP l

3. Normal Operating Loads + SSE+ Chugging + SRVASY-TQ* ALL-T ENVELOPS

4. Normal Operating Loads + SSE + AP j 5. Normal Operating Loads + SSE + COLEVY-1 a

b OUALIFICATION:

PREPARED BY:

Date REVIEGED BY: Date SARGEfJTaLUTJ3Y l

"'".*c d8 m* "o AF? ROVED ';V: Date c~ g

i I ._

Qualification Methods The timer case is securely mounted to the mounting plate using four 8-32 mounting screws. The test specimen is mounted on a vertical surface with the case and timer in a horizontal position.

The monitoring devices are provided for testing.

1. Exploratory Testing Test Method Low level Sine Sweep Input motion Single-axis No. of Tests

^

3 in each orthogonal axis J__ Frequency Range 1 to 100 Hz Sweep Rate 1 octave 1 minute Input 'g' level 0,25 'g' peak

2. Proof Testing OBE Testing DBE Testing Test Method Random Motion Random Motion Input Motion Biaxial Biaxial No. of tests 10'4 with the timer 4-1 with timer de-energized and 1 de-energized and with timer operating, I with timer oper-

.j j in each orientation. ating,. in each j orientation Frequency Range 1-100 Hz l-100 Hz Test Duration 30 Secs / Test 30 Secs / Test

3. Required Response Spectrum:-

Different size control panels were tested to a random multifrequency biaxial testing with the test response spectrum enveloping the floor ,

response spectrum. The response spectrum at different instru ent l locations were obtaiad during this test. The envelop of these response 1 spectrum were obtained and this was the required response spectrum for the instrument qualification.

I I Ref: CQD File No. 000268 3.

SMGEjT h 1.U.0Y I d men:med

_ 4 , c1 q

v Omlification Sumny of Ecuin:ent 78 C', 'LASALLE COUNTY 1&2 (f I. Plant Na.e:

M )

i CECO gg

1. Utility: 1 1

2. NSSS: WR S&L

3. A-E:

I.

Adjustable Timer # 145C3043 II. Cmoonent Nane l HP5 Q untity. 13

1. bbdel Nunt:er l Eagle Signal

2. Vendor l

3. If the caponent is a cabinet or panel, nane and nodel No. of 9 the devices incltxded: --

1 Instrumentation

4. Physical Description a. Appearance l 13 x 5 3 /4" deep

b. Dimensions 4 "x 3 2 lbs 11 oz

c. Weight

( 5. Location: Building: Reactor Bldg. Region CR-1

~

768' on Panels Hl3-Pb32, 642 Elevation; 761' H13-P654, 655

6. Field bbunting Conditions [ X] Bolt (tb. 4 , Size /16 ) i j

[ ] Weld (Length ) i i

I

[ ] n

7. Natural Frequencies in Each Direction: [

hl: h2: V:

Functional

Description:

to initiate a tired oeriod bv an I

8. a. g external signal from a push button, limit switch, photo cell, etc. ,

1

b. Is the equiprent requi. red for[ ] Hot Standby [ ] Cold j ShutdcAn j

[ ]Both '

Other safety function. [

9. Pertinent Beference Design Specifications: - J II l

l Peference: CQD File No. CQD 000268 SARGENTi LUNDY ,

.aua.s sa.Ln

^;4 Q

i e

-1, W

O Ill. Is Equirrent Available for Inspection in the Plant: [X] Yes [ j No lv) Conrnents: _

a I

i=

IV. Equignent Qualification Method: Test: X Analysis: ,

l Ctsbination of Test and Analysis: l

[j

'Ibst and/or Analysis by WYLE Test Report #(wren) dated (name of Conpany or Tahnratory & Report tb.) f/

! V. Vibration Input:

1. Loads considered 1 1 Xl Seismic only 2.[ ] Hydrodynamic only 3.[] Explosive

only e 4.[ ] Other (Specify) 5.[ ] Ctrbination of [

l j 2. Required Response Spectra (attach the graphs): e;r5 /w ; /;c / .c.? , .

E Pox 1 coce4eee-t4on--for-- paae is 1:B-P631, 42, 54; -M i l

NA

("N ' 3. Required /cceleration in Each Direction:

Vi f I h1 = _ _. h2 = V=

{a VI. If Qualification _ .b..y Test, then Comlete:

g

] 1. [ ] Single Frequency DC ] M2lti-Frequency 5

.l 2. . [ ] Single Axis L ] Malti-Ads ])

[ '

3. Frequency Rarca: 1 - 100 Hz

\

) TRS enveloping RRS using Multi-Frequency Test [y] Yes (Attach TRS graph (

4. "

! (L.C TCR) t

[J2

5. g-level Test at hl =_ h2 = V= ,

! F a

(

I 6. Iaboratory tbuntinu:

l 1. [X ] Bolt (tb: 4_ , _

Size 8-32 ) [ ] Weld (Inngth ){ ] !

l 1

[ ] tb [ ] ttt Applicable i

7. Functional op2rability verified: [X] Yes

8. Other tests prform2d (such as fragility test, including results) ;;

Resonance Search Test,

[

q a

d

! ;!d Pcference: CQD File tb. C0D 000268 SARGENT LUfjDY pfj

ssmNannou y

.co, _:

a ih -- --- - -_ _ - - - - _ _ u._ - _ _ _ __2 ~CrlstudEmiwJ

9 f

_a 7/ l VII. If Qualification by Analys,is or by the Cbnbination of 'Ibst and Analysis,the ,

'LJO l CchTplete: NA Description of 'Ibst including Pesults.

1.

l

2. Method of Analysis:

[ ], Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic Analysis !' ,

[ ] Pesponse Spectrum [ ] Tine-History i

3. fedel Type: [ ] 3D [ ] 2D [ ]1D

[ ] Finite Elenent{ ] Beam [ ] Closed Form Solution.

4. [ ] Conputer Codes:

Frequency Fange and No. of nodes considered:

[ ] Hand Calculations

5. Damping: _,____

6. Support Considerations in the nodel:

7. Critical Structural Elements: Governing Seismic 'Ibtal Stress A. Identification Ircation Re ,vnse Conbination Stress Stress Allcwablej t

i l

t i

l Effect L@n Functional l

Incation Oterability i B. Mix. Deflection l

l l

I i

i

) - .ir Peference: CC.D File No. 0002.W SARGENT LUilDY lI -

-s- :a noin a a n sd'ij

--_____..__-___g1

y C

~ ' ll- 14043 INSTRUMENT IDENTIFICATION 8 ("aLIFICATION (V l REQUIREMENTS ' ~h (V

1D'No.:

Name: Tima Indicator Switch Qualification 'g' levels Manufacturer: Eagle Signal

, h,= h= V" i

2 Mode 1 No.: lip-5 Instrument Required 'g' levels Equipment Numbers Location . Class. Remarks h1 h2 v E31-R621 A/B Region CR-1 A Random Multifrequency biaxial El.768' Panel fil3-P632 testing with the TRS enveloping H13-P-642 the RRS.

E32-N600A,E,J,N Region CR-1 El. 761' on Panel li13 -P655 A E32-N601A,E,J,N Region CR-1 El.761' on Panel ill3-P655 A

, E32-N602A,E Region CR-1 El.761' on Panel A til3-P655

, E32 -:a04 Region CR-1 El.761' on Panel H13-P654 A

, M A - Active P - Passive 1E - Class 1E C

s 79 DIVISION I LEAK DETECTION SYSTEM TIMER INDICATING SWITCH E31-R621

() ENVIRONMENTAL QUALIFICATION TABLE E31-3

1. DESCRIPTION The instrument is a Model HP55AG synchronous motor driven timer with a progressive pointer, manufactured by Eagle Company.

2. SAFETY FCNCTION The Leak Detection System (LDS), including the time indicating switch, senses leaks in c,losed syste s and initates the appropriate isolation signals.

The time indicating switch works as a bypass timer, which overrides the isolation signal (from hign differential flow) during the Reactor water clean-up system (RWCU) startup. No function important to safety is performed by this device.

3 SAFETY DESIGN PARAMETERS The Timer must energize with an accuracy of 0.5% a Volt do, 65 mA inductive load.

Worst case: 1200F - 90% R/M, +1.0 in mC A. Contact rating: 10 amp at 120 Vac .

,, B. Sequence:

'/

(1) Energized clutch coil starts timing (2) De-energized coil resets timer (3) Timer resets on power failure (4) Instantaneous contacts operate when clutch coil is energized (5) Delay contacts operate when pointer is at end of timing cycle (reaches 0)

C. Reset time 0.5 see (Full scale)

4. FSAR ENVIRON' ENTAL C0::DITIO: S The instrument is on the Division I Leak Detection V.B. panel (H13-P632) located in the control room. The FSAR environmental conditions are tabu-lated below:

Duration Tecperature Pressure Humidity Radiation N/A 400F Range 10% Operating 0.0005 R/hr. ,

0 40-50%

N/A 60-90 F 0.1 in.

N/A 1200F To 1.0 in. 60% (1) Integrated (40 yrs)

- Water gauge 1.75x10 2 Rad Static Pressure a

.v

(( '

DIVISION I LEAK DETECTION SYSTEM TIMER INDICATING SWITCH E31-R621 (Continued)

5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Temperature Pressure Humidity Radiation N/A 400F Range 10% Operating 0.0005 R/hr N/A 60-900F 0.1 in. 40-50%

N/A 1200F To 1.0 in. 60% (1) Integrated (40 yrs)

Water gauge 1.75x10 2 Rad Static Pressure ENVIRONMENTAL QUALIFICATION TABLE E31-3 (1) During HVAC equipment failure conditions relative humidity =ay approach .

90% 'for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 1200F would not occur sicultaneously.

6. QUALIFICATION METHOD Type Test The HP50A6 was rando 1y withdrawn from stock and placed in t. Tenney Environ-mental Chamber, Model BTRS-30350. The relative humidity was set for 90%

and the cha:ber was cycled fro = 1200F to 400F to 1200F for duration of the test. Base readings were taken at 30% relative humidity and 73 F.

s Time Tecperature Humidity %

~

(L_'> 1 hr 400F 92 1.5 hr 1200F 90 1 hr 400F 90 2 hr 1200F 90 1.5 hr 400F 90 2 hr 1200F 90 1.5 hr 400F 90 3/4 hr 700F 30 17.5 hr 1200F 90 -

7. -RESULTS The unit functioned norcally throughout the tests.

Tests performed show that timer accuracy, contact rating for worst case inductive load, will function in temperatures up to 1E00F. The exceed-s ingly s=all amount of radiation and pressure variations in the control room will have an insignificant effect on the timer.

l%.)}

/t :

l DIVISION I LEAK IETECTION SYSTEM TIMEF. INDICATING SWITCH E32-N603 t ENVIRONMENTAL QUALIFICATION TABLE E31-3

. (v '

1. DESCRIPTION The instrument is a Model HP55AG synchronous motor driven timer with a f t

progressive pointer, manufactured by Eagle Company.

2. SAFETY FUNCTION The Leak Detection System (LDS), including the time indicating switch, .

senses leaks in closed systems and initates the appropriate isolation signals.

The time indicating switch works as a bypass timer, which overrides the isolation signal (from high differential flow) during the Reactor water clean-up system (RWOU) startup. !b function important to safety is performed by this device.

3. SAFETY DESIGN PARAMETERS The Timer must energize with an accuracy of 0.5% a Volt de, 65 mA inductive load.

Worst case: 1200F - 90% R/M, +1.0 in mC A. Contact rating: 10 amp at 120 Vac B. Sequence:

O O/

(1)

(2)

Energized clutch coil starts timing De-energized coil resets timer (3) Timer resets on power failure (4) Instantaneous contacts operate when clutch coil is energized (5) Delay contacts operate when pointer is at end of timing cycle (reaches 0)

C. Reset time 0.5 sec (Full scale) 4 FSAR ENVIRONMENTAL CONDITIONS The instrument is on the Division I Leak Detection V.B. panel (H13-?632) located in the control room. The FSAR environmental conditions are tabu-lated below:

Duration Temperature Pressure Humidity Radiation N/A 400F Range 10% Operating 0.0005 R/hr l N/A 60-900F 0.1 in. 40-50% '

N/A 1200F To 1.0 in. 60% (1) Tntegrated (40 yrs)

Water gauge 1.75x102 Pad

. Static Pressure b) v

a

[h DIVISION I LEAK DETECTION SYSTEM TIMER INDICATING SWITCH E32-N500 (continued)

(jlll S. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Temperature Pressure Humidity Radiati_on N/A 400F Range 10% Operating 0.0005 R/hr N/A 60-900F 0.1 in. 40-50%

N/A 1200F To 1.0 in. 60% (1) Integrated (40 yrs)

Water gauge 1.75x102 Rad Static Pressure ENVIRONFENTAL QUALIFICATION TABLE E31-3 (1) During HVAC equipment failure conditions relative humidity may approach ,

90% for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 1200F would not occur simultaneously.

6. QUALIFICATION METHOD T_yJ_e_Te st The HP50A6 was randomly withdrawn from stock and placed in a Tenney Environ-mental Chamber, Model BTRS-30350. The relative humidity was set for 90%

and the cht:ber was cycled from 120 0 F to 400F to 1200 F for duration of the test. Base readings were taken at 30% relative humidity and 73 F.

v-(} Time Te=perature Humidity % .

1 hr 400F 92 1.5 hr 1200F 90 1~hr 400F 90 2 hr -

1200F 90 1.5 hr 400F 90 2 hr 1200F 90 1.5 hr 400F 90 3/4 hr 700F 30 17.5 hr 1200F 90

7. ,RESULTS The unit functioned normally throughout the tests.

Tests perfor=ed show that timer accuracy, contact rating for worst case

,_s inductive load, will function 'in temperatures up to 120 0F. The exceed-

/ 'i ingly small amount of radiation and pressure variations in the control room will have an insignificant effect on the timer.

. 15 DIVISION I LEAK DETECTION SYSTEM TIMER INDICATING SWITCH E32-N601 ENVIRONMENTAL QUALIFICATION TABLE E31-3 O

D 1. ~ DESCRIPTION Ihe instrument is a Model HP55AG synchronous motor driven timer with a progressive pointer, manufactured by Eagle Company.

2. SAFETY FUNCTION The Leak Detection System (LDS), including the time indicating switch, senses leaks in closed systems and initates the appropriate isolation signals.

The time indicating switch works as a bypass timer, which overrides the isolation signal (from high differential flow) during the Reactor water clean-up system (RWCU) startup. No function important to safety is performed by this device.

3. SAFETY DESIGN PARAMETERS The Timer must energize with an accuracy of 0.5% a Volt de, 65 u inductive f load.

Worst case: 1200F - 90% Rhi, +1.0 in mC A. Contact rating: 10 amp at 120 Vac !

, B. Sequence:

. (1) Energized clutch coil starts timing (2) Dc-energized coil resets timer !

(3) Timer resets on power failure (4) Instantaneous contacts operate when clutch coil is energized I (5) Delay contacts operate when pointer is at end of timing cycle ,

(reaches 0)

C. Reset time 0.5 see (Full scale) i

4. FSAR ENVIRONMENTAL CONDITIONS l l

The instrument is on the Division I Leak Detection V.B. panel (H13-P632) !

located in the control room. The PSAR environmental conditions are tabu- ['

lated below:

Duration Temperature Pressure Humidity Radiation !

N/A 400F Range 10% Operating 0.0005 R/hr N/A 60-900F 0.1 in. 40-50% -

N/A 1200F To 1.0 in. 60% (1) Integrated (40 yrs) 3

. Water gauge 1.75x10 2 Rad Static Pressure i

O

P

/k 1 l

DIVISION I LEAK DETECTION SYSTEM TIMER INDICATING SWITCH to 5

. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5) ,

Pressure Humidity _ Radiation Duration Temperature i

0 Range 10% Operating 0.0005 R/hr N/A 40 F i 0.1 in. 40-50%

N/A 60-900F Integrated (40 yrs) o 1200F To 1.0 in. 60% (1)

N/A Water gauge 1.75x10 2 Rad Static ,

Pressure !

I c,

ENVIRONMENTAL QUALIFICATION TABLE E31-3 .

(1) During HVAC equipment failure conditions relative humidity may approach 90% for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 1200F would not occur simultaneously. !

l

6. QUALIFICATION METHOD IZP_e TestThe HP50A6 was rando=ly withdrawn from stock and placed in a Tenney Environ-The relative humidity was set for 90%

cental Cha:ber, Model STRS-30350. 0 0 and the chamber was cycled from 120 F to 400F to 120 F for duration0 of the test.

Base readings were taken at 30% relative humidity and 73 F.

(b ' Tire Temperature Humidity %_

1 hr 400F 92 1.5 hr 1200F 90 1 hr 400F 90

~

2 hr 1200F 90 1.5 hr 400F 90 2 hr 1200F 90 400F 90 1.5 hr 700F 30 3/4 hr- -

17.5'hr 1200F 90

7. RESULTS The unit functioned normally throughout the tests.

Tests pe. formed show that tieer accuracy, contact rating for Theworst case exceed-

,s inductive load, will function in temperatures up to 1200F.

( )

ingly small amount of radiation and pressure variations in the control room will have an insignificant effect on the ticer.

$$ s DIVISION I LEAK DETECTION SYSTEM TIMER INDICATING SWITCH E32-N602

,g S ENVIRONMENTAL QUALIFICATION TABLE E31-3 O 1. DESCRIPTION The instrument is a Model HP55AG synchronous =otor driven timer with a progressive pointer, manufactured by Eagle Company.

2. SAFETY FUNCTION The Leak Detection System (LDS), including the time indicating switch, senses leaks in closed systems and initates the appropriate isolation signals.

The time indicating switch works as a bypass timer, which overrides the

- isolatica signal (from high differential flow) during the Reactor water clean-up system (RWCU) startup. No function i=portant to safety is performed by this device.

3. SAFETY DESIGN PARA!ETERS ,

The Timer cust energize with an accuracy of 0.5% a Volt de, 65 mA inductive load.

Worst case: 1200F - 90% R/M, +1.0 in mC A. Contact rating: 10 acp at 120 Vac

~~

B. Sequence:

([m,) (1) Energized clutch coil starts timing (2) De-energtzed coil resets timer (3) Timer resets on power failure (4) Instantaneous contacts operate when clutch coil is energized (5) Delay contacts operate when pointer is at end of timing cycle (reaches 0)

C. Reset time 0.5 see (Full scale)

4. FSAR ENVIRCT ENTAL CONDITIONS The instrument is on the Division I Leak Detection V.B. panel (H13-P632) located in the control roc =. The FSAR environmental conditions are tabu-lated below:

Duration Temoerature Pressure Hu=idity Radiation N/A 400F Range 10% Operating 0.0005 R/hr N/A 60-900F 0.1 in. 40-50% -

N/A 1200F To 1.0 in. 60% (1) Integrated (40 yrs)

. Water gauge 1.75x102 Rad Static Pressure E'

s

- If DIVISION I LEAK DETECTION SYSTEM TIMER INDICATING SWITCH E32-N604

, - ~

ENVIRONMENTAL QUALIFICATION TABLE E31-3

(V

)

1. DESCRIPTION The instrument is a Model HP55AG synchronous motor driven timer with a progressive pointer, manufactured by Eagle Company.

2. SAFETY FUNCTION The Leak Detection System (LDS), including the time indicating switch, senses leaks in closed syste=s and initates the appropriate isolation signals.

The time indicating switch works as a bypass timer, which overrides the isolation signal (from high differential flow) during the Reactor water clean-up system (RWCU) startup No function important to safety is performed by this device.

3. SAFETI DESIGN PARAMETERS ,

e The Timer must energize with an accuracy of 0.5% a Volt do, 65 mA inductive load.

Worst case: 1200F - 90% R/M, +1.0 in mC A. Contact rating: 10 amp at 120 Vac B. Sequence:

,~~s (1) Energized clutch coil starts timing (2) De-energized coil resets timer

{t' ') (3) Timer resets on power failure (4) Instantaneous contacts operate when clutch coil is energized (5) Delay contacts operate when pointer is at end of timing cycle (rsaches 0)

C. Reset time 0.5 sec (Full scale)

4. FSAR ENVIRONMENTAL CONDITIONS The instrument is en the Division I Leak Detection V.B. panel (H13-P632) located in the control room. The FSAR environmental conditions are tabu-lated below:

Duration Terperature Pressure Humidity Radiation N/A 400F Range 10% Operating 0.0005 R/hr N/A 60-900F 0.1 in. 40-50%

N/A 1200F To 1.0 in. 60% (1) Integrated (40 yrs) -

2

! Water gauge 1.75x10 Rad Static Pressure O

=i q

DIVISION I LEAK DETECTION SISTEM TIMER INDICATING SWITCH E32-N604 (Continued)

5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 3)

(m'") Duration Te=perature Pressure Humidity Radiation N/A 400F Range 10% Operating 0.0005 R/hr N/A 60-900F 0.1 in. 40-50%

N/A 1200F To 1.0 in. 60% (1) Integrated (40 yrs)

Water gauge 1.75x102 Rad .

Static Pressure ENVIRONMENTAL QUALIFICATION TABLE E31-3 (1) During HVAC equipment failure conditions relative humidity may approach 90% for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 1200F would not occur simultaneously.

6. QUALIFICATION METHOD g e Test The HP50A6 was randomly withdrawn from stock and placed in a Tenney Environ-mental Chamber, Model BTRS-30350. The relative humidity was set for 90%

and the chacber was cycled from 1200F to 400F to 1200F for duration of the test. Base readings were taken at 30% relative humidity and 730F.

Time Te:peratu e Humidity % .

b'"-

1 hr 400F 92 1.5 hr 1200F 90 1 hr 400F 90 ,

2 hr ,

1200F 90 1.5 hr 400F 90 i

2 hr 1200F 90 l 1.5 hr 400F 90 {

I j 3/4 hr 70oF 30 t 17.5 hr 1200F 90 l

7. . RESULTS The unit functioned normally throughout the tests.

Tests perforced show that timer accuracy, contact rating for worst case inductive load, will fenction in te=peratures up to 1200F. The exceed-ingly s=all a cunt of radiation and pressure variations in the control (n room will have an insignificant effect en the titer.

l

. - i

N San hse, California

$/

Project Inn. H. Zirrer /7 n sn110 county ':uclear Power Rentions File No.

Owner Cincinnati Gas and Elect-ic Co. /Cc~nonwea1th Edison Co.

Client Cinci~uti cas and riect-ic cn. /co- nn*..o,1

Fainon en.

C 1.406 .167 DIA 4 Holes I

3.19 DIA

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, . San Jose, California f l Project II" H. 2Lm/La Salle Countv Muclear Power Stations File No.

Owner Cincinnati Gas and Electric Co.!Cor=onwealth Edison Co.

,o Client - _ Cincinnati Gas and Electric Co. /Co onwea1th Edison Co.

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nutech San Jose, California ProI'ect Wm. H. Zirmer/La Salle County Nuclear Power Stations

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<G Owner Cincinnati Gas and Electric Co./ Commonwealth Edison Co.

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San Jose, California g

, Pro;ect Wm. H. Zimmer/La Salle County Nuclear Power Stations File fJo-

,s Owner Cincinnati Gas and Electric Co./ Commonwealth Edison Co.

Chent Cincinnati Gas and Electric co./corronwealth Edison Co. -

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2 b %J Device Name: CRD SYSTEM SOLENOID VALVE # Cll-F099 ..

Model Number: # 21A9317SC i

i l The seismic qualification testing for this device was done at SOUTH WEST RESEARCH INSTITUTE, SAN ANTONIO, TEXAS on 7-25-8/,

One of our Engineers representing COMMONWEALTH EDISON j COMPANY witnessed the testing and he confirms that the device r

passed the test without any structural or functional failure.

Therefore the SQRT forms were completed based on his reporting l and the only items not included were:

'O a) The report number a

b) The TRS and RRS envelops.

This will provided when the report becomes available.

I 1

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f U

l LA SALLE NUCLEAR STATIONS' I I llNIT 182 NSSS EQUIPMENT QUALIFICATION

SUMMARY

EQUIPMENT NAME ; CRD SYSTEM SOLENOID VALVE # 21A9317AC

, EQUIPMENT NO: C11-F009 LOCATION: Reactor Building El. 740' on piping subsystem I'

EQUIPMENT CLASSIFICATION: @ ACTIVE C PASSIVE QUALIFICATION METHOD: Test I

f QUALIFICATION DOCUMENT

REFERENCES:

'1 1. SWRI Test Report # dated

2. NUTECH Test Spec. # MK2-02-112 Rev.0

3. Drawings & Misc. Data.

4.

5.

6.

l 7.

8.

t 9. -

F 10 .

d i

LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

Normal Operating Loads + OBE + RV ALL-T ENVELOP

1. ASY-TQ RV h 2. Normal Opera ting Loads + SSE + COLEVY-2+ ASY-TQ + ALL-TQ ENVELOP :

Normal Operating Loads + SSE+ Chugging + SRV ALL-T ENVELOPi

3. ASY-TQ

4. Normal Operatina Loads + SSE + AP

5. Normal Operating Loads + SSE + COLEVY-1 PREPARED BY:

Date tGUALIFICATION:

REVI"UCD BY:

APPROVED ':v:

Date Date

[ SARGENT& LUNDY

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'O ' QUALIFICATION METHOD

'g A new test is done to meet the requirements of IEEE-344-d975; ,

Recommended Practices for Seismic Qualification of Class lE equipment for Nuclear Power Generating Stations.

The Test Spec'imen'is mounted on a fixture, which' inturn mounted on a vibrational table. ,

The monitoring devices and accessories are provided for vibration test.

1. Exploratory Testing:

Test Method: Low Level Sine Sweep Input Motion: Single Axis No. of Tests: 3 With one in Each Orthogonal Axis Frequency Range: 1 to 100Hz, Sweep Rate: < 2 Octaves / Minute Input 'g' Value: 0.lg Peak

2. Proof Testing: -

a) Upset Condition: Test Method: Random Mction Input Motion: Biaxial No. of Tests: 3 in each of the test specimen orientation, and Time 30 sec/ test.

. Frequency Range: 1 - 50Hz b). Emergency Condition: Test Method: Random Motion Input Motion: Biaxial No. of Tests: 1 in each orientation, 30 sec/ test and Time Frequency Range: 1 - 50Hz

3. Fragility Testial: A fragility test is performed in l

each orthogonal axis, at each ~

resonance frequency 1 - 100Hz.

[ 4. Input Test Levels :

The RMS value of input test 'g' levels shall be:

l OBE 3.0g in each of the three directions

,j g The 'g' SSE 4.0g --

level from the piping system are kept withWits.

these i Ref: CQD File No. 000255 SARGEijT k LUi!DY IU l

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n Qualification Su-rurf of Equipment LASALLE COUNTY 1&2 Utility: CECO EHR 1.

NSSS; GE g x 2.

SEL

3. A-E: .

CRD System Solenoid Valve # ZlA9317 AC II. Cecronent Name

1. Itdel ? Amber HTS 32322 Cuantity: 1 i J

2. Vendor ASCO HVA 166-265 l

[

3. If the ccuponent is a cabinet or panel, name and hodel Ib. of -

the devices incitried: --

i

4. Physical Description a. Appearance 7 16"a x 3 U1 W x2 S "D

b. Dimensions ,

j

c. Weight ,

3.1 lbr

5. Ircation: Building: Reactor Building Elevation; 740' on Piping Subsystem

6. Field tbunting Conditions [ ] Bolt (?b. , Size ) i Pipe counted [ ] Weld (IEngth ) !

l (see attached sketch) g )

7. Natural Frequencies in Each Direction: __ 2 hl: h2: V:

l Supply Instrument Air !

8. a. Functional

Description:

For Actuation of Air operated Valve ,

1

b. Is the equipmnt regtured for[X) Hot Standby [ ] Cold l

' Shutdcun 1 l [ }Both X POST LOCA i l

9. Pertinent Reference Design Specifications: e d

1 l

l t

Peference: CQD File ?b. CQD 0002_55 SARGENT'-i. UNDY h.

E N QiN a a p eL, t j

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v. : . ._ m u 2,_ , _ , ,.-w.. . ...

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I III. Is Equiprent Available for Ir;pection in the Plant: [M Yes []tb (

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X kc IV. Equipmnt O.:alification Method: 'Ibst:

H Analysis:

c l

Casibination of 'Ibst and Analysis: {

Test and/or Analysis by SWRI Report # (LATE R.) dated ,h, (nane of Carpany or Iaboratory & Peport !b.) I I

V. Vibration Input:

}

1. Inads considered 1.[ ] Seismic only 2.[ ] Hydrodynamic only 3.[] Explosive h only p

(

i 4.[ ] Other (Specify) 5.[ ] Ctxtbiration of il I

j 2. Ryuired Pespnse Spectra (attach the graphs):

i e

Required tcceleration in Each Direction:

3. ,

h2 = 4.3 03 V= l 3 o2 hl =- 4 3 0 't -

b i.

l If Qualification by Test, then Corplete- h

, VI. 1 6

,1

1. [ ] Single Frequency [X]bblti-Prequency j l.

1

2. . [ ] Single Axis [X] Multi-Axis ;,

j

) a J 3. Frequency Parg:

l

} 4. TRS enveloping RPS using Multi-Frequency Test { X] Yes ,(Attach TPS gra;td OBE: 3.0g 3.0g 3 og b l

! SSE: 4.0g 4.0g [ ] tb 4.0g l S. g-level 'Ibst at hl = h2 = V=

1 3 6. Iaboratory abunting: Pipe counted ( See attached sheet) i

1. [ ] Bolt (!b. , Si-a _

) 1 ] Weld (Inngth )[ ]

l

7. Functional operability verified: [XJ Yes [ ] tb [ ] tbt Icplicable I 8. Other tests perfor md (such as fragility test, including results) ,j I Exolatory Testing, Proof Testing, and Fragility Te s t in;- ~

."1 H

Peference: CQD File ib.CQD 1255 SARGEffT :-LUNDY lilj

-suomennau ?

I 1 -~xna m m, - - - - - _ - mw e n, , - - _ - . _ - . .

, _ myg

i

.ammumm 97 VII. If Otulification by Analysis or by the Ocr:bination of 'Ibst and Analysis,thc.

Cartplete: NA

1. Description of 'Ibst including Ibsalts:

2. & thod of Analysis:

[ ] Static Analysis [ )Egaivalent Static Aralysis [ JDpumic i

[ ] Response Spectrum [ ] Tine-Histcr'f

3. M:x$el 'lype: 1 ] 3D [ ] 2D [ ]ID

[ ] Finite Elment[ JBeam [ l Closed Form Solution

4. [ ] Cocputer Codes:

Frequency Ranoe and ?b. of nodes censidered:

[ } Hand Calculaticns

5. Da. ping :

6. Suprort Considerations in the ncdel:

G 7. Critical Structural Elments: Governing Seismic 'Ibtal Stress A. Identification Location %ga 0xbination Stress Stress Allcunble.

Effect Upon Functional location Operability B. Max. Deflection i >

Pcference: COD File tb. 00025s _s_ SARGENT - LUNDY l hu

.~a,~....ua w :_.1

e-w SOLDIOID VALVES FOR INSTRUMSNT AIR C11-F009

)

V ENVIRONMENTAL CUALIFICATION TABLE C11 4

1. DESCRIPTION The instru:ents are ASCO, =edel HT832322 solenoid valves used for instru=ent air service.

2, SAFETY FUNCTION The centrol rod drive hydraulic syste: (including the solenoid valve) runs the centrol rod drives (CED) and is designed to cause rapid insertien of the centrol reds (scra:) upon receiving signals fre: the reactor protection system. The solenoid valve centrols the inctrument air supply to the HCUs providing a backup to the individual scra: pilot valves. It also closes valves en the scran discharge volume vent and drain, closing the: during scra=.

3. SAFETT EESICN PARAMETERS A. Capable of centinuous 0;cration at voltage and ambient conditions.

B. Operate at pressure differentials and =ini=um voltages.

4. FSAR ET/IEC:2 ENTAL CCNDITICNS The equip:ent is located in the CRD hydraulic s*/ste . The FSAR environ-

= ental conditions are tabulated below:

n

/ \ *

(v\/ Duration Temperature Pressure Humidity Radiation Nor:al 70CF - 900F ner:al -0.10 to -1.0 40% normal Operation 1040F caximum inch we 90% caxinus 3.5x102 rad 40cF =inicu: 20% mini =um 1 mr/hr Accident 0-1 hour 2120F 7 in. WC All stea 6.5x102 rad

5. E!T/IRGESNTAL QUALIFICATION E!P/ELCPE (Spec. 22A3008, Rev. 5)

Duration Tecocrature Prescure Humidity Radiation Nor:a1 700 F - 90c? ner:21 -0.10 to -1.0 40% nor al Operation 10uoi =axinun inch we 90% =axi um 3.5x102 rad 400 F =tnicu: 20% =inicus 1 mr/hr Accident 0-1 hour 2120F 7 in. WC All stea 6.5x102 rad

6. GUALIFICATIO:IlETHOD Duration Te:perature Precsure Hunidity Radiation

,s 0-1 hour 2120F 7 in. WC All stca: 103 rad total

/ )

'V'/

i i

l 6/80 t

.t 30L"301D YALVES FOR INSTRUMENT AIR C11-F009 (Continued)

ENVIRONMENTAL QUALIFICATION TABLE C11-4

6. QUALIFICATION METHOD Type Test This is a fail-safe device in that it deenergizes when performing its safety func tion. No qualification testing is therefore required.

7. RESULTS No qualification testing has been performed.

e 1

6/80

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(~'s; INSTRUMEt4T 10Ef4TIFICAT!0N ID No.: ~21A9317AC ALIFICATIOil REQUIREMENTS (x)

~..-

'g' Name: CRD System Solenoid Valve Qualification levels ;

- Manufacturer: ASCo h,= h,= V= I Mode 1 No.: IIT832322 Instrument Requ1 red 'g levels !quipment E

Numbers Location -

Class. Remarks h1 h2 V Cll-F009 Reactor Building El. 740'-0" on Piping Subsystem b

A - Active P - Passive 1E - Class 1E

I nutsch /0/

San Jose, California Project Zimner/La Salle SORT Requalification Program File No.

Cincinnati Gas and Electric Comoanv/ Commonwealth Edison Company (Ov) Owner Chent Cincinnati Gas and Electric Company /Corronwealth Edison Company o

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Revision O I p64 f.e 5s* P*E' #5 Pre;a.ed By/Date y 7,q ,y, 1

Crened By/Date V,te. //i,/// 1 ,,

nutech mz San Jose, California Project Ziraner/La Salle SORT Recualification Procram File No.

v) Owner Cincir;nati Gas and Electric company / Commonwealth Edison Company Client Cincinnati can and F1en+-in cn-na ny /cn-nnsm n 1 eh painon ccmpany loo 0MI GR4DuATE t,

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Flutsch .g3 San Jose, California

> Zimmer/La Salle SQRT Requalification Program Project File No.

(j Owner Cincinnati Gas and Electric Company / Commonwealth Edison Company Chent Cincinnati Gas and Electric Comoanv/Cor.onwealth Edison Comoany TABLE I TEST SPECIMEN DATA INSTRUMENT NIdiE: SOLENOID AIR PILOT VALVE MODEL NO.: ASCO 8323A22 SERIAL OR ID. NO.:*

. .. . . _ - . MANUFACTURER.-: AUTOMATIC SWITCH CO.

SPECIAL FEATURES IF ANY: NONE FUNCTION: SUPPLY INSTRUMENT AIR FOR ACTUATION OF AIR OPERATED VALVE l

.y 1

DIMENSIONS: 7 1/16"H X 3,7/16"W X 2 3/4"D

\

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WEIGHT: 3.1 LB REQUIRED RANGE: 14.7 s 100 PSIG MAXIMUM PERMISSIBLE LEAKAGE RATE: 0.1 SCFH/ INCH OF NOMINAL VALVE SIZE MONITORING REQUIREMENTS: CHANGE OF STATE AND VALVE SEAT LEAKAGE MOUNTING DETAILS: SEE FIGURE 1 CHATTER TIME: N/A NOMINAL VALVE SIZE: 1/2" t

/

l rs + l 1 t 1 l \_j TO BE COMPLETED BY SwRI Revision j 0 l l le6N f.r sg ,

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Prepared ,:y;.Date t

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/04 QUALIFICATION OF JUSTIFICATION FOR INTERIM OPERATION The test report submitted by GE meets the specified g levels.

Acceleration level comparisons are shown below. .

Required g level from Panel Analysis h 1 = [' h , h2='7by V = * #/[

g level from Test Report h1 =/,8 h2 "/'O V " [e8g

. Therefore the equipment is qualified as for as test g levels are considered.

However we opted to perform new tests for the following reasons:

a) Documentation of test log was insufficient.

b) Funcional testing of Instruments not adeguately explained, c) Single axis single frequency testing was done.

The new tests will be done to the test requirements as attached as soon as the test specimen is procured. .

For the above reasons we strongly feel that the device is qualified for the interim operation.

O O

/05 '

i LA SALLE NUCLEAR STATIONS'

( l UNIT 18 2 NSSS EQUIPMENT QUALIFICATION

SUMMARY

voltage Preamplifier # 163Cl263AA EQUIPMENT NAME : .

EQUIPMENT NO: C51-K002A/H l

LOCATION: Reactor Bialding El.740'0" on Panels H22-P030, H22-P031, H22-P032 l

EQUIPME!:T CLASSIFICATION: @ ACTIVE C PASSIVE QUALIFICATION METHOD: Test I

l QUALIFICATION DOCUMENT

REFERENCES:

1. GE Document 22A4232, Rev.0

2. GE Dwg. # 163Cl263AA Rev. 6 7-27-73 l

3. GE Document PL 163C1263AA, Rev.7 5-11-74

4. NUTECH Test Spec. MK2-02-099 Rev.0 -

tl !

5.

6.

7.

f 8.

I j 9. .

m.

LOAD COMBINATIONS CONSIDERED IN QUALIFICATION: -

i

1. Normal Operating Loads + OBE + ,SRVASY-TQ + SRVALL-TQ ENVELOP SRV ^

] 2. Normal Operating Loads + SSE + COLEVY-2 # , ASY-TO ALL-TO ENVELOP

~

3. Normal Operating Loads + SSE+ Chugging + SRVASY-TQ* ALL-TQ ENVELOP

4. Normal Operating Loads + SSE + AP

5. Normal Operating Loads + SSE + CO LEVY-1 QUALIFICATION:

PREPARED BY: Date ,

Date REVID ED BY: SAP. GENT &LU.1DY h'd AFPPOVED 'N: Date 7J2"*"7f

s IC6 O

QUALIFICATION SLWiARY single axis single frequency testing was done.

Input 'g' levels h l = 1.8 g h 2 = 1.8 g Natural frequency hl= 29 Hz l h2= 16 Hz V = none.

l I Ref: CQD File No. CQD 000258 - gg,gpf ~

.a maw 2emedi

_ _ - c a c. c 3

Otalification Su:Tury of nruignent /g LASALLE 1 & 2

.j T. Plant ?bre: M CECO PWR

1. Utility:

X NSSS; GE 54R 2.

3. A-E: S&L i <

V lt8se Preamplifier # 163Cl263AA II. Cartoonent tune {

1. 2 del FArter 828E309AA Quantity: 1 i l

2. Vendor GE

3. If the cceponent is a cabinet or panel, nane and hodel ?b. of '

the devices incitried: l

4. Physical Description a. Appearance b, Dinensions 10.5" H x 6.5"W x 5.2"D ,

c. Weight Reactor Building

5. Location: Building:

H22-P030, H22-P031 Elevation; 740'0" on Panels H22-P032, H22-P033

6. Field bbunting Conditions [ X] Bolt (?b. 4 , Size E ) !

[ ] Weld (Iength ) !

M unt d n Panels

[ X] (

i

7. Natural Frequencies in Each Direction:

29 h2: 16 V: none hl:

Functional

Description:

Part of the intermediate !.

8. a.

1 range monitoring subsystem '

(See attached any.Oual. T bl !

b. Is the equiFrent required $ori)] Hot Standby [ ] Cold Shutdcm

[X]Both l

9. Pertinent Peference Design Specifications:

4> 1 Peference: CgD File Ph. CCD 000258 SAINiEifTt LUlfDY

suaisena. n m .. ,m .- ,-(;-% 6 l

l

I

/0/

IIll.IsEquiprentAvailablefor p [x] YCS []?b

() Ocm:ents:

1 X

IV. Equitrent O.nlification Methcx!: 'Ibst:

Analysis:

s Ombination of Test and Analysis: _

Test and/or Analysis by CE Test Report 22A4232 dated 14-8-76 (nane of capany or Laboratory & Report !b.) (

r Vibration Input: l V. r l

l 1. Ioads considered 1.[X] Seismic only 2.[ ] Hydrodynamic only 3.[] Explosive .

on1y '1 l

4.[X] Other (Specify) 5.[ J Orbination of 164 h 1

l ! '

\

j 2. Required Response Spectra (attach the graphs): NA l 1

E ,

' s

3. Required cr celeration in Each Direction: , l h1 = / / u3 h2 = 6> 769 V=6,9f VI. If Qualification by Test, then Ctrolete:

c

1. [X] Single Frequency [ ] Multi-Prequency iI 2. - [ X' Single Axis [ ] Multi-Axis j l

1 - 33 Hz l 3. Frequency Rarc,a:

{

r 4. TRS enveloping RRS using Multi-Frequency Testl ] Yes (Attach TRS graphr-

[ ] tb 1.8g

5. g-level Test at hl = 1.8g h2 = l88 V=

i

6. Iaboratory > bunting: [

I l

l 1. [X l Bolt (!b . 4, size !) [ ] Weld (Iangth )[ ]

l I

I Functional operability verified: [X] Yes [ ] tb [ ] Itt Ipplicable f 7.

8. Other tests p>_rforned (such as fragility test, including results)

I Exploratory Testing, Fatigue Testing, Proof Testing j I

l ,!!

t

Pcference: CQD File ?b. CQD 000258 SAflGENT t LUNDY K

muoise m a na ij l ... .,

, _ -, ,_=-==...m ._ . .m m _. r, l

i 10f O If Qualification by Analysis or by the Cabination of Test and Analysis,the .

VII.

V (bnplete: N/A l

1. Description of Test including Results:

2. Method of Analysis:

[ ] Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic

[ ] Pespnse Spectrum [ ] Tim-History

3. bbdel Type: [ ] 3D [ ] 2D [ ]1D

[ ] Finite Element [ ] Beam [ ] Closed Fom Solution

4. [ ] Conputer Codes:

Frequency Range and !b. of nodes considered:

[ ] Hand Calculations

5. Danping: _ , _ _

6. Support Considerations in the model:

7. Critical Stnictural Elenents: Go'/erning Seismic 'Ibtal Stress .

A. Identification Iccation Feseense Cor.bination Stress Stress Allcvable8 l

Effect Upon Functional Incation Op3rability B. Mix. Deflection i d

aeference: cQD File :b. 000258 ung a sp h

_3_ IENGINEERSU;'

. :e_ a ,,--

nutech ,,g San J:sr, Californi:

Project Zir=er/La Salle SORT Recualification Procram File No.

wner Cincinnati Gas and Electric Commanv/Cor.monwealth Edison Comoany Client Cincinnati Gas and Electric Comcanv/Cc= onwealth Edison Concany TABLE I INSTRUMENT DATA INSTRUMENT NAME: Voltage Preamplifier MODEL NO.: 163C1263AA

SERIAL OR ID. NO.:

MANUFACTURER: General Electric

~

SPECIAL FEATURES IF ANY: None l l Monitor reactor core neutron level and FUNCTION: provide input to Mean Square Voltage Wide Range Monitor. ,

DIMENSIONS: 10.5"H X 6.5"W X 5.2"D WEIGHT:

' REQUIRED RANGE: 8 to 16 KHz and 300 to 600 KHz l

REQUIRED ACCURACY: 1 3 %.

l MONITORING REQUIPF.'ENTS: Input voltage and frequency and output voltage l

MOUNTING DETAILS: See Figure 1 1 .

l l To be completed by test laboratory 1

I I 1

l Revision l 8 l l Page l

Prepared By/Cate l M3[fghj of

I nutsch ,,,

San J:s?, Califunia Protect Zimmer/La Salle SORT Recualification Procrara File No

/ N Owner Cincinnati Gas and Electric Comnanv/Cor-onwealth Edisen Ccrpany

'~

Client Cincinnati Gas and Electric Cernanv/cn-nnwnal *h eM enn en-n,nv CHANNEL

.w[ FENDER y WASHER d[ WLON VOLTAGE PREAMPLIFIER i

[M BUSHING 163C1263AA

. 3 <. -J_.

_ 1/4-20 X 1.25 .81 X 1.62 PAN HEAD SCREW CHANNEL -

$ MOUNTING LUG SECTION A-A 8.75" >

1 4

\ < >/

+ + +

l O

J3 J4 7.94" O

R44 J1 J2

>A

+ + +

l j/ .

N -

>A

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0.30" DIA MOUNTING BOOKEND FIXTURE HOLE (TYP. OF 4)

MOUNTING FOR GENERAL ELECTRIC VOLTAGE l PREAMPLIFIER 163Cl263AA 1

U T Ctio c' 1 Re..sien l O I i l l I Page l Prcuarec ByiCate DLVYp///fll l l ,

i '

r..c , . , ' A m -/"i

nutech /N u

San Ase, California -

Project Zimmer/La Sa1le SORT Recin! i ci c,*i n , n-n g .m File No.

Owner Cincinnati Gas and Elec*-ic c m , n v / r n-n~ n , ' '-k Edire company ,

tcnt Cincinnati Gas and Electric Cencanv/comonwealth Edison Comeany l ll t

VOLTAGE PREAMPLIFIER 163C1263AA-l i

o

\ f J

+ +~ +

I I O

D t

i l

+ + .

+

l l ACCELERO:.1ETER LOCATION FOR GENERAL I

l } ELECTRIC VOLTAGE PBEAMPLIFIER 163Cl263AA FIGURE 2 Rev sion I d l l l I'rc;;ared Sy / Cate 4W 7/f/l f l Of I Ch0%ed E v / O. ate Q3 f/,#3/f/ I i l

II]

YOLTAGE PREAMPLIFIER C51-K002 -

((]

v ENVIRON!GNTAL QUALIFICATION TABLE C51-1 -

1. DESCRIFTION The Instrument is a kItae;c Preacplifier Manufactured by General Electric Company.

2. SAFETY FUNCTION Voltage preacplifiers condition the output signals from the IRM detectors to the IRM's, which are capable of generating a trip signal to the PPS to prevent fuel datase from single operating errors or equipment mlianc-tion in the intermediate power range.

3. SAFETY DESIGN PARAMETERS A. Glin: Low Frequency - 4500 High Frequency - Adjustable 200 to 1000 '

B. Output: Mest drive 75 che load with 4.0 volt peak to peak signal 4 FSAR ENVIRON:GNTAL CONDITIONS The instrument is located in the reactor building. The FSAR environmental conditions are tabulated below:

Duration Te=perature Pressure Humidity Radiatien Normal 1350F 40-55% 1.4x106 Rad b Maxicum

-0.5 to 2.0 psig Normal 2.5x1012ny7 1500F 90% Max.

5. ENVIRONMENTAL QUkLIFICATION ENVELOPE (Spec. 22A3008 Rev. 5)

Duration Tenperature Pressure Humidity Radiation Nor=al

135 F -0.5 to 40-55% 1.4x106 Pa d 2.0 psig Normal Maxi =um 1500F 90% Max. 2.5x1012NVT

6. QUALIFICATION !GTHOD Type Test The high and low frequency output, peak frequency response, and high voltage were monitored in environtental conditicns rangirs frc= 400F to 1400F and 90%

RH. No tes t times .

7. RESULTS

_ The pre.arplifier operated per its design and performance specification during the test environment.

b

NCN TEST PRC CE. DURE jp,i

.. not be considered a malfunction, but shall be noted in the test report. Failure is indicated if the test specimen does not maintain output voltage t5t while undergoing vibration in accordance with paragraph 5.3. Failure is indicated if the test ,

specimen does not meet the operational requirements after vibration in accordance with paragraph 4.2.2.2. All failures shall be rated on the test report.

5.0 TEST REQUIREMENTS 5.1 Exploratory Testing Exploratory testing shall be performed to determine the test specimens' resonant frequencies, if any, within a specified frequency range. A recommended procedure for this testing is provided below. Fast Fourier Transform (FFT) or other testing methods will be acceptable provided they yield the same

^

information about the dynamic characteristics of the test specimens.

5.1.1 Sine Sweep Recommended' Test Parameters Test Method: Low Level Sine Sweep Input Motion: Single axis .

Os Number of Tests: 3 with one in each Orthogonal Axis Frequency Range: 1 to 100 Hz Sweep Rate: Less than 2 Octaves per minute Input g Level: 0.1 g Peak 5.1.2 Exploratory Testing Results The acceleration response in g's and the transfer function for the accelerometer location shall be plotted as a function of frequency.

5.2 Fatigue Testing Fatigue testing shall be performed in order to account for any possible long term effects the SRV and LOCA event may have upon th5 test specimen.

This test phase shall be conducted in two parts, -

first, SRV fatigue testing and second SRV + LOCA l fatigue testing. The RRS to be used are those gen-erated during previous vibration testing.

l l

MK2-02-099 9 i

( .

e

//6 5.2.1 SRV Fatigue Testing.

Test-Method: Rancom motion Input Motion: Biaxial '.

Excitation: 2 independent random signals Level: Table TRS to envelope RRS

. Number of Tests: 1 in each test specimen orientation Test Specimen Orientations: 2 orientations (1) _

Front to back/ vertical (2) Side to side / vertical ,

Frequency Range: 1 to 200 Hz Duration of Individual Time History: Less than 20 sec Total Test Duration: 400 sec each orienta-tion .

RRS Damping: 2%

Required Response Spectra: Figures 5 and 6 5.2.2 SRV Fatigue Testing Results TRS shall be plotted for table accelerometer

("') locations at a damping value of 2% at 1/6

\/ octave intervals. For comparison the table

- .TRS and RRS shall be plotted on the same sheet. Power Spectral Density (PSD) plots shall be developed from the table acceler-ometer time histories for each test specimen orientation.

All accelerometer signals shall be recorded on analog magnetic tape.

5.2.3 SRV + LOCA Fatigue Testi:.g Test Method: Random motion Input Motion: Biaxial Excitation: 2 independent random signals

. Level: Table TRS to envelope RRS Number of Tests: 1 in each test specimen orientation Test Specimen Orientations: 2 orientations l (1) Front to back/ vertical ,'

/ .

(2) Side to side / vertical f

() Frequency Range : 1 to 200 Hz

~

MK2-02-099 10

Ilh Duration of Individual Time History: Less than 20 sec >

g--)s t Total Test Duration: 200 sec each orienta- ,

tion RRS Damping:

2%

Response Spectra: Figures 7 and 8 4

5.2.4 SRV + LOCA Fatigue Testing Results TRS shall be plotted for table accelerometer locations at a damping value of 2% at 1/6 octave intervals. For comparison, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed from the table accelerometer time histories for each test specimen orientation. All accelerometer signals shall be recorded on analog magnetic tape.

5.3 Proof Testing The adequacy of the test specimens for upset and emergency plant conditions will be demonstrated by the proof testing phase. This phase will be divided into two parts, testing for upset plant condition and testing for emergency plant condition, and shall

[' consider the maximum combined dynamic loads the test

\~ specimens may experience under each condition. The RRS to be used are those generated during previous ,

. vibration testing and data reduction.

5.3.1 Upset Condition Testing Test Method: Random Motion -

Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelope RRS '

Test Specimen Operation: As .Cecified below Test Specimen Orientations: 2 orientations -

(1) Front to back/ vertical (2) Side to side / vertical Number of Tests: 5 in each test specimen orientation (1) Before performing the low and high frequency tests repeat paragraph 4.2.2.1. .

(2) Low Frecuency Tes t a) Pre-Vibration

1) Turn OFF all power to the

( ,

voltage preamplifier.

MK2-02-099 11 E _

. t

+

2) Connect the equipment in i .accordance with Figure 4.

(~'/

s-

3) ' Turn ON the power to the

' voltage preamplifier and

. place switch S2 in the OPEN position and switch S1 in the CLOSED Position.

4) : Turn ON the test oscillator sand RMS voltmeter.

, 3) . Set test attenuation to

position 3.

6) , Set the test oscillator out.put frequency to 10 Hz and -adjust the test ,

aoscillator output signal

. amplitude to obtain a reading of 1.0 VAC on the RMS voltmeter.

. b) During Vibration Maintain the above conditions for 2 tests in each test specimen orientation.

(3) High Frequency Test a) Pre-Vioration

1) If testing has been stopped O '

repeat Steps (2) a) 1) and

-(2 ) a) 2).

2) Turn ON the power to the voltage preamplifier and place switch S1 in the OPEN position and switch S2 in the CLOSED position.

. 3) Set test attenuator to position 4.

4) Set the test oscillator output frequency to 350 Hz and ad]ust the test r oscillator output signal amplitude to obtain a reading of 0.5 VAC on the

, RMS v71tmeter, then sweep the test oscillator output frecuency between 350 KHz and 450 KHz to locate the frequency that provides the peak output from the voltage preamplifier as indicated on the RMS voltmeter. Record RMS :

[') voltmeter reading. j

\_/

~

i MK2-02-099 12

8 lll b) During Vibration f_3 Maintain the above xl conditions for 3 tests in

each test specimen

orientation.

Monitoring Requirements: Input voltage and frequency and output voltage.

Frequency Range: 1-200 Hz Test Duration: 30 sec per test RRS Damping: 2%

~

Required Response Spectra: Figures 9 and 10 5.3.2 Upset Condition Testing Results TRS shall be plotted for table accelerometer locations at a damping value of 2% at 1/6 octave intervals. For comparison, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed for the first test in each orientation. All acceler-

- ometer signals shall be recorded on analog magnetic tape.

5.3.3 Emergency Condition Testing

() nput at Excitation:

Ba a 2 independent random signals Level: Table TRS to envelope RRS Test Specimen Operation: As specified below Test Specimen Orientations: 2 orientations (1) Front to back/ vertical (2) Side to side / vertical Number of Tests: 1 in each orientation per-form test in accordance with para-graph 5.3.1 (2) in one orientation and in accordance with paragraph 5.3.1(3) in the other orientation.

Monitoring Requirements: Input voltage and frequency and output voltage.

Frequency Range: 1 to 200 Hz Test Duration: 30 sec. per test RRS Damping: 2%

Required Response Spectra: Figures 11 and 12 Operational Test: Checkout test specimen after emergency condition tests in accordance with paragraph 4.2.2 10

\~j MK2-02-099 13 .

l l

. s

//f s 5.3.4 Emergency Condition Testing Results TRS shall'be plotted for table accelerometer locations at a damping value of 2% at 1/6 octave intervals. For comparison, the Table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed from the table accelerometer time histories for each test specimen's orientation and voltage relay operation. All accelerometer signals shall be recorded on analog magnetic tape. Results of operational test checkout after exitation shall be reported and any significant devia-tion from the baseline shall be noted in the final report.

6.0 WITNESSING OF TESTS 6.1 All tests shall be subject to observation by NUTECH or their authorized representatives.

6.2 All tests shall also be subject to observation by Cincinnati Gas and Electric and Commonwealth Edison Companies or their authorized representatives.

~T 7.0 TEST REPORT REQUIREMENTS *

(G

~

The test laboratory shall supply ten certified copies of a test report which satisfies the requirements of IEEE 344 -

1975. This report wil describe the equipment, calibration, and test procedures, including photographs of the test set up, and provide all results and conclusions from the test. Operational checkout and inspections shall be described and all results summarized and any deficiencies and/or repairs noted. Critical data to be included in this report are as follows:

7.1 Inspection and operational test results reports, verifying adjustments and recording values, also

, noting any significant deficiencies and repairs to 4

device. A description of test equipment and cali-bration information shall be included. ,

7.2 Test Specimen resonance search data 7.3 The test response spectra plots obtained in 5.2.2, 5.2.4, 5.3.2 and 5.3.4. These TRS are to be compu-ted for all accelerations recorded. For each of the two orientations for the test specimen, the TRS shall be computed for both horizontal and vertical I)

\/

table motions to verify that they envelop the cor-responding RRS.

MK2-02-099 14

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c. 2' FREQUENCY - HZ 8 e

Figure 4

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//2 QUALIFICATION OF h/RM-MSt/ Znloymec/ible Rango Menikg JUSTIFICATION FOR INTERIM OPERATION

~

The test repor submitted by CE meets the specified g levels.

Acceleration level comparisons are shown below.

Required g level from Panel Analysis h 1 = /.CZg , h2 = .//g V = .//df g level from Test Report h 1 =$,7g h2 "4 :Sy V =2 5g Therefore the equipment is qualified as for as test g levels are considered. .

However we opted to perform new tests for the following reasons:

a) Documentation of test log was insufficient.

b) Funcional testing of Instruments not adequately explained.

c) Single axis single frequenc'y testing was done.

The new tests will be done to the test requirements as attached as soon as the test specimen is procured. .

For the above reasons we strongly feel that the device l

l is qualified for the interim operation.

i i

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! Ri LA SALLE NUCLEAR STATIONS'

( UNIT 18 2 NSSS EQUIPMENT QUALIFICATION

SUMMARY

t

)j EQU1PMENT NAME . WRM-MSV Intercediate Range Monitor # 368X102AA

! EQUIPMENT NO: c51-K601A/H 1

l LOCATION: Reactor Building El. 768'0" on Panel H13-P635, H13-P636 I

! E00'PMENT CLASSIFICATION: O ACTIVE ] PASSIVE QUALIFICATION METHOD: Test QUALIFICATION DOCUMENT

REFERENCES:

1. GE # 175A7267 Rev.3. ,

2. GE letter dated 11-19-74 on Hanford - 2 Radiator Monitor

3. GE # 262A7244 dated 12-16 75 Rev.0

'.GE # 262A7445 dated 2-13-74 Rev.0 5.GE # 225A6956 dated 11-30-70 Rev 0

6. GE # 225A5766 dated 1-05-78 Rev.7

! 7. GE PPD for # 368X102AA by GE f 8.

i g 9. .

' E 10 .

d 1] LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

1. Normal Operating Loads + OBE + {SRVASY-TQ + SRVALL-TENVELOP !

. l

j 2. Normal Operating Loads + SSE + CO EVY-2+ SRVASY-TQ ALL-TQ ENVELOP 1

! 3. Normal Operating Loads + SLE+ Chugging + 5RVASY-TQ + SRVALL-TQENVELOP

4. Normal Operating Loads + SSF *AP

5. Normal Operating Loads' 2 c. G LEVY-1 QUALIFICATION:

PREPARED BY: Date ,

REVICUED BY: Date SARGEijT& LUTJDY l APPROVED 7Y: "" * "

4r*

Date C M *C A G O

...-7,. . . __ - .- -_ . .

8.

/M 1

'l QUALIFICATION

SUMMARY

1. Test for Hanford - 2 GE Doc. 262A7244_Rev..O and CE letter

. dated 11-19-74.

i .

GE WRM was testcd along with the Hanford Radiation Monitoring Cabinet 4

H13-P606. The cabinet is similar to LASALLE Cabinet.

l a) Low level resonance. earch test from 1 - 33 Hz in each axis l b) High level sweep tests at resonant frequencies in each axis.

V Max Test 'g' levels to Cabinet h t = h 2 = V = 1.73g Max 'g' level for WRM hi =5 9 g h h=45g 2

V25g O

Qualification Su.m of Equirrent /26

( 7, py .

LASALLE COUNTY 1&2 'Pype-

1. Utility; CECO PWR

2. NSSS; GE IMR

3. A-E; S&L ;

i.

II. Cmoonent Nane WRM-MSV Intermediate Range Monitor # 368X102AA l

1. htxiel Nu"ber None Quantity: 8 Vendor :

2. GE

3. If the cmponent is a cabinet or panel, nane and nodel tb. of the devices incitried; l'

4. Physical Description a. Appurance Instrumentation

b. Dinensions 7"H x 19"W x 16"D

c. Weight Reactor Building

5. Location: Building:

Elevation; 768'0" on Panels H13-P635/636

6. Field bbunting Ccnditions [ ] Bolt (!b. , Size )

g!

i i ( See attached figures) [ ] Weld (Inngth ) n

[ ] h

. e

7. Natural Frequencits in Each Direction: None 'i hl: h2: V: ,

e f

8. a. Functional

Description:

_ Used in the neutron monitoring i system ( See attached Env. Qual. Table )

i i

b. Is the equirent 1 required for[ ] Hot Standby [ } Cold Shutdown r

9. Pertinent Reference Design Specifications: ,

I i

1

Reference:

CQD File ?b. CQD 000259 SARGEllT 'r Luff

ewomseneC

... u DY

-~-----ma-.m, . m.a - , , , _ feApy

i r-- - - - - - . , _ , _ _ _

/26 7s III. Is Ecuiprent Available for Inspection in the Plant: [X] Yes []tb

)

(

Ctsments:

X IV. Equipr:ent Qaalification Method: 'Ibst:

~

Analysis: ?

L i

CbiTbination of 'Ibst and Analysis: h l1 Test and/or Analysis by GE Report # 262A7244 Rev.0 [

(name of Ccrpany or Laboratory & Report !b.) h l.

V. Vibration Input: ]

i 6 r 1. Ioads considered 1.lX] Seismic only 2.[ ] Hydrodynamic only 3.[] Explosive ,

only [;

4.[ ]Other (Specify) 5.[ ](bcbination of h

2. Pequired Response Spectra (attach the graphs): NA l,

Pequired Acceleration in Each Direction:

I

3. ,

j I h1 = 1.02g h2 = 48 V= .46g [r.

VI. If Qualification by Test, then Camlete: I)'

l' l. [X] Single Frequency [ ] Wlti-Frequency 3

.) 2. . [X] Single Axis [ ] Multi-Axis .

3. Frequency Rw a: 1-33Hz l i 4. TRS enveloping RRS using Multi-Frequency Test [ ] Yes (Attach TPS grapind NA t f 5.9g 4.5g I3 2.5g

5. g-level 'Ibst at hl = h2 = V=

/

6. Iaboratory obunting: (See sketch attached)

1. [ ] Bolt (ib . , Size ) [ ] Weld (Length )[ ] t

7. Functional operability verified: F ] Yes [ ] tb [ ] tbt Ipplicable j 8. Other tests performcd (such as fragility test, including results) {J I Exploratory Testing i

.3. ,

Pcference: CQD File tb. CQD 000259 SARGENT r LUNDY !ip l

' .~.~...A

. .m. . e E_

____m_.

_m ,, _ , , , _ ,_, ,

i i

/27 VII. If Qualification by Analysis or by the Canbination of '1bst and Analysis,the ,

Cmplete: NA

1. Description of Test including Pesults:

2. M2thod of Analysis:

[ ] Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic .s Analysis

[ ] Pesponse Spectrum [ ] Tine-History

3. bbdel Type: [ ] 3D [ ] 2D [ llD 1 ] Finite Eleannt[ ] Beam [ ] Closed Form Solution'

4. [ ] Conputer Codes:

Frequency Pange and tb. of nodes considered:

[ ] Hand Calculations

5. Damping: _ _ _ _

6. Support Considerations in the model:

D 7. Critical Structural Elenents: Coverning Seismic Total Stress A. Identificaticn Location Pestense Conbination Stress Stress Allcuble' Effect Upon Functionalt Location Operability B. Max. Deflection _

t 000259 SARGENT n LUNDY 4 Pcference: COD File tb. l 2 E NQiNE E54S J; e

1

v INSTRUMENT IDENTIFICATION &

U**

. .( LIFICATION REQUIREMENTS ! /T L)

Name: WRM-MSV Intormedicts R:ng2 Qualification 'g' levels

Honitor Manufacturer: GE hi = 5.9 h 2= 4. 5 V= 2. 5 Model No. : 368X102AA Instrument Required 'g' levels Equipment Numbers Location . Class. Remarks h1 h2 V C51-K601A/H Reactor Building 1.02 .4 .46 IE El. 768'0" on Panel H13-P635/636 A - Active P - Passive 1E - Class 1E

nutech ,g San hs;, California -

c.

Project Wm. H. Zimmer/La Salle County Nuclear Power Stationsfile No.

Owner Cincinnati Gas and Electric Co./Commwealth Edison Co.

) Client Cincinnati Gas and Electric Co. /Comrwealth Edison Co.

i TABLE 5

. INSTRUMENT DATA ,

INSTRUMENT-NAME: Mean Square Voltage-Wide Range

. Monitor MODEL NO.: 368 X 102AA

SERIAL OR ID. NO.:

MANUFACTURER: General Electric SPECIAL FEATURES IF ANY: None i

{ } Receive input current proportional to FUNCTION: neutron flux from voltage preamplifier and provide RPS trip outputs DIMENSIONS: 7"H X 19"W X 16"D WEIGHT:

. REQUIRED PANGE: 8 to 16 KHz and 300 to 600 KHz REQUIRED ACCURACY: + 3%

MONITORING REQUIREMENTS: Input voltage and frequency and output trips and voltage MOUNTING DETAILS: See Figures 1 and 10 To be completed by test laboratory l I Revision l 8 l !

Page 40 Prepared Sy/Date lff/02/g/jpfjl e, 40 Checked By/Date !/,t4 f/4//7 I i

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(3/

STARTUP SYSTEM IRM/MSV C51-K601 i

.,h ENVIRONMENTAL QUALIFICATION TABLE C51-3 (N/ ;

1. DESCRIPTION The instrucent is a General El'ectric Company Intercediate Range Monitor Dws Number 368X102AA. , which measures the mean square value of varia-tions in the average value of the detector signal in one of two dis- -

crete band widths. .

2. SAFETY FUNCTION The I.R.M. provides annuciation outputs, triplight cutputs, co:puter out-puts, and rod block outputs. It also initiates one RPS trip during reactor anosalics.

3 SAFETY DESIGN PARAMETERS A. Power requirements: + 20 Vdc at C .7A B. Signal level: 0.-10 volts C. Output: isolation protected

4. FSAR ENVIRONMENTAL CONDITIONS The instrunent is located in the control room panel H13-P635. The FSAR environmental conditions are tabulated belou:

Duration Temperature Pressure Humidity _ Radiation

(%/[~')

Min 400F Range 10% operating 0.0005 R/hr Normal 60-900F 0.10 in. to 40-50% Accident (6 cos) 3x100Ead thx. 1200F 1.0 in, water 60%(1) Integrated (40 yrs)

Gauge static 1.75x102 Rad .

Pressure 5 ENVIR0 MENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Temperature Pressure Humidity Radiation Min 400F Range 10% Operating 0.0005 R/hr Normal 60-90 F 0.10 in. to 40-50% Accident (6 cos) 3x10 0 Ead Max. 1200F 1.0 in. water 601(1) Integrated (40 yrs)

Gauge static 1.75x10 2 Rad Pressure (1) During HVAC Equipnent failure conditions relative humidity nay approach 90% for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 1200 F would not occur simultaneously.

6. QUALIFICATION METHOD Type Test No data

' - - 7. RESULTS None

NE TEST PROC & DURE

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

6.2.12.7 Adjust the input amplitude to the MSV-WRM until there is 1.000 *

[)

uj

.030v at the recorder output.

6.2.12.8 Lower the frequency until the recorder output is 0.500 + .030v.

Keep the input constant. Verify *

) that the frequency is less than 8.5 kHz.

6.2.12.9 Adjust the frequency of the test oscillator for 100 kHz sinewave and the amplitude for 1.00 volts at the recorder output of the MSV-WRM.

6.2.12.10 It may be necessary to readjust R19 on ARll to obtain the correct recorder indication for range 7 s only. (If R19 is readjusted the calibration signal must be readjusted by adjusting R9 on Z10). Measure the rms input ,

voltage at J1 on the MSV-WRM chassis.

6~.2.12.11 Complete the data required in Table

(~'

\

3. The test frequency for the high and low gain amplifiers will be the

same for the test (100 kHz).

Verify that the output is given in 6.2.12.3.

6.2.13 Check of Relay K10 (ten) in the Mean Square Analog Unit Module 194X669G1 (GEK-855). , ,

6.2.13.1 Check relay K10 in the mean square analog unit to ensure that relay K10 contacts are closed on ranges 1

one through six, and are open on

' ranges seven through ten (use a multimeter - on voltage range -

across the relay contacts). -

7 .'O VIBRATIONAL TEST REQUIREMENTS 7.1 Test Specimen operation During Testing "

, During vibrational testing the test specimen shall be j setup as depicted in Figure 2. During exploratory testing the operation shall be in accordance with i /~T U

MK2-02-037 15 l

u - - -- = ---------- ----- - - -- -- -- -

lS paragraph 7.2.1. During OBE and DBE tests the

_s operation shall be as indicated in paragraphs 7.3.1.

[U T and 7.3.3 respectively.

7.2 Exploratory Testing i

Following the Baseline Operational Testing and Cali-bration (if required), exploratory testing shall be performed to determine the test specimen's resonant frequencies over the frequency range of 1-100 Hz. A recommended procedure for this testing is provided below. Other testing methods will be acceptable provide,d they yield the same information about the dynamic characteristics of the test specimen.

7.2.1 Sine Sweep Recommended Test Parameters Test Method: Low Level Sine Sweep Input Moti~n: o Single Axis Number of tests: Three with one in each Orthogonal Axis i Frequency Range: 1 to 100 Hz

, (~T Sweep Rate: Less than 1 octave per

(_) minute Input g level: 0.25 g Peak Test Specimen Operation: As specified below 7.2.1.1 Pre-Vibration -

(1) Turn OFF the + 26.5 VDC power to the MSV-WRM.

, (2) Connect equipment in accordance with Figure 2.

Place switch S2 in the CLOSED position.

(3) Turn ON the + 26.5 VDC power to the MSV-WRM. -

(4) Turn ON the test oscillator,

( c. digital voltmeter and RMS voltmeter. Verify or set the test oscillator output signal

[Jb amplitude to 0 volts.

MK2-02-037 16

_ , . _ _ _ _ , . _ _ _ _ , .m...-_,- _.- - N*

1 - -

. .r.

l3f I

(5,) Place the MSV-WRM selector

~ switch to the OPERATE posi-

. . tion and momentarily' place the MSV-WRM RESET switch to

,. the TRIP position.

(6) Verify that all MSV-WRM indi-

cating lights, except for the DOWNSCALE LEVEL indicating

, li gh t (DS16B), are ,

extia. ;uished.

(7) Verify that there is 0 j; 0.1 VDC across resistor R3 and 12 j;2 VDC across resistors R1, R2, and R4.

(8) Verify that there is 0 VDC across MSV-WRM receptacle J4, pins H and K.

(9) Place th e range switch to' -

position 1.

l .(10) Set the test oscillator

, frequency to 100 KHz.

(~')

j (11) Increase the test oscillator output signal amplitude until 4

there is 12 + 2 VDC across resistor R3 and the DOWNSCALE l, LEVEL indicating light (D16B)

, extinguishes.

7.2.1.2 During Vibration .

Maintain the above conditions during the exploratory testing.

Test Specimen

, Monitoring: Monitor trips and recorder outputs in accordance with para-i graph S.2 Operational Test: In accordance with paragraph 6.1 L

7.3 Proof Testing

/~ The adequacy of the test specimen for Operating Basis i

km ,)/ Earthquake and Design Basis Earthquake will be demon-4 MK2-02-037 17 4

~

/Ji strated by the proof testing phace.. This phase shall be divided into two parts, 1) testing for OBE plant

(~)-

I condition, and 2) testing for DBE plant condition.

j The tests shall consider the maximum seismic loads the

/ test specimen may experience under each condition.

The defined input response spectra to be used are included in Figures 5 thru 8.

l 7.3.1 OBE Testing Test Method: Random Motion

Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelope RRS Test Specimen Operation: As specified below ,

. 7.3.1.1 Normal Conditio_n_

(1) Pre-Vibration a) If testing has been stopped repeat paragraph 7.2.1.1 (1) through (8) as required to achieve normal condition.

b) Place the range switch to position 2.

c) Set the test oscillator output frequency to 100 KHz.

d) Increase the test oscil-lator output signal amplitude until there is 12 +j2 VDC across Resis-tor R3 and the DOWNSCALE LEVEL indicating light (DS16B) extinguishes.

(2) Durina Vibration g_)

Maintain the above conditions for 1 vibration test in each MSV-WRM orientation.

MK2-02-037 18 m

lbh 7.3.1.2 Downscale Trip

'( ) a) If testing has been stopped repeat steps 7.2.1.l(1) through (8) as required to

./ achieve normal condition.

i b) Place the range switch to position 5.

c) Set the test cscillator '

output frequency to 100 KHz.

(2) During Vibration a) Decrease the test oscil-lator output signal amplitude to the recorded value (+3%) in

, paragraph 6.1.14 and verify that there is O

+ 0.1 VDC across Resis-tor R3 and that the

~

DOWNSCALE LEVEL indi-cating light (DS16B)

/~ illuminates.

N.))

b) . Pe'rform this test once in each MSV-WRM orienta-

, tion.

7.3.1.3 Upscale (Hl) Trip (1) Pre-Vibration ,

a) Repeat steps 7.2.1.l(1) through (8) as required to achieve normal ,

conditions.

b) Place the range switch to position 8. -

c) Set the test oscillator output frequency to 100 l KHz.

(2) During Vibration p ~a) Increase the test oscil-l \,_)s lator output signal l

MK2-02-037 19 ,

i 1

a7 amplitude to the recorded value (+3%) in

() -

paragraph 6.1.12 and verify that there is O

+ 0.1 VDC across Resis-

< tor R2 and that UPSCALE LEVEL indicating light (DSl*/A) illuminates.

b) Perform this test once n-each MSV-WRM orienta- .

tion. -

7.3.1.4 Upscale (HI-HI) Trip) -

(1) Pre-Vibration -

a) If testing has been stopped repeat steps 7.2.1.1(1) through (8) as required to achieve normal condition. f b) Place the range switch to position 11.

c) Set the tect oscilator O- -

output frequency to 100 KHz.

(2) During Vibration a) Increase the test oscil-lator output amplitude to the recorded value (+

3%) i'n paragraph 6.1.13 and verify that there is 0 + VDC across Resistor Rl and that UPSCALE LEVEL indicating light (DSl7B) illuminates. .

b) Perform this test once in each MSV-WRM orienta-tion.

7.3.1.5 Inoperative Trip (1) Pre-Vibration a) Verify the followinc:

O

~

MK2-02-03? 20

r 131

1) + 26.5 VDC MSV-WRM power is ON.

(J^]

2) MSV-WRM selector switch is in the OPERATE position.

3) . Switch S2 is in the CLOSED position.

4) MSV-WRM RESET switch "

has been momentarily placed in the TRIP

. position.

5) The monitoring circuit is connected across Resistor R4 and the voltage reading is 12 + 2, VDC.

6) INOPERATIVE indi-cating light (DS16A) is extinguished.

()- (2) During Vibration a) Place switch S2 in'the OPEN. position. Verify that there is O + 0.1 VDC across ResisI'or R4

~

and that INOPERATIVE indicating light (DS16A) illuminates. .

b) Perform this test once in each MSV-WRM orienta-tion.

Test Specimen Orientation: 2 orientations (1) Front to back/

vertical (2) Side to side /

vertical Number of Tests: 10 with.S in each orientation

l MK2-02-037 21 .

P

/39 Test Specimen

',r- Monitoring: Monitor MSV-WRM trips,

( j .

test oscillator output signal amplitude (signal input) and recorder outputs in accordance with paragraph 5.2 Frequency Range: 1-100 Hz Test Duration: 30'sec per test ,

Damping: 2% ,

Required Response Spectra: . Figures 6 and 7 Operational Tests: If the operational tests performed during the DBE i are satisfactory, then operational test in accordance with para-graph 6.1 may be waived.

7.3.2 OBE Testing Results I' TRS shall be plotted for each accelerometer

,\/

(^T location at a damping value of 2% at 1/6 octave intervals (2.5 damping is acceptable).

-For comparison,.the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be +

developed for the last test in each orienta-tion. The test laboratory shall provide an analog tape of time history response for each accelerometer recorded on standard 14 channel IRIG tape with a voice channel. Response -

shall be unfiltered from 1 to 200 Hz. Test specimen operability shall be noted. Plot downscale trip with recorder output, upscale (hi) trip with recorder output and upscale (hi-hi) trip with recorder output. NUTECH shall be notified of.lo, hi, and hi-hi trip 4

points before proceeding with DBE testing.

2 7.3.3 DBE Testing *

Test Method: Random motion Input Motion: Biaxial l

Excitation: 2 independent random signals k

=.

MK2-02-037 22 i

IMO.

4 4 ,

Level: , ,

Table TRS to envelope 1 ,

i. T,est Specimen Operation: As specified below t

7.3 3 1 Upscale (Hi-Hi) and Inoperative Trip j

, (1) Pre-Vibration

~

a) Repeat paragraph 7.2.1.1 4 as required to achieve '

l 4

normal condition.

(2) During Vibration a )' Increase the test oscil-lator output signal amplitude to the recorded value (-t 3% ) in paragraph 6 3 1.13 and-verify that there is 0

+ 0.1 VDC across

. IIesistor R1 and that UPSCALE LEVEL indicating

() .

light (DS17B) illuminates.

b)

Place switch S2 in the 4 OPEN position. Verify that there is O + 0.1 VDC across Resistor R4 and that INOPERATIVE indicating light (DS16A) i illuminates.

Test Specimen Orientation: 2 orientations

. (1) Front to back/ -

vertical (2) Side to side /

vertical Number of Tests: 2 with 1 in each -

orientation Test Specimen Monitoring: Monitor MSV-WRM trips, test oscillator output signal amplitude (signal O- output) and recorder MK2-02-037 23

-,-y ,we, ._.m-. ,- y. . ,., , _ , , _ . . _ . _ . - . . .,,. . _ , , . , , . . , . . . , . . , , _ , _ _ . _ . -.s,.,-,..-,.__--r, . . , , , . ,-.

IU/

. . outputs in accordance g-with paragraph 5.2

()/ Frequency Range: . 1 to 100 Hz Test Duration: 30 sec. per test Damping: 2%

Required Response Spectra: Figures 8 and 9. .

Operational Tests: After the final DBE test in accordance with paragraph 6.1 7.3.4 DBE Testing Results TRS shall be plotted for each accelerometer location at a damping value of 2% at 1/6 octave intervals (2.5% damping is accept-able). For comparison, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed from the table acceler-ometer time histories for each test specimen orientation. The test laboratory shall

(')

provide an analog tape of time history response for each accelerometer recorded on standard 14 channel IRIG tape with a voice channel. Response shall be unfiltered from 1

to 200 Hz. Test specimen operability shall be noted. For the last DBE, plot lo trip with recorder output, hi trip with recorder output, and hi-hi trip with recorder output.

8.0 WITNESSING OF TESTS 1

8.1 All tests shall be subject to observation by NUTECH or their authorized representative.

All tests shall be subject to observation by 8.2 -

Cincinnati Gas and Electric Company, Commonwealth Edison Company, or their authorized representatives.

9.0 _ TEST REPORT REQUIREMENTS

' The test laboratory shall supply ten certified copies of a test report which satisfies the requirements of IEEE 344-1975. This report will describe the equipment, calibration, and test proce-dures, including photographs of the test set up, and provide all

(^)g results and conclusions from the test.

R.

'MK2-02-037 24 l

- - - ~ ,. e

M2 Operational tests and inspections shall be described and all *

results summarized and any deficiencies and/or repairs noted.

' Critical data to be included in this report are as follows:

9.1 Inspection and operational test results, verifying adjustments and recording values, also noting any significant deficiencies and repairs to the device.

Include a description of test equipment and calibra-ti6n.

i 9.2 Test Specimen resonance data ,

i For each of the two orientations for the test specimen 9.3 and for each test specimen state and operation, the TRS shall be computed for both horizontal and vertical table motions to verify that they envelop the corre-sponding RRS.

9.4 Time history recordings from OBE and DBE tests,

. recorded on standard 14 channel IRIG tape with a voice channel. Response shall be unfiltered from 1 to 200 Hz. Time histories shall also be plotted and included -

in the test report.

9.5 Power Spectral Density Plots from the selected OBE and ,,

DBE tests.

9.6 A record of the number of test runs, including testing level and duration, signal input levels and test ,

specimen operation shall be maintained for test runs 4 in the test -log.

9.7 Any direct records from instrument operational moni-toring (i.e. recorder plots).

9.8 A copy of the test log.

10.0 REFERENCES

10.1 'EEE 344-1975:

. Recommended Practices for Seismic

Qualification of Class lE Equipment for Nuclear Power Generating Stations.

10.2 GEK-45844A G.E. Operation and Maintenance Instructions (MSV-WRM with Range Switch) . .

O -

MK2-02-037 25

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FREQUENCY - HZ F m

Figure 4 H ~

Iforizontal DDE Itequired Response Spectrum N

m 1.

e nLitGCh pg San Jose, California

> Pro;cct k'm . H. Zir er/La Salle County ':uclear Power Stations Fdefio.

O Owner cincinnati Gas and Electric Co./corronwealth Edison Co.

'u Chent Cincinnati Gas and E10ctric co./ccrronwealth Edison Co.

I O

p reci 6 - i- i -

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1. .

QUALIFICATION OF

" O I/FP Yt /MS2@2 a

JUSTIFICATION FOR INTERIM OPERATION l

t The test report submitted by GE .'neets the specified' g levels.

Acceleration level comparisons are shown below.

Required g level from Panel Analysis h 1 =/,0Zg h2 " * //j V = 'l/bh g level from Test Report h1 =4,23

] h2 " //<2g V"6"l/[

, Therefore the equipment is qualified as for as test g levels i

are considered.

l However we opted to perform new tests for the following reasons:

a) Documentation of test log was insufficient.

b) Funcional testing of Instruments not adequately explained.

c) Single axis single frequency testing was done. "

l The new tests will be done to the test requirements as attached

, as soon as the test specimen is procured.

l For the above reasons we strongly feel that the device l

is qualified for the interim operation.

l l

I l

l b

iO

M6 }

%. A I

! LA SALLE NUCLEAR STATIONS' k UNIT 18 2 NSSS EQUIPMENT QUALIFICATION

SUMMARY

EQUIPMENT NAME : Indicator & Trip Unit # 129B2802 EQUIPMENT NO:D18-K609A/D, D18-K611A/B, D18-K615A/D LOCATION: Reactor Building El. 768' on Panels H13-P635 & M13-P636 C PASSIVE l EQUIPMENT CLASS #FICAT10N: @ ACTIVE l seismic Test ( see page 2) i QUALIFICATION METHOD:

i QUALIFICATION DOCUMENT

REFERENCES:

, 1 GE # 175A7267 Rev.3. !

F l 2. GE # 262A7244 dated 12-16-75 Rev.0 !

I

3. GE letter dated 11-19-74 on Hanford-2 Radiation Monitor J 4. GE # 262A7445 dated 12-13-74 Rev.0

5. GE # 225A6970 dated 11-30-70 Rev.0 l g 6. ATR - 510 -EAD05-01 d4!cd O p.77 _

! 7. GE # 225A5766 dated 1-05-78 Rev.7 f 8. GE # 235A1678 dated 9-14-72 Rev.0 l' 9. PPD for 129B2602 by GE g 10 .

)

l .

LOAD COMBINATIONS CONSIDERED IN QUALIFICATION: - ;

1. Normal Operating Loads + OBE + SRVASY-TQ + SRVALL-TO, ENVELOP

2. Normal Operating Loads + SSE + COLEVY-2+ SRVASY-TQ+b YALL-TQ ENVELOP

3. Normal Operating Loads + SSE+ Chugging + SRVASY-TQ + SRVALL-T ENVELOP l

4. Normal Operating Loads + SSE + AP

5. Normal Operating Loads + SSE + COLEVY-1 OUALIFICATION:

PREPARED BY: Date ,

REVIEI.'ED BY : Date ggg gg, APPEOVED 'W: **""" d N Date ,_ y'*

c T ,* 4 l- - - - - -

/47

[] Q'JALIFICATION

SUMMARY

%)

Several Tests were done by GE to qualify this device.

(2 are given below )

1. Test for Hanford-2 GE Doc. 262A7244 Rev.0 and GE letter dated l

11-19-74. I l

Indicator Trip Unit was tested along with the Hanford Radiation f l

Monitoring Cabinet H13-P606. The cabinet is similar to LASALLE cabinet.

I a) Low level resonance search test from 1-33 Hz in each axis.

l b) High level sweep tests at resonant frequencies in each axis.

Max Test 'g' levels to Cabinet h y= h = V = 1.75g 2

Max 'g' level for Indicator Trip Unit h t= 4.2g h 2 = 4.2g V = 5.4g t'x j

) 2. GE Doc. 225A6970. Test of Indicator & Trip Unit.

a) 7 minute sine sweep test - Freq. range 5-33Hz Input .02" DA.

Resonant Frequencies h t = h 2 " 31 H2

{ V = none I N h j b) 2 minute Resonance Dwell test at 31 Hz at 'g' level of

( l l h t= 1.0g I, h 2 = 2.1 g

, c) Vibration Endurance Test 5-33Hz at x = y = z = 1.5g I

d) Max. acceleration reached at 33Hz = 15 g's.

l Ref: CQD File No. ggg, gg,

=r.=u.: am,

{

~ ~ . - _ ~ . . . - - _ . - . . , _ _ = =

i .

Otulification Suminry of Equirttent //'/

/ i l

i

(~h l LASALLE COUNTY 1&2 .pype.

T. Plant Nane:

1. Utility: CECO FWR GE BWR X

2. NSSS; t

SEb j

3. A-E:

n Indicator & Trip Unit #-129B2802 II. Conponent h

1. bbdel Nu:rber None Quantity: 10 !

GE/NID ,;

i 2. Vendor !

L

) 3. If the conponent is a cabinet or panel, nane and itodel No. of the devices included;

{

I

4. Physical Description a. Appearance Instrumentation Dinensions 6"H x 2 ,'4"W x 121 /2"D t

! b.

i f C. Weight 4 lbs. j-

[

5. location: Building: Reactor Building - Control Room tl 9 Elevation; 768'0" On Panels H13-[635, 636 I

6. Field bbunting Cbnditions [ } Bolt (No. , Size ) 1 I

l See attached sheet Mounted on Panels fj i

( } g i -

7. Natural Frequencies in Each Direction:

31 Hz h2 31 Hz v. none from 5-33 Hz

! hl:

1 ;

Functional

Description:

used in connection with t f 8. a.

the Sensor Converter (See Env. Qual. Table)

?

I l b. Is the equipmnt requuul for[ } Hot Stardby[ } Cold Shutdosm

( }Both -

9. Pertinent Reference Design Specifications:

i I

(3 h v

neference: CQD rile No. CQD 000261 SARGrHTs:LUNDY

,== , ,

. - _ - - . _ ~ . _ ,

an, ,r

m,_,. __ ____

_ -xm . or

/ff!! ,

I "' '" '""**"""' ^""**"" ' ' '"""""'* " *" '"" "*"" '*' '*" '"

(vl i i Commnts:

(

n 4

l 1 b i X

IV. Equiptent Qualification Method: Test:

a '

Analysis:

Ombination of Test and Analysis:

'Ibst and/or Analysis by CE Report # 262A7244 Rev.0 ,

l (name of COTpany or laboratory & RcIrrt !b.) 'J J

V. Vibration Input:

a

1. Ioads considered 1.[X ] Seismic only 2.[ ] Hydrodynamic only 3.[] Explosive ['

only 4.[ ] Other (Specify) 5.[ ] Orbination of

2. Required Pesponse Spectra (attach the gra;ts):

Panel accelerations for panels H13-P635, 636

3. Required /cceleration in Each Direction:

{s 1.02 h2 = 0.40 y= 0.46 hl =

p

VI. If Qualification by Test, then Camlete: u

l. [X ] Single Frequency [ ] Malti-Frequency ]

~

-j 2. [X] Single Axis [ ] Multi-Axis

3. Frequency Farm: 1-33 Hz I

4. TRS enveloping RRS using Multi-Frequency Test [ ] Yes (Attach TRS graphs I

1 I J tb f 5. g-level 'Ibst at hl = 4.2g h2 = 4.2 y= 5.4 j l

6. Laborator'f fbunting:

1. [ ] Bolt (tb. , Size ) [ ] Weld (Inngth )[ ]

7. Functional operability verified: [)d Yes [ ] tb [ ] Not Applicable '

8. Other tests performed (such as fragility test, including results)

/ Resonance Search Test from 1-33Hz ;

(]_/ 4 l

o

Reference:

CQD File ID. C0D 000261 SARGENT E LUHDY p

ENGING nEJ y

'*C^

) li l immr n- =_Mw , i~Cg&

(

.~ _a d

'J 4

/9 1 r l

VII. If Qualification by Analysis or by the Ccebination of Test ard Analysis,thd

' l l

1 j Conplete: N.A. ,

l 1

1. Description of Test incltding Results. j s

2. Fbthod of Analysis: j j [ ] Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic i) 1 Analysis

' [ ] Response Spectrum [ ]Tinn-History ,

i

3. htdel Type: [ ] 3D [ ] 2D [ ]1D g [ ] Finite Elenent[ JBeam [ ] Closed Form Solution >

l :

i 4. [ ] Conputer Codes: j

.J Frequency Pange and No. of nodes considered:

) [ ] Hand Calculations 1 l l 5. Danping: _ , _ _ _ -

I

) 6. Support Considerations in the model.

( , 7. Critical Stn2ctural Elments:

Governing Seismic 'Ibtal Stress l' A. Identification location Resconse Canbination Stress Stress Allowabley l

l b

l i

1 1 ,

I

'l 6 l

4 Effect Upon FunctionalI

! B. F'ax. Deflection Iocation Operability -!

l l \

i ff I

I i !

i :

I I

i .

,J

)

(. '

4 4 ,,

i Reference; CQDFile !b. 000261 SARGENT " LUNDY 'O

( Iq g 'auummensan a-----,._-.m___,__.._,__, 4;y. _g

r,, I i

O

{} INSTRUMENT IDENTIFICATION & (~%( ,LIFICATION REQUIREMENTS ? V ID ' No~. s '

specimen vibrated at resonant frequencies (31 Hz) Name: Indicator & Trip' Unit in horizontal axes at 2 g's for 2 minutes.

3 ,

Qualitication 'g' levels Malfunction limit test up to 15 g's. Manufacturer: CE

,jh =4,2g hj=4.2g V=5.4g Model No.: None Instrument Required 'g' levels Equipaent Numbers Location Class. Remarks hg h2 V i

D18-K609A/D Region CR-1 1 02 4 .46 A El.768' on Panels H13-P635, 36 D18-K611A/B Region CR-1 1.02 .4 .46 A El.768' on Panels H13-P635 D18-K615A/D Region CR-1 El.768' on Panels 1.02 .4 .46 A H13-P635, 36 k

A - Active P - Passive 1E - Class 1E

nutGCh

/52 San hse, California Project Zimmer/La Salle SORT Requalification Prograr. Filef4o.

Owner _ Cincinnati Gas and Electric Comnanv/ Commonwealth Edison Comcany Client Cincinnati Gas and Electric Comeanv/ Commonwealth Edison Connany TABLE 2 l

, INSTRUFOT DATA INSTRUMENT-NAME: Indicator and Trip Unit MODEL NO.: 129B2802

SERIAL OR ID. NO.:

MANUFACTURER: General Electric SPECIAL FEATURES IF ANY: hone -

Receive output of sensor and converter (o)

~,

l FUNCTION: and provide containment ventilation isolation and SGTS initiation. .

DIMENSIONS: 6"H X 2 3/4"W X 12 1/2"D WEIGHT: 4 lbs.

' REQUIRED RANGE: 0.01 mR/hr to 100 mR/hr .

REQUIRED ACCURACY: 9.5%

- MONITORING REQUIRE!'ENTS: Output trip -

MOUNTING DETAILSt See Figure 2 CHATTER TIME: 20 milliseconds To be completed by test laboratory Input monitoring at sensor and converter ex

Revision C 1 l .

PaSe Picpared By/Date NR//d#f/

cf l Checked ey/Date p b f />> /t'/ i [ ;C

nl.nech -

/50 San Jose Cahforn.ia Project 'irrO r 'L' CO SnR* Requ'li*~4c'*ien Prncen" File No.

Owner F4"c4n"'t-i R'" N"d "'00*"ir F " ~ " ' " " ' F n ~ ~ ^ " ' " ' ' h " A i " n r F r * " ' n

/ ' ': ./Chent Cincinnati Gas and Electric Cc ran" Cerron',real"h M iron Cernany Nus-INDICATOR ANC TRIP UNIT 129B2802 j.Yh.

^

y f; s- f. SHELF c___.

135B9759 e o

/

e

/

l c c A

I 3_ ANGLE

, ,, (TYP. & PLACES)

/~ _

PANEL -

175A9027 MOUNTING FOR GENERAL ELECTRIC INDICATOR AND TRIP UNIT 129B2802 FIGURE 1 4 .

Revision j L j Pa*a~

Prepared By/Date SEM_ /yt/ ]

Checked Ey/Date 15.9 f637// j l .L __ ___

E Illi.dUl i San Jose, California

/f//

Propct Zimmc r/La Salle SORT Recuali #ication n-on-nr File No.

Owner Cincinnati Gas and Electric Comnanv/Corronwnalth Edison cornanv Cincinnati Gas and Electric Comcany/ Corr.onwealth Edison Comoany Chent INDICATOR AND TRIP -

UNIT 129B2802 Til j? P FT

A

=' ,j CD o ,

/

l '

1 l

I

. <=

_j i /~' - l ACCELEROMETER LOCATION FOR GENERAL ELECTRIC INDICATOR AND TRIP UNIT 129B2002 i ,

FIGURE 3 Revision 6 l l '

page Prepared By/Date e}M;// ///

of Checked Ev/Date ISS //4 /3!!

- - U e1 15$

O DIV II RADIATION MONITORING SYSTEM INDICATOR TRIP UNIT D18-K611 ENVIRONMENTAL QUALIFICATION TABLE D18-4

1. DESCRIPTION The indicator trip unit is in a module designed for counting in an equipment rack that holds as nany as six similar units. Electronic components are mounted on two vertical printed circuit boards. Connections to power supply and sensor convertor unit are made via connections mounted on the rear panel of the codule.

2. SAFETY FUNCTION The building ventilation indicator / trip unit monitors the gross gamma radiation levels on the refueling roo=, drywell and torus, and standby gas treatment ventilation exhaust. Alarm and control actions signal excessive radiation r levels and autenatically isolate the reactor building ventilation system.

3 SAFETY DESIGN PARAMETERS A. Range: 0.01 mr/hr to 100 cr/hr (4 decades) '

B. Relay Response Time: 10 milliseconds to an input step of 100 microatps.

)-

C. Poweri +24 Vde, 26mA

-24 Vde , 21=A

+30 Vdc unregulated, 80mA

4. FSAR ENVIRONMENTAL CONDITIONS

! The equip:cnt is located in the control room panel H13-P636. The FSAR 4

environmental conditions are tabulated below:

Duration Torperature Pressure Humidity Radiation 4 N/A 400F Range 0.1 in. 20% Operating 0.0005 N/A 60-900F to 0.25 in, water 40-50% Integrated 1.75x10 2 N/A 1200F gauge static 60% (1) pressure 1

5. ENVIRONFZNTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

! Duration Temperature Pressure Humidity Radiation i

N/A 400F Range 0.1 in. 20% Operating 0.0005 N/A 60 900F- To 0.25 in, water 40-50% Integrated 1.75x10 2 j N/A 1200F gauge static 60%(1) pressure (1) During HVAC equipment failure conditions, relative humidity cay approach 100% for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 120cf would not occur concurrently.

6. QUALIFICATION METHOD Not Available j 7. RESULTS i

i l

I6]

( ). DIV II RADIATION MONITORING SYSTEM INDICATOR TRIP UNIT D18-K615 I

ENVIRONMENTAL QUALIFICATION TABLE D18-4

1. DESCRIPTION The indicator trip unit is in a module designed for mounting in an cquipment

} rack that holds as many as six similar units. Electronic components are mounted on tuo vertical printed circuit boards. Connections to power. supply and sensor convertor unit are made via connections mounted on the rear

. panel of the codule.

2. SAFETY FUNCTION The building centilatien indicator / trip unit monitors the gross gamma radiation levels on the refueling room, drywell and torus, and standby gas treatment.

ventilation exhaust. Alarm and control actions signal excessive radiation ,

levels and autecatically isolate the reactor bcilding ventilation system.

1

3. SAFETY DESIGN PARAIETERS 1

A. Range: 0.01 mr/hr to 100 mr/hr (4 decades)

B. Relay Response Time: 10 milliseconds to an input step of 100 microamps.

C. Power: +24 Vde, 26mA

~

-24 Vdo, 21mA

() +30 Vdc unregulated, 80mA

4. FSAR ENVIRONMENTAL CONDITIONS i: The equipment is located in the control room panel H13-P636. The FSAR ;

environmental conditions are tabulated below:

Deration Temperature Pressure Humidity Radiation N/A 400F Rango 0.1 in. 20% Operating 0.0005 N/A 60-900F to 0.25 in, water 40-50% Integrated 1.75x102 N/A 1200F gauge static 60% (1) -

pressure

5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Temperature Pressure Humidity Radiation N/A 400F Range 0.1 in. 20% Operating 0.0005

N/A 60 900F To 0.25 in, water 40-50% Integrated 1.75x102 N/A 1200F j gauge static 60%(1) pressure (13 During HVAC equipment failure conditions, relative humidity may approach 100% for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months , but 1200F would not occur concurrently.

6. QUALIFICATION METHOD Not Available

7. RESULTS t

> - . - .,~ ..,,._.__-,,,n,_ _.,,..,n_..,=,, . , - - - , _ , , . . . - - , . , , . , , . , - - , , . ,,.__.,--en, . , . . , - - . . , . . . . . , , - -

NEN TEST PR O C li.D!)RE' jff

. -..=.= .-. . -

accordance with paragraphs 5.3.1 and 5.3.3. Failure is indicated if the test specimen does not meet the

()T

(_ operational requirements after vibration in accor-dance with paragraph 4.2. More than 20 milliseconds chatter shall be considered a failure. Any indica-tion of chatter shall be brought to the attention of NUTECH for further analysis. All failures shall be noted in the test report.

5.0 TEST REQUIREMENTS .

5.1 Exploratory Testing Exploratory testing shall be performed to determine the test specimens' resonant frequencies, if any, within a specified frequency range. A recommended procedure for this testing is provided below. Fast Fourier Transform (FFT) or other tescing methods will be acceptable provided they yield the same information about the dynat 'c characteristics of the test specimens.

5.1.1 Sine Sweep Recommended Test Parameters Test Method : Low Level Sine Sweep Input Motion: Single axis 73 Number of Tests: 3 with one in each

() Orthogonal Axis Frequency Range: 1 to 100 Hz Sweep Rate : Less than 2 Octaves per minute Input g Level: 0.1 g Peak 5.1.2 Exploratory Testing Results The acceleration response in g's and transfer function for each of the accelerometer location shall be plotted as a function of frequency.

5.2 Fatigue Testing (Sensor and Converter Onlv)

Fatigue testing shall be performed in order to account for any possible long term effects the S2V

. and LOCA event may have upor the test specimen.

This test phase shall be conducted in two parts, first, SRV fatigue testing and second SRV + LOCA fatigue testing. The RRS to be used are those generated during previous vibration testing.

(~/b

\_

MK2-02-038 10

/5/

5.2.1 SRV Fatigue Testing

('

, Test Method: Random motion Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelope RRS l

Number of Tests: 1 in each test specimen

, orientation

/ -Test Specimen Orientations: 2, orientations (1) Front to back/ vertical (2) Side to side /vertica1 ,

Frequency Range: 1 to 200 Hz

, Duration of Individual Time History: Less than 20 see Total Test Duration: 400 sec each orientation

'RRS Damping: 2%

Required Response Spectra: Figures 10 and 11 5.2.2 SRV Fatigue Testing Results TRS shall be plotted for table accelerometer locations at a damping value of 2% at 1/6

. octave intervals. For comparison the table TRS and RRS shall be plotted on the same sheet. Power Spectral Density (PSD) plots O' shall be developed from the table accelerometer time histories for each test specimen orientation.

All accelerometer signals shall be recorded on an'alog magnetic tape.

5.2.3 SRV + LOCA Fatigu'e Testing ,

Test Method: Random motion Input Motion: Biaxial Excitation: 2 independent random signals l Level: Table TRS to envelope RRS i

Number of Tests: 1 in each test specimen l orientation l Test Specimen Orientations: 2 orientations j (1) Front to back/ vertical l (2) Side to side / vertical l

l Frequency Range: 1 to 200 Hz l Poration of Individual Time History: Less i than 20 sec l Total Test Duration: 200 sec each orientation MK2-02-038 11 .

l l

~

/6f RRS Damping : 2% +

Response Spectra: Figures 12 and 13 O/

5.2.4 SRV + LOCA Fatigue Testing Results TRS shall be plotted for table accelerometer locations at a damping value of 2% at 1/6 octave intervals. For comparison, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed from the table accelerometer time histories for each test specimen orientation. All accelerometer signals shall be recorded on analog magnetic tape.

5.3 Proof Testing

~

The adequacy of the test specimens for upset /OBE and emergency /DBE plant conditions will be demonstrated by the proof testing phase. This phase will be divided into two parts, testing for upset /OBE plant condition and testing for emergency /DBE plant condition, and shall consider the maximum combined dynamic loads the test specimens may experience j '

, under each condition. The RRS to be used are those generated during previous' vibration testing and data (x reduction. The indicator and trip unit will be

(_) tested to OBE and DBE as a control room item. The 4

sensor and converte. will be tested to earthquake plus hydrodynamic loads in upset and emergency as a i local item.

5.3.1 Upset /OBE Condition Testing Test Method : Random Motion ~

Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelop RRS Test Specimen Operation: As specified below Tes t . Specimen Orientations: 2 orientations (1) Front to back/ vertical (2) Side to side / vertical Number of Tests: 10, 5 in each test specimen orientation R -

V MK2-02-038 12 ,

/60 5.3.1.1 Sensor and converter-Upset

) (1) Pre-Vibration a) Place the power supply PONER SUPPLY OFF-ON switch to the OFF position.

b) Connect the sensor and converter, power supply, indicator and trip unit and monitoring circuit in accordance with Figure 8.

c) Place the TRIP TEST-ZERO-OPERATE switch on the indicator and trip unit to the OPERATE position.

d) Place switch Si to the CLOSED position, e') Place the power supply PONER SUPPLY OFF-ON switch to the ON position. .

f) Verify that the reading on N the indicator and trip unit meter is approx-imately 20 percent of the first decade, g) Depress the RESET push-

. button on the indicator and trip unit and verify that the LON and HIGH indicating lights extinguish.

h) Verify that there is voltage across Resistor R1

. (Relay K2 contacts 6 and 10 closed) and no voltage across Resistor R2 (Relay K1 contacts 3 and 11 opened).

(2) During Vibratio,n Maintain the above conditions i throughout the 5 tests in each

, test specimen orientation.

MK2-02-038 13

161 (3) Post Vibration

(_s}

a) Place the power supply, POWER SUPPLY OFF-ON switch to the OFF position.

b) Dicconnect the monitoring

/ circuit connected in step (1) b).

5.3.1.2 Indicator and Trip Unit - OBE (Normal Condition)

(1) Pre-Vibration a) Place the power supply, POWER SUPPLY OFF-ON switch to the OFF position. ,

- b) Remove the sensor and converter from its case.

c) Connect the sensor and

. converter, power supply, indicator and trip unit

('] and test equipment in -

(_/ accordance with Figure 9.

d) Connect indicator and trip unit receptacle J1 pins 8 '

and 19 to individual monitoring circuits in accordance with Figure

9. .

e) Place the TRIP TEST-ZERO-

, OPERATE switch on the indicator and trip unit to

, the OPERATE position.

f) Place switch Sl to the OPEN position.

g) Place the power supply POWER SUPPLY OFF-ON switch, to the ON position.

h) Turn on the electronic counter and pulse

() generator and adjust the pulse generator output for MK2-02-038 14

- - . - , , = - - - - -

7, , - , - - , , ,- - - - , , , . - , _ - - , - - , _

y- r -,--

16 8 negative pulses of 15 volts peak amplitude.

Os i) Set the pulse generator

, pulse duration so that the pulse length provides a 50 percent duty cycle.

j) Adjust the pulse generator

, output frequency control for a reading of approxi-mately 20 percent of the first decade on the indicator and trip unit meter.

~

k) Depress the RESET push-button on the indicator and trip. unit and verify that the LOW and HIGH indicating lights extinguish.

1) Verify that there is

, , voltage across Resistor R1 (Relay K2 contacts 6 and s

10 closed) and no voltage Os across Resistor R2 (Relay K1 contacts 3 and 11 opened). .

(2) During Vibr'ation Maintain the above conditions for 1 vibration test in each test specimen orientation.

5.3.1.3 Indicator and Trip Unit-OBE (Downscale Trip) l (1) Pre-Vibration .

a) If testing has been stopped repeat steps 5.3.1.2 (1) a)_through 1) as required to achieve normal condition. .

O I

MK2-02-038 15 i

+

/63 (2) During Vibration

() . , a) Decrease the pulse gener-ator output frequency to the recorded value (-t 10%)

in paragraph 4.2.2.3 step 13 and verify that there is voltage across Resistor

-:R2 (Relay K1 contacts 3

, and 11 closed) and the LOW indicating light illuminates.-

b) Perform this test once in each test specimen orientation. --

5.3.1.4 Indicator and Trip Unit-OBE (Downscale Steadv State Condition)

(1) Pre-Vibration -

a) If testing has been stopped repeat steps 5.3.1.2 (1) a) through 1) as required to achieve normal condition.

O' .

b) Maintain the conditions in step 5.3.1.3(2) a) or perform if required.

t (2) During Vibration 1

Maintain the above conditions for 1 vibration test in each test specimen orientation.

5.3.1.5 Indicator and Trip Unit-0BE (Upscale Trip)

(1) Pre-Vibration a) Repeat steps 5.3.1.2 (1)

a) through 1) as required to achieve normal

, condition (2) During Vibration es a) Increase the pulse gener-() ator output frequency to MK2-02-038 16

16 4

- the recorded value (+ 10%)

(/~',)e 'in paragraph 4.2.2.3 ' step 13 and verify that there j ~

is no voltage across

[ ./ Resistor R1 (Relay K2 contacts 6 and 10 opened)

I and the HIGH indicating

/ light illuminates.

b) Perform this test once in each test specimen orientation.

5.3.1.6 Indicator and Trip Unit-OBE (Upscale Steadv State Condition)

(1) Pre-Vibration a) If testing has been stopped repeat steps 5.3.1.2 (1) a) through 1)

. as required to achieve normal condition.

b) Maintain the conditions in step 5.3.1.5(2) a) or

() perform if required.

(2) During Vibration Maintain the above conditions for 1 vibration test in each

! test specimen orientation.

Monitoring Requirements : Indicator and trip' unit output voltage for the sensor and converter test and indicator and trip unit contact position, chatter detection and output voltage for the indicator and trip unit test.

Frequency Range: 1-200 Hz Test Duration: 30 sec per test RRS Damping : 2%

Required Response Spectra : Figures 14 and 15 -

(OBE plus SRV plus chugging or

! LOCA) for the sensor and converter and Figures 16 and 17 (OBE) for the indicator and trip unit.

O MK2-02-038 17

- a ,we s- ,- -- - e >m-w,,- , - a.-. , ,--.---mr-- a - ., -..- ,-. a v ,

e I6C 5.3.2 Upset /OBE Condition Testing Results t h TRS for the indicator and trip unit shall be

[Y s plotted for table accelerometer locations at a damping value of 2% (2 1/2% is acceptable) at'l/6 octave intervals. The TRS for the sensor and converter shall be plotted at a damping value of 1% at 1/6 octave intervals. For comparisen, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed for the first test in each orientation. All accelerometer signals shall be recorded on analog magnetic tape.

5.3.3 Emergency /DEE Condition Testing Test Method: Rendom motion Input Motion: Biaxial Exci' tion: 2 independent random signals Level. Table TRS to envelope RRS Test Specimen Operation: As Specified below Test Specimen Orientations: 2 orientations (1) Front to back/ vertical (2) Side to side / vertical Number of Tests: 1 in each test specimen

( .

orientation ,

5.3.3.1 Sensor and Converter Perform test in accordance with paragraph 5.3.1.1.

5.3.3.2 Indicator and Trip Unit .

Perform test in accordance with paragraph 5.3.1.5.

Monitoring Requirements: Indicator and trip unit output voltage for the sensor and converter test and indicator and trip unit contact position and chatter detection and output voltage for the indicator and trip

~

unit test .

Frequency Range: 1 to 200 Hz Test Duration: 30 sec. per test RRS Damping: 2%

Required Response Spectra: Figures 18 and 19 (DBE plus SRV plus chugging or

()

7 LOCA)'for the sensor and converter MK2-02-033 18 ,

IGf ar.d Figures 20 and 21 (DBE) for the

indicator and trip unit

("

s Operational Test: Checkout Test Specimen after emergency condition tests in accordance with paragraph 4.2.2.1 5.3.4 Emergency /DBE Condition Testing Results TRS shall be plotted for table accelerometer -

locations at a damping value of 2% (2 1/2% is acceptable) at 1/6 octave intervals. For comparison, the Table TRS and RRS shall be plotted on the same sheet. PSD plots shall -

be developed from the table accelerometer time histories for each test specimens orientation and voltage relay operation. All accelerometer signals shall be recorded on analog magnetic tape. Results of operational test checkout after excitation shall be r(gorted and any significant deviation from the baseline shall be noted in the final report.

6.0 WITNESSING OF TE_STS 6.1 All tests shall b~e subject to observation by NUTECH or their authorized representatives.

6.2 All tests shall also be subject to observation by Cincinnati Gas and Electric and Commonwealth Edison '

Companies or their authorized representatives.

7.0 TEST REPORT REQUIREMENTS The test laboratory shall supply ten certified copies of a test report which satisfies the requirements of IEEE 344 -

1975. This report wil describe the equipment, calibration, and test procedures, including photographs of the test set up, and provide all results and conclusions from the test. Operational checkout and inspections shall be described and all results summarized and any deficiencies and/or cepairs noted. Critical data to be included in this report are as follows :

'71

. Inspection and operational test results reports, verifying adjustments and recording values, also -

noting any significant deficiencies and repairs to device. A description of test equipment and calibration information shall be included. -

7.2 Test Specimens resonance search data MK2-02-038 19 '

,~<e .--- --,-,---,,e-. - - . , - - - \- ae n,--- , - - - , - - - - - . --n- - -~ .-,y , -

(67 '

7.3 The test response spectra (TRS) plots obtained in 5.2.2, 5.2.4, 5.3.2 and 5.3.4. These TRS are to be computed for all accelerations recorded. For each O- ,

of the two orientations for the test specimen, the TRS shall be computed for both horizontal and vertical table motions to verify that they envelop the corresponding RRS.

I 7.4 PSD plots obtained in 5.2.2, 5.2.4, 5.3.2 and 5.3.4.

. 7.5 A record'o'f voltage and frequency readings, contact position, test specimen operatinn, and chatter shall

, be maintained in the test log.

7.6 A record of the number of test runs including level and duration shall be maintained in the test log.

7.7 A copy of the tdst log.

7.8 Completed Instrument Data Forms (a partially completed form have been provided as Tables 1 and 2 of this specification).

8.0 REFERENCES

8.1 IEEE 344- 1975: Recommended Practices for Seismic

( Qualification of Class lE Equipment for Nuclear Power Generating Stations.

8.2 GEK32374D G.E. Operation and Maintenance Instructions ( Area Radiation Monitor Sensor and Converter) 8.3 GEK27828G, G.E. Operation and Maintenance Instructions (Area Radiation Monitor Indicator and ,

Trip Unit) s O

1 0

MK2-02-038 20

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O vner Cincinnati Gas and Electric Co. /Coronwealth Edison Co.

f) Client Cincinnati Gar and Electric Co./Corronwealth Ediron Co.

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.l a w ,< A C 75 Che1 16 Che.ked By /Date of D% / 7 ..s f i !du. 9 0r// / I . -,

_n

1 70 QUALIFICATION OF CCW TM C 70R #/N5C3027 JUSTIFICATION FOR INTERIM OPERATION

(' ^')

v The test report submitted by CE meets the specified g levels.

Acceleration level comparisons are shown below.

Required g level from Panel Analysis h1 = .C[f , h2 "l'I$ V " * // d $

g icvel from Test Report h1 = /,$g h V " - 5p 2 " />$}

Therefore the equipment is qualified as for as test g levels are considered.

However we opted to perform new tests for the following reasons:

a) Documentation of test log was insufficient.

- b) Funcional testing of Instruments not adequately explained, c) Single axis single frequenc'y testing was done.

The new tests will be done to the test requirements as attached as soon as the test specimen is procured. .

For the above reasons we strongly feel that the device is qualified for the interim operation.

,, r.

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/7/ :

-. i t i .

c LA SALLE NUCLEAR STATIONS' UNIT 1& 2

$fs 4

! NSSS EQUIPfd5NT QUALIFICATION

SUMMARY

[

i

! EQUIPMENT NAME : contactor # 145C3029 EQUIPMENT NO: C71A-K14A/H I l

l LOCATION: On Panel H13-P609 l

i, EQUIPMENT CLASSIF1 CAT 10N: O ACTIVE C PASSIVE i QUALIFICATION METHOD: Seismic Tests (see page 2) i f QUALIFICATION DOCUMENT

REFERENCES:

1. CE Document # 225A6966 (Scismic Test Summary) 1 l 2 . GE # 225A6279 (Seismic Test Results) i f 3. GE # 225A5766 dated 1-5-78 Rev. 7 4 . DVI4563209 5.

6.

!., 7. f

[ 8.

9.

l 1 j

P j h, LOAD COMBINATIONS CONSIDERED IN QUALIF~ CATION: _

Normal Operating Loads + OBE + V

l. _SRVASY-TO + ALL-TO ENVELOP f 2. Normal Operating Loads + SSE + COLEVY-2+ ASY-TQ + SRVALL-TQ, ENVELOP:

3. Norma 1 Operating Loads + SSE+ Chugging + -SRVASY-TQ + SRVALL-T ENVELOP; c

l .

4. Normal Operating Loads + SSE + AP L

5. Normal Operating Loads + SSE + COLEVY-1 l QUALIFICATION:

i /_ .

PREPARED BY: Date ,

Date SARGEijT& LUijDY IREVICUCDBY:

AFlRO\ D W:

L , _ '. _ __':. _ _ _ ._ _ Date 7Y. ((d" ,#

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's

( ,)

i QUALIFICATION SUSD!ARY l i

.I I

EX?< TING TEST REPORT I

a) Resonance Scarch Test - in all the three axes. i l

Frequency range 5-33 llz Input = .02"DA l Duration 7 minutes sweep l

Resonant frequency h 2= 2711z I

, l hi& V = None l

l 1 b) 2 minute dwell test in b2 direction at 27 liz.

(, l ,l g 1cvel = 2 'g' i' c) Endurance Sweep Test h t = h 2 = 1.5 g i

I V = .5g 1

I d) Malfunction Test up to 12 g's at 27 IIz in h direction, 2

J l

t .

I l

l l l !

l l

l I

I l.

i Ref: CQD File No. CQD 000272 l SARGEijT h LUDDY q' 3_.

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Otalification Sunmry of Faaigrcnt /7J {f 1 G LASALLE COUNTY 1&2

[Q 7, py g .

CECO pwg

1. Utility:

NSSS; CE g X 2.

3. A-E: .

I l Contactor # 145C3209

< II. Conponent tune

1. bbdel Nunber CR105/102 Quantity: 8 :

2. Vendor CE/GPCD

3. If the ccrtponent is a cabinet or panel, nane and itodel Ib. of .

the devices included: l I

I

4. Physical D?scription a. App arance Instrumentation I

b. Dinensions 6.62" x 4.94" x 5.38" 7 lbs. (approx.)

c. Weight Auxiliary Bldg.

5. Incation: Building:

i i l Elevation; on Panel H13-P609 -

1 II

6. Field Mounting Conditions [X] Bolt (No. 3 , Size 3/8")

[ ] Weld (length ) q l

Mounted on Panels j l S I

j 7. Natural Frequencies in Each Direction: .f h2: y: None from 5-33 .

From old test bl . None from 5-33 27Hz

.I

8. a. Functional

Description:

used as scram trip actuator '

relay in the Reactor Protection System

b. Is the equipr:ent required for[ hbt Standby [ ] Cold Shutdown

[ } Both Other Safety Function

9. Pertinent Reference Design Specifications: [

P '

m Fcference:CQD File No. CQD 000272 SARGENTk LUDDY j

m omenmaup j

J

, __ _.. . __ i y. . A us l //// ' o l

.s

' Ill. Is Equip:ent Available for Inspection in the Plant: k] Yes []lb f

. 4 c-nu: ,

t I

( l X j IV. Equiptent Oualification Method: 'Ibst:

Analysis:

Ottibination of hst and Analysis:

! & 225A6279 ;

J a

Test and/or Analysis by Philco Ford GE Document No 225A6966 (name of Capany or Iaboratory & Report tb.)

i V. Vibration Input: ,

1. Ioads considercxi 1.[X ] Seismic only 2.[ ] Hydrodynamic only 3.[] D< plosive only 4.[ ] Other (Specify) 5.[ ] Ccurbination of

2. Recp. tired Response Spectra (attach the graphs):

< NA o

3. Requirod Acceleration in Each Direction:

O I I h1 = .8 g h2 = 1.1 g V= .46 g '

.i VI. If Qualification by Test, then conlete: r i 1. IX] Single Frequency [ ] bblti-Frequency l

l 2. [X] Single Axis [ ] Multi-Axis

3. Frequency Rarep: 5-33 Hz -

l

, 4. TRS enveloping RRS using Multi-Frequency 'Ibst[ ] Yes (Attach TRS graphr' NA

5. g-level 'Ibst at hl = 1.5g h2 = 1.5g V= 0.5g

6. laborator,/ bbunting:

1. [XIBolt (rb. 3x20 Size t" ) [ ] Weld (Iength )[ ]

7. Functional operability verified: [X]Yes [ ] tb [ ] Not Applicable

8. Other tests perforwxi (such as fragility test, including results) g N Resonance frequency test from 5-33 Hz. Resonant frequencyof 27 Hz

/ in Hz direction. Malfunction limit test ronchna en n maximum of 12 }j g's at 33 Hz.

Pcference: CQD File Ib. CQD 000272 -4 SilRGERT t LUfl0Y

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II VII. If Qualification bv Analysis or by the Conbination of Test and Analysis,tho .

Conplete: N.A.

1. Description of Test including Pesults:

1

2. Methcd of Analysis:

i

[ ] Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic .

[ ] Response Spectrum ( } Time-Ilistory

3. Model Type: [ ] 3D [ ] 2D [ ]1D

[ ] Finite Elenent[ ]Deam [ ] Closed Form Solution-;

4. [ ] Conputer Codes: 1 Frequency Pange and tb. of nodes considered:

1

[ ] Iland Calculations

5. Danping:._ ,_

i,

)

6. Support Consid3 rations in the nodel: 1 3 i (V 7. Critical Stn2ctural Elenents: Governing Seismic 'Ibtal Stress A. Identification Iocation Resoonse Canbination Stress Stress Allownblef i l l

i i

Effect Upon Functional.

B. Max. Deflection location Operability i i

l Cq /

a Rnference; CQD File tb. 000272 SARGENT $ LUNDY !

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///

RUGCh San Jose, California Project Wm. II . Zirmer/La Salle County Nuclear Power Stations f 'e No.

[ } Owner Cincinnati Gas and Electric Company /Cormonwealth Edicon Co.

'~

Chent Cincinnati Gas and Electric Comnany/ Commonwealth Edison Co.

- =

0 E I , 3- -20 BOLTS AND NUTS UNIS RUT "

1 --

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) ENCLOSURE

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(_. l LOCAT.EJNS (SilOWN WITl!

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@ g REMOVED)

H $ $

n n CONTACTOR UN: STRUT P-2.000-O# 2-r4007 MOUor1NG NUTS O '

AND 5/16-18 BOLTS TEST SPECIMEN MOUNTING PLATE

( ~'s (7 GAUGE SliEET STEEL) t !

s MOUNTING TECIINIQUE FOR TEST SPECIMEN m

FIGURE 1 POVt5iCn O l Pre;'ared By/Date ,

f a M/d<C,e*f of 15 r nor 6., n ,, , n ... < wt i i

/7/

i CONTACTOR C711-K---

2 ENVIRONMENTAL QUALIFICATION TABLE C71-2 T

1. DESCRIPTION The equipment is a type CR105/CR205 contactor as manufactured by G.E.

2. SAFETY FUNCTION Relay de-energizatien required to trip the Reactor Protection System i.e.,

) initiate rapid insertion of all centrol rods simultaneously (SCRAM).

3 SAFETY DESIGN PARAMETERS The contactor must de-energize as required within a minimum or 20 milliseconds with a 120 volt AC,1250 VA scaling inductive load.

Worst Case: 1200F - 90 % R/H '

Contact Rating Continuous A.C.

Current Ratings NEMA Size (Amperes)

i Enclosed Open i 00 9 to i 0 18 20 a 1 27 30 1 2 45 50 iO l

3 4 135 eo 'oo 150 300 5 27 0 Maximum Contact Voltase: 600 Volts l 4. FSAR ENVIRONMENTAL CONDITIONS The equipacnt is located inside the Control Room. The FSAR environment j conditions are tabulated below.

i

Duration Temperatur_q Prensure Humidity Radiation

! Min 400F Bange 105 Operating 0.0005 Normal 60-900F 0.10 in. to 50% Integrated (40 yrs)

Max. 1200F 1.0 in, water 60% 1.75x10 2 gauge static prcssure

5. ENVIR09 ENTAL QUALIFICATION ENVELOPE (Spec. 22A3008 Rev. 5) ,-

-Duration Terperature Pressure Humidity Radiation Min 400F- Range 10% Operating 0.0005 Normal 60-900F 0.10 in, to 50% Integrated (40 yrs)

Max. 1200F 1.0 in, water 605 1.75x102 gauge static pressure N

--.ma.,w,-rer=- rw.e.,,v w. r m-,,,m .c,-.,ws-. ,..cy_,u -. p e y e rmw. -,,iseie-ym.3_%e-e-, y . ym y.- ,--,wv--r--,,m t i---,w-p - ,r ,,- - - - - - - - ---,--,e . , +>= - --

/7f CONTACTOR C71 A-K--- (Continued)

(N ,,,/; ENVIRONMENTAL QUALIFICATICN TABLE C71-2

6. QUALIFICATION IST!!OD Type Ter.t The devices were placed in the Environ = ental Qaamber and soaked for 16 hours1.851852e-4 days 0.00444 hours 2.645503e-5 weeks 6.088e-6 months at 60 0C nnd 90-95% relative humidity. At the conclusion of the soak period, without change of environmental conditions, cach device was cycled 50 times at rated load. Each cycle consisted of 1 see on and 9 see off except for the selector switch which had 1 sec right,1 sec left, 8 see off.

7. RESULTS All devices passed the 50 cycle test while under specified ambient conditions without (by visual inspection) undue heating or pitting of contacts.

QJ O

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u-

' '~

NEN- -.

TEST PROCED@?E -

11 0

/ 6.0 TEST REQUIREMENTS I(_"')

6.1 Operational Testing q An oper'ational test shall establish a baseline function in accordance with paragraph 5.2.2. During 4

exploratory testing the test specimen shall be energized for the duration of the test. During proof testing the test specimen shall be opera-tionalIy cycled, from energized to de-energized.

The relay shall be maintained in each state for

. fifteen seconds to indicate contact chatter.

Subsequent operational tests shall follow each phase o/ vibrational testing in accordance with paragraph j 5.2.2. Relay coil voltage shall be 105V during all phases of testing. 105V is the low. nominal voltage for all Zimmer and LaSalle Control Room 120V power -(?

busses..

V-

~

6.2 Exploratory Testing After the baseline operational checkout, exploratory testing shall be performed to determine the test specimen's resonant frequencies over the frequency range of 1-100 Hz. A racommended procedure for this testing is provided be low. Other testing methods

% will be acceptable provided they yield the same in"ormation about the dynamic' characteristics of the te + specimen.

6.2.1 Sine Sweep Recommended. Test Parameters Test Method: Low Level Cine Sweep Input Motion: Single Axis -

Number of Tests: 3, 1 in each Orthog-onal Axis Frequency Range: 1 to 100 Hz Sweep Rate: less than 1 octavo per minute Input g Level: 0.25 g Peak Test Specimen State: Energized Test Specimen Monitoring: In accordance with f~}

\_<

Paragraph 5.2.3 MK2-02-039 5

///

Operational Test: In accordance with

() Paragraph 5.2.2 6.2.2 Results The acceleration response in g's from each accelerometer location shall be plotted as a function of frequency. Any detected chatter shall be noted in the final report.

6.3 Proof Testing .

The adequacy of the test specimen for Op; rating Basis Earthquake and Design Easis Earthquake will be demonstrated by the proof testing phase. This phase shall be divided into two parts, 1) testing for OBE plant condition, and 2) testing for DEE plant condi-tion. The tests shall consider the meximum scismic loads the test specimen may experience under each condition. The defined input response spectra to be used are included in Figures 2 through 5.

6.3.1 OBE Testing Test Method: Random Motion

() Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelope RRS Test Specimen State: Energized for first fifteen seconds, then de-energized for the remainder of ' te test Test Specimen Orientation: 2 orier.tations (1) Front to back/ vertical

. (2) Side to side / vertical .

Number of Tests: 10 with 5 in each orientation Test Specimen Monitoring: In accordance with O paragrcph 5.2.3 MK2-0?-039 6

MS

() Frequency Range: 1-100 Hz

,T.est Duration: 30 sec per test I

Damping:

2% ,

Required Responsc

, Spectra: Figures 2 and 3 Operational Tests: .After each group of OBE tests in each orienta-tion, in accordance with paragraph 5.2.2.

6.3.2 OBE Testing Results TRS shall be plotted for each accelerometer

, location at a damping value of 2% at 1/6 octave intervals (2.5% damping is accept-able). For comparison, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed for the last test in cach orientation. The test laboratory shall provide an' analog tape of time history response for each accelerometer recorded on

(. standard 14 channel IRIG tape with a voice channel. Response shall be unfiltered from 1 to 200 Hz. Times of operation and chatter shall be noted. Results of the operational testr shall be documented and any deviation from baseline shall be noted in the final report.

6.3.3 DBE Testing

Test Method: Random motion Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelope RRS ..

Test Specimen State: Energized for first fifteen seconds, then de-energized for the remainder of the test O

~

MK2-02-039 7 i

i

4 ll$

1 /~T Test Specimen

(-) Orientation: 2 orientations (1) Front to back/ vertical

~

. ~, -

(2) Side to

'E side / vertical' Number of Tests: 2 with 1 in each

. orientation Test Specimen -

Monitoring: In accordance with paragraph 5.2.3 Frequency Range: 1 to 100 Hz Test Duration: 30 sec. per test Damping: 2%

Required Response Spectra: Figures 4 and'5.

. Operational Tests: After each DBE test in accordance with para-() 6.3.4 DBE Testing Results graph 5.2.2.

TRS shall be plotted for each accelerometer location at a damping value of 2% at 1/6 octave intervals (2.5% damping is accept-able). For comparison, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed from the table

. accelerometer time histories for each test specimen orientation. The tes~t laboratory shall provide an analog tape of time history

, response for each accelerometer recorded on standard 14 channel IRIG tape with a voice channel. Response shall be unfil..ered from 1 to 200 Hz. Times of operation and chatter

~

shall be noted on these plots. Results of the operational tests shall be documented and any deviation from baseline shall be --i i

noted in the final report.

7.0 WITNESSING OF TESTS 7.1 All tests shall be subject to observation by NUTECH

() or their authorized representative.

MK2-02-039 8

u _. - . m -- - . _ _.m. -

I10

{~ , 7.2 All tests shall be subject to observation by

'- Cincinnati Gas and Electric Company, Commonwealth

}

Edison Company, or their authorized representatives.

l .

8 . 0, TEST REPORT REQUIREMENTS

/ The test laboratory shall supply ten certified copies of a test report which satisfies the requirements of IEEE 344-1975. This report will describe the equipment, calibra-tion, and test procedures, including photographs of the test set up, and provide all results and conclusions from the test.

Operational tests and inspections shall be described and all results summarized and any deficiencies and/or repairs noted. Critical data to be included in this report are as follows:

8.1 Inspection and operational test results, verifying adjustments and recording values, also noting any_

significant deficiencies and repairs to the device. Include a description of test equipment and calibration.

8.2 Test Specimen resonance data ,

8.3 For each of the two orientations for the test specimen and for each test specimen state and operation, the TRS shall be computed for both horizontal and vertical table motions to verify that they envelop the corresponding RRS.

8.4 Time history recordings.from OBE and DBE tests, recorded on standard 14 channel IRIG tape with a -

~

voice channel. Response shall be unfiltered from 1 to 200 Hz. Time histories shall also be plotted and included in the test report.

- 8.5 Power Spectral Density Plots from the selected OBE and DBE tests.

8.6 A record of the number of test runs, including testing level and duration, contact position, test

. specimen operation, and chatter shall be maincained -

for test runs in the test log.

8.7 Any direct records from instrument operational monitoring (i.e. oscillograph recordings).

- --8.8- A copy of the fest log.

O, MK2-02-039 ~~~~'9 ~ ~ ~ - -

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"n Figure 4 w w -

I!orizontal DIlE 11cquired Response Spectrum 5 7) '

nmeen yo Sen Jose, California Project 16. H. Zimer/La Salle County !:uelear Power Stations Fate No.

Owner Cincinnati Gas and Electric Co./Ce r onwealth Edison Co. ..-

Client Cincinnati -Gas and Electric cc./cc r onwealth Edison Co.

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//7

. QUALIFICATION OF MD8 '7M #T 1///4C727 ,

1 JUSTIFICATION FOR INTERIM OPERATION 1 1

f. .' -

i j The test report submitted by GE meets the specified g levels.

?

.I

. Acceleration level comparisons are shown below.

Required g level'from Panel Analysis h 1=(/,2J h2

d'20 V " dI'2p g level from Test Report h 1=[5g h 2 =/'6] V"/'5f i

! Therefore the equipment is qualified as for as test g levels i

L are considered.

However we opted to perform new tests for the following reasons:

2 1

4-a) Documentation of test log was insufficient,

~

b)' Funcional testing of Instruments not adequately explained. ,

! c) Single axis single frequency testing was done.

4

J

The new tests will be done to the test requirements as attached i

as soon as the test specimen is procured. .

For the above reasons we strongly feel that the device is qualified for the interim operation.

e i-3 O

4

.-v+g ,w-i . ew r y- r-,. - , . r,,--..c,--y --,-m --,--.~-,-m, ,,,,-se, w -,ye enrr.-,-3*wr.gw,,,,,re.+,,m._-.c%

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g4 LA SALLE NUCLEAR STATIONS' l.

l I I UNIT 18 2 i

{

! NSSS EQUIPMENT GUALIFICATION

SUMMARY

i EQUIPMENT NAME: Sensor & Converter # 194C927 l

i EQU!PMENT NO: DIS-N009A/D, D18-N015A/D

! RB-2 El. 790' Locally Mounted ;

l' LOCATION: Reactor Building RB-2 El.790' Locally Mounted on Duct f i

EQUIPMENT CLASSIFICATION: O ACTIVE C PASSIVE l

i OUALIFICATION METHOD: Seismic Test ( see page 2) i

! OUALIFICATION DOCUMENT

REFERENCES:

1,GE # 225A6967 dated 11-30-70 Rev.0

2. GE # 225A6607 dated 7-21-70 Rev.0 3.GE # 225A5766 dated 1-05-78 Rev.7 4.

5.

6.

l.

7.

[ 8.

9.

ij 10 .

LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

1. Normal Operating Loads + OBE + SRVASY-TQ + ALL-TQ ENVELOP l 2. Norma 1 Operating Loads + SSE + COLEVY-2+ .SRVAJY-TQ+ .

ALL-TQ ENVELOP-

3. Normal Operating Loads + SSE+ Chugging + SRVASY-TQ+ ALL-TO ENVELOP,

4. Normal Operating Loads + SSE + AP

5. Normal Operating Loads + SSE + COLEVY-1 l

QUALIFICATION:

6 PREPARED BY: Date ,

REVICUCD BY: Date gpygegggy f

- - "*N APPROVED BY:

Date ,._ _ _ _, _ tC Z?gl

-e--am ._ _ . __ _ .mm - -- - --- - - --

i_____ --y 1

Ilf 1

'v' 1

l QUALIFICATION SlDDIARY i

I I

i SEISMIC QUALIFICATION METl!OD: !

e a) Resonance Scarch Test f l

Single axis Freq. range 5-33 112 i

' Duration - 7 minute sweep j' Resonant freq. - none.

(m b) High Level Sweep Test i

Input 'g' = h t = h 2 = V = 1.5g c) Max. endurance 'g' icvel at 33 Hz = 15 g.

l i

i t

l I

Ref: CQD File No. -CQD 000263 Y.,

j SARGEffT bluf!DY d

<g- --,---.--,__ _ __ _

__ ::2g;,j

> . u o . ,.=,o u

c_ , _ _ _ . . _ - - = -->mmew - - .y;.- - ~ . a~. a.===mr;a1 m : a . u.a ,

Otulification Su:mury of Equiprent p/7g [

^

LASALLE COUNTY 1&2 l

/) T. Plant Narre: Type: s

\ /

1. Utility: CECO IVR .

4

2. NSSS; GE IMR X Il S&L 2

3. A-E: it Sensor & Converter # 194C927 II. Couponent Nane

1. bbdel Nu:rber None Quantity: 8 1

~1

2. VcIxior GE l 1

3. If the caponent is a cab 2 net or panel, na:m and nodel No. of !

the devices incitrled:

l

4. Physical Description a. Appearance Instrumentation 10hH x 23j4g x 3 fS"D !

b. Dinensions I

c. Weight

(~\

( ,) 5. Incation: Building: Reactor Building RB-2 Elevation; El.760'

6. Field tbunting Conditions [ ] Ibit (tb. , Size )

9 See att ached sketch yl 1 I ] x 9

7. Natural Frequencies in Each Direction: R 1

v hl: h2: V: 1 Used in connection with l

8. a. Functional

Description:

Indicating Trip Unit (See attached Env. Qual. Table)

I

b. Is the equi Irnnt required' for[ libt Standby [ } Cold [

Shutdown i I JBoth

,t I

Pertinent Ibference Design Specifications: j r 9. '

F n

i

,n '

l

-~

SARGEflT1 LUflDY hj Peference: CQD File ?b. CQD 000263 wam=nout

^ '--~

' M M RdWatLA M T* M ast m g y-wn m y g 7g [-

1 _ . . .

q^- .

e A// l L

Ill. Is Equign2nt Available for Inspection in the Plant: k] Yes [ ] No Il O- ,

i Convents:

F G

i IV. EquipTent Qualification bbth3d: Test: X 9 Analysis:

Orbination of Test and Analysis:

I Test and/or Analysis by GE Report # 225A6607 Rev.0 1 (nane of Cogany or Iideratory & Report Bb.)

i V. Vibration Input:

l. Ioads considered 1.lX] Seismic only 2.[ ] Mwunic only 3.[} Explosive cnly 4.[ ] Other (Specify) 5.[ ] Orbination of

2. Pequired Response Spectra (attach the grapits): NA

3. Pequired tcceleration in Each Direction:

s y , > 1. 2 g r

' \

h1 = > 1.2g h2 = > 1.2g

[

VI. If Qualification by Test, then Ccuplete: -

, 1. [ ] Single Frequency [ ] Pbiti-Frequency t

i 2. [ ] Single Axis [ ] Multi-Axis 5-33 Hz '

3. Frequency Rarc,a:

4. TRS enveloping RRS using Multi-Frequency Test [ ] Yes (Attach TPS graphr

' NA h2 = 1.5 g lsJ tb S. g-level Test at h1 = 1.5g's y= 1.5 g's l

I i ) 6. Laboratory bbunting: (See attached sketch)

l. [ ] Bolt (No. , Size ) [ ] Weld (Icngth )[ ] '

7. Functional operability verified: [ ] Yes [ ] No [ ] lbt Applicable

! 8. Other tests perfor:md (such as fragility test, including results) ..j l i Resonance Search Test from 5-33 Hz. Resorant frequency is none. '

i Malfunction limit test up to 15 g's without any salfunction. _J l

lj q Pcference: CQD File tb.CQD 000263 SAflGENT h LUi10Y L womanus .J Q

& c..c. p 4;mequep!sammanrATsrasar_e -=-amewm -~ -, _ -- - - ,-- m ._ a_ . i -

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

Ob h

O VII. If Qualification by Analysis or by the Conbination of 'Ibst and Analysis,the .

(v, Conplete: N.A.

j

1. Description of Test including Results:

2. Fbthod of Analysis:

[ ] Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic .

[ ] Response Spectrum [ ] Tine-History

3. Fbdel Type: [ ] 3D [ ] 2D [ ]1D

[ ] Finite Elenent[ ] Beam [ ] Closed Form Solution l

4. [ ] Conputer Codes:

Frequency Range and ?b. of nodes considered:

[ ] Ifand Calculations

5. Danping: _ , _

6. Support Considerations in the model:

/m. l

7. Critical Structural Elenunts: Governing Seismic Total Stress Cl Identification Incation Pasponse Cochination Stress Stress Allowable!

A.

Effect Upon Functional, location Operability B. Fhx. Deflection 4

G I fe Reference; COD File tb. 000263 SARGEllT ~ LUNDY

>ruamerno ji 2 * = < o c, o 4 y,

- - -- r u - ----v-.-- -n_ _

i

I

(, INSTRUMENT IDENTIFICATION 8 ALIFICATION REQUIREMENTS ID ' No'. : - 194X927

Name: Sensor and Converter Qualification 'g ' levels Manufacturer: GE/NID h = 1.5 h 2=1. 5 V= 1. 5 Mode 1 No.: None 1

3 Instrument Required 'g' levels Equipment Numbers Location Class. Remarks h1 h2 V Dl8-N009A/D Region RB-2 > 1.2 > l.2 y l.2 A El.790' Locally mounted D18-N015A/D Region RB-2 El.790' > 1. 2 yl.2 y l.2 A Locally mounted

) on duct s

k 1

i

.; t A - Active P - Passive 1E - Class 1E

nuteen gg San J.ose, California Project Zi=er/La Salle SORT Recualification Procram File No.

Ownct Cincinnati Gas and Electric Connany/Cemmonwealth Edison Comoany f ^T Client Cincinnati Gas and Electric Ccnnany/Cc~nonwealth Edison Ccnnany

\ )

l TABLE I INSTRUMENT DATA INSTRUMEN" NAM".: Sensor and Converter MODEL NO.: 194X927

~

SERIAL OR ID. NO.:

MANUFACTURER: General Electric SPECIAI, FEATURES IF ANY: None CN FUNCTION: Monitor reactor building vent and fuel i j pool area radiation and provide input signal to indicator and trip units. -

DIMENSIONS: 10 "H X 2 3/4"W X 3 1/8"D

WEIGHT: .

. REQUIRED RANGE: 0.01 mR/hr. to 100 mR/hr.

REQUIRED ACCURACY: j- 9. 5 % f MONITORING REQUIPI2iENTS: Input frequency MOONTING DETAILS: See Figure 2 To be completed by test laboratory Output monitoring at indicator and trip unit

,e-s x . ,-

Revision 6 l l l Pa i.,e Prepared By/Date h/#392/ l of r e. ,6 - C.. s N e o l C /4 i'/tc///i l l ,.

nutech y San Jose, California Project Zimmer/La Salle SORT Recualification Program file No; Owner Cincinnati Gan and Electric Companv/Com-onwen!th Edison Company n

Client Cincinnati Gas and Fl ec**ic rn-nnny/rn--nnwonleh eM enn enmnnny (v) i

' SENSOR AND COtWERTER

~

194X927

-c +-- 7/32" *

+

98 7/16 DIA ,

DETAIL -

A7 "A" s

BOOKEND m FIXTURE n .

-+ ..

I l A

(-. /h ~

2 7/8" v

~

7/8" *A _[

l 2,,

n w w

_7 --

<4---2 b

164 i

4" MIN.

. h MOUNTING FOR GENERAL ELECTRIC SENSOR AND CONVERTER 194X927 r"m. .

FIGURE 2 Rev;sion C l Page Pres: arco By/Date jf/)/W,Vgj of

.. - .- o , , . - . . .

T' '

bLd,kt,'CiUdi San Jose, California Project Zimmer/La Salle SORT Recualification Procram File No.

Ouner Cincinnati Gas and Electric Connanv/ commonwealth Ediren Companv 7, m Client Cincinnati Gas and Electric Con,canv/Conr.onwealth Edison Connany i

's,_>

SENSOR AND COh"/ERTER 194X927 A

BOOKEND s FIXTURE

,~

\ !

m ,'

~

n -

b - ,

W H=-4 J

ACCELERC.'1ETER LCCATION FOR GENERAL ELECTRIC SENSOR AND CONVERTER 194X927

,e m

( ) .

'x_.>. FIGURE 4 Revisien 8 l l Page Prepared Sy/Cate M / ,[2 /f/ g Checked By /Date NO IOf/I/ l _l__,___ ,.

N P 1 San Jose California Project Zimmer/La Salle SORT Recualification Procram File No Owner Cincinnati Gas and Electric Cemnanv/ Commonwealth Edison compcnv

{

Client Cincinnati Gas and Electric Connany/Comm.onwealth Edison Connany O .

SENSOR AND CONVERTER 194X927

~

O A BOOKEND p FIXTURE

~

O -

l~ ,

~

!=!

1 ACCELEROMETERLOCATIONFORGENERALbLECTRIC SENSOR AND CONVERTER 194X927 FIGURE 4 Revisien S l Page Prepared Sy/Date Wd/d7 of Checked By /Cate Eis 4/#!I/l __

7.

./9/

SENSOR AND CONVERTER D18-N009 ENVIRONMENTAL QUALIFICATION TABLE D18-1 -

jm 1. DESCRIPTION Q

The instrument is a General Electric Sensor and Converter, Dag. No.194X927. -

The detector provides an output, signal to monitor the reactor core during

the heatira operation.

2. SAFETY FUNCTION The sensor and converter units sense ga :a radiation and transmit radiation i level signals to the indicator and trip units in the . control room, which

provide monitoring of the reactor buildirc ventilation exhaust and automatically isolate the reactor building vent.ilation system on high level trips.

i- 4 4

3. SAFETI DESIGN PARIJ:ETERS i

The sensor and converter cast have a sensitivity of .01-100 MR/HR (G11) ,

or 1-103 R/N (017) with an accuracy of 1 7.5%.

Worst Case: 2120F - 100% R/H A. Maximum Pressure: 760 Torr B. Maximum Temperature: 3200F C. Operating Voltage: 100 Vdc i

( 4. FSAR EIVIRO:PSNTAL CONDITIONS The equipment is located in the Reactor Building. The FSAR environmental -

conditions are tabulated below

)

4 Daration Torperature Pressure Huuidity Radiation 0-6 hr 2120F 7.0 in. WC All steam Operating 1x10-3 R/hr I 6-12 hr 1500F 7.0 in. WC 100% Integrated 1.7x10) rad i

12 hr to 1500F 0 in. WC 90% .

100 days j 5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Temperature Pressure Humidity Radiation 0-6 hr 2120F 7.0 in. WC All steam Operating 1x10-3 R/hr 6-12 hr 1500F 7.0 in. WC 100% Integrated 1.7x10 5 rad 12 hr to 1500F 0 in. WC 90% ,

100 days 6.~ QUALIFICATION METHOD Type Test The to perature of the tenny chamber was elevated and maintained at 100 0C.

The senser converter was 1) plcced in the elevated te perature environment of the chanber for six continuous hcurs and 2) subjected to a cesium 137

! radio nuclide source placed near the end of the aluminuu housing containing

[ the sensor converter GM tube to provide approximately a 50% upgrade reading.

i j

3 r"~

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

199 SENSOR AND CONVERTER D18-N009 ENVIRONMENTAL QUALIFICATION TABLE D18-1 r~s) The sensor converter output readings were recorded before, during, and after the elevated te=perature test with a ruskrak recorder.

7. RESULTS Tests de=onstrate that the sensor and converter has the required accuracy, sensitivity, and will perfora under the worst environmental conditions and is therefore qualified for its Class 1 application. The radiation and pressure variations in the reactor building will have. an in316nificant effect on the sensor converter.

9

(

I w.J t

I V

l 7..

L

b 2 00 SENSOR AND CONVERTER D18-N015 i ENVIRONMENTAL QUALIFICATION TABLE D18-1

( 1. DESCRIPTION

Ihc instrument is a General Elcetric Sensor and Converter, Dug. No.1913X927 The detector provides an output signal to monitor the reactor core during the heating operation.

2. SAFETY FUUCTION Ihe sensor and converter units sense gae .a radiation and transmit radiation level signals to the indicator and trip units in the control room, which provide conitoring of the reactor building ventilation exhaust and automatically isolate the reactor building ventilation system on hiSh level trips.

3 SAFETY DESIGN PARAMETERS The sensor and converter cust have a sensitivity of .01-100 MR/HR (011) or 1-103 R/N (017) with an accuracy of 1 7.5%.

Worst Chse: 2120F - 100% R/H A. Maximum Pressure: 760 Torr B. Maximum Temperature: 3200F C. Operating Voltage: 100 Vdc

(" . 11 . FSAR ENVIRONIENTAL C0"DITIONS The equipment is located in the Reactor Building. The PSAR cnvironmental conditions are tabulated below:

Duration Terporature Pressure Hamidity Radiation 0-6 hr 2120F 7.0 in. WC All steam Operating 1x10-3 R/hr 6-12 hr 1500F 7.0 in. UC 100% Integrated 1.7x105 rad 12 he to 1500F 0 in. WC 90%

100 days

5. ENVIRONMENTAL QUALIFICATION ENVELOPE (Spec. 22A3008, Rev. 5)

Duration Torperature Pressure Hunidity Radiation 0-6 hr 2120F 7.0 in. WC All steam Operating 1x10-3 R/hr 6-12 hr 1500F 7.0 in. WC 100% Integrated 1.7x10 5 rad 12 hr to 1500F 0 in. WC 90%

100 days

6. QUALIFICATION M3THOD

_ Type Test The temperature of the tenny chamber was elevated and cnintained at 1000C.

The sensor converter was 1) placed in the clovated tec:perature environtent of the chanber for six continuous hours and 2) subjected to a cesium 137 radio nuclide soaree placed near the end of the aluminum housing containing the sensor converter GM tube to provide approxicately a 50% upgrade reading.

l f

2/

SENSOR f.ND CONVERTER D1S-N015 ENVIRON! ENTAL QUALIFICATION TABLE D18-1

/~~.

The sensor converter output readings were recorded before, during, and

(' ') after the clovated temperature test with a ruskrak recorder.

7. RESULTS Tests de=enstrate that the sensor and converter has the required accuracy, sensitivity, and will perform under the worst environmental conditions and is therefore qualified for its Class 1 application. The radiation and pressure variations in the reactor building will have an insignificant effect on the sensor converter.

(

6

,,\

\, /

i <

\s _,1 m.-

1

= --

29]

accordance with paragraphs 5.3.1 and 5.3.3. Failure is. indicated if the test specimen does not meet the operational requirements after vibration in accor-(~)

\/

dance with paragraph 4.2. More than 20 milliseconds chatter shall be considered a failure. Any. indica-tion of chatter shall be brought to the attention of NUTECH for further analysis. All failures shall be noted in the test report.

5.0 TEST REQUIREMENTS ,

5.1 Exploratorv Testing Explo'ratory testing shall be performed to determine the test specimens' resonant frequencies, if any, within a specified frequency range. A recommended procedure for this testing is provided below. Fast Fourier Transform (FFT) or other testing methods will be acceptable provided they yield the same

. information about the dynamic characteristics of the test specimens.

5.1.1 Sine Sweep Recommended Test Parameters Test Method : Low Level Sine Sweep Input Motion: Single axis Number of Tests : 3 with one in each

(']

(~-

Orthogonal Axis Frequency Range: 1 to 100 Hz Sweep Rate : Less than 2 Octaves per minute Input g Level: 0.1 g Peak 5.1.2 Exploratory Testing Results The acceleration response in g's and transfer function for each of the accelerometer location shall be plotted as a function of frequency.

5.2 Fatigue Testing ( Sensor and Converter Onlv)

Fatigue testing shall be perdormed in order to account for any possible long term ef fects the SRV

- and LOCA event may have upon the test specimen.

This test phase shall be conducted in two parts, first, SRV fatigue testing and second SRV + LOCA fatigue testing. The RRS to be used are those generated during previous vibration testing.

e Ous .

MK2-02-038 10 wem

205 5.2.1 SRV Fatigue Testing

/ Test Method: Random motion

() [

j Input Motion: Biaxial Excitation:

Level:

2 independent random signals Table TRS to envelope RRS Number of Tests: 1 in each test specimen orientation

/ Test Specimen Orientations: 2, orientations (1) Front to back/ vertical

,- (2) Side to side / vertical Frequency Range: 1 to 200 Hz

, Duration of Individual Time History: Less than 20 sec Total Test Duration: 400 sec each orientation '-

RRS Damping: 2%

Required Response Spectra: Figures 10 and 11 5.2.2 SRV Fatigue Testing Results TRS shall be plotted for table accelerometer locations at a damping value of 2% at 1/6 octave intervals. For comparison the table TRS and RRS shall be plotted on the same sheet. Power Spectral Density (PSD) plots ~

shall be developed from the table

[) accelerometer time histories for each test specimen orientation. .

All accelerometer signals shall be recorded on anhlog magnetic tape.

5.2.3 SRV + LOCA Fatigu'e Testing :

Test Method: Random motion Input Motion: Biaxial Excitation: 2 independent random signals

, Level: Table TRS to envelope RRS Number of Tests: 1 in each test specimen

orientation J

Test Specimen Orientations: 2 orientations (1) Front to back/ vertical (2) Side to side / vertical Frequency Range: 1 to 200 Hz Duration of Individual Time History: Less

.' than 20 see Total Test Duraticit: 200 sec each orientation be i s_/ -

-MK2-02-038 11 ,

JW RRS Damping : 21

. Response Spectra: Figures 12 and 13 5.2.4 SRV + LOCA Fatigue Tenting Results TRS shall be plotted for table accelerometer

! locations at a damping value of 2% at 1/6 I octave intervals. For comparison, the table

/ TRS and RRS shall be_ plotted on the same shect. PSD plots-shall be developed from the table accelerometer time histories for each

. test specimen orientation. All accelerometer signals shall be recorded on analog magnetic tape.

5.3 Proof Testing-The adequacy of the test specimens for upset /OBE and emergency /DBE plant conditions will be demonstrated

, by the proof testing phase. This phase will be divided into two parts, testing for upset /OBE plant condition and testing for emergency /DBE plant condition, and shall consider the maximum combined dynamic loads the test specimens may experience

, under each. condition. The RRS to be used are those generated during previous ~ vibration testing and data reduction. The indicator and trip unit will be tested to OBE and DBE as a control room item. The

() sensor and converter will be tested to earthquake plus hydrodynamic loads in upset and emergency as a-

, local item.

5.3.1 Upset /OBE Condition Testing Test Method: Random Motion '

Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelop RRS Test Specimen Operation: As specified below Test Specimen Orientations: 2 orientations (1) Front to back/ vertical (2) Side to side / vertical Number of Tests : 10, 5 in each test specimer.

orientation 5

e O MK2-02-038 12 ,

1

%a PN '

86

. 5.3.1.1 Sensor and Converter-Upset (i) Pre-Vibration A/ ..s a) Place the power supply POWER SUPPLY OFF-ON switch to the OFF position.

b) Connect the sensor and

- converter, power supply, indicator and trip unit and monitoring circuit in

. accordance with Figure 8.

c) Place the TRIP TEST-ZERO-OPERATE switch on the indicator and trip unit to the OPERATE position.

' ~

d) Place switch S1 to the CLOSED position. ,

e') Place the power supply POWER SUPPLY OFF-ON switch to the ON position.

f) Verify that the reading on the ' indicator and trip

(~')T

\- unit meter is approx-imately 20 percent of the first decade.

g) Depress the RESET push-button on the indicator and trip unit and verify -

that the LG1 and HIGH indicating lights extinguish.

h) Verify that there is voltage across Resistor R1

. (Relay K2 contacts 6 and

. . 10 closed) and no voltage across Resistor R2 (Relay K1 contacts 3 and 11 opened).

(2) During Vibration Maintain the above conditions throughout the 5 tests in each test specimen orientation.

[

MK2-02-138 13 b

p,.

. $2f (3) Post Vibration

~

a) Place the power supply, g ') POWER SUPPLY OFF-ON switch

.g

( j f to the OFF position.

-b) Disconnect the monitoring

/ circuit connected in step (1) b).

'~

5.3.1.2 Indicator and Trip Unit - OBE (Normal Condition)

(1) Pre-Vibration

[ a) Place the power supply, POWER SUPPLY OFF-ON switch

, to the OFF position. ,

~

u b) Remove the sensor and converter from its case.

c) Connect the sensor and converter, power supply,

. indicator and trip unit and test equipment in accordance with Figure 9.

' (') d) Connect indicator and trip unit receptacle J1 pins 8 and 19 to individual monitoring circuits in accordance with Figure

9. ,

e) Place the TRIP TEST-ZERO-OPERATE switch on the indicator and trip unit to the OPERATE position, f) Place switch Si to the OPEN position.

g)

Place the power supply POWER SUPPLY OFF-ON switch to the ON position.

h) Turn on the electronic

~

counter and pulse generator and adjust the pulse generator output for MK2-02-038 14 9

- - ...e ym . p, m. . ,.- , g - e .- so as .e.e-e.,* .s w -- e= + + - + = = =

. 107 negative pulses of 15

! volts peak amplitude.

/~' i) Set the pulse generato:

.\

. j -

pulse duration so that the

/ l

. pulse length provides a 50 percent duty cycle.

j) Adjust the pulse generator output frequency control for a reading of approxi-mately 20 percent of the first decade on the i indicator and trip unit meter.

k) Depress the TSSET push-button on the indicator and trip unit and verify that the LG1 and HIGH indicating lights extinguish.

1) Verify that there is

. voltage across Resistor R1 (Relay K2 contacts 6 and 10 closed) and no voltage across Resistor R2 (Relay Os '

K1 contacts 3 and 11 opened). .

(2) ,D,uring Vibration Maintain the above conditions for 1 vibration test in each .

test specimen orientation.

5.3.1.3 Indicator and Trip Unit-OBE (Downscale Trip)

(1) Pre-Vibration a) If testing has been stopped repeat steps 5.3.1.2 (1) a) through 1) as required to achieve normal condition. .

O V{ .

MK2-02-038 , 15 .

. .10/

(2) _During Vibration

, a) Decrease the pulse gener-ator output frequency to O' ,.:

, the recorded value (;t 10%)

. in paragraph 4.2.2.3 step

,13 and verify that there is voltage across Resistor

-:R2 (Relay K1 contacts 3 and 11 closed) and the LOW indicating light

, illuminates.-

b) Perform this test once in each test specimen

,. orientation. --

5.3.1.4 Indicator and Trin Unit-OBE

, (Downscale Steadv State Condition)

(1) Pre-Vibration -

a) If testing has been stopped repeat steps

~

, ,5.3.1.2 (1) a) through 1) as required to achieve normal condition.

1

() ,

b)

Maintain the conditions in step 5.3.1.3(2) a) or perform if required.

(2) During Vibration

, Maintain tite above conditions -

for 1 vibration test in eacn

. test specimen orientation.

i 5.3.1.5 Indicator and Trio Unit-0BE (Upscale Trip)~

1 (1) Pre-Vibration 1

a)

, Repeat steps 5.3.1.2 (1) a) through 1) as required to achieve normal condition (2) During Vibration

, a )- Increase the pulse gener-ator output frequency to HK2-02-038 16 e

n~1

20f

' the recorded value (+ 10%)

~~

l .

'in paragraph 4.2.2.3 step 13 and verify that there O [

j is no voltage across Resistor hl (Relay K2

. contacts 6 and 10 opened) and the HIGH indicating

/ .

light illuminates.

b) Perform this test once in each test specimen orientation.

5.3.1.6 _ Indicator and Trip Unit-OBE (Upscale Steady State Condition) 2 (1) Pre-Vibration a) If testing has been stopped repeat steps 5.3.1.2 (1) a) through 1)

\s

~

, . as required to achieve normal condition.

b) Maintain the conditions in step 5.3.1.5( 2) a) or -

perform if required.

O (2) During Vibration .

~ '

, Maintain the above conditions for 1 vibration test in each test specimen orientation.

Monitoring Requirements: Indicator and trip' unit output voltage for the sensor

. and converter test and indicator and trip unit contact position, chatter detection and output voltage for the indicator and trip unit test.

Frequency Range : 1-200 Hz Test Duration: 30 sec per test RRS Damping : 2%

. Required Response Spectra : Figures 14 and 15 (OBE plus SRV plus chugging or LOCA) for the sensor and converter

, and Figures 16 and 17 (OBE) for the indicator and trip unit.

MK2-02-038 17 r"~'

!!O 5.3.2 Upset /OBE Condition Testing Results TRS for the indicator and trip unit shall be i

(N plotted for table a celerometer locations at

\_ j a damping value of 'h . (2 1/2% is acceptable)

/ at'l/6 octave intervals. The TRS for the j l sensor and converter shall be plotted at a j damping value of 1% at 1/6 octave intervals- For comparison, the table TRS and RRS shall be plotted on the same sheet. PSD plots shall be developed for the first test in each orientation. All acc'elerometer signals shall be recorded on analog magnetic tape.

5.3.3 Emergency /DBE Condition Testing Test Method: Random motion Input Motion: Biaxial Excitation: 2 independent random signals Level: Table TRS to envelope RRS

. , _ Test Specimen Operation: As Specified below Test Specimen Orientations: 2 orientations

~

(1) Front to back/ vertical

, , , (2) Side to side / vertical i Number of Tests: 1 in each test specimen

/~~ orientation N-)T 5.3.3.1 Sensor and Converter Perform test in accordance with paragraph 5.3.1.1.

5.3.3.2 Indicator and Trip Unit -

Perform test in accordance with paragraph 5.3.1.5.

Monitoring Requirements: Indicator and trip unit output voltage for the sensor and converter test and indicator and trip unit contact position and chatter detection and output voltage for the indicator and trip unit test Frequency Range: 1 to 200 Hz Test Duration: 30 sec. per test -

RRS Damping: 2%

Required Response Spectra: Figures 13 and 19 (DBE plus SRV plus chugging or

(^') LOCA)'for the sensor and converter V

MK2-02-038 18

8 N# s

All Cnd Figures 20 and 21 (DBE) for the indicator and trip unit Operational Test: Checkout Test Specimen after emergency condition tests in kN accordance with paragraph 4.2.2.1 I

5.3.4 Emergency /DBE Condition Testing.Results TRS shall be plotted for table accelerometer locations at a damping value of 2% (2 1/2% is acceptable) at 1/6 octave intervals. For comparison, the Table TRS and RRS shall be plotted on the same sheet. PSD plots shall -

be developed from the table accelerometer time histories for each test specimens orientation and voltage relay operation. All accelerometer signals shall be recorded on analog magnetic tape. Results of operational test checkout after excitation shall be reported and any significant deviation from

.the baseline shall be noted in the final report.

6.0 WITNESSING OF TESTS .

6.i ' All tests shall be subject to observation by NUTECH or their authorized representatives. .

6.2 All tests shall also be subject to observation by Cincinnati Gas and Electric and Commonwealth Edison Companies or their authorized representatives.

7.0 TEST REPORT REQUIREMENTS

,/l The test laboratory shall supply ten certified copies of a-test report which satisfies the requirements of IEEE 344 -

. 1975. This report wil describe the equipment, calibration, and test procedures, including photographs of the test set up, and provide all results and conclusions from the test. Operational checkout and inspections shall be described and all results summarized and any deficiencies and/or repairs noted. Critical data- to be included in this report are as follows:

'7 .1 Inspection and operational test results reports, verifying adjustments and recording values, also noting any significant deficiencies and repairs to device. A description of test equipment and calibration information shall be included. -

7.2 Test Specimens resonance search data

~

MK2-02-038 19 ,

9

7.3 The test response spectra (TRS) plots obtained in 5.2.2, 5.2.4, 5.3.2 and 5.3.4. These TRS are to be I computed for all accelerations recorded. For each of the two orientations for the test specimen, the TRS shall be computed for both horizontal and vertical table motions to verify that they envelop

, the corresponding RRS. .

/ 7.4 PSD plots obtained in 5.2.2, 5.2.4, 5.3.2 and 5.3.4.

. , 7.5 A record'of voltage and frequency readings, contact i

position, test specimen operation, and chatter shall be maintained in the test log.

7.6 A record of the number of test runs including level and duration shall be maintained in the test leg.

A copy of the tdst log.

~

7.7

i 7.8 Completed Instrument Data Forms (a partially completed form have been provided as Tables 1 and 2 of this specification). .

8.0 REFERENCES

8.i '

IEEE 344- 1975: 'Rocommended Practices for Seismic Qualification of Class lE Equipment for Nuclear Power Generating Stations.

8.2 GEK32374D G.E. Operation and Maintenance Instructions ( Area Radiation Monitor Sensor and Converter)

N 8.3 GEK27828G, G.E. Operation and Maintenance Instructions (Area Radiarion Monitor Indicator and .

Trip Unit) a s

l '-

l MK2-02-038 20 1 .

( . .

c..

i - -. _-- -

Calc. No. E t.! D - 030011 SO

- Rev: 00 Date: 4-22-81 Proj. No: 6093-00/4130-15

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FREGUZMCY - HZ Required Response Spectrum for Instruments mounted on Local Pancic frR'NFr$WiiiTVEMERGENCY 4&RW ehIr/:IORIZONTAL UPPERBOUND Et."JELOP OF FOLLOWING RSC: - EMSXZ1 A6 72" EMSYZ1 A6 72"-

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Required Response. Spectrum for Instruments mounted on Local Panels

-SRV--10CA/ UPSET /EMDRGnN9Y- VERT-IG%/ HORIZONTAL .

UPPERDOUND ENVELOP OF FOLLOWING RSC: - UPSXZS A6 72" UPSYZ5 A6 72" UPSXZ6 A4 48" UPSYZ6 A4 48" g UPSXZS A6 30" UPSYZ5 A6 30" g

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10 0 -

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. FREGUENCY - KZ Required Response Spectrum for Instruments mounted on Local Panels 3RV-LOCA/UPGB9/BMBRGEWJ' --- VERTICAL /i sR-MeNew UPPERDOUND ENVELOP OF FOLLOWING RSC: -

SVLYZ4 6V 72" SVLXZ1 SV ~48" h SVLXZ2 4V 30" x N

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lif QUALIFICATION OF 2" AIR OPERATED CLOBE VALVE "ITAMMEL DAllL' # Cll-F0li

\m,/ JUSTIFICATION FOR INTERIM OPERATION An analysis was performed on this valve. Accelt s 's n levels of 6 g's in each of the three directions were applied. Pressure load was also taken into account. Stresses at all critical sections were calculated and shown to be within allowable limits. The piping loads were also a'pplied at inlet and outlet ends and stresses checked against allowable limits.

The following critical sections were checked:

Yoke Legs Body / Bonnet Bolting.

( )

\' Body Flange Crotch Region Area at Nozzles Inlet and Outlet Region.

/ .

I S

e S $

e C

/

C%

(

x r-- -

(* 1:0 he

~

I LA SALLE NUCLEAR STATIONS' ;

$ UNIT 182 l NSSS EQUIPMENT QUALIFICAT10t1

SUMMARY

l

EQUIPMENT T4AME

2" Air Operated Globe Valve #21A1750P002 i

f EQUIPMENT NO: Cll-F0ll i

Reactor Building Elev. 740' LOCATION:

. EQUIPMENT CLASSIFlCATION: @ ACTIVE C PASSIVE l

OUALIFICATION METHOD: Analysic l; I

I OUALIFICATION DOCUMErn

REFERENCES:

4 l

1. Calculation by S&L i l

l 2. G.E. document #VPF 3234-2-5

3. G.E. document #VPF 3234-7-7 f

4. G.E. document #VPF 3162-112-1

5. G.E. document #VPF 3234-148-2 g(' 5, G.E. document #VPF 3234-13-6 . l 4

j

7. '

! 8.

1 i- 9.

A I (

{

h LCAD COMBINATIONS CONSIDERED IN QUALIFICATION: -

e

1. Normal Operating Loads + OBE 4 -SRVASY-TQ + ALL-TO ENVELOP

~

d

2. Normal Operating Loads + SSE + COLEVY-2+ SRVggy_7g + SRVgLL_7g ENVELOP h

3. Normal Operating Loadst SSE+ Chugging + SRVASY-TQ+ ALL-TQ ENVELOP i

i

4. Normal Operating Loads + SSE + AP j 5. Normal Operating Loads + SSE + COLEVY-1 -

i

, P

[ QUALIFICATION:

Date PREPARED BY: ,

I Dat i SARGEUTS LU..'GY r REVIEUED BY: i:

I =cevu.uaaamu N

[ AF :WiED N:

p,.,,_,-.,.- - , ,w .. - --- - -. -

_ ~ _

,Stg u

. ,,_, __~ .c n ,.,,4 c

co a

. 22/

,m

)

QUALIFICATION

SUMMARY

Seismic Qualification Method :

Analysis has been done for these following elements:

1. yoke legs

2. yoke / Body bolting

3. Flange i

4, Stem

5. Crotch area at nozzles All elements were qualified to 6 g's seismic loading in all directions.

A test is scheduled for the limit switch 'Hamr.el-Dahl' and the actuator alon,.

with the 2" Globe Valve, Cll-FDll l

l SRV Requalification Method:

O' ,

Qualified to new loads have taken hydrodynamic effect into account.

3 i

l l

M 1 H i .

s F

Ci V t Ref: CGD File No. EDDTW i SARGEf1T h LUT10Y b

>.~mumou4

=2w -

r we wvs 9av- w , - ,-.---e ,. .-w -- e w .c- < .-. - - .w .- c--u. .--= ,,=w- . - - - - - . , we

m.

_ _ _ _ _ . . . _ - _ ___=r--. mxw . - - . m.am - - >., - rua ,- .

Qualification Sunmny of Equirrent g

Nuclear Safety-Pelated Project Nos. 4266/67 pf l}

1 b

Plant Nane: LaSalle County 1&2 Type:

I.

CECO PWR

1. Utility; NSSS; G.E. BWR X l

2.

3. A-C: S&L !

I i i II. Conponent than 2" Air Operated Globe Valve #21A1750P002 1 i 1. bbdel Number 502-JFC62EA29 Quantity: 1 '

0

2. Vendor ITT Hammel Dahl i

f 3. If the cotTonent -is a cab 2 net or panel, nane and 'nodel tb. of tne devices included; N/A

(

4. Physical Description a. Appearance 2" Globe Valve i i !

Dinensions 11-1/4" x 11-5/8" x 35-1/8" b.

l c. Weight 140 lbs.

1

5. Iocation: Building: Reactor Q 5 Elevation; 740' y ,

Bolt (tb.

4

6. Field Fbunting Conditions [ ] , Size )

i

[ ] Weld (Iangth ) i

[y j Pipe mounted h 2 7. Natural Frequencies in Each Direction: 76 Hz - min.

n l 1-bl: h2: V:

i I

'I 8. a. Functional D2scription: Close on scram because of loss i i of pilot air, thus isolating the water discharged frca l the CRD's during scram. }

l l

b. Is the equipent regtnred for[ ] Hot StanrHry[ ] Cold '

Shutdcun I [X]Both

9. ' Pertinent Reference Design Specifications:

, I2 GE #21A1750 l

O i 1

Reference:

File No.

SARGEf1Tk Luf!DY f I

,~muo,..$

w -i I

2 ,-]

. _ , . _ - . - .,__ _ _ _ _ - _ _ - _ . . _ . . _ _ . . _ _ _ _. _. . .s

-ym w x - , - = - __

p-= %*

Nuclear Safetv-Pelated Xu..

Project Nos. 4266/67 III. Is Equiptent Available for Inspection in the Plant: [X] Yes []Ib h n

O '1 Cerments: ,

I h

n IV. Equiptent Qualification ththod: Test:

L Analysis: X ,

Canbination of Test and Analysis:

Test and/or Analysis by Sargent & Lundy l l

(name of Conpany or Iaboratory & Report No.)

V. Vibration Input: ,

~

1. Inads considered 1.[X] Seismic only 2.[ ] hydrodynamic only 3.[) Edplosive only i 4.lX] Other (Specify) Pressure 5.[ ] Cbnbination of __

2. Required Pesponse Spectra (attach tlm graphs):

NA

3. Reglired tcceleration in Each Direction:

(

O h1 = < 2g h2 = <2g V= <2g og gl' Qual. 'g' Tevel 6 g b g VI. If Qualification by Test, then Complete: 4

l. [ ] Single Frequency [ ] Multi-Frequency ,

a

2. [ ] Single Axis [ ] Multi-Axis

3. Frequency Rar.,a:

d

4. TRS enveloping RRS using Multi-Frequency 'Ibst[ ] Yes (Attach TRS graphr i 3 ID

) hl = h2 = V=

5. g-level Test at

? 6. Ialoratory bbunting:

1. I I Bolt (tb. , Size ) [ ] Weld (Length )[ ]

l, I , 7. Functional operability verified: [ ] Yes [ ] No { ] lbt Applicable l

l 8. Other tests performed (such as fragility test, including results) '

01i

.g i

SARGEidT b LUijDY 1 1

Reference:

File tb.

rewr21NytRS h) i e "c*oo 94 im m mm a_e . >. Q

Nuclear Safety-Relatcd g/-

i ,

Project Nos. 4266/67 l

VII. If Otalification by Analysis or by the Conbimtion of Test and Analysis,thc Co m lete:

1. Description of Test incitding Ibsults:

2. Method of Analysis:

[ X] Static Analysis [ ] Equivalent Static Analysis [ ] Dynamic L I

Analysis 1

[ ] Response Spectrum [ ] Tine-liistory l

3. tbdel Type: [] 3D [ ] 2D [ ]1D

[ ] Finite Element [ ]Deam [ ] Closed Form Solution :

4. [ ] Conputer Codes: NA Frequency Range ard No. of nodes considered:

- [ X ] Iland caw 1ations

5. namping:

6. Supfort Considerations in the model: flexible

7. Critical Stn ctural EleTents: Governing Seismic 'Ibtal Stress j A. Identification location Response Canbination Stress Stress Allcwablej Upset & Bnergency Yoke legs 9955 17500 ,

Bcdy/ Bonnet Bolting "

1.282 in2 1.322inf Flange Iang'tudinal 32240 34950 Radial 14993 -

Tangential 11778 l Nozzle Stress 24960 26250 i

Effect Upon Functional B. Pax. Deflection Ircation Operability J NA ,

n U.

Reference;

_3_ SARGENT LUNDY )

2em>w anaLt

_m 4M

bdh3DN San Jose, California Project Zimmer/La Salle SORT Recualification Procram file go, Owner Cincinnati Gas & Electric Comnanv/ Commonwealth Edison Company I l

Client Cincinnati Gas R Electric Com any/Co--onwealth Edison Cocpany L) l 9

i.

i j

lT e m 1=1 - C /\

L C F0F-i Postrian swircut l: q ,'

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t I

) TES T S T'E C IM T fl h ouN TI.N '- 7 F !!=rl = C 4 Rev:sion

~

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229 TABLE I k/ TEST SPECIMEN DATA Device Name: Air operated globe valve

Description:

2" schedule 160 flow control valve side mounted handwheel piston actuator and (2) Nat. ACME switches Primary Service Rating: 600 lb Fluid: Domineralized water Valve Operator: Single acting pneumatic cylinder Air Supply Pressure: 70 ~ 75 psig Operator Action: Air to open, spring to close Maximum operating AP: 1055 psid

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valve body, bonnet, yoke and actuator. Strain gage locations are shown in Figure 3.

V(-) 4.3 Malfunction and Failure Criteria During excitation, the test specimen shall be visually monitored for any evidence of structural failure. The failure or loosening of a part that does not affect the operation of the test specimen would not be considered as malfunction, but shall be noted in the test report. Any inappropriate opera-tion or failure of the test specimen to operate in accordance with paragraph 4.2.3, or if the total leakage is in excess of 1400 cc during proof test, or if leakage rate after proof testing exceeds 40 cc/hr, shall be considered a failure.

5.0 TEST REQUIREMENTS 5.1 Exploratory Testing Exploratory testing shall be performed to determine the test specimon 's resonant frequencies, if any, within a specified frequency range. The procedure for this testing is provided in paragraph 5.1.1. A sine sweep test or other testing methods will be acceptable provided they yield the same information O- about the dynamic characteristics of the test specime n.

5.1.1 Sine Sweep Recommended Test Parameters Test Method: Low Level, Sine Sweep Input Motion: Single Axis Number of Tests: 3, with one in each Orthogonal Axis Frequency Range: 1 to 100 Hz Sweep Rate: Less than 2 Octaves per minute Input g Level: 0.25 g peak 5.1.2 Exploratory Testing Results i

The acceleration response in g's from each accelerometer location shall be plotted as a function of frequency.

MK2-02-ll5 5 L -

5.2 Proof Testing The adequacy of the test specimen for upset and

()' emergency plant conditions will be demonstrated by proof testing. This test phase will consist of biaxial random vibrational excitation input to the equivalent of the maximum combined dynamic loads the test specimen may experience under the upset or emergency plant condition. The testing will be divided into two parts: (1) testing for upset plant condition and (2) testing for emergency plant condition; the tests consider the maximum combined dynamic loads the test specimen may experience under each condition. The maximum g-level used is the analyzed maximum g-level for the piping on which the test specimen is mounted and will experience during either the upset or emergency plant condition.

5.2.1 Upset Condition Testing Test Method: Random Motion Input Motion: Biaxial Excitation: 2 independent randon signals

(s ;

Level: Flat random input with RMS adjusted to envelop a 69 peak horizontal and 4g peak

(_/

vertical.

Test Specimen Operation: Operability demonstration in accordance with paragraph 4.2.2 Test Specimen Orientation: 2 orientations (1) Front to back/ vertical (2) Side to side / vertical Number of Tests: Five in each test specimen orientation.

(1) Test specimen at open position.

(2) Test specimen at close position with inlet pressure maintained at 1055 psig.

(3) Test specimen change of state in accordance with paragraph 4.2.3.

(4) & (5) Repeat (3).

Monitoring Requirements: test specimen inlet pressure, valve leakage detection in accor-dance with paragraph 4.2.3 and deflections or strains at the strain gage locations.

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MK2-02-ll5 6

61 Frequency Range: 1-50 Hz , ,

)

Test Duration: 30 secs. per test 5.2.2 Upset Condition Testing Results Input peak value shall be shown on the time history plots to ensure that it envelops the specified peak g level. Power Spectru.a Density (PSD) plots shall be developed from '

each accelerometer time history for the first test of each orientation. All' accelerometer signals shall be recorded on analog magnetic tape.

5.2.3 Emergency Condition Testing Test Method: Random Motion Input Motion: Biaxial Excitation: 2 independent random signals Level: Plat random input with RMS adjusted to envelop 79 horizontal and Sg vertical.

Test Specimen Operations: Operability O)

(_ demonstration in accordance with paragraph 4.2.2 Test Specimen Orientation: 2 orientations (1) Front to back/ vertical (2) Side to side / vertical Number of Tests: 1 in each orientation Test specimen change of state in accordance with paragraph 4.2.2. .

Monitoring Requirements: Test specimen inlet pressure, valve leakage detection in accor-dance with paragraph 4.2.2, and deflections or strains at the strain gage locations.

Frequency Range: 1 to 50 Hz .

Test Duration: 30 sec. per test Operational Test: Check Test Specimen after emergency condition tests in accordance with

(~N paragraph 4.2.2.

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MK2-02-115 7

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5.2.4 Emergency Condition Testing Results

() Input peak value shall be shown on the time history plots to ensure that it envelops the specified peak g level. PSD plots shall be developed from each accolorometer time history for each test specimen orientation. All accelerometer signals shall be recorded on -

analog magnetic tape. Results of operational test checkout after excitation shall be reported and any significant deviation from the baseline shall be noted in the final report.

5.3 Fragility Testing l Upon completion of the seismic qualification testing, a fragility test shall be performed on the test specimen in -

each orthogonal axis. Test operation shall be in accordance with paragraph 5.1. The fragility test will ,

consist of increasing the input g level until a non-destructive fragility level is reached. The_ test sequence shall be: vertical, side to side and ~ ff6nt to back. The fragility test shall be performed at each resonance frequency determined from paragraph 5.1 or at 50 IIz if no resonance frequencies are detected. Data obtained as a

'(" result of fragility testing shall be recorded and included in the final report. Following fragility testing an operational test shall be performed in accordance with paragraph 4.2.2 The results shall be documented and any deviation from baseline _shall be noted in the final report.

6.0 WITNESSING OF TESTS 6.1 All tests shall be_ subject to observation by NUTECll or their authorized representatives.

6.2 All tests shall also be subject to observation by Cincinnati Gas and Electric Company or their authorized representative.

7.0 TEST REPORT REQUIREMENTS SwRI shall supply ten certified copies of a test report which satisfies the requirements of IEEE 344 - 1975. This report will describe the equipment, calibration, and test procedures, including ' photographs of the test setup, and provide all results and conclusions from the test.

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Operational checkout and inspections shall be described and ;

() all results summarized and any ' deficiencies and/or repairs noted. Critical data to.be included in this report.are as follows:

7.1 Inspection and operational test results reports, verifying adjustments and recording values, also noting any significant deficiencies and repairs to device. A description of test equipment and calibration information shall be included. .

7.2 Test specimen resonance search data.

7.3 PSD and time history plots obtained in 5.2.2 and ,

5.2.4. I A record of pressure supplied and test specimen inlet i 7.4 [

port pressure during operation, valve leakage and strain or deflection of each strain gage shall be l monitored for test runs in the test log. l 7.5 A record of the number of test runs including level e and duration shall be maintained in the test log. i' 7.6 A copy of the test log.

7.7 A completed Test Specimen Data Form (a partially completed form has been provided as Table 1 of this specification.

8.0 REFERENCES

8.1 SwRI QA Procedure XI - E-101: Seismic Test of Electrical and Mechanical Components.

8.2 SWRI QA Procedure XII - E-101: Calibration of Mechanical Science Dynamics Test Equipment.

8.3 IEEE 344 - 1975: Recommended Practices for Seismic Qualification of class lE Equipment for Nuclear Power Generating Stations.

6 9

MK2-02-115 9'

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Specification For Dynamic ~ Test of Two Motor-Operated Valve Assemblies LaSalle County Station Units 1&2 Commonwealth Edison Company Wm. H. Zimmer Nuclear Power Station Unit 1 Cincinnati Gas & Electric Company t

\ Nuclear Safety-Related Prepared By Component Qualification Division

. Sargent & Lundy Engineers l

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Page 1

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SARGENT & LUNDY EN GIN EERs

j CHICAGO f.

Status Summary C\

V f Dynamic Qualification Program for

Motok- Operated Valve Assemblics l . .

Task .

7 Status

. 1) Select Actuators Complete

2) Select Representative Valves & Subsystems domplete

3) Procure Valves & Actuators . Complete

4) Mfg. Inspection of Valves & Actuators Complete

5) Analysis of 4TCO and SRV. traces to determine traces to be used -

Complete

.' 6) Time-History Analysis of Stibsystems Complete

7) Response Spectra Generation Complete

8) Faticue Damage Potential Evaluation of Time-Histories Complete

9) Preparation and Issue of Test Spec Complete

10) Design of Test Fixture Complete 11)- Fabrication of Test Fixture --10-27-81

12) Generation of Equivalent White Noise *

' Input 10-28-81

13) Baseline' Testing 10-28-81 ;

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14) Aging & Oualification Testing Start 10-28-81

15) Test Report by AE 11-11-81 16)'

Test Report by SDRC O

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Project i~.). Approvm Pagn \_/ ,

413Q-15 Specification For Dynamic Testing of Two 4266 10 -

Motor-Operated Valve Assemblies .

4267 10 LaSt.lle County Station.- Units 1&2 -~

Commonwealth Edison Company Wm. H. Zimmer fluclear Power Station - Unit 1 Cincinnati ras & Electric Company Rev. Date Reason For Issue Prepared By Reviewed By Approved By O. .( )

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Table of Contents

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1.0 Purpose 3

2.0 Introduction -

+ , .

3.0 Identification of Test Specimens -

4.0 Responsibilities ,

5.0 Instrumentation 5.1 Control Accelerometers ..

5.2 _ Response Accelerometers 5.3 Contact Chatter Monitors '

5.4. Operability Monitors 5.5l Strain Gauges .

6.0 Test Sequence .

(} 7.0 Test Requirements 7.1 Baseline Testing

'7.2 Resonance Search Test 7.3 SRV Fatigue Aging 7.4 SRV+CIIG Fatigue Aging

, 7.5 Upset Condition Qualification Test .

7.6 Emergency Condition Qualification Test 7.7 Inspection 7.8 Specimen Mount'.ng 8.0 Acceptance Criteria -

9.0 Documentation 10.0 References 9

M-9 Page 3

231 1.0 Purpose ,

The purpose of this specification is to define the technical

(~j'\

\

requirements, documentation requirements, quality assurance 1 .

requirements, and outline the responsibilities for the dyna-

/ mic testing of two motor operated valve assemblies.

2.0 Introduction .

A great amount of work has been done in demonstrating the

~

adequacy of motor operated valves to function during postula-d

- ted seismic events. This previous work has been limited to in-

, vestigating the effects of the relatively short duration dynamic

' seismic loads having a frequency content of 1-33 Hz. The objec-tive of this program is to demonstrate the adequacy of motor operated valves to function during postulated SRV actuation

'~

and LOCA. events in addition to the previously investigated seismic events. This will b'e accomplished by testing two repre-

sentative valves using a dynamic input which simulates the amplitude, frequency content, and duration for the most severe-combination of seismic,.SRV actuation, and LOCA loads.

3.0 Identification of Test Specimens 3.1 16 inch 150! Anchor Darling gate valve with.Limitorque ,

SMB-2-40 actuator ,

3.2 4 inch 300# Powell gate valve wi'th Limitorque SMB-QOO actuator O .

Page 4 -

I

h '

,3 4.0 Responsibilities -

4.1 The Consulting Engineers shall be responsible for pro-O

\2 viding the Test Lab:

. ! - te'st specimens. .

i - design of the test fixture

- valve drawings and *

- wiring diagrams as required ,'

- defining the test input 4.2 The Test Lab shall be responsible for

- fabrication of test fixture

- providing,the electrical hardware (motor control center) required for operating the valves

. . - providing the hardware (expansion tank and piping) required for leakage tests

- conducting the test in accordance with the require-ments of this specification.

5.0 Instrumentation .

. The following instrumentation shall be used. .

5.1 Control Accelerometers Three control accelerometers shall be used to d'etermine the actual input to the test specimens.

5.2 Response Accelerometers Nine response accelerometers per specimen shall be used.

. Their locations shall be as defined below as shown in

- Figure 1 .

l Page 5

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-Accelerometer Orientation Location

~

l Horiz-a Q'(/ > base of yoke 2 Horiz-c

. s 3 Horiz-a

t top of yoke 4 Horiz-c , .

~5 Vert as close as practical

/ to the' limit switch 6 Horiz j mounting screws 7 Vert

8 Horiz-a ) cnd of actuator motor

.- 9 , Horiz-c s i l-

. 4 5.3 Contact chatter Monitors The test specimens utilize a four train, rotor type, geared i

Jew limit switch which consists of four rotary type drum i

.d swi.tches each having four contacts (a total of 16 contacts I per specimen). The regilirements for the contact chatter

~

monitors are: ,

a) four contact chatter monitors per specimen shall be used l

l . b) they shall be wired one contact per monitor and the following guidelines shall.be followed in selecting contacts to be monitored:

- each rotary drum switch shall be nonitored .

(i.e. one monitor per rotary drum switch) i ~

- each contact location (i.e. distance between

~

contact and gear frame) shall be monitored.

. . = = .

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S Page 6 ,

'. . . $0l

. 4 c) the contact chatter monitoring system shall be s.et

(~'i - 'up in such a manner that should contact-chatter occur V

exceeding 2 msec it shall be detected and the duration of such chatter shall be recorded. .This may be accom-plished by use of a chatter boxfalong with a recording oscilloscope ~(triggered automahically or. manually) or any other acceptable technique..' ,

s -

5.4 Operability Monitors '

-The-opening and closing time of each specimen shall be

. recorded. This m'y a be accomplished by using a brush recorder to monitor the voltage across the limit switch, or any other acceptable means to the Consulting Engineers.

(~h (j 5,5 Strain Gages ,

Each test specimen shall be instrumented with strain gages l to determine the stress state versus time at the following locations .

lower portion of one yoke leg upper portion of same yoke leg one of the yoke-actuator bolts Any changes required to be made in the test specimens in order to' instrument them shall be approved by the Consult-ing Engineers. .

6.0 Test Secuence g-s a) Baseline Testing -

%d b) SRV Fatigue Aging Test c) Inspection ',

Page 7 j

.. .ty)

. d) SRV & CHG Fatigue Aging Test.

() e) Inspection f) Upset Condition Qualification Tests I

. g) Inspection (following each of the five upset condition tests)

~

5 .

Emergency. Cor dition Tests h) ,

1) Baseling Test l h) Resonance Search i

1 ,

7.0' 'Test Recuirements 1 -

7.1 Baseline Testing I

The purpose of the baseline test is to provido a data t

t 73 base for evaluating the valve performance during the U remainder of the test program. 'The requirements for 1 ~

the baseline test are specified below: ,

p 7..l.1 Baseline Inspection s

l Verify that all external bolts are tightened to t

the manufacturer's specifications. The bolts to be checked are: body to bonnet bolts bonnet to yoke bolts q , ,

yoke to actuator bolts n

]

n

~1imit switch. screws 1

.s actuator no6cr screws

~

valve flange bolts

.g , e

l i -

Page 8 9

143 7.1.2 Stroking Time -

Determine the opening and closing time for the valve:

l a) *in its normal service condition (valve pres--

sure and voltage according to valve data sheet) ~..

b)' in its normal service condition plus and minus 10% testing margin specified'in paragraph 6.3.1.5 of IEEE-323-1974.

In other words the valve stroking time shall be determined for three different conditions:

a) pressure and voltage at normal service condi-tion b) pressure and voltage at normal service condi-tion minus 10% ,

. c) pressure and, voltage at normal service condi-l .

tion plus 10%

7.1.3 Leakage Test .

Perform hydrostatic leakage tests according to the procedure outlined in M35-SP-61-1977.

7.2 Resonance Search

.The purpose of the resonance search test is to determine the dynamic characteristics (natural frequencies, cross-coupling effects) of the test specimens. The require-

, ments are defined below.

a) test method: uniaxial sine sweep b) frequency range: 1 to 100 IIz .

Page 9

c) input acceleration: 0.2 g minimum d) sweep rate: 1/2 octave per minute maximum

[}

4 -

c) documentation: transmissibility plots (one per I direct' ion of excit'ation per response accelerometer) l -

7.3 'SRV Fatig'ue'Agina The purpose of this test and the following test is to subject the test specimens to the design life mechanical vibration the specimens would experience from the postu-

. lated SRV actuation and LOCA events. The requirements for this. test are defined below:

al test method: triaxial random motion b1 test input: white noise generated by the Test Lab to the following requirements:

0 kl - fatigue damage potential demonstrated to be equivalent to Consulting Engineers supplied

. time history

. test response spectra envelopes required response 4

spectra. Care shall be taken to avoid excessive conservatism between the amplitude of the TRS and RRS (i.e. the enveloping must be close)

~

The equivalent white noise input'shall be approved by the Consulting Engineers prior to testing, c) the Consulting Engineers time history will consist'of

. an approximate 2 second trace which is to be repeated for a total of 9000 times. There shall be no delay

^3

{J between subsequent applications of the tra,ce. ,

Page 10 r- , . - - , , - .- -, .- ,.7 v.m.c-,.,~ y. . - - , ,,r,,., . - - - - - , .

j//[

d) demonstration of operability: the test specimens' s i 'shall be stroked once every 30 minutes f e) required response spectra: identified in Table 1 f) required time histories: identified in Table' 2

./ .

g) documentation:

~

- digitized trace of shake table motion in all three directions

- sample TRS from each control and response accel-erometer

- log of valve stroking durations 7.4 SRV + CHG Fatigue Aging '

., The requirements for this test are: ,

~ a) test method: triaxial rand 6m motion b) test input: white noise generated by the Test Lab '

to the following requirements:

fatigue damage potential demonstrated to be .

equivalent to the fatigue damage-potential of Consulting Engineers supplied time history *

- test response spectra envelopes required response spectra. Care shall be taken to avoid excessive conservatism between the amplitude of the TRS and RRS (i.e. the enveloping must be close).

The equivalent white noise input shall be approved by

_ . the Consulting Engineers prior to testing, LJ Page 11 t

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vr----e-e--w ' ,- - * * ' *

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c) the Consulting Engineer's time history will consist of anapproximate 2 second trace which is to be repeated for a total of 1500 times. There shall be no delay between subsequent applications of t'e h trace.

d) demonstration of operability: ,t'he test specimens shall be st'roked once every 10 minutes e) required response spectra: identified in table 1 f) required time histories:. identified in Table 2

. g) documentation:

- digitized trace of shake table motion in all three directions

- sample TRS from each control and response accel-erometer (R)

- log of valve stroking durations 4

? -

7.5 Upset condition Qualification Test The purpose of this test and the following test is to

. demonstrate the ability of the test specimens to~ function during the most severe loads associated with the upset

and emergency plant conditions respectively. The require-monts for this test are:

, [ a) test method: triaxial random motion b) number of tests: 5 c) test input: white ncise generated by the Test Iab i

! to the following requirements:

- fatigue damage potential demonstrated to be (s ..

equivalent to fatigue damage potential of Con-sulting Engineers supplied time history Page.12

.. . 7. g

jf l ,

. - test response spectra envelopes required response-N spectra. Care shall be taken to avoid excessive T

conservatism between the amplitude of the TRS and 1 RRS (i.e. the enveloping must be close)

'.l .

The equivelent white noise inpdt shall be approved by

~

the Consulting Engineers prior to- esting.

d) The Consulting Engineers time history will consist of-a 15 second. trace which is to be used once for each of the five upset condition tests.

e) demonstration of operability: the test specimens shall be streked cnce per test. Should the stroking time exceed the test duration the test duration SHALL NOT be extended, as the purpose of this test is to

[~}

\s demonstrate functionality during the simultaneous application of normal operating plus pcstulated dynamic loads.

fl required response spectra: identified in Table 1 g) required time histories: identified in Table 2 i

h) documentation:

- digitized trace of shake table motion in each of the three directions a sample TRS from each control and response accel-erometer (from one test only)

- log of , valve stroking durations

. ; Page 13 k - -

t

1 .

!$f 7.6 Emergency Condition Qualification Test -

The requirements for this test are:

[GD a) test method: triaxial random motion l

. I b)' number'of tests: one -

c) test input: white noise generated by the Test Lab to th'e following requirements: .

- fatigue damage potential demonstrated to be

~ equivalent to the fatigue damage potential of Consulting Engineers supplied time history.

--test response spectra envelopes required response spectra.., Care shall be taken to avoid excessive conserv2tirm between the amplitude of the TRS and RRS- (i.e. the enveloping ..

must be close) .

The equivalent white noise input shall be approved by

} .

the Consulting Engincers prior to testing.

! d) the Consulting Engineers time history will consist of d a 15 second trace which is to be applied once.

e) demonstration of operability: the test specimens.

shall be stroked once per test. Should the stroking .

l time exceed the test duration, the test duration t i

SHALL NOT be extended as the purpose of this test is-to demonstrate functionality during the simultaneous application of normal operating plus postulated dynamic loads. .

f) required response spectra: identified in Table 1 i

g) required time histories:

identified in Table 2 {

1

'Page 14 '

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. h) documentation: -

4

- digitized trace-of shake table motion in all

-(v three directions

- s, ample TRS from each control and response accel-crometer

- log of valve stroking durations 7.7 Inspection An inspection of the test specimens shall be made at the intervals in section 6.0 " Test Sequence". The inspection procedure is:

, 1) visually examine specimens for broken or loose parts.

2} verify that all external bolts cra tight (torqued to manufacturers specifications). The bolts to be

/^)

V checked are: bodj to bonnet bolts bonnet to yoke bolts

, yoke to actuator bolts Bolts may be tightened as required 31 remove limit switch cover ,

41 verify that limit switch is secure (i.e. that limit switch mounting screws are tight) . NO TIGHTENING OF ANY INTERNAL SCREWS IS PERMITTED without approval of the Conculting Engineers,

5) replace limit switch cover ,

. 7.8 Specimen Mounting The test specimena shall be mounted using fixture designed

\- by Consulting Engineers in a manner which simulates the Page 15 e

9

gp actual in-service mounting condition as closely as prac-

.tical. The mounting of the valve and test fixture to

/O h i

V j tho shaka table shall be such that the vibratory input

' is transmitted without arnplification or, attenuation.

8.0 Acceptance Criteria -

a) A test failure shall be defined as any occurrence which results in

- failure of the test specimens to stroke; or

- breach of the pressure boundary other.than leakage at gaskets or packing

. - severance of any external portion of the device

,b) A' test anomaly shall be defined as any abnormal occurrence other than a failure, i

c) Should a test failure occur the testing shall be stopped.

Any further course of action shall be determined by the -

Consulting Engineers test representative.

,d) TheConsui.tingEngineer'sbreresponsiblefordetermining the acceptability of any test anomaly.

, e). The Consulting Engineers reserve the right to modify the test procedure 9.0 Documentation A test report shall be prepared by the Test Lab. This report shall include:

a)

details of the test procedure

b) transmissibility plots Page 16

.- . . . _ i b ,..____ , .,[. ,.-- . _ ,_ _ _ . . . , _ .

, gj c) test response spectra plots -

i d) documentation demonstrating how the fatigue damage poten-l( tial of the white noise inputs was shown to be equivalent

{ to the fat,igue damage potential of Consulting Engineers

'i !

/ supplied time histories j -, el digitized' trace of white noise input -

l .

f) photographs of test set-up -

J '

g) descri,ption of monitoring techniques j hl test log i

e il all pertinent measurements and observations j) results with a de,scription of any abnormalities or mal-f I

functions -

^

.kl identification of all tosc equipment and instrumentation

- including last calibration date.

(Oj Ten copies of this test report shall be submitted to the Con-sulting Engineers.

O l

L . .

u .

l .

i L .

Page 17 i

t

. . _ _ ._...-.y._ __.-.............;....,.. . . . _ . . _ . . . . . . . . .

. . . .._ 7

f,Q 10.0 References a) IEEE-323-1974 "IEEE Standard for Qualifying Class lE Equipment for Nuclear Power Generating 7,f Stations." ,

b) IEEE-344-1975 "IEEE Recommended Practiices for Seismic Qualification of Class lE Equipment for

_ Nuclear Power Generating S'tations."

c) IEEE-382-1980 "IEEE Standard for Qualification of Safety-Related Valve Actuators."

dl MSS-SP61-1977 " Pressure Testing of'Stee'l Valves" el Sargent & Lunde-Form MSS-6.2B " Standard Specification for Seismic Quali-fication Criteria for Category I (Essential)

Equipment Installed in Nuclear Power Plants."

f) Sargent & Lundy Calculation CQD-000233 " Time History Dyna-mic Analysis of Piping Systems for Test Motion Input Generation" g) Sargent & Lundy Calculation CQD-000234'" Fatigue Damage

~

Evaluation For Test Input Time Histories" 1

, ~

e Page 18 i

_ . , . , . . . ,,um 2. , ~4 ,

. Y Y YS-+ b '* ~ -' ' ' ' *

. .q p t FIGURE 1 ~*

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l ~

t Acceleroraeter Location . ,

~

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. Limit Switch Compartment, _ c.h L-~

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k

, 7: vertical 8: horiz-a

.' J 9: horiz-c

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~_ V

.UY Specimen DataLSheet '

~

16' inch 150# Motor Operated Gate Valve I:

Actuator: -

i , .

Manufacturer - Limitorque i Model - SMB-2-40

Serial No. - Tag #W-18176 .

Power - - 3 phase 60 cycles 460 volts

Horse Power ' 5.3, RPM - 3600 Full load Amps - 7.55 Locked Rotor Amps - 62.5 Approx. Weight - 660 lbs. .

Valve:. .

' Manufacturer - Darling Valve & Manufacturing Co.

l Model - O.S.&Y carbon steel gate valve with weld ends Serial No. - E-5811-031, Tag #E22-F015 i '

Normal Pressure - '

Seat Test Pressure - 300 psi t .

Bolting Data: ,

Torque (Ft-Lbs'

, - Quantity Description Nominal Max.

Body / Bonnet 24 5/8-11UNC-2Ax3-% 35 Sn Yoke legs 4 7/8-9UNC-2Ax5- 100~ 120 i Packing Gland Foll 2 3/4-10UNC-2AX5-h -

100 1

Limotorque Oper. 8 3/4-lOUNC-2Ax3- 90 100, Total Assembly Weight - 1250 lbs. (Approx. )

Max. Opening or. Closing Time - 16 secs.

e-Page 20 :

e a

c , e= w, ,e m- -m. , , . ,ee,-,e-. .,,,-,_,-a,,,, _g.,r-y_ ,, .p 7 , ,,.y., ,_ , ,._ ,,__ . ,, , _g_

JK TABLE I -

REQUIRED RESPONSE SPECTRA Test Phase Table or Figure No.

, 4" Powell Valve ~ 16" Anchor Darling Valve Vert. Horize.htal Vert. Horizontal b-b a-a .'-c b-b a-a c-c SRV Aging 1 2 3 4 5 6 ,

SRV + CHG. Aging 7 8 9 10 11 12 Upset Condition 13 14 15 16 17 18 Qualification -

Emergency Condition 19 20 21 22 23 24 Qualification '

8 Note: Direction a-a Hori::ontal-Along Pipe Axis A b-b Vertical c-c Horizontal-Perpendicular to Pipe Axis I ,

O ,

Page 21 ,

o jf *'. TABLE 2 ,.7.Tg t

~ ~

List of Information in Tape in Sequence: Read 4 (6x, F12.0)

FILE VALVE CASE DIRECTIOL l #, SIZE . .

1 16" SRV A- B ~

2! 150# -

B 3 Anchor . C Darling .

. . . O

~4 4" SRV A

(

l 5

6 300#

Powell

'B C

> $> A 7 16" SRV + CHUG A 8 150# B C 9 Anchor C A=Along Pipe Axi:

l Darling (Horiz)

B= Vertical 10 4" SRV + CHUG A (up-down) l 11 300# B 12 Powell C 13 16" UPSET A C=.1.er to Pipe 14 150# B Axis (Horiz)

/G 15 Anchor C

'U Darling 16 4" UPSET A 17 300# B Tape No.2303 18 Po_well c 19 16" EMERGENCY A 20 150# B 21 Anchor C .

. Darling 22 4" EMERGENCY A 23 300# B 24 Powell C Qa Page 22 ,

Final Page L _

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