L-08-349, Calculation for Contingency Flaw Evaluation Support

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Calculation for Contingency Flaw Evaluation Support
ML090330371
Person / Time
Site: Perry FirstEnergy icon.png
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)
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Text

"StructuralIntegrityAssociates, 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 RE FE RE 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 .......................................................................... 9 File No.: 0800439.307 Page 2 of 9 Revision: 1 F0306-011

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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.

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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

3. GE Flaw Inspection Reports. SI File 0800439.215
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 Page 6 of 9 Revision: 1 F0306-011

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Path 1 Axial Stresses (SY)

Z0000.

60000C'

-1C-cc00 2C*C00*

  • Po st-Repair

-i-sm NOPL 0

-ýeMSIPON A

+ PAIP OFF

-20000

-~-oNOP2

-4:cc000

-6 0000

-90000 0.2 0.4 0.6 0.8 1 1.2 14 Distance frowm weld Inner Surface On.)

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 80 100 120 140 160 180 1200 Cycles Figure 3. Crack Growth Through 200 Cycles File No.: 0800439.307 Page 9 of 9 Revision: 1 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 0

degrees FWi830 hours.

2113/1987 CD FCR-06012 BHDN -190( 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 0

1116/1987 CD FCR-08264 BHTN/CRDN .-163( 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-0 1/7/1990' HU FCR-13498 Vessel bulk 106( Fihr) Scram event 01-90-01 temperature 1/311992 HU CR-92-001 Main Steam .175(*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) ýC) "PIF-97-1280 BHDDN .Rw*1 isolation HfU 235(-F/hr) 03/26/93 I=D 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 r I Date Event FCR/CR IMeasurement Rate of Ceoment I Number Location change in 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- ohy end) Cooldown moni tored s V !-B21 -

2/19tr7o-T F T H1176 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

-ahm R C, Ieprtr ret Recirculatno p trensientspipetmprtroa S GI C521 0119eaooctor ~

d5/ Rat9r/01 ?i Fmo ~ '

recircuiolat1 117,6on 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 05/08/01 Cie CD- N/A All components <11O00 (F/hr). '(yclc1 9-3 end) SVI-B2l-TtI.76bre0 t-008724 840dte 05/15/01 Start. R H N/A All'components <100 (FF/hr) (Cyclc.972) SVI-B21-TI 176 order l-011041-000 Up 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~

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TABLE 1 Reactor and Recirculation Pipe Heat-Up, Cool Down and Transient History Date Event, FCRCR . Measurement Rate of Comment Number, location change in

__Stemrperature 0f....... 1A 07-12-01 Loss 17ý701-27f7 13JfrY (C e9ý-4 ipCS 0)(7Tollowig cowri. en a scramtomt ant RCtC. injecting. headdrain 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.) MPG r2 jcu

'It P.1BIMi~ha tI- -,Cf- (rinba -s uprY

,~.dgrnIncaxiwm to,frc, ircukoion pipn&2 VT%

Ltru LoopBl k I-Q0*5n'ith hP76O177 )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 PipeHcat-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 'pterminatedbecauseof.RHR A inoperability

'terminated S'Y,-- B21-TI176 lorder 200099438. Maximum vessel temperature recordixd 145!degmre F.

0 "6/7/03 Staft up RU N/A All.compornents <.100:( F/hr) (Cycle- 0-3) SVI - B21-T11176 /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 0

1/06/05' CD CR054X094 All-compaonents, < I(41 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 1 Start

. ptr U00 lU N/A.

/.

AU compfonents l a oet

<l0(tF/hr) (Cycle, 10-5)SVI -B21-T.1176 /order 200139105.

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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- <12-

<10{'/hr) (Cycle 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 -B1321]-T 1761/order 20(0264161

,5/17/07 Heat, Heat up N/A Allcomponents <.100 (F/hr) (Cycle 12-.2 begin) SVI - B21-T1176'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.trcirculation piping bas.don P1 plot May 8, 2007 1?

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 Page A-7 of A-8 Revision: 1 F0306-O1RO

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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 0

6W29107 133: CD) N/A All Components < 100 ( F/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

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APPENDIX B INSPECTION

SUMMARY

SHEETS FROM [3]

File No.: 0800439.307 Page B-1 of B-1O Revision: 1 F0306-O1RO

t StructuralIntegrity Associates, Inc.

eDRF N6:0000-OO9.1-3569 Rev.IG a HITACHI Austenititc, Piping:

Flaw Evaluation Sheet Project: Perry.Unit 1 I

weldlO: BV:31NbA-KB Indication: 1. Sizing Ddta SheetŽ, /A, Measured Rounded Measured Flaw Through Wall = 0:34 0.35 'T" nominal = 1.20 Flaw Length 1T'= 1:40 1A "r ihnea~ued = 1.20: ;1.2 Surface Separatiorf '"'= 0.21 0.2 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, Alow ed

'10.93i 10.93 19 = ;0:175 a valyu Y!= o.125 Ifa/i> .S.jhen all = .5 V= .0*00 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 X1rounding 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 Page B-2 of B-10 Revision: 1 F0306-OIRO

V StructuralIntegrity 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 Xlroundingperformed 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 Page B-3 of B-10 Revision: 1 F0306-OIRO

V StructuralIntegrity 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 1.80 16"= 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 minal n 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 11.86.

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 X1rounding 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 '23 7,0 f 30'3'.

File No.: 0800439.307 Page B-4 of B-10 Revision: 1 F0306-O1RO

~Structural IntegrityAssociates, 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 Qr80 . ~ 'T mnea sured= 12, 2 Surfoce'Sepaortion"S- 0,75 0.75 ASME"SectionXl, 1989 Edition. NoAddenda TABLE IWB-3514,2 Austenitic Steels.i2ZInch 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

-0/1volue '0.031 Y= ,1.0bo Flow isSu6surfoce

  • 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 Page B-5 of B-10 Revision: 1 F0306-O1RO

V StructuralIntegrity Associates, Inc.

eDRF No 0000 0091'3569R6v.I0; SHITACHI :Austienhitid Piping, Flaw Eval1uatioln !heet Project: Perry.Unit 1 Weld ID: 1B13-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 Date: 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 StructuralIntegrityAssociates, 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 Xlfounding 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 Page B-7 of B-10 Revision: I F0306-01RO

V StructuralIntegrityAssociates, 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 2nchk 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 XIrounding performed inaccordance with IWA-3200 and ASTM E29.

Iridiiati6h iscircumferential 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 StructuralIntegrity Associates, Inc.

6DRF N6. 000M6091-3569 Rev:'0, 0 1 HITACHI Austenitic Piping Flaw EvalUation Sheet Rev:'i0 No',0000:0091-3569 6DRF Project.: Periy.Unit 1 Weld ID; -lB13-N6C-KB ExoaDdto Sheet '1Q800.-01-027 indication i '4 Sizii. Data Sheet,'. N/A' Measured Rounded Mea sured Rounded Flow Through Wa!l = .0:24 025 'T'nominal 1 o20 1.2 Flow Length 2.00 '.0 7t'"meoured= i .2b 1.2 Surface Sepomtion "S"-- 0.48 0.5 ASýE SectioriXi, 1989 Edition, NoAddenda TABLE IWB -3514-2 AusterticSteeIs.2~In~chNomi*nal'Thickness,,Ihservice, 0ll Surfa6e% 'Subdff6ce/% S surface 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 Flbw, is Sub surface, Allowedidt-= i0.7%'

a/t= 10.;%.

Flaw is acceptable by TabIe IWB-351*-2.

Comments: ASME Section XIrounding~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 Da te: 09,23-2008 Level: _Dote:,.

P.,e27>t'28&

Page:283_of.303 File No.: 0800439.307 File No.: 0800439.307 Page B-9 of B-10 Revision: 1 F0306-O1RO

V StructuralIntegrity Associates, Inc.

eDRF Nd'.0000!0091'3569 Rev.0' Austenitic Piping 1HITACHI Flaw Evaluation Sheet SPrbjact: Perf9Unitl Weld ID;: '1B13-N6C-KB Exbam Ddto' Sheet: *IQ800-01-027 Indication," 5 .Siziri D*,to Sheet: N/A

.Mesured Rouncýd Flow Through Wqll= 0.23 0325 "77nomindl = 120 1.2 Flow.LengOth '= 1.80 ,T'measured= 12 '12 Surface Separation !'S"= 0:.37 0ý35 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.

-lw is located at.31,9" CW from TDC,,0.1" U stre-am from Weld Centerline (SafeI'End Side)'

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 Page B-10 of B-1O Revision: 1 F0306-O1RO

StructuralIntegrity Associates, Inc.

APPENDIX C PC-CRACK OUTPUT File No.: 0800439.307 Page C-1 of C-7 Revision: 1 F0306-O1RO

StructuralIntegrityAssociates, 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:

stress Coefficients Case ID co Cl C2 C3 Type Unit Membrane 10 '0 0 Coeff 20 0 0 ,0 Coeff Residual consta Through------

wall stresses for Load cases with stress coeff "

Wall Case Case Depth Unit Meihbr 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.

SStress 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 Page C-2 of C-7 Revision: 1 F0306-OIRO

V StructuralIntegrityAssociates, Inc.

PLPBQ. OUT:

0. 0180' 2.37926 4.75853,

.5.49695.

0.0240 2.74848 6. 14906 0.0300 3.07453

0. 0360 3.37o18 6.74036 0.0426 3 64303 7.:28605 0.0480 3.89804 7.79608
0. 0540Q 4.13869 '8. 27738 0.0600 4.36752 8.7,35,03 0.0660 4.58645 9.17291 0.0720 4.79701 9. 59403 0.0780 5,00041 10.0008 0.0840 5.19763 10.3953
0. 0900 5.38951 10. 779 1 153 5
  • 1.
0. 0960 5.,57675
0. 1020 5.75995 11.5199 0.1080 5.93964 11. 87931 0,1140 6.11628 :12.2326

.0.1200 6.29028 12.5806 0.1260! 6.462 12.924:

0. 1320 6.63178 13.2636
o. 1380 6.79992 13. 5998 0.1440 6.96671 '13.9334
0. 1500 7.1324 14.2648
0. 1560. 7. 29724 14.. 5945'
0. 1620, 7.46146 14.9229 0.1680' 7.62527 15ý.'2505 0.1740 7.78889 15. 5778 0.1800 7..95251 15.9051 0.1860 8.11632 '16. 2326 0.1920 8.28053 16.5611
0. 1980 8.44531 16.8906

,0. 2040. 8'. 61084- 17.-2217, 0.2100 8.77732 8.9449 17.5546

0. 2160 17.8898 0.2220 9.11379 18'.2276 0.2280 9.,28416 :18: 5683
0. 2340 9.:4562 18.91224 0.2400 9,'63009 19.2602 19.6121
0. 2460' 9.80602 0.2520 '9.9842 19.,9684 0.2580 10. 1648 20.3296 0.2640 10.3481. 20.6962 0.2700 10.5342 21.0684 0.2760 10. 7235 21.,4469 2:1.832:

0.2820 10.916.

0. 2'880 11. 1121 22.2242 0.2940 11. 3121 22.,62041
0. 3000 11.:5161 *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.

where s = 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 StructuralIntegrityAssociates, 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 Cycl'es Calc. Print Crk. Grw. Mat.

Subblock /Time incre. incre. Law' KiC perryl 200 1 1 Sect XIAus Air -Alloy 182, Keax , Kmin

  • casel,3:D Scal e *F actor Subblock case ioscale Factor Perryl Residual constant 1.5000 5.5o00 Residual constant 1.s0OO unit Memnbrane crack growth results:

Total Subblock Cycles cycles Ddnn a/thk

./Time Kinax l0ni n .Deltal( R /D-aDt Da ,a a/Time Block: 1 1

2. I 6'.64e+001 2 34e+001 4.3 de001 0.35 1.39e-00O :7.39e-0o5! b.1751 0V29 2 6.65e+001 2*35e+001 4.30e+001 '0.35 7-.39e-005 7.'39e-005 0.:1751 0.29 3 3 6.65e+001 2.35e+001 .4.30eL001 0.35 7,40e-005 7.40e-005 0.'1752 0.29 4 4 &6;65e+0012.35e+001 4.J30e+001 0.35 7.41e-005 7.,41e- o05. 0.17.53 .0.29 5 5 6-.65e+001 2 35e001 '4.30e+001 0.35 7.41e-005 7.41e-005, 0.1754.,0.29 6 6 6.65e+*O01 235e+001 '4.30e+001 0.35 7.42e-005 7.,42e-O05 0.'1754,0.29 7 7 6.65e+001 2.35e+001 4.31e+001 0.35 7.43e-005 7.ý43e-005 0.1755 0.29 8 .8 6.66i+001 2.35e+001 4.316-O01 0.35 7.ý43e-005 7.43i-005 0*1756. 0.29 9 9. 6,.66e+001 2:.35e401 ý4.J31ie+0 0.35 7.44e-o05 7.44b-005 0.17,57 ý0.29 10 10 11 6&66e+001 2.35e-+001 4.31e06i 0:35 7.45-6005 7.45e-oo5' 0.1757 '0.29 12 6.66e+001 2.35e+001 4.31e&001 0.35 7.,45e-005 7A45e-005 0.1758 0.29
12. .12 6.66e+001 2.35e+001 4.31e+001 0:35 7146e-005 7.46&- 005 0.1759 0.29 Page 3 File No.: 0800439.307 Page C-4 of C-7 Revision: 1 F0306-O1RO

V9StructuralIntegrityAssociates, Inc.

PLp4Q. OUT 13 6.66e+00i 2.35Se+/-O1i 4.31e&001 0.3'S 7.47e-605 7.46e-OOS' 0.176,0.29 14 6.67e+001 2.Se+001 4.31e+/-- 0.35

  • 7-.47e-005 7.476'005 0.1761 0.29 15 6.67e+001 2.35e+/-001 4.-Je.001 02,35 7'48e-005 7.48e-005' P.1761. 0.29 16 6.67e+0O1 2.35e+001 4.32e+001 0.35 71.,48e-005 7.48e-005ý 0.21762 0.29 17 6.67e+001 2135e+001 4-32e+001 0.35 7.,49e-005 7.'49e-005 0.1763 0.29 18 6.67e001 -2.36e+001 ,4.32e+001 4r32e+'001 0.35 7.50eS005 0.35,7*.50e*005' 7.50e-0O5 0.1763 '0.29 19 6.67e+001 2;36e4001 7.50e-005. 0.1764 0.29

'20 6.68e+001 2.36e+001 4.32e+001 0.3 5 7.51e-005, 7.51e0-005: 0.1765 029 21 G6.68et010 2.36e+001 4.32e+001 0.35$ 7.52e-005 7.526-005' 0.1766 0.29 22 6.68e+001 2.136e+001 4.32e+001 0.35 7T.52e-005 7.526-005' 0.1766 029 23 6.68e+001 2.36e+601 4.32eM001 0.35 7.53e-005 7.53e-005 0.1767 0.29 24 ,6.68e6001 2.36e+001 4.32e+/-001 0.35 7'.54e-005 7.54:e-005 0.1768 0.29 25 6.k69e001 2.36e+001 4.33e+001 0.35 I7,54e-005 7.54e-005 0.1769 0.29 26 '6.69e+001 2.36e+001 4.33e+001 0:35 7.55e-005 7.,55e-005. 0.1769 0.29 27'6.69e+001 2.36e+001 4.33e+001 0.35 7.56e-005 7.56e-005 0'.177 0.30 28'6.69e+dO1 2.;36e+001 4.33e'001 0.35 7.,56e-005 7.566-005 0.1771 0.30 29 669e+001 2.36e+001 4.33e+001 0.35 7.57e-005 7.57eQ005 0.1772 0.30 30 6.69e+001-2.36e+001 4.33e+001 0.35 7.57e-005 7.57e-o005 0.1772,0.30 31 6.70e+001 2.36e+001 4.33et00I 0.35 7;58e-O05 7.58e-005 0.1773 0.30 32 .6.70e+001 2.36e+001 4.33e1& 001 0.35 7.59e-005 7.59e-005. 0.1774 0.30 33 6.70e+001 2.366+001 4.33e4+01 0.35 7.59e-005 7.59e-005 0.1775 0.30 34 6.70e+001 2.37e+001 4.34.4e+001 0.35 7.'60e-005 760e-005 0.1775 0.30 35 6.70e+001 2'37e0O01 4.346001 0.35 7.61e-005 761e-005 0.1776 0.30 36.6.70e+001 2.37e+001 4.34e&001 0.'15 7.61e-00S 7.61e-005 0.1777 0.30 37 6.71e+001 2.37e+001 4.34e4001 0.35 7.62e-005 7.62e-005 0.1778 0.30 38-6.71e+/-001 2.37e&001 4.34e-i001 0.35 7.63e-005 77.63,6-005 0.1779 0.30 39 6,.7le+001 2.37e+001 4.34e+/-001 0.35 7--63e-005 7.,63e-005 0.1779 0.30 40 6.71e+001 2.37e+001 4'.346-001 0.35 7.6i4*O05 7.64e-005' 0.178 0.30 41 '6.71e6001 2.37e+.001 4.34e6001 0.35 7.65e6-005' 7.'65e-005 0:1781 0.30 42.6.72e+001 2.37e+001 4.35e+001 0.35 7.65e-005 7.65e-005 0.1782 0.30 43 6;72e+001 2.37e+001 4.35e6+061 0.35 7Y;66e-005 7.66e-00OS 0.1782 .0.30 44 6,.72e+001 2.37e+001 4.35e+/-001 0.35 7.67e-005 7.67e-005O 0.1783 030 45.6.72e+001 2.37e+001 4.35e+001 '0.35 7,.67e-005 7.T67e-005" 0.1784,0.30 46 6.72e+001 2.37e+001 4.35e+001 0.35 7..68e-005 7.68e-005 0.1785l0.30 47'6.72eP001 2.37e+001 4.3r5eO01 0.35 7696ý005 7.69e-005' 0.1785 0.30 48 6.73e+001 2'37e+001 4.35e+/-001 0.35 7.69e-005 7.69e-005 0.1786 0130 49 6.73e+001 2.37e+001 4.35e+001 0135 7:.70e-005 7.70e-60S0 0.1787 0.30 50 6.73e+001 2.38e+0O1 4..35e+001 0.35 7..71e-005 7.71e-005 0.1788 0.30 51 6.73e+001 2:38e+001 4.36e+001 0.35 7.71ie-005 7.71e-005 0.1789 '0.30 52 6;.73e+001 2.38e+00I 4.36e+001 0.35 7.'72e-00S 7.72e-005' 0.1789 0.30 53 6.73e+/-o001 2.38e+001 4'36e+/-001 0.35 7.73e-005 7'.73e-005 0.179 0.30 54 6.74e+001 2.38e+001 4-36e&00I 0.35 7'-73e-005 7.73e-055 0.1791 030 55 6.74e+001 2.-38e+001 4.36e÷00i 0:35 -7.'74e-005 '7.74e-005 0.1792 9.30 56 6.74e+001 2.38e+001 4.36e+001 0.35 7.75e-005 7.75e-005 0.1792 0.30 57 6.74e+001 2.38e+001 4.36e+001 0.35 '7.76e -005 7.176e-00S 0.1793 0.30 58 6.74e+001 2.38e+QO1 4.36e4001 0.35 7,.76e-005 7.76e-005i 0.1794 0.30 59 6.75e&001 2.38e+001 4.'36e+001 0.35 7.77e-005 7.77e-005 0.1795 -0.30 60 *.75e+001 2.38e+001 4.37e+001 0.35 7.78e-005 7.78e-005 0.1795 0.30 61 6.75e+001 -2.38e+001 4.37e+001 0.35 '7T 78e-005 7.78e-005' 0.1796 0.30 62 6.75e+001 2.38e+001 4.37e+/-001 0."35 7'.79e-005 7.79e-005 0.1797 0.30

  • 63 6.75e+001 2.38e+001 4.37e÷001 0.35 7.80e-005 7.80e-00S 0.1798 0.30 64 6.75e6001 2.38e+001 4.37e+/-001 0.35 7.80e-005 7T80e-005 0.1799 :0.30 65 6.76e+001 2.:38e+001 4.37e6001 0.35 7.481e-005 7.'81e-005 0.1799 0.30 66 6.76ei001 2.39e+001 4.37e+001 0.35 7:82e-005 7.82e 7 005 0.18 0.39 67 6.76e+/-001 2.39e+001 4.37e+/-01 0.,35 7'.82e-005 7.82e-o05 0.1801 0.30 68 6l76e+001 2.39e+00I 4.38e+001 0.35 7.83e-005 7.483e-005. 0.1802 0.30 69 6.76e+00 2;.39e+001 4.38e'001 0.35 7.184e-005 7.84e-005 0.1803:0.30 70 6.77e+001 2.39e+001 438e+001 0.35 7.84e-005 7.84e-005 0.1803 0.30 71 6.77e+001 2.39e6+01 4.36 384001 0.35 7 .85e-005 7.85e-005' 0.1804 0.30 72 6;77e+001 2.39e+001 4A.38e+/-00I 0.35 7.786e005 7.86e-005 0.1805 0.30 73 6.77e+001 2.39e+001 4.386001 oa 3s 7*.8*e-005 7.87e-005 0.1806, 0.30 74 6.77e+001 2.39e+001 4.38e&001 0.35 .7.87e-005 7'87e-0051 0.1806,0.30 75 6.77e+001 2.39e+001 4.386+001 0'.35 7.88e-0o5 7.88el00S 0.180710.30 Page 4 File No.: 0800439.307 Page C-5 of C-7 Revision: 1 F0306-OIRO

V StructuralIntegrityAssociates, Inc.

PLPQ. OUT, 76 76 6.78e+001 2..39e+001 4.38e+001 0.315 7.89e-0O5 7.A9e-00S- 0.1808 0.30 77 77 6.78e+001 2.39e+001 2;39e+/-ooi 4.39e&001 0.35 7289e-oo5 7.89e-OO5 0:1809 0.30 78 78 6.78e+001 4.,39e,0oo1 0.35 7.96e-005 7.96e-005' 0.181 0.30 79 79 6.78e4-001 2.39e60Ol 4.,39e&001 0.35 7.91e-005 7.91e-005 0.181 0.30 80 80 6.78e+001 2;39e+001 4.39e+001 0.35 7.91e4005 7.91e-00S 0.1811 0.30 81 81 6.79e+001 2.39e+001 4.39e+001 0.35 7.92e-005 7.92e-005. 0.1812 0.30 82 82 6.79e+001 2.40e+001 4,39e+001 0.35 7'.93e-005 7.93e-005 0.1813 0.30 83 83 6. 79e+001 2.40e+001 4.39e,001 7;:94e-005 7.94e-005, 0.1814,0.30 84 84'6.79e+001 2.40e+,o0 4. 39e+OO1 :7.94e-005 7.94e-005 0.1814 0.30 85 85 6.79e+001 2.40e+001 4.40e+001 ý0.35 0.35 7'.-95e-005 7.95erO05 0.1815 0.30 86 86 6579e+001 2.40oe+Oo1 4.40&,001 0.35 7.96e'-05 7;96e-005,0.1816 0.30 87 87 6.'80e+001 2.40e+001 4:.40&001 0.35 0.35 7.96e4005 7'96e-005, 0.1817 0.30 88 88.6.80e+001 2.40e400I 4.40e+001 0.35 7 97e 005 7.97e-005. 0.1818 0.30 89 89 6.80e+001 2.40e+001 4.40e+001 0.35 7.98e 005 7.98e-005. 0.1818 0.30 90 90 '6.80e+001 2.40e+001 4. 40e+001 0.35 7'g99e-O005 7.99e-005 0.1819 0.30 91 91 6.80e+001 2.40e+001 4..40e+001 035 7A99e-005 7.99e-005' .0.182 0.30 92 92 6.81e+001 ;40e+001 22.40e+001 4.4Oe+Ol 0.35 8,00e-005 8.90e-Qos 0.1821.'0.30 93' 93 6.81e+001 2.40e+001 4.41e+001 8Ole-005 8.0le-005 0,1822 0.30 94 94 6.8le+001 2.406+001 4.41e4001 0.;35 8 02e-005 8&02e-005 0.1822:0.30 95 95 '6 81e4001 2.40eý-001 4.41e&001 0.35* 8,02e&005 8.02e-005 0.:1823 0.30 96 96 6.1e+/-001 2.41e+001 4 A41e+001 0. 35S 8.03e-005 8.03e-005 0.1824 0.30 97 97 6.82e+001 2.41e+001 4.41ie001 0.*35 8.04e-005 8.04e-005 0o1825 0.3o 98 98 6'.82e+001 2.41e+001 0.35 8i,04e-005 8.04e-005' 0.1826,0.30

99. 99 6.82e+001 2. 41e+001 8.OSe-005 8.OSe-005 0.1826 0.30 100 100 6.'82e+001 4.41e`001' 0.35 8A06e-005 8.06e-00S 0.1827 0.30 2.A41i-001 442e+001 0.35 8A07e-005 8. 07e-00s 0.1828 0.30 101 1016.82e+001 2.41e+001 102 102 6.82e+001 2,.41e+oo1 4.42e:001 8.,07e-005 8.107e-00:s 0.1829 0.30 103 103 6.83e+001 2.41e+0O1 4.42e+001 0.35 8&08e-005 8.08e&005 0.183,0.30 104 104'6.83e+001 2.41e+001 4 .42e+001 0.3,5 8.09e-005, 809e-005 0Y183 0.31 105 105 6.83e+001 4.

4, 4 2 +.001 0.35 8.r1oe-O05 42e+001 8.l10e-005 0.1831 0.31 2 ;41e+001

2. 41e+001 4.42e4001 0.35 8.106-005 8.10e-005 0 1832 0.31, 106 106 6.83e+-001 2.416+001 4. 42 e-f-0 0.35 8l11e-O05.

107 107 6.83e+00i 2 .'41e+001 4.42e+001 8.lle-005 0.1833 031 108 108 6. 84eo001 2,41e+001 0.35 8.12e--05 8.12e-005&6.1834 0.31 109 109 6.84e+ooi 2.41e+001 4.443e+OO 0.35 8.12e-005 8.12e-005 0.1834:0.31 8.13e-005 0.1835 0.31 110 111 11o 6.8464001 111 6.84e+001 2.41e+001 2.42e+001 4.43e-*001

4. 41e+001 .0,3S58A'136-005 4.43e4001 0.35 8 14e-005 8.14e-005 0.1836 0.31.
0. 35 8.15e-005 0.1837 0.31 112 112 6.84e+001 2.42e401 4.43e+001 0.35 8.15e-005 113 113 6.85e+001 2 .42e+001 4,43e*-0l 0.35S8 15e-005 8.15e-005 0.1838 0.31 114 114 6.85e+001 2.42e+001 4.43e+001 0.35 8.16e-005 8. 16e-005 0.1839 :0,31 115 115 6.85e+001 4,.43e+-001 O. 35 8, 17eý0O5 8.17e-005 0.1839 0.31 116 116.6685e+001 2.,42e+001 4.43e+00i 0.35 8.18e-005 8.'18e-005 . 0.184 :0.31 117 117 6.85e+001 2.42e+001 4.44e+00i 0.3.5 8.18e-005 8.18e-005 0.18410631 118 118 6.85e+001 2.42e4001 4.44e4001 0:.35 8.19e-005 8;l9e-005 0.1842.0.31 119 119 6.86e+001 2 .42e+001 4.44e+001 0.3.5 8.20e-005 8.20e-005 0.1843 V03.31

.120 120 6.,86e+001 2.42e+001 8.-2le-005 8.21e-00S 0.1843 0.31 0.,35 8.21e-O05 0.1844 0.31 121 121 6.86e+001 2.42e6001 4.44e-4o00 0.35 8.21e-005 122 122 6.86e+001 2.42e+001 O.AS 8.22e-005 8.22e-005 0.1845 .0.31' 123 123 6.86e+001 2.42e+001 4.44e+001 0.35 8.,23e-005 8.:23e-005 0.1846 0.31

.124 124 6'.87e4001 2. 42e+001 4.44e+001 8.24e-005 8.-24e-005' 0.1847 0.31 0.35 8.24e-005 0.1848 0.31 125 125 6.87e+001 2.42e+001 4.45e+001 0.35 8.24e-005 126 126 6.87e+001 2.43e+601 8.25e-005 8:25e-005 0.1848 0.31 127 127 6M87e4001 2.43e4001 4.454e+ool 0.35 8.126e-005 8.26e-005 0.1849 0.31 0.35 8.27e-005 0.185 0.31 128- 128 6.87e+001 2.,43e+001 4.45e+001 0.35 8..27e-005 129 129 6.88e+001 2.43e+ool01 4.45e+001 8.27e-005 8.27e-005 0.'1851 0.31 0.35 8.28e-005 0.1852 0.31 130 130 6.88e+001 2.43e+001 4.45e+oo1 0.35 8.28e-005 131 131 6;88e+001 2.43e+001 4.45eo001 0.35 8i29e-005 8.29e-005. 0.1853 0;31 132 132 6.88e+001 2.43e+001 445e+001 0.35 8,.30e-005, 8.30e4005 0.1853 0.31

-133 133 6.88e+001 2.43e+001 4.4e6+001 0. 35 8.'31e-005 8.31e-005. 0.18540.31 134 134 6.89e+001 2.43e+0O01 0.35 8,31e-005 8.31e-005 0:1855 0.31 135 135 6-89e+001 2.43e+001 4.46e+/-001 0.35 8.32eOO5 8.32e-0o5 0.1856, 0.31 4C.4664-601 8.33e-0o5 0.1857 0.31 136 136 6.89e+001 2.43e+001 0.35 8.33e-005 137 137 6.89e+001 2.43e+0o01 C;46e&001 8.34e-005 8.34e-005 0.1857-031 138 138 6.89e+001 4 '46e.001 8.'34e-Oo5 8.344o00o5 0.1858 .0.31 Page 5:

File No.: 0800439.307 Page C-6 of C-7 Revision: 1 F0306-OIRO

V StructuralIntegrity Associates, Inc.

PLPBQ. OUT 139 139 6.89e+001 '2.43e+0O1 4:46e+00I 0.35 8.:35e-005 8.,35e-005' 0.1859 0.31 140 1406.90e+001 2.43e+001 4' 46e+001 0.35 8.36e-605 8.36e-005 '0.186:031 141 141 6.90e+001 2.43e+001 4.46e+001 0.35 8.37e-005 8.37e"005 0.1861 0.31 142. 142 6.90e+001 2.44e+0O1 4.47e+001 0.35 8-.37e-oo5' 8.'37e-,005 0.1862 0.31 143 143 6.90e+001 -2.44e+0O1 4.47e+001 0.35 8.38e-OO5 8.38e-005- 0.1863 0.31 144 144 6.90e+001 2.44e+001 4.47e+001 0.35 8.39e-005 8.39e-005, 0.1863 0.31 145 145 6.91e+001 2.44e+001 4.47e+001 0.35 8.40e4005 8.'40e.-005 0.1864 0.31 146 146 6.91e+001 2.44e+001 4..47e+001 0.`35 8.41e-005 8.41e-005: 01865 :0.31 147 147 6.91e+001 2.44e+001 4.47e+001 0'3 5 8.41e-005 8.41e-005 0.1866 0. 31 148 '148 6.91e+001 2.44e+001 4.47e+001 0.35' 8.,42e-005 8.42e-O05 0.1867 0.31 149 149 6.91e+001 2.44e+001 4.47e+001 0.35 8L.-43e-005 8.43e-005, 0.1868 *0:31 150 150 6&.92e+601 2.44e+001 4..48e+001 0.35 8.44e-oo5 8.'44e-005 0.1868 0.31 151 151 6.92e+001 2.44e+001 4.48e+001 0.35i 8'.45e-605 8.45e-oo5. 0-1869 0'31 152. 152 6'.92e+001 2.44e+001 4.48e+001 0.35 8.45e-005 8.45e-005 60.187 0.31 153 153 6.92e+001 2.44e+00I 4:48e+001 0.35 8.46e-005. 8.46e-005w 0.1871 0.,31 154 154 6.92e+001 2.44e+001 4.48e+001 0.35 8.,47e-005, 8A47e-005 0.1872 ;0..31 155 155 6.93e+001 2.44e+001 4.48e+001 0.35 8. 48eo-005 8.48e-005 0.1873 :0.31 156 156 6.93e+001 2.45e+001 4.48e+002 0.35 8.49e-005 8.49e-005 0.1873:0.31 157 157 6.93e+001 2.45e+001 4.'48e*.001 0.35 8.49e-005 8.49e-00S- 0;1874 0.31 158 158 6.93e+001 2.45e+001 4.49e+001 0.35 8. 50e-0051 8.'50e-OOS 0.18750 '31 159 159 6.93e+001 2.45e+001 4.49e+001 0.35 8. 5le-005 8.5,le-005 0.1876 0Q.31' 160 160 6.94e+001 2.45e+001 4.49e+001. 0.35 8. 52e-o05 8.52e-005 0.1877 0.31 161 161 6.94e+001 2.45e+001 4.,49e+001 0.35 8.53e-005 8..53e-005 0.1878 0.31 162 '162 6.94e+001 2.*5e+001 4.49e&001 0.35 8.:53e-005 8.53e6005 0.1879 0.31 163 163 6.94e+001 2.45e+001 4.49e+001 0'. 35 8.54e-005 8.54e-.005 0.1879 A031 164 '164 6.94e+001 2.45e+001 4.49e+001 0.35 8. 55se-005 8.55e-*oS 0.188 0. 31 165 16556.95e+001 2.45e+001 4.49e+001 0.35 8. 56e-005 8.56e-005 0.1881 0.31 166 166 6.,95e+001 2.45e+001 4'50e+001 0.35 8. 57*-005 8.5744005 0.1882 .0.31 167 167 6.95e+001 2.45e+001 4 50e+001 0.35 8. 57e-005 8;57e-005 0.1883 0*31 168 168 6.95e+001 2.45e+001 4.50e+001 0.35 8. 58e-005 8.58e-005. 0.18.84 0.31 169 169.6,.95e+001 2.45e+001 4.50e+001 0.35 8. 59e-005 8.59e-005; 01885 0.31 170 170 6.96e+001 2.46e+001 4.ý50e+001 0.35 8'60e-005 8660e-005 0.1885 .0.31 171 171 6.96e+001 2.46e+001 4.5Oe+*O1 0.35 8..61e-005 8.61e-005 0.1886 0.31.

172 172 6.96e+001 2.46e+001 4.50e-,001 0.35 8.,61e-005 8.61e-005 0.1887 0.31 173 '173 6.96e+001 2.46e4001 4.50oe+o01 06.35 8.62e-005 8.:62e005 0.1888 :031 174 174 6.96e+001 ,2.46e+001 4 51e+001 0.35 8.,63e- 005 8&63e-005 0.1889 '0.31 175 175 6.97e+001 2.46e+O01 4.51e*001 0.35 8.,'64e-005 8.'646-005 '0.189 "0r.31 176 176 6.97e+001 2.46b+001 4.51e+001 0.35 8.65e-0051 8.65e-005 0.1891 0.32 177 177 6'.'97e&001 2.46e+001 4.51eo001 35 8.66e-005 8.ý66e-00S 0.1891 0.32 0.

" 8.66e-OO5 8,66e-00S! 0.1892 0.32 178 178 6.97e+001 2'.,46e+001 4.,51e+O01 0.35 179 179 6..97e+001 2. 46e001 4.51e+001 0'35 8 ?67e-005 8;67eOOS 0.1893:0.32

'180' 180 6.98e+001 2,.46e+o01 4.51e+0ol 0.35 8'. 68e-&05 8.68e&005. 0.1894 0.32 181 181 6.98e+001 2.46e+001 4.52e0o01 0.35 8:'69e-005 8.69e-005 0.1895 0.32

'182 182 6.98e+001 2.46eo001 4.52e+001 035 8.!7e-005 8.7oe005' 0;1896 0.32 183 183:6'.98e+001 2.46e+0o1 '4.5,2e 001' .0.35 8.:71e-0o51 8.71e-005 0.1897 032 184 184 6.'98e+001 2.47eOb01 4..52e+001 .35 8.71e-005 8.71e-00S 0.1898 0.32 185 185 6.99e+001 2.47e+001 4;52e+001 0.35 8.,72e-005 8.72e-OOS 0 1898 L0.32 186 186 6.996e+001 2.47e6001 4.52e+001 0.35 8.73e-005 8.73e-005 0.1899 "0;*32 187 187 6'. 99e+001 2.47e+001 4-52e+001 0.35 8.;74e'005 8.74e-005, 0.19 -0'32 188 188 6.99e+00I 2.47e6001 4.52&+001 .0.35 8.75e-005 8.75e6005 0.'1901:0.32 189 189 6.99e+001 247e+*O01 4.53e6001 0.35 8 76e-005 8. 76e-005 01.902 0.32 190. 190 7.00e+001 2.47e+O01 4. 53e001 0.35 8.76&005' 8.,66e-005 0.1903 0*32 191 191 7.00e+001 2.47e+001 4.53e&001 0.35 8 77e-005 8. 77e-005' 0-1904 0.32 192 192 7.00e+001 2.47e+001 453e+001 0.35 8. 78e-005 8.78e-005 0.1905 0.32 193 193 7.0e+001 2.47e+001 4.53e+001 0,35 8.79e-005: 8.z9e-O05 0.r1905 D.032 194, 194 7.00e+001 2.47e&001 4.53e+001 0.35 8&80e-005 8&80e-005' 0.1906'0.32 195 195 7.01e+001 2.47e+001 4:53e+001 t. 81e-OO5 8 81e-005 0.1907 0"32 196 196 7.01e+001 2:47e+001 4.54e4001 0.35 8.81e-005 8 81e-005 0.1908 0.32 197 197 7.01e+001 2. 47e+401 C.54e1401 0,3.5 8.82e-o05 8,82e-005 0.1909 0.32 198 198 7.01e+001 2,48e+001 4.,54e+001 0.35 8 83e-OO5 8&83e-005 0.191 .0.32 199 199,7.Ole+001 2.48e+001 4.54e+001 03A5 8.84e-005 8.84e-o05 0.1911 0.32 200 200 7.02e+001 2.486+001 4.54e6001 0.35 8 85e-005 8.85e-005' 0.1912 .0 32 Page ,6 File No.: 0800439.307 Page C-7 of C-7 Revision: 1 F0306-O1RO

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