ML17263A210: Difference between revisions

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| number = ML17263A210
| number = ML17263A210
| issue date = 04/05/1993
| issue date = 04/05/1993
| title = Proposed TS Table 3.6-1, Containment Isolation Valves.
| title = Proposed TS Table 3.6-1, Containment Isolation Valves
| author name =  
| author name =  
| author affiliation = ROCHESTER GAS & ELECTRIC CORP.
| author affiliation = ROCHESTER GAS & ELECTRIC CORP.
Line 17: Line 17:


=Text=
=Text=
{{#Wiki_filter:Attachment A Revise the Technical Specification pages as follows:
{{#Wiki_filter:Attachment A
Remove             Insert.
Revise the Technical Specification pages as follows:
3.6-4               3.6-4 3.6-6              3.6-6 3.6-7A              3.6-7A 3.6-10              3.6-10 P'DR 9'304090209 930405 PDR   ADOCK,05000244
Remove 3.6-4 3.6-6 3.6-7A 3.6-10 Insert.
3.6-4 3.6-6 3.6-7A 3.6-10 9'304090209 930405 PDR ADOCK,05000244 P'DR


TABLE 3.6-1 CONTAINMENT ISOLATION VALVES MAXIMUM                    MAXIMUM/
TABLE 3.6-1 CONTAINMENT ISOLATION VALVES PENT.
PENT.                                               ZSOLATZON        ISOLATION      ISOLATION ISOLATION TIME NO.           IDENTIFICATION/DESCRIPTION           BOUNDARY        TIME *(SEC)      BOUNDARY    *(SEC) 29  Fuel Transfer tube                             flange              NA    (1)                NA 100 Charging line to "B" loop                     CV 370B              NA    (2)                NA 101 SZ Pump 1B discharge                           CV 889B              NA    (5)                 NA CV 870B              NA    (5)                 NA 102 Alternate charging to "A" cold leg             CV 383B              NA    (2)                NA 103 Construction Fire Service Water               welded flange        NA    MV  5129            NA 105 Containment Spray Pump 1A                     CV 862A              NA    (3)                NA 106 "A" Reactor Coolant Pump (RCP) seal water     CV 304A              NA    (2) inlet 107 Sump A discharge to Waste Holdup Tank         AOV 1728            60    AOV 1723            60 108 RCP seal water out and excess letdown to     MOV 313              60    (4)                NA VCT 109 Containment Spray Pump 1B                     CV 862B              NA    (3)                NA 110 "B" RCP seal water inlet                       CV 304B              NA    (2)                NA 110 SZ test line                                 MV 879              NA    (5)                NA 111 RHR to "B" cold leg                         MOV 720 (20)        NA    (6)                NA 112 Letdown to Non-regen. Heat Exchanger           AOV 371             60     AOV 200A           60 AOV 200B           60 AOV 202             60 RV 203             NA 113  SZ Pump 1A  discharge                        CV 889A              NA    (5)                 NA CV 870A              NA    (5)                 NA 120  Nitrogen to Accumulators                      CV 8623              NA    AOV 846             60 120  Pressurizer Relief Tank  (PRT) to Gas        AOV 539              60    MV 546 (7)       NA Analyzer (GA)
NO.
29 IDENTIFICATION/DESCRIPTION Fuel Transfer tube 100 Charging line to "B" loop 101 SZ Pump 1B discharge 113 SZ Pump 1A discharge 120 Nitrogen to Accumulators 120 Pressurizer Relief Tank (PRT) to Gas Analyzer (GA) 102 Alternate charging to "A" cold leg 103 Construction Fire Service Water 105 Containment Spray Pump 1A 106 "A" Reactor Coolant Pump (RCP) seal water inlet 107 Sump A discharge to Waste Holdup Tank 108 RCP seal water out and excess letdown to VCT 109 Containment Spray Pump 1B 110 "B" RCP seal water inlet 110 SZ test line 111 RHR to "B" cold leg 112 Letdown to Non-regen.
Heat Exchanger ZSOLATZON BOUNDARY flange CV 370B CV 889B CV 870B CV 383B welded flange CV 862A CV 304A AOV 1728 MOV 313 CV 862B CV 304B MV 879 MOV 720 (20)
AOV 371 CV 889A CV 870A CV 8623 AOV 539 MAXIMUM ISOLATION TIME *(SEC)
NA NA NA NA NA NA NA NA 60 60 NA NA NA NA 60 NA NA NA 60 ISOLATION BOUNDARY (1)
(2)
(5)
(5)
(2)
MV 5129 (3)
(2)
AOV 1723 (4)
(3)
(2)
(5)
(6)
AOV 200A AOV 200B AOV 202 RV 203 (5)
(5)
AOV 846 MV 546 (7)
MAXIMUM/
ISOLATION TIME
*(SEC)
NA NA NA NA NA NA NA 60 NA NA NA NA NA 60 60 60 NA NA NA 60 NA


MAXIMUM                        MAXIMUM/
Pg PENT.
Pg PENT.                                                 ZSOLATION        ISOLATION      ISOLATION      ISOLATION TIME NO             IDENTIFICATION/DESCRIPTION           BOUNDARY        TIME *(SEC)      BOUNDARY          *(SEC) 141  RHR-tl pump suction from     Sump B             MOV 850A (13)       NA    MOV   851A (13)         NA 142  RHR-g2 pump suction from    Sump B            MOV 850B  (13)     NA    MOV   851B (13)         NA g
NO 141 142 g0 143 IDENTIFICATION/DESCRIPTION RHR-tl pump suction from Sump B
0  143  RCDT pump  suction                            AOV 1721            60    AOV 1003A               60 AOV 1003B               60 201 Reactor Compart. Cooling Unit A       & B       MV 4757  (16)      NA MV 4636  (16)      NA 202 "B" Hydrogen recombiner     (pilot & main)   MV 1076B            NA    SOV-IV-3B        NA Normally Closed MV 1084B            NA    SOV<<ZV-5B        NA Normally Closed 203 Contain. Press. Transmitter PT-947       & 948 PT 947              NA    MV 1819C                NA PT 948              NA    MV 1819D                NA 203 Post accident   air sample to "B" fan         MV 1563              NA    MV  1565                NA MV 1566              NA    MV  1568                NA 4P  204 Shutdown Purge Supply Duct [Purge Supply       flange (22)      NA  [5]  AOV 5869    (22)
RHR-g2 pump suction from Sump B
Duct]                                          [AOV 5870]
RCDT pump suction ZSOLATION BOUNDARY MOV 850A (13)
I 205 Hot leg loop sample                             AOV 966C            60    MV 956D  (14)          NA 206 Przr. liquid space sample                       AOV 966B            60    MV 956E (14)            NA 206 "A" S/G sample                                 AOV 5735            60    (17)                    NA 207 Przr. Steam space sample                       AOV 966A            60    MV  956F                NA 207 "B" S/G sample                                 AOV 5736            60    (17)                    NA 209 Reactor Compartment. Cooling Units A       & B MV 4758 (16)       NA                              NA MV 4635 (16)       NA                             NA 210  Oxygen makeup  to  A & B recombiners          MV 1080A            NA    SOV   ZV-2A     NA Normally Closed SOV   IV-2B     NA Normally Closed 0
MOV 850B (13)
AOV 1721 MAXIMUM ISOLATION TIME *(SEC)
NA NA 60 ISOLATION BOUNDARY MOV 851A (13)
MOV 851B (13)
AOV 1003A AOV 1003B MAXIMUM/
ISOLATION TIME
*(SEC)
NA NA 60 60 4P I
201 Reactor Compart. Cooling Unit A & B 202 "B" Hydrogen recombiner (pilot & main) 203 Contain. Press.
Transmitter PT-947
& 948 203 Post accident air sample to "B" fan 204 Shutdown Purge Supply Duct [Purge Supply Duct]
205 Hot leg loop sample 206 Przr. liquid space sample 206 "A" S/G sample 207 Przr.
Steam space sample 207 "B" S/G sample 209 Reactor Compartment.
Cooling Units A & B 210 Oxygen makeup to A & B recombiners MV 4757 (16)
MV 4636 (16)
MV 1076B MV 1084B PT 947 PT 948 MV 1563 MV 1566 flange (22)
[AOV 5870]
AOV 966C AOV 966B AOV 5735 AOV 966A AOV 5736 MV 4758 (16)
MV 4635 (16)
MV 1080A NA NA NA NA NA NA NA NA NA
[5]
60 60 60 60 60 NA NA NA SOV-IV-3B SOV<<ZV-5B MV 1819C MV 1819D MV 1565 MV 1568 AOV 5869 (22)
MV 956D (14)
MV 956E (14)
(17)
MV 956F (17)
SOV ZV-2A SOV IV-2B NA Normally Closed NA Normally Closed NA NA NA NA NA NA NA NA NA NA NA NA Normally Closed NA Normally Closed 0
0
0


PENT.
o'O.
o'O.
PENT.
O315 316 g0 317 318 319 320 IDENTIFICATION/DESCRIPTION Service Water from "C" fan cooler Service Water to "B" fan cooler Leakage test supply Dead weight tester (decomissioned)
IDENTIFICATION/DESCRIPTION ISOLATION BOUNDARY MAXIMUM ISOLATION TZME *(SEC)
Service Water from "A" fan cooler Service water to "C" fan cooler 4P I
ISOLATION BOUNDARY MAXIMUM/
321 A S/G Blowdown 322 B S/G Blowdown 323 Service Water from "D" fan cooler 324 Demineralized water to Containment 332 Cont. Press.
Trans.
PT-944, 949
& 950 ISOLATION BOUNDARY MV 4643 (16)
MV 4628 (16) flange welded shut MV 4629 (16)
MV 4647 (16)
AOV 5738 AOV 5737 MV 4644 (16)
CV 8419 PT 944 PT 949 PT 950 MAXIMUM ISOLATION TZME *(SEC)
NA NA NA NA NA NA 60 60 NA NA NA NA NA ISOLATION BOUNDARY (11)
(ll)
MOV 7443 welded shut (ll)
(11)
(17)
(17)
(11)
AOV 8418 MV 1819G MV 1819F MV 1819E MAXIMUM/
ZSOLATZON TIME
ZSOLATZON TIME
                                                                                              *(SEC)
*(SEC)
O315    Service Water from "C" fan cooler    MV  4643 (16)      NA      (11)                  NA g
NA NA Normally Closed NA NA NA NA NA NA NA NA NA NA 332 Leakage test and hydrogen monitor instrumentation lines MV 7448 MV 7452 MV 7456 SOV 921 SOV 922 SOV 923 SOV 924 NA NA NA NA NA NA NA cap cap cap (21)
316  Service Water to "B" fan cooler      MV  4628 (16)      NA      (ll) 0  317  Leakage test supply                  flange            NA     MOV  7443    NA Normally Closed 318  Dead weight tester (decomissioned)    welded shut        NA     welded shut          NA 319  Service Water from "A" fan cooler    MV  4629 (16)      NA     (ll)                  NA 320  Service water to "C" fan cooler      MV  4647 (16)      NA     (11)                  NA 321  A S/G Blowdown                        AOV 5738          60      (17)                  NA 322  B S/G Blowdown                        AOV 5737          60      (17)                  NA 323  Service Water from "D" fan cooler    MV  4644 (16)      NA      (11)                  NA 324  Demineralized water to Containment    CV 8419            NA     AOV 8418              NA 4P 332 Cont. Press. Trans. PT-944, 949 & 950 PT 944            NA      MV 1819G              NA PT 949            NA      MV 1819F              NA I
(21)
PT 950            NA      MV 1819E              NA 332  Leakage test and hydrogen monitor   MV 7448           NA     cap                  NA instrumentation lines                MV 7452            NA     cap                  NA MV 7456            NA     cap                  NA SOV 921            NA     (21)                 NA SOV 922            NA      (21)                 NA SOV 923            NA      (21)                 NA SOV 924            NA      (21)                 m       ~
(21)
(21)
NA NA NA NA NA NA m
~
0 0
0 0


(10) The pressure transmitter provides a boundary.
(10)
(11) Normally operating incoming and outgoing lines which are connected to closed systems inside containment and protected against missiles throughout their length, are provided with at least one manual isolation valve outside containment (FSAR 5.2.2 pg. 5.2.2-2).
(11)
(12) The single remotely controlled containment isolation valve is normally open and motor operated.     The cooling water return line is not directly connected to the reactor coolant system and, should remain open while the coolant pump is running. A second automatic isolation barrier is provided by the component cooling water loop, a closed system.       (FSAR 5.2.2 pg. 5.2.2-1a)
(12)
(13) See FSAR Table 5.2.2-1 and Figure 5.2.2-2. Sump lines are in operation and filled with fluid following an accident.
(13)
Containment leakage testing is not required. The valves are subjected to RHR system hydrostatic test.
(14)
(14) Normally operating outgoing lines connected to the Reactor Coolant System are provided with at least one automatically operated trip valve and one manual isolation valve in series located outside the containment. In addition to the isolation valves, each line connected to the Reactor Coolant System is provided with a remote operated root valve located near its connection to the Reactor Coolant System.       (FSAR 5.2.2 pg.
(15)
(16)
(17)
The pressure transmitter provides a boundary.
Normally operating incoming and outgoing lines which are connected to closed systems inside containment and protected against missiles throughout their length, are provided with at least one manual isolation valve outside containment (FSAR 5.2.2 pg. 5.2.2-2).
The single remotely controlled containment isolation valve is normally open and motor operated.
The cooling water return line is not directly connected to the reactor coolant system and, should remain open while the coolant pump is running.
A second automatic isolation barrier is provided by the component cooling water loop, a closed system.
(FSAR 5.2.2 pg. 5.2.2-1a)
See FSAR Table 5.2.2-1 and Figure 5.2.2-2.
Sump lines are in operation and filled with fluid following an accident.
Containment leakage testing is not required.
The valves are subjected to RHR system hydrostatic test.
Normally operating outgoing lines connected to the Reactor Coolant System are provided with at least one automatically operated trip valve and one manual isolation valve in series located outside the containment.
In addition to the isolation
: valves, each line connected to the Reactor Coolant System is provided with a remote operated root valve located near its connection to the Reactor Coolant System.
(FSAR 5.2.2 pg.
5.2.2-1)
5.2.2-1)
(15) See FSAR Table 5.2.2-1 and Figure 5.2.2-17.
See FSAR Table 5.2.2-1 and Figure 5.2.2-17.
(16) The Serv'ice Water system operates- at a pressure higher than the containment accident pressure and is missile protected inside containment. Therefore, these valves are used for flow control only and need not be leak tested.
The Serv'ice Water system operates-at a pressure higher than the containment accident pressure and is missile protected inside containment.
(17) The S/G tubes and secondary side provide a closed system inside containment.
Therefore, these valves are used for flow control only and need not be leak tested.
(18) Fire Service Water will be used only to fight fires inside containment. AOV 9227 is closed during power operation. A containment isolation signal to automatically close this valve is not required because a spurious signal during a fire may be hazardous   to personnel   and may   impede fire   suppression activities.
The S/G tubes and secondary side provide a closed system inside containment.
(19) See FSAR Table 5.2.2-1 and Figure 5.2.2-16.
(18) Fire Service Water will be used only to fight fires inside containment.
(20) Containment leakage testing is not, required per L. D. White, Jr. letter to Dennis L. Ziemann, USNRC dated September 21, 1978.
AOV 9227 is closed during power operation.
3.6-10                         Proposed
A containment isolation signal to automatically close this valve is not required because a spurious signal during a fire may be hazardous to personnel and may impede fire suppression activities.
(19)
(20)
See FSAR Table 5.2.2-1 and Figure 5.2.2-16.
Containment leakage testing is not, required per L. D. White, Jr. letter to Dennis L. Ziemann, USNRC dated September 21, 1978.
3.6-10 Proposed


Attachment B Page 1 of 2 Attachment B The purpose   of this amendment is to revise several penetration listings in Technical Specification Table 3.6-1 to support an Integrated Leak Rate Test (ILRT) of the Ginna Station containment during the 1993 Refueling Outage. As a result of preparing for this test, RG&E determined that a discrepancy existed between the Technical Specifications and the NRC approved In-Service Test (IST)
Attachment B
Program. Currently, Technical Specification Table 3.6-1 identifies two manual valves (820 and 204A) as containment isolation valves (CIVs) for Penetration 112. As part of the third 10 year IST program submittal for Ginna Station, RG&E identified that valves 820 and 204A would be removed from the IST program since their pressure and containment isolation functions were being performed by valves 200A, 200B, and 202 (Reference a). The NRC accepted this change by Reference (b). Therefore, RG&E requests that Table 3.6-1 be changed to replace valves 820 and 204A with AOVs 200A, 200B, and 202. In addition, relief valve 203, which is located between containment isolation valves 200A, 200B, 202 and 371 for this penetration, will be added to the table. All five valves are currently in the Ginna Station Appendix J testing program. This change   will enable Penetration 112 to meet the explicit requirements of GDC 56. The current Table 3.6-1 Note 17 will also be deleted since it is no longer used.
Page 1 of 2 Attachment B
Technical Specification Table 3.6-1 also identifies a manual valve in series with an air-operated valve as the CIVs for Penetrations 206, 207, 321, and 322.     These penetrations contain the steam generator (S/G) blowdown and blowdown sample piping. RG&E requests that the manual valves be removed from Table 3.6-1 since the S/G tubes and secondary side provide one containment barrier. These penetrations will then be treated analogous to the main steam and feedwater lines which are of similar configuration. Table 3.6-1 Note 17 will then be revised and added to these four penetrations to reflect the use of the S/G tubes and secondary side as a containment boundary.
The purpose of this amendment is to revise several penetration listings in Technical Specification Table 3.6-1 to support an Integrated Leak Rate Test (ILRT) of the Ginna Station containment during the 1993 Refueling Outage.
Table 3.6-1 Note 7 will also be deleted from these four penetrations. This note was originally applied to the S/G blowdown lines since they penetrate the missile shield inside containment in order to reach the S/Gs. However, the NRC has approved the use of "leak-before-break" (LBB) with respect to large diameter Reactor Coolant System piping at Ginna Station (Reference c). The use of LBB excludes the consideration of the dynamic effects associated with postulated pipe ruptures per 10 CFR 50, Appendix A, GDC 4. In addition, plant walkdowns and a review of Systematic Evaluation Program (SEP) Topic III-S.A, Effects of Pipe Break on Structures, Systems, and Components Inside Containment, (Reference d) confirms that even though these four lines penetrate the missile shield, they are not susceptible to any high energy line sources.       This includes the affects of pipe whip and jet impingement. Therefore, the dynamic effects associated with any high energy line break inside containment does not require consideration with respect to the S/G closed system. The blowdown lines inside containment are also Seismic Category I and Safety Class 2. Consequently, the lines are considered missile protected based on their present location and have the necessary closed system design requirements.
As a result of preparing for this test, RG&E determined that a discrepancy existed between the Technical Specifications and the NRC approved In-Service Test (IST)
Program.
Currently, Technical Specification Table 3.6-1 identifies two manual valves (820 and 204A) as containment isolation valves (CIVs) for Penetration 112.
As part of the third 10 year IST program submittal for Ginna Station, RG&E identified that valves 820 and 204A would be removed from the IST program since their pressure and containment isolation functions were being performed by valves 200A, 200B, and 202 (Reference a).
The NRC accepted this change by Reference (b).
Therefore, RG&E requests that Table 3.6-1 be changed to replace valves 820 and 204A with AOVs 200A, 200B, and 202.
In addition, relief valve
: 203, which is located between containment isolation valves
: 200A, 200B, 202 and 371 for this penetration, will be added to the table.
All five valves are currently in the Ginna Station Appendix J testing program.
This change will enable Penetration 112 to meet the explicit requirements of GDC 56.
The current Table 3.6-1 Note 17 will also be deleted since it is no longer used.
Technical Specification Table 3.6-1 also identifies a manual valve in series with an air-operated valve as the CIVs for Penetrations
: 206, 207,
: 321, and 322.
These penetrations contain the steam generator (S/G) blowdown and blowdown sample piping.
RG&E requests that the manual valves be removed from Table 3.6-1 since the S/G tubes and secondary side provide one containment barrier.
These penetrations will then be treated analogous to the main steam and feedwater lines which are of similar configuration.
Table 3.6-1 Note 17 will then be revised and added to these four penetrations to reflect the use of the S/G tubes and secondary side as a
containment boundary.
Table 3.6-1 Note 7 will also be deleted from these four penetrations.
This note was originally applied to the S/G blowdown lines since they penetrate the missile shield inside containment in order to reach the S/Gs.
However, the NRC has approved the use of "leak-before-break" (LBB) with respect to large diameter Reactor Coolant System piping at Ginna Station (Reference c).
The use of LBB excludes the consideration of the dynamic effects associated with postulated pipe ruptures per 10 CFR 50, Appendix A, GDC 4.
In addition, plant walkdowns and a review of Systematic Evaluation Program (SEP) Topic III-S.A, Effects of Pipe Break on Structures,
: Systems, and Components Inside Containment, (Reference d) confirms that even though these four lines penetrate the missile shield, they are not susceptible to any high energy line sources.
This includes the affects of pipe whip and jet impingement.
Therefore, the dynamic effects associated with any high energy line break inside containment does not require consideration with respect to the S/G closed system.
The blowdown lines inside containment are also Seismic Category I and Safety Class 2.
Consequently, the lines are considered missile protected based on their present location and have the necessary closed system design requirements.


Attachment B Page 2 of 2 RG&E will also   eliminate 10 CFR 50 Appendix J testing related to the four AOVs for Penetrations 206, 207, 321, and 322 since there are not any requirements to perform this testing. Instead, RG&E will hydrostatically test these valves in accordance with 'the original requirements as outlined in the approved third 10 year IST program for Ginna Station (IWV-3421 through 3425) as a minimum.
Attachment B
This will provide the necessary assurance that the valves will perform their required isolation function. These changes will be documented in the Ginna Station IST Program which will be submitted to the NRC following the conclusion of the 1993 Refueling Outage since RG&E expects to make several other unrelated IST Program changes at that time. These changes will not require NRC approval prior to implementation.
Page 2 of 2 RG&E will also eliminate 10 CFR 50 Appendix J testing related to the four AOVs for Penetrations
In accordance with     .10 CFR 50.91, these changes to the Technical Specifications have the  facility in been evaluated to determine if the operation of accordance with the proposed amendment would:
: 206, 207,
: 1. involve   a   significant increase     in the probability or consequences     of an accident previously evaluated; or
: 321, and 322 since there are not any requirements to perform this testing.
: 2. create the possibility of a new or different kind of accident previously evaluated; or
: Instead, RG&E will hydrostatically test these valves in accordance with 'the original requirements as outlined in the approved third 10 year IST program for Ginna Station (IWV-3421 through 3425) as a minimum.
: 3. involve a significant reduction in a margin of safety.
This will provide the necessary assurance that the valves will perform their required isolation function.
These proposed changes         do not increase     the probability or consequences of a previously evaluated accident or create a new or different type of accident. Furthermore, there is no reduction in the margin of safety for any particular Technical Specification.
These changes will be documented in the Ginna Station IST Program which will be submitted to the NRC following the conclusion of the 1993 Refueling Outage since RG&E expects to make several other unrelated IST Program changes at that time.
These changes will not require NRC approval prior to implementation.
In accordance with.10 CFR 50.91, these changes to the Technical Specifications have been evaluated to determine if the operation of the facility in accordance with the proposed amendment would:
1.
involve a
significant increase in the probability or consequences of an accident previously evaluated; or 2.
create the possibility of a new or different kind of accident previously evaluated; or 3.
involve a significant reduction in a margin of safety.
These proposed changes do not increase the probability or consequences of a previously evaluated accident or create a new or different type of accident.
Furthermore, there is no reduction in the margin of safety for any particular Technical Specification.
The detailed changes are described in Attachment C.
The detailed changes are described in Attachment C.
Therefore, Rochester Gas and Electric submits that the issues associated with this Amendment request are outside the criteria of 10 CFR 50.91; and a no significant hazards finding is warranted.
Therefore, Rochester Gas and Electric submits that the issues associated with this Amendment request are outside the criteria of 10 CFR 50.91; and a no significant hazards finding is warranted.


==References:==
==References:==
 
(a)
(a)   Letter from R.C. Mecredy, RG&E, to A.R. Johnson, NRC,  
Letter from R.C. Mecredy, RG&E, to A.R. Johnson, NRC,  


==Subject:==
==Subject:==
Inservice Pump and Valve Testing Program, dated May 23, 1989.
Inservice Pump and Valve Testing Program, dated May 23, 1989.
(b) Letter from A.R. Johnson, NRC, to R.C. Mecredy, RG&E,  
(b)
Letter from A.R. Johnson, NRC, to R.C. Mecredy, RG&E,  


==Subject:==
==Subject:==
 
R.E.
R.E. Ginna Nuclear Power P1ant IST Program for Pumps and Valves, 1990-1999 Third 10-Year Interval, dated April 15, 1991.
Ginna Nuclear Power P1ant IST Program for Pumps and
(c)   Letter from D. DiIanni,       NRC, to R. Kober, RG&E,  
: Valves, 1990-1999 Third 10-Year Interval, dated April 15, 1991.
(c)
Letter from D. DiIanni, NRC, to R.
: Kober, RG&E,  


==Subject:==
==Subject:==
Resol uti on of USI'-2, "Asymmetric LOCA Loads ",
dated September 9,
1986.
(d)
NUREG-0821, Integrated Plant Safety Assessment Systematic Evaluation Program, R.E.
Ginna Nuclear Power Plant, December 1982.


Resol uti on of USI'-2,         "Asymmetric  LOCA  Loads ",   dated September    9, 1986.
I Changes Attachment C
(d)  NUREG-0821,     Integrated Plant Safety Assessment Systematic Evaluation Program, R.E. Ginna Nuclear Power Plant, December 1982.
Technical Specification Changes Effect 2.
3.
Revise Table 3.6-1 Penetration 112 to delete valves 204A and 820 and add valves 200A, 200B,
: 202, and 203.
Revise Table 3.6-1 Penetration
: 206, 207, 321I and 322 to replace manual isolation valves with S/G closed system.
Also delete Note 7 from these penetrations.
Delete current Table 3.6-1 Note 17 and replace with new Note 17.
Penetration now satisfies explicit requirements of GDC 56.
Penetration is now consistent with the main steam and feedwater penetrations.
S/G closed system provides an acceptable containment barrier.
Current Note 17 is no longer used.
New note provides information with respect to S/G closed system.
No technical change.


Attachment C Technical Specification Changes I Changes                          Effect Revise Table 3.6-1              Penetration  now  satisfies Penetration 112 to delete        explicit  requirements of valves 204A and 820 and add      GDC  56.
TABLE 3.6-1 CONTAINMENT ISOLATION VALVES PENT.
valves 200A, 200B, 202, and 203.
NO.
: 2. Revise Table 3.6-1              Penetration is now Penetration 206, 207, 321I      consistent with the main and 322 to replace manual        steam and feedwater isolation valves with S/G        penetrations. S/G closed closed system. Also delete      system provides an Note 7 from these                acceptable containment penetrations.                    barrier.
29 IDENTIFICATION/DESCRIPTION Fuel Transfer tube 100 Charging line to "B" loop 101 SI Pump 1B discharge 113 SZ Pump 1A discharge 120 Nitrogen to Accumulators 120 Pressurizer Relief Tank (PRT) to Gas Analyzer (GA) 102 Alternate charging to "A" cold leg 103 Construction Fire Service Water 105 Containment Spray Pump 1A 106 "A" Reactor Coolant Pump (RCP) seal water inlet 107 Sump A discharge to Waste Holdup Tank 108 RCP seal water out and excess letdown to VCT 109 Containment Spray Pump 1B 110 "B" RCP seal water inlet 110 SI test line 111 RHR to "B" cold leg 112 Letdown to Non-regen.
: 3. Delete current Table 3.6-1      Current Note 17 is no Note 17 and replace with new    longer used. New note Note 17.                        provides information with respect to S/G closed system. No technical change.
Heat Exchanger ISOLATION BOUNDARY flange CV 370B CV 889B CV 870B CV 383B welded flange CV 862A CV 304A AOV 1728 MOV 313 CV 862B CV 304B MV 879 MOV 720 (20)
 
AOV 371 CV 889A CV 870A CV 8623 AOV 539 MAXIMUM ISOLATION TIME *(SEC)
TABLE 3.6-1 CONTAINMENT ISOLATION VALVES MAXIMUM                                      MAXIMUM/
NA NA NA NA NA NA NA NA 60 60 NA NA NA NA 60 NA NA NA 60 ISOLATION BOUNDARY (1)
PENT.                                               ISOLATION        ISOLATION                                  ISOLATION TIME NO.           IDENTIFICATION/DESCRIPTION           BOUNDARY        TIME *(SEC) ISOLATION BOUNDARY                  *(SEC) 29  Fuel Transfer tube                             flange              NA    (1) 100 Charging line to "B" loop                     CV 370B              NA    (2)                                    NA 101 SI Pump 1B discharge                           CV 889B              NA    (5)                                   NA CV 870B              NA    (5)                                   NA 102 Alternate charging to "A" cold leg             CV 383B              NA    (2)                                    NA 103 Construction Fire Service Water               welded flange        NA    MV    5129                            NA 105 Containment Spray Pump 1A                     CV 862A              NA    (3)                                    NA 106 "A" Reactor Coolant Pump (RCP) seal water     CV 304A              NA    (2)                                    NA inlet 107 Sump A discharge to Waste Holdup Tank         AOV 1728            60    AOV 1723                              60 108 RCP seal water out and excess letdown to     MOV 313              60    (4)                                    NA VCT 109 Containment Spray Pump 1B                     CV 862B              NA    (3)                                    NA 110 "B" RCP seal water inlet                       CV 304B              NA    (2)                                    NA 110 SI test line                                 MV 879              NA    (5)                                    NA 111 RHR to "B" cold leg                           MOV 720 (20)        NA    (6)                                    NA 112 Letdown to Non-regen. Heat Exchanger           AOV 371             60     ~%4A XOV:'::200A                   RA 60.
(2)
m Sue
(5)
                                                                                +14~+
(5)
RV,'.::.:2,03 AOi~~20,0E, AOV,".".:":202:.
(2)
MV 5129 (3)
(2)
AOV 1723 (4)
(3)
(2)
(5)
(6)
~%4A XOV:'::200A m Sue AOi~~20,0E,
+14~+
AOV,".".:":202:.
RV,'.::.:2,03 (5)
(5)
AOV 846 MV 546 (7)
MAXIMUM/
ISOLATION TIME
*(SEC)
NA NA NA NA NA NA NA 60 NA NA NA NA NA RA 60. ~
i@
i@
                                                                                                                              ~
NA NA 60 NA
113  SZ Pump 1A  discharge                        CV 889A              NA     (5)                                    NA CV 870A              NA    (5)                                    NA 120  Nitrogen to Accumulators                      CV 8623              NA    AOV 846                                60 120  Pressurizer Relief Tank  (PRT) to Gas        AOV 539              60     MV 546        (7)                      NA Analyzer (GA)


MAXIMUM                        MAXIMUM/
4l Ch I
PENT.                                                 ISOLATION      ISOLATION                    ISOLATION'TIME NO.           IDENTIFICATION/DESCRIPTION             BOUNDARY      TIME *(SEC) ZSOLATZON BOUNDARY      *(SEC) 141 RHR-&#xb9;1 pump   suction from   Sump B             MOV  850A (13)      NA    MOV  851A (13)            NA 142 RHR-&#xb9;2 pump   suction from   Sump B             MOV  850B (13)      NA    MOV  851B (13)            NA 143 RCDT pump   suction                             AOV 1721            60    AOV 1003A                60 AOV 1003B                  60 201 Reactor Compart. Cooling Unit A       & B       MV  4757 (16)      NA                              NA MV  4636 (16)      NA                              NA 202 "B" Hydrogen recombiner     (pilot & main)   MV  1076B          NA    SOV-ZV-3B            NA Normally MV  1084B          NA    SOV-IV-5B              Closed NA Normally~
Ch PENT.
Closed 203 Contain. Press. Transmitter PT-947         & 948 PT 947              NA    MV 1819C                  NA PT 948              NA    MV 1819D                  NA 203 Post accident   air sample to "B" fan         MV  1563            NA    MV  1565                  NA MV  1566            NA    MV  1568                  NA 204 Shutdown Purge Supply Duct [Purge Supply         flange (22)      NA [5]  AOV 5869  (22) 4l      Duct]                                            [AOV 5870]
NO.
Ch 205 Hot leg loop sample                             AOV 966C            60    MV 956D  (14)            NA I
IDENTIFICATION/DESCRIPTION 141 RHR-&#xb9;1 pump suction from Sump B
Ch  206 Przr. liquid space sample                       AOV 966B            60    MV  956E (14)            NA 206 "A" S/G sample                                   AOV 5735            60                              NA 207 Przr. Steam space sample                       AOV 966A            60    MV  956F                  NA 207 "B" S/G sample                                   AOV 5736            60                              NA 209 Reactor Compartment. Cooling Units A         & B MV MV 4758 (16) 4635 (16)
142 RHR-&#xb9;2 pump suction from Sump B
NA NA m      ~
143 RCDT pump suction 201 Reactor Compart. Cooling Unit A & B 202 "B" Hydrogen recombiner (pilot & main) 203 Contain.
210  Oxygen makeup    to  A & B recombiners          MV 1080A          NA    SOV IV-2A           NA  Normally SOV ZV-2B             Closed NA Normally Closed 8
Press.
Transmitter PT-947
& 948 203 Post accident air sample to "B" fan 210 Oxygen makeup to A & B recombiners 204 Shutdown Purge Supply Duct [Purge Supply Duct]
205 Hot leg loop sample 206 Przr. liquid space sample 206 "A" S/G sample 207 Przr.
Steam space sample 207 "B" S/G sample 209 Reactor Compartment.
Cooling Units A
& B ISOLATION BOUNDARY MOV 850A (13)
MOV 850B (13)
AOV 1721 MV 4757 (16)
MV 4636 (16)
MV 1076B MV 1084B PT 947 PT 948 MV 1563 MV 1566 flange (22)
[AOV 5870]
AOV 966C AOV 966B AOV 5735 AOV 966A AOV 5736 MV 4758 (16)
MV 4635 (16)
MV 1080A MAXIMUM ISOLATION TIME *(SEC)
NA NA 60 NA NA NA NA NA NA NA NA NA [5]
60 60 60 60 60 NA NA NA ZSOLATZON BOUNDARY MOV 851A (13)
MOV 851B (13)
AOV 1003A AOV 1003B SOV-ZV-3B SOV-IV-5B MV 1819C MV 1819D MV 1565 MV 1568 AOV 5869 (22)
MV 956D (14)
MV 956E (14)
MV 956F SOV IV-2A SOV ZV-2B MAXIMUM/
ISOLATION'TIME
*(SEC)
NA NA 60 60 NA NA NA Normally Closed NA Normally~
Closed NA NA NA NA NA NA NA NA NA m ~
NA Normally Closed NA Normally Closed 8
0
0


a.
a.
MAXIMUM                        MAXIMUM/
PENT.
PENT.                                         ISOLATION      ISOLATION                    ISOLATION'TZ~
NO.
NO.           IDENTIFICATION/DESCRIPTION     BOUNDARY     TIME *(SEC) ZSOLATION BOUNDARY     *(SEC) 316 Service Water to   "B" fan cooler       MV  4628 (16)      NA    (11)                      NA 317 Leakage test supply                     flange            NA    MOV  7443            NA Normally Closed 318 Dead weight tester (decomissioned)-     welded shut        NA    welded shut              NA 319 Service Water from "A" fan cooler       MV  4629 (16)      NA    (ll)                      NA 320  Service water to "C" fan cooler         MV 4647  (16)      NA    (11)                      NA 321 A S/G Blowdown                           AOV 5738          60                              NA 322 B S/G Blowdown                           AOV 5737          60 323 Service Water from "D" fan cooler       MV  4644 (16)      NA    (ll)                      NA 324 Demineralized water to Containment       CV 8419            NA    AOV 8418                  NA 332 Cont. Press. Trans. PT-944, 949 &   950 PT 944             NA     MV 1819G                  NA PT 949            NA     MV 1819F                  NA PT 950            NA     MV 1819E                  NA 332  Leakage  test and hydrogen  monitor      MV 7448            NA     cap                      NA instrumentation lines                    MV 7452            NA     cap                      NA MV 7456            NA     cap                      NA SOV 921            NA     (21)                     NA SOV 922            NA    (21)                     NA SOV 923            NA    (21)                     NA SOV 924            NA    (21)                     NA
IDENTIFICATION/DESCRIPTION ISOLATION BOUNDARY MAXIMUM ISOLATION TIME *(SEC)
ZSOLATION BOUNDARY MAXIMUM/
ISOLATION'TZ~
*(SEC) 316 Service Water to "B" fan cooler 317 Leakage test supply 318 Dead weight tester (decomissioned)-
319 320 Service Water from "A" fan cooler Service water to "C" fan cooler 321 A S/G Blowdown 322 B S/G Blowdown 323 Service Water from "D" fan cooler 332 Leakage test and hydrogen monitor instrumentation lines 324 Demineralized water to Containment 332 Cont. Press.
Trans.
PT-944, 949
& 950 MV 4628 (16) flange welded shut MV 4629 (16)
MV 4647 (16)
AOV 5738 AOV 5737 MV 4644 (16)
CV 8419 PT 944 PT 949 PT 950 MV 7448 MV 7452 MV 7456 SOV 921 SOV 922 SOV 923 SOV 924 NA NA NA NA NA 60 60 NA NA NA NA NA NA NA NA NA NA NA NA (11)
MOV 7443 welded shut (ll)
(11)
(ll)
AOV 8418 MV 1819G MV 1819F MV 1819E cap cap cap (21)
(21)
(21)
(21)
NA NA Normally Closed NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA


~ P (10) The pressure               transmitter provides                   a boundary.
~
(11) Normally operating incoming and outgoing lines which are connected to closed systems inside containment and protected against missiles throughout their length, are provided with at least one manual isolation valve outside containment (FSAR 5.2.2 pg. 5.2.2-2).
P (10)
(12) The single remotely controlled containment isolation valve is normally open and motor operated.                                     The cooling water return line is not directly connected to the reactor coolant system and, should remain open while the coolant pump is running. A second automatic isolation barrier is provided by the component cooling water loop, a closed system.                                                     (FSAR 5.2.2 pg.         5.2.2-la)
(11)
(13) See FSAR Table 5.2.2-1 and Figure 5.2.2-2.                                             Sump     lines are in operation and filled with fluid following an accident.
(12)
Containment leakage testing is not required. The valves are subjected to RHR system hydrostatic test.
(13)
(14) Normally operating outgoing lines connected to the Reactor Coolant System are provided with at least one automatically operated trip valve and one manual isolation valve in series located outside the containment. In addition to the isolation valves, each line connected to the Reactor Coolant System is provided with a remote operated root valve located near its connection to the Reactor Coolant System.                                               (FSAR 5.2.2 pg.
(14)
(15)
(16)
The pressure transmitter provides a boundary.
Normally operating incoming and outgoing lines which are connected to closed systems inside containment and protected against missiles throughout their length, are provided with at least one manual isolation valve outside containment (FSAR 5.2.2 pg. 5.2.2-2).
The single remotely controlled containment isolation valve is normally open and motor operated.
The cooling water return line is not directly connected to the reactor coolant system and, should remain open while the coolant pump is running.
A second automatic isolation barrier is provided by the component cooling water loop, a closed system.
(FSAR 5.2.2 pg. 5.2.2-la)
See FSAR Table 5.2.2-1 and Figure 5.2.2-2.
Sump lines are in operation and filled with fluid following an accident.
Containment leakage testing is not required.
The valves are subjected to RHR system hydrostatic test.
Normally operating outgoing lines connected to the Reactor Coolant System are provided with at least one automatically operated trip valve and one manual isolation valve in series located outside the containment.
In addition to the isolation
: valves, each line connected to the Reactor Coolant System is provided with a remote operated root valve located near its connection to the Reactor Coolant System.
(FSAR 5.2.2 pg.
5.2.2-1)
5.2.2-1)
(15) See FSAR Table 5.2.2-1 and Figure 5.2.2-17.
See FSAR Table 5.2.2-1 and Figure 5.2.2-17.
(16) The Service Water system operates at a pressure higher than the containment accident pressure and is missile protected inside containment. Therefore, these valves are used for flow control only and need not be leak tested.
The Service Water system operates at a pressure higher than the containment accident pressure and is missile protected inside containment.
Therefore, these valves are used for flow control only and need not be leak tested.
(17)
(17)
MNg+P" >UP 'P~.. 'S%% ..g?N~"y+8%CP ~ MgWC YW:, &#xc3;>Y >g'e QP4CAVPehSWPV Y V ~'P~4Q Tne::,:Sy'G:;;::tubes',:".:::,::and:::;::s'e'conairj:.:."s'iai .':jr'ov'icte ji.:.:,:::,:glosi d~ iyjjtem!rxniiide::,'.:':b'oi"i,0'a!i'n'i''eri'iij (18) Fire Service Water                   will be used only to fight fires inside containment. AOV 9227 is closed during power operation. A containment isolation signal to automatically close this valve is not required because a spurious signal during a fire may be hazardous to personnel and may impede fire suppression activities.
(18)
(19) See       FSAR     Table 5.2.2-1 and Figure 5.2.2-16.
MNg+P">UP 'P~.. 'S%%..g?N~"y+8%CP
. ~ MgWC YW:, &#xc3;>Y>g'e QP4CAVPehSWPV Y V~'P~4Q Tne::,:Sy'G:;;::tubes',:".:::,::and:::;::s'e'conairj:.:."s'iai
.':jr'ov'icte ji.:.:,:::,:glosid~ iyjjtem!rxniiide::,'.:':b'oi"i,0'a!i'n'i''eri'iij Fire Service Water will be used only to fight fires inside containment.
AOV 9227 is closed during power operation.
A containment isolation signal to automatically close this valve is not required because a spurious signal during a fire may be hazardous to personnel and may impede fire suppression activities.
(19)
See FSAR Table 5.2.2-1 and Figure 5.2.2-16.
(20) Containment leakage testing is not required per L. D. White, Jr. letter to Dennis L. Ziemann, USNRC dated September 21, 1978.
(20) Containment leakage testing is not required per L. D. White, Jr. letter to Dennis L. Ziemann, USNRC dated September 21, 1978.
3.6-10
3.6-10

Latest revision as of 10:14, 8 January 2025

Proposed TS Table 3.6-1, Containment Isolation Valves
ML17263A210
Person / Time
Site: Ginna 
Issue date: 04/05/1993
From:
ROCHESTER GAS & ELECTRIC CORP.
To:
Shared Package
ML17263A207 List:
References
NUDOCS 9304090209
Download: ML17263A210 (13)


Text

Attachment A

Revise the Technical Specification pages as follows:

Remove 3.6-4 3.6-6 3.6-7A 3.6-10 Insert.

3.6-4 3.6-6 3.6-7A 3.6-10 9'304090209 930405 PDR ADOCK,05000244 P'DR

TABLE 3.6-1 CONTAINMENT ISOLATION VALVES PENT.

NO.

29 IDENTIFICATION/DESCRIPTION Fuel Transfer tube 100 Charging line to "B" loop 101 SZ Pump 1B discharge 113 SZ Pump 1A discharge 120 Nitrogen to Accumulators 120 Pressurizer Relief Tank (PRT) to Gas Analyzer (GA) 102 Alternate charging to "A" cold leg 103 Construction Fire Service Water 105 Containment Spray Pump 1A 106 "A" Reactor Coolant Pump (RCP) seal water inlet 107 Sump A discharge to Waste Holdup Tank 108 RCP seal water out and excess letdown to VCT 109 Containment Spray Pump 1B 110 "B" RCP seal water inlet 110 SZ test line 111 RHR to "B" cold leg 112 Letdown to Non-regen.

Heat Exchanger ZSOLATZON BOUNDARY flange CV 370B CV 889B CV 870B CV 383B welded flange CV 862A CV 304A AOV 1728 MOV 313 CV 862B CV 304B MV 879 MOV 720 (20)

AOV 371 CV 889A CV 870A CV 8623 AOV 539 MAXIMUM ISOLATION TIME *(SEC)

NA NA NA NA NA NA NA NA 60 60 NA NA NA NA 60 NA NA NA 60 ISOLATION BOUNDARY (1)

(2)

(5)

(5)

(2)

MV 5129 (3)

(2)

AOV 1723 (4)

(3)

(2)

(5)

(6)

AOV 200A AOV 200B AOV 202 RV 203 (5)

(5)

AOV 846 MV 546 (7)

MAXIMUM/

ISOLATION TIME

  • (SEC)

NA NA NA NA NA NA NA 60 NA NA NA NA NA 60 60 60 NA NA NA 60 NA

Pg PENT.

NO 141 142 g0 143 IDENTIFICATION/DESCRIPTION RHR-tl pump suction from Sump B

RHR-g2 pump suction from Sump B

RCDT pump suction ZSOLATION BOUNDARY MOV 850A (13)

MOV 850B (13)

AOV 1721 MAXIMUM ISOLATION TIME *(SEC)

NA NA 60 ISOLATION BOUNDARY MOV 851A (13)

MOV 851B (13)

AOV 1003A AOV 1003B MAXIMUM/

ISOLATION TIME

  • (SEC)

NA NA 60 60 4P I

201 Reactor Compart. Cooling Unit A & B 202 "B" Hydrogen recombiner (pilot & main) 203 Contain. Press.

Transmitter PT-947

& 948 203 Post accident air sample to "B" fan 204 Shutdown Purge Supply Duct [Purge Supply Duct]

205 Hot leg loop sample 206 Przr. liquid space sample 206 "A" S/G sample 207 Przr.

Steam space sample 207 "B" S/G sample 209 Reactor Compartment.

Cooling Units A & B 210 Oxygen makeup to A & B recombiners MV 4757 (16)

MV 4636 (16)

MV 1076B MV 1084B PT 947 PT 948 MV 1563 MV 1566 flange (22)

[AOV 5870]

AOV 966C AOV 966B AOV 5735 AOV 966A AOV 5736 MV 4758 (16)

MV 4635 (16)

MV 1080A NA NA NA NA NA NA NA NA NA

[5]

60 60 60 60 60 NA NA NA SOV-IV-3B SOV<<ZV-5B MV 1819C MV 1819D MV 1565 MV 1568 AOV 5869 (22)

MV 956D (14)

MV 956E (14)

(17)

MV 956F (17)

SOV ZV-2A SOV IV-2B NA Normally Closed NA Normally Closed NA NA NA NA NA NA NA NA NA NA NA NA Normally Closed NA Normally Closed 0

0

PENT.

o'O.

O315 316 g0 317 318 319 320 IDENTIFICATION/DESCRIPTION Service Water from "C" fan cooler Service Water to "B" fan cooler Leakage test supply Dead weight tester (decomissioned)

Service Water from "A" fan cooler Service water to "C" fan cooler 4P I

321 A S/G Blowdown 322 B S/G Blowdown 323 Service Water from "D" fan cooler 324 Demineralized water to Containment 332 Cont. Press.

Trans.

PT-944, 949

& 950 ISOLATION BOUNDARY MV 4643 (16)

MV 4628 (16) flange welded shut MV 4629 (16)

MV 4647 (16)

AOV 5738 AOV 5737 MV 4644 (16)

CV 8419 PT 944 PT 949 PT 950 MAXIMUM ISOLATION TZME *(SEC)

NA NA NA NA NA NA 60 60 NA NA NA NA NA ISOLATION BOUNDARY (11)

(ll)

MOV 7443 welded shut (ll)

(11)

(17)

(17)

(11)

AOV 8418 MV 1819G MV 1819F MV 1819E MAXIMUM/

ZSOLATZON TIME

  • (SEC)

NA NA Normally Closed NA NA NA NA NA NA NA NA NA NA 332 Leakage test and hydrogen monitor instrumentation lines MV 7448 MV 7452 MV 7456 SOV 921 SOV 922 SOV 923 SOV 924 NA NA NA NA NA NA NA cap cap cap (21)

(21)

(21)

(21)

NA NA NA NA NA NA m

~

0 0

(10)

(11)

(12)

(13)

(14)

(15)

(16)

(17)

The pressure transmitter provides a boundary.

Normally operating incoming and outgoing lines which are connected to closed systems inside containment and protected against missiles throughout their length, are provided with at least one manual isolation valve outside containment (FSAR 5.2.2 pg. 5.2.2-2).

The single remotely controlled containment isolation valve is normally open and motor operated.

The cooling water return line is not directly connected to the reactor coolant system and, should remain open while the coolant pump is running.

A second automatic isolation barrier is provided by the component cooling water loop, a closed system.

(FSAR 5.2.2 pg. 5.2.2-1a)

See FSAR Table 5.2.2-1 and Figure 5.2.2-2.

Sump lines are in operation and filled with fluid following an accident.

Containment leakage testing is not required.

The valves are subjected to RHR system hydrostatic test.

Normally operating outgoing lines connected to the Reactor Coolant System are provided with at least one automatically operated trip valve and one manual isolation valve in series located outside the containment.

In addition to the isolation

valves, each line connected to the Reactor Coolant System is provided with a remote operated root valve located near its connection to the Reactor Coolant System.

(FSAR 5.2.2 pg.

5.2.2-1)

See FSAR Table 5.2.2-1 and Figure 5.2.2-17.

The Serv'ice Water system operates-at a pressure higher than the containment accident pressure and is missile protected inside containment.

Therefore, these valves are used for flow control only and need not be leak tested.

The S/G tubes and secondary side provide a closed system inside containment.

(18) Fire Service Water will be used only to fight fires inside containment.

AOV 9227 is closed during power operation.

A containment isolation signal to automatically close this valve is not required because a spurious signal during a fire may be hazardous to personnel and may impede fire suppression activities.

(19)

(20)

See FSAR Table 5.2.2-1 and Figure 5.2.2-16.

Containment leakage testing is not, required per L. D. White, Jr. letter to Dennis L. Ziemann, USNRC dated September 21, 1978.

3.6-10 Proposed

Attachment B

Page 1 of 2 Attachment B

The purpose of this amendment is to revise several penetration listings in Technical Specification Table 3.6-1 to support an Integrated Leak Rate Test (ILRT) of the Ginna Station containment during the 1993 Refueling Outage.

As a result of preparing for this test, RG&E determined that a discrepancy existed between the Technical Specifications and the NRC approved In-Service Test (IST)

Program.

Currently, Technical Specification Table 3.6-1 identifies two manual valves (820 and 204A) as containment isolation valves (CIVs) for Penetration 112.

As part of the third 10 year IST program submittal for Ginna Station, RG&E identified that valves 820 and 204A would be removed from the IST program since their pressure and containment isolation functions were being performed by valves 200A, 200B, and 202 (Reference a).

The NRC accepted this change by Reference (b).

Therefore, RG&E requests that Table 3.6-1 be changed to replace valves 820 and 204A with AOVs 200A, 200B, and 202.

In addition, relief valve

203, which is located between containment isolation valves
200A, 200B, 202 and 371 for this penetration, will be added to the table.

All five valves are currently in the Ginna Station Appendix J testing program.

This change will enable Penetration 112 to meet the explicit requirements of GDC 56.

The current Table 3.6-1 Note 17 will also be deleted since it is no longer used.

Technical Specification Table 3.6-1 also identifies a manual valve in series with an air-operated valve as the CIVs for Penetrations

206, 207,
321, and 322.

These penetrations contain the steam generator (S/G) blowdown and blowdown sample piping.

RG&E requests that the manual valves be removed from Table 3.6-1 since the S/G tubes and secondary side provide one containment barrier.

These penetrations will then be treated analogous to the main steam and feedwater lines which are of similar configuration.

Table 3.6-1 Note 17 will then be revised and added to these four penetrations to reflect the use of the S/G tubes and secondary side as a

containment boundary.

Table 3.6-1 Note 7 will also be deleted from these four penetrations.

This note was originally applied to the S/G blowdown lines since they penetrate the missile shield inside containment in order to reach the S/Gs.

However, the NRC has approved the use of "leak-before-break" (LBB) with respect to large diameter Reactor Coolant System piping at Ginna Station (Reference c).

The use of LBB excludes the consideration of the dynamic effects associated with postulated pipe ruptures per 10 CFR 50, Appendix A, GDC 4.

In addition, plant walkdowns and a review of Systematic Evaluation Program (SEP) Topic III-S.A, Effects of Pipe Break on Structures,

Systems, and Components Inside Containment, (Reference d) confirms that even though these four lines penetrate the missile shield, they are not susceptible to any high energy line sources.

This includes the affects of pipe whip and jet impingement.

Therefore, the dynamic effects associated with any high energy line break inside containment does not require consideration with respect to the S/G closed system.

The blowdown lines inside containment are also Seismic Category I and Safety Class 2.

Consequently, the lines are considered missile protected based on their present location and have the necessary closed system design requirements.

Attachment B

Page 2 of 2 RG&E will also eliminate 10 CFR 50 Appendix J testing related to the four AOVs for Penetrations

206, 207,
321, and 322 since there are not any requirements to perform this testing.
Instead, RG&E will hydrostatically test these valves in accordance with 'the original requirements as outlined in the approved third 10 year IST program for Ginna Station (IWV-3421 through 3425) as a minimum.

This will provide the necessary assurance that the valves will perform their required isolation function.

These changes will be documented in the Ginna Station IST Program which will be submitted to the NRC following the conclusion of the 1993 Refueling Outage since RG&E expects to make several other unrelated IST Program changes at that time.

These changes will not require NRC approval prior to implementation.

In accordance with.10 CFR 50.91, these changes to the Technical Specifications have been evaluated to determine if the operation of the facility in accordance with the proposed amendment would:

1.

involve a

significant increase in the probability or consequences of an accident previously evaluated; or 2.

create the possibility of a new or different kind of accident previously evaluated; or 3.

involve a significant reduction in a margin of safety.

These proposed changes do not increase the probability or consequences of a previously evaluated accident or create a new or different type of accident.

Furthermore, there is no reduction in the margin of safety for any particular Technical Specification.

The detailed changes are described in Attachment C.

Therefore, Rochester Gas and Electric submits that the issues associated with this Amendment request are outside the criteria of 10 CFR 50.91; and a no significant hazards finding is warranted.

References:

(a)

Letter from R.C. Mecredy, RG&E, to A.R. Johnson, NRC,

Subject:

Inservice Pump and Valve Testing Program, dated May 23, 1989.

(b)

Letter from A.R. Johnson, NRC, to R.C. Mecredy, RG&E,

Subject:

R.E.

Ginna Nuclear Power P1ant IST Program for Pumps and

Valves, 1990-1999 Third 10-Year Interval, dated April 15, 1991.

(c)

Letter from D. DiIanni, NRC, to R.

Kober, RG&E,

Subject:

Resol uti on of USI'-2, "Asymmetric LOCA Loads ",

dated September 9,

1986.

(d)

NUREG-0821, Integrated Plant Safety Assessment Systematic Evaluation Program, R.E.

Ginna Nuclear Power Plant, December 1982.

I Changes Attachment C

Technical Specification Changes Effect 2.

3.

Revise Table 3.6-1 Penetration 112 to delete valves 204A and 820 and add valves 200A, 200B,

202, and 203.

Revise Table 3.6-1 Penetration

206, 207, 321I and 322 to replace manual isolation valves with S/G closed system.

Also delete Note 7 from these penetrations.

Delete current Table 3.6-1 Note 17 and replace with new Note 17.

Penetration now satisfies explicit requirements of GDC 56.

Penetration is now consistent with the main steam and feedwater penetrations.

S/G closed system provides an acceptable containment barrier.

Current Note 17 is no longer used.

New note provides information with respect to S/G closed system.

No technical change.

TABLE 3.6-1 CONTAINMENT ISOLATION VALVES PENT.

NO.

29 IDENTIFICATION/DESCRIPTION Fuel Transfer tube 100 Charging line to "B" loop 101 SI Pump 1B discharge 113 SZ Pump 1A discharge 120 Nitrogen to Accumulators 120 Pressurizer Relief Tank (PRT) to Gas Analyzer (GA) 102 Alternate charging to "A" cold leg 103 Construction Fire Service Water 105 Containment Spray Pump 1A 106 "A" Reactor Coolant Pump (RCP) seal water inlet 107 Sump A discharge to Waste Holdup Tank 108 RCP seal water out and excess letdown to VCT 109 Containment Spray Pump 1B 110 "B" RCP seal water inlet 110 SI test line 111 RHR to "B" cold leg 112 Letdown to Non-regen.

Heat Exchanger ISOLATION BOUNDARY flange CV 370B CV 889B CV 870B CV 383B welded flange CV 862A CV 304A AOV 1728 MOV 313 CV 862B CV 304B MV 879 MOV 720 (20)

AOV 371 CV 889A CV 870A CV 8623 AOV 539 MAXIMUM ISOLATION TIME *(SEC)

NA NA NA NA NA NA NA NA 60 60 NA NA NA NA 60 NA NA NA 60 ISOLATION BOUNDARY (1)

(2)

(5)

(5)

(2)

MV 5129 (3)

(2)

AOV 1723 (4)

(3)

(2)

(5)

(6)

~%4A XOV:'::200A m Sue AOi~~20,0E,

+14~+

AOV,".".:":202:.

RV,'.::.:2,03 (5)

(5)

AOV 846 MV 546 (7)

MAXIMUM/

ISOLATION TIME

  • (SEC)

NA NA NA NA NA NA NA 60 NA NA NA NA NA RA 60. ~

i@

NA NA 60 NA

4l Ch I

Ch PENT.

NO.

IDENTIFICATION/DESCRIPTION 141 RHR-¹1 pump suction from Sump B

142 RHR-¹2 pump suction from Sump B

143 RCDT pump suction 201 Reactor Compart. Cooling Unit A & B 202 "B" Hydrogen recombiner (pilot & main) 203 Contain.

Press.

Transmitter PT-947

& 948 203 Post accident air sample to "B" fan 210 Oxygen makeup to A & B recombiners 204 Shutdown Purge Supply Duct [Purge Supply Duct]

205 Hot leg loop sample 206 Przr. liquid space sample 206 "A" S/G sample 207 Przr.

Steam space sample 207 "B" S/G sample 209 Reactor Compartment.

Cooling Units A

& B ISOLATION BOUNDARY MOV 850A (13)

MOV 850B (13)

AOV 1721 MV 4757 (16)

MV 4636 (16)

MV 1076B MV 1084B PT 947 PT 948 MV 1563 MV 1566 flange (22)

[AOV 5870]

AOV 966C AOV 966B AOV 5735 AOV 966A AOV 5736 MV 4758 (16)

MV 4635 (16)

MV 1080A MAXIMUM ISOLATION TIME *(SEC)

NA NA 60 NA NA NA NA NA NA NA NA NA [5]

60 60 60 60 60 NA NA NA ZSOLATZON BOUNDARY MOV 851A (13)

MOV 851B (13)

AOV 1003A AOV 1003B SOV-ZV-3B SOV-IV-5B MV 1819C MV 1819D MV 1565 MV 1568 AOV 5869 (22)

MV 956D (14)

MV 956E (14)

MV 956F SOV IV-2A SOV ZV-2B MAXIMUM/

ISOLATION'TIME

  • (SEC)

NA NA 60 60 NA NA NA Normally Closed NA Normally~

Closed NA NA NA NA NA NA NA NA NA m ~

NA Normally Closed NA Normally Closed 8

0

a.

PENT.

NO.

IDENTIFICATION/DESCRIPTION ISOLATION BOUNDARY MAXIMUM ISOLATION TIME *(SEC)

ZSOLATION BOUNDARY MAXIMUM/

ISOLATION'TZ~

  • (SEC) 316 Service Water to "B" fan cooler 317 Leakage test supply 318 Dead weight tester (decomissioned)-

319 320 Service Water from "A" fan cooler Service water to "C" fan cooler 321 A S/G Blowdown 322 B S/G Blowdown 323 Service Water from "D" fan cooler 332 Leakage test and hydrogen monitor instrumentation lines 324 Demineralized water to Containment 332 Cont. Press.

Trans.

PT-944, 949

& 950 MV 4628 (16) flange welded shut MV 4629 (16)

MV 4647 (16)

AOV 5738 AOV 5737 MV 4644 (16)

CV 8419 PT 944 PT 949 PT 950 MV 7448 MV 7452 MV 7456 SOV 921 SOV 922 SOV 923 SOV 924 NA NA NA NA NA 60 60 NA NA NA NA NA NA NA NA NA NA NA NA (11)

MOV 7443 welded shut (ll)

(11)

(ll)

AOV 8418 MV 1819G MV 1819F MV 1819E cap cap cap (21)

(21)

(21)

(21)

NA NA Normally Closed NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA

~

P (10)

(11)

(12)

(13)

(14)

(15)

(16)

The pressure transmitter provides a boundary.

Normally operating incoming and outgoing lines which are connected to closed systems inside containment and protected against missiles throughout their length, are provided with at least one manual isolation valve outside containment (FSAR 5.2.2 pg. 5.2.2-2).

The single remotely controlled containment isolation valve is normally open and motor operated.

The cooling water return line is not directly connected to the reactor coolant system and, should remain open while the coolant pump is running.

A second automatic isolation barrier is provided by the component cooling water loop, a closed system.

(FSAR 5.2.2 pg. 5.2.2-la)

See FSAR Table 5.2.2-1 and Figure 5.2.2-2.

Sump lines are in operation and filled with fluid following an accident.

Containment leakage testing is not required.

The valves are subjected to RHR system hydrostatic test.

Normally operating outgoing lines connected to the Reactor Coolant System are provided with at least one automatically operated trip valve and one manual isolation valve in series located outside the containment.

In addition to the isolation

valves, each line connected to the Reactor Coolant System is provided with a remote operated root valve located near its connection to the Reactor Coolant System.

(FSAR 5.2.2 pg.

5.2.2-1)

See FSAR Table 5.2.2-1 and Figure 5.2.2-17.

The Service Water system operates at a pressure higher than the containment accident pressure and is missile protected inside containment.

Therefore, these valves are used for flow control only and need not be leak tested.

(17)

(18)

MNg+P">UP 'P~.. 'S%%..g?N~"y+8%CP

. ~ MgWC YW:, Ã>Y>g'e QP4CAVPehSWPV Y V~'P~4Q Tne::,:Sy'G:;;::tubes',:".:::,::and:::;::s'e'conairj:.:."s'iai

.':jr'ov'icte ji.:.:,:::,:glosid~ iyjjtem!rxniiide::,'.:':b'oi"i,0'a!i'n'ieri'iij Fire Service Water will be used only to fight fires inside containment.

AOV 9227 is closed during power operation.

A containment isolation signal to automatically close this valve is not required because a spurious signal during a fire may be hazardous to personnel and may impede fire suppression activities.

(19)

See FSAR Table 5.2.2-1 and Figure 5.2.2-16.

(20) Containment leakage testing is not required per L. D. White, Jr. letter to Dennis L. Ziemann, USNRC dated September 21, 1978.

3.6-10

r, 0,

I t