ML20134F470
| ML20134F470 | |
| Person / Time | |
|---|---|
| Site: | Byron  |
| Issue date: | 10/31/1996 |
| From: | Kofron K COMMONWEALTH EDISON CO. |
| To: | NRC (Affiliation Not Assigned), NRC OFFICE OF INFORMATION RESOURCES MANAGEMENT (IRM) |
| References | |
| BYRON-96-0281, BYRON-96-281, IEB-96-001, IEB-96-1, NUDOCS 9611050325 | |
| Download: ML20134F470 (14) | |
Text
1 Commonweahh 1:diwn Comp.my Ilyron Generating Station
- 4150 North German Church Road Ity ron, 11.61010 9791 Tel H142344411 October 31,1996 4
LTR:
BYRON-96-0281 FILE: 1.10.0101 Office of Nuclear Reactor Regulation U.S. Nuclear Regulatory Commission Washington, DC 20555-001 ATTENTION: Document Control Desk 1
SUBJECT:
Report on Timed Rod Drop Testing and Drag Force Testing Byron Nuclear Power Station Units 1 and/or 2 Facility Operating Licenses NPF-37 and NPF-66 NRC Docket Nos. 50-454 an.i 50-455
REFERENCES:
1.
NRC Bulletin (NRCB) 96-01, " Control Rod insertion Problems," dated March 8,1996.
2.
Letter from J. B. Hosmer (Comed) to U. S. Nuclear Regulatory Commission transmitting Comed's response to NRCB 96-01, dated April 4,1996.
3.
Letter from K. L. Kofron (Comed) to U. S. Nuclear Regulatory Commission transmitting Byron Unit 1, Cycle 8 Rod Drop Testing information, dated July 29,1996.
In Reference 1, the Nuclear Regulatory Commission (NRC) transmitted a request for input from holders of pressurized water reactor operating licenses regarding control rod insertion problems. Comed's response to this Bulletin (Reference 2) committed to providing a report to the NRC within 30 days of any testing results for scheduled refueling outages. Byron Station commenced refueling outage B2R06 on August 19,1996, transitioning from a forced outage resulting from primary-to-secondary tube leakage. Due to the nature of the shutdown into the forced outage, rod drop testing was not conducted at the beginning of the outage sequence. It was determined to be more prudent to stabilize the leakage than hold at a higher pressure and temperature for testing. Drag force testing was performed prior to refueling activities. The results of this testing are included in Attachment 1. Rod drop testing and drag force testing was performed following completion of refueling activities. Testing was completed on October 2,1996. The results of these tests are contained in Attachment 2. Attachment 3 is a core map of rodded fuel assemblies indicating fuel types and current and projected end of cycle burnup.
If Reference 3, Comed submitted timed rod drop test results for refueling outage BIR07. It was later noticed that the drag force testing data had been inadvertently omitted from the report. The drag force test results for BIR07 are included as Attachment 4.
9611050325 961031 i
ADOCK 05Mgg4 S'l PR (p:\\96byltrs\\960281. doc \\l03196)
A tinicom Company
i Byron Ltr: 96-0281 October 31,1996 1
Page 2 l
If there are any additional questions, please contact Marcia Lesniak, Nuclear Licensing Administrator, at (630) 663-6484.
Sincerely, a
K. L. Kofro Station Manager Byron Nuclear Power Station KLK/LZ/rp Attachments cc:
A.B. Beach, NRC Regional Administrator - Rill G.F. Dick, Jr., Byron Project Manager - NRR S. D. Burgess, Senior Resident inspector - Byron Office of Nuclear Safety - IDNS 1$3 ubscribed and sworn to before me, a Notary Public, f his day of iMMUU,19_9[p YY J
Notary P(bfic q
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{
Results of B2R06 Drag Force Testing i
1 prior to commencing Refucling Activitics 1
(P:\\96byltrs\\960281.doci103196)
e RCCA Droo Times and Draa Forces at the End of Byron Unit 2 Cycle 6 No.
RCCA Fuel Drop Time Difference Drop Time Difference Adequate Maximum
( *.), Location Assembly (to Entry from (Dashpot from Recoil Drag Forces Burnup -
into Average Entry to Average (Yes/No) during Dashpot)
Drop Time Full Dashpot Unlatching Insertion)
Time 1
B-04 35,921 20 2
B-06 l 24,355 20 3
B-08 24,598 20 4
B-JJ 25,676 25 5
B-12 36,197 20 6
C-05 44,556 30 7
C-07 41,643 25 8
C-09 41,996 s
25 9
C-11 43,885 20 10 D-02 35,874 25 11 D-04 49,655 40 12 D-08 47,872 30 13 D-12 49,305 20 14 D-14 35,972 20 15 E-03 44,862 25 16 E-13 44,402 20 17 F-02 25,030
~
10 18 F-06 49,290 20 19 F-08 41,188 15 20 F-10 49,067 25 r
21 F-14 24,456 15 --
1 22 G-03 41,733 20 23 G-13 41,684 15 24 H-02 24,554 20 25 H-04 47,801 20 26 H-06 41,091 20 27 H-08 51,671 20 28 H-10 40,926 20 29 H-12 47,864 15 30 H-14 24,488-15 31 J-03 41,620 20 32 J-13 41,551 20 33 K-02 24,703 20 l
34 l-06 49,039 25 35 K-08 41,347 20 36 K-10 49,019 15 37 K-14 24,948 15 38 L-03 44,554 15 39 L-13 44,182 15 40 M-02 36,110 10 41 M-04 49,495 15 42 M-08 47,820 10 43 M-12 49,807 15 44 M-14 36,000 10 45 N-05 44,839 15 46 N-07 41,673 15 47 N-09 41,632 20 48 N-11 45,690 10 49 P-04 35,591 20 50 P-06 25,139 20 51 P-08 24,591 10 52 P-10 25,125 20 53 P-12 36,066 20 Average Drop Time
- No rod drops were performed at the end of Byron Unit 2 Cycle 6. A Steam Generator tube leak forced the earty shutdown.
Results of B2R06 Timed Rod Drop and Drag Force Testing following completiv.' of Refueling Activities i
1 l
l l
I l
(p:\\96byltrs\\960281. doc \\l03196)
RCCA Droo Times and Draa Forces at the Bea!nina of Byron Unit 2 Cvele 7 No.
RCCA Fue1 Drop Time Difference Drop Time Difference Adequate Manmum (n)
Location Assembly (to Entry from (Dashpot from Recoil Drag Forces Burnup into Average Entry to Average (Yes/No) during Dashpot)
Drop Time Full Dashpot tJnlatching Insertion)
Time 1
B-04 25,139 1.460
-0.044 0.445
-0.026 Yes 15 2
B-06 0
1.530 0.026 0.390
-0.081 Yes 25 3
B-08 0
1.475
-0.029 0.435
-0.036 Yes 30 i
4 B-10 0
1.480
-0.024 0.480 0.009 Yes 20 1
5 B-12 25,125 1.435
-0.069 0.430
-0.041 Yes 20 6
C-05 24,320.
1.495
-0.009 0.465
-0.006 Yes 20 7
C- 0 7-24,919 1.525 0.021 0.465
-0.006 Yes 20 8
C-09 24,599 1.525 0.021 0.485 0.014 Yes 20 9
C-11 24,629 1.515 0.011 0.480 0.009 Yes 20 10 D-02 24,456 1.535 0.031 0.465
-0.006 Yes 20 11 D-04 25,737 1.485
-0.019 0.470
-0.001 Yes 20 i
12 D-08 24,488 1.485
-0.019 0.465
-0.000 Yes 20 I
l 13 D-12 24,971 1.475
-0.029 0.490 0.019 Yes 20 l
14 D-14 25,030 1.550 0.046 0.490 0.019 Yes 20 15 E-03 24,755 1.545 0.041 0.475 0.004 Yes 20 16 E-13 24,732 1.510 0.006 0.485 0.014 Yes 15 17 F-02 0
1.560 0.056 0.470
-0.001 Yes 20 18 F-06 25,307 1.515 0.011 0.485 0.014 Yes 20 19 F-08 31,507 1.475
-0.029 0.425
-0.046 Yes 20 20 F-10 25,749 1.515 0.011 0.460
-0.011 Yes 15 21 F-14 0
1.525 0.021 0.485 0.014 Yes 15 22 G-03 24,768 1.540 0.036 0.500 0.029 Yes 15 23 G-13 24,843 1.490
-0.014 0.455
-0.016 Yes 15 24 H-02 0
1.485
-0.019 0.475 0.004 Yes 20 25 H-04 24,598 1.465
-0.039 0.495 0.024 Yes 15 26 H-06 31,469 1.485
-0.019 0.473 0.004 Yes 10 27 H-08 34,028 1.500
-0.004 0.495 0.024 Yes 15 28 H-10 31,702 1.475
-0.029 0.435
-0.036 Yes 10 29 H-12 24,591 1.450
-0.054 0.460
-0.011 Yes 15 30 H-14 0
1.485
-0.019 0.475 0.004 Yes 15 31 J-03 24,664 1.500
-0.004 0.515 0.044 Yes 15 32 J-13 24,952 1.500
-0.004 0.465
-0.006 Yes 15 33 K-02 0
1.550 0.046 0.480 0.009 Yes 15 34 K-06 25,076 1.465
-0.039 0.480 0.009 Yes 15 35 K-08 31,631 1.475
-0.029 0.450
-0.021 Yes 10 36 K-10 25,626 1.515 0.011 0.470
-0.001 Yes 15 37 K-14 0
1.550 0.046 0.490 0.019 Yes 15 38 L-03 24,156 1.540 0.036 0.475 0.004 Yes 15 39 L-13 24,119 1.525 0.021 0.475 0.004 Yes 15 40 M-02 24,948 1.475
-0.029 0.460
-0.011 Yes 15 41 M-04 25,597 1.520 0.016 0.505 0.034 Yes 15 42 M-08 24,554 1.500
-0.004 0.495 0.024 Yes 15 43 M-12 25,181 1.525 0.021 0.465
-0.006 Yes 10 44 M-14 24,703 1.535 0.031 0.475 0.004 Yes 15 45 N-05 24,701 1.520 0.016 0.480 0.009 Yes 10 46 N-07 24,941 1.540 0.036 0.460
-0.011 Yes 15 47 N-09 24,703 1.500
-0.004 0.500 0.029 Yes 10 48 N-11 24,519 1.515 0.011 0.475 0.004 Yes 15 49 P-04 24,355 1.450
-0.054 0.440
-0.031 Yes 10 50 P-06 0
1.520 0.016 0.470
-0.001 Yes 10 51 P-08 0
1.500
-0.004 0.465
-0.006 Yes 15 5
52 P-10 0
1.510 0.006 0.460
-0.011 Yes 10 53 T-12 25,676 1.475
-0.029 0.485 0.014 Yes 5
Average Drop Time 1.504 0.471
i Unit 2, Cycle 7 Core Map of Rodded Fuel Assemblies / Fuel Types and Current and Projected End of Cycle Burnup j
1 1
i 1
l i
l 1
(p:\\96byltrs\\960281. doc \\l03196)
Byron Unit 2 Cycle 7 Fuel Types Region 7 Westinghouse 17X17 Vantage-5 (0.360 in. O. D. fuel rod), with anti-snag grids, Removable Top Nozzle (RTN), Debris Filter Bottom Nozzle (DFBN), intermediate Flow Mixing Grids (IFM), inconel top and bottom grids, Zr-4 cladding, mid-grids, IFMs, guide and instrument thimbles. Guide thimble inner diameter dimension: 0.422 in. and 0.3970 in. in dashpot.
i Region 8 Westinghouse 17X17 Vantage-5 (0.360 in. O. D. fuel rod), with anti-snag grids, oxide coated fuel rod bottom ends, Removable Top Nozzle (RTN), Debris Filter Bottom Nozzle (DFBN) Intermediate Flow Mixing Grids (IFM), Debris filter bottom grid, Inconel i
top and bottom grids, Zr-4 cladding, mid-grids, IFMs, guide and instrument thimbles.
Guide thimble inner diameter dimension: 0.422 in. and 0.3970 in. in dashpot.
Region 9 Westinghouse 17X17 Vantage-5 (0.360 in. O. D. fuel rod), V5 with anti-snag grids, oxide coated fuel rod bottom ends, Removable Top Nozzle (RTN), Debris Filter Bottom Nozzle (DFBN), Intermediate Flow Mixing Grids (IFM), Debris filter bottom grid, Inconel top and bottom grids, ZlRLO cladding, mid-grids, IFMs, guide and instrument thimbles.
Guide thimble inner diameter dimension: 0.422 in. and 0.3970 in. in dashpot.
i
+
1 l
4 BYRON UNIT 2, CYCLE 7 l
REFERENCE CORE LOADING PATTERN j
4 l
R P
N M
L K
J H
G F
E D
C B
A 1
l 4
{
X70K X64K X797.
W70J X73K X58K X40K 1
1 F-13 E-9 J-14 F-15 G-14 F-9 K-13 i
l W59J X77K Y39K Y78K Y23K YO1J Y28K Y80K Y44K X85K W46J 2
E-3 K-14 FERD FERD FEED FEED FERD FEED FRED F-14 P-3 W52J Y46K Y52K X17J Y59K X66K X60K X72K Y64K X16J Y53K Y38K W58J 3
N-14 FRED FRED D-3 FEED I,- 9 E-4 E-9 FRED M-3 FRED FEED C-14 X74K Y56K X38K YO7J X11J Y66K X24J Y72K X01J Y10J X55K Y40K X87K 4
E-6 FEED I,- 5 FEED P-5 FEED E-8 FERD E-5 FRED E-5 FEED P-6 X43K Y49K X15J Y12J X34J X31J Y28K M48J Y34K X30J X36J Y18J X20J YSOK X57K t'
- 5 j
C-10 FRED N-12 FRED X-7 G-12 FEED R-11 FRED J-12 G-8 FEED C-12 FRED N-10 X46K Y81K Y73K X02J X33J X11K Y19J W45J YO6J X68K K27J XO4J YSOK Y82K X53K G-6 FEED FEED In-2 D-9 E-12 FEED E-1 FEED M-11 M-9 E-2 FERD FRED J-6 X76K Y35K X42K Y16K Y22K Y20J XO5J Y60K X10J Y08J Y36K Y69K X69K Y24K X88K 7
2 E-7 FERD G-5 FRED FRED FEED N-3 FERD C-3 FEED FRED FERD J-5 FRED P-7 l
W64J YO2J X61K X14J Nd T W56J Y70K
- 71J Y67K W60J W57J X19J X65K YO3J W66J 900 8
A-6 FRED M-5 E-2 E-R-5 FRED R-6 FERD A-11 I,-1 E-14 D-11 FRED R-10 i
X84K Y31K X62K Y68K Y3k.C Y15J XO8J Y63K XO9J Y16J Y29K Y65K X48K Y30K X83K
- 9 4
E-9 FEED G-11 FEED FEED FEED N-13 FEED C-13 FEED FRED FEED J-11 FEED P-9 X63K Y83K YS7K XO6J X35J X56K Y13J W50J Y14J X50K X29J XO7J Y71K Y77K X54K 10 G-10 FRED FRED I,-14 D-7 D-5 FEED I,-15 FERD 1.- 4 M-7 E+14 FEED FRED J-10 j
X49K Y47K X22J YO9J X25J X28J Y25K W55J Y27K X26J X32J Y11J X23J Y48K X52K 11 4
j C-6 FEED N-4 FEED J-8 G-4 FEED A-5 FEED J-4 E-9 FEED C-4 FRED N-6 I
X82K Y43K X41K YO5J X12J Y62K X13J Y61K XO3J Y17J X51K Y45K X81K E-10 FEED I,-11 FRED P-11 FEED P-8 FERD E-11 FRED E-11 FERD P-10 l
M49J Y37K Y51K X18J Y75K 137K X67K X44K Y74K X21J Y42K Y41K W51J 13 i
N-2 FEED FRED D-13 FEED I,-7 In-12 E-7 FEED M-13 FEED FRED C-2 1
W53J X75K Y55L YS4K Y21K YO4J Y33K Y79K YS4K x86K W54J a
f 14 1
l E-13 K-2 FEED FEED FRED FERD FRED FEED FEED F-2 P-13
{-
Y YY Assembly Identifier X47K X59K X78K W84J X80K X45K X39K 15 4
l E-EE Frevious Cycle I,ocation F-3 K-7 J-2 K-1 G-2 F-7 K-3 00 h
a REGION 7 Y.J REGION SA i
( 3.996W/o)
( 4.800*/o)
X REGION SA REGION 95 i
( 4.4098/o)
( 4.600w/o) i x
mEGZoM 85 t
( 4.204W/o) i e
L 1
i wm r
v w
et m-
e qw. - - - - -
m m
am
?
BYRON UNIT 2, CYCLE 7 CONTROL AND SHUTDOWN ROD LOCATIONS j
R P
N M
L K
'J H
G F
E D
C B
A 1
l 1
l u
a c
a n
2 j
sD ss as ac 3
2 sa D
as D
sA 4
i a
se so
-5 i
a c
A c
a
-6 l
l as as
-7 900 e
as A
D A
sa c
-8 sa as
-9
)
a e
A c
s
- 10 so sc
- 11 sA D
s2 D
sA 12 sc sa as sD 13 sA a
c a
sA 14 15 00 Bank Number of Bank Number of Identifier Locations Identifier Locations A
4 SA 8
B 8
SB 8
C 8
SC 4
D 5
SD 4
SE 4
. ~.
. ~ -.,
i o
1 0 mfd /NfD 1434 PPM 100 % POWsR 1.478 CORs F-DsLTA-s j
7 Da 7
7 8A Sa SA 7
.895 1.147
.984 1.020 1.154 1.105 1.181
.428
.923 1.276 1.043 1.078 1.210 1.157 1.340
.684 33731 0
31135 31135 24482 25524 0
33731
)
i 9a BA SA 9a 9s Sa 9a 8a 1.147 1.197 1.200 1.360 1.258 1.118 1.090
.489 2
1.276 1.353 1.436 1.478 1.411 1.191 1.295
.767 O
20374 0
3 0
0 25053 0
24486 I
1 9A Sa SA SA Ss 9s 8a
.984 1.278 1.201 1.253 1.258 1.200 1.007
.462 t
1.043 1.435 1.268 1.325 1.357 1.353 1.254
.721 31135 0
25524 25055 21858 0
0 25449 4
I 7
Da SA 8A SA SA 9a 8a 1.020 1.361 1.251 1.219 1.294 1.124
.976
.342 1.078 1.477 1.323 1.2 90 1.422 1.206 1.232
.648 31135 0
25055 25853 0
24094 0
25866 i
SA 9s SA 9A Sa Da 8s 1.154 1.254 1.256 1.293 1.147 1.198
.585 i
1.210 1.410 1.355 1.420 1.231 1.359
.931
{
24482 0
21858 0
25471 0
24414 es 8s 9m SA Sa 9a 7
y i
1.105 1.115 1.207 1.123 1.198
.902
.299 e
j 1.157 1.188 1.351 1.20 1.358 1.242
.635 -
]
25524 25053 0
24094 1
0 0
30341 9A 9a 9a 9a 8m 7
1.181 1.089 1.085
.975
.585
.299 1.340 1.293 1.252 1.230
.931
.635 C
0 0
0 24414 30341 7
On 8s 8s 1A maeIow
.428
.488
.461
.341 Ar AsasseLY rour.R
.684
.7g6
.720
.648 MP seutInuu roten AB AssanssLy somrgy 33731 24486 25449 25856 m
+
a era m I
i I
REGION NUMBER OF POWER BURNUPS IDENT.
ASSEMBLIES SHARING TOTAL CYCLE 7
21
.620 31451 0
9B 64 1.150 0
0 l
BA 36 1.204 23636 0
8B 52
.726 25158 0
9A 20 1.265 0
0 BYRON UNIT 2 CYCLE 7 POWER AND BURNUP DISTRIBUTION AT 0
MWD /MTU, HFP, ARO, NO XENON
s.
_--._..__m._.
j J
i o
i 22400 3AfD/MrU 3 PPM 4
52 % POWER
}
1.411 CORE P-DELTA-N 7
9.
7 8.
7
.908 1.308
.908
.868
.985
.952 1.233
.521 i
.939 1.353
.952
. 928 -
1.030
.9.73 1.325
.754 54304-28959 52106 51821 47494 47579' 27234 44240 9.
8A 9A 9.
9.
i
=
- 8..
l_
1.300 1.08.6 1.322 1.284 1.288 1.002 1.239
.597 4
1.353 1.162 1.382 1.352 1.361 1.0i0 1.361
.853 28959 45881 30011 29758 48262 26698 36597 7
9A Sm SA SA 9a De Os.
j
.908
'1.321
.962
.975 1.051 1.342 1.256
.585 l
.952
'1.381 1.037 1.030 1.136 1.411 1.398
.840 i,
52106 29980 48538 48399 46722 29850 27563 37273 i
.388 1.284
.975
.967 1.311 1.034 1.116
.447
.928 1.352 1.030 1.038 1.381 1.095 1.306
.769 51821 29762 48387 48789 29527 47882 24082 34747 8A 93 SA SA 83 93 SS
.985 1.287 1.050 1.311
.999 1.211
.648
)
1 1.030
'1.360 1.136 1.382 1.047 1.302
.896 47494 29023 46707 29518 48750 27138
- 38030 h
83 83 93 BA 93 93 7
.952 1.001 1.342 1.034 1.211 1.035
.382
.993 1.070 1.411 1.095 1.302 1.250
.703 47579 48238 g 29837 47877 27137 21824 37836 9A 93 95 93 83 7
1.233 1.239 1.257 1.116
.648
.382 1.325 1.361 1.398 1.306
.896
.703 27234 26687 27556 24078 38030 37836 7
85 83 85 la amorou
.521
.597
.585
.447 At assmusLY Possa
.754
.855
.840
.769 se saxasms possa A'
IN 44240 36591
'37271 34746 m
aesar Canoman REGION NUMBER OF POWER BURNUPS IDENT. ASSEMBLIES SHARING TOTAL CYCLE I
7 21
.630 45222 13771 9B' 64 1.238 27439 27439 8A 36 1.018 47568 23932 j
8B 52
.729 41127 15969 9A 20 1.299 29254 29254 BYRON UNIT 2 CYCLE 7 POWER AND BURNUP DISTRIBUTION AT 22400 MWD /MTU, COASTDOWN, ARO, EQUILIBRIUM XENON
I 1
l Results of BIR07 Drag Force Testing following completion of Refueling Activities 1
i 1
i l
l (p:\\96byttrs\\960281. doc \\l03196) i
I 1
4 av
~ RCCA Droo Times and Draa Forces at the Beainina of Byron Unit 1 Cvele 8 2
No.
RCCA Fuel Drop Time Difference Drop Time Difference Adequate Maximum (n)
Location Assembly (to Entry from (Dashpot from Recoil Drag Forces Burnup into Average Entry to Average (Yes/No) during
{
Dashpot)
Drop Time Pull Dashpot Unlatching Insertion)
Time i
1 B-04 21,185 1.475
-0.023 0.450
-0.018 Yes 10 i
2 B-06 0
1.475
-0.023 0.470 0.002 Yes 15 3
B-08 0
1.485
-0.013 0.495 0.027 Yes 10 4
B-10 0
1.490
-0.008 0.460
-0.008 Yes 15 5
B-12 20,918 1.490
-0.008 0.470 0.002 Yes 20 6
C-05 18,060 1.495
-0.003 0.445
-0.023 Yes 15 7
C-07 21,389 1.465
-0.033 0.430
-0.038 Yes 15 8
C-09 21,542 1.470
-0.028 0.460
-0.008 Yes 15 9
C-11 18,052 1.500 0.002 0.470 0.002 Yes 15 10 D-02 20,880 1.520 0.022 0.460
-0.008 Yes 10
{
11 D-04 16,976 1.485
-0.013 0.440
-0.028 Yes 10 12 D-08 0
1.480
-0.018 0.470 0.002 Yes 20 13 D-12 17,194 1.480
-0.018 0.455
-0.013 Yes 10 14 D-14 20,582 1.510 0.012 0.450
-0.018 Yes 15 15 E-03 18,902 1.535 0.037 0.470 0.002 Yes 10 16 E-13 18,370 1.510 0.012 0.495 0.027 Yes 10 17 F-02 0
1.505 0.007 0.475 0.007 Yes 15 18 F-06 21,012 1.505 0.007 0.445
-0.023 Yes 10 19 F-08 18,956 1.505 0.007 0.450
-0.018 Yes 10 20 F-10 20,974 1.525 0.027 0.460
-0.008 Yes 10 l
21 F-14 0
1.535 0.037 0.505 0.037 Yes 15 22 G-03 21,486 1.515 0.017 0.450
-0.018 Yes 15 23 G-13 21,381 1.485
-0.013 0.480 0.012 Yes 15 24 H-02 0
1.510 0.012 0.480 0.012 Yes 10 25 H-04 0
'1.480
-0.018 0.490 0.022 Yes 10 26 H-06 18,572 1.495
-0.003 0.455
-0.013 Yes 10 27 H-08 34,846 1.505 0.007 0.485 0.017 Yes 15 28 H-10 18,868 1.480
-0.018 0.455
-0.013 Yes 10 29 H-12 0
1.490
-0.000 0.485 0.017 Yes 15 30 H-14 0
1.495
-0.003 0.485 0.017 Yes 10 31 J-03 21,330 1.490
-0.008 0.475 0.007 Yes 10 32 J-13 21,324 1.520 0.022 0.470 0.002 Yes 10 4
33 K-02 0
1.530 0.032 0.470 0.002 Yes 20 34 K-06 20,609 1.470
-0.028 0.450
-0.018 Yes 10 35 K-08 18,496 1.490
-0.008 0.465
-0.003 Yes 15 36 K-10 20,984 1.490
-0.000 0.465
-0.003 Yes 15 37 K-14 0
1.500 0.002 0.460
-0.000 Yes 10 38 L-03 18,542 1.535 0.037 0.510 0.042 Yes 10 39 L-13 18,479 1.520 0.022 0.465
-0.003 Yes 10 40 M-02 21,038 1.535 0.037 0.485 0.017 Yes 10 41 M-04 17,466 1.490
-0.008 0.465
-0.003 Yes 10 42 M-08 0
1.475
-0.023 0.495 0.027 Yes 15 43 M-12 17,103 1.500 0.002 0.475 0.007 Yes 15 44 M-14 20,673 1.520 0.022 0.450
-0.018 Yes 10 s
45 N-05 18,533 1.520 0.022 0.485 0.017 Yes 10 46 N-07 21,382 1.485
-0.013 0.455
-0.013 Yes 10 47 N-09 21,508 1.470
-0.028 0.475 0.007 Yes 10 48 N-11 17,994 1.490
-0.008 0.485 0.017 Yes 10 49 P-04 20,965 1.495
-0.003 0.455
'-0.013 Yes 10 50 P-06 0
1.480
-0.018 0.450
-0.018 Yes 10 51 P-08 0
1.520 0.022 0.475 0.007 Yes 10 52 P-10 i
0 1.495
-0.003 0.480 0.012 Yes 20 53 P-12 l 21,044 1.475
-0.023 0.480 0.012 Yes 15 Average Drop Time 1.498 0.468