NRC 2003-0095, To Fracture Mechanics Evaluation of Point Unit 2 Top Head CRDM 43.5 Degree Azimuth Penetration Weld Repair
| ML032940314 | |
| Person / Time | |
|---|---|
| Site: | Point Beach  |
| Issue date: | 10/04/2003 |
| From: | Fujikawa K, Gustin H, Limpus C Structural Integrity Associates |
| To: | Document Control Desk, Office of Nuclear Reactor Regulation |
| References | |
| NRC 2003-0095 PBCH-70Q-301 | |
| Download: ML032940314 (43) | |
Text
I FILE No.: PBCH-07Q-301 rX STRUCTURAL CALCULATION INTEGRITY PACKAGE PROJECT No.: PBCH-07Q Associates, Inc.
PROJECT NAME: Point Beach Unit 2 CRDM Top Head Analysis CLIENT: Nuclear Management Company, LLC (Point Beach U2)
CALCULATION TITLE: Fracture Mechanics Evaluation of Point Beach Unit 2 Top Head CRDM 43.5 Degree Azimuth Penetration Weld Repair Project Mgr.
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1-18 Initial Issue H. L. Gustin C. R. Limpus Al -A2)kz 49 Project K. K. Fujikawa Computer Files Page 1 of 18 F200IR1
Table of Contents
1.0 INTRODUCTION
3 2.0 METHODOLOGY..
3...................
3.0 ASSUMPTIONS........................
3 4.0 ANALYSIS........................
3 4.1 Finite Element Model........................
4 4.2 Loads and Boundary Conditions........................
5 4.2.1 Loads 4.2.2 Boundary Conditions 6
5.0 RESULTS OF ANALYSIS.14
6.0 REFERENCES
.18 APPENDIX A FILE LISTING Al List of Tables Table 5-1: Stress Intensity Factor Results (psi-4 in).15 List of Figures Figure 4-1:
Figure 4-2:
Figure 4-3:
Figure 4-4:
Figure 4-5:
Figure 4-6:
Figure 4-7:
Figure 5-1:
Figure 5-2:
DEI Coarse 43.5° CRDM Finite Element Model............................................................
7 DEI Coarse Post-Nozzle Repair Weld Plus Chamfer CRDM Finite Element Model........... 8 Refined Post-Nozzle Repair Weld Plus Chamfer CRDM Finite Element Model................. 9 Boundary Conditions for CRDM Finite Element Model.................................................... 10 Crack Tip Elements of CRDM Finite Element Model........................................................ 11 DEI Stress Distribution on Crack Surface, Post-Weld Repair + Chamfer.......................... 12 Resultant Applied Pressure Loading to Crack Face, DEI + 10 ksi...................................... 13 Location of Stress Intensity Factor Calculation Points....................................................... 16 Stress Intensity Factor Distribution on Uphill Flaw of 43.5 Degree CRDM Nozzle.......... 17 File No.
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1.0 INTRODUCTION
The purpose of this calculation is to evaluate the nozzle weld repair configuration for the Point Beach Unit 2 43.5° top head CRDM penetration. The nozzle weld repair process removes a portion of the existing CRDM nozzle and applying Alloy 52 weld material to attach the nozzle to the head. The repair weld that attaches the cut-off portion of the nozzle to the head is usually inside the hole region, away from the J-groove weld zone. For the 43.5° top head CRDM penetration, the geometry of the head and nozzle is such that a repair weld will overlap a portion of the original J-groove weld. Section 4.0 contains a description of the CRDM nozzle repair sequence.
This calculation determines the stress intensity factors for an assumed axial crack in the original J-groove weld region on the uphill side for a 43.5° top head CRDM penetration using finite element analysis. The downhill side is not susceptible since the repair weld would be located on the low alloy head material.
2.0 METHODOLOGY Build a three-dimensional finite element model representing the 43.5° CRDM penetration nozzle with the assumed flawed geometry and repair weld configuration.
Apply the appropriate loads to the finite element model and use the fracture mechanics features of ANSYS [2] to calculate the stress intensity factor at the tip of the flaw.
3.0 ASSUMPTIONS The fracture mechanics evaluation for the nozzle repair weld is performed with the following assumptions:
The entire J-groove and weld butter are assumed to be cracked up to the vessel-butter interface.
The axial flaw is not within any portion of the CRDM nozzle body.
Although the J-groove/repair weld overlap condition only occurs for a peripheral nozzle (43.5°), a simplifying assumption was made to model the overlap condition using a 00 nozzle geometry. The stresses in the 00 repair weld model are representative of those present in the uphill side of the actual repaired 43.5° nozzle, where the repair weld overlaps the J-groove weld.
4.0 ANALYSIS The nozzle weld repair configuration evaluated in this analysis is described in the Dominion Engineering, Inc. (DEI) Calculation "Point Beach Unit 2 CRDM Nozzle Repair Weld Analysis" [lb].
The finite element model developed from [lb] will be modified for the fracture mechanics evaluation performed herein this calculation. The DEI finite element model is for the top-dead center or 00 nozzle geometry with the weld repair configuration simulated for the most peripheral nozzle, the 43.5° Revision 0
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nozzle CRDM. The J-groove/repair weld overlap geometry occurs on the uphill side of the 43.5° nozzle. The J-groove weld and weld butter are assumed completely cracked. A more refined finite element model is produced using the DEI model. Crack tip elements are incorporated to represent the axial flaw to be analyzed.
4.1 Finite Element Model The CRDM nozzle is a 4-inch nominal diameter nozzle, which penetrates the hemispherical closure head at multiple locations. The dimensions of the top head CRDM nozzle penetration are obtained from the finite element model constructed by Dominion Engineering, Inc. [1]. The CRDM nozzle at the 43.5° location is considered in this evaluation and Figure 4-1 shows the DEI developed finite element model.
The finite element model constructed in Reference lb is modified to include a finer mesh at and near the J-groove weld and nozzle in order to perform the fracture mechanics evaluation. Modifications include mesh refinement, crack tip element creation, as well as application of appropriate boundary conditions. Figure 4-2 shows the coarse DEI finite element model that was obtained from Reference
[lb]. The refined finite element model of the nozzle penetration developed in this calculation is shown in Figure 4-3 and is built using ANSYS [2]. The model reflects the nozzle repair weld and chamfer configuration. The crack tip mesh refinement occurs everywhere around the J-groove weld; i.e. at the vessel interface and nozzle interface. The postulated crack in the J-groove and weld butter is located at the uphill side of the penetration. The edges of the hemispherical closure head finite element model are set far from the nozzle penetration in order to prevent any end effects.
Taking advantage of symmetry, only one half (1800) of the closure head and nozzle penetration is modeled. The finite element model is constructed such that the crack tip region is sufficiently detailed for the stress intensity factor calculation. Quadratic 20-node triangular brick finite elements (SOLID95) from the ANSYS element library are used for the elements at the crack fronts and 8-node structural solid elements (SOLID45) are used for the remainder of the model. In order to more closely represent the singularity at the crack tip, the mid-side nodes of the crack front elements are moved to the quarter point. Furthermore, point-to-point contact gap elements (CONTAC52) are applied to the nodes of the crack face in order to prevent overlap of the crack face under compressive stress loading.
Refer to Figure 4-5 for a plot of the crack tip elements surrounding the uphill side flaw in the J-groove weld region.
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The material properties used in the analysis are the modulus of elasticity and Poisson's ratio. The modulus of elasticity is taken at 3000F from the ASME Code [3]. The material and corresponding modulus of elasticity for each of the different components of the CRDM assembly are as follows:
Modulus of Elasticity, E Component Material (106 psi)
Nozzle Alloy 600 29.9 RPV Top Head Shell Low alloy Steel (SA-302, Grade B) 28.0 Cladding Stainless Steel (Type 304 assumed) 27.0 J-Groove Weld Alloy 182 (Equivalent to Alloy 600) 29.9 Weld Butter Alloy 182 (Equivalent to Alloy 600) 29.9 Weld Repair Alloy 52 (Equivalent to Alloy 690) 29.1 A constant Poisson's ratio of 0.3 is used for all the materials.
4.2 Loads and Boundary Conditions 4.2.1 Loads The finite element model is not used to generate stresses from basic loads. Stresses obtained from another nearly identical geometric finite element model of the nozzle, which does not contain the crack, are input as pressures on the crack face using a standard fracture mechanics superposition technique.
Stresses in the CRDM penetration were obtained from analyses performed by DEI [Ib] for the following load cases:
Load Case 1.
Load Case 2.
Load Case 3.
Load Case 4.
Load Case 5.
Load Case 6.
Load Case 7.
Original J-groove weld sequence (2 passes)
Code Hydrotest + Operating temperature and pressure loads Removal of operating temperature and pressure loads Removal of nozzle material for repair weld prep Simulation of repair weld sequence (8 passes)
Removal of J-groove material to simulate chamfer Operating temperature and pressure on post-repair model The hoop stresses are obtained at Time step 20012, which is the end of Load Case 7. Since the postulated crack to be analyzed is an axial crack (with respect to the CRDM nozzle penetration axis),
the hoop stresses on the elements representing the crack face are extracted from the stress results [Ib]
and applied in the form of pressure loading. The stresses obtained from the nozzle repair weld model of the DEI analysis is for the 0° CRDM nozzle geometry. Although the nozzle repair weld configuration is representative of the 43.5° CRDM nozzle geometry. Per Reference [la], the operating plus residual stress results [la] shows that the maximum uphill inside diameter (ID) hoop stresses are Revision 0
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49.2 ksi and 56.1 ksi for the 0° and 43.5° nozzles, respectively. This corresponds to an increase of 56.1 - 49.2 ksi = 6.9 ksi in the operating stresses between the 00 and 43.5° nozzles pre-nozzle repair weld implementation. Since the DEI nozzle repair weld analysis [lb] was performed using a 00 configuration to simulate the uphill side of the 43.5° nozzle, the stresses from the nozzle repair weld analysis [lb] need to be increased to account for the difference in the operating stresses between the 00 CRDM and the 43.5° CRDM results. Thus, the applied pressure loading for the fracture mechanics analysis is the nozzle weld repair results [lb] conservatively increased by 10 ksi. Figure 4-6 shows the pressure load applied to the fracture mechanics model crack face developed herein for the actual post-weld repair plus chamfer process and operating stresses of the DEI analysis. Figure 4-7 reflects that described in Figure 4-6 plus the additional 10 ksi described above as the resultant applied pressure load.
4.2.2 Boundary Conditions Symmetry boundary conditions were imposed on the uncracked regions of the crack plane.
Translational constraints are applied at the ends of the hemispherical top head. Refer to Figure 4-4 for the boundary conditions that are applied to the finite element model for the nozzle repair weld configuration.
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Figure 4-1: DEI Coarse 43.5° CRDM Finite Element Model Revision 0
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1 ANSYS OCT 2 2003 09:06:49 Point Beach U2 CRDX 0 Dog.
CRDM AZIMUTH - Weld Repair Figure 4-2: DEI Coarse Post-Nozzle Repair Weld Plus Chamfer CRDM Finite Element Model Revision 0
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POINT BEACH U2 POST-WELD REPAIR + CHAMFqR I
Figure 4-3: Refined Post-Nozzle Repair Weld Plus Chamfer CRDM Finite Element Model Revision 0
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1 POINT BEACH U2 POST-WELD REPAIR + CHAMPK Figure 44: Boundary Conditions for CRDM Finite Element Model Revision 0
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I T JW CRACK TIP ELEMENTS POINT BEACH U2 POST-WELD REPAIR + CHAMFI Figure 4-5: Crack Tip Elements of CRDM Finite Element Model Revision 0
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-1
25380 38743 32062 Point Beach Repair Figure 4-6: DEI Stress Distribution on Crack Surface, Post-Weld Repair + Chamfer Revision 0
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42062 Point Beach Repair 95514 Figure 4-7: Resultant Applied Pressure Loading to Crack Face, DEI + 10 ksi Revision 0
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I I'I 5.0 RESULTS OF ANALYSIS Using KCALC, the built-in feature of ANSYS for stress intensity factor calculations, the results of the stress analysis are post-processed and the stress intensity factor is determined at multiple locations along the crack tip. Those locations are shown in Figure 5-1. The stress intensity factors are computed at each location along the crack front on the weld butter-vessel interface. The crack tip locations depicted in Figure 5-1 correspond to the local coordinate system numbers that are tabulated in Table 5-1. Figure 5-2 plots the K distributions along the embedded uphill side flaw. All stress intensity factor results are tabulated in Table 5-1 for the uphill flaw.
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Table 5-1: Stress Intensity Factor Results (psi-qin)
Uphill Nozzle Interface K Results (psi-in1 2)
Local Coord. System Post-Repalr Weld + Chamfer 101 47128 102 60323 103 64819 104 67813 105 71780 106 74626 107 76574 108 78808 109 80507 110 80953 111 80508 112 79939 113 78930 114 77454 115 76024 116 74345 117 72097 118 68965 119 63737 120 55895 121 34376 122 53826 123 60236 124 63998 125 66542 126 68484 127 69957 128 69422 129 66671 130 63118 131 59012 132 54644 133 43200 Revision 0
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Crack Tip 133 Nozzle Interface Crack Tip 121 Kink Crack Tip 101 Vessel ID POINT BEACH U2 POST-WELD REPAIR + CHAMFER Figure 5-1: Location of Stress Intensity Factor Calculation Points Revision 0
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Point Beach U2 CRDM Repair Weld Stress Intensity Factors 90 80 V
0 Y.1 L:
0 1--
V LL r-I.4-U, 1..
70 60 50 40 30 20 10 0
I I
I I
I I
I I
101 103 105 107 109 111 113 115 117 119 121 123 125 127 129 131 133 Crack Tip Location Figure 5-2: Stress Intensity Factor Distribution on Uphill Flaw of 43.5 Degree CRDM Nozzle Revision 0
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6.0 REFERENCES
- 1. Dominion Engineering, Inc. Calculations, SI File No. PBCH-07Q-201:
- a. No. C-4429-00-1, "Point Beach Unit 2 CRDM Stress Analysis," Revision 0.
- 2. ANSYS/Mechanical, Revision 6.1 (w/Service Packs 2 & 3), ANSYS, Inc., April, 2002.
- 3. ASME Boiler and Pressure Vessel Code,Section II, Part D, 1998 Edition with no addenda.
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The following list of electronic files is included in the project files:
FILENAME DESCRIPTION DEI MODEL.INP Generates original DEI finite element model.
GET COORD.INP Obtains node/element connectivity from DEI model.
COORD.INP Output of GET COORD.INP and used for refined model.
REFINED MODEL.INP Generates refined fracture mechanics finite element model.
FM MODEL.INP Adds crack tip elements and applies pressure loading to crack face.
STRESS MACRO.INP Contains pressure loading input.
FM RUN.INP Performs fracture mechanics finite element analysis.
KCALC.INP Calculates and extracts stress intensity factors.
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FILE No.: PBCH-07Q-302 v~ STRUCTURAL CALCULATION INTEGRITY PACKAGE PROJECT No.: PBCH-07Q Associates, Inc.
PROJECT NAME: Point Beach Unit 2 CRDM Top Head Analysis CLIENT: NMC Point Beach Nuclear Plant CALCULATION TITLE: PWSCC Crack Growth Correlations and Crack Growth Calculations for Point Beach Unit 2 Project Mgr.
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1-6 Original Issue H. L. GUSTIN H. L. GUSTIN Al -A17 1/
10/9/03 10/9/03 G. L. STEVENS 10/9/03 Page I of 6 F2001R1
Table of Contents 1.0 STATEMENT OF PROBLEM..........................................................
3 2.0 METHODOLOGY...........................................................
3 3.0 CRACK GROWTH CALCULATIONS..........................................................
4 4.0 RESULTS...........................................................
5
5.0 REFERENCES
6 APPENDIX A FLAW GROWTH CALCULATIONS PC-CRACK OUTPUT.
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1.0 STATEMENT OF PROBLEM In order to evaluate repair options for the Point Beach Unit 2 Top Head CRDM penetrations, it is necessary to evaluate growth of hypothetical flaws in the proposed weld repair fusion line with the low alloy steel base material. The industry Materials Reliability Program (MRP) has prepared a document that predicts PWSCC growth in components such as the CRDM penetration tubes [1].
This approach has been presented to the NRC, and has generally been accepted. The MRP correlation of available crack growth data is normalized in [1] to a service temperature of 617 'F.
The reported top head temperature for Point Beach Unit 2 is 592 'F [2]. The crack growth rate is a strong function of temperature, and so to reasonably represent the Point Beach condition, it is necessary to adjust the MRP crack growth correlation for the lower temperature.
In the following, a temperature-adjusted crack growth correlation is developed. This correlation is then used to predict the crack growth of bounding assumed flaws as a function of time.
2.0 METHODOLOGY MRP-55 [1, page 13] presents a general form of the PWSCC crack growth correlation, based on the data collected:
da/dt = exp[-Qg/R (l/T -/Tref)] cx(K-Kth)P where:
da/dt
= crack growth rate at temperature T in in/yr Qg
= thermal activation for crack growth
= 31.0 kcallmole R
= universal gas constant
= 1.103 x 10-3 kcal/mole 'R T
= absolute operating temperature at location of crack. 'R Tref
= absolute reference temperature used to normalize data
= 598.15 K (1076.67 'R) a
= crack growth amplitude
= 3.69 x 10-3 at 617 'F for da/dt in units of in/yr and K in units of ksi-in K
= crack tip stress intensity factor Kth
= crack tip stress intensity factor threshold
= 8.19 ksi-in 3
= exponent = 1.16 File No.
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To adjust this correlation for Point Beach 2 operating conditions, the operating temperature of 5921F (1051.67 'R) [2] is used for the operating temperature T, above. This gives a plant specific PWSCC growth correlation of:
da/dt = 1.98x 10-3 (K-KYh)I'1 6 in/yr
= 2.26 x 10-7 (K-Kci,)'
6 in/hour The above rates assume that the plant is operating 100% of the time (8760 hour0.101 days <br />2.433 hours <br />0.0145 weeks <br />0.00333 months <br />s/year).
This correlation is applicable to evaluating the growth of ID connected axial flaws in the CRDM penetration tube material.
3.0 CRACK GROWTH CALCULATIONS The objective of the calculation is to determine the time that would be required for a crack at the interface of the Alloy 52 repair material, the low alloy steel head material, and the underlying J-groove material to propagate parallel to the repair weld by a PWSCC mechanism through a distance defined by the repair weld ligament. If the time for such propagation is greater than the remaining service life of the head, no penetration of the pressure boundary due to such a crack would be predicted.
The above crack growth correlation was used with the SI program pc-CRACK [3] to perform PWSCC crack growth calculations. Two hypothetical flaw types were considered, which represent the bounds on geometries that may be encountered. These were:
- 1. A flaw in the axial-radial plane, across the entire remaining J-groove + butter. Such a flaw would be opened by hoop stress, resulting in a tunnel crack under the repair weld.
- 2. A flaw in the axial-circumferential plane, parallel to tube wall, which would be opened by radial stress (which are comparatively small). The resulting crack would be "laminar", or parallel to the tube OD.
PWSCC is driven by both applied and weld residual stresses. Based on analyses performed by Dominion Engineering [2], as summarized in another SI calculation [4], the normal operating stresses plus the weld residual stresses in the hoop direction can reasonably be represented by a constant through wall stress intensity factor of 45 ksi - winch, at the junction of the Alloy 52 repair weld and the low alloy steel head material.
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The analysis assumed that the entire remaining J-groove weld material was degraded (cracked), so no credit was taken for any flaw initiation or growth time in the remaining J-groove material.
Because a constant applied K is assumed, starting flaw size has no effect on crack growth. For the purpose of this analysis, an arbitrary starting flaw depth of 0.1 inch is used, and a final depth of 0.36 inch therefore represents growth through the minimum ligament The flaw located in the axial-radial plane (opened by hoop stresses) was determined to be the governing flaw case, since the applied plus residual stresses in the hoop direction, as determined in the Dominion analysis [2] are greater than those in the radial direction by a factor of two to four. As a result, crack growth in this plane would be slower by a comparable factor.
The pc-CRACK output follows the reference section of this calculation (Appendix A).
3.1 Fatigue crack growth Fatigue crack growth is driven by cyclic stresses. For the present case, the stress state for the assumed flaws is dominated by weld residual stresses, which are steady state secondary stresses.
These residual stresses will not vary with heat-up/cooldown and other plant cycles, and will therefore have only a limited effect on fatigue crack growth (that is, they will have some effect on R-ratio, but none on cyclic delta K values due to cyclic plant operation. For the limited period of remaining plant operation with the current vessel head (estimated at less than 100 heat-up/cooldown cycles), propagation of the hypothetical cracks considered herein by a fatigue mechanism is estimated at approximately 0.0002 inch, and is therefore considered negligible compared to PWSCC propagation. The pc-CRACK fatigue crack growth results are attached.
4.0 RESULTS The above analysis produces the following results:
- 1. An axial-radial crack tunnel would propagate through the worst case remaining ligament (0.26 inch) in about 1.5 EFPY (13,900 EFPH)
- 2. An axial-radial crack tunnel would propagate through the best estimate remaining ligament (0.75 inch) in about 4.5 EFPY
- 3. A laminar (axial-circumferential plane) crack would propagate through the worst case remaining ligament in more than twice the time Revision 0
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A crack would have to propagate through the remaining ligament before leakage and possible wastage could occur.
Using the as-found weld measurements it will be demonstrated that no leakage will occur.
5.0 REFERENCES
- 1. Materials Reliability Program (MRP), "Crack Growth Rates for Evaluating Primary Water Stress Corrosion Cracking (PWSCC) of Thick-Wall Alloy 600 Materiarl, MRP-55. EPRI Proprietary.
- 2. Dominion Engineering, "Point Beach Unit 2 CRDM Nozzle Repair Weld Analysis" Calculation C-4429-00-2, Revision 0, April 2002
- 3. Structural Integrity Associates, pc-CRACK for Windows, version 3.1-98348.
- 4. SI Calculation, "Fracture Mechanics Evaluation of Point Beach Unit 2 Top Head CRDM 43.5 Degree Azimuth Penetration Weld Repair," PBCH-07Q-301, Revision 0.
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APPENDIX A FLAW GROWTH CALCULATIONS PC-CRACK OUTPUT Revision 0
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pc-CRACK for Windows Version 3.1-98348 (C) Copyright '84 - '98 Structural Integrity Associates, Inc.
Linear Elastic Fracture Mechanics Date: Fri Oct 03 08:48:17 2003 Input Data and Results File: TUNNEL1.LFM ritle: Growth of tunnel crack in axial-radial plane, constant 45 ksi -(in)A0.5 Load Cases:
Case ID: constant 45 -- K vs a Depth K
0.0000 45.0000 0.1000 45.0000 0.5000 45.0000 1.5000 45.0000 2.5000 45.0000 Stress Coefficients Case ID Co Cl C2 C3 Type constant 45 0
0 0
0 Kvsa Crack Model: User Input K Versus Crack Size Crack Parameters:
Max. crack size:
1.5000
Stress Intensity Factor------- --------
Crack Case Size constant 4 0.0300 45 0.0600 45 0.0900 45 0.1200 45 0.1500 45 Revision 0
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0.1800 0.2100 0.2400 0.2700 0.3000 0.3300 0.3600 0.3900 0.4200 0.4500 0.4800 0.5100 0.5400 0.5700 0.6000 0.6300 0.6600 0.6900 0.7200 0.7500 0.7800 0.8100 0.8400 0.8700 0.9000 0.9300 0.9600 0.9900 1.0200 1.0500 1.0800 1.1100 1.1400 1.1700 1.2000 1.2300 1.2600 1.2900 1.3200 1.3500 1.3800 1.4100 1.4400 1.4700 1.5000 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 Crack Growth Laws:
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Law ID: MRP55-592 Type: Corrosion Model: Paris da/dN = c * (dK)An where dK = Kmax - Kmin dK > Kthres Kmax < Klc Material parameters:
c = 2.2600e-007 n=
1.1600 Kthres =
8.1900 Material Fracture Toughness KIc:
Material ID: Limit Depth KIc 0.0000 1.5000 3.0000 200.0000 200.0000 200.0000 Initial crack size=
Max. crack size=
0.1000 1.5000 Number of blocks=
1 Print increment of block=
1 Cycles Calc. Print Crk. Grw.
Subblock
/Time incre. incre. Law Mat.
KIc axradiall 30000 100 100 MRP55-592 Limit Kmax Kmin Subblock Case ID Scale Factor Case ID Scale Factor axradiall constant 45 1.0000 Crack growth results:
Total Subblock Cycles Cycles DaDn Revision 0
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/Time frime Kmax Kmin DeltaK R
/DaDt Da a a/thk Block:
100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000 3100 3200 3300 3400 3500 3600 3700 3800 3900 4000 4100 4200 4300 4400 4500 I
100 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.1019 0.00 200 4.50e-+00 1 0.00c+000 4.50e+00 1 0.00 1.87c-005 1.87e-003 0.1037 0.00 300 4.50c+001 400 4.50e+001 500 4.50e+001 600 4.50e+001 700 4.50c+001 800 4.50c+001 900 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.1056 0.00 0.OOc+000 4.50c+001 0.00 1.87c-005 0.OOc+000 4.50e+001 0.00 1.87c-005 0.OOc+000 4.50e+001 0.00 1.87e-005 0.OOe+000 4.50c+001 0.00 1.87e-005 0.OOc+000 4.50c+001 0.00 1.87c-005 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1075 0.00 1.87e-003 0.1093 0.00 1.87e-003 0.1112 0.00 1.87e-003 0.1131 0.00 1.87e-003 0.115 0.00 1.87e-003 0.1168 0.00 1000 4.50e+001 0.OOc+000 4.50e+001 1100 4.50e+001 0.OOc+000 4.50c+001 1200 4.50e+001 0.OOe+000 4.50c-+001 1300 4.50e+001 0.OOc+000 4.50c+001 1400 4.50c+001 0.OOc+000 4.50c+001 1500 4.50e+001 0.OOc+000 4.50e+001 1600 4.50e+001 0.OOc+000 4.50c+001 1700 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1187 0.00 0.00 1.87e-005 1.87e-003 0.1206 0.00 0.00 1.87e-005 1.87e-003 0.1224 0.00 0.00 1.87e-005 1.87e-003 0.1243 0.00 0.00 1.87e-005 1.87e-003 0.1262 0.00 0.00 1.87e-005 1.87c-003 0.128 0.00 0.00 1.87e-005 1.87c-003 0.1299 0.00 0.00 1.87e-005 1.87e-003 0.1318 0.00 1800 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1337 0.00 1900 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1355 0.00 2000 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1374 0.00 2100 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.1393 0.00 2200 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.1411 0.00 2300 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.143 0.00 2400 4.50c+001 0.OOe+000 4.50 c+001 0.00 1.87c-005 1.87c-003 0.1449 0.00 2500 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1467 0.00 2600 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.1486 0.00 2700 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.1505 0.00 2800 4.50e+001 2900 4.50e+001 3000 4.50c+001 3100 4.50c+001 3200 4.50c+001 3300 4.50e+001 3400 4.50c+001 3500 4.50c+001 3600 4.50e+001 3700 4.50c+001 3800 4.50c+001 3900 4.50c+001 4000 4.50c+001 4100 4.50c+001 4200 4.50c+00 1 4300 4.50c+001 4400 4.50c+001 4500 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1524 0.00 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1542 0.00 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.1561 0.00 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.158 0.00 0.OOc+000 4.50e+001 0.00 1.87c-005 1.87c-003 0.1598 0.00 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1617 0.00 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1636 0.00 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.1654 0.00 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.1673 0.00 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1692 0.00 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1711 0.00 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1729 0.00 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.1748 0.00 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.1767 0.00 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.1785 0.00 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87c-003 0.1804 0.00 0.OOc+000 4.50c+00 1 0.00 1.87e-005 1.87c-003 0.1823 0.00 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.1841 0.00 Revision 0
Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A5 of A17
4600 4600 4.50e+00 1 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.186 0.00 4700 4700 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.1879 0.00 4800 4800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.1898 0.00 4900 4900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.1916 0.00 5000 5000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.1935 0.00 5100 5100 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.1954 0.00 5200 5200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.1972 0.00 5300 5300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.1991 0.00 5400 5400 4.50e+00 1 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.201 0.00 5500 5500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2028 0.00 5600 5600 4.50e+00 1 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2047 0.00 5700 5700 4.50e+00 1 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2066 0.00 5800 5800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2085 0.00 5900 5900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2103 0.00 6000 6000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2122 0.00 6100 6100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2141 0.00 6200 6200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2159 0.00 6300 6300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2178 0.00 6400 6400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2197 0.00 6500 6500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2215 0.00 6600 6600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2234 0.00 6700 6700 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2253 0.00 6800 6800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2272 0.00 6900 6900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.229 0.00 7000 7000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2309 0.00 7100 7100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2328 0.00 7200 7200 4.50e+00 1 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2346 0.00 7300 7300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2365 0.00 7400 7400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2384 0.00 7500 7500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2402 0.00 7600 7600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2421 0.00 7700 7700 4.50e+00 1 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.244 0.00 7800 7800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2459 0.00 7900 7900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2477 0.00 8000 8000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2496 0.00 8100 8100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2515 0.00 8200 8200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2533 0.00 8300 8300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2552 0.00 8400 8400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2571 0.00 8500 8500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2589 0.00 8600 8600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2608 0.00 8700 8700 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2627 0.00 8800 8800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2646 0.00 8900 8900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2664 0.00 9000 9000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2683 0.00 9100 9100 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2702 0.00 9200 9200 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.272 0.00 9300 9300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2739 0.00 9400 9400 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.2758 0.00 Revision 0
V9 Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A6 of A17
9500 9600 9700 9800 9900 10000 10100 10200 10300 10400 10500 10600 10700 10800 10900 11000 11100 11200 11300 11400 11500 11600 11700 11800 11900 12000 12100 12200 12300 12400 12500 12600 12700 12800 12900 13000 13100 13200 13300 13400 13500 13600 13700 13800 13900 14000 14100 14200 14300 9500 4.50c+00 1 0.OOc+000 4.50c+00 1 0.00 1.87e-005 1.87e-003 0.2776 0.00 9600 4.50c+00 1 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.2795 0.00 9700 4.50e+00 1 0.OOe+000 4.50c+00 1 0.00 1.87e-005 1.87e-003 0.2814 0.00 9800 4.50c+00 1 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.2833 0.00 9900 4.50e+00 1 0.OOc+000 4.50c+00 1 0.00 1.87e-005 1.87e-003 0.2851 0.00 10000 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.287 0.00 10100 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.2889 0.00 10200 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.2907 0.00 10300 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.2926 0.00 10400 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.2945 0.00 10500 4.50c+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.2963 0.00 10600 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.2982 0.00 10700 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3001 0.00 10800 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.302 0.00 10900 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3038 0.00 11000 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3057 0.00 11100 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3076 0.00 11200 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3094 0.00 11300 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3113 0.00 11400 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3132 0.00 11500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.315 0.00 116004.50c+001 0.OOe+0004.50e+001 0.00 1.87e-005 1.87e-003 0.3169 0.00 11700 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3188 0.00 11800 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3207 0.00 11900 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3225 0.00 12000 4.50c+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.3244 0.00 12100 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3263 0.00 12200 4.50e+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.3281 0.00 12300 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.33 0.00 12400 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3319 0.00 12500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.3337 0.00 12600 4.50e+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3356 0.00 12700 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3375 0.00 12800 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3394 0.00 12900 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3412 0.00 13000 4.50e+001 13100 4.50c+001 13200 4.50e+001 13300 4.50c+001 13400 4.50c+001 13500 4.50e+001 13600 4.50c+001 13700 4.50c+001 13800 4.50c+001 13900 4.50c+001 14000 4.50c+001 14100 4.50e+001 14200 4.50c+001 14300 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.3431 0.00 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.345 0.00 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.3468 0.00 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.3487 0.00 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.3506 0.00 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.3524 0.00 0.OOe+000 4.50c+001 0.00 0.OOc+000 4.50c+001 0.00 0.OOc+000 4.50e+001 0.00 0.OOc+000 4.50e+001 0.00 0.OOc+000 4.50e+001 0.00 0.OOc+000 4.50c+001 0.00 0.OOe+000 4.50c+001 0.00 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.3543 0.00 1.87c-005 1.87c-003 0.3562 0.00 1.87c-005 1.87c-003 0.3581 0.00 1.87e-005 1.87c-003 0.3599 0.00 Ligament Depth + 0.1 Start Flaw 1.87e-005 1.87e-003 0.3618 0.00 1.87e-005 1.87e-003 0.3637 0.00 1.87e-005 1.87e-003 0.3655 0.00 1.87e-005 1.87e-003 0.3674 0.00 Revision 0
V Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A7 of A17
14400 14400 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3693 0.00 14500 14500 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3711 0.00 14600 14600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.373 0.00 14700 14700 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3749 0.00 14800 14800 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3768 0.00 14900 14900 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3786 0.00 15000 15000 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3805 0.00 15100 15100 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3824 0.00 15200 15200 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3842 0.00 15300 15300 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3861 0.00 15400 15400 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.388 0.00 15500 15500 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3898 0.00 15600 15600 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3917 0.00 15700 15700 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3936 0.00 15800 15800 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3955 0.00 15900 15900 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3973 0.00 16000 16000 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.3992 0.00 16100 16100 4.50e+001 O.OOe+0004.50e+001 0.00 1.87e-005 1.87e-003 0.4011 0.00 16200 16200 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4029 0.00 16300 16300 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.40480.00 16400 16400 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4067 0.00 16500 16500 4.50e+001 0.00e+0004.50e+001 0.00 1.87e-005 1.87e-003 0.40850.00 16600 16600 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4104 0.00 16700 16700 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4123 0.00 16800 16800 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4142 0.00 16900 16900 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4160.00 17000 17000 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4179 0.00 17100 17100 4.50e+001 0.00e+0004.50e+001 0.00 1.87e-005 1.87e-003 0.4198 0.00 17200 17200 4.50e+001 0.00e+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4216 0.00 17300 17300 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4235 0.00 17400 17400 4.50e+001 0.00e+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.4254 0.00 17500 17500 4.50e+001 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.4272 0.00 17600 17600 4.50e+001 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.4291 0.00 17700 17700 4.50e+001 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.431 0.00 17800 17800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4329 0.00 17900 17900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4347 0.00 18000 18000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4366 0.00 18100 18100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4385 0.00 18200 18200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4403 0.00 18300 18300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4422 0.00 18400 18400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4441 0.00 18500 18500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4459 0.00 18600 18600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4478 0.00 18700 18700 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4497 0.00 18800 18800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4516 0.00 18900 18900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4534 0.00 19000 19000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4553 0.00 19100 19100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4572 0.00 19200 19200 4.50e+0001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.459 0.00 Revision 0
V Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A8 of A17
19300 19300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4609 0.00 19400 19400 4.50e+001 0.00e+000 4.50e+001 0.00 1.87c-005 1.87c-003 0.4628 0.00 19500 19500 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4646 0.00 19600 19600 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.4665 0.00 19700 19700 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4684 0.00 19800 19800 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.4703 0.00 19900 19900 4.50c+0001 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.4721 0.00 20000 20000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.474 0.00 20100 20100 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.4759 0.00 20200 20200 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.4777 0.00 20300 20300 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4796 0.00 20400 20400 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4815 0.00 20500 20500 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4833 0.00 20600 20600 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87c-003 0.4852 0.00 20700 20700 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4871 0.00 20800 20800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.489 0.00 20900 20900 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4908 0.00 21000 21000 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4927 0.00 21100 21100 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.4946 0.00 21200 21200 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.4964 0.00 21300 21300 4.50e+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.4983 0.00 21400 21400 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5002 0.00 21500 21500 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.502 0.00 21600 21600 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.5039 0.00 21700 21700 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.5058 0.00 21800 21800 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.5077 0.00 21900 21900 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87c-003 0.5095 0.00 22000 22000 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.51140.00 22100 22100 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5133 0.00 22200 22200 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.5151 0.00 22300 22300 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.517 0.00 22400 22400 4.50+e+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5189 0.00 22500 22500 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5207 0.00 22600 22600 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87c-005 1.87e-003 0.5226 0.00 22700 22700 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5245 0.00 22800 22800 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5264 0.00 22900 22900 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5282 0.00 23000 23000 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5301 0.00 23100 23100 4.50c+001 0.OOe+000 4.50e+001 0.00 1.87c-005 1.87c-003 0.532 0.00 23200 23200 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.5338 0.00 23300 23300 4.50e+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5357 0.00 23400 23400 4.50e+001 0.OOe+000 4.50c+0001 0.00 1.87e-005 1.87e-003 0.5376 0.00 23500 23500 4.50e+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5394 0.00 23600 23600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5413 0.00 23700 23700 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5432 0.00 23800 23800 4.50c+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5451 0.00 23900 23900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87c-005 1.87e-003 0.5469 0.00 24000 24000 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.5488 0.00 24100 24100 4.50e+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5507 0.00 Revision 1
0 Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A9 of A17
24200 24200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5525 0.00 24300 24300 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5544 0.00 24400 24400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5563 0.00 24500 24500 4.50e+001 O.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5581 0.00 24600 24600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.56 0.00 24700 24700 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5619 0.00 24800 24800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5638 0.00 24900 24900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5656 0.00 25000 25000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5675 0.00 25100 25100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5694 0.00 25200 25200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5712 0.00 25300 25300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5731 0.00 25400 25400 4.50e+001 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.575 0.00 25500 25500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5768 0.00 25600 25600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5787 0.00 25700 25700 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5806 0.00 25800 25800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5825 0.00 25900 25900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5843 0.00 26000 26000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5862 0.00 26100 26100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5881 0.00 26200 26200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5899 0.00 26300 26300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5918 0.00 26400 26400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5937 0.00 26500 26500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5955 0.00 26600 26600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5974 0.00 26700 26700 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.5993 0.00 26800 26800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6012 0.00 26900 26900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.603 0.00 27000 27000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6049 0.00 27100 27100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6068 0.00 27200 27200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6086 0.00 27300 27300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6105 0.00 27400 27400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6124 0.00 27500 27500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6142 0.00 27600 27600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6161 0.00 27700 27700 4.50e+001 0.OOe+000 4.50e+00 1 0.00 1.87e-005 1.87e-003 0.618 0.00 27800 27800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6199 0.00 27900 27900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6217 0.00 28000 28000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6236 0.00 28100 28100 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6255 0.00 28200 28200 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6273 0.00 28300 28300 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6292 0.00 28400 28400 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6311 0.00 28500 28500 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6329 0.00 28600 28600 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6348 0.00 28700 28700 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6367 0.00 28800 28800 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6386 0.00 28900 28900 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6404 0.00 29000 29000 4.50e+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6423 0.00 Revision 0
V9 Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page AIO of A17 li
29100 29200 29300 29400 29500 29600 29700 29800 29900 30000 29100 4.50e+001 0.OOc+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6442 0.00 29200 4.50e+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.646 0.00 29300 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.6479 0.00 29400 4.50c+001 0.OOe+000 4.50e+001 0.00 1.87e-005 1.87e-003 0.6498 0.00 29500 4.50e+001 0.OOe+000 4.50c+001 0.00 1.87c-005 1.87e-003 0.6516 0.00 29600 4.50c+001 0.OOc+000 4.50c+001 0.00 1.87c-005 1.87c-003 0.6535 0.00 29700 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.6554 0.00 29800 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.6573 0.00 29900 4.50c+001 0.OOe+000 4.50c+001 0.00 1.87e-005 1.87e-003 0.6591 0.00 300004.50e+001 0.OOe+0004.50c+001 0.00 1.87e-005 1.87e-003 0.661 0.00 End of pc-CRACK Output Revision 1 0 V
Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page All of A17
tm pc-CRACK for Windows Version 3.1-98348 (C) Copyright '84 - '98 Structural Integrity Associates, Inc.
Linear Elastic Fracture Mechanics Date: Wed Oct 08 15:47:58 2003 Input Data and Results File: FATIGUE.LFM
Title:
fatigue crack growth analysis for Point Beach repair Load Cases:
Case ID Stress Coefficients CO Cl C2 C3 Type Applied residual 20 60 0
0 0
0 0 Coeff 0 Coeff
Through Wall Stresses for Load Cases With Stress Coeff-----
Wall Case Case Depth Applied residual 0.0000 0.1000 0.2000 0.3000 0.4000 0.5000 0.6000 0.7000 0.8000 0.9000 1.0000 20 20 20 20 20 20 20 20 20 20 20 60 60 60 60 60 60 60 60 60 60 60 Crack Model: Single Edge Cracked Plate Crack Parameters:
Plate width:
2.0000 Max. crack size:
1.0000
Stress Intensity Factor------------------
Crack Case Case Size Applied residual 0.0200 0.0400 0.0600 0.0800 0.1000 0.1200 0.1400 0.1600 0.1800 0.2000 0.2200 0.2400 0.2600 0.2800 0.3000 0.3200 0.3400 0.3600 0.3800 0.4000 0.4200 0.4400 0.4600 0.4800 0.5000 0.5200 0.5400 0.5600 0.5800 0.6000 0.6200 0.6400 0.6600 0.6800 0.7000 0.7200 0.7400 0.7600 0.7800 0.8000 0.8200 0.8400 0.8600 5.42685 7.7279 9.52983 11.0793 12.4711 13.7535 14.955 16.0939 17.1829 18.2313 19.4953 20.7529 22.007 23.2598 24.513 25.7681 27.0263 28.2884 29.5552 30.8275 32.3354 33.8605 35.4029 36.9626 38.5394 40.1334 41.7446 43.3727 45.0179 46.6799 48.7773 50.9049 53.0621 55.2486 57.464 59.7079 61.98 64.2799 66.6073 68.9619 72.3064 75.7008 79.1444 16.2806 23.1837 28.5895 33.2379 37.4133 41.2605 44.8649 48.2816 51.5488 54.6939 58.4858 62.2586 66.021 69.7794 73.5391 77.3044 81.0788 84.8651 88.6656 92.4824 97.0061 101.582 106.209 110.888 115.618 120.4 125.234 130.118 135.054 140.04 146.332 152.715 159.186 165.746 172.392 179.124 185.94 192.84 199.822 206.886 216.919 227.102 237.433 Revision 0
V?
Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A13 of A17
0.8800 0.9000 0.9200 0.9400 0.9600 0.9800 1.0000 82.6366 86.1767 89.7641 93.3982 97.0783 100.804 104.575 247.91 258.53 269.292 280.195 291.235 302.412 313.724 Crack Growth Laws:
Law ID: PB-I Model: ASME Section Xl - austenitic stainless steel in air environment da/dN = C
- I OAF
- S
- dKA3.3 where S= 1.0 forR<0
= 1.0+ 1.8
- R for0<R<0.79
= -43.5 + 57.97
- R for 0.79 < R < I F = code specified function of temperature dK = Kmax - Kmin R = Kmin / Kmax where:
C I OAF= 1.9352e-010 is for the currently selected units of:
force: kip length: inch temperature: 592.0000 Fahrenheit Material Fracture Toughness KIc:
Material ID: Shell Depth KIc 0.0000 1.0000 2.0000 200.0000 200.0000 200.0000
[nitial crack size=
Wax. crack size=
0.1000 1.0000 Number of blocks=
Print increment of block=
Il Revision 0
V Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A14 of A17
Cycles Calc. Print Crk. Grw.
Mat.
Subblock
[Time incre. incre. Law Klc PB Fatigue 100 1
I PB-I Shell Kmax Kmin Subblock Case ID Scale Factor Case ID Scale Factor PB Fatigue Applied 1.0000 residual 1.0000 residual 1.0000 Crack growth results:
Total Subblock Cycles Cycles DaDn
/Time /Time Kmax Kmin DeltaK R
/DaDt Da a a/thk Block:
I I
1 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 2
2 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 3
3 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 4
4 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 5
5 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 6
6 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 7
7 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 8
8 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 9
9 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 10 104.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 11 11 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 12 124.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 13 13 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 14 144.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 15 15 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 16 164.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 17 174.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 18 18 4.99c+001 3.74e+001 1.25e+001 0.75 1.88c-006 1.88c-006 0.1 0.05 19 19 4.99e+001 3.74e+001 1.25e+001 0.75 1.88c-006 1.88c-006 0.1 0.05 20 204.99e+001 3.74e+001 1.25e+001 0.75 1.88c-006 1.88c-006 0.1 0.05 21 21 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88c-006 0.1 0.05 22 22 4.99e+001 3.74e+001 1.25e+001 0.75 1.88c-006 1.88c-006 0.1 0.05 23 23 4.99e+001 3.74e+001 1.25e+001 0.75 1.88c-006 1.88e-006 0.1 0.05 24 24 4.99e+001 3.74e+001 1.25e+001 0.75 1.88c-006 1.88c-006 0.1 0.05 25 25 4.99e+001 3.74e+001 1.25e+001 0.75 1.88c-006 1.88e-006 0.1 0.05 26 26 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1 0.05 27 27 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 28 28 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88c-006 0.1001 0.05 File No.
PBCH-07Q-302 I
29 29 4.99e+00 1 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 30 30 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 31 31 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 32 32 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 33 33 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 34 34 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 35 35 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 36 36 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 37 37 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 38 38 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 39 39 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 40 40 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 41 41 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 42 42 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 43 43 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 44 44 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 45 45 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 46 46 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 47 47 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 48 48 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 49 49 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 50 50 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 51 51 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 52 52 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 53 53 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 54 54 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 55 55 4.99e+001 3.74e+001 1.25e+00 1 0.75 1.88e-006 1.88e-006 0.1001 0.05 56 56 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 57 57 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 58 58 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 59 59 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 60 60 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 61 61 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 62 62 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 63 63 4.99e+001 3.74e+001 1.25e+00 1 0.75 1.88e-006 1.88e-006 0.1001 0.05 64 64 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 65 65 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 66 66 4.99e+001I 3.74e+001I 1.25e+001I 0.75 1.88e-006 1.88e-006 0.1001 0.05 67 67 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 68 68 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 69 69 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 70 70 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 71 71 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 72 72 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 73 73 4.99e+001 3.74e+001 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 74 74 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 75 75 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.88e-006 1.88e-006 0.1001 0.05 76 76 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.89e-006 1.89e-006 0.1001 0.05 77 77 4.99e+001I 3.74e+001I 1.25e+001 0.75 1.89e-006 1.89e-006 0.1001 0.05 Revision 9
~~Preparer/Date HLG 10/9/03 Vb~~Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A16 of A17
78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 78 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89c-006 0.1001 0.05 79 4.99e+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1001 0.05 80 4.99c+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89c-006 0.1002 0.05 81 4.99e+001 3.74c+001 1.25e+001 0.75 1.89c-006 1.89e-006 0.1002 0.05 82 4.99e+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89c-006 0.1002 0.05 83 4.99e+001 3.74c+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 84 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89c-006 0.1002 0.05 85 4.99e+001 3.74c+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 86 4.99e+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 87 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89e-006 0.1002 0.05 88 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89e-006 0.1002 0.05 89 4.99e+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 90 4.99c+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 91 4.99e+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 92 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89c-006 0.1002 0.05 93 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89e-006 0.1002 0.05 94 4.99e+001 3.74c+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 95 4.99e+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 96 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89e-006 0.1002 0.05 97 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89c-006 0.1002 0.05 98 4.99e+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89e-006 0.1002 0.05 99 4.99e+001 3.74e+001 1.25e+001 0.75 1.89e-006 1.89e-006 0.1002 0.05 100 4.99c+001 3.74e+001 1.25e+001 0.75 1.89c-006 1.89e-006 0.1002 0.05 End of pc-CRACK Output Revision 0
V Preparer/Date HLG 10/9/03 Checker/Date GLS 10/9/03 File No.
PBCH-07Q-302 Page A17 of A17