L-08-349, Calculation for Contingency Flaw Evaluation Support
| ML090330371 | |
| Person / Time | |
|---|---|
| Site: | Perry  |
| Issue date: | 10/06/2008 |
| From: | Gustin H, Herrmann T Structural Integrity Associates |
| To: | FirstEnergy Nuclear Generation Corp, Office of Nuclear Reactor Regulation |
| References | |
| L-08-349 0800439.307 | |
| Download: ML090330371 (35) | |
Text
" Structural Integrity Associates, Inc.
File No.: 0800439.307 CALCULATION PACKAGE Project No.: 0800439 Quality Program: X Nuclear El Commercial PROJECT NAME:
Contingency Flaw Evaluation Support for Perry CONTRACT NO.:
55108513 CLIENT:
PLANT:
FirstEnergy Nuclear Operating Co.
Perry Nuclear Power Plant.
CALCULATION TITLE:
Evaluation of fabrication defects in N6A and C nozzle to safe end welds Document Affected Project Manager Preparer(s) &
Revision Pages Revision Description Approval Checker(s)
Signature & Date Signatures & Date 1 - 9 Initial Issue A-i - A-8 B-1 -B-10 C-1 -C-7 H. L. Gustin H. L. Gustin HLG 10/6/08 HLG 10/6/08 T. J. Herrmann TJH 10/6/08 Page 1 of 9 F0306-O1RO
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Table of Contents
1.0 INTRODUCTION
/STATEMENT OF PROBLEM/ OBJECTIVE.......................... 3 2.0 TECHNICAL APPROACH OR METHODOLOGY...............................................
3 3.0 ASSUMPTIONS / DESIGN INPUTS.................................
3......................
................. 3 4.0 FLAW CHARACTERIZATION.............................................................................
4 5.0 CA LCU LA TIO N S...................................................................................................
4 6.0 STRUCTURAL EVALUATION............................................................................
5
7.0 CONCLUSION
S AND DISCUSSIONS.................................................................
5 8.0 R E FE R E N C E S.........................................................................................................
5 APPENDIX A PERRY PLANT CYCLE RECORDS (FROM [5].................
A-i APPENDIX B INSPECTION
SUMMARY
SHEETS FROM [3]...................................
B-1 APPENDIX C PC-CRACK OUTPUT............................................................................
C-1 List of Figures Figure 1. Path 1 Through-Wall Axial Stress (psi)..............................................................
7 Figure 2. Center-Cracked Plate Fracture Mechanics Model..............................................
8 Figure 3. Crack Growth Through 200 Cycles..........................................................................
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1.0 INTRODUCTION
/STATEMENT OF PROBLEM/ OBJECTIVE The N6 A, B, and C nozzle to safe end welds at Perry are dissimilar metal welds connecting the low alloy steel nozzle forgings to the Alloy 600 safe ends. The welds are Alloy 82/182 weld metal [2,5].
These welds were last ultrasonically inspected in 2001, and all results were acceptable per IWB-3500 criteria, requiring no further evaluation. Data from that inspection was re-examined in September, 2008, in preparation for the upcoming refueling outage (February, 2009). This re-examination of the earlier data identified three flaw indications (two in the N6-A weld and one in the N6-C weld) which were determined to slightly exceed the flaw acceptance standards of IWB-3514-2 [1,3]. All of these flaw indications were determined to be subsurface indications with no connection to the inside surface of the welds. All were classified as fabrication-related defects.
The purpose of this calculation is to evaluate the identified flaw indications per the requirements of IWB-3600, to demonstrate that these indications do not affect the structural adequacy of the nozzle to safe end welds.
2.0 TECHNICAL APPROACH OR METHODOLOGY A fracture mechanics-based evaluation of the flaws is performed per the requirements of IWB-3600.
The observed flaws are assumed to have been growing by a fatigue crack growth mechanism since the previous inspection in 2001.
The resulting flaws after projected growth to the next refueling outage are evaluated to demonstrate that all structural criteria are maintained.
3.0 ASSUMPTIONS / DESIGN INPUTS
- 1. A composite flaw was assumed, combining the greatest length, greatest through-wall dimension, and greatest eccentricity of any of the three reported flaws. This hypothetical flaw conservatively bounds the evaluation of all three reported flaws.
- 2. In a previous calculation performed by SI [2], finite element analysis of the nozzle-safe end welds was performed to determine the weld residual stresses present in the welds following the application of a mechanical stress improvement process (MSIP) in 1992. The bounding residual stress distribution is shown in Figure 1, taken from [2]. Note that in that distribution, the residual stress following MSIP varies from compressive to tensile through the thickness of the weld. In the present calculation, the weld residual stress is conservatively taken to be the maximum tensile from that distribution, and is considered to be a constant membrane stress across the weld thickness. Note that weld residual stress is a steady state secondary stress which is not limited by the ASME Code. In a fatigue crack growth calculation such as that which follows, residual stress acts only as a mean stress, since its magnitude does not cycle with time.
- 3. The N6 nozzles are assumed to experience stress cycles due to plant start-ups and shut downs, and due to system operation in the RHR mode. RHR cycles are assumed to occur twice as frequently as File No.: 0800439.307 Page 3 of 9 Revision: 1 F0306-011
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start-up/shut down cycles, and to have the same magnitude. Over the eight year period from 2001 until the next refueling outage in 2009, the estimated number of such combined cycles is assumed to be less than 100 (49 cycles reported through April 2008 [6]).
- 4. Crack growth is calculated from 2001 until the next refueling outage, at which time the N6 nozzles with reported flaw indications will be re-examined.
- 5. In the following, all applied stresses are modeled as membrane stresses (i.e., constant magnitude across the wall thickness). This is very conservative since the stress combination PL+PB+Q includes significant bending stresses in the PB and Q terms, and treating bending stresses as membrane is conservative.
- 6. Since all reported flaws are subsurface with no connection to the weld inside surface or to the coolant chemistry, the intergranular stress corrosion crack (IGSCC) growth mechanism is not active. This mechanism requires reactor water chemistry to be present in the crack.
- 7. The fatigue crack growth law for Austenitic material in Air was taken from ASME Section XI, Appendix C [1]. Since the flaws are subsurface and not wetted, the air law is appropriate.
4.0 FLAW CHARACTERIZATION There are three subsurface flaws requiring further evaluation [3]. Two of these are located in the N6A weld, and one is located in the N6C weld. These flaws are characterized as follows:
Flaw 1 (N6A): Length: 1.4", Through wall dimension: 0.35", Separation from outside surface: 0.2" Flaw 2 (N6A): Length: 1.0", Through wall dimension: 0.3", Separation from outside surface: 0.4" Flaw 3 (N6C): Length: 11", Through wall dimension: 0.3", Separation from outside surface: 0.4" The inspection summary sheets from [3] are attached.
5.0 CALCULATIONS The SI fracture mechanics program pc-CRACK [4] was used to perform the crack growth calculations.
The bounding flaw from the flaw characterizations above (see assumption 1) was taken as: Length: 11",
Through wall dimension: 0.35", Separation from outside surface: 0.2".
This flaw was used as the starting point for the fatigue crack growth calculation. The center-cracked plate model was used to represent the flaw geometry for the crack growth calculation. This is illustrated in Figure 2.
File No.: 0800439.307 Page 4 of 9 Revision: 1 F0306-01
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Reference [5 page 2] gives the maximum stresses experienced at the weld as PL+PB+Q=55.03 ksi for the Inconel material. This is conservatively used to bound the stress magnitude associated with the startup-shutdown and RHR cycles.
For the purposes of the fatigue crack growth calculation, the Kmax is taken as
{PL+PB+Q+RESIDUAL} and the Kmin is taken as RESIDUAL. Consistent with assumption 5, all stresses are conservatively treated as membrane stresses.
The pc-CRACK crack growth results are shown in Figure 3, and the output is included in Appendix C.
It may be seen from these results that for the anticipated number of bounding cycles expected to occur from 2001 to February 2009, only a minimal amount of growth is predicted to occur, even under the very conservative set of assumptions contained herein. The resulting throughwall dimension of the bounding flaw after 100 cycles is 0.366", corresponding to less than 0.02" growth. This meets the acceptance criteria of IWB-3641 [1].
6.0 STRUCTURAL EVALUATION The presence of flaws will reduce the amount of wall thickness in the weld that is available to carry load.
The existing flaws in nozzle N6A have areas of: Flaw 1: Length (1.4) x Throughwall dimension (0.35),=
0.49 in 2; Flaw 2: Length (1.0) x Throughwall dimension (0.3) = 0.3 in2. The combined area is 0.79 in2.
The flaw in N6C has an area of 11 x 0.3 = 3.3 in2 The cross sectional area of the weld without flaws is A=nr(OR 2-IR2)=(49.87-33.78)=50.56 in 2 [7]. So the reported flaws in N6A represent less than 1% of the total area of the weld. The flaw in N6C represents 6.5% of the total area. Removing that amount of material in either weld would increase the stress in the remaining material by the same %. All ASME Allowable stress limits as reported in [5]
continue to be met after projected flaw growth.
7.0 CONCLUSION
S AND DISCUSSIONS The presence of the three reported subsurface fabrication defects and their projected growth due to fatigue does not reduce the capacity of the welds in N6A and C below Code allowable. All Code margins are maintained.
8.0 REFERENCES
- 1. ASME Section XI, 1989 Edition and 2001 Edition with Addenda through 2003
- 2. SI Calculation 0800439.306R0, Residual Heat Removal/Low Pressure Core Injection (RHR/LPCI)
Nozzle, N6, ID Repair Weld Residual + MSIP Analysis
- 4. SI Program "pc-CRACK for Windows", version 3.1-98348
- 5. CB&I Stress Report "238" BWR Vessel" Section S-13 sheet 2. SI File Number 0800439.216 File No.: 0800439.307 Page 5 of 9 Revision: 1 F0306-01
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- 6. E-mail transmittal from D. Patten (First Energy) to Hal Gustin (SI) "Reactor and Recirculation Pipe Heat-Up,Cool Down and Transient History", October 2, 2008 SI File 0800439.214
- 7. CB&I Drawing N6 Nozzle Forging (RHR-LPCI MODE)," CBI VPF No. 3521-257, Rev. 1, June 1973 SI File 0800439.208 File No.: 0800439.307 Revision: 1 Page 6 of 9 F0306-011
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Path 1 Axial Stresses (SY)
Z0000.
60000C'
-1C-cc00 2C*C00*
0
-20000
-4:cc000
-6 0000
-90000 A
Po st-Repair
-i-sm NOPL
-ýeMSIPON
+ PAIP OFF
-~-oNOP2 0.2 0.4 0.6 0.8 1
1.2 Distance frowm weld Inner Surface On.)
14 Figure 1. Path 1 Through-Wall Axial Stress (psi)
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a = C0 REQUIRED INPUTS:
b: plate half width a: maximum crack depth (ax < 0.9b)
Figure 2. Center-Cracked Plate Fracture Mechanics Model File No.: 0800439.307 Page 8 of 9 Revision: 1 F0306-01:
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Crack Growth 0.192 0.190 0.188 0.186 0184 (4
t9 0
20 40 60 80 100 Cycles 120 140 160 180 1200 Figure 3. Crack Growth Through 200 Cycles File No.: 0800439.307 Revision: 1 Page 9 of 9 F0306-017
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APPENDIX A PERRY PLANT CYCLE RECORDS (FROM [61)
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TABLE 1 Reactor and Recirculation Pipe Heat-Up, Cool Down and Transient History Date Event FCRICR Mveasurement Rate of Comment Number Location change in temperature 8/3/1986 CD' CR-86-0740 BIEDN
-I52(*Flhr)
. Event occurred during non-nuclear heat up with reactor pressure:at 760 psig. Bottom head drain temperature recorded at 424 degrees F @ 1730 hours0.02 days <br />0.481 hours <br />0.00286 weeks <br />6.58265e-4 months <br /> and 272 degrees FWi830 hours.
2113/1987 CD FCR-06012 BHDN
-190( 0 F/hr)
Observed cooldouo rate was in the bottom head drain.
Condition enveloped by'loas of feedwatei event of -
00 dem.-F/hr 3/2/1987 CI)
FCR-06128 Bl-DN/CRDN A 80('F/hr)
F'dst qcram issue,'bottom head drain, Recirculation CR-87'01 I I pumps Off-CR-87-0109, 6/1"7/1987 CD FCR-07036 BI-LDN/CRDN "160(°Fdhr)
Bottm head drain experienced a cooldown rate of 160 CR-87-0294 deg, F. Recirculation pumps were secured prior to the
__ "scram with R-WCU isolated stratification to.occurred, 10/27/1987 CDý FCR-08103 B3HDN/CRDN
-230('Ffhx)
Bottom'Iead. drain 10/27/1987 HU FCR-08 103 BI1DN/CRDN 130('F/hr)
Bottom head drain 1116/1987 CD FCR-08264 BHTN/CRDN
.-163(0 Fihr)
Bottom hca drain 1/29/1988:
1'U.
CR488-0049 BIIDN/CRDN
.290(."Fhr)
Bottom head :drain. Hotsstartup RWCU to normal MCR-08944 recirculation mode.
3/10/1988 CJD'
.CR-88-0J-69 BHDN/CRDN
-105(*Fdhr)
B&ttbin head dri.Readtor waterclean up isolatidn.
ýFCR-09324 3/1.1/1988 HU CR-88-0069" BI{DN/CRDN
,1"0('F/hr)
'Bottom,head draii. Reactor water cleanup isolation.
FCR-09324 4/28/1988 CD,
.CR-0-669 B1-[DN/CRDN
.-240(lF/hr)
Bottom head dmin. GE recommended using the ERIS trend plot: fr.temperaitre data.
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TABLE 1 Reactor and Recirculation Pipe Heat-Up, Cool Down and Transient History Date Event FCR/CR Measurement Rate of Comment Number LocAtion cinnge in tern perature 4/28/1988 HU FCR-09669 BI.IDN/CRDN I OWF/hr)
-Bottom head drain 1/7/1990 Cfl.
FCR 13498 Vessel bulk
-I 4C'*hF;r)
Scram event 01-90-01. Based on,ERIS react6r vessel temperature temperature-1/7/1990' HU FCR-13498 Vessel bulk 106(0 Fihr)
Scram event 01-90-01 temperature 1/311992 HU CR-92-001 Main Steam
.1 75(*F/hr)
Downstream of inboard NMSIVs 9111/1992 CD
-PIF-97-I280' All Components
-110(
OF/hr)
Bottom hcad (cwluding drain tcmpcraturc).
LER 97-008
<100(-F)
Re6iiculation'pipinr remained within limits. Do&s not I
I I include bottom head drain.
9/11/1992) 03/26/93
ýC)
HfU I=D "PIF-97-1280 BHDDN 235(-F/hr)
.Rw*1 isolation 115 from page 8 of P*F for one.hour period..
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TABLE i Reactor and Recirculation Pipe Heat-Up, Cool Down and Transient History rI Date Event FCR/CR IMeasurement Rate of Ceoment Number Location change in I
I Transformer outage 9/14/9.7 CD NIA AllComponentsý
<100 (CF/hr) -(Cycle 6-4 end) Cooldown monitoredby SVIB21-Refuel-6 T 1176 dated 9/13197 with no discrepanciesi-ientified
'12/19197(Cyctel-end) Cooldown m oni tored ohy s V !-B21 -
2/19tr7o-T T 1176 F
H dated, - 2121/)T7 wh no diasdrcpaicies identified.
hydýrauic
';6ecirculation pipe and bottom head-siayed above 400 cdontrol (N32) deg. F. No SRV setuations no MS V clontre, no
_ECCS ihectienK 07-0198 CD CR-98-1421 BIDN 32 (Cycle 72) Following'a ara,*bottosa ead drain Inadvertent 40("Fimýi) cooled dovn then heated back up.,,SID2l1T-176
- RCIC, dated1/J79,8 indicated vesl maintained'above 400:
Injection d...
03/27/99' N/A All ComipoientS
<100I(,F~hr)
- (Cycle7-31end) SVYIB21 -Tl 176dated'3/27/99 review.
Refuel outage 7
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TABLE 1 Reactor and Recirculation Pipe Heat-Up, Cool Down and Transient History Date Event FC RI R Measurement Rate of Comment.
Number Location change in temperature 0&04100 Fuel CD N/A All components
<100 ('F/br)
(Cycle 8-1 end) SVI-1321-T 1l76 dated 615/00 defect Outage 02/17101 CD N/A All components
<100,(PF/hr)
.(Cycle,8-2ecnd) SVIB21-TI176datec 2/19i01 Refuel - 8 03/22/01 Start HU N/A All components
<100(1F/hr)
-(Cycle-9-1) SVI-B21-Tl.176,order 01-006979-000 Urp 0119eaooctor d5/ Rat9r/01
~
?i Fmo
~
-ahm ret p
trensients S GI C521 R
C, Ieprtr Recirculatno pipetmprtroa 05/1.5101 'Start.
RU N/A AIl'componnts:
<100 ('F/b'r)
(Cyelc. 9-2) SVI -B21-T1 176.order!0 *010584 00 up 05/06'/0lir CD" N/A
.All components
.<300 ('F/br-)
'(vycle'9-2end).SVl-B32 -TI I376 01-c0012-01008dated recircuiolat1 117,6on 05/15/01 Start.
H R
N/A All'components
<100 (FF/hr)
(Cyclc.972) SVI-B21-TI 176 order l-011041-000 Up 05/08/01 Cie CD-N/A All components
<11O00 (F/hr).
'(yclc1 9-3 end) SVI-B2l-TtI.76bre 0
t-008724 840dte 05/1.5-0 1 ýStart HU N/A Aullcomaponents.
<100 ('IFfh)
(Cycle 974) SY1-S21-T I I Xorder 0,1 -0,10571;-090 Up~
Pa&,4 of'S File No.: 0800439.307 Revision: 1 F0306-O1RO Page A-4 of A-8
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TABLE 1 Reactor and Recirculation Pipe Heat-Up, Cool Down and Transient History Date
- Event, FCRC R.
Measurement Rate of Comment
- Number, location change in
__Stemrperature 07-12-01 Loss 17ý701-27f7 13JfrY (C
e9ý-4 en 0)(7Tollowig a scramtomt headdrain 0f....... 1A cowri.
ipCS ant RCtC. injecting. 4Noo*her Unplanned cbrýomponents oted as affectic..ei~cuintio<
Power cmrgc
.l2riFI' 7
nordoecirla-Le )
on Adata. SVl.
07117/01 KTU-N/A All components
<100 (CF/hr)
SVI-B21 -771.76-order 01-012463-000 Heat up partial heat up terminated at 388 degrees F 07/30/01 Start 1HU NIA All components
<l00(*F/hr)
(Cycle.9-S)SVI-B21-77176 order'01-012800-000
("l (Cceý.5'nd) Followinkja plant sermiRýCM Z-1I i.)
r2 MPG jcu
'It BIMi~ha P.1 tI- -,Cf-(rinba -s uprY
,~.dgrnIncaxiwm to, frc, ircukoion pipn&2 VT%
Ltru LoopBl hP76O177 k
I -Q0*5n'ith
)1-1MrdidanoteCoMPk4 ely" 12/18/1 Start HU N/A A~llComponcnt e ]X) ("rI*) (Cyclel9-6) B21 -.T1I!76-ord&-01-018093-000 VceAel up heat-i, hegannwithl-shell flange at 410 dbeg. F.
6/04/02.
CD N/A AlltComponents
.<100:(*Fbr)
- (Cycle 9-6 end) Operators reduced power to ebout 25%
'Turbine Trip prior to0trip. Steam bypass used. SVI-.B21-TrI76 exciter g*round noted no abnormal cooldown rates.
06/12/02 Start FI-U N/A All Components
< 100 ('Fihr)
(Cycle 977) SVI-B21 -TI 176 order 02-006681-000 Up 9/22/02 CD N/A All Components. ý<100 (F/1hr)
(Cycle 9-7 cnd) SVI-.1321-T 176 order 02-010433-
,Readtor scram 000: noted no abnormal cooldown rates-durng turbine toverVs>ed test 10/03/02'Start M-U N/A All-omponntsý,
<1(0('eý/hr)'
(Cyyc!, 9-8)'SV.-I-21M 11-6 order 02-010919-0O00 fp, 4/05/03 Refuel
,C7D' NIA AIWCoijp.dneuits-
<100 ("F/hr). (Cycle 9-8 end) SVI --B2 1-T1.176 order 03-003499ý-
10 shutdowri I
(M."
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TABLE.1 Rcactor and Rcecirculation P ipeHcat-Up, Cool Down and Transient History.
Date Event FCR/CR Measurcment Rate of Comment Number Location change in temperature 5/30/03 Sart I-HU N/A All components
< 100 (CF/hr).
(Cycle !0-l)'Sl - B21-TI 176/order 03-5567 up 8/14/03 Grid CD NIA Rcciroulation
< 100 (CFihr)
(Cycle 10-1,cd)
SVI -B21-TI 176/order 200047329 Instability pipe shutdown I
I 8/21/03"Start rU N/A All components
<100 (*Fib)
(CyVcle 10-2)sVI -B21 -TI1.76.forder.200047975 10115/2003 N/A CR 03-N/A N/A Notemperature transient for recirculation pipe or Inadvertent 05745 vessel..
SRV. lifts at power 5/22/04 ESW
- CD NIA All compt'nents
<:100 (CF/hr) (Cycle 10-2.end).SVI-B21T! 1,76,/ordcr,20009.7558 pump A,fiilure Reactor shufdown
,63/04 Startup HU N/A All components
<100 (CF/hr) Heat
'pterminated becauseof.RHR A inoperability
'terminated S'Y,-- B21-TI176 lorder 200099438. Maximum vessel temperature recordixd 145!degmre F.
"6/7/03 Staft up RU N/A All.compornents
<.100:( 0 F/hr)
(Cycle- 0-3) SVI - B21-T1 1176 /order-200(V9931.
12/23/04 CDr CR 04-Alleomponents
<100 '(F/hr) '(Cycle 10-3 end) SVI -- B21-T1 176 /order 200134592.
- Redt'or Recire 06763 Follvvirgý rcir. pummp shi*t, reactor'scrsmmedoat 2354 pumps shifted hours,.level-3. at 2355 hours0.0273 days <br />0.654 hours <br />0.00389 weeks <br />8.960775e-4 months <br /> reactor feed,Purp turbine; to low spe-d tripped-on level 8.
12/25/04 Start HUti NIA All,components
<100 ?Fihr)
,(Cycle O--4),SV -B21-Ti 1,76 larder 200134661.
Up Head flange iemperature-atsamt.ias385 degrees F 1/06/05' CD CR054X094 All-compaonents,
< I(410 F/br)
(Cycle 10-4tend) Reaetorseram SVI 321-rtI117 Reiriruiation
/order.200135950. Notethis'evolutibn referred toas-
- -pumps*
-Cycle
.0-5'cooldown.. Manual scram, mptor fee*dmp downshifted I would-not start, RCIC inlecion.
1/30/05 Start U
N/A.
AU compfonents
<l0(tF/hr)
(Cycle, 10-5)SVI -B21-T.1176 /order 200139105.
1 U00 ptr l
/.
l a
oet 5
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TABI.,E I Reactor and Recirculation Pipe Heat-Up, Cool. D1own and l'ransient History Date Event FCR/CR Measurement Rate of' Comment Number Location change in temperature 2M22/05 CD, N/A All c poanent
<100 ("F/hr)
(Cycle 10-5 end or Cycle I I cooldown) tripped.main Shutdown turbine for RFO. 10. SVI - 1321 -Ti 176 /order
.Refuel 10 200143104.
5/l/05'Start up HU N/A All components
< 100:(°F/hr)
(Cycle.11-1) SVI - B21-Tr176/order 200149024 and 200149436 5/08/06 B33 N/A -
N/A N/A:
N/A (Cycle 11 - 1) Turbine trip. Plant maintained.at.5%
'hydraulic line Power leak 12/13/06 P52 CD-N/A All components.
< I0 (F/hi)
'(Cycle 1.1-1 ends or cycle. 11-2 cooldn).Scram 0354 airt line rupture, houws. 'SVI -*B2l-T1 176/orders 200244661 and 662.
12/18106 Start HRU N/A All components
< 00f'Fihr)
(Cycle 1:1-2)ýSVI - B21-T 1176/order 200245021 4/02/07:Refuel CD CR 07-Reciirculation
< 109 (°F/hr)
(Cycle 1.1 - 2 ends) SVI - 1321-T.I 176/order.
11 17349 Pipe and other 200258535. Attachment i to CR identifies'bounding corm ponents rates.
5/10/07strt
.-HeamLup.
N/A N/A
<100 (.FAr).
(Cycle'12-1.):SVI - B21-TI 1.76 /order. 200263389 up Cycle 12 5/12/07.
N/A N/A N/AI
<100("1/hr)
(Cycle 1.2-),.nqtfull~power, 205.4 per Iog !nry. Trip at Turbi.e trip
.06:50 houri.3 NNR cir ulationtcmpcmture changes.
-perPl plot 5/12/07 - 5/14107 5/13/07.
'N/A N/A All componerits-
<10{'/hr)
(Cycle
<12-Reator cr ieal at 0:28 hours. Per,1 plot Turbine trip
.ractor.remaifn critical 5/15/07, CD N/A All components'
- 10 (WF/hi) (Cycle.12-I end) 3lipowir00:58,hours..FW tuning Reactor scram.
issues SVI -B 1321]-T 1761/order 20(0264161
,5/17/07 Heat, Heat up N/A Allcomponents
<.100 (F/hr)
(Cycle 12-.2 begin) SVI - B21-T 1176'lorder up I200264205 5/18/07.
N/A N/A All'component~s,
<100 (fi)
(Cycle 12,2.).Reactor-remains criticasnothermal Turbine trip
/hanges io.t rcirculation piping bas.don P1 plot May 1? 8, 2007 6/22/07 FCV.
N/A N/A AllWCom poncnts
< 0f(,F/hr)
(Qycle. 12-2 end )'semmat 0329 SVI - B21 LT 1-76' lockup"
/order 200270642 Vessel maintained at approximately page 7 of 9-File No.: 0800439.307 Revision: 1 Page A-7 of A-8 F0306-O1RO
V Structural Integrity Associates, Inc.
TABLE I Reactor and Recirculation Pipe Heat-Up, Cool Down and Transient -History Dale Event.
FCRFCR Mteasuremend Rate or Comment Number LocalIon change In temperature 400 degrees 6/24/07 start Heat up N/A All Components
<100 ("F/hr).
(Cycle I12-3) SVI - B21 -TI 1176/order 200270642 UP Vessel warm up from approximately 400 degrees 6W29107 133:
CD)
N/A All Components
< 100 (0F/hr), ý(ycle 12-3 end ) S'V - B2 1-T) 176 /order 200270642 rmotor replacement 7r23/07start Heat up N/A AlI.ComponenLs
<100("F/hr)
(Cycle 12-4) SV[ - B21-TIl76 /order 200275907 Notes:
J1. Hig31lighted events hive recirculation temperature rates exceeding-115 degrees F. flit Page,8" of 8-File No.: 0800439.307 Page A-8 of A-8 Revision: 1 F0306-OIRO
V Structural Integrity Associates, Inc.
APPENDIX B INSPECTION
SUMMARY
SHEETS FROM [3]
File No.: 0800439.307 Revision: 1 F0306-O1RO Page B-1 of B-1O
t Structural Integrity Associates, Inc.
eDRF N6:0000-OO9.1-3569 Rev.IG a
HITACHI Austenititc, Piping:
Flaw Evaluation Sheet Project: Perry.Unit 1 weldlO:
I BV:31NbA-KB Indication: 1.
Sizing Ddta SheetŽ,
/A, Measured
'T" nominal =
1.20 "r ihnea~ued =
1.20:
Flaw Through Wall =
Flaw Length 1T'=
Surface Separatiorf '"'=
Measured Rounded 0:34 0.35 1:40 1A 0.21 0.2
- 1.2 ASME Sectibn XI, 196.EdItion,,No Addehd a
-TABLE IWB-3514-2 AUstenitic Steels,,1.2:lnchNdffiinhal Thibkness - Inservice aA surfdce96 Subsurfa&e.
Surfae%
subsrface 46 0.00 105
-103.5 OOs 10.6 10.6 0.10 10.9 10.9
.10.93, 10.93 Y O:AS 11.0 11.0 0120 1.1:3r 11:3 0:25 11.4 11:4 030 11:6 1166.
035 11.8 11.8 0.40 12.0 12.0 0.45 121 12.1 0-S.0 12.3
- 12:3 kAll-ov O6,
A low ed
'10.93i 10.93 19 =
- 0
- 175 a
Y!
valyu
=
o.125 V =
.0*00 Ifa/i>.S.jhen all =.5 Y Sa W>1 hnV=
Flaw isSPbsurface at 1-4.6%.
Flaw is unaccel*tableby Table iWB-3514-2,:
Rei.d: 112710 Comments:-ASME Section X1 rounding performed. inaccordance with IWA-3200:and ASTM E29.
Indication is circumferential in orientation.
Flaw is locaLed aL 12.7': CW rirTDCXO.2l'UpsL-earn fioufWeldCeirlerlirie(Safe-End Side)
Evaluated, By Ro bert Healey.
RO.vewerd. By:
Level:
Ill Date: 09-13'2008 Level::., __
ate:1 lPoge 20 of-.213 P6ge;235'of 303.
File No.: 0800439.307 Revision: 1 Page B-2 of B-10 F0306-OIRO
V Structural Integrity Associates, Inc.
eDRF No 00001-0091 -3569 Rev."0 O
HITACHI A1stenitic Pipi-ng Fla'W'*Eva luadtiph sheet Project F Perry Unit 1 Weld ID ; IB13-N6A;KB Exam Data Sheet: ; 1Q800-01-021 Indication: 2 Sizing Data Sheet.:;.N/A Measured Rounded Measured Rounded FRaw Through Wall=
028 10..3 i'7nomina =
12.0
- 1. 2 Flaw Length ""=
1!00 1.0:
'T<measu.d
,20 1.2 Su rface-Sepa ration S"S' 0..40 0.4ý eASlE Section XI, J989 Edi tion, No-Addenda TABLE IWB*3514:2 Austenitic Steels.l1.2 Inch Nmrnial Thickness-Inservice 6/1 Surface.
. Subsbrfaoc% ýSurfdcel Sublurfoi~eyo/
0.00.
10.5 10.5 0.05, 106 10:6 0.10 10.9 10.9 015 11.0
.11"0 10.98
,I098Y 0.20.
113 11.3 0.25 11.4
- 11.4 0.30 11.6 11.66, 0.35 11.8 11.8.
0.40 i.b 12,.0 0.45 12.1 121 Allowed Allowed "10.98
'10.98 i
=
- 0`150
- q/ivolue=
-f0.150 Yz=
1.000 Flqwis 'Subsurfoce Allowed aot=.
lf.o%:
Flaw is unacceptable by Table IWB-3514-2.
Comments: ASME Section Xl roundingperformed in occordance with IWA-3200 ond ASTM E29.
Indication is circumferential in ofientotiob.
Flaw is. located dt.21.7"CW from TDC, 0 2"UpStreom~frorn -Weld,Cdnterline (Safe:End Side)'
Evoluatea 13y:
Robert Healey Reviewed By:
Levelh IlI Dote: 09-13-2008 Level:.
Dote: __
Page'21.bf 23' Pege:236.of 303 File No.: 0800439.307 Revision: 1 Page B-3 of B-10 F0306-OIRO
V Structural Integrity Associates, Inc.
eDRF Not 0000,091-3569Rev.a0, SHITACHI Au steinitic.Pipjng Fiaw: EVa luationh sheent Project Perry Unit I Weld ID: 1B134N6A-KB Exam Doto, Sheetl: 1Q800-01-021 Indication: 3 Sizing Data Sheet.: N/A Measured Rodnded:
Mea suied
-Rounded Flaw Through W6.=1 017
.15
'T'nomina/=
1?29 112 Flow Length 16"=
1.80 18
'7,meosured=
1420 SutoceSeparationS=
0.:5Q
!05,:
ASM E'Section X1, 1989 Edition, No Addenda TABLE IWB-3514 -2 Austenitic Steels, 1:2.1'nch l n
minal Thickness - inseryice
.I Surface %
, Subsurfb6e,%
'Surfacb %
- Subsurfuc%.
0U001 10.5 10.5 10.58 10.58Y 0.05 10.6 110.6 0.10 10:9 10.9 0.15 110 11.0:
0.20 113 41.3 0.25 114
.11.4 0.30 11.6
.11.6 0.35 11.8 11.8 6.
0.46 10b
'12.6 0.45 12.Y t12.1 All6wed
'Allowed 10.58, 10.58 0 =
0:075 oa/value=
0,0'42 Flow, is S bsur-face.
'4liowed'a/t =
.10ý6 o/.t=
6.3%
Flaw is acceptable by Table IWBý3514-2.
Comments, ASME Section X1 rounding performed in accordahne with IWA-3200.and'AST1 E29..
Indicatidr is circumferentidl in oriehtotion.
Flow is located ot.37.6"'CW from TDC,0..I" Uostream from.Weld.Centerlinet(SdfoeEhd Side)
Evaluated B'y:
Rbert Hedleyz
,eviewed By:
Level:
IIl Date: 09-13:2008 Levdi:,
Dote:.
-Page 22of 23
ý' age '2 3 7,0 f 30'3'.
File No.: 0800439.307 Revision: 1 Page B-4 of B-10 F0306-O1RO
~Structural Integrity Associates, Inc.
eDRF No. 0000:0091-3569 Rev. 0.
O HITACHI Austenitiq.Piping Project: Perry Unit 1 Weld ID: 1B13-N6A-KB Exam Data Sheet.:';.Q800-O1-021 Indication: 4 Sizing Data Sheet; VN/A Measured Rounded Heasbredl R6unded Flow Through Wall =
0.07 0.05
'7"nominal =
1.20 12, Flow Length Qr 80.
~
'T mnea sured=
12, 2
Surfoce'Sepaortion "S-0,75 0.75 ASME"SectionXl, 1989 Edition. NoAddenda TABLE IWB-3514,2 Austenitic Steels.i 2Z Inch Nominal Thickness-Inservice 6/I Suiface%
Sub'surf66e%
fSrfoýe,%'
Subs6ffdc %
0.00 10.5 105 10.56 10.56Y 0.05 10.6
'10.6 0.10 10.9 10.9 0.15 1110 1-.0 020 11.3
.11.3, 0.25 11,4 11.4 0.30 11.6
.11.6
-~
0.35 11.8 11.8 0:40 12.0' 12.0 0.45 12.1
ý12.1 0.50 123J 12.3 Allowed' AIlowed 10:56
- 10.56,
- a =
"0025
-0/1 volue
'0.031 Y=
,1.0bo Flow is Su6surfoce
- Ailowedi a/t =
16o
,6%,
oat=
2:1%
Flaw is acceptablelby Table IWBZ3514ý2.
Comments: ASME Section Xl roundincgperformed in accordancewith IWA-3200 and ASTM E29.
Indication is circumferential in orientation.
Flow is locatedat 4010" CW from TDC,0:2"Upstream fromWeld"Center line (Sdfe-End.Side)
Evoluated By:
Robert Healey JRevewed'By:
Level:
I1.
Date: 01§'13-2008 Level__
Dota te:_
Page 231of 23' PFage 238 of 303,:
File No.: 0800439.307 Revision: 1 Page B-5 of B-10 F0306-O1RO
V Structural Integrity Associates, Inc.
eDRF No 0000 0091'3569R6v.I0; SHITACHI
- Austienhitid Piping, Flaw Eval1uatioln !heet Project: Perry.Unit 1 Weld ID: 1B 13-N6C-KB Exoin Dto Sheet. '1Q800-01-027 Indicati'on ; 1
.Sizig Dotd Sheet N/A Measdred Rounded
ýMeasuied Rounded
'Flow Through Wo!l=
0.14 0.15
.T' nominal=
120 1.2 Flaw Length 'T.=
0:60
ý0.6
.',measured=
120 1.2 Surfoce Seporotion '"
05.8 006 ASME'SectionXiX, i§8§ Edition, INoAddenda TABLt IW1B-35i*4-, Austenitic Steels,' 2 Inch:Nominc Thickness - inservice, o/I SurfaCe %
Sub*drfdceA%
'Serfac %W Sibsuifde6' %
0.00 10.5 410.5 0.05 10.6 10.6 7
0.10 109 10.9 10:93 10,93,'
0.15 11.0 110 0.20.
113
.11.3 0.25 114 11.4 030 11.6 11.6 0.35 11.8 11U8 0.40
'12.0"
'12.0 0.45 12.1' 121 0.50.
12.3 12.3 Allowed Allowed,-
10.93 10.93.
o=
b.075 a/.0alue 012
- Y=
- 1.000 Flaw;is: Subsurface.
,Allowed'a/t
'10:9%:
o/t=
.6.3%9 FlWe is aciceptable by T*bi6 IWB'3514ý2:..
Comments: ASME Section XI r0undinqgperformed:in accorddnce:with IWA-3200,and ASTM E29.
Indication is circumferential in oFientation; Flaw is located at 4:5" CW from TDC 0.1' Downstream ffom Weld Centerline (Nozzle Side)
Evaluated By:.
FobertHealey, Reviewed By:
Level:
III D ate: 022.32b008, LeveI:
Dote:,__
Pqgea24-'df.28:
Page 280of 303 File No.: 0800439.307 Page B-6 of B-10 Revision: 1 F0306-OIRO
V Structural Integrity Associates, Inc.
eDRF Nol 0000-0091-3569 Rev. 0' HITACHI Austenfitc-Piping-Flaw Evaluatiodn'Sheet Project: Perry Uhiti1 Weld ID" 4.B13-N6C-KB Exom DataShe$et:.1Q800-01-027 Indication.' 2; Sizing: Dat ShdeSt N'/A I1eosdired Rounded Mea sUregd Roinded Flow Through Wall.=
0.19 0.2ý "Týnominol:=
1.20 1,2 Flaw Length 'T"=
3.70 3.7' ti7'measured=
1.20 1.2 SurfaceSeparation "S'=
0.45 0.45 ASHtE.Section XJ, i§89 Edition, No Addenda TABLE IWB.-35l44-iAustenitic Steels;'l.2/Inch Nominal Thickness - Inservice.
aiI Surface %
".Subs6rfac.%'
Surface %,
Subsu-rfdte %
0.00 10.5
'10.5 10.54 A10.54 Y 0.05 10.6 10.6 0.10.
10'9 10.9 0.15 11.0 Iit0 0.20:
11.3 11.3 0,25 11.4 11.4 0.30:
11.6 11.6 0.35 11:8 11.8 040 i2.b"
'i2.6 0:4S i2 1i2.1 00o 12.3j 12*3 Allowed Alowed 10.54 10.54t
,a =
d:4lOo
"=
o1o00 Flow is'S'b sur'ffce
- Allowed o/t =
10.5%.
o/t =
8:3%9 Flaw is acteptable by Table IWB83514-2.
Comments:. ASME Section Xl founding performed, inbccordonce with IWA-3200 ond'ASTM E29:
Indidotion is circumferentidl ih ohentatioii Flawvis locoted ot.8.0" W6,'from tTDQ 0:1" DoWnstrerianfrom Weld Centerline(NozzleSidel Evaluated Ey:
Robert Healeyl Rýeviewed By:..
Level:
III.
'Date: 0§2.3-2b08 Level:
oe:._
Page 25-Of 28 Pa ge'28.1',of b3 File No.: 0800439.307 Revision: I Page B-7 of B-10 F0306-01RO
V Structural Integrity Associates, Inc.
eDRF No 00007009173569 Rev. 0 HITACHI Amsttenitid Pip'ing F.id.w. Eval~uation Sheet Project: Perry Unit 1 Weld ID: 1B13-N6C-KB Eom Data Sheet.- '.iQ800-01-027 Indication: 3 Sizing Ddtd Sheet: N/A Measured Rounded
,Hesuid RoUnded Flow Through Wal =
0.31 0.3
'T'nominalo=
1.20 1.2 Flow Length "r"=
11.0:
i1.0 T'measured=
1.20 1.2 Sufiace'Separation ""=
042 04
'ASM'ESection XI 19 89 Edi'tion, NoAddenda TABLE IWB-3514-24Austeritic Steels i.2II 2nch k Nominal Thickness I-"nseruIice.,
6/I Surface %
'Sub06rf0ad/%
Si'rfoce %'
Subsirf6e %.
0.00 10.5
ý10.5 10.51,
- 1.51iY-0,05 10.6 10.6 0.10, 1019 10.9 7.
0.15 11.0 11i0 0.20 11.3 11.3
.0.25 11.4
,11.4 0.30, 11.6
.11.6 0.35 11ý 11.86 0.40 12.6 12.0 0.45 f2 121
-,12.
.5" 12,.3
ý123 kllowed
!Ilowved.
10.51 10.51 a,=.
0'150 a/l value=
.0014 Y = 1.000 Flow-is "%.6bsurface
- lowed a/tf=
105%:
a/t=
12.5%,
Flaw is unacceptable by Table IWB-3514-2.
- Re e 1/2T/
Comments: ASME Section XI rounding performed inaccordance with IWA-3200 and ASTM E29.
Iridiiati6h is circumferential in orientation.
Flaw is locdtdd at 15.1"'CW from.TDC, otthe Weld CeriteFlihe Evaluated By:
RobertHealey
-ýeviewed Iy:,
Level:
III Date: 09-23-2008 Level:
Date:.:
Pag e 26 of281 Pge282ýOf 33 File No.: 0800439.307 Page B-8 of B-10 Revision: 1 F0306-0IRO
C Structural Integrity Associates, Inc.
6DRF N6. 000M6091-3569 Rev:'0, 0
1 HITACHI Austenitic Piping Flaw EvalUation Sheet Project.: Periy.Unit 1 Weld ID; -lB13-N6C-KB ExoaDdto Sheet '1Q800.
indication i '4 Sizii.
Data Sheet,'. N/A' Measured Rounded Mea Flow Through Wa!l =
.0:24 025
'T'nominal 1
Flow Length 2.00
'.0 7t'"meoured=
i Surface Sepomtion "S"--
0.48 0.5 ASýE SectioriXi, 1989 Edition, NoAddenda TABLE IWB -3514-2 Aust erticSteeIs.2~In~chNomi*nal'Thickness,,Ihservice, 0ll Surfa6e%
'Subdff6ce/%
surface S
o%' Subsrd6e,%"
0.00 10.5 110.5 0.0S 10.6 10.6 10.67
- 10.07y' 0,10 10.9 10.9 0.15 11.0
'I1.0 0.20 11:3 11:3 0.25 11.4
- 11.4 0.30 11.6
-11.6 035 11.8
.8 0o40 o
1.0
- 12.b 0.45 1I2 f2.1 0.50' 123 12ý.3 Allowed Alowed 16.67.
. 10.67'
".0=
0.125 a/I value =
0063 F lbw, is S ub surface, Allowedidt-=
i0.7%'
a/t=
10.;%.
Flaw is acceptable by TabIe IWB-351*-2. 027 sured o20
.2b 6DRF No', 0000:0091-3569 Rev:'i0 Rounded 1.2
- 1. 2 Comments: ASME Section XI rounding~performed in accordance with IWA-3200,bnd.ASTM E29..
lrwltrctinn i'~ circi imfprpntinl innriPntritinrt Fldw is. b6ated at 25.2" CW frorh TDC, 0.1" Upstream from Weld Centerline (Safe-End Side)
Evaluated By:.
ober*tHealey
'Reviewed by:..
Level:
iII D a te: 09,23-2008 Level:
_Dote:,.
P.,e27>t'28&
Page:283_of.303 File No.: 0800439.307 File No.: 0800439.307 Revision: 1 F0306-O1RO Page B-9 of B-10
V Structural Integrity Associates, Inc.
eDRF Nd'. 0000!0091'3569 Rev.0' 1HITACHI Austenitic Piping Flaw Evaluation Sheet SPrbjact: Perf9Unitl Weld ID;: '1B13-N6C-KB Indication," 5 Flow Through Wqll=
Flow.LengOth '=
Surface Separation !'S"=
.Mesured 0.23 1.80 0:.37 Rouncýd 0325 0ý35 Exbam Ddto' Sheet: *IQ800-01-027
.Siziri D*,to Sheet : N/A "77 nomindl =
120
,T'measured=
12 1.2
'12 ASM E Section M, 1 989 Edition,,o Addenda
'TABLE IWB-3514-2 Austeni-tic Stee'ls.'-1.2.lnch.Nominal. Thic.kness - Inservice Q =
10:25 a/I value =
Vo0§ F.,ow:is:S'Ubsur"oce Aiiowed c/th= 107% "
a t=
i06.0 %
Flow is acceptable 6y Tdiol* IWB-3514,;2.
Comments:. ASME Section XI rounding performed inioccordance with IWA-3200 andASTM E29..
Indication is circumferential in orientotion.
Evaluated By:
Robert Healey Reviewed By:_
Level:.
Ili Odte: 09-,23-2008 Level:
Date:.
IPage 28ot '28' Raqge'"284-of 303 File No.: 0800439.307 Revision: 1 Page B-10 of B-1O F0306-O1RO
Structural Integrity Associates, Inc.
APPENDIX C PC-CRACK OUTPUT File No.: 0800439.307 Revision: 1 F0306-O1RO Page C-1 of C-7
Structural Integrity Associates, Inc.
PLPBQ. our tm pc-CRACK for windows Version 3:.,1-98348 (C) copyright ! 84 -
'98 Structural Integrity Associates, Inc.
3315 Almaden. Expr6ssway, suite 24
'San Jose,. CA,95118-1557 Voice:
408-978-8200 Fax:
408-978-8964 E-mail : pccrackestructint.com Linear Elastic Fracture Mechanfics, Date:, Thu Oct 02 13:22:16 2008 Input Data and Results File" PLPBQ.LFM
Title:
0800439: N6 A and C Flaw Evaluation Load Cases:
Case ID Unit Membrane Residual consta Through wall Wall Case Depth Unit Meihbr stress Coefficients co Cl 10
'0 20 0
C2 0
C3 0,0 Type Coeff Coeff stresses for Load cases with stress coeff "
Case Residual c 0.0000 10
- 20 0:0300 10 20 0.0600 10
.20 0.0900:
10 20 0.1200 10 20 0.1500 10 20 0.1800' 10*
26, 0.2100 10
- 20 0.2400 10
- 20 0.2700 10 20 0.30006 10 20 crack Model : center cracked Plate 'under Remote Tension Stress Crack Parameters:
Plate Half width:
0.6000 crack depth:
0.3000 CO = Remote Tension stress All other stress coefficients are neglected.
S Stress Intensity Factor................----
Crack Case Case Size unit Membr Residual c 0.0060 1.37302 2.74604 0.0120 1.94209
- 3.88417 Page '1 File No.: 0800439.307 Revision: 1 Page C-2 of C-7 F0306-OIRO
V Structural Integrity Associates, Inc.
PLPBQ. OUT:
- 0. 0180' 0.0240 0.0300
- 0. 0360 0.0426 0.0480
- 0. 0540Q 0.0600 0.0660 0.0720 0.0780 0.0840
- 0. 0900
- 0. 0960
- 0. 1020 0.1080 0,1140
.0.1 200 0.1260!
- 0. 1320
- o. 1380 0.1440
- 0. 1500
- 0. 1560.
- 0. 1620, 0.1680' 0.1740 0.1800 0.1860 0.1920
- 0. 1980
,0. 2040.
0.2100
- 0. 2160 0.2220 0.2280
- 0. 2340 0.2400
- 0. 2460' 0.2520 0.2580 0.2640 0.2700 0.2760 0.2820
- 0. 2'880 0.2940
- 0. 3000 2.37926 2.74848 3.07453 3.37o18 3 64303 3.89804 4.13869 4.36752 4.58645 4.79701 5,00041 5.19763 5.38951 5.,57675 5.75995 5.93964 6.11628 6.29028 6.462 6.63178 6.79992 6.96671 7.1324
- 7. 29724 7.46146 7.62527 7.78889 7..95251 8.11632 8.28053 8.44531 8'. 61084-8.77732 8.9449 9.11379 9.,28416 9.:4562 9,'63009 9.80602
'9.9842
- 10. 1648 10.3481.
10.5342
- 10. 7235 10.916.
- 11. 1121
- 11. 3121 11.:5161 4.75853,
.5.49695.
- 6. 14906 6.74036 7.:28605 7.79608
'8. 27738 8.7,35,03 9.17291
- 9. 59403
- 10. 0008 10.3953
- 10. 779 1
- 1. 153 5 11.5199
- 11. 87931
- 12.2326 12.5806 12.924:
13.2636
- 13. 5998
'13.9334 14.2648 14.. 5945' 14.9229 15ý.'2505
- 15. 5778 15.9051
'16. 2326 16.5611 16.8906 17.-2217, 17.5546 17.8898 18'.2276
- 18: 5683 18.91224 19.2602 19.6121 19.,9684 20.3296 20.6962 21.0684 21.,4469 2:1.832:
22.2242 22.,62041
- 23..0322; crack Growth Laws:
Law ID:
Sect -XI AUS Air Model:
ASME Section XI - austehitic stainless steel in air environment da/dN = C'4 lOAF
- S dKA3.3.
wheres = 10 for R<0
= 1.0 4 1.8
- R fdorO <.R c.'0.79
= -43.5 + 57.97 1ý R for 0M79 < R < 1, F = code specified functionr.of temperatdre dK = Kmax -
Kmih R m *in/'
Kmaxk Page 2 File No.: 0800439.307 Page C-3 of C-7 Revision: 1 F0306-OIRO
V Structural Integrity Associates, Inc.
PLPBQ.OUT where:
C
- 10AF =
1.8403e-010 is for the currently selected units of::
force: kip length: inch temperature:
550.0000 Fahrenheit Material Fracture Toughness KIC:.
Material ID: Alloy 182 Depth KIc 0.0000 200.0000 0.5000 200.0000 1.0000 200.0000 1.50006 200.0000 Initial crack size--
0.1750, Max. crack size= '
0.3000 Number.of blocks=
Print increment of'block=
1 Subblock Cycl'es Calc.
Print Crk. Grw.
/Time incre. incre. Law' Mat.
KiC perryl 200 1
1 Sect XIAus Air -Alloy 182, Subblock Keax case ioscale Factor
, Kmin
- casel,3:D Scal e *F actor Perryl Residual constant unit Memnbrane 1.5000 Residual constant 5.5o00 1.s0OO crack growth results:
Total Cycles a/Time a/thk Subblock cycles
./Time Kinax l0ni n
.Del tal(
Ddnn R /D-aDt Da
,a Block:
1 1
2.
3 4
5 6
78 9
10 12 12.
I 2
3 4
5 6
7
.8 9.
10 11
.12 6'.64e+001 2 34e+001 4.3 de001 0.35 1.39e-00O 6.65e+001 2*35e+001 4.30e+001 '0.35 7-.39e-005 6.65e+001 2.35e+001.4.30eL001 0.35 7,40e-005
&6;65e+001 2.35e+001 4.J30e+001 0.35 7. 41e-005 6-.65e+001 2 35e001 '4.30e+001 0.35 7.41e-005
- 6.
65e+*O01 235e+001 '4.30e+001 0.35 7. 42e-005 6.65e+001 2.35e+001 4.31e+001 0.35 7.43e-005 6.66i+001 2.35e+001 4.316-O01 0.35 7.ý43e-005 6,.66e+001 2:.35e401 ý4.J31ie+0 0.35 7.44e-o05 6&66e+001 2.35e-+001 4.31e06i 0:35 7.45-6005 6.66e+001 2.35e+001 4.31e&001 0.35 7.,45e-005 6.66e+001 2.35e+001 4.31e+001 0:35 7146e-005 Page 3
- 7.39e-0o5!
7.'39e-005 7.40e-005 7.,41e-o05.
7.41e-005, 7.,42e-O05 7.ý43e-005 7.43i-005 7.44b-005 7.45e-oo5' 7A45e-005
- 7.
46&- 005 b.1751 0V29 0.:1751 0.29 0.'1752 0.29 0.17.53.0.29 0.1754.,0.29 0.'1754,0.29 0.1755 0.29 0*1756. 0.29 0.17,57 ý0.29 0.1757 '0.29 0.1758 0.29 0.1759 0.29 File No.: 0800439.307 Revision: 1 Page C-4 of C-7 F0306-O1RO
V9Structural Integrity Associates, Inc.
13 6.66e+00i 2.35Se+/-O1i 14 6.67e+001 2.Se+001 15 6.67e+001 2.35e+/-001 16 6.67e+0O1 2.35e+001 17 6.67e+001 2135e+001 18 6.67e001 -2.36e+001 19 6.67e+001 2;36e4001
'20 6.68e+001 2.36e+001 21 G6.68et010 2.36e+001 22 6.68e+001 2.136e+001 23 6.68e+001 2.36e+601 24,6.68e6001 2.36e+001 25 6.k69e001 2.36e+001 26 '6.69e+001 2.36e+001 27'6.69e+001 2.36e+001 28'6.69e+dO1 2.;36e+001 29 669e+001 2.36e+001 30 6.69e+001-2.36e+001 31 6.70e+001 2.36e+001 32.6.70e+001 2.36e+001 33 6.70e+001 2.366+001 34 6.70e+001 2.37e+001 35 6.70e+001 2'37e0O01 36.6.70e+001 2.37e+001 37 6.71e+001 2.37e+001 38-6.71e+/-001 2.37e&001 39 6,.7le+001 2.37e+001 40 6.71e+001 2.37e+001 41 '6.71e6001 2.37e+.001 42.6.72e+001 2.37e+001 43 6;72e+001 2.37e+001 44 6,.72e+001 2.37e+001 45.6.72e+001 2.37e+001 46 6.72e+001 2.37e+001 47'6.72eP001 2.37e+001 48 6.73e+001 2'37e+001 49 6.73e+001 2.37e+001 50 6.73e+001 2.38e+0O1 51 6.73e+001 2:38e+001 52 6;.73e+001 2.38e+00I 53 6.73e+/-o001 2.38e+001 54 6.74e+001 2.38e+001 55 6.74e+001 2.-38e+001 56 6.74e+001 2.38e+001 57 6.74e+001 2.38e+001 58 6.74e+001 2.38e+QO1 59 6.75e&001 2.38e+001 60 *.75e+001 2.38e+001 61 6.75e+001 -2.38e+001 62 6.75e+001 2.38e+001
- 63 6.75e+001 2.38e+001 64 6.75e6001 2.38e+001 65 6.76e+001 2.:38e+001 66 6.76ei001 2.39e+001 67 6.76e+/-001 2.39e+001 68 6l76e+001 2.39e+00I 69 6.76e+00 2;.39e+001 70 6.77e+001 2.39e+001 71 6.77e+001 2.39e6+01 72 6;77e+001 2.39e+001 73 6.77e+001 2.39e+001 74 6.77e+001 2.39e+001 75 6.77e+001 2.39e+001 PLp4Q. OUT 4.31e&001 0.3'S 7.47e-605 4.31e+/--
0 *.35 7-.47e-005 4.-Je.001 02,35 7'48e-005 4.32e+001 0.35 71.,48e-005 4-32e+001 0.35 7.,49e-005
,4.32e+001 0.35 7.50eS005 4r32e+'001 0.35,7*.50e*005' 4.32e+001 0.3 5 7.51e-005, 4.32e+001 0.35$ 7.52e-005 4.32e+001 0.35 7T.52e-005 4.32eM001 0.35 7.53e-005 4.32e+/-001 0.35 7'.54e-005 4.33e+001 0.35 I7,54e-005 4.33e+001 0:35 7.55e-005 4.33e+001 0.35 7.56e-005 4.33e'001 0.35 7.,56e-005 4.33e+001 0.35 7.57e-005 4.33e+001 0.35 7.57e-005 4.33et00I 0.35 7;58e-O05 4.33e1& 001 0.35 7.59e-005 4.33e4+01 0.35 7.59e-005 4.34.4e+001 0.35 7.'60e-005 4.346001 0.35 7.61e-005 4.34e&001 0.'15 7.61e-00S 4.34e4001 0.35 7.62e-005 4.34e-i001 0.35 7.63e-005 4.34e+/-001 0.35 7--63e-005 4'.346-001 0.35 7.6i4*O05 4.34e6001 0.35 7.65e6-005' 4.35e+001 0.35 7.65e-005 4.35e 6+061 0.35 7Y;66e-005 4.35e+/-001 0.35 7.67e-005 4.35e+001 '0.35 7,.67e-005 4.35e+001 0.35 7..68e-005 4.3r5eO01 0.35 7696ý005 4.35e+/-001 0.35 7.69e-005 4.35e+001 0135 7:.70e-005 4..35e+001 0.35 7..71e-005 4.36e+001 0.35 7.71ie-005 4.36e+001 0.35 7.'72e-00S 4'36e+/-001 0.35 7.73e-005 4-36e&00I 0.35 7'-73e-005 4.36e÷00i 0:35 -7.'74e-005 4.36e+001 0.35 7.75e-005 4.36e+001 0.35 '7.76e -005 4.36e4001 0.35 7,.76e-005 4.'36e+001 0.35 7.77e-005 4.37e+001 0.35 7.78e-005 4.37e+001 0.35 '7T 78e-005 4.37e+/-001 0."35 7'.
79e-005 4.37e÷001 0.35 7.80e-005 4.37e+/-001 0.35 7.80e-005 4.37e6001 0.35 7.481e-005 4.37e+001 0.35 7:82e-005 4.37e+/-01 0.,35 7'.82e-005 4.38e+001 0.35 7.83e-005 4.38e'001 0.35 7.184e-005 438e+001 0.35 7.84e-005 4.36 384001 0.35 7.85e-005 4A.38e+/-00I 0.35 7.786e005 4.386001 oa 3s 7*.8*e-005 4.38e&001 0.35.7.87e-005 4.386+001 0'.35 7.88e-0o5 Page 4 7.46e-OOS' 0.176,0.29 7.476'005 0.1761 0.29 7.48e-005' P.1761. 0.29 7.48e-005ý 0.21762 0.29 7.'49e-005 0.1763 0.29 7.50e-0O5 0.1763 '0.29 7.50e-005. 0.1764 0.29 7.51e0-005: 0.1765 029 7.526-005' 0.1766 0.29 7.526-005' 0.1766 029 7.53e-005 0.1767 0.29 7.54:e-005 0.1768 0.29 7.54e-005 0.1769 0.29 7.,55e-005. 0.1769 0.29 7.56e-005 0'.177 0.30 7.566-005 0.1771 0.30 7.57eQ005 0.1772 0.30 7.57e-o005 0.1772,0.30 7.58e-005 0.1773 0.30 7.59e-005. 0.1774 0.30 7.59e-005 0.1775 0.30 760e-005 0.1775 0.30 761e-005 0.1776 0.30 7.61e-005 0.1777 0.30 7.62e-005 0.1778 0.30 77.63,6-005 0.1779 0.30 7.,63e-005 0.1779 0.30 7.64e-005' 0.178 0.30 7.'65e-005 0:1781 0.30 7.65e-005 0.1782 0.30 7.66e-00OS 0.1782.0.30 7.67e-005O 0.1783 030 7.T67e-005" 0.1784,0.30 7.68e-005 0.1785l0.30 7.69e-005' 0.1785 0.30 7.69e-005 0.1786 0130 7.70e-60S0 0.1787 0.30 7.71e-005 0.1788 0.30 7.71e-005 0.1789 '0.30 7.72e-005' 0.1789 0.30 7'.73e-005 0.179 0.30 7.73e-055 0.1791 030
'7.74e-005 0.1792 9.30 7.75e-005 0.1792 0.30 7.176e-00S 0.1793 0.30 7.76e-005i 0.1794 0.30 7.77e-005 0.1795 -0.30 7.78e-005 0.1795 0.30 7.78e-005' 0.1796 0.30 7.79e-005 0.1797 0.30 7.80e-00S 0.1798 0.30 7T80e-005 0.1799 :0.30 7.'81e-005 0.1799 0.30 7.82e 7005 0.18 0.39 7.82e-o05 0.1801 0.30 7.483e-005. 0.1802 0.30 7.84e-005 0.1803:0.30 7.84e-005 0.1803 0.30 7.85e-005' 0.1804 0.30 7.86e-005 0.1805 0.30 7.87e-005 0.1806, 0.30 7'87e-0051 0.1806,0.30 7.88el00S 0.180710.30 File No.: 0800439.307 Revision: 1 Page C-5 of C-7 F0306-OIRO
V Structural Integrity Associates, Inc.
76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93' 94 95 96 97 98 99.
100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119
.120 121 122 123
.124 125 126 127 128-129 130 131 132
-133 134 135 136 137 138 76 6.78e+001 77 6.78e+001 78 6.78e+001 79 6.78e4-001 80 6.78e+001 81 6.79e+001 82 6.79e+001 83 6. 79e+001 84'6.79e+001 85 6.79e+001 86 65 79e+001 87 6.'80e+001 88.6.80e+001 89 6.80e+001 90 '6.80e+001 91 6.80e+001 92 6.81e+001 93 6.81e+001 94 6.8le+001 95 '6 81e4001 96 6.1e+/-001 97 6.82e+001 98 6'.82e+001 99 6.82e+001 100 6.'82e+001 1016.82e+001 102 6.82e+001 103 6.83e+001 104'6.83e+001 105 6.83e+001 106 6.83e+-001 107 6.83e+00i 108 6. 84eo001 109 6.84e+ooi 11o 6.8464001 111 6.84e+001 112 6.84e+001 113 6.85e+001 114 6.85e+001 115 6.85e+001 116.6 685e+001 117 6.85e+001 118 6.85e+001 119 6.86e+001 120 6.,86e+001 121 6.86e+001 122 6.86e+001 123 6.86e+001 124 6'.87e4001 125 6.87e+001 126 6.87e+001 127 6M87e4001 128 6.87e+001 129 6.88e+001 130 6.88e+001 131 6;88e+001 132 6.88e+001 133 6.88e+001 134 6.89e+001 135 6-89e+001 136 6.89e+001 137 6.89e+001 138 6.89e+001 2..39e+001 2.39e+001 2;39e+/-ooi 2.39e60Ol 2;39e+001 2.39e+001 2.40e+001 2.40e+001 2.40e+,o0 2.40e+001 2.40oe+Oo1 2.40e+001 2.40e400I 2.40e+001 2.40e+001 2.40e+001 2 ;40e+001 2.40e+001 2.40e+001 2.406+001 2.40eý-001 2.41e+001 2.41e+001 2.41e+001
- 2. 41e+001 2.A41i-001 2.41e+001 2,.41e+oo1 2.41e+0O1 2.41e+001 2 ;41e+001 2.416+001 2.'41e+001
- 2. 41e+001 2,41e+001 2.41e+001 2.41e+001 2.42e+001 2.42e401 2.42e+001 2.42e+001 2.,42e+001 2.42e+001 2.42e4001 2.42e+001 2.42e+001 2.42e6001 2.42e+001 2.42e+001
- 2. 42e+001 2.42e+001 2.43e+601 2.43e4001 2.,43e+001 2.43e+ool01 2.43e+001 2.43e+001 2.43e+001 2.43e+001 2.43e+0O01 2.43e+001 2.43e+001 2.43e+0o01 PLPQ. OUT, 4.38e+001 4.39e&001 4.,39e,0oo1 4.,39e&001 4.39e+001 4.39e+001 4,39e+001 4.39e,001
- 4. 39e+OO1 4.40e+001 4.40&,001 4:.40&001 4.40e+001 4.40e+001
- 4. 40e+001 4..40e+001 4.4Oe+Ol 4.41e+001 4.41e4001 4.41e&001 4 A41e+001 4.41ie001 4.41e`001' 442e+001 4.42e:001 4.42e+001 4.42e+001
- 4. 4 2 +.001 4, 42e+001
- 4. 42 e-f-0 4.42e4001 4.42e+001 4.443e+OO
- 4. 41e+001 4.43e-*001 4.43e4001 4.43e+001 4,43e*-0l 4.43e+001 4,.43e+-001 4.43e+00i 4.44e+00i 4.44e4001 4.44e+001 4.44e-4o00 4.44e+001 4.44e+001 4.45e+001 4.454e+ool 4.45e+001 4.45e+001 4.45e+oo1 4.45eo001 445e+001 4.4e6+001 4.46e+/-001 4C.4664-601 C;46e&001 4 '46e.001 Page 5:
0.315 0.35 0.35 0.35 0.35 0.35 0.35
ý0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 035 0.35 0.;35 0.35*
- 0. 35S 0.*35 0.35 0.35 0.35 0.35 0.3,5 0.35 0.35 0.35 0.35 0.35 0.35
- 0. 35 0.35
.0,3S5 0.35 O. 35 0.35 0.35S 0.3.5 0:.35 0.3.5 0.,35 0.35 O.AS 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35
- 0. 35 0.35 0.35 0.35 0.35 7.89e-0O5 7.A9e-00S- 0.1808 0.30 7289e-oo5 7.89e-OO5 0:1809 0.30 7.96e-005 7.96e-005' 0.181 0.30 7.91e-005 7.91e-005 0.181 0.30 7.91e4005 7.91e-00S 0.1811 0.30 7.92e-005 7.92e-005. 0.1812 0.30 7'.93e-005 7.93e-005 0.1813 0.30 7;:94e-005 7.94e-005, 0.1814,0.30
- 7.94e-005 7.94e-005 0.1814 0.30 7'.-95e-005 7.95erO05 0.1815 0.30 7.96e'-05 7;96e-005,0.1816 0.30 7.96e4005 7'96e-005, 0.1817 0.30 7 97e 005 7.97e-005. 0.1818 0.30 7.98e 005 7.98e-005. 0.1818 0.30 7'g99e-O005 7.99e-005 0.1819 0.30 7A99e-005 7.99e-005'.0.182 0.30 8,00e-005 8.90e-Qos 0.1821.'0.30 8Ole-005 8.0le-005 0,1822 0.30 8 02e-005 8&02e-005 0.1822:0.30 8,02e&005 8.02e-005 0.:1823 0.30 8.03e-005 8.03e-005 0.1824 0.30 8.04e-005 8.04e-005 0o1825 0.3o 8i,04e-005 8.04e-005' 0.1826,0.30 8.OSe-005 8.OSe-005 0.1826 0.30 8A06e-005 8.06e-00S 0.1827 0.30 8A07e-005 8. 07e-00s 0.1828 0.30 8.,07e-005 8.107e-00:s 0.1829 0.30 8&08e-005 8.08e&005 0.183,0.30 8.09e-005, 809e-005 0Y183 0.31 8.r1oe-O05 8.l10e-005 0.1831 0.31 8.106-005 8.10e-005 0 1832 0.31, 8l11e-O05. 8.lle-005 0.1833 031 8.12e--05 8.12e-005& 6.1834 0.31 8.12e-005 8.12e-005 0.1834:0.31 8A'136-005 8.13e-005 0.1835 0.31 8 14e-005 8.14e-005 0.1836 0.31.
8.15e-005 8.15e-005 0.1837 0.31 8 15e-005 8.15e-005 0.1838 0.31 8.16e-005 8. 16e-005 0.1839 :0,31 8, 17eý0O5 8.17e-005 0.1839 0.31 8.18e-005 8.'18e-005. 0.184 :0.31 8.18e-005 8.18e-005 0.18410631 8.19e-005 8;l9e-005 0.1842.0.31 8.20e-005 8.20e-005 0.1843 V03.31 8.-2le-005 8.21e-00S 0.1843 0.31 8.21e-005 8.21e-O05 0.1844 0.31 8.22e-005 8.22e-005 0.1845.0.31' 8.,23e-005 8.:23e-005 0.1846 0.31 8.24e-005 8.-24e-005' 0.1847 0.31 8.24e-005 8.24e-005 0.1848 0.31 8.25e-005 8:25e-005 0.1848 0.31 8.126e-005 8.26e-005 0.1849 0.31 8..27e-005 8.27e-005 0.185 0.31 8.27e-005 8.27e-005 0.'1851 0.31 8.28e-005 8.28e-005 0.1852 0.31 8i29e-005 8.29e-005. 0.1853 0;31 8,.30e-005, 8.30e4005 0.1853 0.31 8.'31e-005 8.31e-005. 0.18540.31 8,31e-005 8.31e-005 0:1855 0.31 8.32eOO5 8.32e-0o5 0.1856, 0.31 8.33e-005 8.33e-0o5 0.1857 0.31 8.34e-005 8.34e-005 0.1857-031 8.'34e-Oo5 8.344o00o5 0.1858.0.31 File No.: 0800439.307 Page C-6 of C-7 Revision: 1 F0306-OIRO
V Structural Integrity Associates, Inc.
139 140 141 142.
143 144 145 146 147 148 149 150 151 152.
153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179
'180' 181
'182 183 184 185 186 187 188 189 190.
191 192 193
- 194, 195 196 197 198 199 200 139 6.89e+001 1406.90e+001 141 6.90e+001 142 6.90e+001 143 6.90e+001 144 6.90e+001 145 6.91e+001 146 6.91e+001 147 6.91e+001
'148 6.91e+001 149 6.91e+001 150 6&.92e+601 151 6.92e+001 152 6'.92e+001 153 6.92e+001 154 6.92e+001 155 6.93e+001 156 6.93e+001 157 6.93e+001 158 6.93e+001 159 6.93e+001 160 6.94e+001 161 6.94e+001
'162 6.94e+001 163 6.94e+001
'164 6.94e+001 16556.95e+001 166 6.,95e+001 167 6.95e+001 168 6.95e+001 169.6,.95e+001 170 6.96e+001 171 6.96e+001 172 6.96e+001
'173 6.96e+001 174 6.96e+001 175 6.97e+001 176 6.97e+001 177 6'.'97e&001 178 6.97e+001 179 6..97e+001 180 6.98e+001 181 6.98e+001 182 6.98e+001 183:6'.98e+001 184 6.'98e+001 185 6.99e+001 186 6.996e+001 187 6'. 99e+001 188 6.99e+00I 189 6.99e+001 190 7.00e+001 191 7.00e+001 192 7.00e+001 193 7.0e+001 194 7.00e+001 195 7.01e+001 196 7.01e+001 197 7.01e+001 198 7.01e+001 199,7.Ole+001 200 7.02e+001 PLPBQ. OUT
'2.43e+0O1 4:46e+00I 2.43e+001 4' 46e+001 2.43e+001 4.46e+001 2.44e+0O1 4.47e+001
-2.44e+0O1 4.47e+001 2.44e+001 4.47e+001 2.44e+001 4.47e+001 2.44e+001 4..47e+001 2.44e+001 4.47e+001 2.44e+001 4.47e+001 2.44e+001 4.47e+001 2.44e+001 4..48e+001 2.44e+001 4.48e+001 2.44e+001 4.48e+001 2.44e+00I 4:48e+001 2.44e+001 4.48e+001 2.44e+001 4.48e+001 2.45e+001 4.48e+002 2.45e+001 4.'48e*.001 2.45e+001 4.49e+001 2.45e+001 4.49e+001 2.45e+001 4.49e+001.
2.45e+001 4.,49e+001 2.*5e+001 4.49e&001 2.45e+001 4.49e+001 2.45e+001 4.49e+001 2.45e+001 4.49e+001 2.45e+001 4'50e+001 2.45e+001 4 50e+001 2.45e+001 4.50e+001 2.45e+001 4.50e+001 2.46e+001 4.ý50e+001 2.46e+001 4.5Oe+*O1 2.46e+001 4.50e-,001 2.46e4001 4.50oe+o01
,2.46e+001 4 51e+001 2.46e+O01 4.51e*001 2.46b+001 4.51e+001 2.46e+001 4.51eo001 2'.,46e+001 4.,51e+O01
- 2. 46e001 4.51e+001 2,.46e+o01 4.51e+0ol 2.46e+001 4.52e0o01 2.46eo001 4.52e+001 2.46e+0o1 '4.5,2e 001' 2.47eOb01 4..52e+001 2.47e+001 4;52e+001 2.47e6001 4.52e+001 2.47e+001 4-52e+001 2.47e6001 4.52&+001 247e+*O01 4.53e6001 2.47e+O01 4. 53e001 2.47e+001 4.53e&001 2.47e+001 453e+001 2.47e+001 4.53e+001 2.47e&001 4.53e+001 2.47e+001 4:53e+001 2:47e+001 4.54e4001
- 2. 47e+401 C.54e1401 2,48e+001 4.,54e+001 2.48e+001 4.54e+001 2.486+001 4.54e6001 Page,6 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.`35 0'3 5 0.35' 0.35 0.35 0.35i 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0'. 35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 0.35 06.35 0.35 0.35 0.35
- 0. 3 5 0.35 0'35 0.35 0.35 035
.0.35
.35 0.35 0.35 0.35
.0.35 0.35 0.35 0.35 0.35 0,35 0.35 0.35 0,3.5 0.35 03A5 0.35 8.:35e-005 8.36e-605 8.37e-005 8-.37e-oo5' 8.38e-OO5 8.39e-005 8.40e4005 8.41e-005 8.41e-005 8.,42e-005 8L.-43e-005 8.44e-oo5 8'.45e-605 8.45e-005 8.46e-005.
8.,47e-005,
- 8. 48eo-005 8.49e-005 8.49e-005
- 8. 50e-0051
- 8. 5le-005
- 8. 52e-o05 8.53e-005 8.:53e-005 8.54e-005
- 8. 55se-005
- 8. 56e-005
- 8. 57*-005
- 8. 57e-005
- 8. 58e-005
- 8. 59e-005 8'60e-005 8..61e-005 8.,61e-005 8.62e-005 8.,63e- 005 8.,'64e-005 8.65e-0051 8.66e-005 8.66e-OO5 8 ?67e-005 8'. 68e-&05 8:'69e-005 8.!7e-005 8.:71e-0o51 8.71e-005 8.,72e-005 8.73e-005 8.;74e'005 8.75e-005 8 76e-005 8.76&005' 8 77e-005
- 8. 78e-005 8.79e-005:
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