ML093360324

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Calculation, 0800368.301, Rev 0, Material Properties for Davis-Besse Unit 1, RCP Suction, RCP Discharge, Cold Leg Drain and Core Flood Nozzles Preemptive Weld Overlay Repairs.
ML093360324
Person / Time
Site: Davis Besse Cleveland Electric icon.png
Issue date: 04/21/2009
From: Chintapalli A, White S
FirstEnergy Nuclear Operating Co, Structural Integrity Associates
To:
Office of Nuclear Reactor Regulation
References
L-09-268, TAC ME0477, TAC ME0478 0800368.301, Rev 0
Download: ML093360324 (50)
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Structural Integrity Associates, Inc. File No.: 0800368.301 CALCULATION PACKAGE Project No.: 0800368 I Quality Program: [F Nuclear El Commercial PROJECT NAME: Davis Besse Phase 2 Alloy 600 CONTRACT NO.: 49151. RevI CLIENT: PLANT: Welding Service Inc (WSI) Davis-Besse Nuclear Power Station. Unit I CALCULATION TITLE: Material Properties for Davis-Besse Unit 1. RCP Suction, RCP Discharge, Cold Leg Drain and Core Flood Nozzles Preemptive Weld Overlay Repairs Document Affected Project Manager Co-Preparer(s)

&Revision Pages Revision Description Approval Checker(s)

Signature

& Date Signatures

& Date 0 1-23 Initial Issue Preparers:

Al -A27 /z Computer Files 04/21/09 04/21/09 Steve White 04/21/09 Checker: Vikram Marthandam 04/21/09 Page I of 23 F0306-OI RO Structural Integrity Associates, Inc.Table of Contents 1.0 O B JE C T IV E .................................................................................................................................

3 2.0 M E T H O D O L O G Y .......................................................................................................................

3 3.0 A S SU M P T IO N S ...........................................................................................................................

3 4 .0 D E SIG N IN PU T S .........................................................................................................................

4 5.0 C O N C L U SIO N S ..........................................................................................................................

4 6.0 R E FE R E N C E S .............................................................................................................................

5 APPENDIX A MATERIAL PROPERTY INPUT FILES ..........................................................

Al List of Tables Table 1: M aterial D esignation

........................................................................................................

6 Table 2: Elastic Properties for SA-508, Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

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8 Table 3: Elastic-Plastic Properties for SA-508, Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

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9 Table 4: Elastic Properties for Alloy 82/182 .................................................................................

10 Table 5: Elastic-Plastic Properties for Alloy 82/182 ..........................................................................

11 Table 6: Elastic Properties for Alloy 52M/152 .............................................................................

12 Table 7: Elastic-Plastic Properties for Alloy 52M/152 .................................................................

13 Table 8: Elastic Properties for SA-240-304L, SA-371 ER308L and ER308L (18Cr-8Ni)

...........

14 Table 9: Elastic-Plastic Properties for SA-240-304L, SA-371 ER308L and ER308L (18Cr-8Ni)

.... 15 Table 10: Elastic Properties for A-376, Type 316, A-351 Grade CF8M, A-336 Grade F8M, SA-403 WP 316 (16Cr-12Ni-2Mo)

...................................................................................

16 Table 11: Elastic-Plastic Properties for A-376, Type 316, A-351 Grade CF8M, A-336 Grade F8M, SA-403 WP 316 (16Cr-12Ni-2Mo)

...................................................................

17 Table 12: Elastic Properties for SA-105, Grade 2 (C>0.3%) ........................................................

18 Table 13: Elastic-Plastic Properties for SA-105, Grade 2 ............................................................

19 Table 14: Elastic Properties for A-106 Grade C (C>0.3%) ...........................................................

20 Table 15: Elastic-Plastic Properties for A-106 Grade C ...............................................................

21 Table 16: Elastic Properties for SA-516 Grade 70 (<4" thick, C<0.3%) ......................................

22 Table 17: Elastic-Plastic Properties for SA-516 Grade 70 (<4" thick, C<0.3%) ..........................

23 FileNo.: 0800368.301 Page 2 of 23 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.1.0 OBJECTIVE The purpose of this calculation is to identify the materials of the Reactor Coolant Pump (RCP)Suction, RCP Discharge, Cold Leg Drain and Core Flood Nozzle components to be analyzed for preemptive weld overlay repair for Davis-Besse, Unit 1. Material property datavalues are obtained for use in subsequent finite element analyses using the commercial software package ANSYS [1].2.0 METHODOLOGY The material component information for the nozzles of interest are obtained from References 6 through 9. The material property data values are obtained from the ASME Code,Section II, Part D, 2001 Edition with Addenda through 2003 [2] and ASME Code,Section II, Part A, Ferrous Material Specification

[4].Two input files are developed containing the material property data for use within ANSYS for specific analyses.

Material property data values are defined for linear and nonlinear type analyses, which will be temperature dependent.

Linear material property data values will be used for thermal-mechanical analyses (MProp LinearDB.INP).

Nonlinear material property data values will be used for weld residual analyses (MPropMISONLinearDB.INP).

3.0 ASSUMPTIONS

The following assumptions are made with respect to the analyses (i.e., linear, nonlinear):

o The nozzle-to-safe end weld for the RCP Discharge and the safe end-to-pipe weld for the Core Flood Nozzle are identified as SS Type 316. SS Type 316 is assumed to have similar properties to SA-376, Type 316.o The cladding for the Core Flood Nozzle is listed in Reference 6 as Stainless Steel and is assumed to have similar properties to SA-240-304L.

  • Any ID weld repairs are assumed to be Alloy 82/182.o The weld overlay material is assumed to be Alloy 52M, which has similar material properties to Alloy 690. Alloy 52M is assumed for the overlay weld filler metal based on Reference 3." A buffer layer of ER308L is assumed to be applied over the stainless steel components prior to the application of the Alloy 52M overlay material.o Poisson's ratio and density are assumed temperature independent.

File No.: 0800368.301 Page 3 of 23 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.o Linear interpolation is-used obtain material properties that are not provided in the ASME Code.o The Reactor Vessel is assumed to be clad with the equivalent of SA-240-304L.

  • High Temperature material properties (above ASME Code values) are based on values and assumptions from Reference 5.* The RCP cold leg drain nozzle-to-cold leg weld is not modeled. Instead, the materials transition instantly.

Stress from this transition will be local to the transition and remote from the weld overlay repair. Therefore, those stresses are insignificant to the weld overlay repair.o The Spray Nozzle-to-RCP Discharge Safe End weld and Pressure Tap-to-RCP Discharge Safe End weld are assumed to be SS Type 316. SS Type 316 is assumed to have similar properties to SA-376, Type 316.4.0 DESIGN INPUTS Material designations for the various components are shown in Table 1. The thermal and structural properties (E, a, k, cp) are obtained from Reference

2. Non-linear material properties required for residual stress analysis based on multi-linear isotropic hardening (MISO) principles are obtained from Reference
5. Linear and non-linear (elastic and elastic-plastic) properties at high temperatures are necessary for simulating the molten metal for the residual stress analysis.

Elastic and elastic-plastic properties for these materials are shown in Tables 2 through 17. For the ASME Code,Section III stress evaluation, only temperatures up to design temperature are necessary.

5.0 CONCLUSION

S Two input files have been developed in this calculation for use in the subsequent finite element analyses.

They are included in Appendix A and the computer files.File No.: 0800368.301 Revision:

0 Page 4 of 23 F0306-01RO Structural Integrity Associates, Inc.

6.0 REFERENCES

1. ANSYS/Mechanical, Release 8.1 (w/Service Pack 1), ANSYS, Inc., June 2004.2. ASME Boiler and Pressure Vessel Code,Section II, Part D, Material Properties, 2001 Edition with Addenda through 2003.3. Materials Reliability Program Technical Basis for Preemption Weld Overlays for Alloy 82/182 Butt Welds in PWRs (MRP-169), EPRI, Palo Alto, CA and Structural Integrity Associates, Inc., San Jose, CA : 2005. 1012843.4. ASME Boiler and Pressure Vessel Code,Section II, Part A, Ferrous Material Specifications, 2001 Edition with Addenda through 2003.5. SI Calculation No. 0800777.302, Rev. 2, "Material Properties for Residual Stress Analyses, Including MISO Properties." 6. "Input List -Design Data," Rev. 1, Design Input Information Supplied by FirstEnergy Nuclear Operating Company on 9/12/08, SI File No. 0800368.241.
10. ASME Boiler and Pressure Vessel Code,Section III, Appendices, 1974 Edition.11. ASME Boiler and Pressure Vessel Code,Section II, Material Specifications, 1974 Edition.File No.: 0800368.301 Revision:

0 Page 5 of 23 F0306-O IRO V Structural Integrity Associates, Inc.Table 1: Material Designation Nozzle-to-SE Nozzle-to-Attached Component Nozzle Forging Safe -End Clad Butter and Weld pipe butter Pipe/Elbow Weld and weld RCP Inlet/Suction A-351, Grade N/A SA240-304L N/A N/A Alloy A-516, CF8Ml 0 82/182' Grade 70 A-351, Grade A-376, S Alloy A-516, RCP Discharge CF8M'0 Type 316 (Assumed)6 82/1821 N/A Grade 70 SA-105 SA-371 Alloy SA-403 RCP Cold Leg Drain GAde N/A SA371L 3 N/A N/A 82/82 SA340 Grade 28 ER308L3 82/1821 WP316 ss SA-508 SA-336, Stainless Steel Alloy Tp SA-376, Core Flood Nozzle Class 25 Grade F8M 7 (Assumed)3 82/1821 (Assumed)6 Type 316 Core Flood Vessel Shell I Core Flood Vessel Clad SS Clad 3 (Assumed)ID Weld Repair Alloy 82/182' (Assumed)Weld Overlay Alloy 52M 2 (Assumed)Cold Leg Straight Pipe Cold Leg Clad SA-240-304L Spray Nozzle on -Discharge Nozzle Pressure Tap on Discharge Nozzle Spray Nozzle and Pressure Tap welds to the SS Type 316 (Assumed)6 RCP Discharge Safe End Buffer Layer ER308L 3 (Assumed)Notes: 1.2.3.4.5.6.7.8.9.10.Alloy 82/182 elastic properties are equivalent to Alloy 600.Alloy 52M properties will be treated as equivalent to Alloy 690.SA-371 ER308L, ER308L, the stainless steel clad for Core Flood Nozzle and Vessel Shell will be treated as SA-240-304L.All materials in this table are obtained from Reference 6 unless otherwise specified.

SA-508 Grade 2, Class 1 was formerly known as SA-508 Class 2 in Reference 4.SS Type 316 will be treated as SA-376 Type 316.SA-336, Grade F8M is not mentioned in Reference

4. Going back to the 1974 Edition of the ASME Code [10, 11], A-336, Grade F8M has similar chemical composition as well as allowables for Design Stress Intensity, Sm, Yield Strength, Sy, and Ultimate Strength when compared to SA-430 FP316. Therefore, material properties of SA-430 FP316 from the 2001 Edition of the ASME Code [2, 4] will be used in substitution for A-336, Grade F8M.SA-105 Grade 2 is now defined in Reference 4 as SA-105.A-182 F316 has similar composition and material properties as SA-376 Type 316.SI's past experience has shown that when using available thermally aged cast austenitic stainless steel (CASS)toughness data, thermal aging of the CASS does not significantly affect the results of the weld overlay residual File No.: 0800368.301 Revision:

0 Page 6 of 23 F0306-O1RO V Structural Integrity Associates, Inc.stress analysis.

Thermal aging affects the mechanical properties of the CASS, increasing the yield and ultimate strengths, and reducing the elongation and reduction of area. SI performed a search of published data, investigating the effects of thermal aging at temperatures ranging from 300 to 400'C (572 to 752°F) for from 10000 to 50000 hours on mechanical properties of CASS. The result of that search indicated that one could reasonably represent the thermal aging effects on yield strength and ultimate tensile strength by increasing these by approximately 15% and correspondingly decrease the elongation and reduction of area by 15-20% to see the effect on residual stress following a weld overlay application.

Taking our investigation one step further, a two-dimensional finite element analysis was performed where we compared the ID and through wall residual stresses of a 30-inch diameter weld overlay repaired CASS component in the unaged condition to one in the aged condition where the properties were adjusted as described in the paragraph above. The investigation revealed that the change in properties had very minimal effect on the as-welded residual stresses, when comparing the unaged to the aged condition.

The change was of the order of a few ksi, well within any anticipated scatter in the raw data. There is also no effect on the applied loads, or the physical properties, such as modulus of elasticity, thermal conductivity, thermal diffusivity, thermal expansion, and specific heat. Consequently, the effects on the above properties need not be adjusted for thermal aging.File No.: 0800368.301 Revision:

0 Page 7 of 23 F0306-01RO V Structural Integrity Associates, Inc.Table 2: Elastic Properties for SA-508, Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

Temperature Young's Mean Thermal Thermal Conductivity Specific Heat 2 Modulus Expansion (OF) (x10 6 psi) (xl0" 6 in/in/0 F) (x1- Btu/sec-in-°F) (Btu/Ib-°F) 70 27.8 6.4 5.44 0.105 100 27.61 6.5 5.46 0.107 150 27.4' 6.6 5.46 0.110 200 27.1 6.7 5.46 0.114 250 26.91 6.8 5.44 0.116 300 26.7 6.9 5.42 0.119 350 26.4' 7.0 5.39 0.122 400 26.1 7.1 5.35 0.125 450 25.91 7.2 5.30 0.128 500 25.7 7.3 5.25 0.130 550 25.51 7.3 5.21 0.133 600 25.2 7.4 5.14 0.135 650 24.9' 7.5 5.07 0.137 700 24.6 7.6 5.00 0.140 1100 21.5 8.2 4.40 0.173 1500 3 16 8.6 3.50 0.154 25003 0.1 9.5 1.16 0.204 Density (p) = 0.283 lb/in 3 , assumed temperature independent.

Poisson's Ratio (u) = 0.3, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat = TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 8 of 23 F0306-OIRO V Structural Integrity Associates, Inc.Table 3: Elastic-Plastic Properties for SA-508, Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

True True Temperature Strain Stress (in/in) (psi)0.0017986 50000 0.0065369 60250 70 0.0183386 70500 0.0508884 80750 0.1308399 91000 0.0016809 43200 0.0042582 55150 500 0.0131226 67100 0.0432616 79050 0.1306929 91000 0.0016545 40700 0.0037548 53275 700 0.0116755 65850 0.0407883 78425 0.1306539 91000 0.0011163 24000 0.0129052 36000 1100 0.0430001 48000 0.1136083 60000 0.2542214 72000 0.0004375 7000 0.0289125 17750 1500 0.1012202 28500 0.2377615 39250 0.4545419 50000 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 9 of 23 F0306-OIRO V Structural Integrity Associates, Inc.Table 4: Elastic Properties for Alloy 82/182 Temperature Young's Mean Thermal Thermal Conductivity Specific Heat 2 Modulus Expansion (OF) (x,0 6 psi) (xl0-6 in/in/°F) (x10- Btu/sec-in-°F) (Btu/lb-°F) 70 31.0 6.8 1.99 0.108 100 30.81 6.9 2.01 0.109 150 30.5' 7.0 2.06 0.111 200 30.2 7.1 2.11 0.113 250 30.0' 7.2 2.15 0.114 300 29.8 7.3 2.22 0.116 350 29.7' 7.4 2.27 0.116 400 29.5 7.5 2.34 0.118 450 29.3' 7.6 2.38 0.118 500 29.0 7.6 2.45 0.120 550 28.9' 7.7 2.50 0.121 600 28.7 7.8 2.57 0.123 650 28.5' 7.8 2.62 0.123 700 28.2 7.9 2.69 0.125 1100 25.9 8.4 3.19 0.139 15003 23.1 9.0 3.70 0.148 25003 0.1 10.0 5.09 0.177 Density (p) = 0.300 lb/in 3 , assumed temperature independent.

Poisson's Ratio (u) = 0.29, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat = TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 10 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 5: Elastic-Plastic Properties for Alloy 82/182 Temperature True True (OF) Strain Stress (0 F) (in/in) (psi)0.0017581 54500 0.0626142 77125 70 0.1323668 99750 0.2410555 122375 0.3972410 145000 0.0016379 47500 0.0608769 67625 500 0.1300082 87750 0.2382802 107875 0.3943945 128000 0.0016596 46800 0.0622784 66350 700 0.1321471 85900 0.2412033 105450 0.3980922 125000 0.0017375 45000 0.0688026 62250 1100 0.1404333 79500 0.2499634 96750 0.4053648 114000 0.0012900 29800 0.1814980 41100 1500 0.2996116 52400 0.4484683 63700 0.6285114 75000 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 11 of 23 F0306-O1RO Structural Integrity Associates, Inc.Table 6: Elastic Properties for Alloy 52M/152 Temperature Young's Mean Thermal Thermal Conductivity Specific Heat 2 Modulus Expansion TX1S4 (OF) (x,0 6 psi) (xl0-6 in/in/0 F) (x10- Btu/sec-in-0 F) (Btu/lb-0 F)70 30.3 7.7 1.57 0.107 100 30.1 1 7.8 1.62 0.108 150 29.81 7.8 1.69 0.110 200 29.5 7.9 1.76 0.112 250 29.3 1 7.9 1.83 0.114 300 29.1 7.9 1.90 0.116 350 29.01 8.0 1.97 0.117 400 28.8 8.0 2.04 0.118 450 28.61 8.1 2.11 0.119 500 28.3 8.1 2.18 0.121 550 28.21 8.1 2.25 0.122 600 28.1 8.2 2.31 0.123 650 27.91 8.2 2.38 0.124 700 27.6 8.3 2.45 0.125 1100 25.3 8.5 3.03 0.135 1500' 22.6 8.8 3.59 0.147 25003 0.1 9.5 5.09 0.167 Density (p) = 0.293 lb/in 3 , assumed temperature independent.

Poisson's Ratio (u) = 0.29, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat = TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 12 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 7: Elastic-Plastic Properties for Alloy 52M/152 True True Temperature Strain Stress (0 F) (in/in) (psi)0.0016073 48700 0.0630592 75275 70 0.1421644 101850 0.2663752 128425 0.4441853 155000 0.0012898 36500 0.0396551 59125 500 0.1033755 81750 0.2147115 104375 0.3873830 127000 0.0012500 34500 0.0354049 57125 700 0.0968184 79750 0.2076735 102375 0.3836597 125000 0.0012530 31700 0.0493023 50775 1100 0.1202071 69850 0.2373289 88925 0.4112380 108000 0.0012434 28100 0.2618302 44075 1500 0.4304344 60050 0.6289623 76025 0.8547593 92000 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 13 of 23 F0306-OIRO Structural Integrity Associates, Inc.Table 8: Elastic Properties for SA-240-304L, SA-371 ER308L and ER308L (18Cr-8Ni)

Temperature Young's Mean Thermal Thermal Conductivity Specific Heae Modulus Expansion (X104 (OF) (x10 6 psi) (xlO-6 in/in/°F)

Btu/sec-in-0 F) (Btu/lb-0 F)70 28.3 8.5 1.99 0.116 100 28.11 8.6 2.01 0.117 150 27.91 8.8 2.08 0.120 200 27.6 8.9 2.15 0.122 250 27.31 9.1 2.22 0.124 300 27.0 9.2 2.27 0.125 350 26.81 9.3 2.34 0.127 400 26.5 9.5 2.41 0.129 450 26.21 9.6 2.45 0.130 500 25.8 9.7 2.52 0.131 550 25.61 9.8 2.57 0.132 600 25.3 9.8 2.62 0.133 650 25.11 9.9 2.69 0.134 700 24.8 10.0 2.73 0.135 1100 22.1 10.5 3.15 0.140 1500 3 18.1 10.8 3.54 0.145 2500' 0.1 11.5 4.86 0.159 Density (p) = 0.283 lb/in 3 , assumed temperature independent.

Poisson's Ratio (u) = 0.3, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat = TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 14 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 9: Elastic-Plastic Properties for SA-240-304L, SA-371 ER308L and ER308L (18Cr-8Ni)

True True Temperature Strain Stress (7 F) (in/in) (psi)0.0012367 35000 0.0777489 64750 70 0.1821409 94500 0.3382732 124250 0.5503345 154000 0.0008527 22000 0.0358911 42750 500 0.1059492 63500 0.2314091 84250 0.4262954 105000 0.0008065 20000 0.0281096 40000 700 0.0908367 60000 0.2111270 80000 0.4075613 100000 0.0007421 16400 0.0138355 30050 1100 0.0519078 43700 0.1392265 57350 0.3044729 71000 0.0007182 13000 0.0652982 18250 1500 0.1354897 23500 0.2429079 28750 0.3950595 34000 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 1 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 15 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 10: Elastic Properties for A-376, Type 316, A-351 Grade CF8M, A-336 Grade F8M, SA-403 WP 316 (16Cr-12Ni-2Mo)

Temperature Young's Mean Thermal Thermal Conductivity Specific Heat 2 Modulus Expansion TX1S4 (OF) (x,0 6 psi) (xl0" 6 in/in/0 F) (x10 4 Btu/sec-in-°F) (Btu/lb-0 F)70 28.3 8.5 1.90 0.121 100 28.11 8.6 1.92 0.121 150 27.91 8.8 1.99 0.124 200 27.6 8.9 2.04 0.124 250 27.31 9.1 2.11 0.127 300 27.0 9.2 2.15 0.127 350 26.81 9.3 2.20 0.128 400 26.5 9.5 2.27 0.129 450 26.21, 9.6 2.31 0.130 500 25.8 9.7 2.36 0.130 550 25.61 9.8 2.43 0.133 600 25.3 9.8 2.48 0.133 650 25.11 9.9 2.52 0.133 700 24.8 10.0 2.59 0.135 1100 22.1 10.5 3.01 0.141 15003 18.1 10.8 3.40 0.145 2500' 0.1 11.5 4.40 0.155 Density (p) = 0.283 lb/in 3 , assumed temperature independent.

Poisson's Ratio (i)) = 0.3, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat = TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 16 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 11: Elastic-Plastic Properties for A-376, Type 316, A-351 Grade CF8M, A-336 Grade F8M, SA-403 WP 316 (16Cr-12Ni-2Mo)

True True Temperature Strain Stress (0 F) (in/in) (psi)0.0014982 42400 0.1300043 69800 70 0.2546138 97200 0.4219726 124600 0.6325849 152000 0.0012791 33000 0.0616081 52500 500 0.1421800 72000 0.2692310 91500 0.4511647 111000 0.0011573 28700 0.0471341 48775 700 0.1211840 68850 0.2457186 88925 0.4321680 109000 0.0010407 23000 0.0262971 38000 1100 0.0768737 53000 0.1739465 68000 0.3357481 83000 0.0006630 12000 0.0301352 17250 1500 0.0772324 22500 0.1632721 27750 0.3037215 33000 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 17 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 12: Elastic Properties for SA-105, Grade 2 (C>0.3%)Temperature Young's Mean Thermal Thermal Conductivity Specific Heat2 Modulus Expansion (X104 (OF) (x10 6 psi) (xl0-6 in/in/0 F) ( tu/sec-in-0 F) (BtuIb-0 F)70 29.3 6.4 8.13 0.103 100 29.11 6.5 8.03 0.105 150 28.91 6.6 7.89 0.108 200 28.6 6.7 7.78 0.112 250 28.41 6.8 7.62 0.115 300 28.1 6.9 7.48 0.118, 350 27.8' 7.0 7.31 0.121 400 27.5 7.1 7.15 0.123 450 27.31 7.2 7.01 0.125 500 27.1 7.3 6.83 0.128 550 26.8' 7.3 6.67 0.130 600 26.5 7.4 6.48 0.132 650 25.9' 7.5 6.32 0.135 700 25.3 7.6 6.16 0.138 1100 17.9 8.2 4.84 0.171 1500' 8.0 8.6 3.63 0.198 2500' 0.1 9.5 2.31 0.204 Density (p) = 0.283 lb/in 3 , assumed temperature independent.

Poisson's Ratio (u) = 0.3, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat = TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 18 of 23 F0306-01RO V Structural Integrity Associates, Inc.Table 13: Elastic-Plastic Properties for SA-105, Grade 2 True True Temperature Strain Stress (0 F) (in/in) (psi)0.0012287 36000 0.0189353 49500 70 0.0529716 63000 0.1239287 76500 0.2543922 90000 0.0010812 29300 0.0122960 44475 500 0.0419116 59650 0.1124188 74825 0.2541804 90000 0.0010198 25800 0.0097556 41850 700 0.0369914 57900 0.1068094 73950 0.2540781 90000 0.0010615 19000 0.0917640 25750 1100 0.1708286 32500 0.2830538 39250 0.4330697 46000 0.0015000 12000 0.2466409 15000 1500 0.3545140 18000 0.4818666 21000 0.6286895 24000 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 1 1 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 19 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 14: Elastic Properties for A-106 Grade C (C>0.3%)Temperature Young's Mean Thermal Thermal Conductivity Specific Heat 2 Modulus Expansion (OF) (x10 6 psi) (xl0" 6 in/in/°F) (x1- Btu/sec-in-'F) (Btu/lb-°F) 70 29.3 6.4 8.13 0.103 100 29.11 6.5 8.03 0.105 150 28.91 6.6 7.89 0.108 200 28.6 6.7 7.78 0.112 250 28.41 6.8 7.62 0.115 300 28.1 6.9 7.48 0.118 350 27.81 7.0 7.31 0.121 400 27.5 7.1 7.15 0.123 450 27.3' 7.2 7.01 0.125 500 27.1 7.3 6.83 0.128 550 26.81 7.3 6.67 0.130 600 26.5 7.4 6.48 0.132 650 25.9' 7.5 6.32 0.135 700 25.3 7.6 6.16 0.138 1100 17.9 8.2 4.84 0.171 15003 8.0 8.6 3.63 0.198 25003 0.1 9.5 2.31 0.204 Density (p) = 0.283 lb/in 3 , assumed temperature independent.

Poisson's Ratio (u) = 0.3, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat =TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 20 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 15: Elastic-Plastic Properties for A-106 Grade C True True Temperature Strain Stress (0 F) (in/in) (psi)0.0013652 40000 0.0242564 52500 70 0.0607202 65000 0.1313209 77500 0.2545637 90000 0.0012030 32600 0.0153223 46950 506 0.0471649 61300 0.1180426 75650 0.2543331 90000 0.0011304 28600 0.0118318 43950 700 0.0409899 59300 0.1113772 74650 0.2542167 90000 0.0012291 22000 0.1147927 28000 1100 0.1928368 34000 0.2979323 40000 0.4333004 46000 0.0002500 2000 0.1694709 2875 1500 0.2879455 3750 0.4375783 4625 0.6183490 5500 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 21 of 23 F0306-O1RO V Structural Integrity Associates, Inc.Table 16: Elastic Properties for SA-516 Grade 70 (<4" thick, C<0.3%)Temperature Young's Mean Thermal Thermal Conductivity Specific Heat 2 Modulus Expansion (OF) (x10 6 psi) (xl0-6 in/in/°F) (x1- Btu/sec-in-°F) (Btu/lb-°F) 70 29.5 6.4 8.13 0.103 100 29.31 6.5 8.03 0.105 150 29.11 6.6 7.89 0.108 200 28.8 6.7 7.78 0.112 250 28.61 6.8 7.62 0.115 300 28.3 6.9 7.48 0.118 350 28.01 7.0 7.31 0.121 400 27.7 7.1 7.15 0.123 450 27.51 7.2 7.01 0.125 500 27.3 7.3 6.83 0.128 550 27.01 7.3 6.67 0.130 600 26.7 7.4 6.48 0.132 650 26.1' 7.5 6.32 0.135 700 25.5 7.6 6.16 0.138 1100 18.0 8.2 4.84 0.171 15003 5.0 8.6 3.63 0.198 25003 0.1 9.5 2.31 0.204 Density (p) = 0.283 lb/in 3 , assumed temperature independent.

Poisson's Ratio (u) = 0.3, assumed temperature independent.

Notes: 1. Interpolated.

2. Specific Heat values are derived from the equation shown in General Note (a) of Table TCD [2], Specific Heat = TC / (TD x density).3. Values per Reference 5.File No.: 0800368.301 Revision:

0 Page 22 of 23 F0306-01RO V Structural Integrity Associates, Inc.Table 17: Elastic-Plastic Properties for SA-516 Grade 70 (<4" thick, C<0.3%)True True Temperature Strain Stress (0 F) (in/in) (psi)0.0012881 38000 0.0031809 48250 70 0.0104401 58500 0.0374803 68750 0.1224852 79000 0.0011355 31000 0.0021324 43000 500 0.0069050 55000 0.0303574 67000 0.1222991 79000 0.0010667 27200 0.0018781 40150 700 0.0056595 53100 0.0271289 66050 0.1222079 79000 0.0011667 21000 0.0917411 27000 1100 0.1656717 33000 0.2713432 39000 0.4143524 45000 0.0030000 15000 0.2558446 18750 1500 0.3673114 22500 0.4988409 26250 0.6504237 30000 0.0100000 1000 0.2543666 2000 2500 0.4621339 3000 0.7070397 4000 0.9840915 5000 File No.: 0800368.301 Revision:

0 Page 23 of 23 F0306-O1RO V Structural Integrity Associates, Inc.APPENDIX A MATERIAL PROPERTY INPUT FILES File No.: 0800368.301 Revision:

0 Page Al of A27 F0306-OIRO V Structural Integrity Associates, Inc.MPropLinearDB.INP

/COM,*** * ** *** *** ******** ****************

  • /COM, MATERIAL PROPERTIES for Thermal-Mechanical Analyses MAT 1: Nozzle Forging -RCP Inlet/Suction, Discharge A-351, Grade CF8M (16Cr-12Ni-2Mo)

MAT 2: Nozzle Forging -RCP Cold Leg Drain SA-105 Grade 2 (Carbon Steel, C>0.3%)MAT 3: Nozzle Forging -Core Flood Nozzle SA-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

MAT 4: Nozzle-to-Safe End Weld -Core Flood Alloy 82/182 MAT 5: Safe End- RCP Discharge A-376, Type 316 (16Cr-12Ni-2Mo)

MAT 6: Safe End -Core Flood Nozzle A-336, Grade F8M (assumed similar to SA-430 FP316 (l6Cr-l2Ni-2Mo))

MAT 7: Pipe Internal Clad -RCP Inlet/Suction, Discharge, cold leg clad SA-240-304L (18Cr-8Ni)

MAT 8: Nozzle Internal Clad -RCP Cold Leg Drain, Core Flood SA-371 ER308L (assumed SA-240-304L (18Cr-8Ni))

MAT 9: ID Weld Repair Alloy 82/182 MAT 10: Safe End-to-Pipe Weld -RCP Discharge Alloy 82/182 MAT 11: Safe End-to-Pipe Weld -Core Flood SS Type 316 (assumed similar to SA-376 TP316 (l6Cr-l2Ni-2Mo))

MAT 12: Attached Pipe/Elbow

-RCP Inlet/Suction, Discharge A-516 Grade 70 (Carbon Steel, (<=4" C < 0.3%))MAT 13: Attached Pipe/Elbow

-RCP Cold Leg Drain SA-403 WP316 (l6Cr-12Ni-2Mo)

MAT 14: Attached Pipe/Elbow

-Core Flood Nozzle SA-376, Type 316 (l6Cr-l2Ni-2Mo)

MAT 15: Cold Leg Pipe -RCP Cold Leg Drain A-106 Grade C (C>0.3%)MAT 16: Core Flood Vessel Shell A-508 Class 2 (3/4Ni-1/2Mo-l/3Cr-V)

MAT 17: Core Flood Vessel Clad SS Clad (assumed SA-240 304L (18Cr-8Ni))

MAT 18: Weld Overlay Alloy 52M MAT 19: Nozzle to Pipe Weld -RCP Inlet/Suction, RCP Cold Leg Drain Alloy 82/182 1 MAT 20: Butter material Alloy 82/182 MAT 21: Buffer Layer ER308L (assumed SA-240-304L (18Cr-8Ni))

MAT 22: RCP Discharge Nozzle-to-SE Weld, Spray Nozzle and Pressure Tap welds to RCP Discharge SE SS Type 316 (assumed similar to SA-376 TP316 (l6Cr-l2Ni-2Mo))

MAT 23: Pressure Tap -Discharge Nozzle A-336, Grade F8M (assumed similar to SA-430 FP316 (l6Cr-l2Ni-2Mo))

MAT 24: Spray Nozzle -Discharge Nozzle A-182 F 316 (16Cr-12Ni-2Mo)

MPTEMP,, 70, 100 MPTGEN,, 12, 150, 50! MAT 1: A-351, Grade CF8M (16Cr-12Ni-2Mo)

MPDATA,EX, 1,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 1,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 1,, 25.1e6, 24.8e6 MPDATA,ALPX, 1, , 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 1, , 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 1,, 9.9E-6, IOE-6 MPDATA,KXX, 1,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 1,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 1,, 2.52E-4, 2.59E-4 MPDATA,C, 1,, 0.121, 0.121, 0.124, 0.124, 0.127, 0.127, MPDATA,C, 1,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C, 1,, 0. 133, 0.135 MP, DENS, 1, 0.283 MP, NUXY, 1, 0.3! MAT 2: SA-105 Grade 2 (Hi Carbon)MPDATA,EX, 2,, 29.3e6, 29.1e6, 28.9e6, 28.6e6, 28.4e6, 28. 1e6 MPDATA,EX, 2,, 27.8e6, 27.5e6, 27.3e6, 27.1e6, 26.8e6, 26.5e6 MPDATA,EX, 2,, 25.9e6, 25.3e6 MPDATA,ALPX, 2,, 6.4E-6, 6.5E-6, 6.6E-6, 6.7E-6, 6.8E-6, 6.9E-6 MPDATA,ALPX, 2,, 7.OE-6, 7.1E-6, 7.2E-6, 7.3E-6, 7.3E-6, 7.4E-6 MPDATA,ALPX, 2,, 7.5E-6, 7.6E-6 MPDATA,KXX , 2,, 8.13E-4, 8.03E-4, 7.89E-4, 7.78E-4, 7.62E-4, 7.48E-4 MPDATA,KXX , 2,, 7.3 1E-4, 7.15E-4, 7.01E-4, 6.83E-4, 6.67E-4, 6.48E-4 File No.: 0800368.301 Revision:

0 Page A2 of A27 F0306-01RO Structural Integrity Associates, Inc.MPDATA,KXX, 2,, 6.32E-4, 6.16E-4 MPDATA,C, 2,, 0.103, 0.105, 0.108, 0.112, 0.115, 0.118, MPDATA,C , 2,, 0.121, 0.123, 0.125, 0.128, 0.130, 0.132, MPDATA,C, 2,, 0.135, 0.138 MP, DENS, 2, 0.283 MP, NUXY, 2, 0.3! MAT 3: SA-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

MPDATA,EX , 3,, 27.8e6, 27.6e6, 27.4e6, 27.1e6, 26.9e6, 26.7e6 MPDATA,EX , 3,, 26.4e6, 26.1e6, 25.9e6, 25.7e6, 25.5e6, 25.2e6 MPDATA,EX , 3,, 24.9e6, 24.6e6 MPDATA,ALPX, 3,, 6.4E-6, 6.SE-6, 6.6E-6, 6.7E-6, 6.8E-6, 6.9E-6 MPDATA,ALPX, 3,, 7E-6, 7.1E-6, 7.2E-6, 7.3E-6, 7.3E-6, 7.4E-6 MPDATA,ALPX, 3,, 7.5E-6, 7.6E-6 MPDATA,KXX, 3,, 5.44E-4, 5.46E-4, 5.46E-4, 5.46E-4, 5.44E-4, 5.42E-4 MPDATA,KXX, 3,, 5.39E-4, 5.35E-4, 5.3E-4, 5.25E-4, 5.21E-4, 5.14E-4 MPDATA,KXX, 3,, 5.07E-4, 5E-4 MPDATA,C , 3,, 0.105, 0.107, 0.11, 0.114, 0.116,0.119, MPDATA,C , 3,, 0.122, 0.125, 0.128, 0.13, 0.133, 0.135, MPDATA,C , 3,, 0.137, 0.14 MP, DENS, 3, 0.283 MP, NUXY, 3, 0.3! MAT 4: Alloy 82/182 MPDATA,EX

,4,, 31e6, 30.8e6, 30.5e6, 30.2e6, 30e6, 29.8e6 MPDATA,EX

,4,, 29.7e6, 29.5e6, 29.3e6, 29e6, 28.9e6, 28.7e6 MPDATA,EX

,4,, 28.5e6, 28.2e6 MPDATA,ALPX,4,, 6.8E-6, 6.9E-6, 7E-6, 7.1E-6, 7.2E-6, 7.3E-6 MPDATA,ALPX,4,, 7.4E-6, 7.5E-6, 7.6E-6, 7.6E-6, 7.7E-6, 7.8E-6 MPDATA,ALPX,4,, 7.8E-6, 7.9E-6 MPDATA,KXX

,4,, 1.99E-4, 2.01E-4, 2.06E-4, 2.11E-4, 2.15E-4, 2.22E-4 MPDATA,KXX

,4,, 2.27E-4, 2.34E-4, 2.38E-4, 2.45E-4, 2.5E-4, 2.57E-4 MPDATA,KXX

,4,, 2.62E-4, 2.69E-4 MPDATA,C ,4,, 0.108, 0.109, 0.111,0.113, 0.114, 0.116, MPDATA,C ,4,, 0.116, 0.118, 0.118, 0.120, 0.121, 0.123, MPDATA,C ,4,, 0.123, 0.125 MP, DENS,4, 0.300 MP, NUXY,4, 0.29! MAT 5: A-376, Type 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 5,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 5,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 5,, 25.1e6, 24.8e6 MPDATA,ALPX, 5,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 5,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 5,, 9.9E-6, 1OE-6 MPDATA,KXX, 5,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 5,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 5,, 2.52E-4, 2.59E-4 MPDATA,C , 5,, 0.121, 0.121, 0.124, 0.124, 0.127, 0.127, MPDATA,C , 5,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C, 5,, 0.133, 0.135 File No.: 0800368.301 Page A3 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.MP, DENS, 5, 0.283 MP, NUXY, 5, 0.3! MAT 6: A-336, Grade F8M (assumed similar to SA-430 FP316 (16Cr-l2Ni-2Mo))

MPDATA,EX, 6,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 6,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 6,, 25.1e6, 24.8e6 MPDATA,ALPX, 6,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.IE-6, 9.2E-6 MPDATA,ALPX, 6,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 6,, 9.9E-6, 1OE-6 MPDATA,KXX, 6,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 6,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 6,, 2.52E-4, 2.59E-4 MPDATA,C, 6,, 0.121, 0.121, 0.124, 0.124, 0.127, 0.127, MPDATA,C , 6,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C , 6,, 0.133, 0.135 MP, DENS, 6, 0.283 MP, NUXY, 6, 0.3! MAT 7: SA-240-304L (18Cr-8Ni)

MPDATA,EX , 7,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX , 7,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX , 7,, 25.1e6, 24.8e6 MPDATA,ALPX, 7,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 7,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 7,, 9.9E-6, 1OE-6 MPDATA,KXX, 7,, 1.99E-4, 2.01E-4, 2.08E-4, 2.15E-4, 2.22E-4, 2.27E-4 MPDATA,KXX, 7,, 2.34E-4, 2.41E-4, 2.45E-4, 2.52E-4, 2.57E-4, 2.62E-4 MPDATA,KXX, 7,, 2.69E-4, 2.73E-4 MPDATA,C , 7,, 0.116, 0.117, 0.12, 0.122, 0.124, 0.125, MPDATA,C , 7,, 0.127, 0.129, 0.13, 0.131, 0.132, 0.133, MPDATA,C , 7,, 0.134, 0.135 MP, DENS, 7, 0.283 MP, NUXY, 7, 0.3! MAT 8: SA-371 ER308L (assumed SA-240-304L (18Cr-8Ni))

MPDATA,EX , 8,, 28.3e6, 28. 1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX , 8,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX , 8,, 25.1e6, 24.8e6 MPDATA,ALPX, 8,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.IE-6, 9.2E-6 MPDATA,ALPX, 8,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 8,, 9.9E-6, lOE-6 MPDATA,KXX, 8,, 1.99E-4, 2.O1E-4, 2.08E-4, 2.15E-4, 2.22E-4, 2.27E-4 MPDATA,KXX, 8,, 2.34E-4, 2.41E-4, 2.45E-4, 2.52E-4, 2.57E-4, 2.62E-4 MPDATA,KXX, 8,, 2.69E-4, 2.73E-4 MPDATA,C , 8,, 0.116, 0.117, 0.12, 0.122, 0.124, 0.125, MPDATA,C , 8,, 0.127, 0.129, 0.13, 0.131, 0.132, 0.133, MPDATA,C , 8,, 0.134, 0.135 MP, DENS, 8, 0.283 MP, NUXY, 8, 0.3! MAT 9: Alloy 82/182 MPDATA,EX

,9,, 31e6, 30.8e6, 30.5e6, 30.2e6, 30e6, 29.8e6 File No.: 0800368.301 Revision:

0 Page A4 of A27 F0306-O1RO Structural Integrity Associates, Inc.MPDATA,EX

,9,, 29.7e6, 29.5e6, 29.3e6, 29e6, 28.9e6, 28.7e6 MPDATA,EX

,9,, 28.5e6, 28.2e6 MPDATA,ALPX,9,, 6.8E-6, 6.9E-6, 7E-6, 7.1E-6, 7.2E-6, 7.3E-6 MPDATA,ALPX,9,, 7.4E-6, 7.5E-6, 7.6E-6, 7.6E-6, 7.7E-6, 7.8E-6 MPDATA,ALPX,9,, 7.8E-6, 7.9E-6 MPDATA,KXX

,9,, 1.99E-4, 2.01E-4, 2.06E-4, 2.11E-4, 2.15E-4, 2.22E-4 MPDATA,KXX

,9,, 2.27E-4, 2.34E-4, 2.38E-4, 2.45E-4, 2.5E-4, 2.57E-4 MPDATA,KXX

,9,, 2.62E-4, 2.69E-4 MPDATA,C ,9,,0.108,0.109, 0.111, 0.113, 0.114, 0.116, MPDATA,C ,9,, 0.116, 0.118, 0.118, 0.120, 0.121, 0.123, MPDATA,C ,9,,0.123, 0.125 MP, DENS,9, 0.300 MP, NUXY,9, 0.29! MAT 10: Alloy 82/182 MPDATA,EX

,10,, 31e6, 30.8e6, 30.5e6, 30.2e6, 30e6, 29.8e6 MPDATA,EX , 10,, 29.7e6, 29.5e6, 29.3e6, 29e6, 28.9e6, 28.7e6 MPDATA,EX , 10,, 28.5e6, 28.2e6 MPDATA,ALPX, 10,, 6.8E-6, 6.9E-6, 7E-6, 7.1E-6, 7.2E-6, 7.3E-6 MPDATA,ALPX, 10,., 7.4E-6, 7.5E-6, 7.6E-6, 7.6E-6, 7.7E-6, 7.8E-6 MPDATA,ALPX, 10,, 7.8E-6, 7.9E-6 MPDATA,KXX, 10,, 1.99E-4, 2.O1E-4, 2.06E-4, 2.11E-4, 2.15E-4, 2.22E-4 MPDATA,KXX, 10,, 2.27E-4, 2.34E-4, 2.38E-4, 2.45E-4, 2.5E-4, 2.57E-4 MPDATA,KXX, 10,, 2.62E-4, 2.69E-4 MPDATA,C ,10,, 0.108, 0.109, 0.111, 0.113, 0.114, 0.116, MPDATA,C , 10,,0.116,0.118,0.118,0.120,0.121,0.123, MPDATA,C , 10,, 0.123, 0.125 MP, DENS, 10, 0.300 MP, NUXY, 10, 0.29! MAT 11: SS Type 316 (assumed as SA-376, Type 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 11,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 11,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 11,, 25.1e6, 24.8e6 MPDATA,ALPX, 11,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 11,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 11,, 9.9E-6, 1OE-6 MPDATA,KXX, 11,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 11,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 11,, 2.52E-4, 2.59E-4 MPDATA,C, 11,, 0.121, 0.121, 0.124, 0.124, 0.127, 0.127, MPDATA,C, 11,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C, 11,, 0.133, 0.135 MP, DENS, 11, 0.283 MP, NUXY, 11,0.3! Mat 12: A-516 Grade 70 (Carbon Steel, (<=4" C<0.3%))MPDATA,EX, 12,, 29.5E6, 29.3E6, 29.1E6, 28.8E6, 28.6E6, 28.3E6 MPDATA,EX, 12,, 28.0E6, 27.7E6, 27.5E6, 27.3E6, 27.0E6, 26.7E6 MPDATA,EX, 12,, 26. 1E6, 25.5E6 MPDATA,ALPX, 12,, 6.4E-6, 6.5E-6, 6.6E-6, 6.7E-6, 6.8E-6, 6.9E-6 MPDATA,ALPX, 12,, 7.OE-6, 7.1E-6, 7.2E-6, 7.3E-6, 7.3E-6, 7.4E-6 MPDATA,ALPX, 12,, 7.5E-6, 7.6E-6 File No.: 0800368.301 Page A5 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.MPDATA,KXX, 12,, 8.13E-4, 8.03E-4, 7.89E-4, 7.78E-4, 7.62E-4, 7.48E-4 MPDATA,KXX, 12,, 7.31E-4, 7.15E-4, 7.O1E-4, 6.83E-4, 6.67E-4, 6.48E-4 MPDATA,KXX, 12,, 6.32E-4, 6.16E-4 MPDATA,C, 12,,0.103,0.105, 0.108, 0.112,0.115,0.118, MPDATA,C, 12,,0.121,0.123,0.125,0.128,0.130,0.132, MPDATA,C, 12,,0.135,0.138 MP, DENS, 12, 0.283 MP, NUXY, 12, 0.3 Mat 13: SA-403 WP 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 13,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 13,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 13,, 25.1e6, 24.8e6 MPDATA,ALPX, 13,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 13,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 13,, 9.9E-6, IOE-6 MPDATA,KXX, 13,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 13,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 13,, 2.52E-4, 2.59E-4 MPDATA,C, 13,, 0.121, 0.121, 0.124, 0.124,0.127,0.127, MPDATA,C, 13,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C, 13,, 0.133, 0.135 MP, DENS, 13, 0.283 MP, NUXY, 13, 0.3! Mat 14: SA-376, Type 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 14,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 14,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 14,, 25.1e6, 24.8e6 MPDATA,ALPX, 14,, 8.5E-6, 8.6E-6, 8.8E-6,8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 14,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 14,, 9.9E-6, 1OE-6 MPDATA,KXX, 14,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 14,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 14,, 2.52E-4, 2.59E-4 MPDATA,C, 14,,0.121,0.121,0.124,0.124,0.127,0.127, MPDATA,C, 14,,0.128,0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C, 14,, 0.133, 0.135 MP, DENS, 14, 0.283 MP, NUXY, 14, 0.3! Mat 15: A-106 Grade C (C>0.3%)MPDATA,EX , 15,, 29.3e6, 29.1e6, 28.9e6, 28.6e6, 28.4e6, 28.1e6 MPDATA,EX , 15,, 27.8e6, 27.5e6, 27.3e6, 27.1e6, 26.8e6, 26.5e6 MPDATA,EX , 15,, 25.9e6, 25.3e6 MPDATA,ALPX, 15,, 6.4E-6, 6.5E-6, 6.6E-6, 6.7E-6, 6.8E-6, 6.9E-6 MPDATA,ALPX, 15,, 7.OE-6, 7.1E-6, 7.2E-6, 7.3E-6, 7.3E-6, 7.4E-6 MPDATA,ALPX, 15,, 7.5E-6, 7.6E-6 MPDATA,KXX, 15,, 8.13E-4, 8.03E-4, 7.89E-4, 7.78E-4, 7.62E-4, 7.48E-4 MPDATA,KXX, 15,, 7.31E-4, 7.15E-4, 7.01E-4, 6.83E-4, 6.67E-4, 6.48E-4 MPDATA,KXX, 15,, 6.32E-4, 6.16E-4 MPDATA,C , 15,,0.103,0.105,0.108,0.112,0.115,0.118, File No.: 0800368.301 Revision:

0 Page A6 of A27 F0306-O1RO V Structural Integrity Associates, Inc.MPDATA,C , 15,,0.121,0.123,0.125, 0.128, 0.130, 0.132, MPDATA,C , 15,,0.135,0.138 MP, DENS, 15, 0.283 MP, NUXY, 15, 0.3! Mat 16: A-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

MPDATA,EX

,16,, 27.8e6, 27.6e6, 27.4e6, 27.1e6, 26.9e6, 26.7e6 MPDATA,EX , 16,, 26.4e6, 26.1e6, 25.9e6, 25.7e6, 25.5e6, 25.2e6 MPDATA,EX , 16,, 24.9e6, 24.6e6 MPDATA,ALPX, 16,, 6.4E-6, 6.5E-6, 6.6E-6, 6.7E-6, 6.8E-6, 6.9E-6 MPDATA,ALPX, 16,, 7E-6, 7.1E-6, 7.2E-6, 7.3E-6, 7.3E-6, 7.4E-6 MPDATA,ALPX, 16,, 7.5E-6, 7.6E-6 MPDATA,KXX, 16,, 5.44E-4, 5.46E-4, 5.46E-4, 5.46E-4, 5.44E-4, 5.42E-4 MPDATA,KXX, 16,, 5.39E-4, 5.35E-4, 5.3E-4, 5.25E-4, 5.21E-4, 5.14E-4 MPDATA,KXX, 16,, 5.07E-4, 5E-4 MPDATA,C , 16,,0.105, 0.107, 0.11, 0.114, 0.116, 0.119, MPDATA,C , 16,,0.122, 0.125, 0.128, 0.13, 0.133, 0.135, MPDATA,C , 16,,0.137, 0.14 MP, DENS, 16, 0.283 MP, NUXY, 16, 0.3 Mat 17: SA-371 ER308L (assumed SA-240-304L (18Cr-8Ni))

MPDATA,EX , 17,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX , 17,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX , 17,, 25.1e6, 24.8e6 MPDATA,ALPX, 17,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 17,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 17,, 9.9E-6, 1OE-6 MPDATA,KXX, 17,, 1.99E-4, 2.O1E-4, 2.08E-4, 2.15E-4, 2.22E-4, 2.27E-4 MPDATA,KXX, 17,, 2.34E-4, 2.41E-4, 2.45E-4, 2.52E-4, 2.57E-4, 2.62E-4 MPDATA,KXX, 17,, 2.69E-4, 2.73E-4 MPDATA,C , 17,,0.116, 0.117, 0.12, 0.122, 0.124, 0.125, MPDATA,C , 17,, 0.127, 0.129, 0.13, 0.131, 0.132, 0.133, MPDATA,C , 17,, 0.134, 0.135 MP, DENS, 17, 0.283 MP, NUXY, 17, 0.3! Mat 18: Alloy 690 for Alloy 52M MPDATA,EX

,18,, 30.3e6, 30.1e6, 29.8e6, 29.5e6, 29.3e6, 29.1e6 MPDATA,EX , 18,, 29e6, 28.8e6, 28.6e6, 28.3e6, 28.2e6, 28.1e6 MPDATA,EX , 18,, 27.9e6, 27.6e6 MPDATA,ALPX, 18,, 7.7E-6, 7.8E-6, 7.8E-6, 7.9E-6, 7.9E-6, 7.9E-6 MPDATA,ALPX, 18,, 8E-6, 8E-6, 8.1E-6, 8.1E-6, 8.1E-6, 8.2E-6 MPDATA,ALPX, 18,, 8.2E-6, 8.3E-6 MPDATA,KXX, 18,, 1.57E-4, 1.62E-4, 1.69E-4, 1.76E-4, 1.83E-4, 1.9E-4 MPDATA,KXX, 18,, 1.97E-4, 2.04E-4, 2.11E-4, 2.18E-4, 2.25E-4, 2.31E-4 MPDATA,KXX, 18,, 2.38E-4, 2.45E-4 MPDATA,C , 18,, 0.107, 0.108, 0.110, 0.112, 0.114, 0.116, MPDATA,C , 18,, 0.117, 0.118, 0.119, 0.121, 0.122, 0.123, MPDATA,C , 18,, 0.124, 0.125 MP, DENS, 18, 0.293 MP, NUXY, 18, 0.29 File No.: 0800368.301 Page A7 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.! Mat 19: Alloy 82/182 MPDATA,EX

,19,, 31e6, 30.8e6, 30.5e6, 30.2e6, 30e6, 29.8e6 MPDATA,EX

,19,, 29.7e6, 29.5e6, 29.3e6, 29e6, 28.9e6, 28.7e6 MPDATA,EX

,19,, 28.5e6, 28.2e6 MPDATA,ALPX,19,, 6.8E-6, 6.9E-6, 7E-6, 7.1E-6, 7.2E-6, 7.3E-6 MPDATA,ALPX,19,, 7.4E-6, 7.5E-6, 7.6E-6, 7.6E-6, 7.7E-6, 7.8E-6 MPDATA,ALPX, 19,, 7.8E-6, 7.9E-6 MPDATA,KXX

,19,, 1.99E-4, 2.O1E-4, 2.06E-4, 2.11E-4, 2.15E-4, 2.22E-4 MPDATA,KXX

,19,, 2.27E-4, 2.34E-4, 2.38E-4, 2.45E-4, 2.5E-4, 2.57E-4 MPDATA,KXX

,19,, 2.62E-4, 2.69E-4 MPDATA,C ,19,,0.108,0.109, 0.111,0.113,0.114,0.116, MPDATA,C ,19,,0.116,0.118,0.118,0.120,0.121,0.123, MPDATA,C ,19,,0.123,0.125 MP, DENS,19, 0.300 MP, NUXY,19, 0.29! Mat 20: Alloy 82/182 MPDATA,EX

,20,, 31e6, 30.8e6, 30.5e6, 30.2e6, 30e6, 29.8e6 MPDATA,EX

,20,, 29.7e6, 29.5e6, 29.3e6, 29e6, 28.9e6, 28.7e6 MPDATA,EX

,20,, 28.5e6, 28.2e6 MPDATA,ALPX,20,, 6.8E-6, 6.9E-6, 7E-6, 7.1E-6, 7.2E-6, 7.3E-6 MPDATA,ALPX,20,, 7.4E-6, 7.5E-6, 7.6E-6, 7.6E-6, 7.7E-6, 7.8E-6 MPDATA,ALPX,20,, 7.8E-6, 7.9E-6 MPDATA,KXX

,20,, 1.99E-4, 2.01E-4, 2.06E-4, 2.1 1E-4, 2.15E-4, 2.22E-4 MPDATA,KXX

,20,, 2.27E-4, 2.34E-4, 2.38E-4, 2.45E-4, 2.5E-4, 2.57E-4 MPDATA,KXX

,20,, 2.62E-4, 2.69E-4 MPDATA,C ,20,,0.108,0.109,0.111,0.113,0.114,0.116, MPDATA,C ,20,,0.116,0.118,0.118,0.120, 0.121, 0.123, MPDATA,C ,20,,0.123,0.125 MP, DENS,20, 0.300 MP, NUXY,20, 0.29! Mat 21: ER308L (assumed SA-240-304L (18Cr-SNi))

MPDATA,EX

,21,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX , 21,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX

,21,, 25.1e6, 24.8e6 MPDATA,ALPX, 21,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 21,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 21,, 9.9E-6, 1OE-6 MPDATA,KXX, 21,, 1.99E-4, 2.O1E-4, 2.08E-4, 2.15E-4, 2.22E-4, 2.27E-4 MPDATA,KXX, 21,, 2.34E-4, 2.41E-4, 2.45E-4, 2.52E-4, 2.57E-4, 2.62E-4 MPDATA,KXX, 21,, 2.69E-4, 2.73E-4 MPDATA,C ,21,, 0.116, 0.117, 0.12, 0.122, 0.124, 0.125, MPDATA,C ,21,, 0.127, 0.129, 0.13, 0.131, 0.132, 0.133, MPDATA,C ,21,, 0.134, 0.135 MP, DENS, 21, 0.283 MP, NUXY, 21, 0.3! MAT 22: SS Type 316 (assumed as SA-376, Type 316 (l6Cr-l2Ni-2Mo)

MPDATA,EX , 22,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 22,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 22,, 25.1e6, 24.8e6 File No.: 0800368.301 Page A8 of A27 Revision:

0 F0306-O1RO Structural Integrity Associates, Inc.MPDATA,ALPX, 22,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 22,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 22,, 9.9E-6, 1OE-6 MPDATA,KXX, 22,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.1 1E-4, 2.15E-4 MPDATA,KXX, 22,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 22,, 2.52E-4, 2.59E-4 MPDATA,C, 22,, 0.121, 0.121, 0.124, 0.124, 0.127, 0.127, MPDATA,C, 22,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C, 22,, 0.133, 0.135 MP, DENS, 22, 0.283 MP, NUXY, 22, 0.3! MAT 23: A-336, Grade F8M (assumed similar to SA-430 FP316 (16Cr-12Ni-2Mo))

MPDATA,EX, 23,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 23,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 23,, 25.1e6, 24.8e6 MPDATA,ALPX, 23,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 23,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 23,, 9.9E-6, IOE-6 MPDATA,KXX, 23,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 23,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 23,, 2.52E-4, 2.59E-4 MPDATA,C, 23,, 0.121, 0.121, 0.124, 0.124, 0.127, 0.127, MPDATA,C, 23,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C, 23,, 0.133, 0.135 MP, DENS, 23, 0.283 MP, NUXY, 23, 0.3! MAT 24: A-182 F 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 24,, 28.3e6, 28.1e6, 27.9e6, 27.6e6, 27.3e6, 27e6 MPDATA,EX, 24,, 26.8e6, 26.5e6, 26.2e6, 25.8e6, 25.6e6, 25.3e6 MPDATA,EX, 24,, 25.1 e6, 24.8e6 MPDATA,ALPX, 24,, 8.5E-6, 8.6E-6, 8.8E-6, 8.9E-6, 9.1E-6, 9.2E-6 MPDATA,ALPX, 24,, 9.3E-6, 9.5E-6, 9.6E-6, 9.7E-6, 9.8E-6, 9.8E-6 MPDATA,ALPX, 24,, 9.9E-6, 1OE-6 MPDATA,KXX, 24,, 1.9E-4, 1.92E-4, 1.99E-4, 2.04E-4, 2.11E-4, 2.15E-4 MPDATA,KXX, 24,, 2.2E-4, 2.27E-4, 2.31E-4, 2.36E-4, 2.43E-4, 2.48E-4 MPDATA,KXX, 24,, 2.52E-4, 2.59E-4 MPDATA,C, 24,, 0.121, 0.121, 0.124, 0.124, 0.127, 0.127, MPDATA,C , 24,, 0.128, 0.129, 0.13, 0.13, 0.133, 0.133, MPDATA,C , 24,, 0.133, 0.135 MP, DENS, 24, 0.283 MP, NUXY, 24, 0.3 File No.: 0800368.301 Page A9 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.MPropMISO_NLinearDB.INP

/COM, Material Properties for Residual Stress Analyses MAT 1: Nozzle Forging -RCP Inlet/Suction, Discharge A-351, Grade CF8M (16Cr-12Ni-2Mo)

MAT 2: Nozzle Forging -RCP Cold Leg Drain SA-105 Grade 2 (Carbon Steel, C>0.3%)MAT 3: Nozzle Forging -Core Flood Nozzle SA-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

MAT 4: Nozzle-to-Safe End Weld -Core Flood Alloy 82/182 MAT 5: Safe End -RCP Discharge A-376, Type 316 (16Cr- 12Ni-2Mo)MAT 6: Safe End -Core Flood Nozzle A-336, Grade F8M (assumed similar to SA-430 FP316 (16Cr-12Ni-2Mo))

MAT 7: Pipe Internal Clad -RCP Inlet/Suction, Discharge, cold leg clad SA-240-304L (18Cr-8Ni)

MAT 8: Nozzle Internal Clad -RCP Cold Leg Drain, Core Flood SA-371 ER308L (assumed SA-240-304L (I 8Cr-8Ni))MAT 9: ID Weld Repair Alloy 82/182 MAT 10: Safe End-to-Pipe Weld -RCP Discharge Alloy 82/182 MAT 11: Safe End-to-Pipe Weld -Core Flood SS Type 316 (assumed similar to SA-376 TP316 (16Cr-12Ni-2Mo))

MAT 12: Attached Pipe/Elbow

-RCP Inlet/Suction, Discharge A-516 Grade 70 (Carbon Steel, (<=4" C < 0.3%))MAT 13: Attached Pipe/Elbow

-RCP Cold Leg Drain SA-403 WP316 (16Cr-12Ni-2Mo)

MAT 14: Attached Pipe/Elbow

-Core Flood Nozzle SA-376, Type 316 (16Cr-12Ni-2Mo)

I MAT 15: Cold Leg Pipe -RCP Cold Leg Drain A-106 Grade C (C>0.3%)MAT 16: Core Flood Vessel Shell A-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

MAT 17: Core Flood Vessel Clad SS Clad (assumed SA-240 304L (18Cr-8Ni))

MAT 18: Weld Overlay Alloy 52M MAT 19: Nozzle to Pipe Weld -RCP Inlet/Suction, RCP Cold Leg Drain Alloy 82/182 MAT 20: Butter material Alloy 82/182 MAT 21: Buffer Layer ER308L (assumed SA-240-304L (18Cr-8Ni))

MAT 22: RCP Discharge Nozzle-to-SE Weld, Spray Nozzle and Pressure Tap welds to RCP Discharge SE SS Type 316 (assume(TP316 (16Cr-12Ni-2Mo))

MAT 23: Pressure Tap -Discharge Nozzle A-336, Grade F8M (assumed similar to SA-430 FP316 (16Cr-12Ni-2Mo))

MAT 24: Spray Nozzle -Discharge Nozzle A- 182 F 316 (16Cr- 12Ni-2Mo)d similar to SA-376 MPTEMP, 1, 70,500,700,1100,1500,2500 cv = 60* 12 !Convert hour-foot to minute-inch

! MAT 1: A-351, Grade CF8M (16Cr-12Ni-2Mo)

MPDATA,EX, 1,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX, 1, , 8.5E-6, 9.7E-6,10.0E-6,10.5E-6,10.8E-6, I 1.5E-6 MPDATA,KXX, 1, , 8.2/cv, 10.2/cv, 11.2/cv, 13.0/cv, 14.7/cv, 19.0/cv MPDATA,C, 1,, 0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 1,0.283 MP,NUXY, 1,0.300! MAT 2: SA-105 Grade 2 (Hi Carbon)MPDATA,EX, 2,, 29.3E6, 27.1E6, 25.3E6, 17.9E6, 8.0E6, 0.1E6 MPDATA,ALPX, 2,, 6.4E-6, 7.3E-6, 7.6E-6, 8.2E-6, 8.6E-6, 9.5E-6 MPDATA,KXX, 2,, 35.1/cv,29.5/cv,26.6/cv,20.9/cv,15.7/cv, 1.0/cv MPDATA,C, 2,, 0.103, 0.128, 0.138, 0.171, 0.198, 0.204 MP,DENS, 2,0.283 MP,NUXY, 2,0.300! MAT 3: SA-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

MPDATA,EX, 3,, 27.8E6, 25.7E6, 24.6E6, 21.5E6, 16.0E6, 0.1E6 MPDATA,ALPX, 3,, 6.4E-6, 7.3E-6, 7.6E-6, 8.2E-6, 8.6E-6, 9.5E-6 MPDATA,KXX, 3,, 23.5/cv,22.7/cv,21.6/cv,19.0/cv,15.1/cv, 5.0/cv MPDATA,C, 3,, 0.105, 0.130, 0.140, 0.173, 0.154, 0.204 MP,DENS, 3,0.283 MP,NUXrY, 3,0.300 MAT 4: Alloy 82/182 MPDATA,EX, 4,, 31.0E6, 29.0E6, 28.2E6, 25.9E6, 23.1E6, 0.1E6 MPDATA,ALPX,4,, 6.8E-6, 7.6E-6, 7.9E-6, 8.4E-6, 9.OE-6,10.OE-6 File No.: 0800368.301 Revision:

0 Page A10 of A27 F0306-OIRO V Structural Integrity Associates, Inc.MPDATA,KXX, 4,, 8.6/cv,l0.6/cv,11.6/cv,13.8/cv,16.0/cv,22.0/cv MPDATA,C, 4,, 0.108, 0.120, 0.125, 0.139, 0.148, 0.177 MP,DENS, 4,0.300 MP,NUXY, *4,0.290! MAT 5: A-376, Type 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 5,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,5,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 5,, 8.2/cv,10.2/cv, 1 .2/cv,13.0/cv,14.7/cv,19.0/cv MPDATA,C, 5,, 0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 5,0.283 MP,NUXY, 5,0.300! MAT 6: A-336, Grade F8M (assumed similar to SA-430 FP316 (16Cr-12Ni-2Mo))

MPDATA,EX, 6,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,6,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 6,, 8.2/cv,10.2/cv,I 1.2/cv,13.0/cv,14.7/cv,19.0/cv MPDATA,C, 6,,0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 6,0.283 MP,NUXY, 6,0.300! MAT 7: SA-240-304L (18Cr-8Ni)

MPDATA,EX, 7,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,7,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 7,, 8.6/cv,10.9/cv,1 1 .8/cv,13.6/cv,15.3/ev,21.0/cv MPDATA,C, 7,, 0.116, 0.131, 0.135, 0.140, 0.145, 0.159 MP,DENS, 7,0.283 MP,NUXY, 7,0.300! MAT 8: SA-371 ER308L (assumed SA-240-304L (I8Cr-8Ni))

MPDATA,EX, 8,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,8,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 8,, 8.6/cv,10.9/cv, 11.8/cv,13.6/ev,15.3/cv,21.0/cv MPDATA,C, 8,, 0.116, 0.131, 0.135, 0.140, 0.145, 0.159 MP,DENS, 8,0.283 MP,NUXY, 8,0.300! MAT 9: Alloy 82/182 MPDATA,EX, 9,, 31.0E6, 29.0E6, 28.2E6, 25.9E6, 23.1E6, 0.1E6 MPDATA,ALPX,9,, 6.8E-6, 7.6E-6, 7.9E-6, 8.4E-6, 9.OE-6,10.OE-6 MPDATA,KXX, 9,, 8.6/cv,10.6/cv,11

.6/cv,13.8/cv,16.0/cv,22.0/cv MPDATA,C, 9,,0.108, 0.120, 0.125, 0.139, 0.148, 0.177 MP,DENS, 9,0.300 MP,NUXY, 9,0.290! MAT 10: Alloy 82/182 MPDATA,EX, 10,, 31.0E6, 29.0E6, 28.2E6, 25.9E6, 23.1E6, 0.1E6 MPDATA,ALPX,10,, 6.8E-6, 7.6E-6, 7.9E-6, 8.4E-6, 9.OE-6,10.OE-6 MPDATA,KXX, 10,, 8.6/cv,10.6/cv, 11.6/cv,13.8/cv,16.0/cv,22.0/cv MPDATA,C, 10,,0.108, 0.120, 0.125, 0.139, 0.148, 0.177 MP,DENS, 10,0.300 MP,NUXY, 10,0.290! MAT 11: SS Type 316 (assumed as SA-376, Type 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 11,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,1 1,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 11,, 8.2/cv, 10.2/cv, 11 .2/cv,13.0/cv,14.7/cv,19.0/cv MPDATA,C, 11,, 0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 11,0.283 MP,NUXY, 11,0.300! Mat 12: A-516 Grade 70 (Carbon Steel, (<=4" C<0.3%))MPDATA,EX, 12,, 29.5E6, 27.3E6, 25.5E6, 18.0E6, 5.0E6, 0.1E6 MPDATA,ALPX, 12,, 6.4E-6, 7.3E-6, 7.6E-6, 8.2E-6, 8.6E-6, 9.5E-6 MPDATA,KXX, 12,, 35.1/cv,29.5/cv,26.6/cv,20.9/cv,15.7/cv, 1.0/cv MPDATA,C, 12,, 0.103, 0.128, 0.138, 0.171, 0.198, 0.204 MP,DENS, 12,0.283 File No.: 0800368.301 Page A11 of A27 Revision:

0 F0306-01RO V Structural Integrity Associates, Inc.MP,NUXY, 12,0.300! Mat 13: SA-403 WP 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 13,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,13,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 13,, 8.2/cv,10.2/cv, 1 1.2/cv,13.0/cv,14.7/cv,19.0/cv MPDATA,C, 13,,0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 13,0.283 MP,NUXY, 13,0.300! Mat 14: SA-376, Type 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 14,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,14,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 14,, 8.2/cv,10.2/cv, 11.2/cv,13.0/cv,14.7/cv,l9.0/cv MPDATA,C, 14,,0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 14,0.283 MP,NUXY, 14,0.300! Mat 15: A-106 Grade C (C>0.3%)MPDATA,EX, 15,, 29.3E6, 27.1E6, 25.3E6, 17.9E6, 8.0E6, 0.1E6 MPDATA,ALPX, 15,, 6.4E-6, 7.3E-6, 7.6E-6, 8.2E-6, 8.6E-6, 9.5E-6 MPDATA,KXX, 15,, 35.1/cv,29.5/cv,26.6/cv,20.9/cv,15.7/cv, 1.0/cv MPDATA,C, 15,,0.103, 0.128, 0.138, 0.171, 0.198, 0.204 MP,DENS, 15,0.283 MP,NUXY, 15,0.300! Mat 16: A-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

MPDATA,EX, 16,, 27.8E6, 25.7E6, 24.6E6, 21.5E6, 16.0E6, 0.1E6 MPDATA,ALPX, 16,, 6.4E-6, 7.3E-6, 7.6E-6, 8.2E-6, 8.6E-6, 9.5E-6 MPDATA,KXX, 16,, 23.5/cv,22.7/cv,21.6/cv,19.0/cv,15.1/cv, 5.0/cv MPDATA,C, 16,,0.105, 0.130, 0.140, 0.173, 0.154, 0.204 MP,DENS, 16,0.283 MP,NUXY, 16,0.300! Mat 17: SA-371 ER308L (assumed SA-240-304L (18Cr-8Ni))

MPDATA,EX, 17,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,17,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 17,, 8.6/cv, 10.9/cv,11.8/cv,13.6/cv,15.3/cv,21.0/cv MPDATA,C, 17,,0.116, 0.131, 0.135, 0.140, 0.145, 0.159 MP,DENS, 17,0.283 MP,NUXY, 17,0.300! Mat 18: Alloy 690 for Alloy 52M MPDATA,EX, 18,, 30.3E6, 28.3E6, 27.6E6, 25.3E6, 22.6E6, 0.1E6 MPDATA,ALPX,18,, 7.7E-6, 8.1E-6, 8.3E-6, 8.5E-6, 8.8E-6, 9.5E-6 MPDATA,KXX, 18,, 6.8/cv, 9.4/cv,10.6/cv,13.

1/cv,15.5/cv,22.0/cv MPDATA,C, 18,,0.107, 0.121, 0.125, 0.135, 0.147, 0.167 MP,DENS, 18,0.293 MP,NUXY, 18,0.290! Mat 19: Alloy 82/182 MPDATA,EX, 19,, 31.0E6, 29.0E6, 28.2E6, 25.9E6, 23.1E6, 0.1E6 MPDATA,ALPX,19,, 6.8E-6, 7.6E-6, 7.9E-6, 8.4E-6, 9.OE-6,10.OE-6 MPDATA,KXX, 19,, 8.6/ev, 10.6/cv,11.6/cv,13.8/cv,16.0/cv,22.0/cv MPDATA,C, 19,, 0.108, 0.120, 0.125, 0.139, 0.148, 0.177 MP,DENS, 19,0.300 MP,NUXY, 19,0.290! Mat 20: Alloy 82/182 MPDATA,EX, 20,, 31.0E6, 29.0E6, 28.2E6, 25.9E6, 23.1E6, 0.1E6 MPDATA,ALPX,20,, 6.8E-6, 7.6E-6, 7.9E-6, 8.4E-6, 9.OE-6,10.OE-6 MPDATA,KXX, 20,, 8.6/cv, 10.6/cv, 1 1.6/cv, 13.8/cv, 16.0/cv,22.0/cv MPDATA,C, 20,,0.108, 0.120, 0.125, 0.139, 0.148, 0.177 MP,DENS, 20,0.300 MP,NUXY, 20,0.290! MAT 21: ER308L (assumed SA-240-304L (18Cr-8Ni))

MPDATA,EX, 21,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,21,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 File No.: 0800368.301 Page A12 of A27 Revision:

0 F0306-01RO V Structural Integrity Associates, Inc.MPDATA,KXX, 21,, 8.6/cv, 10.9/cv,1 1.8/cv,13.6/cv, 15.3/cv,21.0/cv MPDATA,C, 21,,0.116, 0.131, 0.135, 0.140, 0.145, 0.159 MP,DENS, 21,0.283 MP,NUXY, 21,0.300! MAT 22: SS Type 316 (assumed as SA-376, Type 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 22,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,22,, 8.5E-6, 9.7E-6,10.0E-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 22,, 8.2/ev, 10.2/cv, 11.2/cv,13.0/cv,14.7/cv, 19.0/cv MPDATA,C, 22,,0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 22,0.283 MP,NUXY, 22,0.300! MAT 23: A-336, Grade F8M (assumed similar to SA-430 FP316 (16Cr-12Ni-2Mo))

MPDATA,EX, 23,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,23,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 23,, 8.2/cv, 10.2/cv, 11.2/cv,13.0/cv,14.7/cv, 19.0/cv MPDATA,C, 23,, 0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 23,0.283 MP,NUXY, 23,0.300! MAT 24: A-182 F 316 (16Cr-12Ni-2Mo)

MPDATA,EX, 24,, 28.3E6, 25.8E6, 24.8E6, 22.1E6, 18.1E6, 0.1E6 MPDATA,ALPX,24,, 8.5E-6, 9.7E-6,10.OE-6,10.5E-6,10.8E-6,11.5E-6 MPDATA,KXX, 24,, 8.2/cv,10.2/cv, 11.2/cv,13.0/cv,14.7/cv,19.0/cv MPDATA,C, 24,,0.121, 0.130, 0.135, 0.141, 0.145, 0.155 MP,DENS, 24,0.283 MP,NUXY, 24,0.300***********

    • ****** *** *** *** *** **** ** *** ** **********
    • *******/COM, Multilinear Isotropic Properties MAT 1: A-351, Grade CF8M (16Cr-12Ni-2Mo)

TB,MISO,1,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0.13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0. 14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,1 11000 TBTEMP,700 TBPT,,0.00 115726,28700 TBPT,,0.04713410,48775 TBPT,,0.12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP,I 100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0. 17394654,68000 TBPT,,0.33574811,83000 TBTEMP,1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0. 16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.0 1000000,1000 TBPT,,0.25436656,2000 File No.: 0800368.301 Page A13 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 2: SA-105 Grade 2 (Hi Carbon)TB,MISO,2,6,5 TBTEMP,70 TBPT,,0.00122867,36000 TBPT,,0.01893525,49500 TBPT,,0.05297164,63000 TBPT,,0. 12392872,76500 TBPT,,0.25439221,90000 TBTEMP,500 TBPT,,0.00108118,29300 TBPT,,0.01229602,44475 TBPT,,0.04191157,59650 TBPT,,0.11241880,74825 TBPT,,0.25418036,90000 TBTEMP,700 TBPT,,0.00101976,25800 TBPT,,0.00975556,41850 TBPT,,0.03699139,57900 TBPT,,0. 10680945,73950 TBPT,,0.25407809,90000 TBTEMP, 1100 TBPT,,0.00106145,19000 TBPT,,0.09176400,25750 TBPT,,0.17082863,32500 TBPT,,0.28305377,39250 TBPT,,0.43306968,46000 TBTEMP, 1500 TBPT,,0.00 150000,12000 TBPT,,0.24664089,15000 TBPT,,0.3 5451397,18000 TBPT,,0.48186660,2 1000 TBPT,,0.62868946,24000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000 MAT 3: SA-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

TB,MISO,3,6,5 TBTEMP,70 TBPT,,0.00179856,50000 TBPT,,0.00653691,60250 TBPT,,0.01833861,70500 TBPT,,0.05088838,80750 TBPT,,0.13083992,91000 TBTEMP,500 TBPT,,0.00168093,43200 TBPT,,0.00425816,55150 TBPT,,0.01312261,67100 TBPT,,0.04326163,79050 TBPT,,0.13069290,91000 TBTEMP,700 TBPT,,0.00165447,40700 TBPT,,0.00375477,53275 TBPT,,0.01167549,65850 TBPT,,0.04078828,78425 TBPT,,0.13065390,91000 TBTEMP, 1100 TBPT,,0.001 11628,24000 TBPT,,0.01290523,36000 TBPT,,0.04300007,48000 TBPT,,0.11360829,60000 TBPT,,0.25422138,72000 File No.: 0800368.301 Page A14 of A27 Revision:

0 F0306-01RO Structural Integrity Associates, Inc.TBTEMP,1500 TBPT,,0.00043750,7000 TBPT,,0.02891253,17750 TBPT,,0.10122020,28500 TBPT,,0.23776149,39250 TBPT,,0.45454186,50000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 4: Alloy 82/182 TB,MISO,4,6,5 TBTEMP,70 TBPT,,0.00175806,54500 TBPT,,0.06261424,77125 TBPT,,0.13236682,99750 TBPT,,0.24105550,122375 TBPT,,0.39724103,145000 TBTEMP,500 TBPT,,0.00163793,47500 TBPT,,0.06087695,67625 TBPT,,0.13000821,87750 TBPT,,0.23828025,107875 TBPT,,0.39439449,128000 TBTEMP,700 TBPT,,0.00165957,46800 TBPT,,0.06227835,66350 TBPT,,0. 13214714,85900 TBPT,,0.24120331,105450 TBPT,,0.39809217,125000 TBTEMP, 1100 TBPT,,0.00173745,45000 TBPT,,0.06880255,62250 TBPT,,0.14043334,79500 TBPT,,0.24996336,96750 TBPT,,0.40536485,114000 TBTEMP, 1500 TBPT,,0.00129004,29800 TBPT,,0.18149804,41100 TBPT,,0.29961162,52400 TBPT,,0.44846834,63700 TBPT,,0.62851140,75000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 5: A-376, Type 316 (l6Cr-l2Ni-2Mo)

TB,MISO,5,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0.13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0. 14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,111000 TBTEMP,700 TBPT,,0.001 15726,28700 TBPT,,0.04713410,48775 File No.: 0800368.301 Revision:

0 Page A15 of A27 F0306-OIRO V Structural Integrity Associates, Inc.TBPT,,0. 12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP, 1100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0. 17394654,68000 TBPT,,0.33574811,83000 TBTEMP,1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0.16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 6: A-336, Grade F8M (assumed similar to SA-430 FP316 (16Cr-12Ni-2Mo))

TB,MISO,6,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0.13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0. 14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,111000 TBTEMP,700 TBPT,,0.00 115726,28700 TBPT,,0.04713410,48775 TBPT,,0. 12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP, 1100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0. 17394654,68000 TBPT,,0.33574811,83000 TBTEMP,1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0.16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.0 1000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 7: SA-240-304L (18Cr-8Ni)

TB,MISO,7,6,5 TBTEMP,70 TBPT,,0.00123675,35000 TBPT,,0.07774887,64750 TBPT,,0.1 8214087,94500 TBPT,,0.33827321,124250 TBPT,,0.55033453,154000 File No.: 0800368.301 Page A16 of A27 Revision:

0 F0306-O1RO Structural Integrity Associates, Inc.TBTEMP,500 TBPT,,0.00085271,22000 TBPT,,0.03589114,42750 TBPT,,0. 10594921,63500 TBPT,,0.23140905,84250 TBPT,,0.42629537,105000 TBTEMP,700 TBPT,,0.00080645,20000 TBPT,,0.02810960,40000 TBPT,,0.09083667,60000 TBPT,,0.21112697,80000 TBPT,,0.40756128, 100000 TBTEMP, 1100 TBPT,,0.00074208,16400 TBPT,,0.0 13 83547,30050 TBPT,,0.05190777,43700 TBPT,,0.13922645,573 50 TBPT,,0.30447287,7 1000 TBTEMP,1500 TBPT,,0.00071823,13000 TBPT,,0.06529820,18250 TBPT,,0. 13548971,23500 TBPT,,0.24290793,28750 TBPT,,0.39505954,34000 TBTEMP,2500 TBPT,,0.0 1000000, 1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 8: SA-371 ER308L (assumed SA-240-304L (18Cr-8Ni))

TB,MISO,8,6,5 TBTEMP,70 TBPT,,0.00123675,35000 TBPT,,0.07774887,64750 TBPT,,0.18214087,94500 TBPT,,0.33827321,124250 TBPT,,0.55033453,154000 TBTEMP,500 TBPT,,0.00085271,22000 TBPT,,0.03589114,42750 TBPT,,0.10594921,63500 TBPT,,0.23140905,84250 TBPT,,0.42629537,105000 TBTEMP,700 TBPT,,0.00080645,20000 TBPT,,0.02810960,40000 TBPT,,0.09083667,60000 TBPT,,0.21112697,80000 TBPT,,0.40756128,100000 TBTEMP,1100 TBPT,,0.00074208,16400 TBPT,,0.01383547,30050 TBPT,,0.05190777,43700 TBPT,,0.13922645,57350 TBPT,,0.30447287,71000 TBTEMP,1500 TBPT,,0.00071823,13000 TBPT,,0.06529820,18250 TBPT,,0.13548971,23500 TBPT,,0.24290793,28750 TBPT,,0.39505954,34000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000 File No.: 0800368.301 Page A17 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.! MAT 9: Alloy 82/182 TB,MISO,9,6,5 TBTEMP,70 TBPT,,0.00175806,54500 TBPT,,0.06261424,77125 TBPT,,0.13236682,99750 TBPT,,0.24105550,122375 TBPT,,0.39724103,145000 TBTEMP,500 TBPT,,0.00163793,47500 TBPT,,0.06087695,67625 TBPT,,0.13000821,87750 TBPT,,0.23828025,107875 TBPT,,0.39439449,128000 TBTEMP,700 TBPT,,0.00165957,46800 TBPT,,0.06227835,66350 TBPT,,0.13214714,85900 TBPT,,0.24120331,105450 TBPT,,0.39809217,125000 TBTEMP,1 100 TBPT,,0.00173745,45000 TBPT,,0.06880255,62250 TBPT,,0.14043334,79500 TBPT,,0.24996336,96750 TBPT,,0.40536485,114000 TBTEMP,1500 TBPT,,0.00129004,29800 TBPT,,0.18149804,41100 TBPT,,0.29961162,52400 TBPT,,0.44846834,63700 TBPT,,0.62851140,75000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 10: Alloy 82/182 TB,MISO, 10,6,5 TBTEMP,70 TBPT,,0.00175806,54500 TBPT,,0.06261424,77125 TBPT,,0. 1323 6682,99750 TBPT,,0.24105550,122375 TBPT,,0.39724103,145000 TBTEMP,500 TBPT,,0.00163793,47500 TBPT,,0.06087695,67625 TBPT,,0. 13000821,87750 TBPT,,0.23828025,107875 TBPT,,0.39439449,128000 TBTEMP,700 TBPT,,0.00165957,46800 TBPT,,0.06227835,66350 TBPT,,0. 13214714,85900 TBPT,,0.24120331,105450 TBPT,,0.39809217,125000 TBTEMP, 1100 TBPT,,0.00173745,45000 TBPT,,0.06880255,62250 TBPT,,0.14043334,79500 TBPT,,0.24996336,96750 TBPT,,0.40536485,114000 TBTEMP, 1500 TBPT,,0.00 129004,298 00 TBPT,,0.18149804,41100 File No.: 0800368.301 Page Al8 of A27 Revision:

0 F0306-01RO V Structural Integrity Associates, Inc.TBPT,,0.29961162,52400 TBPT,,0.44846834,63700 TBPT,,0.62851140,75000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 11: SS Type 316 (assumed as SA-376, Type 316 (l6Cr-l2Ni-2Mo)

TB,MISO, 11,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0.13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0. 14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,1 11000 TBTEMP,700 TBPT,,0.001 15726,28700 TBPT,,0.04713410,48775 TBPT,,0.12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP, 1100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0. 173 94654,68000 TBPT,,0.33574811,83000 TBTEMP,1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0. 163 27215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.0 1000000, 1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! Mat 12: A-516 Grade 70 (Carbon Steel, (<=4" C<0.3%)TB,MISO, 12,6,5 TBTEMP,70 TBPT,,0.00128814,38000 TBPT,,0.00318094,48250 TBPT,,0.01044011,58500 TBPT,,0.03748028,68750 TBPT,,0. 12248521,79000 TBTEMP,500 TBPT,,0.00 113553,31000 TBPT,,0.00213243,43000 TBPT,,0.00690500,55000 TBPT,,0.03035742,67000 TBPT,,0. 12229910,79000 TBTEMP,700 TBPT,,0.00106667,27200 TBPT,,0.00187807,40150 TBPT,,0.00565952,53 100 TBPT,,0.02712894,66050 TBPT,,0. 12220785,79000 File No.: 0800368.301 Page A19 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.TBTEMP, 1100 TBPT,,0.00 116667,21000 TBPT,,0.09174106,27000 TBPT,,0. 16567172,33000 TBPT,,0.27134322,39000 TBPT,,0.41435243,45000 TBTEMP,1500 TBPT,,0.00300000,15000 TBPT,,0.25584461,18750 TBPT,,0.36731136,22500 TBPT,,0.49884093,26250 TBPT,,0.65042369,30000 TBTEMP,2500 TBPT,,0.0 1000000, 1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000 Mat 13: SA-403 WP 316 (16Cr-12Ni-2Mo)

TB,MISO,13,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0. 1300043 0,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0. 14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,1 11000 TBTEMP,700 TBPT,,0.00l 15726,28700 TBPT,,0.04713410,48775 TBPT,,0.12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP, 1100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0. 17394654,68000 TBPT,,0.33574811,83000 TBTEMP, 1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0. 16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.0 1000000, 1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! Mat 14: SA-376, Type 316 (16Cr-12Ni-2Mo)

TB,MISO, 14,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0. 13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 File No.: 0800368.301 Page A20 of A27 Revision:

0 F0306-01RO V Structural Integrity Associates, Inc.TBPT,,0.14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,111000 TBTEMP,700 TBPT,,0.00 115726,28700 TBPT,,0.04713410,48775 TBPT,,0.12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP,I 100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0.17394654,68000 TBPT,,0.33574811,83000 TBTEMP,1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0. 16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.0 1000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! Mat 15: A-106 Grade C (C>0.3%)TB,MISO, 15,6,5 TBTEMP,70 TBPT,,0.00136519,40000 TBPT,,0.02425642,52500 TBPT,,0.06072018,65000 TBPT,,0. 13132092,77500 TBPT,,0.25456366,90000 TBTEMP,500 TBPT,,0.00120295,32600 TBPT,,0.0 1532231,46950 TBPT,,0.04716487,61300 TBPT,,O. 11804259,75650 TBPT,,0.25433308,90000 TBTEMP,700 TBPT,,0.001 13043,28600 TBPT,,0.01183181,43950 TBPT,,0.04098994,59300 TBPT,,O. 11137719,74650 TBPT,,0.25421675,90000 TBTEMP, 1100 TBPT,,0.00122905,22000 TBPT,,0.11479271,28000 TBPT,,0. 19283680,34000 TBPT,,0.29793227,40000 TBPT,,0.43330045,46000 TBTEMP,1500 TBPT,,0.00025000,2000 TBPT,,0.16947088,2875 TBPT,,0.28794548,3750 TBPT,,0.43757830,4625 TBPT,,0.61834898,5500 TBTEMP,2500 TBPT,,0.0 1000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000 Mat 16: A-508 Class 2 (3/4Ni-1/2Mo-1/3Cr-V)

TB,MISO, 16,6,5 File No.: 0800368.301 Page A21 of A27 Revision:

0 F0306-01RO V Structural Integrity Associates, Inc.TBTEMP,70 TBPT,,0.00179856,50000 TBPT,,0.00653691,60250 TBPT,,0.01833861,70500 TBPT,,0.05088838,80750 TBPT,,0.13083992,9 1000 TBTEMP,500 TBPT,,0.00168093,43200 TBPT,,0.00425816,55150 TBPT,,0.0 1312261,67100 TBPT,,0.04326163,79050 TBPT,,0.13069290,9 1000 TBTEMP,700 TBPT,,0.00165447,40700 TBPT,,0.00375477,53275 TBPT,,0.01 167549,65850 TBPT,,0.04078828,78425 TBPT,,O. 13065390,9 1000 TBTEMP, 1100 TBPT,,0.001 11628,24000 TBPT,,0.0 1290523,36000 TBPT,,0.04300007,48000 TBPT,,0. 11360829,60000 TBPT,,0.25422138,72000 TBTEMP,1500 TBPT,,0.00043750,7000 TBPT,,0.02891253,17750 TBPT,,0. 10 122020,28500 TBPT,,0.23776149,39250 TBPT,,0.45454186,50000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! Mat 17: SA-371 ER308L (assumed SA-240-304L (18Cr-8Ni))

TB,MISO, 17,6,5 TBTEMP,70 TBPT,,0.00123675,35000 TBPT,,0.07774887,64750 TBPT,,0.18214087,94500 TBPT,,0.33827321,124250 TBPT,,0.55033453,154000 TBTEMP,500 TBPT,,0.00085271,22000 TBPT,,0.03589114,42750 TBPT,,0. 10594921,63500 TBPT,,0.23140905,84250 TBPT,,0.42629537,105000 TBTEMP,700 TBPT,,0.00080645,20000 TBPT,,0.02810960,40000 TBPT,,0.09083667,60000 TBPT,,0.21112697,80000 TBPT,,0.40756128, 100000 TBTEMP, 1100 TBPT,,0.00074208,16400 TBPT,,0.0 1383547,30050 TBPT,,0.05190777,43700 TBPT,,0. 13922645,573 50 TBPT,,0.30447287,7 1000 TBTEMP,1500 TBPT,,0.00071823,13000 TBPT,,0.06529820,18250 TBPT,,0.13548971,23500 TBPT,,0.24290793,28750 TBPT,,0.39505954,34000 File No.: 0800368.301 Page A22 of A27 Revision:

0 F0306-O IRO V Structural Integrity Associates, Inc.TBTEMP,2500 TBPT,,0.0 1000000, 1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! Mat 18: Alloy 690 for Alloy 52M TB,MISO,18,6,5 TBTEMP,70 TBPT,,0.00160726,48700 TBPT,,0.06305922,75275 TBPT,,0. 14216441,101850 TBPT,,0.26637521,128425 TBPT,,0.44418534,155000 TBTEMP,500 TBPT,,0.00128975,36500 TBPT,,0.03965509,59125 TBPT,,0.10337548,81750 TBPT,,0.21471146,104375 TBPT,,0.3 873 8296,127000 TBTEMP,700 TBPT,,0.00125000,34500 TBPT,,0.03540485,57125 TBPT,,0.09681837,79750 TBPT,,0.20767351,102375 TBPT,,0.38365967,125000 TBTEMP, 1100 TBPT,,0.00125296,31700 TBPT,,0.04930235,50775 TBPT,,0. 12020713,69850 TBPT,,0.23732894,88925 TBPT,,0.41123796,108000 TBTEMP,1500 TBPT,,0.00124336,28100 TBPT,,0.26183017,44075 TBPT,,0.43043443,60050 TBPT,,0.62896232,76025 TBPT,,0.85475925,92000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! Mat 19: Alloy 82/182 TB,MISO,19,6,5 TBTEMP,70 TBPT,,0.00175806,54500 TBPT,,0.06261424,77125 TBPT,,0.13236682,99750 TBPT,,0.24105550,122375 TBPT,,0.39724103,145000 TBTEMP,500 TBPT,,0.00163793,47500 TBPT,,0.06087695,67625 TBPT,,0.13000821,87750 TBPT,,0.23828025,107875 TBPT,,0.39439449,128000 TBTEMP,700 TBPT,,0.00165957,46800 TBPT,,0.06227835,66350 TBPT,,0. 13214714,85900 TBPT,,0.24120331,105450 TBPT,,0.39809217,125000 TBTEMP, 1100 TBPT,,0.00173745,45000 TBPT,,0.06880255,62250 File No.: 0800368.301 Page A23 of A27 Revision:

0 F0306-01RO V Structural Integrity Associates, Inc.TBPT,,0.14043334,79500 TBPT,,0.24996336,96750 TBPT,,0.40536485,114000 TBTEMP,1500 TBPT,,0.00129004,29800 TBPT,,0.18149804,41100 TBPT,,0.29961162,52400 TBPT,,0.44846834,63700 TBPT,,0.62851140,75000 TBTEMP,2500 TBPT,,0.0 1000000, 1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! Mat 20: Alloy 82/182 TB,MISO,20,6,5 TBTEMP,70 TBPT,,0.00175806,54500 TBPT,,0.06261424,77125 TBPT,,0. 13236682,99750 TBPT,,0.24105550,122375 TBPT,,0.39724103,145000 TBTEMP,500 TBPT,,0.00163793,47500 TBPT,,0.06087695,67625 TBPT,,0. 13000821,87750 TBPT,,0.23828025,107875 TBPT,,0.39439449,128000 TBTEMP,700 TBPT,,0.00165957,46800 TBPT,,0.06227835,66350 TBPT,,0.13214714,85900 TBPT,,0.24120331,105450 TBPT,,0.39809217,125000 TBTEMP,1 100 TBPT,,0.00173745,45000 TBPT,,0.06880255,62250 TBPT,,0. 14043334,79500 TBPT,,0.24996336,96750 TBPT,,0.40536485,114000 TBTEMP, 1500 TBPT,,0.00129004,29800 TBPT,,0.18149804,41100 TBPT,,0.29961162,52400 TBPT,,0.44846834,63700 TBPT,,0.62851140,75000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 21: ER 308L (assumed SA-240-304L (18Cr-8Ni))

TB,MISO,21,6,5 TBTEMP,70 TBPT,,0.00123675,35000 TBPT,,0.07774887,64750 TBPT,,0. 18214087,94500 TBPT,,0.33827321,124250 TBPT,,0.55033453,154000 TBTEMP,500 TBPT,,0.00085271,22000 TBPT,,0.03589114,42750 TBPT,,0.10594921,63500 File No.: 0800368.301 Page A24 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.TBPT,,0.23140905,84250 TBPT,,0.42629537,105000 TBTEMP,700 TBPT,,0.00080645,20000 TBPT,,0.02810960,40000 TBPT,,0.09083667,60000 TBPT,,0.21112697,80000 TBPT,,0.40756128, 100000 TBTEMP, 1100 TBPT,,0.00074208,16400 TBPT,,0.01383547,30050 TBPT,,0.05190777,43700 TBPT,,0. 13922645,57350 TBPT,,0.30447287,7 1000 TBTEMP,1500 TBPT,,0.00071823,13000 TBPT,,0.06529820,18250 TBPT,,0.13548971,23500 TBPT,,0.24290793,28750 TBPT,,0.39505954,34000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 22: SS Type 316 (assumed as SA-376, Type 316 (16Cr-12Ni-2Mo)

TB,MISO,22,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0. 13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0. 14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,111000 TBTEMP,700 TBPT,,0.001 15726,28700 TBPT,,0.04713410,48775 TBPT,,0.12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP, 1100 TBPT,,0.00104072,23 000 TBPT,,0.02629713,3 8000 TBPT,,0.07687375,53000 TBPT,,0. 17394654,68000 TBPT,,0.33574811,83000 TBTEMP, 1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0. 16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.01000000,1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 23: A-336, Grade F8M (assumed similar to SA-430 FP316 (l6Cr-l2Ni-2Mo))

TB,MISO,23,6,5 TBTEMP,70 File No.: 0800368.301 Page A25 of A27 Revision:

0 F0306-O1RO V Structural Integrity Associates, Inc.TBPT,,0.00149823,42400 TBPT,,0. 13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0. 14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,111000 TBTEMP,700 TBPT,,0.00115 726,28700 TBPT,,0.04713410,48775 TBPT,,0.12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP, 1100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0. 17394654,68000 TBPT,,0.33574811,83000 TBTEMP,1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0.16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 TBPT,,0.0 1000000, 1000 TBPT,,0.25436656,2000 TBPT,,0.46213394,3000 TBPT,,0.70703966,4000 TBPT,,0.98409152,5000

! MAT 24: A-182 F 316 (16Cr-12Ni-2Mo)

TB,MISO,24,6,5 TBTEMP,70 TBPT,,0.00149823,42400 TBPT,,0.13000430,69800 TBPT,,0.25461383,97200 TBPT,,0.42197259,124600 TBPT,,0.63258489,152000 TBTEMP,500 TBPT,,0.00127907,33000 TBPT,,0.06160812,52500 TBPT,,0.14218000,72000 TBPT,,0.26923098,91500 TBPT,,0.45116470,11 1000 TBTEMP,700 TBPT,,0.001 15726,28700 TBPT,,0.04713410,48775 TBPT,,0.12118403,68850 TBPT,,0.24571857,88925 TBPT,,0.43216804,109000 TBTEMP,1 100 TBPT,,0.00104072,23000 TBPT,,0.02629713,38000 TBPT,,0.07687375,53000 TBPT,,0. 17394654,68000 TBPT,,0.33574811,83000 TBTEMP, 1500 TBPT,,0.00066298,12000 TBPT,,0.03013522,17250 TBPT,,0.07723242,22500 TBPT,,0. 16327215,27750 TBPT,,0.30372152,33000 TBTEMP,2500 File No.: 0800368.301 Page A26 of A27 Revision:

0 F0306-O1RO Structural Integrity Associates, Inc.TBPT,,O.O 1000000, 1000 TBPT,,O.25436656,2000 TBPT,,O.46213394,3000 TBPT,,O.70703966,4000 TBPT,,O.98409152,5000 File No.: 0800368.301 Revision:

0 Page A27 of A27 F0306-O1RO

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