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{{#Wiki_filter:Attachment A Revise the Technical Specification pages as follows: Remove 3.5-22 3.6-5 3.6-6 3.6-7'.6-11 3.8-1 4.4-7 4.4-8 Insert 3.5-22 3.6-5 3.6-6 3.6-7 3".6-7A 3.6-11 3.8-1 4.4-7 4.4-8 gg j 0',031~0g000244 jjg102>.DR PQOCK o PQR P I TABLE 3.5-7, Radiation Accident Monitorin Instrumentation Instrument 1.Containment Area (R-29 and R-30)2.Noble Gas Effluent Monitors Minimum Channels~Oerable Action Plant Vent (R-14)ii.A Main Steam Line (R-31)iii.B Main Steam Line (R-32)iv.Containment Purge (R-12A)v~Air Ejector (R-15A)Action Statements Action 1-With the number of operable channels less than required by the Minimum Channels Operable requirements, either restore the inoperable channel(s) to operable status within 7 days of the event, or prepare and submit a Special Report to the Commission within 30 days following the event outlining the action taken, the cause of the inoperability and the plans and schedule for restoring the system to operable status.*only when the shutdown purge system flanges are removed.3.5-22 Proposed III lt t k ll lk 1 1' PENT.NO.121 121 121 121 123 124 124..125 126 127 128 e 129 g 130 131 132 140 IDENTIFICATION/DESCRIPTION Nitrogen to PRT Reactor Makeup water to PRT Cont.Press.transmitter PT-945 (10)Cont.Press.transmitter PT-946 (10)Reactor Coolant Drain Tank (RCDT)to (R Excess letdown supply and return to heat exchanger Post Accident air sample"C" fan Canponent Gooling Water (CW)fran 1B RCP QOW fran 1A RCP RCDT 8(PRT to Vent Header E-CCW to reactor support cooling QOW to reactor support cooling blini-Purge exhaust--RHR pump suction fran"A" Hot leg ISOZATION BOUNDARY CV 528 CV 529 PT 945 PT 946 AOV 1789 AOV 745 CV 743 MV 1569 MV 1572 MOV 759B MOV 759A CV 750A CV 750B AOV 1787 CV 1713 MOV 813 MOV 814 AOV 7970 MOV 701(20)MAXKMUM ISOZATION TIME*(SEC)60 60 60 60 60 ISOZATION BOUNDAHY MV 547(8)AOV 508 MV 1819A MV 1819B MV 1655(7)MV 1571 MV 1574 (12)(12)MOV 749A MOV 749B AQV 1786 (19)AOV 7971 (6)MMGMUM ISOZATION TIME*(SEC)60 60 60 60 1 L 0 lI I it'h 1'I l 71 III PENT.NO.141 142 143 201 202 203 203 204 205 206 206 207 0 207 209 210 IDENTIFICATION/DESCRIPTION RHR-//1 pump suction from Sump B RHR-jj2 pump suction from Sump B RCDT pump suction Reactor Compart.cooling Unit A 6 B"B" Hydrogen recombiner (pilot 6 main)Contain, Press.transmitter PT-947 S 948 Post accident air sample to"B" fan Shutdown Purge Supply Duct Hot leg loop sample Zrzr.liquid space sample"A" S/G sample Przr.Steam space sample"B" S/G sample Reactor Compart.cooling Units A 8 B Oxygen makeup to A 8 B recombiners 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 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 60 60 60 60 60 NA NA NA ISOLATION BOUNDARY MOV 851A(13)MOV 851B(13)AOV 1003A AOV 1003B SOV IV-3B SOV IV-5B MV 1819C MV 1819D MV 1565 MV 1568 AOV 5869 (22)MV 956D(14)MV 956E(14)MV 5733(7)MV 956F MV 5734(7)SOV IV-2A SOV IV-2B C HAXIMUM ISOLATION TIME"-(SEC)-.NA NA 60 60 NA NA Normally Closed NA Normally'Closed NA NA NA NA NA NA NA NA.NA NA NA NA Normally Closed NA Normally Closed 0 ,u r." f PENT.No.300 301 303 304 305 305 305 307 308 309 310 310 0~o 311 312 313 IDENTIFICATION/DESCRIPTION Shutdown Purge Exhaust Duct Aux.steam supply to containment Aux.steam condensate return"A" Hydrogen recombiner (pilot and main)Radiation Monitors R-ll, R-12 S R-10A Auto Inlet Isol.R-ll, R-12 S R-10A Outlet Post Accident air sampler (containment)
{{#Wiki_filter:Attachment A Revise the Technical Specification pages as follows:
Fire Service Water Service Water to"A" fan cooler Mini-Purge supply Service Air to Contain.Instrument Air to Contain.Service Water from"B" fan cooler Service Water to"D" fan cooler Ieakage test depressurization ISOLATION BOUNDARY flange (22)MV 6151 MV 6175 MV 1084B MV 1076A AOV 1597 AOV 1599 MV 1554 MV 1557 MV 1560 CV 9229 MV 4627(16)AOV 7478 CV 7226 CV 5393 MV 4630(16)MV 4642(16)flange 60 AOV 1598 MV 1556 MV 1559 MV 1562't NA-AOV 9227 NA NA NA NA NA NA AOV 7445 MV 7141 AOV 5392 NA NA MOV 7444 MAXIMUM IsoLAnom--IsoLAnoN TIME" (SEC)BOUNDARY NA AOV 5879 (22)NA-MV 6165(15)NA-MV 6152(15)NA SOV IV-5A NA.-SOV XV-3A 60~MV 1596 MAXIMUM IsoI,Anom TIME"(SEC)NA NA NA Normallly Clos~NA NormaU.ly Clo~NA 60 60 NA NA (18)NA NA 60 NA NA.NA Normally Closed
Remove                     Insert 3.5-22                    3.5-22 3.6-5                     3.6-5 3.6-6                    3.6-6 3.6-7                     3.6-7 3".6-7A
                              '.6-11 3.6-11 3.8-1                    3.8-1 4.4-7                     4.4-7 4.4-8                    4.4-8 jjg102>.
gg j 0',031~
PQOCK 0g000244 o   PQR DR P


PENT.NO.316 317 318 320 321~322 323 324 332 332 IDENTIFICATION/DESCBIPTION Service Water fran"C" fan cooler Service Water to"B" fan cooler Leakage test supply Dead weight tester (deccmissioned)
I TABLE  3.5-7, Radiation Accident Monitorin Instrumentation Minimum Channels Instrument                                ~Oerable        Action
Service Water frcm"A" fan cooler Service water to"C" fan cooler A S/G Blmrdown B S/G Blcwdown Service Water frcm"D" fan cooler Demineralized water to Containment Cont.Press.Trans.PT-944, 949 6 950 Leakage test and hydrogen mnitor instrumentation lines ISOZATION 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 MV 7448 MV 7452 MV 7456 SOV 921 SOV 922 SOV 923 SOV 924 MAXIMUM ISOZATION TIME*(SEC)60 60 MOV 7443 welded shut MV 5701(7)MV 5702(7)AOV 8418 MV 1819G MV 1819F MV 1819E cap cap cap (21)(21)(21)(21)MAXDIUM ISOZATION TIME*(SEC)Nh.Normally Closed.0 II 1 h 1 II K I.h.h t I t r II," I I 75 ()~)I I t t (,/~(>>~~'v/t)p I<-4 5 C 4 I/1 (c'CI F' (21)Acceptable isolation capability is provided for instrument lines by two isolation boundaries outside containment.
: 1. Containment Area (R-29 and R-30)
One of the boundaries outside containment may be a Seismic Class 1 closed system which is subjected to Type C leak rate testing.(22)The flanges at penetrations 204 and 300 can only be removed at cold or refueling shutdown.The flanges and associated double seals provide containment isolation and are a containment boundary for all modes of operation between cold shutdown and normal operation.
: 2. Noble Gas  Effluent Monitors Plant Vent (R-14) ii. A Main Steam Line (R-31) iii. B Main Steam Line (R-32) iv. Containment Purge (R-12A) v ~ Air Ejector  (R-15A)
During cold and refueling shutdown when the flanges are removed integrity is provided by the 48 inch valves.3.6-11 Proposed I I J II f.~), It Jw"''I I d r 4 ,>>II l~d'X)A~U~', k~'V/4
Action Statements Action 1  With the number of operable channels less than required by the Minimum Channels Operable requirements, either restore the inoperable channel(s) to operable status within 7 days of the event, or prepare and submit a Special Report to the Commission within 30 days following the event outlining the action taken, the cause of the inoperability and the plans and schedule for restoring the system to operable status.
~v 3.8 REFUEZING A licabilit 3.8.1 Applies to operating limitations during refueling operations.
* only when the shutdown purge system flanges are removed.
~b'o ensure that no incident could occur during refueling operations that would affect public health and safety.During refueling operations the following conditions shall be satisfied.
3.5-22                    Proposed
a~The equipment door, or a closure plate that restricts air flow from the containment, and at least one personnel door in the equipment door or closure plate and in the personnel air lock shall be properly closed.In addition, all automatic containment isolation valves shall be b.operable or at least one valve in each line I shall be',locked closed.The" 48 inch"shutdown lt purge valves must also be operable or closed or the associated flange must be installed'.
II Radiation levels in the containment shall be c~monitored continuously.
Core subcritical neutron flux shall be contin-uously monitored by at least two source range neutron monitors, each with continuous visual.indication in the control room and one with audible indication in the contairpnent and control room available whenever core geometry is being changed.When core geometry is not being changed at 3.8-1 Proposed v shutdown and depressurized until repairs are effected and the local leakage meets the acceptance criterion.
4.4.2.4 Test Fre uenc a~b.~'i<c i Except as specified in b., c., and d.below, individual penetrations and containment isolation valves shall be tested during each reactor shutdown for refueling, or other convenient intervals, but in no case at, intervals greater than two years.The containment equipment hatch, fuel transfer tube, and shutdown purge system flanges shall be n tested at each refueling shutdown or after each use, if, that.be sooner.t(~',-The, containment,air'o'cks'hall be tested at, intervals of no more than six months by pressurizing the space between the air lock doors.In addition, following opening of the air lock door during the interval, a test shall be performed by pressurizing between the dual seals of each door opened, within 48 hours of the opening, unless the reactor was in the cold shutdown condition at the time of the opening or has been subsequently brought to the cold shutdown condition.
A test shall also be performed by pressurizing between the dual seals of each door within 48 hours of leaving the cold shutdown condition, unless the doors have not been open since the last test performed either by pressurizing the space between the air lock doors or by pressurizing between the dual door seals.4.4-7 Proposed  


====4.4.3 Recirculation====
III ll lt t
e t e ov l S stems 4.4.3.1 Test a~The portion of the residual heat removal system that is outside the containment shall either be tested by use in normal operation or hydrostati-cally tested at 350 psig at the interval specified in 4.4.3.4.b.Suction piping from containment sump B to the reactor coolant drain tank pump and the discharge piping from the pumps to the residual heat removal system shall be hydrostatically gested at go less that 100 psig at the interval specified)in$.4.3.4.4.4-,8 Proposed Attachment B Containment purge and vent operations became a generic concern in 1978.Since that time containment purge and vent has been the subject of many letters between the Staff and Rochester Gas and Electric Corp.(RG&E).In Reference 1, the Staff transmitted to RGSE a Safety Evaluation Report (SER)which found RGE's interium commitments to be acceptable.
k lk 1
The SER provides a good summary of the correspondance and the commitments made concerning this subject.The existing purge and vent systems at Ginna consist of a 48 inch purge system and a 6 inch containment vent (depressurization) system.The major issue concerning the purge system is the operability of the 48 inch purge valves during a design basis accident-loss of coolant accident (DBA-LOCA).
1'
Therefore, RGGE has committed to maintaining the 48 inch purge valves closed while the reactor is critical until information demonstrating operability is submitted.
 
In response to the Staff's request to limit purge/vent operations to safety-related needs RG6E committed to limiting vent system operation to a total of 90 hours per year.To permanently resolve the purge and vent issue RG6E has decided to modify the 48 inch purge system so that it will only be used when the reactor is in cold or refueling shutdown, and install a mini-purge system which will allow unlimited purging of containment.
MAXKMUM                MMGMUM PENT.                                                  ISOZATION    ISOZATION  ISOZATION    ISOZATION NO.      IDENTIFICATION/DESCRIPTION                  BOUNDARY    TIME *(SEC) BOUNDAHY    TIME *(SEC) 121      Nitrogen to  PRT                            CV 528                  MV  547(8) 121      Reactor Makeup water    to PRT              CV 529                  AOV 508        60 121      Cont. Press. transmitter PT-945 (10)        PT 945                  MV 1819A 121      Cont. Press. transmitter PT-946 (10)        PT 946                  MV 1819B 123      Reactor Coolant Drain Tank    (RCDT) to (R  AOV 1789        60      MV  1655(7) 124      Excess letdown supply and    return        AOV 745        60 to heat exchanger                            CV 743 124      Post Accident    air sample "C" fan          MV 1569                MV 1571 MV 1572                MV 1574
  ..125      Canponent Gooling Water    (CW) fran 1B RCP MOV 759B                (12) 126      QOW  fran  1A RCP                            MOV 759A                (12) 127                                                    CV 750A                MOV  749A      60 128                                                    CV 750B                MOV  749B      60 e  129 E
RCDT  8( PRT to Vent  Header                AOV 1787        60      AQV  1786      60 CV 1713 g  130    -
CCW  to reactor support cooling              MOV 813        60 131      QOW  to reactor support cooling              MOV 814        60      (19) 132      blini-Purge exhaust                          AOV 7970                AOV 7971 140    --RHR pump  suction fran "A" Hot leg          MOV 701(20)            (6)
 
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C MAXIMUM                      HAXIMUM PENT.                                                ISOLATION      ISOLATION  ISOLATION        ISOLATION NO. IDENTIFICATION/DESCRIPTION                      BOUNDARY      TIME ='(SEC) BOUNDARY        TIME "-(SEC) 141  RHR-//1 pump  suction from    Sump B          MOV  850A(13)    NA      MOV  851A(13)      NA 142  RHR-jj2 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 6 B      MV  4757(16)      NA MV  4636(16)      NA                          NA 202  "B" Hydrogen recombiner      (pilot  6 main)  MV  1076B        NA        SOV  IV-3B    NA Normally Closed MV  1084B        NA        SOV  IV-5B    NA Normally 'Closed 203  Contain, Press. transmitter  PT-947  S 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                      flange (22)      NA        AOV  5869 (22) 205  Hot leg loop sample                            AOV 966C          60      MV  956D(14)      NA 206  Zrzr. liquid  space sample                    AOV 966B          60      MV  956E(14)      NA 206  "A" S/G sample                                  AOV 5735          60        MV  5733(7)        NA 207  Przr. Steam space    sample                  AOV 966A          60        MV  956F            NA 0
207  "B" S/G sample                                  AOV  5736        60        MV  5734(7)        .NA 209  Reactor Compart. cooling Units        A 8 B    MV  4758(16)      NA                            NA MV  4635(16)      NA                            NA 210  Oxygen makeup    to  A 8 B  recombiners        MV  1080A        NA        SOV  IV-2A    NA Normally Closed SOV  IV-2B    NA Normally Closed
 
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MAXIMUM                              MAXIMUM PENT.                                              ISOLATION    IsoLAnom
                                                                                  - -IsoLAnoN            IsoI,Anom No. IDENTIFICATION/DESCRIPTION                  BOUNDARY    TIME " (SEC)          BOUNDARY      TIME "(SEC) 300  Shutdown Purge Exhaust Duct                  flange (22)      NA                AOV 5879  (22) 301  Aux. steam supply  to containment          MV  6151        NA        -      MV  6165(15)        NA 303  Aux. steam condensate  return              MV  6175        NA              -MV  6152(15)        NA 304  "A" Hydrogen recombiner    (pilot  and main) MV  1084B        NA                SOV  IV-5A    NA Normallly  Clos~
MV  1076A        NA    .          SOV  XV-3A    NA NormaU.ly  Clo~
305  Radiation Monitors  R-ll,  R-12 S  R-10A    AOV 1597        60      ~
MV  1596            NA Auto  Inlet Isol.
305  R-ll,  R-12 S R-10A  Outlet                  AOV 1599        60                AOV 1598            60 305  Post Accident  air  sampler (containment)    MV  1554        NA                MV  1556            60 MV  1557        NA                MV  1559            NA MV  1560        NA                MV  1562            NA
                                                                                    't 307  Fire Service Water                          CV  9229        NA              -AOV  9227          (18) 308  Service Water to "A" fan cooler              MV  4627(16)    NA                                    NA 309  Mini-Purge supply                            AOV 7478                          AOV 7445 310  Service Air to Contain.                      CV  7226        NA                MV  7141            NA 310  Instrument Air to Contain.                  CV  5393        NA                AOV  5392          60 0
~o 311  Service Water from "B" fan cooler            MV  4630(16)    NA                                    NA 312  Service Water to "D" fan cooler              MV  4642(16)                                          NA.
313  Ieakage  test depressurization              flange          NA                MOV  7444      NA  Normally Closed
 
MAXIMUM                  MAXDIUM PENT.                                      ISOZATION    ISOZATION              ISOZATION NO. IDENTIFICATION/DESCBIPTION                        TIME *(SEC)            TIME *(SEC)
Service Water fran "C" fan cooler    MV  4643(16) 316  Service Water to "B" fan cooler      MV  4628(16) 317  Leakage  test supply                  flange                  MOV  7443  Nh. Normally Closed 318  Dead  weight tester (deccmissioned)  welded shut              welded shut Service Water frcm "A" fan cooler    MV  4629(16) 320  Service water  to  "C" fan cooler    MV  4647(16) 321  A S/G Blmrdown                        AOV 5738        60      MV  5701(7)
~ 322  B S/G Blcwdown                        AOV 5737        60      MV  5702(7) 323  Service Water frcm "D" fan cooler    MV  4644(16) 324  Demineralized water  to Containment  CV 8419                  AOV 8418 332  Cont. Press. Trans. PT-944, 949 6 950 PT 944                  MV 1819G PT 949                  MV 1819F 332  Leakage  test and hydrogen instrumentation lines mnitor PT 950 MV 7448 MV 7452 MV 1819E cap cap
                                                                                                    .0 MV 7456                  cap SOV 921                  (21)
SOV 922                  (21)
SOV 923                  (21)
SOV 924                  (21)
 
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(21) Acceptable isolation capability is provided for instrument lines by two isolation boundaries outside containment. One of the boundaries outside containment may be a Seismic Class 1 closed system which is subjected to Type C leak rate testing.
(22) The flanges  at penetrations 204 and 300 can only be removed at cold or refueling shutdown. The flanges and associated double seals provide containment isolation and are a containment boundary for all modes of operation between cold shutdown and normal operation. During cold and refueling shutdown when the flanges are removed integrity is provided by the 48 inch valves.
3.6-11                  Proposed
 
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~ v 3.8  REFUEZING A    licabilit Applies to operating limitations during refueling operations.
          ~b'o ensure  that no incident could occur during refueling operations that would affect public health and safety.
3.8.1 During refueling operations the following conditions shall  be  satisfied.
a  ~    The equipment door,  or a closure plate that restricts air flow from the containment, and at least one personnel door in the equipment door or closure plate and in the personnel air lock shall be properly closed. In addition, all automatic containment isolation valves shall be operable or at least one valve in each line I
shall be',locked closed. The" 48 inch "shutdown lt purge valves must also be operable or closed or the associated flange must be installed'.
II
: b.      Radiation levels in the containment shall be monitored continuously.
c  ~    Core subcritical neutron flux shall be contin-uously monitored by at least two source range neutron monitors, each with continuous visual    .
indication in the control room and one with audible indication in the contairpnent and control room available whenever core geometry is being changed. When core geometry is not being changed at 3.8-1              Proposed
 
v shutdown and depressurized    until repairs  are effected and the  local leakage  meets the acceptance  criterion.
4.4.2.4  Test Fre uenc a    ~  Except as specified    in b., c., and d. below, individual penetrations and containment isolation valves shall be tested during each reactor shutdown for refueling, or other convenient intervals, but in no case at, intervals greater than two years.
: b.      The containment equipment hatch, fuel transfer tube, and shutdown purge system flanges shall be tested at each refueling shutdown or after each n
          ~  'i use, if, that .be sooner.
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          < c i
The, containment,air'o'cks'hall be tested at,
                          ~',-
intervals of no more than six months by pressurizing the space between the air lock doors. In addition, following opening of the air lock door during the interval, a test shall be performed by pressurizing between the dual seals of each door opened, within 48 hours of the opening, unless the reactor was in the cold shutdown condition at the time of the opening or has been subsequently brought to the cold shutdown condition. A test shall also be performed by pressurizing between the dual seals of each door within 48 hours of leaving the cold shutdown condition, unless the doors have not been open since the    last test performed either by pressurizing the space between the air lock doors or by pressurizing between the dual door seals.
4.4-7                      Proposed
 
4.4.3   Recirculation   e t e ov   l S stems 4.4.3.1 Test a ~   The portion of the residual heat removal system that is outside the containment shall either be tested by use in normal operation or hydrostati-cally tested at 350 psig at the interval specified in 4.4.3.4.
: b. Suction piping from containment sump B to the reactor coolant drain tank pump and the discharge piping from the pumps to the residual heat removal system shall be hydrostatically gested at go less that 100 psig at the interval specified
                                              )
in $ .4.3.4.
: 4. 4-,8                 Proposed
 
Attachment B Containment purge and vent operations became a generic concern in 1978. Since that time containment purge and vent has been the subject of many letters between the Staff and Rochester Gas and Electric Corp. (RG&E). In Reference 1, the Staff transmitted to RGSE a Safety Evaluation Report (SER) which found RGE's interium commitments   to be acceptable. The SER provides a good summary of the correspondance   and the commitments made concerning this subject.
The existing purge and vent systems at Ginna consist of a 48 inch purge system and a 6 inch containment vent (depressurization) system. The major issue concerning the purge system is the operability of the 48 inch purge valves during a design basis accident   loss of coolant accident (DBA-LOCA). Therefore, RGGE has committed   to maintaining the 48 inch purge valves closed while the reactor is critical until information demonstrating operability is submitted.
In response to the Staff's request to limit purge/vent operations to safety-related needs RG6E committed to limiting vent system operation to a total of 90 hours per year.
To permanently resolve the purge and vent issue RG6E has decided to modify the 48 inch purge system so that     it will only be used when the reactor is in cold or refueling shutdown, and install a mini-purge system which will allow unlimited purging of containment.
The technical specification changes presented in Attachment A are necessary to implement these modifications.
The technical specification changes presented in Attachment A are necessary to implement these modifications.
The following changes will be made to the 48 inch purge system: The inboard 48 inch, butterfly-type containment isolation valves from both the supply and exhaust lines will be removed.Each valve will be replaced with a, special blind-flange type closure utilizing double 0-ring seals to provide redundant containment isolation barriers.Test ports will be provided.to permit peri-odic local leak rate testing of the double,O-ring seal."The blind flange closures will be securely bolted,in place,,dur'ing
The following changes will be made to the 48 inch purge system:
.reactor operation and will only be'removed during plant shutdowns.
The inboard 48 inch, butterfly-type containment isolation valves from both the supply and exhaust lines will be removed. Each valve will be replaced with a, special blind-flange type closure utilizing double 0-ring seals to provide redundant containment isolation barriers. Test ports will be provided.to permit       peri-odic local leak rate testing of the double,O-ring     seal. "The blind flange closures will be securely bolted,in place,,dur'ing   .
reactor operation and will only be'removed during plant shutdowns.
The existing outboard 48 inch, butterfly-type automatic containment.
The existing outboard 48 inch, butterfly-type automatic containment.
isolation valves will remain in place to provide an isolation barrier during refueling operations.
isolation valves will remain in place to provide an isolation barrier during refueling operations.
Since the blank flanges have a double seal, it will no longer be necessary to rely on the outer 48 inch valves for containment isolation during power operation.
Since the blank flanges have a double seal,     it will no longer be necessary to rely on the outer 48 inch valves for containment isolation during power operation. During cold or refueling shutdown, the flanges could be removed and the outer valves will be relied upon for refueling integrity. Since the 48 inch valves are no longer relied upon for containment integrity the mechanical stops on the valves will be removed. These stops were installed to reduce stresses in the valves resulting from closure during a DBA-LOCA. Since the valves 'are no longer subject to a DBA-LOCA there is no reason to continue restricting air flow in the 48 inch system during shutdown.
During cold or refueling shutdown, the flanges could be removed and the outer valves will be relied upon for refueling integrity.
 
Since the 48 inch valves are no longer relied upon for containment integrity the mechanical stops on the valves will be removed.These stops were installed to reduce stresses in the valves resulting from closure during a DBA-LOCA.Since the valves'are no longer subject to a DBA-LOCA there is no reason to continue restricting air flow in the 48 inch system during shutdown.
II M I         II II I't I
II M I II II I't I I A new mini-purge system will be installed to provide the capability to purge containment atmosphere during all modes of reactor'peration.
I
This 2000-cfm mini-purge system will consist of a pair of redundant blowers for supplying'air to the containment through existing 6-inch Integrated Leak Rate Test (ILRT)vent line penetration 309."New 6 i*nch, air'-.operated, butterfly-type, inboard and outboar'd automatic containment isolation valves will be installed at penetration 309.Air will be exhausted through the existing 6 inch depressurization penetration 132 and will be ducted into the Auxiliary Building ventilation system where it will be filtered and monitored prior to its release to the envi-ronment via the plant vent.The existing 6 inch valves at pene-tration 132 will be replaced with new 8 inch, air-operated, butterfly-type, inboard and outboard containment.
 
isolation valves.All four new containment isolation valves will be automatic and will be fully-qualified to close within 5 seconds from the time the isolation setpoint is reached against the maximum containment pressures anticipated during a DBA-LOCA.The inboard ends of the mini-purge supply and exhaust lines will be equipped with 1/2-inch mesh debris screens.The radiation accident monitor R-12A (Containment Purge)monitors the 48 inch purge exhaust.Since the 48 inch purge will only be operable during cold and refueling shutdown, R-12A need only be operable during cold and refueling shutdown.Therefore, Table 3.5-7 was modified to be consistant with operation of the shutdown purge system.In accordance with 10 CFR 50.91, these changes to the Technical Specifications have been evaluated against three criteria to determine if the operation of the facility in accordance with 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 from any accident previously evaluated; or 3.involve a significant reduction in a margin of safety.The modification does not involve an increase in the probability or consequences of an accident previously evaluated.
A new mini-purge system will be installed to provide the capability to purge containment atmosphere during all modes of This 2000-cfm mini-purge system will consist of a reactor'peration.
Installing a mini-purge system and installing flanges on the 48 inch valves does not increase the probability of an accident because the flanges eliminate the effects of any malfunction of the 48 inch valves and the new mini-purge valves are small and inherently more reliable than the 48.inch valves.The consequences of any previously evaluated accident are not increased by the modification because the flanges prevent any accident associated with the 48 inch system and clearly any accident associated with the mini-purge system is less limiting than an accident associated with the 48 inch sytem.
pair of redundant blowers for supplying'air to the containment through existing 6-inch Integrated Leak Rate Test (ILRT) vent line penetration 309. "New 6 i*nch, air'-. operated, butterfly-type, inboard and outboar'd automatic containment isolation valves will be installed at penetration 309. Air will be exhausted through the existing 6 inch depressurization penetration 132 and will be ducted into the Auxiliary Building ventilation system where will be filtered and monitored prior to its release to the envi-it ronment via the plant vent. The existing 6 inch valves at pene-tration 132 will be replaced with new 8 inch, air-operated, butterfly-type, inboard and outboard containment. isolation valves.
0~V I f''I k li l, I'l';t b b lf P The modification does not create the possibility of a new or different kind of accident.Replacing the 48 inch purge system with a mini-purge system basically decreases the size of the purge system and therefore does not create a new or different kind of accident.The modification does not significantly reduce the margin of safety because the con'sequences of any accident with the mini-purge system would be less severe than an accident associated with the 48 inch system.As outlined above, Rochester Gas and Electric submits that the issues associated with this amendment request are outside the criteria of 10 CFR 50.91, and therefore, a no significant hazards finding is warranted.
All four new containment isolation valves will be automatic and will be fully-qualified to close within 5 seconds from the time the isolation setpoint is reached against the maximum containment pressures anticipated during a DBA-LOCA. The inboard ends of the mini-purge supply and exhaust lines will be equipped with 1/2-inch mesh debris screens.
Reference 1 NRC letter from D.M.Crutchfield to R.W.Kober,"Completion of Generic Issue On Containment Purge and Vent Operation" June 21, 1984.3}}
The radiation accident monitor R-12A (Containment Purge) monitors the 48 inch purge exhaust. Since the 48 inch purge will only be operable during cold and refueling shutdown, R-12A need only be operable during cold and refueling shutdown. Therefore, Table 3.5-7 was modified to be consistant with operation of the shutdown purge system.
In accordance with 10 CFR 50.91, these changes to the Technical Specifications have been evaluated against three criteria to determine if the operation of the facility in accordance with 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 from any accident previously evaluated; or
: 3. involve a significant reduction in a margin of safety.
The modification does not involve an increase in the probability or consequences of an accident previously evaluated. Installing a mini-purge system and installing flanges on the 48 inch valves does not increase the probability of an accident because the flanges eliminate the effects of any malfunction of the 48 inch valves and the new mini-purge valves are small and inherently more reliable than the 48. inch valves. The consequences of any previously evaluated accident are not increased by the modification because the flanges prevent any accident associated with the 48 inch system and clearly any accident associated with the mini-purge system is less limiting than an accident associated with the 48 inch sytem.
 
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The modification does not create the possibility of a new or different kind of accident. Replacing the 48 inch purge system with a mini-purge system basically decreases the size of the purge system and therefore does not create a new or different kind of accident.
The modification does not significantly reduce the margin of safety because the con'sequences of any accident with the mini-purge system would be less severe than an accident associated   with the 48 inch system.
As outlined above, Rochester Gas and Electric submits that the issues associated with this amendment request are outside the criteria of 10 CFR 50.91, and therefore, a no significant hazards finding is warranted.
Reference 1   NRC letter from D.M. Crutchfield to R.W. Kober, "Completion of Generic Issue On Containment Purge and Vent Operation" June 21, 1984.
3}}

Latest revision as of 11:39, 4 February 2020

Proposed Tech Specs,Incorporating New Containment mini-purge Sys & Deleting Requirements Associated W/Old 48-inch Containment Purge Sys
ML17254A603
Person / Time
Site: Ginna Constellation icon.png
Issue date: 10/22/1985
From:
ROCHESTER GAS & ELECTRIC CORP.
To:
Shared Package
ML17254A600 List:
References
NUDOCS 8510220379
Download: ML17254A603 (21)


Text

Attachment A Revise the Technical Specification pages as follows:

Remove Insert 3.5-22 3.5-22 3.6-5 3.6-5 3.6-6 3.6-6 3.6-7 3.6-7 3".6-7A

'.6-11 3.6-11 3.8-1 3.8-1 4.4-7 4.4-7 4.4-8 4.4-8 jjg102>.

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PQOCK 0g000244 o PQR DR P

I TABLE 3.5-7, Radiation Accident Monitorin Instrumentation Minimum Channels Instrument ~Oerable Action

1. Containment Area (R-29 and R-30)
2. Noble Gas Effluent Monitors Plant Vent (R-14) ii. A Main Steam Line (R-31) iii. B Main Steam Line (R-32) iv. Containment Purge (R-12A) v ~ Air Ejector (R-15A)

Action Statements Action 1 With the number of operable channels less than required by the Minimum Channels Operable requirements, either restore the inoperable channel(s) to operable status within 7 days of the event, or prepare and submit a Special Report to the Commission within 30 days following the event outlining the action taken, the cause of the inoperability and the plans and schedule for restoring the system to operable status.

  • only when the shutdown purge system flanges are removed.

3.5-22 Proposed

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MAXKMUM MMGMUM PENT. ISOZATION ISOZATION ISOZATION ISOZATION NO. IDENTIFICATION/DESCRIPTION BOUNDARY TIME *(SEC) BOUNDAHY TIME *(SEC) 121 Nitrogen to PRT CV 528 MV 547(8) 121 Reactor Makeup water to PRT CV 529 AOV 508 60 121 Cont. Press. transmitter PT-945 (10) PT 945 MV 1819A 121 Cont. Press. transmitter PT-946 (10) PT 946 MV 1819B 123 Reactor Coolant Drain Tank (RCDT) to (R AOV 1789 60 MV 1655(7) 124 Excess letdown supply and return AOV 745 60 to heat exchanger CV 743 124 Post Accident air sample "C" fan MV 1569 MV 1571 MV 1572 MV 1574

..125 Canponent Gooling Water (CW) fran 1B RCP MOV 759B (12) 126 QOW fran 1A RCP MOV 759A (12) 127 CV 750A MOV 749A 60 128 CV 750B MOV 749B 60 e 129 E

RCDT 8( PRT to Vent Header AOV 1787 60 AQV 1786 60 CV 1713 g 130 -

CCW to reactor support cooling MOV 813 60 131 QOW to reactor support cooling MOV 814 60 (19) 132 blini-Purge exhaust AOV 7970 AOV 7971 140 --RHR pump suction fran "A" Hot leg MOV 701(20) (6)

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C MAXIMUM HAXIMUM PENT. ISOLATION ISOLATION ISOLATION ISOLATION NO. IDENTIFICATION/DESCRIPTION BOUNDARY TIME ='(SEC) BOUNDARY TIME "-(SEC) 141 RHR-//1 pump suction from Sump B MOV 850A(13) NA MOV 851A(13) NA 142 RHR-jj2 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 6 B MV 4757(16) NA MV 4636(16) NA NA 202 "B" Hydrogen recombiner (pilot 6 main) MV 1076B NA SOV IV-3B NA Normally Closed MV 1084B NA SOV IV-5B NA Normally 'Closed 203 Contain, Press. transmitter PT-947 S 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 flange (22) NA AOV 5869 (22) 205 Hot leg loop sample AOV 966C 60 MV 956D(14) NA 206 Zrzr. liquid space sample AOV 966B 60 MV 956E(14) NA 206 "A" S/G sample AOV 5735 60 MV 5733(7) NA 207 Przr. Steam space sample AOV 966A 60 MV 956F NA 0

207 "B" S/G sample AOV 5736 60 MV 5734(7) .NA 209 Reactor Compart. cooling Units A 8 B MV 4758(16) NA NA MV 4635(16) NA NA 210 Oxygen makeup to A 8 B recombiners MV 1080A NA SOV IV-2A NA Normally Closed SOV IV-2B NA Normally Closed

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MAXIMUM MAXIMUM PENT. ISOLATION IsoLAnom

- -IsoLAnoN IsoI,Anom No. IDENTIFICATION/DESCRIPTION BOUNDARY TIME " (SEC) BOUNDARY TIME "(SEC) 300 Shutdown Purge Exhaust Duct flange (22) NA AOV 5879 (22) 301 Aux. steam supply to containment MV 6151 NA - MV 6165(15) NA 303 Aux. steam condensate return MV 6175 NA -MV 6152(15) NA 304 "A" Hydrogen recombiner (pilot and main) MV 1084B NA SOV IV-5A NA Normallly Clos~

MV 1076A NA . SOV XV-3A NA NormaU.ly Clo~

305 Radiation Monitors R-ll, R-12 S R-10A AOV 1597 60 ~

MV 1596 NA Auto Inlet Isol.

305 R-ll, R-12 S R-10A Outlet AOV 1599 60 AOV 1598 60 305 Post Accident air sampler (containment) MV 1554 NA MV 1556 60 MV 1557 NA MV 1559 NA MV 1560 NA MV 1562 NA

't 307 Fire Service Water CV 9229 NA -AOV 9227 (18) 308 Service Water to "A" fan cooler MV 4627(16) NA NA 309 Mini-Purge supply AOV 7478 AOV 7445 310 Service Air to Contain. CV 7226 NA MV 7141 NA 310 Instrument Air to Contain. CV 5393 NA AOV 5392 60 0

~o 311 Service Water from "B" fan cooler MV 4630(16) NA NA 312 Service Water to "D" fan cooler MV 4642(16) NA.

313 Ieakage test depressurization flange NA MOV 7444 NA Normally Closed

MAXIMUM MAXDIUM PENT. ISOZATION ISOZATION ISOZATION NO. IDENTIFICATION/DESCBIPTION TIME *(SEC) TIME *(SEC)

Service Water fran "C" fan cooler MV 4643(16) 316 Service Water to "B" fan cooler MV 4628(16) 317 Leakage test supply flange MOV 7443 Nh. Normally Closed 318 Dead weight tester (deccmissioned) welded shut welded shut Service Water frcm "A" fan cooler MV 4629(16) 320 Service water to "C" fan cooler MV 4647(16) 321 A S/G Blmrdown AOV 5738 60 MV 5701(7)

~ 322 B S/G Blcwdown AOV 5737 60 MV 5702(7) 323 Service Water frcm "D" fan cooler MV 4644(16) 324 Demineralized water to Containment CV 8419 AOV 8418 332 Cont. Press. Trans. PT-944, 949 6 950 PT 944 MV 1819G PT 949 MV 1819F 332 Leakage test and hydrogen instrumentation lines mnitor PT 950 MV 7448 MV 7452 MV 1819E cap cap

.0 MV 7456 cap SOV 921 (21)

SOV 922 (21)

SOV 923 (21)

SOV 924 (21)

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(21) Acceptable isolation capability is provided for instrument lines by two isolation boundaries outside containment. One of the boundaries outside containment may be a Seismic Class 1 closed system which is subjected to Type C leak rate testing.

(22) The flanges at penetrations 204 and 300 can only be removed at cold or refueling shutdown. The flanges and associated double seals provide containment isolation and are a containment boundary for all modes of operation between cold shutdown and normal operation. During cold and refueling shutdown when the flanges are removed integrity is provided by the 48 inch valves.

3.6-11 Proposed

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~ v 3.8 REFUEZING A licabilit Applies to operating limitations during refueling operations.

~b'o ensure that no incident could occur during refueling operations that would affect public health and safety.

3.8.1 During refueling operations the following conditions shall be satisfied.

a ~ The equipment door, or a closure plate that restricts air flow from the containment, and at least one personnel door in the equipment door or closure plate and in the personnel air lock shall be properly closed. In addition, all automatic containment isolation valves shall be operable or at least one valve in each line I

shall be',locked closed. The" 48 inch "shutdown lt purge valves must also be operable or closed or the associated flange must be installed'.

II

b. Radiation levels in the containment shall be monitored continuously.

c ~ Core subcritical neutron flux shall be contin-uously monitored by at least two source range neutron monitors, each with continuous visual .

indication in the control room and one with audible indication in the contairpnent and control room available whenever core geometry is being changed. When core geometry is not being changed at 3.8-1 Proposed

v shutdown and depressurized until repairs are effected and the local leakage meets the acceptance criterion.

4.4.2.4 Test Fre uenc a ~ Except as specified in b., c., and d. below, individual penetrations and containment isolation valves shall be tested during each reactor shutdown for refueling, or other convenient intervals, but in no case at, intervals greater than two years.

b. The containment equipment hatch, fuel transfer tube, and shutdown purge system flanges shall be tested at each refueling shutdown or after each n

~ 'i use, if, that .be sooner.

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The, containment,air'o'cks'hall be tested at,

~',-

intervals of no more than six months by pressurizing the space between the air lock doors. In addition, following opening of the air lock door during the interval, a test shall be performed by pressurizing between the dual seals of each door opened, within 48 hours5.555556e-4 days <br />0.0133 hours <br />7.936508e-5 weeks <br />1.8264e-5 months <br /> of the opening, unless the reactor was in the cold shutdown condition at the time of the opening or has been subsequently brought to the cold shutdown condition. A test shall also be performed by pressurizing between the dual seals of each door within 48 hours5.555556e-4 days <br />0.0133 hours <br />7.936508e-5 weeks <br />1.8264e-5 months <br /> of leaving the cold shutdown condition, unless the doors have not been open since the last test performed either by pressurizing the space between the air lock doors or by pressurizing between the dual door seals.

4.4-7 Proposed

4.4.3 Recirculation e t e ov l S stems 4.4.3.1 Test a ~ The portion of the residual heat removal system that is outside the containment shall either be tested by use in normal operation or hydrostati-cally tested at 350 psig at the interval specified in 4.4.3.4.

b. Suction piping from containment sump B to the reactor coolant drain tank pump and the discharge piping from the pumps to the residual heat removal system shall be hydrostatically gested at go less that 100 psig at the interval specified

)

in $ .4.3.4.

4. 4-,8 Proposed

Attachment B Containment purge and vent operations became a generic concern in 1978. Since that time containment purge and vent has been the subject of many letters between the Staff and Rochester Gas and Electric Corp. (RG&E). In Reference 1, the Staff transmitted to RGSE a Safety Evaluation Report (SER) which found RGE's interium commitments to be acceptable. The SER provides a good summary of the correspondance and the commitments made concerning this subject.

The existing purge and vent systems at Ginna consist of a 48 inch purge system and a 6 inch containment vent (depressurization) system. The major issue concerning the purge system is the operability of the 48 inch purge valves during a design basis accident loss of coolant accident (DBA-LOCA). Therefore, RGGE has committed to maintaining the 48 inch purge valves closed while the reactor is critical until information demonstrating operability is submitted.

In response to the Staff's request to limit purge/vent operations to safety-related needs RG6E committed to limiting vent system operation to a total of 90 hours0.00104 days <br />0.025 hours <br />1.488095e-4 weeks <br />3.4245e-5 months <br /> per year.

To permanently resolve the purge and vent issue RG6E has decided to modify the 48 inch purge system so that it will only be used when the reactor is in cold or refueling shutdown, and install a mini-purge system which will allow unlimited purging of containment.

The technical specification changes presented in Attachment A are necessary to implement these modifications.

The following changes will be made to the 48 inch purge system:

The inboard 48 inch, butterfly-type containment isolation valves from both the supply and exhaust lines will be removed. Each valve will be replaced with a, special blind-flange type closure utilizing double 0-ring seals to provide redundant containment isolation barriers. Test ports will be provided.to permit peri-odic local leak rate testing of the double,O-ring seal. "The blind flange closures will be securely bolted,in place,,dur'ing .

reactor operation and will only be'removed during plant shutdowns.

The existing outboard 48 inch, butterfly-type automatic containment.

isolation valves will remain in place to provide an isolation barrier during refueling operations.

Since the blank flanges have a double seal, it will no longer be necessary to rely on the outer 48 inch valves for containment isolation during power operation. During cold or refueling shutdown, the flanges could be removed and the outer valves will be relied upon for refueling integrity. Since the 48 inch valves are no longer relied upon for containment integrity the mechanical stops on the valves will be removed. These stops were installed to reduce stresses in the valves resulting from closure during a DBA-LOCA. Since the valves 'are no longer subject to a DBA-LOCA there is no reason to continue restricting air flow in the 48 inch system during shutdown.

II M I II II I't I

I

A new mini-purge system will be installed to provide the capability to purge containment atmosphere during all modes of This 2000-cfm mini-purge system will consist of a reactor'peration.

pair of redundant blowers for supplying'air to the containment through existing 6-inch Integrated Leak Rate Test (ILRT) vent line penetration 309. "New 6 i*nch, air'-. operated, butterfly-type, inboard and outboar'd automatic containment isolation valves will be installed at penetration 309. Air will be exhausted through the existing 6 inch depressurization penetration 132 and will be ducted into the Auxiliary Building ventilation system where will be filtered and monitored prior to its release to the envi-it ronment via the plant vent. The existing 6 inch valves at pene-tration 132 will be replaced with new 8 inch, air-operated, butterfly-type, inboard and outboard containment. isolation valves.

All four new containment isolation valves will be automatic and will be fully-qualified to close within 5 seconds from the time the isolation setpoint is reached against the maximum containment pressures anticipated during a DBA-LOCA. The inboard ends of the mini-purge supply and exhaust lines will be equipped with 1/2-inch mesh debris screens.

The radiation accident monitor R-12A (Containment Purge) monitors the 48 inch purge exhaust. Since the 48 inch purge will only be operable during cold and refueling shutdown, R-12A need only be operable during cold and refueling shutdown. Therefore, Table 3.5-7 was modified to be consistant with operation of the shutdown purge system.

In accordance with 10 CFR 50.91, these changes to the Technical Specifications have been evaluated against three criteria to determine if the operation of the facility in accordance with 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 from any accident previously evaluated; or
3. involve a significant reduction in a margin of safety.

The modification does not involve an increase in the probability or consequences of an accident previously evaluated. Installing a mini-purge system and installing flanges on the 48 inch valves does not increase the probability of an accident because the flanges eliminate the effects of any malfunction of the 48 inch valves and the new mini-purge valves are small and inherently more reliable than the 48. inch valves. The consequences of any previously evaluated accident are not increased by the modification because the flanges prevent any accident associated with the 48 inch system and clearly any accident associated with the mini-purge system is less limiting than an accident associated with the 48 inch sytem.

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The modification does not create the possibility of a new or different kind of accident. Replacing the 48 inch purge system with a mini-purge system basically decreases the size of the purge system and therefore does not create a new or different kind of accident.

The modification does not significantly reduce the margin of safety because the con'sequences of any accident with the mini-purge system would be less severe than an accident associated with the 48 inch system.

As outlined above, Rochester Gas and Electric submits that the issues associated with this amendment request are outside the criteria of 10 CFR 50.91, and therefore, a no significant hazards finding is warranted.

Reference 1 NRC letter from D.M. Crutchfield to R.W. Kober, "Completion of Generic Issue On Containment Purge and Vent Operation" June 21, 1984.

3