ML19309A457: Difference between revisions

From kanterella
Jump to navigation Jump to search
(Created page by program invented by StriderTol)
(StriderTol Bot change)
 
(One intermediate revision by the same user not shown)
Line 13: Line 13:
| document report number = NUDOCS 8003310105
| document report number = NUDOCS 8003310105
| package number = ML19309A455
| package number = ML19309A455
| document type = REPORTABLE OCCURRENCE REPORT (SEE ALSO AO,LER), TEXT-SAFETY REPORT
| document type = REPORTABLE OCCURRENCE REPORT (SEE ALSO AO LER), TEXT-SAFETY REPORT
| page count = 9
| page count = 9
}}
}}
Line 19: Line 19:
=Text=
=Text=
{{#Wiki_filter:~
{{#Wiki_filter:~
L. O                                                                                                         .
L. O WISCOREln Elactac rosca coueur
WISCOREln Elactac rosca coueur                                                       ecember 30, 1975
?31 WEST MICHIGAN,f/.lLWAUKEE, WISCONSIN 53201
            ?31 WEST MICHIGAN,f/.lLWAUKEE, WISCONSIN 53201     [.p ,
[.,
                                                              'f             .              'D   '
ecember 30, 1975 p
                                                                                                                        . e . . . ..
'f
g/              % ..                  .,
'D g/
14r. Benard C. Rusche, Cirector             C     s.!; , 'l ,-~     .,
. e.....
                                                                                                                            '    'r Office of fluclear Reactor Regulation /
14r. Benard C. Rusche, Cirector C
                                                                                                              'd[l U. S. !!uclear Regulatory Conmission O < ' , '
s.!;, 'l,-~
                                                                                            <                                    (sij}
'r U. S. !!uclear Regulatory Conmission O < ', '
                                                                                                              -4                       '.      'JA
'd[l (sij}
              !!ashington, D. C. 20555                     \."
Office of fluclear Reactor Regulation /
j                         ,
'JA
                                                                                                                          'i i97e...;;.y
-4
!!ashington, D. C.
20555
\\.
j


==Dear fir. Rusche:==
==Dear fir. Rusche:==
                                                        , ,                  . ' u"{f').             . ./q LICE:lSEE EVEllT REPORT T10. 50-266/75-18                               $'                          (
. ' u"{f').
b&
i97e...;;.y
FAILED FUEL Iti ASSE;;BLY D-03, POSITION K-6, CYCLE 3                                                   .d .19. ''
../q
POINT BEACH ?mCLEAR PLAflT This letter is to report in detail the discovery and results of sub-sequent investigation of a failed fuel assembly during 17,                          the1975.
'i
Cycle 3-4 An refuel-initial ing of Unit 1 at Point Beach         I!uclear Plant on Decemberto comply with the ten-day report of this event '..Ts filed December 23, 1975 rt. porting requirenants of the Point Beach Technical Specification Section 15.6.6.A.2.
(
On Decerber 17, 1975, during the refueling of Unit 1, the Core Load-ing Supervisor noted sorething protruding from the side of fuel assembly D-03 as it was being lowered into the fuel assembly upender. Fuel novement was stcpped innediately while the R.: actor Engineering Group representativeThe                              moved pre-the underwater TV carara in position to observe the affected area.                                       The liminary inspection indicated that a section of fuel rod was missing.
.d.19. ''
Reactor Engineer was notified of the finding after thich the subject assembly was coved to the fuel inspection periscope in the spent fuel pit where a more detailed exanination was made.
LICE:lSEE EVEllT REPORT T10. 50-266/75-18 b&
FAILED FUEL Iti ASSE;;BLY D-03, POSITION K-6, CYCLE 3 POINT BEACH ?mCLEAR PLAflT This letter is to report in detail the discovery and results of sub-sequent investigation of a failed fuel assembly during the Cycle 3-4 refuel-17, 1975.
An initial ing of Unit 1 at Point Beach I!uclear Plant on Decemberto comply with the ten-day 23, 1975 report of this event '..Ts filed December rt. porting requirenants of the Point Beach Technical Specification Section 15.6.6.A.2.
On Decerber 17, 1975, during the refueling of Unit 1, the Core Load-ing Supervisor noted sorething protruding from the side of fuel assembly D-03 Fuel novement was as it was being lowered into the fuel assembly upender.
stcpped innediately while the R.: actor Engineering Group representative moved the underwater TV carara in position to observe the affected area.
The pre-liminary inspection indicated that a section of fuel rod was missing.
The Reactor Engineer was notified of the finding after thich the subject assembly was coved to the fuel inspection periscope in the spent fuel pit where a more detailed exanination was made.
VISUAL EXA'4It!ATION OF FUEL ASSE"7LY C 03, EAST FACE, 12-17-75 The results of detailed visual examination of the fuel assembly are sunnarized below, starting with the top of the fuel assembly.
VISUAL EXA'4It!ATION OF FUEL ASSE"7LY C 03, EAST FACE, 12-17-75 The results of detailed visual examination of the fuel assembly are sunnarized below, starting with the top of the fuel assembly.
Top of the Fuel Asserbly Rods 12 and 13 were observed
Top of the Fuel Asserbly Rods 12 and 13 were observed *.o be slightly below other rods (approxi-aately 1/16") ar.d esduced spacing betuean rods 12 and 13 was evident.
                                                                  *.o be slightly below other rods (approxi-aately 1/16") ar.d esduced spacing betuean rods 12 and 13 was evident.
Top of Grid 1 Rods 12 and 13 shcwed indications of wear adjacent to grid flow vanes.
Top of Grid 1 Rods 12 and 13 shcwed indications of wear adjacent to grid flow vanes.
The vane at rod 13 uas partially worn away.
The vane at rod 13 uas partially worn away.
5.'L
5.'L PC->
PC->
?..,
        ?..,
t Q
t Q
8008310     .        306
8008310 306


            !!r. Benard C. Itusche                           December 30, 1975 At Grid 1 Rust narks were evident on the grid and rods 12 and 13. Clad of rods 12 and 13 worn away to the extent that fuel springs were visible be-hind slots in the grid.
!!r. Benard C. Itusche December 30, 1975 At Grid 1 Rust narks were evident on the grid and rods 12 and 13.
Clad of rods 12 and 13 worn away to the extent that fuel springs were visible be-hind slots in the grid.
Below Grid 1 A fuel fra5nent was observed to be lodged between rods 13 and 14.
Below Grid 1 A fuel fra5nent was observed to be lodged between rods 13 and 14.
Gouge marks could be seen in rods 12 and 13 adjacent to grid tab and a hole was visible in rod 12 at grid tab. A tab was touching rods.12 and 13 and a narrow gap exists between rods 12 and 13.
Gouge marks could be seen in rods 12 and 13 adjacent to grid tab and a hole was visible in rod 12 at grid tab. A tab was touching rods.12 and 13 and a narrow gap exists between rods 12 and 13.
l           Between Grids 1 and 2 1
l Between Grids 1 and 2 f!o apparent damage to rods was noticeable at,this location, but 1
f!o apparent damage to rods was noticeable at,this location, but the spacing between rods 12 and 13 was reduced'.
the spacing between rods 12 and 13 was reduced'.
Top of Grid 2 4
Top of Grid 2 4
>                      The cladding of rod 12 was separated near vane with no cladding or fuel behind the upper part of grid. Rod i3 has a cut nark near upper edge of the clad and a hole on the left side. A fuel fragnent was visible between rods 13 and 14. The vane near rod 12 was bent in slightly.
The cladding of rod 12 was separated near vane with no cladding or fuel behind the upper part of grid.
At Grid 2 The spring for rod 12 was missing. Fuel fragnents and open clad on rod 13 was visible at this location.
Rod i3 has a cut nark near upper edge of the clad and a hole on the left side.
A fuel fragnent was visible between rods 13 and 14. The vane near rod 12 was bent in slightly.
At Grid 2 The spring for rod 12 was missing.
Fuel fragnents and open clad on rod 13 was visible at this location.
Below Grid 2 A two-inch sect on of clad for rod 12 from behind the grid had slipped down and pinr.ed between the grid and the lower section of rod 12.
Below Grid 2 A two-inch sect on of clad for rod 12 from behind the grid had slipped down and pinr.ed between the grid and the lower section of rod 12.
This rod has several holes natching the contact points of the grid springs.
This rod has several holes natching the contact points of the grid springs.
              "o fuel was visible.
"o fuel was visible.
Rod 13 has a hole under the grid tab with an outline similar to the tab.
Rod 13 has a hole under the grid tab with an outline similar to the tab.
                                                                                      ~
~
                "atucen Grids 2 and 3 4                        About a four-inch open split in rod 13 with no fuel visible except at the top and of the split.
"atucen Grids 2 and 3 About a four-inch open split in rod 13 with no fuel visible except 4
;              'Tc6 of Grid 3 Open cut in cladding on rod 12 adjacent to -vane. The vane is severely worn down cn the side near rod 12.
at the top and of the split.
'Tc6 of Grid 3 Open cut in cladding on rod 12 adjacent to -vane.
The vane is severely worn down cn the side near rod 12.
4
4


    ~
Iir. Benard C. Rusche December 30. 1975
Iir. Benard C. Rusche                                         December 30. 1975 Complete separation of rod 13 at point just above grid with the section of rod between grids 2 and 3 resting on prid 3 between rod 12 and the second rod in from 12.
~
The section of clad for rod 13 that was behind the grid springs made contact. Also a lot of gouge marks are present on that section of clad. No fuel fragments are visible..
Complete separation of rod 13 at point just above grid with the section of rod between grids 2 and 3 resting on prid 3 between rod 12 and the second rod in from 12.
The section of clad for rod 13 that was behind the grid springs made contact. Also a lot of gouge marks are present on that section of clad.
No fuel fragments are visible..
A fuel fragnent was visible on top of the grid near rod 8.
A fuel fragnent was visible on top of the grid near rod 8.
At Grid 3 Missing grid spring for rod 13.
At Grid 3 Missing grid spring for rod 13.
No clad for rod 13 visible behind grid.
No clad for rod 13 visible behind grid.
Below Grid 3 Holes visible in rod 11 near grid tab. Large hole in rod 12 with large fuel fragment sticking out.
Below Grid 3 Holes visible in rod 11 near grid tab.
Section of cladding for rod 13 missing frcm behind grid. Fresh scrape narks on top edge of the existing rod 13 cladding. No fuel visible at top edge of this section of rod 13.
Large hole in rod 12 with large fuel fragment sticking out.
!        Between Grids 3 and 4 Rub nark on rod 13.
Section of cladding for rod 13 missing frcm behind grid.
Fresh scrape narks on top edge of the existing rod 13 cladding.
No fuel visible at top edge of this section of rod 13.
Between Grids 3 and 4 Rub nark on rod 13.
t Top of Grid 4 Uide gap between rods 12 and 13.
t Top of Grid 4 Uide gap between rods 12 and 13.
At Grid 4               '
At Grid 4 Center of grid spring for rod 12 separated.
Center of grid spring for rod 12 separated. Many small fuel frag-r.2nts visible behind grid at rods 12 and 13.
Many small fuel frag-r.2nts visible behind grid at rods 12 and 13.
L' ear in grid spring at rod 13.
L' ear in grid spring at rod 13.
Felow Grid 4                                                             ,
Felow Grid 4 Gouge narks and hole in rod 12.
Gouge narks and hole in rod 12. Fuel visible in hole. Rod 13 miss-ing completely from grid to midway between grids 4 and 5. Gouge marks on se     i rod in from rod 13.
Fuel visible in hole.
          ,Catween Grids 4 and 5 1
Rod 13 miss-ing completely from grid to midway between grids 4 and 5.
Top 11 inches of rod 13 missing. End of rod 13 bent to a horizon-tal condition about two inches 1cng.
Gouge marks on se rod in from rod 13.
 
i
: r. Ecnard C. I'usche                   -                                                                         #
,Catween Grids 4 and 5 1
                                                                          , December 30, 1975 Too of Grid 5
Top 11 inches of rod 13 missing.
                    !! car in rod 11 adjacent to vane. Rod 12 clad worn through 'at vane with vane worn down also.
End of rod 13 bent to a horizon-tal condition about two inches 1cng.
Rod 13 has an unusual ragged hole next to but not parallel to the edge of the grid vane. The vane is severely worn and bent.
: r. Ecnard C. I'usche
--4
, December 30, 1975 Too of Grid 5
!! car in rod 11 adjacent to vane.
Rod 12 clad worn through 'at vane with vane worn down also.
Rod 13 has an unusual ragged hole next to but not parallel to the edge of the grid vane.
The vane is severely worn and bent.
A piece of clad about one-half inch long is lodged between rod 14 crd the grid.
A piece of clad about one-half inch long is lodged between rod 14 crd the grid.
Eelow Grid 5                                     .
Eelow Grid 5 Rod 12 has a hole with gouge marks around it.
Rod 12 has a hole with gouge marks around it. A fuel fragment is visible in the hole.
A fuel fragment is visible in the hole.
Eelo.t Grid 6 Hole 'in rod 12. Couge marks and hole in rod 13 with fuel showing.
Eelo.t Grid 6 Hole 'in rod 12.
        ''otton Grid and I;czzle Rod 12 alr.ast bottcmed out and resting on bottom.       The normal rods are about 3/4 inch off the bottom.
Couge marks and hole in rod 13 with fuel showing.
''otton Grid and I;czzle Rod 12 alr.ast bottcmed out and resting on bottom.
The normal rods are about 3/4 inch off the bottom.
SL""'ARY OF FUEL ASSE",ELY D-03 OPERATlilG HISTORY A brief suntary of the operating history of fuel assembly D-03 is as follows:
SL""'ARY OF FUEL ASSE",ELY D-03 OPERATlilG HISTORY A brief suntary of the operating history of fuel assembly D-03 is as follows:
Fuel Assenbly Identification:
Fuel Assenbly Identification:
D-03
D-03
        ?rspressurized low parasitic design with fuel rods off the bottom nozzle.
?rspressurized low parasitic design with fuel rods off the bottom nozzle.
Fericated at !!estinghouse !!uclear Fuel Division, Cheswick, Pennsylvania.
Fericated at !!estinghouse !!uclear Fuel Division, Cheswick, Pennsylvania.
Da:e received on site: August 22, 1972
Da:e received on site: August 22, 1972
:nitial inspection revealed no abnornalities.
:nitial inspection revealed no abnornalities.
Leided into Unit 1, Cycle 2 at core location H-1.       Insert was a thiable plug device. Burnup during Cycle 2 was 7,071 M'!D/liTU.                       ~
Leided into Unit 1, Cycle 2 at core location H-1.
Leidad into Unit -1, Cycle 3 at core location Ve6. Insert was a thimble plug davice. Burnup during Cycle 3 was 16,306 !C!D/MTU.
Insert was a thiable plug device.
Burnup during Cycle 2 was 7,071 M'!D/liTU.
~
Leidad into Unit -1, Cycle 3 at core location Ve6.
Insert was a thimble plug davice. Burnup during Cycle 3 was 16,306 !C!D/MTU.
Tc:a1 buraup: 23,377 :".!D/MTU.
Tc:a1 buraup: 23,377 :".!D/MTU.
        'bre as no difficulty in the fuel handling operation during Refueling 2, which irc olved 0-03 and/or adjacent assemblies.
'bre as no difficulty in the fuel handling operation during Refueling 2, which irc olved 0-03 and/or adjacent assemblies.
l
l


    /   Hr. Benard C. Ruscha                                       December 30, 1975 DETAILED FUEL HAflDLIliG STEPS LEADING TO DISCOVERY OF OCCURRE!1CE
/
                  . Anonalous behavior was first noted during the fuel reloading se-quence when fuel assembly E-06 was being lowered into adjacent core position K-5. The operator noted some deflections of the order of 120 pounds in the load cell '..hich monitors the weight of the fuel assembly and mast. This occurrence is .10t particularly unusual as the assembly slides into its opening between four other assenblies. He also noted that this assembly was slightly higher in elevation (1/8" to 1/4") when it was positioned on the lower core support plate. Uhen it was observed that there was a section of fuel rod approximately 11 inches long missing from D-03, its forner location (K-6) was inspected and nothing abnormal was noted, assembly E-33 was then loaded into core position K-6. Fuel assenbly E-06 was then removed froi, core position K-5 to facilitate an inspection of the core support plate. A portion of fuel rod, approximately 11 inches long, was observed to be lying diagonally across the K-5 location.
Hr. Benard C. Ruscha December 30, 1975 DETAILED FUEL HAflDLIliG STEPS LEADING TO DISCOVERY OF OCCURRE!1CE
Assemblies in J-5 and L-5 (E-29 and G-24, respectively) were removed from the core to give clear access to the broken piece of rod. An air-operated vise grip was utilized to retrieve the rod.       Several small piles of debris were also noted and reno'v ed by using an underwater vacuun.
. Anonalous behavior was first noted during the fuel reloading se-quence when fuel assembly E-06 was being lowered into adjacent core position K-5.
Faces and corners of assemblies which could have been affected either during Cycle 3 operation of D-03 or during the fuel movements were inspected.
The operator noted some deflections of the order of 120 pounds in the load cell '..hich monitors the weight of the fuel assembly and mast.
This effort included the southwest ccrner of F-07; the southeast corner of E-33; the south face of G-24; the north face of E-29; the west face of F-25; and t!- .:est face of D-34. A small plug-like object was noted on top of the botton nozzle of F-07 and this was removed to the bottom of the refueling cavity where it was vacuumed. On D-34's west face several fuel fragments were observed uedged between the rods and grids.     Scratches were also noted
This occurrence is.10t particularly unusual as the assembly slides into its opening between four other assenblies.
  .      on D-34 in the area of the gross failure on adjacent fuel assenbly D-03.       There was no apparent failure to D-34. D-34 was later renoved permanently from the core per the preplanned refueling procedure.
He also noted that this assembly was slightly higher in elevation (1/8" to 1/4") when it was positioned on the lower core support plate. Uhen it was observed that there was a section of fuel rod approximately 11 inches long missing from D-03, its forner location (K-6) was inspected and nothing abnormal was noted, assembly E-33 was then loaded into core position K-6.
PR03ABLE CAUSE OF FUEL CLAD FAILURE The nuclear steam supply system vendor, Westinghouse, has stated that a nighly prcbable initiating Tactor for the fuel failure was water im-pingenent through the baffle plate while the failed assembly was in its origi-nal Cycle 2 position H-1. This problem was experienced previously at two for-eign nuclear plants.
Fuel assenbly E-06 was then removed froi, core position K-5 to facilitate an inspection of the core support plate.
Experience at the foreign plants has indicated that flow through the stitch weld joining in the baffle plate, or bolted baffle plates as may be the case at Point Beach, has occurred at locations similar to H-1.       This can result in a water inpincrent on the corner or near corner fuel rods of the assembly at this position, thus leading to vibration and fretting wear of one or more fuel rods.
A portion of fuel rod, approximately 11 inches long, was observed to be lying diagonally across the K-5 location.
In the Point Coach case, assembly D-03 occupied position H-1 during Cycle 2 before being moved to position Ps-6 for the ensuing Cycle 3. A small hole in the affected fuel rods due to Tretting from fuel rod vibration is postu-lated to have taken place prior to relocaticn of the assenbly into position K-6.
Assemblies in J-5 and L-5 (E-29 and G-24, respectively) were removed from the core to give clear access to the broken piece of rod.
The Cycle 3 position subjected the assably to.a masurably higher power rat-ing than in its Cycle .2 position.       ,
An air-operated vise grip was utilized to retrieve the rod.
Several small piles of debris were also noted and reno' ed by using an underwater vacuun.
v Faces and corners of assemblies which could have been affected either during Cycle 3 operation of D-03 or during the fuel movements were inspected.
This effort included the southwest ccrner of F-07; the southeast corner of E-33; the south face of G-24; the north face of E-29; the west face of F-25; and t!-.:est face of D-34.
A small plug-like object was noted on top of the botton nozzle of F-07 and this was removed to the bottom of the refueling cavity where it was vacuumed.
On D-34's west face several fuel fragments were observed uedged between the rods and grids.
Scratches were also noted on D-34 in the area of the gross failure on adjacent fuel assenbly D-03.
There was no apparent failure to D-34.
D-34 was later renoved permanently from the core per the preplanned refueling procedure.
PR03ABLE CAUSE OF FUEL CLAD FAILURE The nuclear steam supply system vendor, Westinghouse, has stated that a nighly prcbable initiating Tactor for the fuel failure was water im-pingenent through the baffle plate while the failed assembly was in its origi-nal Cycle 2 position H-1.
This problem was experienced previously at two for-eign nuclear plants.
Experience at the foreign plants has indicated that flow through the stitch weld joining in the baffle plate, or bolted baffle plates as may be the case at Point Beach, has occurred at locations similar to H-1.
This can result in a water inpincrent on the corner or near corner fuel rods of the assembly at this position, thus leading to vibration and fretting wear of one or more fuel rods.
In the Point Coach case, assembly D-03 occupied position H-1 during Cycle 2 before being moved to position Ps-6 for the ensuing Cycle 3.
A small hole in the affected fuel rods due to Tretting from fuel rod vibration is postu-lated to have taken place prior to relocaticn of the assenbly into position K-6.
The Cycle 3 position subjected the assably to.a masurably higher power rat-ing than in its Cycle.2 position.
I
I
_h
_h


11r. Benard C. Ruscha                                       December 30, 1975 The ' initial escalation to power at the beginning of Cycle 3 was at a rate higher than the present operating guidelines and a sharp increase in reactor coolant activity was noted between power levels of 40 to 50%. It is presumed that the fuel rods containing holes in the clad became water-logged during the shutdciin and burst due to steam pressure and/or the lack of suffi-cient time for the Zircaloy to plastically deform during the power escala-tion phase.
11r. Benard C. Ruscha December 30, 1975 The ' initial escalation to power at the beginning of Cycle 3 was at a rate higher than the present operating guidelines and a sharp increase in reactor coolant activity was noted between power levels of 40 to 50%.
SAFETY EVALUATIO;i A!!D CORRECTIVE ACTION Two potential safety concerns have been evaluated:       (1)   The poten-tial for and consequences of addi     t ional fuel failures and '(2) the effect of loose fuel pellets in the coolan; system on the health and safety of plant operating personnel and the public.
It is presumed that the fuel rods containing holes in the clad became water-logged during the shutdciin and burst due to steam pressure and/or the lack of suffi-cient time for the Zircaloy to plastically deform during the power escala-tion phase.
The first item requiring a safety evaluat[ ion is the potential for and the consequences of additional fuel failures of a'similar nature. If baffle inpingement at core location H-1 is the problem, a potential problem exists in two additional assenblies. Fuel assembly F-36 had been located in position H-1 during Cycle 3 and has been .ovad to position J-3 for Cycle 4 operation. Iew fuel asscmbly G-07 is presently located in position H-1 for Cycle 4 operation. Both assemblies will be carefully inspected at the end of Cycle 4 oper-ation.
SAFETY EVALUATIO;i A!!D CORRECTIVE ACTION Two potential safety concerns have been evaluated:
In reviewing the safety aspects of locating assembly F-36 at position J-3 during Cycle 4, it was confirmed that the assembly does not contain a con-trol rod in this position; therefore no possibility exists of a danaged fuel rod interferrinq with a control rod dropping action. A notable factor mitigating the possibility of cladding damage to this assembly during Cycle 4 is that some months ago Uestinghouse instigated guidelines governing the rate of power escala-tion following a cold shutdown of the reactor. These guidelines will be fol-lowed rigidly during future startups from the cold condition for Unit 1, Cycle 4.
(1)
The poten-tial for and consequences of addi ional fuel failures and '(2) the effect of t
loose fuel pellets in the coolan; system on the health and safety of plant operating personnel and the public.
The first item requiring a safety evaluat[ ion is the potential for and the consequences of additional fuel failures of a'similar nature.
If baffle inpingement at core location H-1 is the problem, a potential problem exists in two additional assenblies.
Fuel assembly F-36 had been located in position H-1 during Cycle 3 and has been.ovad to position J-3 for Cycle 4 operation.
Iew fuel asscmbly G-07 is presently located in position H-1 for Cycle 4 operation.
Both assemblies will be carefully inspected at the end of Cycle 4 oper-ation.
In reviewing the safety aspects of locating assembly F-36 at position J-3 during Cycle 4, it was confirmed that the assembly does not contain a con-trol rod in this position; therefore no possibility exists of a danaged fuel rod interferrinq with a control rod dropping action.
A notable factor mitigating the possibility of cladding damage to this assembly during Cycle 4 is that some months ago Uestinghouse instigated guidelines governing the rate of power escala-tion following a cold shutdown of the reactor.
These guidelines will be fol-lowed rigidly during future startups from the cold condition for Unit 1, Cycle 4.
The purpose of centrolled power escalation is to allow fuel rods which might have taken in water via pinhole leaks to expel the water, thus preventing the bursting of cladding due to steam pressure buildup within the fuel rod as appear nay have happened in this instance.
The purpose of centrolled power escalation is to allow fuel rods which might have taken in water via pinhole leaks to expel the water, thus preventing the bursting of cladding due to steam pressure buildup within the fuel rod as appear nay have happened in this instance.
It is considered that careful nonitoring of the reactor coolant activ-ity during reactor startup and later operation will provide the necessary informa-tion for nonitoring the condition of fuel assembly F-36, as well as the other fuel assemblies in the reactor. Reactor coolant system activity monitoring and allowable limits will be continued as prescribed by the Technical Specification.
It is considered that careful nonitoring of the reactor coolant activ-ity during reactor startup and later operation will provide the necessary informa-tion for nonitoring the condition of fuel assembly F-36, as well as the other fuel assemblies in the reactor.
The second item requiring safety evaluation is that of loose fuel pel-lets in the reactor ccolant system during subsequent plant operation. As de-scribcd previously, all reasonable attccpts to locate and renove loose pellets
Reactor coolant system activity monitoring and allowable limits will be continued as prescribed by the Technical Specification.
The second item requiring safety evaluation is that of loose fuel pel-lets in the reactor ccolant system during subsequent plant operation.
As de-scribcd previously, all reasonable attccpts to locate and renove loose pellets


December 30, 1975 lir. Cenard C. Rusche from adjacent fuel assemblics and the loner core support plate were performed.
lir. Cenard C. Rusche December 30, 1975 from adjacent fuel assemblics and the loner core support plate were performed.
flo known loose pellets. remained in the reactor vessel or on fuel remaining in the core. If there are any pellets or parts of pellets remaining in the reactor vessel they would be small fragments that traveled upward between the adja-cent fuel assenblies during Cycle 3 operation (assembly to assembly nominal clearance is .040 inches) or larger fragrants that dropped. to and through the lower core support plate when fuel was noved .during Cycle 4 reloading. itater-ial on the lower core support plate was removed.
flo known loose pellets. remained in the reactor vessel or on fuel remaining in the core.
It is not known if pellets below the lower core support plate would stay in place or be lifted by the coolant flow. If the pellets are lifted by the coolant flow, they are small enough to pas's through the botton nozzle but they would be caught by the fuel assenbly bottom grid.     This might cause some local flow blockage, but it is tolerable at this axial core location.
If there are any pellets or parts of pellets remaining in the reactor vessel they would be small fragments that traveled upward between the adja-cent fuel assenblies during Cycle 3 operation (assembly to assembly nominal clearance is.040 inches) or larger fragrants that dropped. to and through the lower core support plate when fuel was noved.during Cycle 4 reloading.
If pellets remaining in the system retain' their integrity, there should be no significant reactor coolant activity increase because these pel-lets will not be exposed to core neutron flux and hence cannot generate fission products. Should the pellets disintagrate, it is expected that temporary and ninor increases in reactor coolant activity will be detected. The chemical and volume control system purification dcminerali7.crs and filters will remove par-ticulate and dissolved material from this source. It is not' expected that opera-tion will result in reactor coolant activity levels higher than those experi-cnced during Cycle 3.
itater-ial on the lower core support plate was removed.
Therefore, based on the safety evaluation given above, operation of the Unit 1, Cycle 4 core is not considered to pose a hazard to the health and safety of the public. Investigation as to the exact cause of the fuel failure will continue. Present plans are to remove all fuel and the lower core barrel of the Unit 1 reactor vessel during its Cycle 4-5 refueling as part of the in-service inspection program. This will permit a thorough fuel inspection and investigation of baffle plate joints to determine if this is the cause of D-03 failed fuel rods.
It is not known if pellets below the lower core support plate would stay in place or be lifted by the coolant flow.
Very truly yours, s   ,          .
If the pellets are lifted by the coolant flow, they are small enough to pas's through the botton nozzle but they would be caught by the fuel assenbly bottom grid.
Executive Vice President Sol Burstein                                                         .
This might cause some local flow blockage, but it is tolerable at this axial core location.
If pellets remaining in the system retain' their integrity, there should be no significant reactor coolant activity increase because these pel-lets will not be exposed to core neutron flux and hence cannot generate fission products.
Should the pellets disintagrate, it is expected that temporary and ninor increases in reactor coolant activity will be detected.
The chemical and volume control system purification dcminerali7.crs and filters will remove par-ticulate and dissolved material from this source.
It is not' expected that opera-tion will result in reactor coolant activity levels higher than those experi-cnced during Cycle 3.
Therefore, based on the safety evaluation given above, operation of the Unit 1, Cycle 4 core is not considered to pose a hazard to the health and safety of the public.
Investigation as to the exact cause of the fuel failure will continue.
Present plans are to remove all fuel and the lower core barrel of the Unit 1 reactor vessel during its Cycle 4-5 refueling as part of the in-service inspection program.
This will permit a thorough fuel inspection and investigation of baffle plate joints to determine if this is the cause of D-03 failed fuel rods.
Very truly yours, s
Executive Vice President Sol Burstein


                      .-                                                          ~COP.E !.0ADitlG Para rR:1 P0lllT P.EACil IHilT 1               CYCL.E 3 8          9,      10      11          12            13
~ OP.E !.0ADitlG Para rR:1 C
                                      )           '/.         3           4   .
P0lllT P.EACil IHilT 1 CYCL.E 3
5       6       7
)
                                                      .                                                  270' F01     F32     F33 A.                                            .            .
'/.
PD       PD       PD                                       .            .
3 4
    ~
5 6
F22       F00         E41     F16 EOS           F02       F13 0
7 8
                                                                  ~
9, 10 11 12 13 270' F01 F32 F33 A.
PD         PD ~       n12     12P16 R33           PD         PD                                           ,
PD PD PD F22 F00 E41 F16 EOS F02 F13
e D16       D15     D12       D23     D24       E] 5     F26 F29          E07 C                               --
~
4P1         n32       PD       nl5 rD             aOS       ar12     PD
0 PD PD ~
        ,                                                    PD C04     E02 D30             E03       007     EOS         F19 FIS        10 6        DOS        E0l
n12 12P16 R33 PD PD
                                        ~
~
SP34     PD       8P21 PD           SP35     R22     4P10         ED h                        PD          4P]l        n27 E27     Dll     E29       D36       E10     D13         F10 F03        D14          Ell        DlO 8P2s    n02          PD E -             ,-      PD           n20         sP23       R17       4r8     nS4     4el4     n07 A40     E23 1,18           E31       D02     D0G         E40           F35 F04          E38          D18          D17          E39 6P27 R30           4P2       PD     SS2         R26           PD
e F29 E07 D16 D15 D12 D23 D24 E] 5 F26 C
: b.           PD          ROG          PD          PD          4P16    R18 E2s     E34       E25       D25       E24     D35         F23           F27           ,.
PD 4P1 n32 PD nl5 rD aOS ar12 PD h
F20          F34        D09          E18          D01 G                                                                                  R19       BP29       RS2     SP31     R14         SSS           TD PD          SSG        R13          8F2B        nS3      SP33 502       E19 D41             E21     D40     D31         E35           F21 F36          E37        D32          D26        E22 b,'                                                            4P5       R09     EP30 R21           4P7     PD       PD           R01           PD PD          R04        SS1          PD t
~
d                                            E12         DOC       E32     D20     E30       D22       E04     D37         F17 F14        D27
FIS 10 6 DOS E0l C04 E02 D30 E03 007 EOS F19 PD 4P]l n27 SP34 PD 8P21 PD SP35 R22 4P10 ED F03 D14 Ell DlO E27 Dll E29 D36 E10 D13 F10 E -
                          !                                                  8P36         Rll     4P15     RS1     4P9         R10     8P24     R16         PD PD          R25 D21         E06     D29     E14 D33             328     D38     E09         F06 F09        R17 SP25 PD              SP32    R29      4P4
PD n20 sP23 R17 4r8 nS4 4el4 n07 8P2s n02 PD F04 E38 D18 D17 E39 A40 E23 1,18 E31 D02 D0G E40 F35 PD ROG PD PD 4P16 R18 6P27 R30 4P2 PD SS2 R26 PD b.
                      %j                             PD         4P13         R24         SP22     PD                                                         [?D Fll         E20         D34     D03     D19       D2 8       D39. E13     F18 ge'                                                                      PD       R28     PD         .408   4P6     PD PD          4P3          R31 F12         F07     E33     F31 E3G             F05 . F24
F20 F34 D09 E18 D01 E2s E34 E25 D25 E24 D35 F23 F27 G
{             s                                   PD           PD       R03   12P15 !<23             PD       PD                             -
PD SSG R13 8F2B nS3 SP33 R19 BP29 RS2 SP31 R14 SSS TD F36 E37 D32 D26 E22 502 E19 D41 E21 D40 D31 E35 F21 PD R04 SS1 PD 4P5 R09 EP30 R21 4P7 PD PD R01 PD b,'
                                            \
t F14 D27 E12 DOC E32 D20 E30 D22 E04 D37 F17 d
                                              'N                                                   F25     F30     F28                             -
PD R25 8P36 Rll 4P15 RS1 4P9 R10 8P24 R16 PD F09 R17 D21 E06 D29 E14 D33 328 D38 E09 F06
c.'. r. t r o
%j PD 4P13 R24 SP22 PD SP25 PD SP32 R29 4P4
                                                                                                                                                                  ^ " 4 FH hk ~
[?D Fll E20 D34 D03 D19 D2 8 D39.
                                                    '                                              pp     pD       PD                                 .
E13 F18 ge PD 4P3 R31 PD R28 PD
so-s
.408 4P6 PD F12 F07 E33 F31 E3G F05.
                $'ucl Anne::bly I'D 8 +                             s                                                                                                             .
F24
x
{
                                                                          \
s PD PD R03 12P15 !<23 PD PD
Other Davice ID E                         +               \                                                                   . .                          .
\\
                                                                                \                             .
'N F25 F30 F28 c.'. r. t r o
                                                                                  \fpproxi;,ati Diiaction of Itpinc.r.ent Flos -
^ " 4 FH hk ~
I                                                                                                                                                                                       .
pp pD PD so-s
                      -                                                                                                      g f.
$'ucl Anne::bly I'D 8 +
s x
\\
\\
Other Davice ID E
+
\\
\\fpproxi;,ati Diiaction of Itpinc.r.ent Flos -
I g
f.


CORE LOADING PATlERN, POINT BEAcil UNIT               1-            cycw __ _ ' 4 Tl(N TEST ASSDiBLY
CORE LOADING PATlERN, POINT BEAcil UNIT 1
_FlJEL ID f N REGl0H 3                               :(     ) F1011tulIT 2 Insert ID       :          PD - Pluq Device R - RT,CControl Rod Z                           SS - Activated Secondary 50.
cycw __ _ ' 4 Tl(
270                           RS - RCC Partial Length Control Rod 0 29       G 0   G2G A-                                                       7         7     7                     12P - 12 Burneble Poison A
TEST ASSDiBLY N
____.J n           _S.S-2 __PlL                             Rods G3i       GIS         F05       F32   F07     O c.3   Gi7           (Reinserted)
_FlJEL ID f N REGl0H 3
D                                   7       .7             6       6   6-       7         7                                   B
: (
                                  .          _l'D_ _ P.D_-L               12 PM     R       PD       PD
) F1011tulIT 2 Insert ID PD - Pluq Device R - RT,CControl Rod Z
                                    ._G 23   F01       E01                   E02     EOS   E03     F33     C- 12 7
SS - Activated Secondary 50.
E41 C                                   6         5       5           5       5     5         6       7                         C PD Pn_           p     r_n           a _E D_ _P          JD         PD D -.--       GC6         F04     E16       E30       F24         E23     F12   E32     E08     F35     C C4 7                   5         5       6           5       6     5       5       6       7                 D 6
270 RS - RCC Partial Length Control Rod 0 29 G 0 G2G A-7 7
                          -DP          eg     .a       og       Pa ._       99     P_D   on   a    P     on       PD E = --      G$           Eli     E21       F29       A83         B51   033     F26       F22     E10     6W 7
7 12P - 12 Burneble Poison A
5       5                          E PD                                       FD       R     P PD
____.J n
                                                                                  ~
_S.S-2 __PlL Rods G3i GIS F05 F32 F07 O c.3 Gi7 (Reinserted)
p    ~Gf      F17       E38     F06       A6T     E07         Fl6   EIS 7JO           Fog     E40   F14   G06 6         5       6                   5           6       5               6       5             7 (1                          6                 F
D 7
                    '' O     P,     pn       PD         (Q R         PD       R   PD)        P D. PD      p      PD
.7 6
                  ~ Gly     F20           E18 E26         E82   F34         E34   F23     B75     E25     E24   F27 180                                                                                                                    E.RN-l O, Y                       6             5       5                 6           5       6               5        5      6        7X G       PD   ;;S6/12.'         R     Pn     h)      PD            R    PD      b)      PD          R SSS/12k PD        '
6 6-7 7
                                                                                                                                        ,l G
B
T[7       F10       E37       F19       A85     E20         F31   E13   A67       FIS       E35 F03     G25 il             6         5           6                             6           (1) .       6         5   6       7 PD                                        (1)    5                  5 PD
_l'D_ _ P.D_-L 12 PM R
                                                                                                                                              }{
PD PD
R      PD         PD         PD       R         PD       o              PD         PD     R     PD G"                             Fil     A59 B81   A34   F18                         G 20 7          E12    E31                                                      E39      E04 I                                                                                 6                            7 PD            5 n
._G 23 F01 E01 E41 E02 EOS E03 F33 C-12 7
5 Pn 6
C 6
R    (l[P J(2)     hl)D     R 5
5 5
of t 5
5 5
o      PD
5 6
                                                                                                                                            'I Go3         F36   El7         E29' F13           El9     F22   E27       .E09     F21     G 22, J               7                   5                             5 6                   5       6                  6     5         5       6       7 PD                                                                                                               g PD       R         PD     n,g _     PD      PD    pn        R        pn      PD s' '                                   G 15     F25       EOS       E33     E14   E36     t2e       F28     (f01 1,.                          7         6         5                 5     5       5         6       7 5
7 C
PD       PD                                                                                           I' R   _M           R   Pn         R       PD     _P.D
PD Pn_
          ;
p r_n a
                                        '      G' 7
_E D__P JD PD D -.--
l~ 4       F02     F3D     F08     G 27     6 09 6       6         6     7         7                                 L PD       PD                 17pM n
GC6 F04 E16 E30 F24 E23 F12 E32 E08 F35 C C4 7
                                                                        ~
6 5
o    Pn         PD G l4       &II   G'21
5 6
          <                                                            7         7      7 1,.
5 6
PD       SS-1   PD 99 X         -
5 5
1       2           3         4         S         c       7       8                                                     '
6 7
q                  q.                                9       10       11       12     13 g        e        A            o.       ,
D P
(Revision 1         12/17/75)}}
-D eg
.a og Pa._
99 P_D on P
on PD a
G$
Eli E21 F29 A83 B51 033 F26 F22 E10 6W E = --
7 5
5 PD E
PD FD R
P
~Gf
~
F17 E38 F06 A6T E07 Fl6 EIS 7JO Fog E40 F14 G06 p
(1 6
5 6
7 (Q
5 6
5 6
5 6
PD)
F
'' O P D.
PD p
PD P,
pn PD R
PD R
180
~ Gly F20 E18 E26 E82 F34 E34 F23 B75 E25 E24 F27 E.RN-l 5
5 6
7X O, Y
6 5
5 6
5 6
b)
PD R SSS/12k PD
,l h)
PD R
PD G
PD
;;S6/12.'
R Pn G
T[7 F10 E37 F19 A85 E20 F31 E13 A67 FIS E35 F03 G25 il 6
5 6
(1) 5 6
5 (1).
6 5
6 7
}{
PD PD PD PD R
PD R
PD PD PD R
PD o
G" 7
E12 E31 Fil A59 B81 A34 F18 E39 E04 G 20 I
(l[
J(2) hl) 6 5
5 7
PD 5
5 6
'I P
D R
of t o
PD n
Pn R
Go3 F36 El7 E29' F13 El9 F22 E27
.E09 F21 G 22, J
7 6
5 5
6 5
6 5
5 6
7 PD PD pn R
pn PD g
PD PD R
PD n,g _
s' '
G 15 F25 EOS E33 E14 E36 t2e F28 (f01 1,
7 6
5 5
5 5
5 6
7 PD PD I'
R
_M R
Pn R
PD
_P.D G'
l~ 4 F02 F3D F08 G 27 6 09 7
6 6
6 7
7 L
PD PD n
17pM o
Pn PD
~
G l4
&II G'21 7
7 7
1,.
PD SS-1 PD 99 X
1 2
3 4
S c
7 8
9 10 11 12 13 q
q.
A (Revision 1 12/17/75) o.
g e
,}}

Latest revision as of 03:58, 2 January 2025

RO 50-266/75-18:on 751217,during Facility Refueling,Failed Fuel Assembly Discovered on D-03 Fuel Rods.Caused by Water Impingement Through Baffle Plate While Failed Assembly Was in Cycle 2 Position H-1.Thorough Insp Program Is Underway
ML19309A457
Person / Time
Site: Point Beach NextEra Energy icon.png
Issue date: 12/30/1975
From: Burstein S
WISCONSIN PUBLIC SERVICE CORP.
To:
Shared Package
ML19309A455 List:
References
FOIA-80-3 NUDOCS 8003310105
Download: ML19309A457 (9)


Text

~

L. O WISCOREln Elactac rosca coueur

?31 WEST MICHIGAN,f/.lLWAUKEE, WISCONSIN 53201

[.,

ecember 30, 1975 p

'f

'D g/

. e.....

14r. Benard C. Rusche, Cirector C

s.!;, 'l,-~

'r U. S. !!uclear Regulatory Conmission O < ', '

'd[l (sij}

Office of fluclear Reactor Regulation /

'JA

-4

!!ashington, D. C.

20555

\\.

j

Dear fir. Rusche:

. ' u"{f').

i97e...;;.y

../q

'i

(

.d.19.

LICE:lSEE EVEllT REPORT T10. 50-266/75-18 b&

FAILED FUEL Iti ASSE;;BLY D-03, POSITION K-6, CYCLE 3 POINT BEACH ?mCLEAR PLAflT This letter is to report in detail the discovery and results of sub-sequent investigation of a failed fuel assembly during the Cycle 3-4 refuel-17, 1975.

An initial ing of Unit 1 at Point Beach I!uclear Plant on Decemberto comply with the ten-day 23, 1975 report of this event '..Ts filed December rt. porting requirenants of the Point Beach Technical Specification Section 15.6.6.A.2.

On Decerber 17, 1975, during the refueling of Unit 1, the Core Load-ing Supervisor noted sorething protruding from the side of fuel assembly D-03 Fuel novement was as it was being lowered into the fuel assembly upender.

stcpped innediately while the R.: actor Engineering Group representative moved the underwater TV carara in position to observe the affected area.

The pre-liminary inspection indicated that a section of fuel rod was missing.

The Reactor Engineer was notified of the finding after thich the subject assembly was coved to the fuel inspection periscope in the spent fuel pit where a more detailed exanination was made.

VISUAL EXA'4It!ATION OF FUEL ASSE"7LY C 03, EAST FACE, 12-17-75 The results of detailed visual examination of the fuel assembly are sunnarized below, starting with the top of the fuel assembly.

Top of the Fuel Asserbly Rods 12 and 13 were observed *.o be slightly below other rods (approxi-aately 1/16") ar.d esduced spacing betuean rods 12 and 13 was evident.

Top of Grid 1 Rods 12 and 13 shcwed indications of wear adjacent to grid flow vanes.

The vane at rod 13 uas partially worn away.

5.'L PC->

?..,

t Q

8008310 306

!!r. Benard C. Itusche December 30, 1975 At Grid 1 Rust narks were evident on the grid and rods 12 and 13.

Clad of rods 12 and 13 worn away to the extent that fuel springs were visible be-hind slots in the grid.

Below Grid 1 A fuel fra5nent was observed to be lodged between rods 13 and 14.

Gouge marks could be seen in rods 12 and 13 adjacent to grid tab and a hole was visible in rod 12 at grid tab. A tab was touching rods.12 and 13 and a narrow gap exists between rods 12 and 13.

l Between Grids 1 and 2 f!o apparent damage to rods was noticeable at,this location, but 1

the spacing between rods 12 and 13 was reduced'.

Top of Grid 2 4

The cladding of rod 12 was separated near vane with no cladding or fuel behind the upper part of grid.

Rod i3 has a cut nark near upper edge of the clad and a hole on the left side.

A fuel fragnent was visible between rods 13 and 14. The vane near rod 12 was bent in slightly.

At Grid 2 The spring for rod 12 was missing.

Fuel fragnents and open clad on rod 13 was visible at this location.

Below Grid 2 A two-inch sect on of clad for rod 12 from behind the grid had slipped down and pinr.ed between the grid and the lower section of rod 12.

This rod has several holes natching the contact points of the grid springs.

"o fuel was visible.

Rod 13 has a hole under the grid tab with an outline similar to the tab.

~

"atucen Grids 2 and 3 About a four-inch open split in rod 13 with no fuel visible except 4

at the top and of the split.

'Tc6 of Grid 3 Open cut in cladding on rod 12 adjacent to -vane.

The vane is severely worn down cn the side near rod 12.

4

Iir. Benard C. Rusche December 30. 1975

~

Complete separation of rod 13 at point just above grid with the section of rod between grids 2 and 3 resting on prid 3 between rod 12 and the second rod in from 12.

The section of clad for rod 13 that was behind the grid springs made contact. Also a lot of gouge marks are present on that section of clad.

No fuel fragments are visible..

A fuel fragnent was visible on top of the grid near rod 8.

At Grid 3 Missing grid spring for rod 13.

No clad for rod 13 visible behind grid.

Below Grid 3 Holes visible in rod 11 near grid tab.

Large hole in rod 12 with large fuel fragment sticking out.

Section of cladding for rod 13 missing frcm behind grid.

Fresh scrape narks on top edge of the existing rod 13 cladding.

No fuel visible at top edge of this section of rod 13.

Between Grids 3 and 4 Rub nark on rod 13.

t Top of Grid 4 Uide gap between rods 12 and 13.

At Grid 4 Center of grid spring for rod 12 separated.

Many small fuel frag-r.2nts visible behind grid at rods 12 and 13.

L' ear in grid spring at rod 13.

Felow Grid 4 Gouge narks and hole in rod 12.

Fuel visible in hole.

Rod 13 miss-ing completely from grid to midway between grids 4 and 5.

Gouge marks on se rod in from rod 13.

i

,Catween Grids 4 and 5 1

Top 11 inches of rod 13 missing.

End of rod 13 bent to a horizon-tal condition about two inches 1cng.

r. Ecnard C. I'usche

--4

, December 30, 1975 Too of Grid 5

!! car in rod 11 adjacent to vane.

Rod 12 clad worn through 'at vane with vane worn down also.

Rod 13 has an unusual ragged hole next to but not parallel to the edge of the grid vane.

The vane is severely worn and bent.

A piece of clad about one-half inch long is lodged between rod 14 crd the grid.

Eelow Grid 5 Rod 12 has a hole with gouge marks around it.

A fuel fragment is visible in the hole.

Eelo.t Grid 6 Hole 'in rod 12.

Couge marks and hole in rod 13 with fuel showing.

otton Grid and I;czzle Rod 12 alr.ast bottcmed out and resting on bottom.

The normal rods are about 3/4 inch off the bottom.

SL""'ARY OF FUEL ASSE",ELY D-03 OPERATlilG HISTORY A brief suntary of the operating history of fuel assembly D-03 is as follows:

Fuel Assenbly Identification:

D-03

?rspressurized low parasitic design with fuel rods off the bottom nozzle.

Fericated at !!estinghouse !!uclear Fuel Division, Cheswick, Pennsylvania.

Da:e received on site: August 22, 1972

nitial inspection revealed no abnornalities.

Leided into Unit 1, Cycle 2 at core location H-1.

Insert was a thiable plug device.

Burnup during Cycle 2 was 7,071 M'!D/liTU.

~

Leidad into Unit -1, Cycle 3 at core location Ve6.

Insert was a thimble plug davice. Burnup during Cycle 3 was 16,306 !C!D/MTU.

Tc:a1 buraup: 23,377 :".!D/MTU.

'bre as no difficulty in the fuel handling operation during Refueling 2, which irc olved 0-03 and/or adjacent assemblies.

l

/

Hr. Benard C. Ruscha December 30, 1975 DETAILED FUEL HAflDLIliG STEPS LEADING TO DISCOVERY OF OCCURRE!1CE

. Anonalous behavior was first noted during the fuel reloading se-quence when fuel assembly E-06 was being lowered into adjacent core position K-5.

The operator noted some deflections of the order of 120 pounds in the load cell '..hich monitors the weight of the fuel assembly and mast.

This occurrence is.10t particularly unusual as the assembly slides into its opening between four other assenblies.

He also noted that this assembly was slightly higher in elevation (1/8" to 1/4") when it was positioned on the lower core support plate. Uhen it was observed that there was a section of fuel rod approximately 11 inches long missing from D-03, its forner location (K-6) was inspected and nothing abnormal was noted, assembly E-33 was then loaded into core position K-6.

Fuel assenbly E-06 was then removed froi, core position K-5 to facilitate an inspection of the core support plate.

A portion of fuel rod, approximately 11 inches long, was observed to be lying diagonally across the K-5 location.

Assemblies in J-5 and L-5 (E-29 and G-24, respectively) were removed from the core to give clear access to the broken piece of rod.

An air-operated vise grip was utilized to retrieve the rod.

Several small piles of debris were also noted and reno' ed by using an underwater vacuun.

v Faces and corners of assemblies which could have been affected either during Cycle 3 operation of D-03 or during the fuel movements were inspected.

This effort included the southwest ccrner of F-07; the southeast corner of E-33; the south face of G-24; the north face of E-29; the west face of F-25; and t!-.:est face of D-34.

A small plug-like object was noted on top of the botton nozzle of F-07 and this was removed to the bottom of the refueling cavity where it was vacuumed.

On D-34's west face several fuel fragments were observed uedged between the rods and grids.

Scratches were also noted on D-34 in the area of the gross failure on adjacent fuel assenbly D-03.

There was no apparent failure to D-34.

D-34 was later renoved permanently from the core per the preplanned refueling procedure.

PR03ABLE CAUSE OF FUEL CLAD FAILURE The nuclear steam supply system vendor, Westinghouse, has stated that a nighly prcbable initiating Tactor for the fuel failure was water im-pingenent through the baffle plate while the failed assembly was in its origi-nal Cycle 2 position H-1.

This problem was experienced previously at two for-eign nuclear plants.

Experience at the foreign plants has indicated that flow through the stitch weld joining in the baffle plate, or bolted baffle plates as may be the case at Point Beach, has occurred at locations similar to H-1.

This can result in a water inpincrent on the corner or near corner fuel rods of the assembly at this position, thus leading to vibration and fretting wear of one or more fuel rods.

In the Point Coach case, assembly D-03 occupied position H-1 during Cycle 2 before being moved to position Ps-6 for the ensuing Cycle 3.

A small hole in the affected fuel rods due to Tretting from fuel rod vibration is postu-lated to have taken place prior to relocaticn of the assenbly into position K-6.

The Cycle 3 position subjected the assably to.a masurably higher power rat-ing than in its Cycle.2 position.

I

_h

11r. Benard C. Ruscha December 30, 1975 The ' initial escalation to power at the beginning of Cycle 3 was at a rate higher than the present operating guidelines and a sharp increase in reactor coolant activity was noted between power levels of 40 to 50%.

It is presumed that the fuel rods containing holes in the clad became water-logged during the shutdciin and burst due to steam pressure and/or the lack of suffi-cient time for the Zircaloy to plastically deform during the power escala-tion phase.

SAFETY EVALUATIO;i A!!D CORRECTIVE ACTION Two potential safety concerns have been evaluated:

(1)

The poten-tial for and consequences of addi ional fuel failures and '(2) the effect of t

loose fuel pellets in the coolan; system on the health and safety of plant operating personnel and the public.

The first item requiring a safety evaluat[ ion is the potential for and the consequences of additional fuel failures of a'similar nature.

If baffle inpingement at core location H-1 is the problem, a potential problem exists in two additional assenblies.

Fuel assembly F-36 had been located in position H-1 during Cycle 3 and has been.ovad to position J-3 for Cycle 4 operation.

Iew fuel asscmbly G-07 is presently located in position H-1 for Cycle 4 operation.

Both assemblies will be carefully inspected at the end of Cycle 4 oper-ation.

In reviewing the safety aspects of locating assembly F-36 at position J-3 during Cycle 4, it was confirmed that the assembly does not contain a con-trol rod in this position; therefore no possibility exists of a danaged fuel rod interferrinq with a control rod dropping action.

A notable factor mitigating the possibility of cladding damage to this assembly during Cycle 4 is that some months ago Uestinghouse instigated guidelines governing the rate of power escala-tion following a cold shutdown of the reactor.

These guidelines will be fol-lowed rigidly during future startups from the cold condition for Unit 1, Cycle 4.

The purpose of centrolled power escalation is to allow fuel rods which might have taken in water via pinhole leaks to expel the water, thus preventing the bursting of cladding due to steam pressure buildup within the fuel rod as appear nay have happened in this instance.

It is considered that careful nonitoring of the reactor coolant activ-ity during reactor startup and later operation will provide the necessary informa-tion for nonitoring the condition of fuel assembly F-36, as well as the other fuel assemblies in the reactor.

Reactor coolant system activity monitoring and allowable limits will be continued as prescribed by the Technical Specification.

The second item requiring safety evaluation is that of loose fuel pel-lets in the reactor ccolant system during subsequent plant operation.

As de-scribcd previously, all reasonable attccpts to locate and renove loose pellets

lir. Cenard C. Rusche December 30, 1975 from adjacent fuel assemblics and the loner core support plate were performed.

flo known loose pellets. remained in the reactor vessel or on fuel remaining in the core.

If there are any pellets or parts of pellets remaining in the reactor vessel they would be small fragments that traveled upward between the adja-cent fuel assenblies during Cycle 3 operation (assembly to assembly nominal clearance is.040 inches) or larger fragrants that dropped. to and through the lower core support plate when fuel was noved.during Cycle 4 reloading.

itater-ial on the lower core support plate was removed.

It is not known if pellets below the lower core support plate would stay in place or be lifted by the coolant flow.

If the pellets are lifted by the coolant flow, they are small enough to pas's through the botton nozzle but they would be caught by the fuel assenbly bottom grid.

This might cause some local flow blockage, but it is tolerable at this axial core location.

If pellets remaining in the system retain' their integrity, there should be no significant reactor coolant activity increase because these pel-lets will not be exposed to core neutron flux and hence cannot generate fission products.

Should the pellets disintagrate, it is expected that temporary and ninor increases in reactor coolant activity will be detected.

The chemical and volume control system purification dcminerali7.crs and filters will remove par-ticulate and dissolved material from this source.

It is not' expected that opera-tion will result in reactor coolant activity levels higher than those experi-cnced during Cycle 3.

Therefore, based on the safety evaluation given above, operation of the Unit 1, Cycle 4 core is not considered to pose a hazard to the health and safety of the public.

Investigation as to the exact cause of the fuel failure will continue.

Present plans are to remove all fuel and the lower core barrel of the Unit 1 reactor vessel during its Cycle 4-5 refueling as part of the in-service inspection program.

This will permit a thorough fuel inspection and investigation of baffle plate joints to determine if this is the cause of D-03 failed fuel rods.

Very truly yours, s

Executive Vice President Sol Burstein

~ OP.E !.0ADitlG Para rR:1 C

P0lllT P.EACil IHilT 1 CYCL.E 3

)

'/.

3 4

5 6

7 8

9, 10 11 12 13 270' F01 F32 F33 A.

PD PD PD F22 F00 E41 F16 EOS F02 F13

~

0 PD PD ~

n12 12P16 R33 PD PD

~

e F29 E07 D16 D15 D12 D23 D24 E] 5 F26 C

PD 4P1 n32 PD nl5 rD aOS ar12 PD h

~

FIS 10 6 DOS E0l C04 E02 D30 E03 007 EOS F19 PD 4P]l n27 SP34 PD 8P21 PD SP35 R22 4P10 ED F03 D14 Ell DlO E27 Dll E29 D36 E10 D13 F10 E -

PD n20 sP23 R17 4r8 nS4 4el4 n07 8P2s n02 PD F04 E38 D18 D17 E39 A40 E23 1,18 E31 D02 D0G E40 F35 PD ROG PD PD 4P16 R18 6P27 R30 4P2 PD SS2 R26 PD b.

F20 F34 D09 E18 D01 E2s E34 E25 D25 E24 D35 F23 F27 G

PD SSG R13 8F2B nS3 SP33 R19 BP29 RS2 SP31 R14 SSS TD F36 E37 D32 D26 E22 502 E19 D41 E21 D40 D31 E35 F21 PD R04 SS1 PD 4P5 R09 EP30 R21 4P7 PD PD R01 PD b,'

t F14 D27 E12 DOC E32 D20 E30 D22 E04 D37 F17 d

PD R25 8P36 Rll 4P15 RS1 4P9 R10 8P24 R16 PD F09 R17 D21 E06 D29 E14 D33 328 D38 E09 F06

%j PD 4P13 R24 SP22 PD SP25 PD SP32 R29 4P4

[?D Fll E20 D34 D03 D19 D2 8 D39.

E13 F18 ge PD 4P3 R31 PD R28 PD

.408 4P6 PD F12 F07 E33 F31 E3G F05.

F24

{

s PD PD R03 12P15 !<23 PD PD

\\

'N F25 F30 F28 c.'. r. t r o

^ " 4 FH hk ~

pp pD PD so-s

$'ucl Anne::bly I'D 8 +

s x

\\

\\

Other Davice ID E

+

\\

\\fpproxi;,ati Diiaction of Itpinc.r.ent Flos -

I g

f.

CORE LOADING PATlERN, POINT BEAcil UNIT 1

cycw __ _ ' 4 Tl(

TEST ASSDiBLY N

_FlJEL ID f N REGl0H 3

(

) F1011tulIT 2 Insert ID PD - Pluq Device R - RT,CControl Rod Z

SS - Activated Secondary 50.

270 RS - RCC Partial Length Control Rod 0 29 G 0 G2G A-7 7

7 12P - 12 Burneble Poison A

____.J n

_S.S-2 __PlL Rods G3i GIS F05 F32 F07 O c.3 Gi7 (Reinserted)

D 7

.7 6

6 6-7 7

B

_l'D_ _ P.D_-L 12 PM R

PD PD

._G 23 F01 E01 E41 E02 EOS E03 F33 C-12 7

C 6

5 5

5 5

5 6

7 C

PD Pn_

p r_n a

_E D__P JD PD D -.--

GC6 F04 E16 E30 F24 E23 F12 E32 E08 F35 C C4 7

6 5

5 6

5 6

5 5

6 7

D P

-D eg

.a og Pa._

99 P_D on P

on PD a

G$

Eli E21 F29 A83 B51 033 F26 F22 E10 6W E = --

7 5

5 PD E

PD FD R

P

~Gf

~

F17 E38 F06 A6T E07 Fl6 EIS 7JO Fog E40 F14 G06 p

(1 6

5 6

7 (Q

5 6

5 6

5 6

PD)

F

O P D.

PD p

PD P,

pn PD R

PD R

180

~ Gly F20 E18 E26 E82 F34 E34 F23 B75 E25 E24 F27 E.RN-l 5

5 6

7X O, Y

6 5

5 6

5 6

b)

PD R SSS/12k PD

,l h)

PD R

PD G

PD

S6/12.'

R Pn G

T[7 F10 E37 F19 A85 E20 F31 E13 A67 FIS E35 F03 G25 il 6

5 6

(1) 5 6

5 (1).

6 5

6 7

}{

PD PD PD PD R

PD R

PD PD PD R

PD o

G" 7

E12 E31 Fil A59 B81 A34 F18 E39 E04 G 20 I

(l[

J(2) hl) 6 5

5 7

PD 5

5 6

'I P

D R

of t o

PD n

Pn R

Go3 F36 El7 E29' F13 El9 F22 E27

.E09 F21 G 22, J

7 6

5 5

6 5

6 5

5 6

7 PD PD pn R

pn PD g

PD PD R

PD n,g _

s' '

G 15 F25 EOS E33 E14 E36 t2e F28 (f01 1,

7 6

5 5

5 5

5 6

7 PD PD I'

R

_M R

Pn R

PD

_P.D G'

l~ 4 F02 F3D F08 G 27 6 09 7

6 6

6 7

7 L

PD PD n

17pM o

Pn PD

~

G l4

&II G'21 7

7 7

1,.

PD SS-1 PD 99 X

1 2

3 4

S c

7 8

9 10 11 12 13 q

q.

A (Revision 1 12/17/75) o.

g e

,