ML20125B950

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Forwards Info Required for NRC to Review IST Program & Requests for Relief from ASME Code Section XI Requirements
ML20125B950
Person / Time
Site: Monticello 
Issue date: 12/14/1977
From: Mayer L
NORTHERN STATES POWER CO.
To:
NRC
References
NUDOCS 9212100225
Download: ML20125B950 (134)


Text

{{#Wiki_filter:. MSP R!GUK02Y DOCET E COPY NORTHERN STATES POWEM COMPANY Q'_1 ' " /, \\ K Decembre 14, 1977 ?' N3([ l/l/p 7 Lv Q 4 Wcae ~ J U.s.socan,,1977 I Mr Victor 9tello, Di roi t or i Division of eperatIng Heactors 9 'g8 N c/o Distribution Services Branch, LP1. AD;t y 11 S Nucienr Eegulatory Consnission 4 k'a sh i n g t on. DC 20555

Dear Mr Stello:

MONTICELLO UltCl.;A CENERATING P! ANT Docket No. 50-263 Liccase No. DPR-22 Information Required for NPC Review of Inservice Irispection and Testing Program and Requesta for Relief from ASMF code Sec'ior XI Requirements The inservice inspection testing requirements for nuclear power t lant compon-ents delineated in 10CFR50, Section 50.55a, were changed by a rMston to the Regulations published on February 27, 1976. As a result of thf2 revi si on, Northern States Power Company must comply with the examinatio ard +est ing requirements contained in current e<litions of Sect ion XI of the AT:E l u t ter and Pressure Vessel Code. In a letter dated November 24, 1976 f rou Mr D L Ziemann, Chiet Operating Reactors Branch No. 2, (TSURC, Nort e n States Power Compar. 54; advised of the h procedure to follow in implementing the revi sions to 10CTR50, &c aon 50.55a. This letter a equested the submissic of a description of our ptanned inservice inspection a. d testing program and requests for relief f rom ASME Code require-ments. The attached report entitled, ASME C,de Section XI Inservice Inspection and Testing Program Beginning February 28, 1978 and Information Required for NRC Review of Requests for Relief f rom AS'E Code Section XI Requirements", provides all of the information requested in your November 24, 1977 letter with the exception of: a) Identification of components to be subjected to leakage, hydrostatic and pressure tests e) Identification of Quality c roup C coraponents to be visually inspected It is our intention to supply thie irfo e ion in the fonn of system drawings showing Quality Group boundaries. U< recific list of Quality Group C 9212100225 771214 PDR ADOCK 05000263 773490086 G PDR 4

1 NORTHEHN CTATED POWER COMPANY lir Victor Stello Page 2 December 14, 1977 (oraponents (iucluding supports and hangers) will be submitted. We believe these drawings will be sufficiently detailed for your review of our Quality Groun C Program. We are required to irnplement thi s p rogram on Februa ry 28, 1978. To pemit us to meet this schedule, we ask that you complete review of the attached report as soon at consible and issue the necessary Technical Specification changes requested in nur License Amendment Request dated August 30, 1977. You rs very t ruly, h-h&fV L 0 Mayer, PE Manager of Suelear Suppt ". 1xtt /ttet /deh cc: J G Keppler G Charnoff MPCA Attn: J W Ferman Attachment l

4 4 4 NORTilERN STATES POWER COMPANY MONTICELLO NUCLEAR CENERATING PLANT DOCKET No. 50-263 LICENSE NO. DPR-22 ASME CODE SECTION XI INSERVICE INSPECTION AND TESTING PROGRAM BEGINNING FEB".UARY 28, 1978 ANE INFORMATION. REQUIRED FOR NRC REVIEW OF REQUESTS FOR RELIEF FR04 ASME CODE SECTION XI REQUIREMENTS Submitted:. December 14, 1977 _., ~ - -. _ - - ~. - - - - - ~.., _. -.

f ? f .f l a ? f l-1 .i TABLE OF CONTEfffS l SECTION i I 1 Inservice Inspuction Program. Visual Obwrvation and Nondestructive Testing 2 Inservice Inspection. Program - I Pressure Tests 3 Inservice Testing of Pumps and Valves 3 and Valves 1 4 Requests for Relief from ASME Code Section XI Requirements Determined to be Impractical 5 Proposed Technical Specification Changes f i I D - I + b 4 .L. -ii - c_,.._,..._-. m.

!L SECTION 1 INSERVICE INSPECTION PROCP&1 VISUAL 03SERVATION AND IiOI: DESTRUCTIVE TESTINC f ASME Section XI Nondestructive Examination Progra 2 - Class 1 ASME Code Edition and Addenda: 1974 Edition through end including Surraer 1975 Addenda Program Period: February 28, 1978 to June 30,1981 (Third Inspection Period) J' NOTES: 1. The following tables identify the specific Class I cccponents and parts to be examined. These tables can be directly correlated with Table IWB-2500 and Table ITJB-2600 of Section XI identify the examination method for each listed item. The inspections that were completed during period one and period two are identified in the tables, along with the running percent completed during 'each of. these periods. No effort was 12ade to retrofit i i*. Items into the first two periods that tera not previously required for examination. The tables shcv the amount of items required to be examined during period three and the corresponding percentage that will have been con- . pleted by the end of this period. l 2. Repairs will be performed in accordance with the applicable requirements of the latest edition ar;d addenda of the ASME Code, Section XI. However, if rule.c for a particular repair are not specified in Section XI, the original design specification and Construction Code of the component or system, or .later editions of the Construction Code or ASME Code Section III, either in their entirety or portions thereof, may be used. LEGE!G Exam' nation method: V - visual U.T. - ultrasonic R.T. - radiography S - surface. examination, either liquid penetrant or magnetic particle Inspection" Period O*E . June 30, 1971 to October 30, 1975 IVO - Octobei 30, 1974 to February 28,.1978 THREE. February 281.1978 to June 30, 1981 1 r, .__..,__m_.

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    . D MN N FT I L O T ON P I '5 f T Ywfo G Sr N C I B A B I E HTI D .T P OP M M N I N N m M +_ It n U O U O IO TRP I I D y I T, X i TA TB A l M TE TE 2 1 JRm )D TA A A E Ml t U Cs I L UL f L A AN AN arg t t 1 I D L D i E L I I 1 I E t C O CO M. B O S C C Y 1 T UL t' L w a T *, u r R D s l I IA IF RF I N DR N I I T I N P s I 1 t NI RN R M vA p oaf ] T CP CN CN tTI NT !AP EF ER A AN A CA CA s2 E N EY EA EA oF TO mM 'u O RB PM R N BD SC HD RD R D y C T t ( sn i R t Ev: C t A 2 mn r uTt Cm A i f m T. B N aM N t E 9 s 6 B 7# ASME Section XI Nondestructive Examination program - Class 2 ASME Code Edition and Addenda: 1974 Edition through and including Summer 1975 Addenda Program Period: Feb rua ry 28, 1978 to June 30, 1981 (Third Inspection Period) NOTES: 1. The following tables identify the specific class 2 components and parts to be examined. These tables can be-directly correlated with Table IWC-2520 and Table IWC-2600 of Section XI and identify the examination method for each listed item. In period'one and two, Class 2 components and parts were not required to be examined; because of this, the Class 2 inspection program will begin with period three. The tables identify the number of-items required to be examined over a forty (40) year service lifetime, and the amount required for a ten (10) year inspection interval.. The tables also show the amount of items required to be examined during period three (which is approximately 1/3 of that required for an inspection interval), and the percentage that will have been completed 'by the end of that period based on the 40 year requirements. i 2. The scope of the inspection program for Class 2 components was based on the exemption criteria of IWC-1220. 3. In accordance with the requirements of IWC 2411 the nondestructive examinations were selected so that the 1 total examinations completed over forty '(40) years will be 100% of the required examinations of the system or j portions of the systems with a single stream or be equivalent to having performed 100% of the required examinations 11n one of the streams of a multiple stream system. The only exception is that the selection of 0 pressure retaining bolting for valves was based on the type, manufacturer, and design of valve and not on tlue 4 total number of certain size valve bonnet bolts per system. ~ 4. Repairs will be performed'in accordance with the applicable requirements of the latest edition and addenda of the ASFE Code, Section XI. However, if rules for a particular repair are not specified in Section XI, the original design. specification and Construction Code of the canponent or system, or later nditions of the Construction Code or ASME Code Section III, either in their ' entirety or portions thereof, may be used. + IEGEND: Examination method: V - visual U.T. - ultrasonic ^ R.T. - radiography S - surface examination, either liquid penetrant or magentic particle Inspection Period ONE - June 30,,1971 to October 30,-1974 TWO - October 30, 1974 to February 28, 1978 TIIREE - February 28, 1978 to ~ June 30,l1981 -y w,.. v. y. N -eege e a gggg 3 a
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    eEh e-g g Dbc ~ ~ ep 5"* U Eh! ~ E F ($ [ E E5 g C W e', t 't 2-3{ $$ th NN Ch Q , a.. ..a I& t gg S a ~ ~ ~ ~ RJ. L { [ [ 6 gg e n E E s-U.. t e o. k E5 BE
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    b3 + r3 y m 5 "k E p g a ys g 2 F B G. g E g* a w v t5 t b $ p$ E f k h W zu e ee t e y ? 5 L a k e@a. st? sq 3...ooo y y A 5 f d~ e a e e v-aeee s e 1.k9 j ( 4 + I l t ASME Section XI Nondestructive Examination Program - Class 3 ASME Code Edition and Addenda: 1974 Edition through and including Suwr 1975 Addenda Program Period February 28, 1978 to June 30, 1981 (Third Inspection Feriod) l ' An?.S : The classificationdiagrams*.dentify the systems that are required for exa=lnation in accordance with IWD-2000. 1. these examinations were not required, and no effort will be made ..o retrofit During period one and perid two, these examinations. the inspection program for Class 3 components is based on the classification of the plant's The scope of. The inspection program will confort 2. inspection boundaries and exuaptions as allowed for in IWD-2600 and IWD-5'400. to IWD-2400 (Inspection Schedule), and will begin with period three of the first inspection interval. 1 3. Visual examination. rill N .onducted for evidence of component leakage, structural distress, or corrosion when the system is andergoing - ther a system inservice test, compoaent functional test, or a systen pressure test. Supports and hangers for em:ponents will be visually examined to detect any loss of support capability or evidence of.aadequate restraint. y Repairs will be performed in accordance with the applicable requirements of the latest edition and 5. addenda of the ASME Code, Section XI. However, if rules for a particular repair are not specified in Section XI, the original design specification and Construction Code of the component or system, or later editions of the Construction Code or ASME Code Section III, either in their entirety or portions thereof, may be used. I.EGEND Inspection Period ONE - June 30, 1971 to October 30, 1974 TWO - October 30, 1974 to February 28, 1978 THREE - February 28, 1978 to June 30, 1981 l
    • These drawings will be submitted as a supplement to this report.
    1 ] I a l w k c2 tt O B
    a ASME Section XI Pressure Testing Pror, ram rd ASME Code. Edition and Addenda: 1974 Edition through and including Su=:2er 1975 Addenda Program Period: February 26, 1976 through october 26, 1979 g ]
    m
    4 6
    w R Co=ponents to be subjected to pressure tests vill be shown on systar2 drawings showing Q Quality Group boundaries. 'Ihese dmvings vill be sub:sitted as a supplemnt to this NWd-d h ] M O ASME TEST TEST CODE CLASS ' TYPE FREQUENCY == Leakage refueling IVB-5210(a) 26 3 IWB-5221 8 g IWA-5000 1 to l,o Hydrostatic 10 years IWB-5210(b) 26 i IWB-5222 IVA-5000 2 ' Pressure 10 years IWC-2412 25, 26 IWC-2510 Pressure 10 years IWD-2410 (b) 25, 26 l 3 l ..._.._.m g n SECTION 3 INSSHVICE TESTI!C _OF PUNPS AND VALVES A. enp1'ie:able ASME code F41 tion and Addendat 197h Diition
    < rwah and including Summer 1975 Addenda
    . Program Period: February 28, 1978 to October 28, 1979 c f' ..a- - f r -I ~.il 3-1 C. Pu_,) Testirg Applicable ASME Code Punp Description Class Test Parameter Requests for Relief L N Pi aP Q V j 73 11 Emergency Service Water 3 hR PR RR NR ;M NA RR 1, 2, 3 12 Emergency Service Water 3 hR RR RR hR.M NA RR 1, 2, 3 11 Standby Liquid Control 2 .2 M M M M M RR 2, 3 12 Standby Liquid Control 2 hR M M M M M RR 2, 3 11 Core Spray 2 NR M M M M NA RR Z, 3 12 Core Spray 2 hR M M M M NA RR Z, 3 11 Residual lieat Renoval 2 hR M M M M NA RR Z, 3 12 Residual licat Removal 2 NR M M M M NA RR Z, 3 3 13 Residual licat Removal 2 hR M M M M NA RR 2, 3 i 14 Residual lieat Removal 2 NR M M M M NA RR 2, 3 11 RIR Service Water 3 hR RR RR M M NA RR 1, 2, 3 j 12 ElR Service Water 3 hR RR RR M M NA RR 1, 2, 3 13 RIR Scryice Water 3 hR RR RR M M NA RR 1, 2, 3 14 RIR Service Water 3 i NR RR RR M M NA FR 1, 2, 3 RR 2, 3 High Pressure Coolant Injection 2 M M M M M M l w L Reactor Lore Isolation Cooling 2 M' M M M ! M !M RR 2, 3 Key M= Monthly NR = Not required (constant speed drive or fixed resistance systen) WA = Not applicable (sealed bearings) RR = See request for relief D. Valve Testirg FSAR Valve Valve Applicable ASME Valve Test Request Code Class Catecory Frequency Test For Relief System Nu ber No. Description Fhin stea A0 2-80A 80-A Main Steam Isolation 1 A Q Full Stroke-Time 4 Shin stra AO 2-80B S0-B Main Steam Isolation 1 A Q Full Stroke-Time 4 ! bin
    seen, AO 2-80C 80-C Phin Steam Isolation 1
    A Q Full Stmke-Time 4 bbin seenn AO 2-80D 80-D hhin Steam Isolation 1 A Q Full Stroke-Time 4 hhin Steam A0 2-86A 86-A Main Steam Isolation 1 A Q Full Stroke-Time 4 bbin Steam AO 2-86B 86-B thin Steam Isolation 1 A Q Full Stroke-Time 4 thin Steam A0 2-86C 86-C hhin Steam Isolation 1 A Q Full Stroke-Time 4 Bhin 1 A Q Full Stroke-Time 4 Steam AO 2-86D 86-D 1 bin Steam Isolation Y Abin Steam 50-2373 74 Steamline Drain Isolation 1 A Q Full Stroke-Time 4 Fhin Steam MO-23?4 77 Steamline Drain Isolatio 1 A Q Full Stroke-Time 4 bbin Steam RV-2-71A RV-71-A Main Steam Safety Relief 1 C IhV-3510 Setpoint l Main Steam RV-2-71B RV-71-B Main Steam Safety Relief 1 C IhV-3510 Setpoint bbin Steam RV-2-71C RV-71-C Main Steam Safety Relief I C IhV-3510 Setpoint Ahin Steam RV-2-71D RV-71-D Main Steam Safety Relief I C IhV-3510 Setpoint Main Steam RV-2-71E None Main Steam Safety Relief 1 C IhV-3510 Setpoint bbin Steam RV-2-71F None Main Steam Safety Relief 1 C IhV-3510 Setpoint Vain Steam RV-2-71G None ? bin Steam Safety Felief 1 C IhV-3510 Setpoint Main Steam RV-2-7111 None Main Steam Safety Relief l 1 C IhV-3510 Setpoint L-___..h__ l. E 4 i j; j i FSAR 4 } Valve Valve Applicable AS1E Valve Test Request System-Nunber No. Description Ccde Class ' Category Frecuency Test For Relief Lii FW FW 91-1 27B FW Inlet Check Valve 2 C RR RR 7 l t i FN FW 91-2 27A FW Inlet Check Valve 2 C RR RR 7 g FW -FW 94-1 '96B Outboard Isolation 1 l A, C RR RR 4, 8 1 i FW FW 94-2 96A Outboard Isolation 1 A, C RR RR 4, 8 FW FW 97-1 28B Inboard Isolation 1 A, C RR RR 4, 8 l l f FW -FW 97-2 28A Inboard Isolation 1 A, C RR RR 4, 8 i + j FW FW 98-1 29B Feedwater Block Valve 1 E NR Valve Lineup f i FW FW 98-2 29A Feedwater Block Valve 1 E NR Valve Lineup Recirc CV-2790 39- -Rx Water Sample Isolaticrt 2 A Q Full Stroke-Tire 4 Recirc CV-2791 40 Rx Water Sample Isolaticrt 2' A Q Full Stroke-Tbe 4 Recirc hD-2-43/ 43A Recirc Suction 1 B CSIQ Full Stroke-Tim i 2- ,43B Recirc Suction 1 B CSIQ Full Stroke-Tim r Recirc h0-2-431; 1 -Recirc-30-2-S3/ 53A Recire Disct::rge 1 B-CSIQ Full Stroke-Tim i .Recirc 3D-2-53I 53B Recirc Discharge 1' B CSIQ Full Stroke-Tim 1 Recirc 'h0-2-54/ 54A' Recirc Disch.' Bypass .1 - B -Q Full' Stroke-Tim j. 2Recirc-FD-2-54I 54B-Recire Disch. Bypass 1 B Q Full Stroke-Tim i } Recirc-3D-2-65/ 65B' Recirc Loop Crosstie 1 B CSIQ Full Stroke-Tire j Recire 3D-2-651 -65A Recirc Loop Cross' tie 1 B CSIQ. FullStroke-Tihe I FSAR Valve Valve Applicable ASME Valve Test Request System Ntnber No. Description Code Class Categorv Frequency Test For Relief i Recire ?D-2-66A 66B Recirt Crosstie Bypass 1 B CSIQ Full Stroke-Tire Recirc ?D-2-66E 66A Recirc Crosstie Bypass 1 B CSIQ Full Stroke-Tire Block Valve on Full Stroke-Tin le Recirc None Urrer Seal Lealoff 2 B RR 5 Block Valve on + Recirc None Urner Seal Leakoff 2 B RR Full Stroke-Tire 5 j ma RV-1990 72A Pump Suction Relief 2 C IhY-3510 Setpoint l mR RV-1991 72B Ptep Suction Relief 2 C IhV-3510 Setpoint ma RV-1992 72C Pump Suction Relief 2 C IhV-3510 Setpoint l 4 v pla RV-1993 72D Pump Suction Relief 2 C IhV-3510 Setpoint j PJ R RV-2004 35A Pu:7 Disch Relief 2 C IhV-3510 Setpoint RIR RV-2005 35B Ptep Disch Relief 2 C IhV-3510 Setpoint mm Nonc lix Shell Side Relief 2 C IhV-3510 Setpoint pl R None IIx Shell Side Relief 2 C IhV-3510 Setpoint pl a AO-10-461 AO-46A LPCI Loop Check 1 A, C CSIQ Exercise 4 PJ R A0-10-403 AO-46B LPCI Loop Check 1 A, C CSIQ Exercise 4 pja RIR-2-1 48A PJR Pump Discharge Check 2 C Q Exercise PJ R RIR-2-2 48B PJR Pump Discharge Check 2 C Q Exercise pj n FJR-2-3 4SC RIR Pump Discharge Check 2 C Q Exercise l Exercise pjR PJ R-2-4 4SD FJR Pump Discharge Check 2 C Q FSAR Valve Valve Applicable ASE Valve Test Reque.,t System Ntrber No. Description Code Class Cateprv Frequency Test For Relief RIR PJ R-21 29 Pac 11 cad C1g Check 1 C CSIQ Exercise RIR RIR-8-1 19A RIR Min Flow Check 2 C RR RR 7 RIR 30-1986 50-13A Toms Suction 2 E NR Valve Lineup PJR 5D-1987 3D-13B Torus Suction 2 E NR Valve Lineup RIE 30-1988 BD-15A Shutdown C1g Suction 2 C CSIQ Full Stroke-Tim RIR 30-1989 ?D-15B Shutdown Cig Suction 2 B CSIQ Full Stroke-Tim A PJR 3D-2002 'D-65A lix Bypass 2 E NR Valve Lineup RIR 50-2003 30-65B lix Bypass 2 E NR Valve Lineup i RIE 3D-2006 ?D-39A Disch to Torus 2 A Q Full Stroke-Tim 4 RIR 30-2007 3D-39B Disch to Torus 2 A Q Full Stroke-Tire 4 RIR 50-2008 BD-34A Torus C1g Inlet 2 A Q Full Stroke-Time 4 PJR 30-2009 30-34B Torus C1g Inlet 2 A Q Full Stroke-Tim 4 RIR 30-2010 ?D-33A Torus Spray 2 A Q Full Stroke-Tity 4 RIR 50-2011 50-38B Torus Sprav 2 A Q Full Stroke-Tim 4 RIR FD-2012 TD-27A LPCI Injection 2 B Q Full Stroke-Tim RIE 50-2013 3D-27B LPCI Injection 2 B Q Full Stroke-Tim RIR 50-2014 3D-25A LPCI Injection 1 A Q Full Struke-Tim 4 RIR 50-2015 3D-25B ll'CI Injection 1 A Q Full Stroke-Tim 4 FSAR Valve Valve Applicable ASE Valve Test Request System Nu:nber No. Description Code Class Category Frequency Test For Relief Cont Spray PJR 10-2020 3D-26A Outboard Isolation 2 A O Full Stroke-Tine 4 1 Cont Spray PJR 3D-2021 3D-26B Outboard Isolation 2 A 0 Full Stmke-Time 4 Cont Spray RIR 3D-2022 3D-31A Inner Isolaticn 2 A 0 Full Stroke-Tire 4 Cont Spray i RIR 3D-2023 3D-31B Inner Isolation 2 A 0 Full Struke-Tire 4 PJR h0-2026 hD-33 11ead Sorav Isolation I A Q Full Stroke-Tire 4 RIR 3D-2027 30-32 licad Spray Isolation 1 A Q Full Stroke-Tire 4 RIR 3D-2029 3D-18 Shutdown C1n Isolation 1 A CSIQ Full Stroke-Tire 4 RIR 3D-2030 3D-17 Shutdown C]n Isolation 1 A CSIQ Full Stroke-Tire 4 RIR 3D-2033 3D-20 PJR Loop Crosstie 2 E NR Valve Lineup PJR 30-2032 30-37 Disch to haste Surne 2 B Q Full Stroke-Tire RIR CV-1994 CV-153A PJR Purp Min Flow 2 B Q Full Stroke-Tire RIR CV-1995 CV-153B PJR Ptro Min Flow 2 B Q Full Stroke-Tine RIR CV-1996 CV-153C RIR hrp Min Flow 2 B Q Full Stmke-Tirte l RIR CV-1997 CV-153D PJR hro Min Flow 2 B Q Full Stroke-Tire t } FJR RV-2025 44 IIcad Spray Line Relief 2 C IhV-351( Setpoint RIR RI R-8-2 19B PJR Min Flow Check 2 C RR RR 7 r RIR RIR-SW-1 7 182 SW Imere Supply to FJR 2 C RR RR 11 ElR RV-2031 40 PJR Shutdown C1n Relief 2 C IhY-351t Setpoint 1 FS?R Valve Valve Applicable AS!-IE Valve Test Request System Number No. Description Code Class Categorv Frequency Test For Relief RIR RIR-6-1 81A PJR Loop Block 1 E hR Valve Lineup RIR RIR-6-2 81B RIE Loop Block 1 E hR Valve Lineup l RIR RIR-1-1 152A RIR Pump Suction Block 2 E NR Valve Lineup FJR RIR-1-2 152B FJR Pump Suction Block 2 E NR Valve Lineup RIE RIR-1-3 152C RIR Pump Suction Block 2 E hR Valve Lineup RIR RiiR-1-4 152D RIR Pump Suction Block 2 L hR Valve Lineup RIR RIR-3-1 47A RIR Pu.p Disch Block 2 E NR Valve Lineup i RIR RIR 2 47B RiR Pump Disch Block 2 E AR Valve Lineup RIR RIR-3-3 47C RIR Pump Disch Block 2 E hR Valve Lineup ElR RIR-3-4 47D RIR Pump Disch Block 2 E hR Valve Lineup RIE RIR-18-1 30A CST to PIR Block 2 E hR Valve Lineup RfR RIR-18-2 30B CST to RIR Block 2 E NR Valve Lineup Core Snrn e A0-14 -13! A0-13A Loop Inj. Check 1 AC CSIQ Exercise 4 I Core Snray A0-14-13B A0-13B I;;op Ini. Check 1 A, C CSIQ Exercise 4 Core i Serav 50-1753 f.0-12A Core Spray Injection 1 A Q Full Stroke-Tirt 4 Core Full Stroke-Tir.el Scrav 3D-1754 ?D-12B Core Sprav Injection 1 A Q 4 Core i Snrm- ?-D-17 51 ?0-11A Core Spray injection 2 B Q Full Stroke-Tire Core l Sorav 50-1752 hD-11B Core Spray Injection B Q ! Full Stroke-Time 1 I i FSAR Valve Valve Applicable ASME Valve Test " quest A System Number No. Description Code Class Categorv Frecuency Test For Relief fre RV-1745 20A Disch Line Relief 2 C IhY-3510 Setpoint h((. RV-1746 20B Disch Line Relief 2 C IhY-3510.Setpoint hU((y 4 CS-9-1 10A Pump Disch Check 2 C Q Exercise c k [*. CS-9-2 10B Pump Disch 0:eck 2 C Q Exercise [*, 50-1741 7A Cere Spray Suction 2 B Q Full Stroke-Tira h((y 30-1742 7B Core spray Suction 2 B Q Full Stroke-Tim: re Spr CS-10-1 18A Min Flow Block 2 E AR Valve Lineup i ]} fr CS-10-2 ISB Min Flow Block 2 E NR Valve Lineup y n[*, MO-1749 30-26A Test Line to Torus 2 B Q Full Stroke-Tim: Core 30-1750 FO-26B Test Line to Torus 2 B Q Full Stroke-Tin: Arnv h[,[y CS-1-1 32A Torus Suction Block 2 E NR Valve Lineup { l ^ k((y CS-1-2 32B Tonis Suction Block 2 E NR Valve Lineup h((y CS-13 14A Core Spray Block 1 E NR Valve Lineup
    n. ((y CS-13-2 14B Core Spray Block 1
    E NR Valve Lineup l 4 h((y CS-3-1 8A CST Suctien. Block 2 E NR Valve Lineup i [*y CS-3-2 8B CST Suction Block-2 E NR Valve Lineup Hpr r RV-2056 66 Relief Valve 3 C IhV-3510 Setpoint IIPCI I!PCI-18 130 C1g h'ater Return Check 3 C Q Exercise i FSAR Valve Valve Applicable AS"E Valve Test Request System Number No. Description Code Class Category Frecuency Test For Relief IPCI 50-2068 ?D-19 Ptep Discharge Isol 2 B Q Full Stroke-Time liPCI A0-23-1F A0-18 C1g htr Disch Check 2 C CSIQ Exercise !!PCI BD-207] ?D-21 Test retum to CST 2 B Q Full Stroke-Tirx l IPCI 3D-2067 10-20 Coolant Pump Disch. 2 B Q Full Stroke-Tim IIPCI CV-2065 41 Min Flow Bypass 2 B Q Full Stroke-Tirx f IFCI IPCI-42 62 Min Flow Bypass Check 2 C RR RR 7 IPCI RV-2064 34 Relief Valve 2 C IhV-3510 Setpoint f a
    (
    IIPCI IFCl-32 32 CST Suction Check 2 C Q Exercise
    a I
    IIPCI F0-2063 3D-17 CST Suction 2 B Q Full Stroke-Tire IIPCI 50-2062 3D-57 Torus Suction 2 B Q Full Stroke-Tizp f liPCI IPCI-31 61 Tores Suction Check 2 C FR RR 7 f liPCI FD-2061 3D-53 Torus Suction 2 B Q Full Stroke-Tire ? IFCI ITCI-33 33 Pump Suction Block 2 E NR Valve Lineup l IIPCI 3D-2034 !D-15 Steam Supply Isolation 1 A Q Full Stroke-Tire 4 IIPCI FD-2035 3D-16 Steam Outboard Isolatior 1 A Q FullStroke-Tide 4 IIPCI 5D-2036 50-14 Turbine Steam Supply 2 B Q Full Stroke-Tire IIPCI 10-7 10 Turbine Stop Valve 2 B Q Full Stroke 10 IFCI 10-8 1D Turbine Control Valve 2 B Q Full Stroke-Tire m _.... FSAR Valve Valve Applicable ASME Valve Test Request System Number No. Description Code Class Categorv Frequency Test For Relief l Cooling hater Supply Cont. 2 B RR RR 14 IPCI PCV-3492 PCV-50 Cooling Water IPCI IIPCI-20 131 Retum Check 2 C Q Exercise IPCI ITCI-14 56 Ex. Line Drain Pot Check 2 AC RR RR 7, 4 l !!PCI IPCI-15 45 Ex. Line Drain Pot Check 2 C RR RR 7. IPCI IFCI-9 65 Turbine Ex. Line Check 2 AC Q Exercise 4 1 IFCI 1H 0 -10 12 Ex. Line Stop Check 2 C Q Exercise l ITCI le 1-69 None Vac. Pkr Check 2 C RR RR 7 i i f, IPCI IIPCI-67 None Vac. Ukr Check 2 C RR RR 7 ITCI PSD-2038 None Ex. Line Rupture Disc 2 D NR RCIC 50-2096 30-2096 Cooling Miter to Cond. 2 B Q Full Stroke-Tim RCIC RV-2097 RV-2097 Relief Valve 3 C IhV-351C Setpoint RCIC RCIC-14 None Condenser Cond Pump Disc 1 2 C Q Exercisc RCIC RCIC-17 None Vac Pump Disch Check 2 C RR .RR 7 l RCIC RCIC-9 None Turbine Exhaust Check 2 A,C Q Exercise 4 i f RCIC RCIC-10 None Steam Exh Stop Check 2 C Q Exercise h RCIC RCIC-57 None Vac Brkr Check 2 C RR RR 7 RCIC RCIC-59 None Vac Brkr Check 2 C RR RR 7 RCIC PSD-2089 PSD-2089 Rupture Disc 2 D NR FSAR Valve Valve Applicable AS4E Valve Test Request Systen Ntnber No. Description Code Class Category Frequency Test For Relief RCIC 3D-2075 3D-2075 Stemi Supply Isolation 1 A Q Full Stroke-Tirx 4 RCIC ?D-2076 3D-2076 Steam Supply Isolation 1 A Q Full Stroke-Tirx 4 PfIC 30-2078 3D-2078 Steam Supply to Turbine 2 B Q Full Stroke-Tire RCIC RCIC-7 None Throttle Trip Valve 2 B Q Full Stroke 10 RCIC 10 None RCIC Goreming 2 B RR RR 14 e RCIC PCV-2092 PCV-2092 Cor. denser Press Cont 2 B RR RR 14 RCIC RCIC-16 None Vac Pump Disch Check 2 A, C RR RR 4, 7 (f PflC 50-2100 50-2100 Inboard Torus Suction 2 B Q Full Stroke-Tirx ~" RCIC RCIC-31 None Check Valve to Torus 2 C RR RR 7 RCIC 3D-2101 3D-2101 Outboard Torus Suction 2 B Q Ftt11 Stroke-Tinc RCIC PfIC-41 None Check Valve to CST 2 C Q Exercise RCIC 30-2102 3D-2102 CST Suction 2 B Q Full Stroke-Tim RCIC RV-2103 RV-2103 QSertion Line Relief 2 C 1hV-351CSetpoint l RCIC CV-2104 CV-2104 Min Flow rypass 2 B Q Full Stroke-Tirx l PfIC RCIC-37 None Min Flow Pypass Check 2 C RR RR 7 RCIC 3D-2106 3D-2106 Punp Disclurge 2 B Q Full Stroke-Time RCIC 3D-2107 3D-2107 Pump Discharge 2 B Q Full Stroke-Tinc RCIC A0-13-22 A0-13-22 Punp Disch Check 2 C CSIQ Ekcrcise FSAR Valve Valve Applicable ASE Valve Test Request System Number No. Description Code Class Categorv Frequency Test For Relief RCIC 30-2110 FD-2110 Test Return to Cond Stor 2 B Q Full Struke-Tiro alve Lineup RCIC RCIC-32 Slone Pump Suction Block 2 E NR SELC XP-3-1 43A Pump Disch Check 2 C Q Exercise SBLC XP-3-2 43B Pump Disch Check 2 C Q Exercise SBLC XP-6 16 Outboard Isolation Check 1 A, C PR E 4, 13 SBLC XP-7 17 Inboard Isolation Check 1 A, C ER R 4, 13 SELC RV-11-39A 39A Relief Valve 2 C IhV-35105ctpoint 6 SBLC RV-11-393 39B Relief Valve 2 C IhY-3510Setpoint 1 SBLC 11-14A 14A Explosive Actu.ited Valve 2 D IhV-3610Actuation SBLC 11-14B 14B Explosive Actuated Valve' 2 D IhV-3610 Actuation i SBLC XP-17 i 41 Suction from Test Tank 2 E NR L'alve Lineup SBLC XP-20 None Suction Ileader Drain 2 E ?R L'alve Lineup SBLC DM-56 None Demin Water to Suction 2 E NR L'alve Lineup SBLC XP-13 26 Test Line Return 2 E NR L'alve Lineup SBLC XP-11-1 34 Pum.p Discharge Drain 2 E hR L'alve Lineup SBLC XP-18 None Poison Tank Drain 2 E AR Valve Lineup SBLC XP-1 11 Poison Tank Outlet 2 E NR L'alve Lineup SELC XP-2-1 12A Pump Suction Block 2 E NR l'alve Lineup FsxR I Valve Valve Applicable A9tE. Valve Test Request System h;riber No. Description Code Class 'Cate g Frequency Test For Relief SBLC XP-2-2 12B Purp Suction Block 2 E NR Valve Lineup SBLC XP-4-1 13A Purp Disch Block 2 E NR Valve Lineup i SBLC XP-4-2 13B Purp Disch Block 2 E NR Valve Lineup r SBLC XP-5 15 Injection ileader Block 2 E NR Valve Lineup 4 SBLC XP-8 18 Injection I! ender Block 1 E NR Valve Lineup CRD CV-3-32A CV-32A Scram Disch Volume Vent 1 B Q Full Stmke-Tim: CRD CV-3-32B CV-32B Scram Disch Volume Vent 1 B Q rull Stmke-Tin: ' T CRD CV-3-33 CV-33 Scram Disch Volume Drain 1 B Q Full Stroke-Tin deram Disch \\olume 4 CRD RV-3-34 34 Relief Valve 2 C IhT-3510 Setpoint CRD CRD-114 114 Scram Riser Check 2 C RR RR 9 Accumulator Chargmg CRD CRD-115 115 Water Check 2 C RR RR 9 CRD CRD-138 138 Cooling Water Check 2 C RR RR 9 t CRD CV-126 CV-126 Inlet Scram Valve 1 B RR RR 9 CRD CV-127 CV-127 Outlet Scram Valve 2 B RR RR 9 t. RIR SW CV-1728 CV-1728 RIR SN Control Valve 3 3 B Q Full Stroke-Tin RIR SW CV-1729 CV-1729 klR SW Control Valve 3 B Q Full Stroke-Tin: RIR-SW, RIR-SW ElR SW Pump RIR SW 1-1 1-1 Disch Check 3 C Q Exercise RIR-SW RIR-SW R1R SW Pun;, [ l RIR SW 1-2 1-2 Disch Check 3 C Q Exercise FSAR Valve Valve Applicable ASME Valve Test Request System Number No. Description Code Class Category Frecuency Test For Relief FJ R-SW-RIR-SW RIR SW Pu p RIR SW 1-3 1-3 Disch Ch t r-n Exerci se PJR-SW RIR-SW RIR SW Pt=p RIR SW 1-4 1-4 Disch Ch 3 r o ryerciso Pttp !btor Cooling RIR SW RV-3038 RV-3038 Line RV 3 C Thy-3sinscemint Pump Motor Cooling RIR SW RV-3039 RV-3039 Line RV 3 r Thy-v;1 nserm i nt Ptrp Motor Cooling PJR SW PCV-3004 PCV-3004 Line PCV 3 E RR. rm ta Pump 'btor Cooling RIR Si PCV-3005 PCV-3005 Line PCV 3 R RR RR 13 RIR SW AV-3147 AV-3147 Ptro Disch Air Vent 3 C 0 rycrcisn RIR SW AV-3148 AV-3148 Ptro Disch Air Vent 3 C 0 Exorcise i RIR SW AV-3149 AV-3149 Ptro Disch Air Vent 3 C 0 Evercise PJR SN AV-3150 AV-3150 Ptro Disch Air Vent 3 C D Exercise RiR SW SW-21-1 None 3btor Cooline Line Check 3 C PR 3R 7 PJR SW SW-21-2 None 3btor Cooline Line Check 3 C PR )R 7 RIR SN RV-3202 None RIR IN RV 3 C IhV-3510setmint RIR SW RV-3203 None RIR IN RV 3 C IhV-3510 3etmint Emerg Serv Wtr ESW-4-1 None S.W. Check Valve 3 C PR ?R 7 Emerg Serv Wtr ESW-4-2 None S.W. Check Valve 3 C PR 3R 7 Emerg Serv Ktr SW-101 None E.S.W. Check Valve 3 C RR 3R 7 Energ Serv Wtr SW-102 None E.S.N. Check Valve 3 C RR 3R 7 FSAR Valve Valve Applicable /SIE talve Test Request System Number No. Description Code Class Categorv Frequency Test For Relief Emerg Serv Wtr SW-103 None E.S.W. Check Valve 3 C RR RR 7 Emerg Serv Wtr SW-104 None E.S lf. Check Valve 3 C RR RR 7 Emerg Serv Wtr ESW-1-1 ESW-1-1 Pum Check Valve 3 L 0 Fm rcice Emerg Serv Wtr ESN-1-2 ESW-1-2 Ptro Check Valve 3 C 0 Fvarcise Emerg Serv Wtr SW-16 SW-16 E.S.W. Check Valve 3 C RR FR 7 Emerg Serv Wtr SW-18 SW-18 E.S.W. Check Valve 3 C RR RR 7 Emerg Serv Ktr AV-3155 AV-3155 Punp Disch Air Vent 3 C 0 Exercise Emerg ( Serv Ktr AV-3156 AV-3156 Ptro Disch Air Vent 3 C 0 Exercise n Emerg Serv Wtr ESW-3-1 ESN-3-1 Basket Strainer Bypass 3 E NR Valve Lineup Energ Serv Wtr ESW-3-2 ESW-3-2 Basket Strainer Evrass 3 E NR Valve Linetc Primary Containm. A0-2377 None Cont. Purne Isolation 2 A 0 Full Stroke-Tid 4 Primry Containm. A0-2378 None Tonts Purne Isolation 2 A 0 Full Stroke-Tim? 4 Prinarv
    ontain' n, AO-2379 None Torus Vac Nx Isolation 2
    A 0 Full Stroke-Tim 4 Primary
    ontainn.
    A0-2380 None Torus Vac Ekr Isolation 2 A 0 Full Stroke-Tim 4 Primry
    ontainm.
    A0-2381 None Drywell Purne Isolation 2 A 0 Full Stroke-Tim 4 Primary
    ontainm.
    A0-2383 None Torus Vent Isolation 2 A 0 Full Stroke-Tim 4 i'runarv
    ontainn.
    A0-2386 None Dnvell Vent Isolation 2 A 0 Full Stroke-Tim 4 i'runary
    onta iren.
    AO-2387 None Dnvell Vent Isolation 2 A Q Full Stroke-Tim 4 FSAR Valve Vale Applicable ASME Valve Test Request System Ntraber No. Description Code Class Catecorv Frequency Test For Relief Prinary Containm. AO-2896 None Torus Vent Isolation 2 A 0 Full Stroke-Time 4 Primary Sec Cont to Containn. DhV-8-1 None Ton's Vac Ekr 2 A. C 0 Exercise 4 Primary Sec Cont to l Containm. DhV-8-2 None Torus Vac F.kr 2 A. C 0 Exercise 4 e Primary Containm. CV-7436 None N7 Ptrmback Isolation 2 A O Full Stroke-Tim 4 Primary Contsinn. CV-7437 None N, Ptepback Isolation 2 A Q Full Stroke-Tim 4 Primary Containm. CV-2384 None Torus Vent Isolation 2 A Q Full Stroke-Tim 4 l Primary Containn. CV-2385 None Dnwell Vent Isolation 2 A O Full Stroke-Timc 4 Primary ' i' Containm. CV-3267 None Toms N, Makeup Iso. 2 A Q Full Stroke-Tinc 4
    Z Primary,
    CV-3268 None Drwell N2 Makeup Iso. 2 A 0 Full Stroke-Timc 4 Containe.' Finary Containm. CV-3269 None Cont N., Makeup Iso 2 A Q Full Stroke-Timc 4 Primary Containn. CV-3305 None Dnvell 02 Analy Iso 2 A Q Full Stmke-Tinc 4 Primary Containm. CV-3306 None Dnvell 07 Analy Iso 2 A Q Full Stroke-Tinc 4 Prima y Containm. CV-3307 None Drywell 02 Analy Iso 2 A Q Full Stroke-Timc 4 Primay Containm. CV-3308 None Dnvell 02 Analy Iso 2 A Q Full Stmke-Timc 4 Prima n-Containm. CV-3309 None Drywell 07 Analy Iso 2 A Q Full Stroke-Tinc 4 Primary Containn. CV-3310 None Drvwell 0; Analy Iso 2 A Q Full Stmke-Tinc 4 Primary Containm. CV-3311 None Drywell 02 Analy Iso 2 A Q Full Stroke-Tinc 4 Primary Containn. CV-3312 None D.ywell 02 Analy Iso 2 A Q Full Stmke-Time 4 FSAR Valve Valve Applicable ASE Valve Test Request System Number No. Description Code Class Categorv Frequency Test For Relief Primary nntnins CV-3313 None Drywell O, Analy Iso 2 A O Full Stroke-Time 4 Prirary nontnin CV-3314 None Drwell 0, Analy Iso 2 A 0 Full Stmke-Time 4 Primary -nnt ains CV-7440 None Torus to Drvwell N7 Iso 2 A 0 Full Stroke-Tine 4
    ond Serv System Dif-53 None Drvwell Denin Ktr Iso 2
    A FR RR
    4. 12 1PCCW 50-1426 BD-1426 Drvwell RPCCN Isolation 2
    A CSIO Full Stroke-Tim 4 IBCCW RPCC-15 None Drvwell RFCCW Isolation 2 A. C RR FR
    4. 6 1hRII 30-2397 30-2397 Pump Suction Isolation 1
    A Q Full Stroke-Tim 4 1WCU -3D-2398 BD-2398 Pump Suction Isolation 1 A 0 Full Stroke-Tim a Liquid Drywell Floor Drn Sep Iso 2 A Q Full Stroke-Tirn 4 bdwaste A0-2541A None Liquid bdwaste A0-2541B None Drywell Floor Drn Srp Isr 2 A 0 Full Stroke-Tire 4 Liquid L ladwaste A0-2561A None Drvwell D1uip Sunn Iso 2 A 0 Full Stroke-Tim 4 miquid Radwaste A0-2561B None Drwell Eauip Sump Iso 2 A Q Full Stroke-Tim 4 uel Pool ':1g 6 C1p PC-20-1 None Fuel Storage Pool Check 3 C RR RR 7 uel Pool -:1g S C1p PC-20-2 None Fuel Storage Pool Che:k 3 C RR RR 7
    omp Air CV-1478 CV-1478 Drvwell Como Air Iso 2
    A CSIQ Full Stmke-Time 4 ':omp Air CV-7956 None Torus Inst Air Iso 2 A Q Full Stroke-Time 4
    orn Air AS-39 None Service Air Iso 2
    A RR RR 4, 12 4 i Key For Valve Testing Table Q = Quarterly NR = Not Required i. RR = See request for relief ) 'CSIQ = Cold Slutdown, not more oftm than quarterly. IhV-3510 = In accordance with the requirmmts of paragraph IhV-3510. IhV-3610 = In accordance with the requirements of paragraph IhV-3610. l 4 . e 4 4 4 - e y - 4 y e . w -.a h. Fequests for Relief From AS4E Code Section XI Requirements Detemined to be Irpractical 1. RECUEST R)R RRTFW 034PONENT RRCTION APPLICABLE ASTE Q)DE CLASS 11, 12 Emergency Service Provide cooling water to the emergency 3 hter Pumps diesel generators and critical reactor building equipment. 11, 12, 13, 14 RIE Provide cooling water to the ElR 3 Service Water Pumps heat exchangers. i' 9 Code Requirement Inlet pressure and differential pressure will not be measured directly as required by IhP-3100 and Ih?-4213. Basis There is no installed instrumentation for directly measuring the inlet pressure and differential pressure of these punps. These ptmps are submerged and take suction several feet below the river level. Alternate Testing The river level elevation will be neasured to detemine the inlet pressure for these punps. Differential pressure will be detemined by taking the difference between the discharge pressure and calculated inlet pressure. Scheduled for Imnlementation Februar/ 28, 1978- me. ' e 9 4 - OL m I 2. Request for Relief OCNPONEhT FUNCTION APPLICABLE ASE CODE CLNSS 11, 12 Emergency Provide cooling water to the emergency 3 Service Water diesel generators and critical reactor building equipnent. I h 11, 12 Standby Provide a redundant means of reactor 2 Liquid Control shutdown as a backup to the Control 1 Rod Drive System. t l 11, 12 Core Spray Provide cooling water to the reactor 2 under emergency conditions. l 11, 12, 13, 14 Provide cooling water to the reactor 2 7 Residual Heat and to containment under accident m Removal conditions. 11, 12, 13, 14 Provide cooling water to the RIR heat 3 RIR Service Kater exchangers. High Pressure Provide cooling water to the reactor 2 Coolant Injection under emergency conditions. Reactor Core Provide cooling water to the reactor 2 Isolation Cooling under emergency conditions. Code Requirement Pump bearing temperature will not be measured as required by IhP-3100 and IhP-4310. Pasis 'Ihere is no instnnentation installed to measure lube oil or bearing temperature. The use of external temperature measuring devices is not considered meaningful because of the environmental influence on these parameters. ~ .s A i q 2. REGUEST FOR RELIEF (Cont'd.1 Alternate Testing-The mechanical condition of the ptrip will be assessed by using vibration data. Schedule for Implenentation February 28, 1978 3 U a. W' s 3. RffUEST FOR RELIE_F CmPONENT FUNCTION APPLICABLE CODE CIASS 1 11, 12 Emergency Provide cooling water to the emergency 3 Service Water diesel generators and critical reactor l Punps building equipment. 11, 12 Standby Provide a redundant means of reactor 2 Liquid Control shutdown as a backup to the Control Pumps Rod Drive System. 11,12 Core Provide cooling water to the reactor 2 Spray Pumps under emergency conditions. 11, 12, 13, 14 Provide cooling water to the reactor 2 Residual Heat and to containment under accident Removal Pumps conditions, 11, 12, 13, 14 Provide cooling water to the RHR heat 3 s-1- RIR Service exchangers. Water Pumps High Pressure Provide cooling water to the reactor 2 Cooling Injection under emergency conditions. Reactor Core Provide cooling water to the reactor 2 Isolation Cooling under emergency conditions. Code Requirment Displacement vibration amplitude will not be used to evaluate the condition of the ptrip as required by IWP-3110, 3210, 4500, 4510. Basis We prefer to measure vibration velocity due to its superiority in detecting wear and interior machine failure. ~ Alternate Testing Vibration velocity measurements will be used to evaluate the condition of the pump. Schedule for Implementation February 28, 1978 5 4 REQUEST FOR RELIEF Applicable Valve Cormonent Function ASIE Code Class Category All Category A Valves Containment Isolation 1, 2 A ( Code Requirement lhV 3420 will not be used to govern the cenduct of Category A valve leak rate testing. Basis Valve leak rate testing will be conoucted in accordance with Appendix J to 10CFR50 subject to NRC concurrence with planned modifications and NRC approval of exemptions from Appendix J (see letter from L. O, bbyer to Victor Stello, subject, " Planned Modifications to Pemit Testing to be Conducted in Accordance with 10CFR50, Appendix J", dated Fby 5,1976, and letter from L. O. 5byer to Victor Stello, subject, " Request for Excr:ption f from Certain Requirements of 10CFR50, Appendix J at Monticello", dated hby 5,1976). Appendix J to 10CFR50 imposes detailed and restrictive requirements on leak rate testing to assure containment integrity. Appendix J is recognized by the NRC and the utilities as the goveming regulation for containment leak rate testing. All Category A yt1ves are containment isolation valves. There is nothing to be gained by applying another leak rate test program to these valves. Alternate Testing-See Basis Schedule for Impicmentatien February 28, 1978 1 5. RIQJEST FOR RELIEF l Applicable Valve AS!E Code Class Category Function Corpenent Shutoff Recirc Pump #11 Upper Seal 2 B Flow hhen Punp is Shutdown Shutoff Recirc Pump #12 Upper Seal Flow 2 B hhen Pump is Shutdown Code Requiremeqt, These valves cannot be tested at the frequency required by IhV-3410 ) Basis These valves are located inside primary containment which has an inerted atmosphere. The only way to e 6. verify valve stroke and measure stroke time is by direct observation of the valve stem. I Alternate Testing i These valves will be full stroked and timed during each refueling outage when the Containment is de-inerted and open for general access. Schedule for Implementation Febt aary 28, 1978 { i i ,4 6. Request for Relief .A tj Applicable Valve Component Function A9IE Code Class Category RDCC-15 To provide containment isolation for the 2 A, C Reactor Building Closed Cooling water -4 drywell inlet line. .. s Code Requirement I This valve will not be exercised as required by IhV-3520. y ? Basis '0 There are no means provided for detemining that the disc travels to the seat promptly on cessation j - or reversal of flow. 4 Alternate Testing t This line will be modified upon concurrence of the NRC to allow leak testing of this valve (see letter I from L. O. Mayer to Victor Stello, subject, " Planned Modifications to Permit Testing to be Conducted in Accordance with 10CFR50,. Appendix J', dated May 5,1976). Proper seating of the valve disc will be
    f.
    verified during the'1eak rate test. ( i Schedule for Implementation See Alternate Testing. .5 I J .a'
    y. y,-,
    7. REQUEST FOR RELIEF J. Applicable AS4E Valve Component Function Code Class Category SW-101 Prevent flow of emergency service water 3 C into the nomal service water system SW-102 3 C: when the emergency serv. ice water syst m a Sf-103 is operating. 3 C Si-104 3 C ESW-4-1 Prevent reversal of flow into redundant 3 C emergency service water line. ESW-4-2 3 C FW-91-1 Prevent reversal of flow into the 2 C e ter system. FW-91-2 2 C RIR 8-1 Prevent reversal of ficw into RIR 2 C Pump Discharge Line. 7 RIR 8-2 2 C IIPCI-14 Prevent reversal of flow from 2 C IS "" IIPCI-15 2 C IIPCI-42 2 C IIPCI-31 Prevent reversal of flow from IIPCI Systen 2 C into Torus. IIPCI-69 Prevent ilPCI Exhaust Steam flow to 2 C . Torus Air Space. IIPCI-67 2 C RCIC-57 Prevent RCIC exhaust steam flow to 2 C Toms Air Space. 2 C RCIC-59 RCIC-37 Prevent Reversal of Flow from the 2 C Torus Into the RCIC System. RCIC-16 2 C FfIC-17 2 C RCIC-31 Prevent Reversal Flow of RCIC Flow 2 C to Torus. 1 l i i 7. RITAIEST FOR RELIEF (Cont'd.) Component Function Applicable ASE Valve Code Class Category SW-21-1 Prevent Reversal of Normal Cooling 3 SV-21-2 Flow Into the Service Water System. C 3 C SW-16 Prevent Reversal of Flow From 3 C SN-18 Emergency Service Water System Into Service Water System. 3 C PC-20-1 Prevent siphoning of Water From 3 C PC-20-2 uel Storage Pool Into Fuel Pool Cleanun System. ,3 C Code Requirement y These valves will not be tested as required by IhV-3520. Basis There is no means available to verify that the disc travels promptly to the seat on cessation or reversal of flow for nomally open valves or that the disc moves promptly away from the seat when the closing differential is removed and flow through the valve is initiated for nomally closed valves. Alternate Testing demonstrate proper operation.The systems in which these valves are located will be functionally tested on a p Schedule For Implementation N A. j 8. REQUEST mR RELIEF Applicable AR E Valve Code Class Category Function Cumponent 1 A, C FW 94-1 1 A, C To provide containnent isolation for Pd 94-2 the feedwater injection lines. 1 A, C FW 97-1 1 A, C FN 97-2 Code Requirement These valves will not be exercised as required by IhV-3520. Basis Verification that There are three check valves in series in each of the feedwater injection lines. i each valve disc travels to the seat promptly on cessation of flow cannot be completed by observing pressure 1 e The valves cannot 'oe directly observed and there is no instrumentation installed to monitor j o indications. disc position. Alternate Testing Proper seating of the valve disc will be verified during the valve leak rate testing. Schedule for Implementation February 28, 1978 r 9. REQUEST FOR RELIEF Applicable A9fE Valve Component Function Code Class Category CRD-114 Prevent scram discharge flow from 2 C flowing back into the CRD during a scram. CRD-115 Prevent scram accumulator pressure 2 C from discharging into CRD acctrnulator I charging water circuit during a scram. I 1 CRD-138 Prevent scram accumulator pressure from 2 C discharging into CRD cooling water circuit during a scram. CV-126 Provide scram accumulator pressure 1 B to the bottom of the control rod drive piston during a scram. CV-127 lixhaust scram discharge water from 2 B 7 the top of the control rod drive p piston during a scram. Code Requirement These valves will not be tested as required by IhV-3410 and IhV-3520. Basis The above listed valves are located on each of the 121 hydraulic control units. H ere is no practical method of testing these valves in accordance with Section XI requirements. There is no instnznentation installed to verify proper seating of the check valves and the control valves operate too rapidly to measure stroke time. Technical Specifications require all control rods to be scram tested once per operating cycle. R ese valves are all exercised one full cycle during a scram. Proper operation of these valves and the safety function of the control rod drive system are verified by the scram testing. Alternate Testing See Basis Schedule For Implementation February 28, 1978 4r
    10. RBQUEST FOR RELIEF Applicable ASE Valve Conponent Function Code Class Category ID-7 Imediately stop the steam flow to the 2
    B IIPCI Turbine. RCIC-7 Imediately stop the steam flow to the 2 B RCIC Turbine. Code Requirement These valves will not be stroke timed as required by IhV-3410. Basis These valves operate too fast to obtain meaningful stroke time. v-4, Alternate Testing ru These valves will be full stroked as required by IhV-3410 and proper operation will be verified. Schedule for Implementation February 28, 1978
    11. REQJEST FOR RELIEF Applicable ASME Valve Component Function Code Class Category RIR SW-17.
    Prevent reversal of flow c.f RIR water 2 C into RIR Service Water System. Code Requirement This valve cannot be exercised as required by IhV-3520. Basis Exercising of this valve would require pumping river water into the RIR System. 7 Alternate Testing U None [ hedule for Imp 1 mentation NA a
    12. REQUFAT FOR RELIEF Applicable ASME Valve Component Function Code Class Category IM-58 Shutoff demineralized water to drywell.
    2 A AS-39 Shutoff service air to drywell. 2 A Code Requirement These valves will not be tested as required by IhV-3410. -Basis These manual valves are nomally closed and will be tested as required by IhV-3410(f). e 4 Alternate Testing e See Basis Schedule For Implementation February 28, 1978 f i s a n 1
    13. REQUEST FOR RELIEF Applicable ASIE Valve Component Function Code Class Category XP-6 Prevent reversal of flow of reactor.,
    1 A, C water into SBLC System. yp,7 1 A, C Code Requirement These valves will not be exercised at the frequency required by IhV-3520. Basis Exercising of these valves can only be accomplished by initiation of the SBLC System, including actuation of an explosive valve, and pumping to the reactor vessel. Alternate Testing [ These valves will be exercised by initiation of the SELC System, actuating an explosive valve and ptunping demineralized water to the reactor vessel during each refueling outage. u Schedule For Implementation February 28, 1978 m-_. .m._ ^ 1 14. REQJEST FOR RELIEF Applicable ASME Valve Component Function Code Class Category 1 PCV-3004 Control PJiR Service Water motor 3 B cooling water pressure. 4 PCV-3005 3 3 10 Controls Steam Flow to RCIC Turbine. 2 B l PCV-2092 Controls Cooling Water Pressure to 2 B RCIC Barametric Condenser. ] PCV-3492 Controls cooling water pressure to 2 B 1 IIPCI Gland Seal Condenser. Code Requirement ] f~ These valves will not be tested as required by IhV-3410. 5 Basis No mears are provided for full stroke _ testing of these valves. l Alternate Testing These valves will be functionally tested during routine operability tests of their associated systems. Schedule For Implementation February 28, 1978 ^ -s 15. REQUEST FOR RELIEF -COMPONENT CODE EXAM CLASS TABLE ITEM CATEGORY i REACTOR VESSEL Longitud' nal and Circumferential Welds in Core Region 1 1.1 Bl.1 B-A j -1) i
    2) Iongitudinal and Circumferential. Welds in Shell (other than 1
    1.1 Bl.2 B-B' - B-A' and B-C) and Merididnal Welds in Bottom Head: 'I VIAA-1 &-2, VCBB-1 : &-3, and HMAB-1 through '-10 '3) Nozzle-to-Vessel Welds and Inside Radius: Standby. Liquid 1 1.1 Bl.4 B-D 3 f Control CPAD-1 J CODE REQUIREPENTS. . i'
    1) and 2) Volumetric examination of 107. of each longitudinal weld and 57. of each circumferential. weld
    ) y 4, will not.be performed as required by Exam Category B-A and B-B. 4
    3) Volumetric examination.of nozzle-to-vessel wald and inside radius will not be perfonned l
    as required by Exam Category B-D. BASIS The des.ign of the reactor' internals and the external biological shield and vessel insulation prevents.both internal and external access to these welds. _It should be noted that the Monticello reactorL vessel was fabricated.and subjected. to as-built inspection under' very demanding : specifications. Because the site was: " inaccessible to a river barge.of the capacity'necessary to transport a. fully assembled vessel, the. vessel was i. assembled at the site from' shop-fabricated subassemblies. All requirements of Section III of the ASPE Boiler
    and Pressure Vessel Code,.1965 Edition, including Addenda through Summer 1966, were satisfied.just as if the 1
    vessel'were shop fabricated. :In addition, additional. requirements more ' stringent than those ' required ! by the Code were applied by General Electric due'to the unique circumstances. surrounding the vessel fabrication.
    Refer to Volume VII'~of the Monticello Final' Safety Analysis Report, " Reactor Pressure Vessel Design Report " =for details concerning vessel fabrication and inspection..In addition, it should be noted:that: based on analysis of the dosimeter removed from the reactor vessel,:the maximum neutron fluence level at T/4 of the reactor vessel: wall vill be'only 1.23 x~1018nyt at - the end of designed life -(40 years). Based on'the high .qualityLlevel established for vessel fabircation and.the relative low neutron fluence level at the vessel. walli _ the' inability to examine these welds is not' considered to have any'significant decrease in safety. ^ a e n d -{ 7 h r %.v-- -,-i-4% w
    1. 4p-+4 m-
    . a. 15 REDUEST FOR RELIEF (continued) ALTERNATE As the result of their inaccessibility, no examinations will be performed on these welds, other than the vessel pressure tests. SCHEDULE FOR IMPLE}{ENTATION i ~f '1 February 28, 1978 .. t i i e b .I
    t V
    'L 8W 0 O [ l b W e ? .i 'I f d 1 A g l 16. IURUEST FOR RELIEF COMPONENT CODE EXAH CIASS TABLE ITEM CATECORY P REACTOR VESSEL
    1) Longitudinal and Circumferential Welds in Shell: VLCB-1, 1
    1. I*
    Bl.2 B-B VLCB-2, VLDA-1, VLDA-2, and VCBB-4
    2) Integrally Welded Vessel Stabilizer Lugs 1
    1.1 Bl.12 B-H e f CODE REQUIREMENT i
    1) Volumetric examination of 107. of each longitudinal veld and 5% of each circumferential veld will not be performed as required by Exem Category B-B.
    f
    2) Volumetric examination of the vessel stabilizer lugs will not be performed as required by Exam Category B-H.
    y_ O C BASIS The dcaign of the biological shield and vessel insulation prevents external access to these welds. Internal access is available but surface preparation of the vessel cladding would be required to provide dependable 2 ultrasonic results. Approximately 20 ft of cladding would need to be ground to permit the above-examinations. Our experience indicates that even after hydro lancing the vessel wall, and the use of a concrete plug over the core 8 and lead blankets on the wall for shielding, we could still expect personnel exposure to be in the 600-700 mr/hr I range. t Based on the high quality level of the Monticello vessel and the relatively low neutron fluence level that the vessel wall will see during its service life (refer to Request for Relief No. 15), we do not believe that exposure to personnel is warranted for the preparation and the performance of these examinations. Especially, j-since there are vessel welds at euch higher stress levels (such as the vessel and head flange welds, nozzle a welds, and head welds) that are being examined at greater'frequence and, thus, their exanination results should provide a sufficient means to measure the maintenance of vessel integrity. i, It should also be noted that for the integrally welded stabilizer lugs (Item 2), they are part of a mechanical snubber system for seismic loading and have no support function. Therefore, the examination of these lug welds is probably not within the scope of Section XI inservice inspection requirements. l ?g ~ I 16. REQtTEST FOR RELIEF (continued) ALTERNATE As the result of their inaccessibility, no examinations will be performed on these velds, other than the vessel pressure tests. SC11EDULE FOR IMPIBIENTATION February 28, 1978 V e IV O l
    • 1
    'l l ..i...... 17. REQUEST FOR RELIEF a CODE EXAM COMPONENT CIASS TAELE ITEM CATEGORY d, VESSEL PENETRATIONS l Control Rod Drive and Bottom Head Drain 1 1.1 Bl.S B-E t CODE REQUIREMENT The area surrounding each penetration cannot be visually examined for evidence of leakage during the vessel pressure test as required by Exam Category B-E. PASIS h The design of the vessel, the biological shield, and vessel insulation prevents access to these areas that are directly adjacent to the vessel penetrations. ALTERNATE 'Ihe areas below these penetrations will be visually examined for evidence of leakage during the vessel pressure test. SCHEDULE FOR IMPLEMENTATION February 28, 1978 t. I 18. REQUEST FOR RELIEF CODE EXAM COMPCNENT CIASS TABE ITEM CATEGORY -1 REACTOR VESSEL Closure Head Flange Leakage Sensors (Nozzle N-13 and N-14) 1 1.1 Bl.5 B-E J l CODE REQUIRDIEhT .c The area surrounding these two penetrations will not be visually examined for evidence of leakage durisg the [. vessel pressure test as required by Exam Category B-E. j BASIS 'Ty These penetrations never see pressure during either operation or vessel pressure test, unless the vessel flange o-rings leak. ALTERNATE e No examinations of these penetrations are scheduled. SCHEDULE FOR IMPETENTATION February 28, 1978 - =... =. - _ - m ......... _... ~. - 19. REQUEST FOR RELIEF CODE EXAM COMPONENT. CLASS TABLE ITEM CATECORY REACTOR VESSEL Standby Liquid Control Nozzle-to-Safe End Welds 1 1.1 Bl.6 B-E CODE REQUIREMENT .) The ultrasonic examination, and possibly the liquid penetrant examination, csnnot be performed for the total. weld as required by Exam Category B-E. BASIS The design of the biological shield prevents access to the bottom portion of this weld for ultrasonic examination. y Eo u ALTERNATE Effort will be made to ultrasonically examine as much of the veld as physically possible and to liquid penetrant examine the total weld, provided undue radiatien exposure will not result to personnel. SCHEDULE FOR IMPIDENTATION February 28, 1978 -ti m 1 20. REQUEST FOR RELIEF CODE EXAM COMPONENT CIASS TABLE ITEM CATECORY REACTOR VESSEL Closure Head Cladding 1 1.1 Bl.13 B-I-l CODE REQUIREMENT The liquid penetrant examination of the closure head cladding will not be scheduled as required by Exam Category B-I-1. BASIS From our past experience in liquid penetrant examining the Monticello vessel cladding, we have discovered that 7 the roughness of the closure head cladding e ults in considerable number of nonrelevant indications that required grinding to eliminate any possible masking effects. In addition, to assure success in the detect. ion of tight cracks, the cladding has a need to be ground to eliminate the oxides and crud that develop during service. The design stress analysis for the Monticello vessel did not take any credit for cladding thickness. The purpose of the cladding was to maintain water quality. It should be noted that many of the new BWR vessel designs have eliminated this cladding, and later editions of ASME Section XI Code has eliminated all requirements for the inspection of the closure head cladding. ALTERIMTE Visual examination will be performed on the closure head cladding. SCILEDULE FOR IMPLEMEIGATION Febntary 28, 1978 21. REQUEST FOR RELIEF 9 CODE EXAM COMPONENT CIASS TABLE ITEM CATEGORY Reactor Vessel Safe-end Welds 1 1.1 Bl.6 B-F Pipe Weld Inspection 1 1.4 B4.5 B-J 1 1.4 B4.6 B-J 1 1.4 B4.9 B-K 1 1.4 B4.1 B-F 2 2.2.1 C2.1 C-F 2 2.2.1 C2.1 C-G .2 2.2.1 C2.5 C-E-1 CODE REQUIREMENT T$ The ultrasonic examination method requirements (Appendix I of Section XI and Article 5 of Section V) of the Code Addenda.in effect will not be used to govern the ultrasonic examination procedures for the inspection of pipe welds and welds of ccanponents fabricated froa pipe components. BASIS The use of side drill holes (instead of slots) tc establish a distance amplitude correction curve (DAC) for pipe veld inspections, as required by Appendix.I of Section XI and Article 5 of Section V, results in an excessive instrument gain setting which greatly impairs the inspector's ability to detect and to interprete indications by producing a lower signal-to-noise ratio and reducing the range of useable DAC. ALTERNATE The rules of Appendix III, including Supplement 7, of _ the 1975 Winter and 1976 Summer Addenda to ASME Section XI Code will govern the ultrasonic examination method for the inspection of pipe velds and welds of components fabricated from pipe components. SCHEDULE FOR IMPLEMENTATION February 28, 1978 ~ 4 8
    s. )
    ^ .a- ) 22. REQUEST FOR RELIEF CODE EXAM COMPONENT CLASS TABLE ITEM CATEGORY. ? j Piping Socket Welds - Drain lines (REW28-2"-EF and REW29-2"-EF) of 1 1.4 B4.8 B-J l recirculation system A & B a 1 Valve Bonnet Bolting - Valves XR-6-1, XR-7-1, XR-6-2, and XR-7-2 1 1.6 B6.9 B-G-2 I CODE REQUIRFl!ENT The surface examination of the 2" socket welds and the visual examination of the valve bonnet bolting of these two drain lines were not scheduled for examination as required by Exam Category B-J and B-G-2, respectively. [ BASIS m These two, 2-inch drain lines are reading in excess of 2R/hr. The location of these lines prevents the use of shielding or distance to provide any significant reduction in radiation exposure to personnel. We have estimated. that exposure to inspection and insulating personnel would be in access of 1 man-rem for the examination of approximately four socket velds and the bolting of four valves. ALTERNATE These lines would be examined in accordance with the requirements of Exam Category B-P, upstream from and including their first isolation valve. S_0REDULE FOR IMPLEMENTATION February 28, 1978 m n l 2
    23. REQUEST FOR RELIEF 8
    CODE EXAM COMPONENT CIASS TABLE ITEM . CATEGORY , J Non-Welded' Piping and Valve Supports 1 1.4 B4.10 B-K-2' 2 2.2 C2.6
    C-E-2 4
    2 2.3 C3.4 C-E-2 2 2.4 C4.4 C-E-2 . IWD-2600(c) 3 4 CODE REQUIREMENT Examination Category B-K-2 and C-E-2 requires all areas of the. support component frce the piping, valve, ' and. pump attachment to and including the attachment to the supporting structure. Insulation will not be remnoved for' visual examination of these support components. y BASIS Ihe general radiation background field for the inspection of' Class 1 systems located within containment' ranges from 30 to 400 mR and.the Class 2 systems have permanent type of insulation (insulation not designed' for removal and.. replacement). 4 i It has been our experience that any loss.of support capability or inadequate restraint can usually be. detected through the inspection of the uninsulated portion of the support and the surrounding insulation. It is'our contention'that the removal and replacement of-insulation for the sole purpose of. inspecting Class I supports would result in undue radiation; exposure to personnel without providing significant increase in safety. The. governing Codes and Regulations used in the design and construction of those systems that~are now classified as Class 2 and 3 did not require provisions for inspection access for these systems., Thus, it would' be an undue, burden without compensating increase in safety to require insulation-removal for support ' inspection. : ' ALTERNATIVE. The ' insulation will= be removed from a supported component for further inspections whenever. an abnormality is. detected.that may have-been a result of a loss of support capability or inadequate restraint. SCHEDULE FOR IMPIIMENTATION 36: R@7F ..u... .x 24. REQUEST FOR RELIEF i CODE EXAM COMPONENT CIASS TABLE ITEM CATEGORY Pressure Boundary Bolts and Studs 1 1.5 B5.1 B-G-1 1 1.5 B5.2 B-C-1 2 2.3 C3.2 C-D 2 2.4 C4.2 C-D CODE REQUIREFEIT volumetric examination of bolts / studs 2 inch and larger will not have a DAC constructed (distance amplitude curve) as described in Article 5, Section V. 7 BASIS Es The variation in ultrasonic attenuation between bolts and/or studs diminishes the usefulness of a DAC generated from a particular test specimen. ALTERR\\TE Bolts and/or studs will be ultrasonically examined by longitudinal straight berm, utilizing the response from the thread roots or back reficctions as described in Northern States Power in-house approved procedures. SCHEDULE FOR IMPLEMENTATION February 28, 1978 ^ 6 L
    25. REQUEST FOR RELIFS ASEE COMPONENT FUNCTION Code Viv Class Cat
    - A11 Class 2 Components pressure retaining 2 CODE REQUIREMEhT The system pressure tests will not be distributed as required by IWC-2412. BASIS Scheduling system pressure tests in this manner is not practical as mechanisms are not available for isolation of f the piping systems at the various boundaries created by the NDE exmption criteria. Consequently numerous redun-g dant pressure tests will be perfomed whicham not warranted considering the operational problems (system valve lineups, leak off or over pressure protection, radiation exposure, generation of waste, etc.) involved. Addition-ally the majority of these systems are either normally pressurized or pressurized during the performance of a pump or valve functional test such that any system degradation would be immediately known. ALTERNATE INSFECTION (TESTING) .All' components will be pressure tested at or near the end of each inspection interval. This is consistant with proposed revisions (Winter 1976 Addenda) to ASME-XI. Subsection IWC and Section XI Subcommittee interpretation of C.1. ass 2 Pressure Test Requirements (attached). SCHEDULE FOR IMPLD4ENTATION February 28, 1978 25. Request for Relicf -(continued) ,'(;.N The A.merican Society of Mechanical Engineers 3 g United Engineering Center / 345 E. 47th St., New York, N Y. 10017 /212 644 7815 YHf 00lLER AND entuunt, vtv.st v.~vw a t, s 5 co,simun
    .s
    o t P. Zick v.c. cru,mua W.L HARDING
    '1ho liart ford Steam Boiler Inspection and Insurance Company 7n'I$vT 56 Prospect Street H Ilartford, Connecticut 06102 C W Atu$0N sW.sact Att: F.'T. Duba RO BONNER ^' p N.'en s'Ttn

    Subject:

    ASMC File #BC-76-418 H M CAN AVAN Section XI, Division 1, System Isressure Tests H.J Lts'LUCH , LJ cHOCKif

    Dear Mr. Duba:

    WI. cooper W O. DOTY G [ FR ATcHER Your inquiry of February 24, 1976 has been considered by the 3, gannison cogninant comrrit tee. We are responding to the following question: E.J HEM 2Y w.p. JOHN %oN yg g3m. E.t KEMMLEn-E.L MVE J E. t ATTAN

    1. Are System leakage tests required for Class 2 and Class 3' systems 7-J L',co
    2. Are systiem hydrostatic tests required for Class 2 and 3 systems?

    y $1 H LioE LLt H Tf NOUHUr REPLY: ct.nAwuNs $ " $$$t is*"'

    l. System Icakage tests are not required for Class 2 'and 3, components.
    2. System hydrostatic tests are required for. Class 2'and 3 components at or near the end o,f each inspection-interval. In addition, a system hydrostatic test is required on components which have been repaired by welding prior to returning the plant to service.

    Very truly y'ours, m' unt June Ling Nuclear Engi ing Administrator JL:lc R E C E IV E Da ENomrRwo i i9 2 ?. nib [ f. E. L KEMu.t.t,1 ".r Dr. g.4,,.. Member of Engincris Council for Professional Development and Engineers Joint Council 4-30 m 9

    • .m W -

    e.es 9 w r.2,vv ,-s-v e W r-* e e-e u-w v'e-,, v v-'s -w-

    1

    26. RMUEST FOR I0'LTU ASME COMPONENT FUNCTION Code Viv Class Cat i

    All Class 1, 2, and 3 Components pressure retaining 1,2,3 CODE REQUIREMENT Not all system pressure tests will be conducted for a minimum of four hours as required by IWA-5210(a). BASIS g This requirement is not practical nor meaningful'when perforlaing pressure tests of areas that are exposed for visual i -i examination. The four hour requirement is based on detection of leakage from insulated areas. Where areas are exposed for visual examination a shorter time period is justified. ALTERNATE INSPECTION (TESTIPC) Where areas of examination are not exposed, the test pressure and temperature will be maintained for a minimumi of four hours as_ required by IWA-5210(a). I Where areas to be examined are exposed for visual examination, the test pressure and temperature will be maintained for a minimum of ten minutes as established by IWA-5210(a) - Winter 1975 Addenda. SCHEDULE FOR IMPLDfENTATION February.28, 1978

    5 SECTION 5 - PROPOSED TECHNICAL SPECIFICATION CHANGE Reproduced in this Section are the proposed Technical Specification changes included in Northern States Power Company's License Amendment Bequest _ dated August 30, 1977. Pages

    • 11
    • iii
    • v
    • vii
    • 1x 88 89 90 94 96 97 98 99 100 101 102 103 104 105 106
    • 107 108A ilh 119 120
    • 122 - 129 (renumbered pages 121A - 123) 135 136 137
    • 138 lk6 151 152 189R (new page) 189S (new page) 189T (new page) i l'

    l-j

    • Tnese pages have not been reproduced.

    Changes made to these pages l involve only layout, numbering, and_the table of contents. 5-1 o

    -4 .-.c_. m. ?<. a, s 1 i e 1 3.0 LIMITING CONDITIONS FOR OPERATION .h.O SURVEILIANCE REQUIRD4ENTS - i j '3.4 STANDBY ' LIQUID CONTROL SYSTEM 4.h STANDBY LIQUID CONTROL SYSTD4 Applicability: Applicability: I AppliesL to the operating status of the Applies to the periodic testing require- -]' . standby liquid control system. ments for 'the' standby. liquid control system. ' 4 Objective: Obj ective: i 1 4-independent ' reaetivity control' mechanism. liquid control system. d To assure the availability of an To verify the operability of the ' standby 4 SPEX'IFICATION : SPECIFICATION: } A. Normal Operation A. 'Ihe opembility of the. standby liquidJ control. system shall be verified by' l ..1. The. standby liquid control system performance of the'following tests: .; g j. - shall be operable at-all times when J T < fuel -is in the reactor.and the-L:f reactor is not ' shutdown by -control.. 1. At.least once each operating cycle rods, except as.:specified in 3.4.B. manually initiate one of.the two ~ standby liquid control systems.and

    2. Each standby liq tid control ' system pump Pump. demineralized. water. into the

    .,1 . shall be. capable 3r delivering 24 gpm reactor vessel. Both systems shall-( - against -aIreactor pressure of 1275-psig, be tested and inspected in:the. 1 ~ course of two' operating cycles.:- ~3 ' The system pressure : relief valves shall' ~ be. operable with a setpoint.between. .s

    4

    .-1 50 and 1 50 psig.-

    88-F 34/4 A LhEVI

    j i 3.0 LIMITIIRG C0erDITIONS FOR OPERATION 4.0 SURVEILIANCE RDQUIRD4DffS

    2. Inservice inspection and testirg of components shall be conducted in d

    accordance with Specification 4.13 l 1 ) ~ 4 Y te B. Operation with Inoperable Componente B. Surveillance with Inoperable Componente Fmm and after the date that a mdundant When a component becomes inoperable, its component is ende or found to be inoperable, redundant coe snent shall be demonstruted Specification 3 4.A shall be conside md to be operable immediately and daily fulfilled, provided tint the component is the reafte r. returned to an operable condition within seven days. 89 34/4.4 REV

    I i %O LIMITING CONDITIONS FOR OPEFJTION hO SURVEILLLNCE RKUIR&M3 i C. Volume-Concentration Requireseents i C. The availability of the proper boron The liquid poison tank shall conta' ~ bearing solution shall be verified by a boron bearing solution that satisfies perfor=nnee of the ro14cving tests: the' volume-concentration requirenents 1. At least once N r month - of Figure 3.h.1 and at all times when the standby liquid poison system is re-quired to be operable the tempersture Baron concentration shall be detervined. In cdditi x, the boron shall not be less than the solution te-P-erature presented in Figure 3.4.2. In concentration shall be determined addition, the heat trscing on the punp any time water or baron are added suction lines shall be operable whenever or if the solution temperuture drops the room tempersture is less than the below the limits specified by u Figure 3.k.2. solution temperature presented in Figure 3.4.2. 1 I 3.4/h.4 99 REV l

    j Eases 3.4 and 4.4-V A. The design objective of the standby liquid control system is to provide the capability of bringing the reactor from full power to a cold, xenon-free shutdown assuming that none of the withdrawn con-trol rode can be inserted. To meet this objective, the liquid control system is designed to inject l a quantity of boron which produces a concentration of 900 ppm of boron in the reactor core in less than 125 minutes. 900 ppm boron concentration in the reactor core is required to bring the reactor from fuil power to a 37. o k suberitical condition considering the hot to cold reactivity swing, xenon poisoning and an additional 257. boron concentration margin for possible imperfect mixing of the chamaical solution in the reactor water and dilution from the water in the ecoldown circuit. A ministas net quantity of 1400 gallons of solution having a 21.47. sodium pentaborate concentration is required to meet this shut-down requirement. i he time requirement (125 minutes) for insertion of the borcn solution was selected to override the d rate of reactivity insertion due to cooldown of the reactor following the menon poison peak. The J msximum net storage volume of the boron solation is 2935 gallcas. ( 256 gallons are contained beJov the pump suction and, therefore, have not been used in the net quantities above.) 4 m 1 e \\ Boron concentration, solution te=perature, and volume (including check of tank heater and pipe l heat tracing system) are checked on a frequen, y to assure a high reliability of operation of the system should it ever be required. Experience with pu=p operability demoetrates that testin6 at a three-conth interval is adequate to detect if failures have occurred. Standby liquid control eyetms co ponente are insp-etad and tested in necordance with the requirewnts l of 10 CFR 50, Section 50 55a(g). These requirements are delineated in Specification 4.13 his inspection and testirc program, combined with the additional surveillance requirements contained in this section, provide a high degree of assurance that the standby liquid control system will perfor= as required when needed. The relief valves in the standby liquid control system protect the system piping and positive dis-- placement pumps which are nominally designed for 1500 psi from overpressure. The pressure relier valves discharge back to the standby liquid control solution tank. 3.4/4.4 BASES p arv

    S 4 30 LIMITING CONDITIONS FOR OPERATION k.O SURVEIIJX;CE REQUIRDE2iTS 4 3.5 CORE AND CONTAIDMENT COOLING SYSTOG k.5 CORE AND CONTAIf0E2rf COOLING SYSTDG Applicability: Applicability-Applies to the operational status of the energency cooling syste=s. Applies to periodic testing of the emergency cooling syste=s. Objective: Objective: To insure adequate cooling capability for heat removal in the event of a loss of coolant To verify the operability of the emergency cooling systems. accident or isolation frac: the nort:2al reactor heat sink. im Specification: Specifiestion: Iov Pressure Core Cooling Capability Low Pressure Core Cooling Capabilf ty A. Core Spray System A. Surveillance of the core spray system shall be performed as follows: 1. Except as specified in 3 5. A.2., 3.5. A. 3., and 3 5. A.S. below, both core 1. Boutine Testing spray subsystems shall be operable when-- ever irradiated fuel is in the reactor 1 vessel ani reactor coolant water t mpera-

    a. A simulated auto::ntic actuation test ture is greater than 21Y2F.

    shall te conducted each refueling outag?.

    b. Core spray headerap instrumentation shall be checked once each day, tested once each ::2enth, and calibrated once each 3-c:onth period.

    3 5/h.5 96 Rav

    ei 2# -m - ~ s I 3 1 4 ) i 1 ( i 30 LIMITING CONDITIONS FOR OPERATION - k.O SURVEIILANCE REQUIRIMENTS j i i l 1

    c. Inservice inspection and testing of components shall be conducted in accordsnee with Specification h.13 1

    's i 4 3 1 'f' + w 3 ' 2. From and after the date that one of the 2. When it is determined that one core core spray systems is mde or found to be spray system is inoperable, the opec- [ inoperable for any reason, reactor opern-able core spray system and the IECI i tion is permissible only during the suc-mode cf the RER system ard the diesel l ceeding fifteen' days:unless such system generators required for operation of is sooner mde operable, provided that-such components (if no external source during such fifteen-days all active cow of power were available) ah=11 be l nents of tne other core spray system and demonstrsted to be ' operable immedia-I' the. LPCI mode of the RHR system and the tely. The operable core spray system i-diesel generators required for operation shall be demonstrated to be_ operable l of such components (if no extermi source. daily thereafter. i-of power were available) shall be operable. 4 3 From and after the date that both core 3 When 'it is de' ermined that both core t spray systems' are made or found to be spray systems are inoperable, the inoperable for any reason, reactor IECI mode of the RHR system and the j; 3 5/h.5 'W c l-REV _ ~.. -,. ..~.. -.

    3 0. LIMITIIU CONDITICI!S FOR OPEPATIO'i L.O FtKEIIIAI:N FE;UIRD'.DITS operation is pemissible only during Ilesel generitors required fvr the succeedir4 seven days unless at operation of such coepenents (if least one of such systems is sooner no external source of power were mde operable, provided that during available) shall be deme:nstrated such seven days all active components to be cperable ir=ediately and of the LPCI mode of RHR system and the hily thereafter. diesel. generators required for operation of such components (if no extemal source of power were available) shall be opera-ble. k. Each core spray system shall be capable of delivering 3,020 gpm against a reactur Y pressure of 130 psig. If.this rate of delivery requirement cannot be met, the system shall be considered inoperable. S-If the requirements of 3 5.A.1 - 3 cannot be met, an ^ orderly shutdown of the reactor will be initiated and the reactor water temperstum shall be mduced to less than 212 0F vithin 2h hours. a 3 5/h.5 98 m

    a L 30 LIMITING CONDITIONS FOR OPEPATION h.O SURVEILIANCE REQUIRIMDITS B. Lov Pressure Coolant Injection (LPCI) Subsystem B. Surveillance of the Low Pressure Coolant (LPCI mode of EHR cystem) Injection (LPCI) Subsystem (LPCI mcmie of EHR cystem) chall be perfor=ed as follows: f 1. Except as specified in 3.S.B.2 and 3 5.B.3 below, the LPCI shall be operable

    1. Routine Testing whenever irradiated fuel is in the reactor
    a. A simulated autocntic actuation test i

    vessel and reactor coolant temperature is greater than 212 F. shall be conducted each refueltre outage. f 0 b. Inservice inspection and testirg of j components shall be conducted in accor: lance with Specification I.13 4 'T

    c. During each five year period, an air test shall be performed on the drywell l

    spray headers and nozzles. i 2. Frn: and after the date that one of the 2. When it is deterr.ined that one of the LPCI pumps or cdmission valves is made LPCI pumps is incperable, the rennining er found to be inopernble for any reason, active components of the LPCI and con-reactor operation is permissible orly tainment coolir4 subsystem, both core during the succeedirg thirty days unless spray systems and the diesel generators such pump or admission valve is sooner required for operation of such coe:ponents . rnde operable, provided that iurirg su-h (if na external source of power were l thirty dayu the r m ining active compenents wailable) chall be demonstrsted to be of the i D I and contairent x ; ling sub-uperable inmediately and the operable sya*,c=; and all a ctive e s p rmta >f both LPCI pumps laily thereafter. et.. spray rystems and tne dierel genera-tors required for operation ;f such com j ponents (if no external source of power [ were evn11able) shall be operable. 3 5/a 5 fgy

    .. ~. ~ i 30 LIMITING CONDITION 3 FOR OPERATION k.O SURVEILI/ dice REQUIRD4CETs 3 From and after the date that two of the 3 Wen it is detemined that the IECI LPCI pumps or admission valves are made subsystem is inoperable, both core or found to be inoperable for any reason, spray systems, the containment coolina i reactor cperation is pemissible only subsystem, and the diesel generstors during the succeeding seven days unless required for operation of such com-such pu=ps or admission valves are made ponents (if no external source of operable sooner, provided that during such power were available) shall be seven days all active components of both demonstrated to be operable immedi-core spray systems, the containment ately and daily thereafter. cooling subsystem (including 2 LPCI pumps) and the diesel generators required for 4 operation of such components (if no o external source of power were available) shall be demonstrated to be operable at least once each day. h. A maximum of one dryvell spray loop (containment cooling mode of RHR) may be inoperable for 30 days when the reactor water temperature is greater than 212 F. Jr tha loop is not returned to service within 30 days, the orderly shutdown of the reactor will be initiated and the reactor water temperature chall be reduced tn less than 212 F. 0 5 Each LPCI cubsystem (RHR) pump shall be cepble af ieliverirg h,000 gpm against - a reactor pressure of 20 psig. If this 3 5/h.5 100 REV ^

    \\ 3.0 LIMITING CONDITIONS FOR OPEPJCIrn L.O SURVEILIAUCE RE71IFCC.TS rate of delivery requirement cannot be met, the pu=p chall be considered inoper-able. 6. If the requirments of 3 5.B.1-4 cannot be met, an onlerly shutdown of the reactor vill be initiated and the reactor water t _rature chall be reduced to less then 212 F vithin 24 hours. Containment Cooling Capability m e Containment Cooling Capability W H C. Residual Heat Removal (RHR) Service khter C. Surveillance of the RHR service water System system shall be perfomed as follows: 1. Except as specified in 3 5.C.2 and 3.S.C.3 below, both RHR service water system loaps 1. Inservice inspection and testing of shall be operable whenever irradiated fuel con:ponents shall be conducted in is in the react 3r vessel and reactar coolant acconiance with Specification 4.13 temperature is grmter than 2120F. 2. From and a f ter the date that une of the 2. BHR service viter system pumps is made or When it is determined that one RHR found to be inaperable for any reason, service water pu=p is inoperable, the redundant coc:ponents of the 101 3 5/4.5 .~. ~ - ~

    Ja L 3 6 3.0 LDETIE CONDITION 3 FOR OPERATION k.O SURym1ANCE FREJIRDENTS t reactor operation is pemissible only reminir4 subsystem shall be during the succeeding thirty days unless demonstrated to be operable immedi-l such pump is sooner made operable, pro-ately and daily thereafter. vided.that during such thirty days all other active components of the RER service water system are opemble. 3 From and after the date that one of the 3 'w' hen one RHR service water system RER service water systems is made or found becomes inoperable, the opezeble ^ to be inoperable for any reason, reactor system shall be demonstruted to be' operstion is pemissible only during the opersble inmediately and daily t-succeeding seven days unless such system thereafter. is sooner made operable, provided that during such seven days all active co=po-y' nents of the operable EHR service water g system shall be demonstrated to be opers-ble at least once each day. h. To be considered operable, a RER service. vater ptanp shall be capable'or. delivering 3500 gpa against a head of 500 feet. 5 If the recuirements or 3 5.c.1-3 carmot i be met, an orderly shutdown of the reactor vill bc initiated and the reactor water ter:perature shall be reduced to less than 2120F vithin 24 hours. i' i 3 5/h.5 loe PAv 4 +-w, p m + ' +~, s e e N~-r m'- "w--,*-o-- v~ -er* "----w w

    I l l 3.0 LIIIlTING CO!!DITICI:3 FCR CPEFICICII L.O CURVEILLADCE FE:,UIFE"E.75 High Pressure Core Cooling Capabilit. iiirh Fressure Core Cooling capability i D. High Pressure Coolant In. ject ion (HFCI) Synten D. 3nrveillince of EPCI Systen shall te p rfar ed as follows: 1. Except as specified in 3.S.D.2 below, 1. Foutine Testirs the HPCI systen shall be operatle then-ever the reactor pressure is greater than

    n. A siz21sted automatic acttantion test 150 psig and irradiated fuel is in the shall be conducted each refueling reacter vessel.

    outage.

    b. Inservice inspection arxi testing of co::ponents shall be conducted

    ? in accordance with Sp=cification k.l~. Pw 2. From and after the data that tha HPCI 2. k' hen it is determined that HNI system is made or foun 1 to be ino;. arable system is inoperable, the RCIC system, for any reason, reactor operation is por-the LPCI rubsysten, an1 both af the care nissible only durin.- the succeedin ce.tn spray systens shsll be decionstrated days unless such :,ysten c: noonor rcile t o be gerable irred i ately. opera: Ic provi'Je_d th,*. !ur w h se. <_ n days all of the Aut', at i, Pr+ snure Relief system, the FCIC syrton, ieth of the core spray syatu r, wJ th-LPCI nl:.ystem 2n! contairc.ent coviinc r.O ie of the REF system are operable. 5.5/4.5 105 REV i

    . -, ~ M ~' 4 q l ~ !0 LIMITING CONDITIONS FOR OPEFATION 'k.O StJRVEIIIANCE REQUIRC4E*;TS i. 4 3 To be considered operable, the HPCI system shall meet the following conditions: 1 The HPCI shall;be capable of delivering a. l 3,000 spa into the reactor vessel for ' the reactor pressure range of 1120 psig 1-to 150 peig. - b. He condensate storage tanks shall j. contain at least 75,000 gallons of l ]- condensate water. u l- ]; #. c. The controls for autoentic transfer of the HFCI pucip suction from the l' condensate storage tank to the ]. suppression chamber shall be operable. k. If the requirements of 3 5.D.1-2 cannot be met, an orderly reactor shutdown shall be initiated innsediately and the' reactor ) pressure shall be reduced to 150 psig i within 2k hours thereafter. t E 7 e i I a 104 l .3 5/4.5 RW I

    t l l i I I I f -3.0 LIMITING CC'IDITIONS FOR OPERATIO;I 4.0 SUR'IEILLECE FEquIREMCITS L E. Automatic Pressure Belief System E. Surveillmace of the Automatic Pressure Belief System shall be performed as follows: j 1. Except as specified in 3 5.E.2 and 3 5.E.3 below, the entire auto :stie

    1. Poutire Testing I.

    pressure relief system shall be operable l at any time the reactor pressure is above

    a. A simulated automatic actuation 150 psig and irradiated fuel is in the test shall be conducted each oper-reactor vessel.

    ating cycle. j- [

    b. Once each operating cycle, valve oper-2.

    From and after the date that one of the ability shall be verified by cycling i-automatic pressure relief system valves is tne valves and observing a compensating rede or. found to be incperable for any change in turbine bypass valve position w .L reason, reactor cperation is permissible m' only during the succeeding seven days Inservice inspection and testing of c. unless such ' valve is sooner :cade operable, components shall be conducted in i accordance with Specification 4.13. provided that during such seven days both remaining autccatJ relief system l valves and' the HPCI system are operable. 3 From and after the date that more: than one of the automatic pressure relier valves are cade or found to be inoperuble l 1 for any reason, reacto* cperation 'is permissible only during the succeeding Een it is determined that one or 2. 5 24 hours unless repairs are made and more automatic preeeure relief welves provided that during such time the EFCI of the Automatic Pressure Relief a j system 1 gerable. system is inoperable, the RPCI system shall be demonstrated to be operable i

    k..If the requirements of 3.% E.1-3 cant.at I-diately and weekly thereafter.

    i be met, an orderly re. actor shutdown shall i be initiated immediately and the reactor shall be' reduced to 150 psig within 24 3 1 hours thereafter. ] 3 5/4.5 105 REV 4 0 e.. m

    3.0 LIMITING CCHDITION5'FGt OPEPATION k.O SURVEILIATE REQUIRDENTS F. -Reactor Core Isolation Cooling System (RCIC) F. Surveillance of Reactor Core Isolation Cooling System (RCIC) Surveillance of the RCIC System aball be perferned as follows: 1. Except as specified in 3.5.F.2 below, the

    1. Routine Testing RCIC-syste= shall be operable whenever the reactor pressure is greater than 150
    a. A simulated automatic actuation test

    ~ psig ani irradiated fuel is in the reactor shall be conducted each refueling outage. vessel. a. To be considered o;erable, the RCIC

    b. Inservice inspection aal testing of components shall be conducted system shall be capable of delivering 4

    LOO gpm into the rmetor vessel. in accordance with Specification 4.13 os 2. From and after the date that the RCIC sys-2. tem is taie or found to Le inoperable for k"nen it is determined that the RCIC sys-any reason, reactor operation is permissible tem is inoperable, the HPCI system shall only'during the succeeding 15 days unless be demonstrated to be operable inur.ediately such system is sooner cade oper able, provided and daily thereafter. that durin6 such 15 days all_ active compo-nents of the HPCI system are operable. 3. If the requirements of 3 5.F.1 - 2 cannot be met, an orderly ' shutdown of the reactor shall be: initiated immediately and the reactor pressure shall be reduced to 150 psig within 2h hours thareafter. g 35/4.5 RW

    7 -_. 3 3.0 LIMITING CONDITIONS FOR OPERATION 4.0 SURVEILIANCE REQUIREN.NTS 1. Recirculation System I. Recirculation System I 1. Except as specified in 3.5.1.2 below, whenever 1. Once per month, when irristed fuel is in the irradiated fuel is in the reactor, with reactor coolant temperature greater than 212*F and both reactor with reactor coolant temperature greater than 212 F and both reactor recirculation reactor recirculation pumps operating, the recirculation system cross tie valve inter 10cks pumps operating, the recirculation system crose shall be operable. tie valve interlocks shall be deemnetrated to be operable by verifying that the cros tie valves cannot be opened using the normel control 2. The recirculation system cross tie valve inter-switch. locks may be inoperable if at least one cross tie valve is maintained fully closed. w 2. When a recirculation system cross tie velve 4 interlock is inoperable, the position of at N least one fully closes cross tie velve shall 3. Valves in the equalizer' piping between the be recorded daily. recirculation loops shall be closed. Reactor operation with one loop shall be limited to 24 hours. 3 Inservice. inspection and testin6 of co:::ponents shall be conducted in accordance with Specification 1.13 4 3.5/4.5 108A REV

    ~ Bases 4.5: The testing interval for the core and containment cooling systems is based en a quantitative reliability analysis, judgment, and practicality. The core cooling systems have not been designed to be fully testable during operation. For exa~ pie, the core spray final admission valves do not open until reactor Pressure has fallen to 450 psig; thus, during operation even if hi h drywell pressure were simulated, the 6 final valves would not open. In the case of the HPCI, automatic initiation during power operation would result in pumping cold water into the reactor vessel, which is not desirable. The systems can be automatically actuated during a refueling outage and this will be done. To increase the availability of the individual components of the core and containment coolicg systems, the coagnmeents idrich make up the system, i.e., instrumentation, puarps, valve operators, etc., are tested more frequently. The instrumentation will initially be fitnetionally tested once per month until a trend is established and thereafter according to Figure k.1 (see Section 3.1/4.1) with an interval not greater then three months. Core and containment cooling system components are inspected and tested in accordance with the requirements of 10 CFR 50, Section 50 55a(g). These requirements are delineated in Specification cn 4.13 This inspection and testing program, co=bined with the additional curveillance requirements contained in this section, provide a high degree of assurunce that the core and contairment cooling systems will perfom as required when needed. i With components or subsystems out-of-service,. overall core and containment cooling reliability is main-tained by demonstrating the operability of the remaining cooling equipment. The degree of operability to be demonstrated depends on the nature of the reason for the out-of-service equipment. For routine i out-of-service periods caused by preventative maintenance, etc., the pump and valve operability checks will be performed to demonstrate operability of the remaining components. However, if a failure, design deficiency, etc., caused the out-of-service period, then the demonstration of operability should be thorough enough to assure that a similar problan does not exist en the remaining components. For example, if an out-of-service period were caused by fnilure of a pump to deliver rated capacity due to a desigrt deficiency, the other pm ps of tnis type might be subjected to a flow rate test in addition to the operability enecks. 4 4.5 BASES 114 REV

    ~.- 3.0 LIMITING CONDITIONS FOR OPERATION 4.0 StTRVEILIANCE REQUIREMENTS E. Safety / Relief Valves E. Safety / Relief Valves 1. Durin; power operating conditions and whenever 1. The inteerity of the safety / relief reactor coolant pressure is greater than 110 psig valve bellows shall be continuously and temperature is greater than 345 F : monitored. a. The safety valve function (self-actuation) o f

    2. The opembility of the bellows seven safety / relief valves shall be operable, monitorirg system shall be demonstrated at least once every three months.

    b. The solenoid activated relief function

    3. Inservice inspection ar4 testirg of

    ( Automatic Pressure Reller) shall be coc:ponents shall be conducted in operable as required by Specification accordance with Epecification I+.13 [

    3. % E.

    e l 1 I I 1 3.6/4.6 119 REV ^ ~ l l

    T^ 7' l I 3 0 - LIMITING CONDITIONS FOR OPEPATION k.0 SURVEILIANCE RB;lUIRDE:GS [ F. deleted F. deleted i + l i . [0. Jet Pumps G. Jet Pumps .o d. Whenever the reactor is in the Startup Whenever there is recirculation flow with the or Run modes, all Jet pumps shall be oper-reactor,in the Startup or Run modes, jet pump able. If it is ' determined that a jet pump is operability shall be checked daily by verify-inoperable, the plant shall be placed in a ing that all-the following conditions do not cold shutdown condition within 24 hours. occur simuftaneously: ~ 1. The two recirculation loop flows are unbalanced by 1% or more when the I recirculation pumps are operating at the same speed. 2. The indicated value of core flow. rate is 10% or more less than the value de-rived frors loop flow measurements. i 3,6/4.6 13 REV -w yr 4-' WY D-- P N

    • T'bb-

    vr-- Tr 1& 1----=--y, vg

    q 'l l Bases Continued 3.6 and h.6: h e safety / relief valves have two ibnctions; i.e. power ralief or self-actuated by high pressure. he solenoid actuated function (Autenatic Pressure Eelief) in which external instn=entation signals of coincident high dryvell pressure and low-low veter level initiate opening of the valves. This function is discussed in Specification 3 5.E. In addition, the valves een be operated manually. he safety function is performed by the same safety / relief valve with self-actuated integral bel. lows and pilot valve causing main valve cperation. Article 9 or the AmE Pressure vessel Code sec+ ion III Ihiclear Vessels requires that these bellows te menitored for failure since this would defeat the safety function of the safet.y/ relief valve. It is realized that there is no vay to repair or replace the bellows during creration and the plant must be shut down to do this. The thirty-day pariod to do this allovs the crerster flexibility to choose his time for shutdown; meenuhile, because of the redundancy present in the design and the continuin6 monitoring.of the integrity of 'the other valves, the overpressure pressure protection has not teen compro:mised. he auto-relief function vould not be impnited by a failure of the bellows. However, the self-actuated overpressure safety function vould be imp 91 red by such a f allure. w r0 P Provision also has been made to detect failure of the bellows monitoring system. Testin6 of this system quarterly provides assurance of bellows integrity. When the setpoint is being bench checked, it is prudent to disassenble one of the safety / relief ~ valves to examine for crud buildup, bendin6 of certain actuator members or other signs of possible deterioration. The program of earety/ relief valve testing confonts to the requirements of 10 CFR 50, rection 50 55a(g). hese requirements are delineated in Specification 4.13 . mis inspection and testing program, combined with the additional surveillance requirements contained in this section, provide a high degree of assurance that the safety / relief valves vill perform as required when needed. l 3.6/4.6 FAfEs 135 Pr.' I

    A Awmh eJ.a+..a -si-v -~h 4 -v1_-+-,,eAma-ass ry,, --u--m-a4AL,e---Lb 6,- fa K,s,-2,L 4uAu AL w--m%4 + 4, 1,w-9,--, b:. m W l P ? s i. s$ t t I b f 4 b I B L 44 N t 3 e. T m o UW T w p i. 3 G C T l f3 are +3 Q O A - c to g 60 w - t 1-5-22 In

    s - t j Bases Continued 3.6 and h.6: G. Jet pumps Failure of a ' jet pu=p nozzle assembly hold down mechanism, nozzle asse=bly and/or riser, would -increase'the cross-sectional flov area for blevdown following the design basis double-ended line break. 'lherefore, if a failure occurred, repairs must be made. The detection technique is as follows. With the two recirculation pu=ps talanced in speed to within + 5%, the flow rates in both recirculation locps vill be verified.by Control Roca =onitoring instru=ents. Tf the two. flow rate values do not differ by more than 10%, riser and nozzle assembly integrity has been verified. If they do differ by 10% or more, the core flow rate measured by the jet pu=p diffuser differential pressure system must be checked against.the core flow rate derived from the measured values of loop flow to core flov. correlation. If the difference betvaen measured and derived core flow rate is 10% or more (with the derived value higher) diffuser measurements vill be taken to define the location within the vessel of failed jet pu=p norzie (or riser) and the plant shut devn fer repairs. If the potential blevdown flow arco is increased, the system resistance to the recirculation picp is also reduced; hence, u r$) the affected drive pump vill '2mn out' to a substantially higher flow rate (approximately 115% to 120% for a single nozzle failura). If the two loops are balanced in flow at the same pu=p speed, the resistance characteristics cannot have changed. ' Any imbalance between drive loop flow rates vculd be indicated by the plant process -instr centation. In addition, the affected jet pep would provide a leakage path past - the core thus reducing the core flev rate. The reverse flow throuEh the insetive Jet pe p would still be indicated by a positive differential pressure but the_ riet effect vould be a slight decrease (3% to 6%) in the total core flow measured. 'Ihis decrease, together with the loop flov increase, would result in a lack of correlation between measured and derived core flev rate. -Finally, the affected jet pump diffuser ' differential pressure signal vould be reduced because the backflow would be less than the nomal forward flow. A nozzle-riser system failure could also generate the coincident failure of a jet pump body; benever, the converse is not true. The lack of any substantial stress in the jet pung body makes failure impossible - without an initial nozzle-riser system failure. 137 3 6/4.6 BASES FEV s %.m -r- -r m--- .,_m m

    n m ~ ~ a t 3.0 LIMITING CONDITIOIG FOR OPD1ATION h.0 SURVEILIRiCE PMUIRDETS 3 Pressure Suppression Chamber - 3 Pressure Suppression Charter - Reactor Building Vacuum Breakers Reactor Building Vacuum Breakers i 3 Except as specified in 3.7.A.3.b a. a. The pressure suppression chamber-reactor below, two pressure suppression building vacuum brerkers and associated in-chamber-reactor building vacuum strumentation including set point shall be i breakers shall be operable at all checked for proper operation every three times when the primary containment months. integrity is required. The set i point of the differential pressure b. Inservice inspection and testing of instrumentation which actuates the components shall be conducted in w pressure suppression cha*ar-reacter accordance with specification 4.13. /u building vacuum breakers chall be

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    o.5 psi. b. From and after the date that one of the pressure suppression chamber-reactor building vacuum breakers is made or found to be inoperable f or any reason, reactor operation is permissible only during the suceed-ing seven days unless such vacuum breaker is sooner made cperable, provided thst the repair procedure does not violate primary cent lintent integrity. Ik6 REV 3.7/4.7

    ~ ~ .. ~, e p .n s .) 4 3.0 LIMITING CONDITIONS FOR OPFRATION h.O SURVEILLAIICE FIQUIRENS d. The fbel cask or irradiated fuel is not being moved within the reactor building. D. Primary Containment Isolation Valves D. Primary Containment Isolation Valves 1. During reactor power operating conditions, 1. The primary contairment isolation valves all isolation valves listed in Table 3.7.1 surveillance shall de performed as follows: and all primry system instru lent line 4 flow check valves shall be operable except At least once per operatira; cycle the a. vi as specified in 3.7.D.2. operable isolation valves that are power operated and autocatically initiated shall be tested for simulated auto atic initiation and closure times, b. Inservice inspection and testing of components shall be conducted in accordance with Specification 4.13. 3.7/4.7 131 Rsv

    j 3.0 LIMITDIG CO!iDITIO*iG FOR OPEPATION k.O SURETIJAICE FMUIREMDCS Y Pn 2. In the event any isolation valve specified 2. Whenever an isolation valve listed in in Table 3.7.1 becomes inope rab le, reac tor operation in the run mode may continue Table 3.7.1 is inoperable, the position or provided at least one valve in each line at least one ibily closed valve in each line having an inoperable valve is closed. having an inoperable valve shall be recorded daily. 3. If Specifica tion 3. 7.D.1 and 3.7.D.2 cannot be met, initiate norr.a1 orderly shutdown and have reactor in the cold shutdown condition within 24 hours. 3.7/4.7 IW av 4

    J 30 LIMITIIU C0!;DITIO?C FOR OPERATION h.0 SUFIEILIANCE REQUIREMENI'S 3 13 INSERVICE IfCPECTION A?D TESTIIG h.13 INSEH7 ICE IIiSPECTION AND TESTIIU Applicability: Applicability: Applies to components which are part of Applies to the periodic inspection and the reactor coolant pressure boundary and testing of components which are part of their supports and other safety-related the raaetor coolant pressure boundary pressure vessels, piping, pu=ps, and and their supports and other safety-valves. related pressure vessels, piping, pumps, and valves. Objective: Objective: To assure the integrity of the reactor To verify the integrity of the reactor coolant pressure boundary ruxl the coolant pressure boundary and the w -6 operational readiness of safety-related operational readiness of safety-N pressure vessels, piping, pumps, and related pressure vessels, pipin6, pumps, valves. and valves. t Specification: Soecification: i A. Inservice Inspection A. Inservice Inspection la To be considered operable, Quality

    1. Inservice inspection of Quality l

    Group A, B, and C components shall Group A, B, and C components shall l satisfy the requiraments contained be perfomed in acconlance with l in Dection XI of the ASME Boiler the requirements for ASME Code Class l and Pressure Vessel Code and appli-1, 2, and 3 components, respectively, cable Mdend t for continued service contained in Section XI of the ASME of ASME Code Class 1, 2, and 3 compo-Boiler and Pressure Vessel (: ode and nents, respectively, except where applicable Addenda as required by relier has been requested from the 10 CFR 50, Section SO.55a(g), except Conmission pursuant to 10 CFR 50, where relief has been requested from Seetion 50 55a(g)(6)(1), the Comission pursuant to 10 CFR 50, Section 50 55a(g)(6)(1), 3 13/h.13 189R REV J l

    A 30 LIMITUU 00NDITIONS FOR OPEFATION h.O SURVEIIJANCE IEQUIRD4ENIS B. Inservice Testing of Pu=ps and Valves B. Inservice Testirg of Pms and Valves 1. To be considered operable, Quality

    1. Inservice testing of Quality Group Group A, B, and C pu=ps and valves A, B, and C pu=ps and valves shall be l 4 shall satisfy the requirements cou-perfomed in accordance with the o>

    tained in Section XI of the AliME ik>iler requi m=ents for ASME Code Class 1, and Pressure Vessel Code and appli-2, and 3 pu=ps and valves, respectively, cable Addenda for operability of contained in Section XI of the ASME ASME Code Class 1, 2, and 3 pumps Boiler and Pressure Vessel Code and and valves, respectively, except applicable Addenda as required by where relief has been requested from 10 CFR 50, Section 50 55a(g), except the Commission pursuant to J O CFR 50, where relief has been requested from Section 50 55a(g)(6)(1). the Co= mission pursuant to 10 CFR 50, Section 50 55a(g)(6)(i). 313/h.13 189s REV

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