Text

Flaw Evaluation of Unit 2 Residual Heat Removal Suction Weld Joint
	ML17138B138
Person / Time
Site:	Diablo Canyon
Issue date:	05/18/2017
From:	Welsch J; Pacific Gas & Electric Co
To:	; Document Control Desk, Office of Nuclear Reactor Regulation
References
	DCL-17-049
	Download: ML17138B138 (148)
	v • d • e

{{#Wiki_filter:Pacific Gas and Electric Company May 18, 2017 PG&E Letter DCL-17-049 U.S. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001 Docket No. 50-323, OL-DPR-82 Diablo Canyon Unit 2 James M. Welsch Vice President, Nuclear Generation Flaw Evaluation of Unit 2 Residual Heat Removal Suction Weld Joint

Dear Commissioners and Staff:

Diablo Canyon Power Plant Mail Code 104/6 P. 0. Box 56 Avila Beach, CA 93424 805.545.3242 Internal: 691.3242 Fax: 805.545.4884 In accordance with the requirements of the American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code Section XI, 2001 Edition through 2003 Addenda, Paragraphs IWB-3132.3, IWB-3134(b), and IWB-3640, Pacific Gas & Electric Company (PG&E) is submitting the results of the analytical evaluation of a flaw found in Diablo Canyon Power Plant (DCPP) Unit 2, on the 14-inch diameter ASME Code Class 1 weld identified as WIB-245. IWB-3134(b) states, "Analytical evaluation of examination results as required by IWB-3132.3 shall be submitted to the regulatory authority having jurisdiction at the plant site." PG&E identified a circumferential indication in the Residual Heat Removal (RHR) suction weld joint WIB-245 using ultrasound examination techniques (UT) during a DCPP routine scheduled risk-informed inservice inspection (RI-ISI) performed during Unit 2 nineteenth refueling outage. WIB-245 is on the RHR hot leg suction wrought stainless steel pipe in containment and it is the pipe-to-45° elbow weld downstream of the reactor coolant system (RCS) hot leg branch connection. The indication was found to have exceeded the acceptance standards of ASME Section XI, 2001 Edition with 2003 addenda, Table IWB-3514-2. The flaw was initially dispositioned as unacceptable. Subsequently, an analytical evaluation was performed based on the rules of ASME Code, Section IWB-3640, to demonstrate that the weld containing the flaw is acceptable for continued service for Cycle 20 operation, which will not exceed two years. Several crack growth and degradation mechanisms were investigated as part of this evaluation since the cracking did not conform to any known industry operating experience. The specific mechanisms considered include thermal shock from cyclic swirl penetration and cyclic thermal stratification of the unisolable horizontal pipe section, and stress corrosion cracking. Temperature monitoring was conducted to further refine the analysis. Vibration was ruled out as a possible cause based on the A member of the STARS Alliance Callaway

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Document Control Desk May 18, 2017 Page 2 PG&E Letter DCL-17-049 inspections performed by PG&E, which concluded that physical evidence indicative of excessive vibration was not present. Because the evaluation could neither rule out nor specify the specific flaw growth mechanism, a conservative analysis was performed combining the effects of two different flaw growth mechanisms comprised of fatigue crack growth (FCG) and stress corrosion cracking (SCC) for justification of continued operation for an additional cycle. PG&E is not attributing SCC with respect to RI-ISI weld inspections due to uncertainty regarding the flaw growth mechanism. The results of the analysis show that it would take 35 months for the as-found flaw depth of 0.34 inches to reach the allowable flaw size using the most limiting crack growth law. Therefore, operation for an additional cycle was determined to be acceptable. The analysis, methodology, and results are shown in the Enclosure. During the Unit 1 twentieth refueling outage, the same weld in the Unit 1 RHR system was examined as part of an extent of condition investigation. The results indicated a flaw, with the same orientation but with a smaller size compared to that found in Unit 2. This condition has been entered into the corrective action program, and the Resident Inspector has been notified. An additional evaluation per IWB-3640 is currently in progress. The results of the Unit 1 analysis will be communicated to the NRC upon completion. PG&E makes no new or revised regulatory commitments (as defined by NEI 99-04) in this letter. If you have any questions or require additional information, please contact Mr. Hossein Hamzehee at (805) 545-4720. Sincerely, J~~ Vice President, Nuclear Generation rntt/4231/SAPN 50852155-40 Enclosure cc: Diablo Distribution cc/enc: Kriss M. Kennedy, NRC Region IV Administrator Christopher W. Newport, NRC Senior Resident Inspector Gonzalo L. Perez, Branch Chief, California Department of Public Health Balwant K. Singal, NRR Project Manager State of California, Pressure Vessel Unit A member of the STARS (Strategic Teaming and Resource Sharing) Alliance Callaway

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Diablo Canyon Power Plant, Unit 2 Enclosure PG&E Letter DCL-17 -049 Flaw Evaluation of RHR Suction Weld Joint Final Report 1

Prepared by: Reviewed by: Approved by: Report No. 1600539.401 Revision 0 Project No. 1600539 May 2017 Flaw Evaluation of RHR Suction Weld Joint Final Report at Diablo Canyon Power Plant, Unit 2 Prepared for: Pacific Gas & Electric (PG&E) Company Diablo Canyon Power Plant, Unit 2

PO Box 56, Avila Beach, California, 93424 Contract No. 3501102331, 3501092695, Rev. 1 Prepared by:

Structural Integrity Associates, Inc. San Jose, California ~ Date: Apama Alleshwaram ~ t~ Date: Francis Ku ~ Date: Apama Alleshwaram 05/03/2017 05/03/2017 05/03/2017 l)s~nu:tutallnlegrlty Associates. 1nc.*

REVISION CONTROL SHEET Document Number: 1600539.401

Title:

Flaw evaluation ofRHR Suction Weld Joint Final Report at Diablo Canyon Power Plant, Unit 2 Client: Pacific Gas & Electric Company SI Project Number: 1600539 Quality Program: 1:8] Nuclear D Commercial Section Pages Revision Date Comments 1.0 1 1-2 0 05/03/2017 Initial Issue 2.0 2-1-2-5 3.0 3-1-3-1 4.0 4-1-4-6 5.0 5-1-5-18 6.0 6-1-6-14 7.0 7-1 8.0 8-1-8-2 App.A A-1-A-3 App.B B B-87 !S)s~ntctutallnlef/rlly Associates. Inc.*

Table of Contents Section Page

1.0 INTRODUCTION

.......................................................................................................... 1-1 2.0 METHODOLOGY........................................................................................................ 2-1 3.0 ASSUMPTIONS............................................................................................................. 3-1 4.0 DESIGN INPUT............................................................................................................. 4-1 4.1 Inverse Green Function Analyses.................................................................................... 4-1 4.2 RHR Piping Dimensions.................................................................................................. 4-2 4.3 Thermocouple Data.......................................................................................................... 4-3 4.4 Hot Leg Entrance Temperature......................... '............................................................... 4-3 4.5 Hot Leg Thermal Anchor Movements............................................................................. 4-A 4.6 Stress due to Internal Pressure......................................................................................... 4-4 5.0 CALCULATIONS......................................................................................................... 5-1 5.1 RHR Piping Green's Function.Ap.alyses......................................................................... 5-1 5.2. Thermal Stress Analyses.................................................................................................. 5-1

5. 2.1 Thermal boundary Conditions................................................................................. 5-1 5.2.2 Mechanical Boundary Conditions........................................................................... 5-2

5. 2. 3 Thermal Stress Analyses Cases................................................................................ 5-2 5.2.4 Unit Internal Pressure Stress Analysis.................................................................... 5-3 5.2.5 Allowable Flaw Size................................................................................................. 5-3 5.2. 6 Stress Intensity factors............................................................................................. 5-4 5.2. 7 Fatigue Crack growth.............................................................................................. 5-4 5.2.8 Treatment of Negative Stress Intensity Factors for FCG........................................ 5-7 5.2.9 Determination Projected Number ofCycles............................................................ 5-8 5.3 SCC Growth..................................................................................................................... 5-8 5.3.1 SCCGrowthLaw..................................................................................................... 5-9 6.0 RESULTS *OF THE ANALYSES................................................................................. 6-1 6.1 Thermocouple Temperature Results................................................................................ 6-1 6.2 Thermal Stress Results..................................................................................................... 6-1 Report No. 1600539.401RO 111

(;SintclumllniBgrlty Associates. Inc.*

6.3 Unit Pressure Stress Results............................................................................................. 6-2 6.4 Crack Growth Analyses Results...................................................................................... 6-3

7.0 CONCLUSION

S............................................................................................................ 7-1

8.0 REFERENCES

............................................................................................................... 8-1 APPENDIX A COMPUTER FILES....................................................................................... A-1 APPENDIX B PC-CRACK OUTPUT FILES......................................................................... B-1 Report No. 1600539.401RO lV

List of Tables Table 4-1: Thermal Anchor Movements..................................................................................... 4-5 Table 5-2: Applied Stress Summary for Allowable Flaw Size Calculation............................. 5-12 Table 5-3: Allowable Flaw Size Results................................................................................... 5-12 Table 5-4: Number of Cycles per Month.................................................................................. 5-13 Table 6-1: Thru-Wall Axial Stress Summary at TC 102 from Finite Element Analyses............ 6-4 Table 6-2: Crack Growth Results............................................................................................... 6-4 Table 6-3: Monthly Crack Depth................................................................................................ 6-5 Report No. 1600539.401RO v S)Stmclulallntegdly Associates, Inc.*

List of Figures Figure Figure 1-1: RHR Piping and Flaw Indication Location.............................................................. 1-2 Figure 2-1: RHR Piping Thermocouple Locations and Flaw Orientation.................................. 2-5 Figure 4-1: Thermocouple TC 102 Data and Time Period Analyzed in FEA............................. 4-5 Figure 4-2: Thermal Anchor Movements at 100% Power.......................................................... 4-6 Figure 5-2: Representative Applied RHR Thermal Stratification Temperature Profiles......... 5-15 Figure 5-3: Stress Intensity Factors.......................................................................................... 5-16 Figure 5-4: Outside Metal Temperature during Thermal Stratification Transient................... 5-17 Figure 5-5: Crack Growth Rates Comparison for R < 0........................................................... 5-18 Figure 6-1: Channel 102 Measured Temperature and Calculated Fluid Temperature............... 6-6 Figure 6-2: Channel102 Measured Temperature and Calculated Fluid Temperature, Detail.... 6-7 Figure 6-3: Channel102 Measured and Calculated Outside Surface Temperature.................... 6-8 Figure 6-4: Comparison of Measured TC and FEA Predicted OD Temperature....................... 6-9 Figure 6-5: Representative Axial Stress Contour at Elapsed Time= 3,511,020 seconds........ 6-10 Figure 6-6: Through-wall Stress Extraction Location.............................................................. 6-11 Figure 6-7: Representative Stress Intensity Contour Plot for Unit Pressure Case.................... 6-12 Figure 6-8: Fatigue plus SCC Growth Results from an Initial Flaw Size of0.34 in................ 6-13 Figure 6-9: Crack Length per Circumference Growth Results................................................. 6-14 Report No. 1600539.401RO Vl ~Stnu:tumllntegrlly Associates, Inc.*

1.0 INTRODUCTION

During refueling outage 2R19 in May 2016, a circumferential indication was identified in the RHR suction weld joint WIB-245 at Diablo Canyon Power Plant (DCPP), Unit 2 [Attachment 4-A of 1 a]. The location of this weld is shown in Figure 1-1. This evaluation is performed to address the safety and serviceability of the degraded RHR suction weld joint WIB-245 per requirements of the ASME Code, Section XI [3] which specifically addresses piping. The guidance and rules of Section XI are applied for the evaluation. A conservative analysis was performed using two different flaw growth mechanisms of fatigue and stress corrosion cracking (SCC) for justification of continued operation for an additional cycle [3]. Several crack growth and degradation mechanisms were investigated as part of that evaluation since the cracking did not conform to any known industry operating experience. The specific mechanisms considered include thermal shock from cyclic swirl penetration, cyclic stratification of the unisolable horizontal pipe section and stress corrosion cracking (note that vibration was ruled out as a possible cause). Per the investigation, it became clear that SCC was plausible with a pre-existing flaw, while the thermal fatigue theories did not appear to be realistic and were found to be unlikely contributors to crack initiation and growth. The justification for continued operation presented in the conservative analysis was principally based on the assumption that the observed indication at Weld WIB-245 is due to SCC in austenitic stainless steel with a pre-existing flaw in a PWR environment. Based on the conservative analysis [3], SI recommended the application of temporary thermocouples to both welds of the 45° elbow (or as close as possible) and then review the temperature time history data after the plant reaches normal operating conditions. The review would focus on evidence of thermal cycling, frequency of cycling and any measured thermal stratification. A revised analysis was then performed the thermocouple data to more realistically calculate thermal stresses. This will provide more realistic local stresses and global bending loads due to Report No. 1600539.401RO 1-1

stratification and thermal expansion. Thus, a refined crack growth analysis was performed using the cycles determined from the thermocouple data. Flaw {-OCA/tON Figure 1-1: RHR Piping and Flaw Indication Location (Image from Reference 1 a) DETAIL 4-~ Report No. 1600539.401RO 1-2 ~Sttuclumllntegrlly Associates, Inc.*

2.0 METHODOLOGY The temperature monitoring conducted by DCPP was implemented by attaching thermocouples to the outside surface of the piping at several locations as shown in Figure 2-1. For unsteady fluid temperatures, the outside pipe surface temperature may not-be an accurate representation of the inside pipe surface. The inside temperature time histories are estimated from the outside measured temperatures provided by DCPP to conservatively account for the temperature response attenuation in the pipe wall. This will provide the ID temperature history needed for the stress analysis, which is performed by finite element modeling and analysis. The use of Green's functions is a widely-accepted approach for producing the stress response due to changing temperature boundary conditions. A software tool, INVGREEN for DCPP RHR, is developed to perform an inverse Green's function; that is, it determines the required boundary input time history to produce a specified response time history for a Green's Function. INVGREEN for DCPP RHR is programmed in Excel Visual Basic for Applications (VBA), and is based on an earlier SI-developed program called INVGREEN 1.0. INVGREEN for DCPP RHR is used to determine internal fluid temperature time histories that are consistent with measured outside surface temperatures. The fluid temperatures are.checked by performing a heat transfer analysis to calculate the expected outside surface temperatures, which should match the measured values. The DCPP Unit 2 RHR suction line was previously screened out as part of the EPRI MRP-146 [22] program implemented across the US PWR fleet. It is possible that thermal stratification and thermal cycling are considered potential damage mechanisms that could have initiated and grown a fatigue crack. Stress corrosion cracking (SCC) was postulated as one potential damage mechanism that could have initiated and grown an inside surface crack in the heat affected zone (HAZ) of the DCPP Unit 2 RHR suction line elbow weld. Report No. 1600539.401RO 2-1 S)Stnn:trtmltniBgrlty Assaclates, Inc.*

It is stated in the product abstract of Reference 23 that: "Field experience has shown that the majority of incidences of SCC in high-temperature PWR primary water are attributed to the low-flow or stagnant regions of the plant,... the transient presence of oxygen, combined with anionic impurities,... can lead to susceptibility of austenitic stainless steel to sec and is believed to be the cause of the majority of incidences of SCC in PWR primary circuit environments... The presence of cold work in austenitic stainless steel is the primary metallurgical factor found to contribute to sec susceptibility in many plant occurrences. Finally, laboratory test has shown that cold-work stainless steel can sustain crack propagation even in good (low oxygen, chloride and sulfate) PWR primary chemistry." It has been demonstrated that the duplex microstructure of a stainless steel weld is highly resistant to SCC propagation. However, if the flaw is located in the sensitized HAZ of the piping elbow weld joint, sec can be postulated. Since the exact root cause of the failure is not confirmed, thus the current evaluation includes both FCG and SCC as plausible degradation mechanisms. Thermal shock from cyclic swirl penetration and cyclic thermal stratification of the unisolable horizontal pipe section are considered in FCG. The results from the analysis show that FCG is the predominant contributor to flaw growth while SCC is not a common phenomenon in PWR primary piping environments. Thus, the current evaluation is a conservative application of both degradation mechanisms only to estimate the flaw growth rate in order to bound the risk to piping integrity. However, the current evaluation is not assigning SCC as a degradation mechanism to this piping segment, with any degree of certainty. The thermal stratification stresses in the RHR line are calculated using the resultant internal fluid temperature from the thermocouple data at 100% power. The modeled portion of the RHR line starts from the 45-degree downward piping from the hot leg and ends at the riser piping after the Report No. 1600539.401RO 2-2 S) Stroctumllntegrlly Associates, Inc.*

horizontal pipe section. Stresses due to the thermal stratification transient based on temperatures taken from the thermocouples within the modeled piping portion will be calculated using finite element analysis (FEA). Based on the thermocouple data, the analysis will consider a combination of thermal shock, stratification, and global bending. As such, the stresses due to global bending as well as local thermal stresses will be captured together in one analysis. The thermal analysis for 100% power bounds the 48% power data, because the analysis idealizes that the plant starts up instantaneously at 100% power, neglecting any small temperature fluctuations and the 48% power interval throughout a regular start up process. Thus, the 100% power thermal cycles are assumed to occur at the beginning of plant start up (time= 0). A separate unit internal pressure evaluation will also be performed such that the resulting stresses can be scaled to any corresponding operating pressure. The analyses will evaluate four temperature/stratification cases to bound the uncertainties in the hot leg entrance temperature and the hot leg piping thermal anchor movement, as well as the unit internal pressure evaluation. The stresses from all cases evaluated will be reported. Stress intensity factors (K) for a semi-elliptical surface circumferential crack in cylinder are determined using representative fracture mechanics models. The Ks due to the various applied loads are computed as a function of postulated crack depth and linearly superimposed for the various operating states. Stresses from the applied loads that contribute to fatigue crack growth (FCG) and stress corrosion cracking (SCC) are compiled from the previous calculation [3]. For the fatigue crack growth, two different crack growth rates are considered. One is the equation for Austenitic Steels from ASME Code Section XI [2], and the other one is from ASME Code Case N-809 [5]. The details of the fatigue crack growth laws are discussed in Section 2.2 ofReference [3]. Report No. 1600539.401RO 2-3

The SCC growth rate is calculated, based on the approach for determining the SCC growth rate in a BWR environment. PWR environment parameters are applied in order to obtain the crack growth rate. SCC is dependent on 3 factors: material, stress and environment. The differences in environmental conditions between a BWR and a PWR are accounted for in deriving the crack growth rate (CGR) used for DCPP. The details of the SCC growth rate are discussed in Section 4.3.3 in Reference [3]. The allowable flaw size is also updated by including the stress results from the thermal stratification cycling [20]. The resulting crack growth will be compared to the updated allowable flaw size. The software pc-CRACK [6] is used to determine the allowable flaw size and perform the crack growth calculations. The version used has been verified and validated for this project [7]. Report No. 1600539.401RO 2-4 l}Stnu:lumllniBgrlly Associates, Inc.*

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3.0 ASSUMPTIONS The following assumptions are used in this evaluation: It is assumed that conditions are at steady state at the first time point. The file containing thermocouple data is assumed to have extension XLSX, to contain one column with a combined date and time, and to contain at least one column with thermocouple data. The data are assumed to start at row 2 of the column immediately to the right of the date/time. For determining external heat transfer coefficient, a containment temperature of 120°F is assumed. An hin value of 10,000 Btu/hr-ft2-°F is chosen, corresponding to essentially perfect heat transfer between the fluid and the surface. The portion of RHR piping evaluated is assumed to have constant material, diameter, and thickness (i.e., no weld preparation such as counter bores or weld crowns are modeled). In the FEA, the temperature at the RHR pipe-to-hot leg connection is assumed to be constant around the RHR pipe. For the horizontal pipe run portion, the stratification height is assumed to be at the pipe mid-height, with the upper half of the pipe seeing the upper TC data and the lower half of the pipe seeing the lower TC data. The interface region did not see specific applied temperature loading to allow for the calculation of transition temperature behavior. Axial temperature variation was assumed to occur linearly. The 45° angled piping uses the temperature data from TC102 through TC104, and assumes each TC represents a 90° segment of the pipe (TC 102 is also used for the TC 101 location). The first 12-inch length of the modeled 45-degree RHR pipe is assumed to be at one of the two constant hot leg entrance temperatures to be evaluated. It is assumed that the temperature gradient is linear along the length of the pipe. The normal operating transients (Heatup, Cooldown, and steady state operation) are not considered in the fatigue crack growth since those transients contribute a negligible amount of crack growth [Section 2.2.1, 3]. No interaction between fatigue and corrosion crack growth are considered. Report No. 1600539.401RO 3-1 (3 Stnn:lulallntegrlly Associates, Inc.*

4.0 DESIGN INPUT 4.1 Inverse Green Function Analyses The following information is used as input to PIPE-TS2. The DCPP RHR piping is 14" schedule 160 [Attachment 4-A, 1a], resulting in a thickness and outside diameter of 1.406" and 14.000", respectively [8], and yielding the following geometric input: Inside radius= 5.594" Outside radius= 7.000" PIPE-TS2 allows for two materials through the wall thickness; in this case, there is only one pipe material, so the material interface radius is chosen as halfway between the inside and outside radii. The DCPP RHR piping has a maximum external heat transfer rate of 65 Btu/hr-ft2 [1 a, p. 7 of ]. (Note that the reference actually gives this as "65 Btu/hr-ft2-F"; however, this is interpreted as 65 Btu/hr-ft2 since those are the correct units for a heat rate, and since 65 Btu/hr-ft2-0F is an unreasonably high heat transfer coefficient for insulated piping.) Using the normal hot leg temperature of 61 0°F' the temperature difference across the insulation is 610 - 120 = 490°F, which results in a heat transfer coefficient of 65/490 = 0.133 Btu/hr-ft2-°F for the outside surface. During heatup and cooldown, reactor coolant temperature can range from 70 to 574.6°F [1a, Attachments 1-A and 1-B]. Therefore, an approximate average temperature of 300°F is used to determine heat transfer properties. The piping is SA-376 grade TP316 [1a, p. 30 of Attachment 4-A], such that heat transfer properties are as follows [9, Section II, Part D, Table TCD]: Thermal conductivity (TC) = 9.3 Btu/hr-ft-°F Thermal diffusivity (TD) = 0.150 ft2/hr TC/TD = density*specific heat= 9.3/0.150 = 62.0 Btu/ft3-°F Report No. 1600539.401RO 4-1 (;StnlclumllniBgrlly Associates. Inc.*

For the purposes of generating a Green's function, in the PIPE-TS2 analysis, the fluid temperature undergoes a step change from 0 to 1000°F at time zero. The following inputs required by PIPE-TS2 are used to calculate thermal stress and therefore have no effect on the results of interest: modulus of elasticity= 28,300 ksi at 70°F [9, Section II, Part D, Table TM-1] coefficient of thermal expansion= 8.5(10t6 in/in/°F at 70°F [9, Section II, Part D, Table TE-l] Poisson's ratio= 0.3 [10, Section III, NB-3672.4] Stress-free temperature = 0°F (arbitrarily chosen) The remaining inputs affect the accuracy of results; the following values are chosen: Number of pipe nodes = 20 Nodes in first material = 1 0 The number of time control intervals, end of interval (sec), time step (sec), and output interval (sec) are chosen for numerical stability. 4.2 RHR Piping. Dimensions The RHR piping dimensions and material identification are provided by DCPP [2]. The RHR piping material is SA-376, TP316 [1 b, p. 30 of Attachment 4-A]. The RHR piping has an outside diameter ( 0 D) of 14 inches, and pipe thickness of 1.406 inches [ 1 a, Attachment 4-B]. Temperature dependent material properties are obtained from the ASME Code [9] and listed in Table 4-1. Report No. 1600539.401RO 4-2

4.3 Thermocouple Data Approximately two months of 100% power OD surface thermocouple data from 6/14/2016 to 8/10/2016 was recorded and supplied [11]. The thermocouple locations are identified in Figure 2-1. An analysis was performed in Reference 12 and discussed in Section 4.1, to calculate the corresponding ID surface temperature that will result in the measured 0 D surface temperature at each time point and location. The temperature fluctuation time history for each TC is very similar. Hence a sample of 3000 second interval is extracted, which represents 51 data points for each TC. This sample covers enough variability among all TCs. The OD temperature and calculated ID temperature time history for thermocouple TC 102, where the flaw is located, is plotted in Figure 4-1. It can be seen from the lower plot that the temperature fluctuations within the two-month period are fairly steady. Consequently, only a representative time period of 3,000 seconds is analyzed, which envelops the maximum temperature fluctuation and represents the elapsed time between 3,510,420 seconds and 3,513,420 seconds. As shown in Figure 4-1, the 3,000 seconds of representative time period selected for analysis includes the maximum temperature fluctuation for the entire set of measured temperature data. It is also noted that the temperature fluctuations at 100% power envelops that at 48% power collected previously [13], so the use of only 100% power based temperature data is conservative. 4.4 Hot Leg Entrance Temperature Near the RHR 45-degree pipe-to-hot leg junction, the temperature around the hot leg circumference varies between 592.99°F to 607.40°F per the thermocouple data [14]. As mentioned in Section 3.0, for the thermal stress evaluation portion of the FEA, the temperature at the RHR pipe-to-hot leg connection is assumed to be constant around the RHR pipe. As such, two cases will be analyzed to capture the bounding hot leg entrance temperature: 593 oF and 607.4°F. Report No. 1600539.401RO 4-3 SJ Stntclunlllniegrlly Assaciales. Inc.*

4.5 Hot Leg Thermal Anchor Movements The effects on the RHR piping due to thermal anchor movements are also considered. At 1 00% power, the movement at the fluid head penetration connection is zero, and at the hot leg connection, ox= -1.014", oy = -0.074", and oz = 0.412", where +X is South, +Y is Vertical Up, +Z =West [14], as listed in Table 4-1 and shown in Figure 4-2. In the PEA, two cases are analyzed to capture the bounding thermal anchor movement effects: maximum hot leg movement at 100% power, and zero hot leg movement. Note that each thermal anchor movement case is analyzed for each hot leg entrance temperature case, while the same RHR piping thermal stratification thermocouple data are used for all cases. As a result, four cases are analyzed by PEA. 4.6 Stress due to Internal Pressure A constant through-wall stress of 1 ksi is applied to account for the internal pressure acting on the crack face. The constant through-wall stress is conservatively scaled by the normal operating pressure for the FCG and SCC evaluation. Report No. 1600539.401RO 4-4 ~Stnlctumllnfegrlty Associates. Inc.*

Table 4-1: Thermal Anchor Movements Flued Head Penetration RHR-to-Hot Leg Junction Nozzle* (inch) ANSYS ANSYS ANSYS ANSYS ox oy oz ox Zero 0 0 0 0 Movement Maximum 0 0 0 -1.014 Movement

See Section 4.5 for further description of the applied displacements

(;,lJO 500 400 300 200 ~--------------------~ 100 3510420 3510 920 400 /!XJ 100 TC102 Data 6/14/2016 through 8/10/2016 This time period is analyzed in PEA 3511420 3511920 Elap; ed Time (setond) TC102 Data 6/14/2016 through 8/10/2016 3512420 500000 1()0000() 150J0:)0 2000000 2500000 3000000 3EOOOOD Elap;ect Time {$e, ondl (inch) ANSYS oy 0 -0.074 3512920 ~ 00~000 Figure 4-1: Thermocouple TC 102 Data and Time Period Analyzed in PEA ANSYS oz 0 0.412 3513420 Report No. 1600539.401RO 4-5 ~Stnu:lumllntegrlly Associates. Inc.*

'AIL. CAl-l.f!O NORTH r:se~ -v.;.~"R~wtu... Y-Pio,TTe!>!t>l ~~i. ST~M 1,041-Z-~351'1 T*5a V4' i<'oCJ(wilL 'HWI't'llJ(t.l 9'1:t 'STEM Figure 4-2: Thermal Anchor Movements at 100% Power Report No. 1600539.401RO 4-6 ~Stnn:tluallllfBgrlly Associates, Inc.*

5.0 CALCULATIONS 5.1 RHR Piping Green's Function Analyses INVGREEN contains built in Green's functions specific to the DCPP RHR piping. The SI-developed PIPE-TS2 program [15] is used to prepare the Green's functions. The cross section properties and heat transfer characteristics specific to the DCPP RHR piping are used as input to the PIPE-TS2 analysis. Further details of the analyses is given in Reference 12. 5.2 Thermal Stress Analyses 5.2.1 Thermal boundary Conditions The RHR thermocouple data temperature history from TC 1 0 1 through TC 112 are applied onto the FEM as part of the thermal transient analyses. Elapsed time between 3,510,420 seconds and 3,513,420 seconds is analyzed. The inside surface temperature history derived in a separate SI calculation [12] is applied onto the inside metal surface of the FEM. The specific applied RHR piping ID surface temperature history is tabulated in Table 5-1. Note that TC 101 and TC 1 04 data are essentially identical and thus TC 101 data is not listed. Similarly, TC 109 data is essentially identical to TC 110 data thus TC 1 09 data is not listed. The riser pipe section temperature was based solely on TC108 temperature data. As mentioned in Section 3.0, the 45° angled piping uses the temperature data from TC102 through TC 104, and assumes each TC represents a 90° segment of the pipe (TC 102 is also used for the TC 101 location). The interface region between each of the 90° segment do not see specific applied temperature loading to allow for the calculation of transition temperature behavior. Report No. 1600539.401RO 5-1 l) Slntctumlln#Bgrlly Associates. Inc!

A gap in applied temperature occurs between the 90° horizontal elbow and the 45° elbow to allow for the calculation of transition temperature behavior. The same is true in the 45° pipe where the TC data transitions to the constant hot leg pipe temperature. Representative applied temperature profiles are shown in Figure 5-2, where the first 12-inch length of the modeled 45-degree RHR pipe is assumed to be at one of the two constant hot leg entrance temperatures to be evaluated. 5.2.2 Mechanical Boundary Conditions As shown in Figure 5-1, the free end of the riser pipe is constrained in all translations and rotations. Hot leg anchor movements are applied as translations on the 45-degree RHR pipe end, which is constrained in all rotations. However, radial expansion and contraction at both free ends of the FEM is permitted. Since there are no rigid restraints in between the modeled portion of the RHR piping [14], no additional boundary conditions are applied on the FEM. A stress free reference temperature of 70°F is used for all cases evaluated. The application of hot leg thermal anchor movements is via a pilot node setup at the center of the RHR 45-degree pipe end (ANSYS TARGE170 and CONTA174 elements pairing). The ANSYS files are described in Appendix A. 5.2.3 Thermal Stress Analyses Cases Four thermal stress load cases are input into the finite element model to compute the resulting stresses. The four load cases are:

1. Hot leg connection at 593 °F, zero hot leg anchor movements, derived RHR inside surface temperature history from TC 1 02 to TC 112 thermocouple data.

2. Hot leg connection at 607.4 oF, zero hot leg anchor movements, derived RHR inside surface temperature history from TC 102 to TC 112 thermocouple data.

3. Hot leg connection at 593°F, maximum hot leg anchor movements, derived RHR inside surface temperature history from TC 1 02 to TC 112 thermocouple data.

Report No. 1600539.401RO 5-2

4. Hot leg connection at 607.4 oF, maximum hot leg anchor movements, derived RHR inside surface temperature history from TC 1 02 to TC 112 thermocouple data.

The stress results for each case are reported in this calculation. The most limiting stress results will be used in the separate crack growth calculation package. 5.2.4 Unit Internal Pressure Stress Analysis Stresses due to unit internal pressure are also evaluated to support crack growth evaluation. A unit internal pressure, P = 1.0 ksi, is applied to the interior surfaces of the FEM. An induced end-cap load is applied to the free end of the RHR 45-degree pipe in the form of tensile axial pressure, as calculated below. p P*ID2 = 1.0*11.1882 =1.767 ksi end-cap-QD2 -JD2 14.02-11.1882

where, Pend-cap =End cap pressure on free end (ksi)

P =Internal pressure (ksi) ID =Inside diameter (in), 11.188 inches OD =Outside diameter (in), 14.0 inches For the unit internal pressure analysis, the mechanical boundary conditions stated in Section 5.2.2. are applied to the model except for the pilot node at the RHR -to-Hot leg junction. The pilot node at the center of the RHR 45-degree pipe end and contacts at the RHR 45-degree pipe end are removed from the model. The applied mechanical boundary conditions and unit internal pressure load are shown in Figure 5-1. 5.2.5 Allowable Flaw Size The allowable flaw size was determined per ASME Code, Section XI, Appendix C, Article C-5000 [2] in Reference [3]. The details of the allowable flaw size determination are discussed in Report No. 1600539.401RO 5-3 S)Stluctumltntegrtty Associates. Inc.*

Section 2.1, 4.1, and 5.1 of Reference [3]. The stress due to the thermal stratification transient provided in Table 5-2 is additionally considered to determine the allowable flaw size. The updated applied stresses including the stress due to the thermal stratification transient for each Service Level, as shown in Table 5-2, are entered to input of the pc-CRACK [6, 7] to calculate the allowable flaw size. The allowable flaw size results are shown in Table 5-3. With the initial 1/circum.ference = 0.18, the allowable flaw size is 75% of wall thickness under membrane and bending loading or membrane loading only. Note that, as indicated in the table, the allowable flaw size decreases as the 1/circum.ference ratio of the flaw increases. 5.2. 6 Stress Intensity factors The through-wall axial stress distributions for the internal pressure, thermal piping load, thermal stratification transient load, and weld residual* at 70°F were input into pc-CRACK [6, 7], a fracture mechanics program developed by.Structural Integrity Associates under its quality assurance program. The coefficients of third polynomial curve-fit axial stress distributions were input into pc-CRACK, and using "Crack Model309-Semi-Elliptical Circumferential Crack in Cylinder on the Inside Surface," as shown in Figure 12 of Reference [3], the K distributions were determined. The through-wall distribution of the stress intensity factors for each load cases are shown in Figure 5-3. The crack model is a semi-elliptical crack in cylinder, with varying crack aspect ratio and an initial flaw depth of 0.34" and initial a half crack length of 4", corresponding to an aspect ratio, c/a of 11.8. 5.2. 7 Fatigue Crack growth The FCG laws used in this analysis are discussed in the following subsections. Report No. 1600539.401RO 5-4

In FCG, the individual terms that constitute nominal Kmax and Kmin for the calculation of L1K are summarized in the following tabulations. Kmax Kresidual Kdead weight Kpressure Kcrack face pressure Kthermal transient max Kmin Kresidual Kdead weight Kpressure Kcrack face pressure Kthermal transient min The individual Ks for nominal Kmax and combined (summed) with all appropriate scale factors applied. Similarly, the individual Ks for nominal Kmin are combined (summed) with all appropriate scale factors applied. L1K is computed by taking the difference of the resulting summed Kmax and Kmin. Note that Kpressure, Kdead weight, Kthermal piping load, and Kresidual are constant loads during the thermal stratification transient and therefore, do not contribute to the L1K range. However, these Ks affect the value of the R-ratio (Kmin/Kmax).

5. 2. 7.1 Fatigue crack growth Law For Austenitic Steels 'in Air The FCG law for austenitic steels in air is per Subsubarticle C-3210 of the ASME Code, Section XI [2], as shown below, but with a multiplier of2 [16] to account for a PWR environment.

da/dN = 2*Co(L1K)n, units of inch/cycle where: Co = C*S C = 1 o[-10.009 + 8.12x10-4T -1.13 x10-6T2 + 1.02 x10-9T"3] S = 1. 0 when R :::; 0 = 1.0 + 1.8R when 0 < R:::; 0.79 = -43.35 + 57.97R when 0.79 < R < 1.0 Report No. 1600539.401RO 5-5 S)Stnlclumllntegrlly Associates. Inc.*

T =metal temperature, op (taken as the average fluid temperature during the transient) R = Kmin/Kmax = R-ratio ~K = Kmax-Kmin (range of applied K), ksi.Yin n = 3.3 per Section XI, Appendix C [2] Figure 6-3 shows the inside and outside temperature at the crack location during the thermal stratification transients. The metal temperature of 450°F is applied to calculate the crack growth rate. 5.2. 7.2 Fatigue Crack Growth Law using Code Case N-809 Equation The FCG law for Type 3 04 and Type 316 stainless steels and associated weld metals from ASME Code Case N-809 [5] is also considered in order to compare the results of the FCG law shown in Section 5.2.7.1. da/dN = Co* ~Kn, units of inch/cycle where: Co = scaling parameter that accounts for the effect of loading rate and environment on fatigue crack growth rate = C Sr SR SENV n =slope of the log (da/dN) versus log (~K) curve= 2.25 C = nominal fatigue crack growth rate constant = 4.43 x 10-7 for ~K ~ ~Kth = 0 for ~K < ~Kth ~K =stress intensity factor range, ksi.Yin ~Kth = 1.10 ksi.Yin Sr = parameter defining effect of temperature on FCG rate = e-25161rK for 300°F :::; T:::; 650°F Report No. 1600539.401RO 5-6 SJ Stnlclumlllllegrlty Associates. tnc.*

= 3.39x1 05 e[C-251611K)-0.030ITKJ for 70°F :S T < 300°F T = metal temperature, op SR =parameter defining the effect ofR-ratio on FCG rate = 1.0 for R < 0 = 1 + e8.02(R-0.748) for 0 :S R < 1.0 R = Kmin/Kmax = R ratio SENV = parameter defining the environmental effects on FCG rate = TR03 TR =loading rise time, sec TK = [(T-32)/1.8+273.15], K The metal temperature of 450oF shown in Figure 6-3, is applied to calculate the crack growth rate. The loading rise time is determined based on the metal outside temperature from the PEA results, since the rise time of outside temperature is larger than the one of inside temperature. Figure 5-4 shows the outside metal temperature fluctuation. The maximum loading rise time of 180 seconds can be obtained from Figure 5-4. Since a larger loading rise time gives larger crack growth rates, the rise time of 360 seconds is applied to calculate the crack growth rate. The crack growth rate is changing when different R-ratio is used. The calculated ~K-daldN is entered into pc-CRACK [6, 7] to calculate crack growth using ~ode Case N-809 FCG equation. Both crack growth rates for negative R-ratio are compared in Figure 5-5. As shown in Figure 5-5, the calculated crack growth rate using Code Case N-809 FCG equation is larger than the calculated crack growth rate using ASME Code Austenitic Stainless Steels FCG equation for ~K range between 0 and 3 5 ksi-~in. 5.2. 8 Treatment of Negative Stress Intensity Factors for FCG If the stress intensity factor is negative, the FCG analysis is handled as follows: Report No. 1600539.401RO 5-7

1. If both Kmax and Kmin in a load cycle are negative, zero fatigue crack growth is assumed.

This is a reasonable assumption based on the work on compression fatigue crack growth (FCG for which Kmax and Kmin are negative) in Reference 17, in which it was shown that although FCG is present. It is very small in the beginning and remains insignificant afterward. For compression fatigue crack growth, da/ dn of 1. Ox 1 o-30 inch per cycle is assumed.

2. For negative R-ratios, the parameters for effect ofR-ratio are 1.0 for both crack growth laws stated in Sections 5.2.7.1 and 5.2.7.2.

5.2.9 Determination Projected Number of Cycles Based on the stress results, the number of cycles at an assigned amplitude range is determined using rainflow cycle counting technique. The axial stresses at inside surface of the crack location are extracted to count number of cycles. Determined number of cycles is projected to number of cycles per month to enter the input of the pc-CRACK [6, 7]. Table 5-4 lists number of cycles and scale factors for thermal stratification transient. The scale factor is determined as average value of the range. 5.3 SCC Growth SCC is a time dependent phenomenon and occurs during sustained loading conditions. Given that the great majority of plant operation is at steady state normal operating conditions (NOC), sec is defined by the stress condition at NOC. sec is defined to be active when the KI at steady state NOC is a positive number. If SCC is active, crack growth is determined for one-month time period, similar to the FCG calculation, using the crack growth rate in Section 5.3.1. Alternating one-month blocks (periods) ofFCG and SCC growth (ifSCC is active) are used to calculate total cumulative crack growth. Even though the stress due to the thermal stratification is cyclic in nature, the frequency is high enough that the maximum thermal stratification stress is treated as a constant stress in the sec growth evaluation. For sec, the KI is calculated in the following tabulation. Report No. 1600539.401RO 5-8 S)Stlllsturatlntegrlty Associates. Inc.*

KI Kresidual Kpressure Kcrack face pressure Kcteadweight Kthermal transient max 5.3.1 SCC Growth Law The SCC growth law for the Type 304 is referred from BWRVIP-14-A [18]. Note that the use of this equation for the evaluation of Type 316 weld is conservative since Type 316 austenitic stainless steel is more resistant to IGSCC. The basis of the application of this equation is stated in the previous calculation [3]. 1n(daJ = 2.181ln(K)-0.787 Cond-0586 +0.00362 ECP+ 6730 -33.235 dt TABS where: da/dt = crack growth rate (change in crack depth per unit time), mm/s K = stress intensity, MPa~m Cond average conductivity (determined at room temperature), 1-1S/cm ECP electrochemical corrosion potential, m V (SHE) SHE Standard Hydrogen Electrode TABS temperature, K The above crack growth equation is converted to following simpler K -dependent form:

where, Report No. 1600539.401RO 5-9

~ Stnu:lunlllntegr/ty Assoclatlls, Inc.*

da/ dt = crack growth rate, inch/hour C, n = material constants K =stress intensity factor, ksi~in The constants, C and n, are calculated with the same methodology used in Section 5.2.8 of Reference [3]. The metal temperature 450oF is applied to calculate the material constants, C and

n. The calculated constants, C = 2.42x1o-7 and n = 2.181, are applied to calculate SCC growth.

No stress corrosion crack growth threshold is considered. Report No. 1600539.401RO 5-10 ~Sinlclumllnfegrlty Associates. Inc.*

Table 5-1 : Applied RHR Piping ID Temperature Transient Time History Baps.ed Themtoooup~e Data f'F) Time (sec.onrl) TC102. TC10J TC10<4 TC108 TC110 TC111 TC112 3.5*11!]420 452 2 394.0 535.0 450.7 2?4..2 278.6 434.5 35*10480 4 ~ 8.7 391;>.4 554.1 42 3.4 250*.8 258.9 453.6 35 *1 0~0 ~5 *1.0 395. ~ 545.5 456.5 217.. 5 287.. 2; 483.8 35*1*IJe-{10 440.0 398.3 544.3 42 5.7 255.3 25&5 467.6 3-.51(1000 447.2 39Si.7 523.3 453.e; 268.9 286:t 479.3 35*10720 429.3 397.5 554.3 428.5 269.3 257.9 461.2 3.510780 461.3 397.5 52t:k3 458t.3 267.9 286.2 483.4 35*108.40 450.0 402:.7 540.6 43*1.9 269.2 253.7 483.0 35*1(1000 454.9 39S'.6 5*'U 1.2 46117 266.3 289.9 444.3 3510000 424.5 400.9 548..2 440.6 27!!.. 1 252.2 488.5 35*111;1.20 532'.4 412'.0 491l7 44 4.5 262:;! 286.4 447.3 3511080 355.5 396.3 520.0 448.7 273. 1 258.. 0 470..5 35*11*140 495.1 404.5 512:.0 440.7 267.6 282.6 44&.9 35*11 Z.lJO 391l5 403.3 543:~ 435.7 272'.2 262_ *~ 467.9 35*11260 467.5 395.4 535.4 447. 1 26!:!-.3 280.6 460*.0 3.5*11320 405-.6 403.3 553..0 428.7 27'1.0 261.3 ~53.0 3.5113SIJ! 470.6 395.4 529.7 44119

268.9

.282.5 4.rt:k5 3511 44D 404.2 404.4 554.3 44*1.3 265.9 .258\\.2 461.3 35*11500 46f1.4 393.5 536.5 433.6 27fi6 282.3 462'.5 3.5*11660 411.3 404.. 0 55!i7 432:.0 .260.6 259.. 9 477.3 35*11820 451.3 395.2 547.7 441.9 27e*.3 280.7 438.3 3511e..ao 424.0 400.0 553 6 437.3 265*.7 265.4 482'.3 38*11740 44e*.O 395*.4 547.e; 432.6 211.5 271.0 458. 1 3511&.:::10 428.0 39!;'.6 5520 442.5 266.0 216.0 479.9 35*118130 461.6 398.7 543.4 429.3 2.r3.. 7 262'. ~ 464.3 3.5*119120 432..2 40L~ 53*1.5 447.8 264.3 279.8 484.9 35*11980 442.5 398.7 54*1.6 437.3 2/3.6 265.~ 452~.7 35 *12040 45e*.7 403.9 514.7 442.9 265.6 2.re*.~ 478.4 3512'1-00 4!36.5 398.9 548:.2 440.8 272.5 270.8 457.8 35*12*160 452~9 400*. 1 512.9 443. 1 262.3 271.6 484.5 3512220 425.7 401.5 556.. 7 438.0 280.0 263. 1l 442'.2 35*12280 447.5 397.5 5*30.9 447.0 25e*.3 28[1 3 486.8 3.5*12340 42*1.8 3 !;t9 ;~ 558.2 4135*.7 27Qi.e; 263.3 45*1.7 35*12400 46*1.9 398.4 539.3 442.4 257.9 2l7.1 47eA 3.5*12480 448.0 400.3 5<2&e; 445.7 279.9 269.3 473.3 3612520 433.6 401. ~ 544.9 444.4 258.3 27'1.3 468.. 0 l512e.. so 449.7 400.2 542.0 433.9 279.6 271.0 478.0 35*12640 434.2 400.0 54*1.3 450.2 260.3 27'1.0 468.5 3512700 454.0 400.5 5*35*.1 440.0 271.-1 272.4 485.0 35*12760 428.3 3@l7 552. 1 458.9 .258.7 269.2 450. 1 3512820 465.4 399.3 52 6.2 4137.*1 27*1.2 275.5 499:1 35*12880 425.3 399.3 548.. 7 448.4 269.5 267.7 459.9 3-51 294[;1 461.4 399.8 542.3 450.3 266.3 274.3 487. t l513()1JD 423.5 402.5 549.5 4!37.*11 270.9 266.4 472.4 J5*13C60 453.4 397.0 543.D 455.4

267.9 274.5 474.6 35*13120 429':1!

398:.3 542.2 440.7 269.2 27*1.3 472.3 35*13*180 453.3 399.1 548.5 445.2 265.6 .2 / 0.D 466.6 3.51 3240 428.1! 399.0 550.8 450.9 273.1 273.4 492.5 35*132(10 470.2 400*.[1 545.9 433.9 268.9 2'70.9 467.7 3..513360 428.2 40'1.5 525*.4 463.5 268.3 267.3 490.. *1 35*13420 449.3 400*.2 54G. ~ 432.3

269.3 272.2 454.6 Note: Data given in this table is fi*om Reference 12.

Report No. 1600539.401RO 5-11 ~StnlctumllnfBgrlly Associates, Inc.*

Table 5-2: Applied Stress Summary for Allowable Flaw Size Calculation Service Pressure O'e (ksi) O'm O'b Thermal Thermal Level (psia) (ksi) (ksi) Total Load Stratification A 2510 6.19 0.11 2.56 9.362 11.918 B 2681 6.61 0.67 3.15 9.362 12.511 c 2681 6.61 0.89 3.32 9.362 12.686 D 2681 6.61 1.03 3.44 9.362 12.804 Note: Table reproduced from Reference 21. Table 5-3: Allowable Flaw Size Results II circumference >0.7 >0.7 0.2 0.3 0.4 0.5 0.6 0.2 0.3 0.4 0.5 0.6 5 5 Membrane+ Bending Membrane Only Level A 0.75 0.69 0.55 0.49 0.45 0.44 0.75 0.74 0.67 0.57 0.52 0.47 Level B 0.75 0.66 0.53 0.46 0.43 0.42 0.75 0.75 0.71 0.61 0.55 0.50 Level C 0.75 0.70 0.57 0.49 0.45 0.43 0.75 0.75 0.75 0.73 0.68 0.62 Level D 0.75 0.72 0.61 0.52 0.47 0.44 0.75 0.75 0.75 0.75 0.75 0.71 Minimum 0.75 0.66 0.53 0.46 0.43 0.42 0.75 0.74 0.67 0.57 0.52 0.47 Allowable a/t Note: Table reproduced from Reference 21. Report No. 1600539.401RO 5-12

Table 5-4: Number of Cycles per Month No. of cycle No. of cycles Scale Range for 3000 sec per month Factor 99 -100% 1 876 1 97-99% 0 0 0.98 94-97% 0 0 0.955 90-94% 0 0 0.92 85-90% 0 0 0.875 79-85% 0 0 0.82 72-79% 0 0 0.755 64-72% 1 876 0.68 55-64% 0 0 0.595 45-55% 0 0 0.5 34-45%* 2 1752 0.395 22-34% 6 5256 0.28 9-22% 12 10512 0.155 4-9% 1 876 0.065 0- 4% 1 876 0.02 Note: Table reproduced from Reference 21. Report No. 1600539.401RO 5-13 lJ Stluclumllntegrlly Associates, Inc.*

F.T.F'Jv!F'I,ITS TYPF', NrJM End of riser pipe is constrained in all translations and rotations. However, radial expansion and End cap pressure is applied on this end. -1. '/6'/24 -1.1S2J -. SJ'lJ-':>6 .O'f'/.I)B6 .692.':>29 -1.4'.:;9"/'/ -.~~4828 -.22988!.:> .38'.:;0!.:>'1 Figure 5-l: Applied Unit Pressure and Mechanical Boundary Conditions 1 Report No. 1600539.401RO 5-14 l) StroclunlllniBgrlly Associates, Inc.*

Case of 5 93 op hot leg temperature 266. 59 339. 142 4]1.694 484. 24~ 556.797 _ _]_02. 866 375. 418 447. 969 520.521 593.073 ~--- ---- 266. 59 304. 469 342. 347 418. ]0 380. 226 Case of 607.4 op hot leg temperature 493. 862 455. 984 531. 741 607. 498 Figure 5-2: Representative Applied RHR Thermal Stratification Temperature Profiles Report No. 1600539.401RO 5-15

20 10 0 ~ -10 ci c., ~

.:: -20 K vs. a

~ / ...._ _______,.., - DW -40 -50 0 Unit Crack Face Pressure Residual Stress -- Thermal Strat. max -- Thermal Strat. min 0.2 0.4 0.6 0.8 Crack Depth from Inside Surface (in) Figure 5-3: Stress Intensity Factors Note: Table reproduced from Reference 21 Report No. 1600539.401RO 5-16 1 1.2

Outside Meta I Tenl perature 455 u:

__ 45

~

J,

~ Q.l Q._ E 44 440 435 510600 35 9Xl 3511200 3511500 Tim ( c) 3511800 3512100 35 2400 Figure 5-4: Outside Metal Temperature during Thermal Stratification Transient Notes: I. Table reproduced from Reference 21.

2. The maximum loading rise time is 180 seconds. Since a larger loading rise time yields a greater crack growth rate, the rise time of 3 60 seconds is applied to calculate the crack growth rate.

Rep_ort No. 1600539.401RO 5-17 S) Slnlcbnlln#Bgrtty Associates, Inc.*

...9:! u > u 2.00E-04 l.SOE-04 c l.OOE-04 z "'0 (\\) "'0 5.00E-05 O.OOE+OO 0 --Code Case N-809 R<O --ASM E Code Equation X2 R<O 5 10 15 20 25 30 35 ~K (ksi-in°*5) Figure 5-5: Crack Growth Rates Comparison for R < 0 Note: Table reproduced from Reference 21 40 45 50 Report No. 1600539.401RO 5-18 l) Stntctumllntegrlly Associates. tnc.*

6.0 RESULTS OF THE ANALYSES 6.1 Thermocouple Temperature Results Figure 6-1 plots the calculated fluid temperature (Boundary Input, equivalent to inside surface metal temperature) and measured temperature (Response, equivalent outside surface metal temperature) for a typical thermocouple data column (channel 1 02) from the run with data written June 3, 2016. Note that the fluid temperature varies more widely than the measured temperature; this is especially noticeable at the end ofheatup. Figure 6-2 shows a selected portion of the results from Figure 6-1, providing greater detail. (Note that the interval of 86400 seconds on Figure 6-1 corresponds to one day.) Figure 6-3 shows the results of the PIPE-TS2 run using calculated fluid temperature for channel 102, with a job name ofRHR-102. The calculated and measured outside surface metal temperature agree to within about 1 op. In general, output from the data sets written 6/14/2016 and 8/1 0/2016 are similar in magnitude to that shown in Figure 6-1 after the maximum operating temperature has been reached. Therefore, the data and conversion results shown in Figures 6-1 through 6-3 are representative. The PEA predicted metal OD surface temperature at thermocouple TC102 and TC104locations are compared in Figure 6-4. The comparison demonstrates that the PEA predictions are within 6°F of the corresponding thermocouple measurements. The 6°F maximum discrepancy is deemed insignificant and, therefore, the applied thermal boundary conditions and assumptions in the PEA are adequate. 6.2 Thermal Stress Results The stresses due to RHR thermal stratification, hot leg thermal displacement, and hot leg entrance temperature effects are calculated at each time point of the elapsed time period between 3,510,420 seconds and 3,513,420 seconds. Representative resulting axial stresses in the flaw Report No. 1600539.401RO 6-1 S) Stnu:lumllntegrlly Associates, Inc.*

region are plotted in Figure 6-5 at elapsed time= 3,511,020 seconds (where the temperature at TC102 is at the maximum). The axial stresses are plotted with respect to a local coordinate system aligning with the 45-degree RHR pipe. Linearized through-wall stresses as well as detailed through-wall stresses on a linear path through the centerline of the flaw, as shown in Figure 6-6, are extracted from each analysis cases. The linearized membrane-plus-bending (Pm+Pb) axial stresses are compared within each analysis case to determine the maximum and minimum axial stress time points. Utilizing linearized Pm+Pb stresses is a common practice to assess the stress results within a thermal transient for fracture mechanics analysis. The axial stress results are summarized in Table 6-1. The through-wall axial stresses at the corresponding minimum and maximum time points are fit into a third order polynomial, which is a convenient method to represent the stress distribution through the thickness. The curve fit coefficients will be used in the subsequent crack growth calculation. As tabulated in Table 6-1, the quality of the curve fits, R2, are all close to 0.999 which means very high quality fit. The curve-fit polynomial is represented in the form: where a =axial stress as function of depth from inside surface (ksi) Ci =polynomial coefficients, i = 0, 1, 2, and 3 x =distance from inside surface (in) 6.3 Unit Pressure Stress Results The stresses due to unit internal pressure load are shown in Figure 6-7. Linearized through-wall stresses, as well as detailed through-wall stresses, are extracted on a linear path through the Report No. 1600539.401RO 6-2 ~ Stnu:lurallntegrlly Associates, Inc.*

centerline of the flaw, as shown in Figure 6-6. The axial stress results are summarized in Table 6-1. 6.4 Crack Growth Analyses Results The stress intensity factor results for each load case are presented in Figure 5-3. The crack growth results are shown in Table 6-2 and Figure 6-8. The allowable flaw size is calculated based on the 1/circumference at each crack depth since the 1/circumference is also changed for every month as shown in Figure 6-9. At the weld location, it takes 41 months for the initial flaw of 0.34 inches to reach the allowable flaw size when ASME Code FCG equation is used. It takes 35 months for the initial flaw of 0.34 inches to reach the allowable flaw size when Code Case N -809 FCG equation is used. As shown in Table 6-3, the crack growth due to SCC is about 0.0385 inches. When the crack reaches about 0.6 inches, there is a crack growth less than 0.0001 inches due to sec because the residual stress is compressive enough that the total applied K is less than 0.05 ksi.Vin, Figure 6-8. As a result, the crack growth has a tendency to arrest near a depth of around 0.6 inches. Report No. 1600539.401RO 6-3 S)Stmlumllnlegrlly Associates, tnc.*

Table 6-1: Thru-Wall Axial Stress Summary at TC102 from Finite Element Analyses Linearized Stresses Load Case (ksi) Pm+Pb Pm+Pb (Inside) (Outside) Min -23.429 2.433 Case 1 Max 9.362 -13.696 Min -23.440 2.428 Case2 Max 9.351 -13.701 Min -25.110 2.079 Case 3 Max 7.656 -14.035 Min -25.124 2.073 Case4 Max 7.641 -14.042 Unit Internal Pressure 1.846 1.688 Table reproduced from Reference 20 Cases: Polynomial Curve Fit Coefficients (ksi) Co c1 c2 c3 -32.017 62.244 -46.571 12.153 21.014 -78.073 69.498 -20.254 -32.028 62.249 -46.572 12.153 21.003 -78.067 69.496 -20.254 -33.738 63.382 -46.764 12.195 19.244 -76.783 69.167 -20.171 -33.752 63.388 -46.765 12.196 19.230 -76.775 69.165 -20.170 1.871 -0.283 0.262 -0.111 Quality R2 0.99974 0.99897 0.99974 0.99897 0.99975 0.99890 0.99975 0.99890 0.99675

1.

Hot leg connection at 593°F, zero hot leg thermal anchor movement, derived RHR inside surface temperature history from TC1 02 to TC112 thermocouple data.

2.

Hot leg connection at 607.4°F, zero hot leg thermal anchor movement, derived RHR inside surface temperature history from TC1 02 to TC112 thermocouple data.

3.

Hot leg connection at 593°F, maximum hot leg thermal anchor movement, derived RHR inside surface temperature history from TC 1 02 to TC 112 thermocouple data.

4.

Hot leg connection at 607.4°F, maximum hot leg thermal anchor movement, derived RHR inside surface temperature history from TC1 02 to TC112 thermocouple data. Table 6-2: Crack Growth Results ASME Code Eq. Code Case N -809 Austenitic Steel in Air Time for Initial Flaw to 41 months 35 months Reach Allowable Flaw Size Table reproduced from Reference 20 Report No. 1600539.401RO 6-4 lJ SllucbuaiiiiiBgrlty Associates, Inc.*

Table 6-3: Monthly Crack Depth Crack Depth (in) Time ASME Code Eq. (In month) Austenitic Steel in Air Code Case N-809 Times 2 0 0.3400 0.3400 FCG 0.4065 0.4573 1 sec 0.4373 0.4723 FCG 0.4973 0.5451 2 sec 0.5040 0.5464 FCG 0.5502 0.5913 3 sec 0.5512 0.5913 FCG 0.5918 0.5949 4 sec 0.5918 0.5949 FCG 0.5959 0.5989 5 sec 0.5959 0.5989 FCG 0.5993 0.6024 6 sec 0.5993 0.6024 FCG 0.6134 0.6166 12 sec 0.6134 0.6166 FCG 0.6277 0.6298 36 sec 0.6277 0.6298 FCG 0.6300 0.6298 111 sec 0.6300 0.6298 FCG 0.6300 203 sec 0.6300 Table reproduced from Reference 20 Report No. 1600539.401RO 6-5 ~Stnn:lunlllnlegrlly Associates, Inc.*

bUU soo 400 ~t

l

~ 300 OJ 0... E Cl) t-200 100 0 0 ,Rf)400 17/.ROO ~ 4snoo 4 ~700 0 S1.R400 n04.ROO Elapsed t ime, sec -- Boundary Input -- Response Figure 6-1: Channel 102 Measured Temperature and Calculated Fluid Temperature Report No. 1600539.401RO 6-6 S) Stntclumllntegrtty Associates, Inc.*

600 500 400 ~l

J

~ 300 Q) Q.. E Q_l f-200 100 0 331200 332400 333600 334800 336000 337200 338400 339600 340800 342000 343200 344400 345600 Elapsed t ime, sec -- t1oundary Input -- Kesponse Figure 6-2: Channel 102 Measured Temperature and Calculated Fluid Temperature, Detail Report No. 1600539.401RO 6-7 l}Sinlclulallntegrlty Associates, Inc.*

162 160 158 !;!.- 156 ~'

J

~ 154 Q) a.. E Q) r-152 150 148 146 0 500 1000 1500 2000 2500 Time, sec -- inside fluid, calc -- outer surface, calc -- outer surface, measured Figure 6-3: Channell02 Measured and Calculated Outside Surface Temperature Report No. 1600539.401RO 6-8 S)Stnn:tumllntegrtty Associates. Inc.*

Measured TC and FEA Predicted OD Surface Temperature 560 - 550 540 r 530 r 520 - ~ 510 l ~ 500 _l t 490 1 ~ 480 I i ::: l 450 r 440 f

I 400 - *---

3510500 3511000 TC104

FEA104

-- TC102

FEA102 3511500 3512000 3512500 3513000 3513500 Elapsed Time (second)

Figure 6-4: Comparison of Measured TC and PEA Predicted OD Temperature Report No. 1600539.401RO 6-9 ~ Stnrclumllntegrlly Associates. Inc.*

tr:-1 rl!£-.. '\\ L£*L>""' t,:..-.. , -,- -!1 [J ~. - 1 *- 7 !0:: ~~~~;)~~)\\.; ~ ll

t..D-1 Case 1:

593 op HL Temp. ' a: -. ~: Lt. -J1 1.::.:-u

re-.- t.:". ;.' J

~ t :- r., 11.111

lt.E- --F-;,1.:.!,:

.it'!... I. -. H "'-{"!'...-*1.*,, Case 3: 593 op HL Temp. "-*ll .1? *1

1':-...: u-:,:;;,

~~~~: : : ~. *1.'1 ~~~!:;*~,*~ . : c ~.. 1. i: * -, ... c::- ;-J.r*,-*r Case 2: 607.4°F HL Temp. Case 4: 607.4°F HL Temp. Figure 6-5: Representative Axial Stress Contour at Elapsed Time= 3,511,020 seconds (Axial stress w.r.t. the 45-degree RHR pipe. Stress contour scale in KSI unit) Report No. 1600539.401RO 6-10 'l. 1 7 ~ ~

Through-wall stress extraction location is at flaw centerline Approx. flaw extent / Figure 6-6: Through-wall_ Stress Extraction Location Report No. 1600539.401RO 6-11 l)Sintclumllntegrlty Associates, tnc.*

N(D.A.L :=:OTjiTTO\\T Sl'F'.P=l Si_lB =1 'l'lt<l!!:.=l

.ilN'l' (l'NG)

RSYS:--0 DH!- =. Otd294 St*N =/.. 9877:i

SAX =6. 29.322 2.997'/b 5. 92'/0S 3_.3o391 6.29322 Figure 6-7: Representative Stress Intensity Contour Plot for Unit Pressure Case Report No. 1600539.401RO 6-12 (J: Sttuclulallnfegrlly Associates, tnc.*

l. ii:. J

.l ***m

( 1,8*.* }

=>~

0 w Cl.h II) ~ u U.': ( Ll ...:! JD lLl' ' 11) L't fi I ati ue + SCC Growth ~~ 1,- J~.,..** ~....... Jo; r~ Crack depth and allowa,tbe inte-rcepts: at 35 montns when the Code Cade N.. sog f CG @qu.ati.on is: used f.ta nf' ( *nn lq Crack depth and allow able i'ntercept s at 41 mont hs: whe n the ASME Aust enitic St eel in Air X2 FCG equation is used Figure 6-8: Fatigue plus SCC Growth Results from an Initial Flaw Size of 0.34 in Report No. 1600539.401RO 6-13 l)Stntcllnltntegrlly Associates, Inc.*

0.90 0.80 0.70 0.60 <l) u c: ~ ~ E o.so

J

. ~ u 0.40 0.30 0.20 0.10 I 0 Crack Length I Circumference Growth .. --(16,,.. ,./

ASM E Aust enitic Steel in Air X2 5

-- Code Case N-809 10 15 20 25 30 35 40 45 Time (month) Figure 6-9: Crack Length per Circumference Growth Results 50 55 60 Report No. 1600539.401RO 6-14

7.0 CONCLUSION

S The evaluation herein determines an allowable flaw depth and expected crack growth for the RRR suction line at DCPP, Unit 2 where cracking was discovered. The cracking is located in Weld WIB-245, the first 45° elbow-to-pipe weld downstream of the RCS nozzle weld. Using the methods of ASME Section XI, Appendix C, an allowable flaw depth curve as a function of the flaw's length-to-circumference ratio has been determined. In order to calculate crack growth over the next operating cycle, both FCG and SCC as plausible degradation mechanisms were considered as part of the evaluation performed in Reference 3 because the exact root cause of the failure is not confirmed. Thermal shock from cyclic swirl penetration and cyclic thermal stratification of the unisolable horizontal pipe section are included in the FCG calculation. Vibration was not included since it was ruled out as a possible cause-:- Temperature data along the affected RRR suction line has been collected during plant operation, which shows significant thermal stratification cycling near the location of the identified flaw. Consequently, a refined analysis has been performed in this report to calculate the crack growth using the detailed temperature data obtained from the thermocouples. The results indicate that at the weld location, it would take 3 5 months for the as-found flaw depth of 0.34" during the 2Rl9 refueling outage to reach the allowable flaw size using the most limiting crack growth law. The results also indicate that FCG is the predominant contributor to flaw growth while SCC is not a common phenomenon in PWR primary piping environments. Thus, the current evaluation is a conservative application of both degradation mechanisms to estimate the flaw growth rate in order to bound the risk to piping integrity. However, the current evaluation is not assigning sec as a degradation mechanism to this piping segment, with any degree of certainty. Thus, based on the crack growth rates presented in this report, the flaw in the 45° elbow weld of the RRR suction line at DCPP, Unit 2 is acceptable for continued operation until the 2R20 refueling outage which will not exceed a two-year duration. Report No. 1600539.401RO 7-1 () Stluclunfllntegdty Associates, Inc.*

8.0 REFERENCES

1. DCPP Design Input Transmittals:

a. DCPP Design Input Transmittal No. DIT-50852155-001-01, "RCS Cooldown and Heatup STP M-55," SI File No. 1600539.208.

b. DCPP Design Input Transmittal No. DIT-50852155-002-00, "2R19 RHR Suction Weld Joint Flaw Evaluation," SI File No. 1600539.207.

2. ASME Boiler and Pressure Vessel Code, Section XI, 2001 Edition, with Addenda through 2003.

3. SI Calculation No. 1600539.301, Rev. 0, "Evaluation of the Flaw in the RHR Suction Weld Joint."

4. Email from Brandon Mainini (DCPP) to Anderson Lin (DCPP), "RE: Pre-Job Brief on RHR Suction Joint Flaw Evaluation with TIC Data," dated 8/29/2016 10:10 AM, SI File No. 1600539.216.

5. ASME Code Case N-809, "Reference Fatigue Crack Growth Rate Curves for Austenitic Stainless Steels in Pressurized Water Reactor Environments Section XI, Division 1,"

Cases the ASME Boiler and Pressure Vessel Code, June 23, 2015.

6. pc-CRACK 4.1 CS, Version Control No. 4.1.0.0, Structural Integrity Associates, December 31, 2013.

7. SI V&V Report No. 1600539.305, Rev. 0, "Verification ofpc-CRACK 4.2 beta Output."

8. American National Standard ANSI/ASME B36.10M-1985, Welded and Seamless Wrought Steel Pipe.

9. ASME Boiler and Pressure Vessel Code, Section II, Part D - Properties, 2001 Edition w/ Addenda through 2003.

10. ASME Boiler and Pressure Vessel Code, 2001 Edition with addenda through 2003.

11. DCPP Design Input Transmittal No. DIT-50852155-003-02, "2R19 RHR Suction Weld Joint Flaw Evaluation," SI File No. 1600539.211.

12. SI Calculation Package No. 1600539.302, Rev. 0, "Inverse Green's Function Calculations for Diablo Canyon RHR Piping."

13. DCPP Design Input Transmittal No. DIT-50852155-003-00, "2R19 RHR Suction Weld Joint Flaw Evaluation," SI File No. 1600539.211.

14. DCPP Design Input Transmittal No. DIT-50852155-004-00, "Unit 2 RHR Suction Weld Joint Flaw Evaluation," SI File No. 1600539.215.

15. PIPE-TS2, Version 1.01, Program to Compute the Transient Thermal and Stress Response of an Axisymmetric Two-Material Cylinder, Structural Integrity Associates.

16. Section XI Task group for Piping Flaw Evaluation, ASME Code, the Journal of Pressure Vessel Technology, "Evaluation of Flaws in Austenitic Piping" Volume 108, Number 3, dated August 1986.

Report No. 1600539.401RO 8-1

17. Lenets, Y.N., "Compression Fatigue Crack Growth Behavior of Metallic Alloys: Effect of Environment," Engineering Fracture Mechanics, Vol. 52, No.5, 1997.

18. BWRVIP-14-A: BWR Vessel and Internals Project, Evaluation of Crack Growth in BWR Stainless Steel RPV Internals, EPRI, Palo Alto, CA: 2008. 1016569.

19. ANSYS Mechanical APDL, Release 14.5 (w/ Service Pack 1 UP20120918), ANSYS, Inc., September 2012.

20. SI Calculation No. 1600539.303, Rev. 0, "Finite Element Stress Analysis of the RHR Piping Due to Thermal Stratification Transient."

21. SI Calculation No. 1600539.304, Rev. 0, "Crack Growth Evaluation in the RHR Suction Weld Joint."

22. Materials Reliability Program: Management of Thermal Fatigue in Normally Stagnant Non-Isolable Reactor Coolant Branch Lines (MRP-146, Revision 1), EPRI, Palo Alto, CA, 6/22/2011 (1022564). PROPRIETARY.

23. Materials Reliability Program: Studies of Stress Corrosion Cracking Initiation in Stainless Steels in Off-Normal PWR Primary Water Chemistry Environments (MRP-292), EPRI, Palo Alto, CA, 1021016. Product Abstract.

Report No. 1600539.401RO 8-2

Report No. 1600539.401RO APPENDIX A COMPUTER FILES A-1 (; Stntctuml lntegrlly Associates, Inc.*

ANSYS Files For Finite Element Analyses File Name Description STACK.INP Control analysis input file PIPE_GEOM2.1NP Create RHR piping finite element model COMPONENTS Component definition file STRAT _HL593.1NP Perform Case 3 analysis STRAT _HL607.1NP Perform Case 4 analysis STR_NoTAM593.1NP Perform Case 1 analysis STR_NoTAM607.1NP Perform Case 2 analysis TMH_HL396_mntr.inp Transient time step history file for 593°F HL temperature case TMH_HL607 _mntr.inp Transient time step history file for 607.4°F HL temperature case UNITPRES.INP Perform unit internal pressure loading analysis GETPATH.TXT Stress extraction path definition file

.OUT Raw stress output text files(*= STRAT_HL593, STRAT_HL607, STR_NoTAM593, STR_NoTAM607 and UNITPRES)

Formatted stress output text files(*= STRAT _HL593,

.CSV STRAT_HL607, STR_NoTAM593, STR_NoTAM607 and UNITPRES) 1600539.303.xlsx Excel spreadsheet of stress results pc-CRACK Files For Fracture Mechanics and Crack Growth Analyses File Name Description LevelA.pcf Allowable flaw size for service level A pc-CRACK input file LevelB.pcf Allowable flaw size for service level B pc-CRACK input file LevelC.pcf Allowable flaw size for service level C pc-CRACK input file LevelD.pcf Allowable flaw size for service level D pc-CRACK input file LevelA.rpt Allowable flaw size for service level A pc-CRACK output file LevelB.rpt Allowable flaw size for service level B pc-CRACK output file Report No. 1600539.401RO A-2

LevelC.rpt Allowable flaw size for service level C pc-CRACK output file LevelD.rpt Allowable flaw size for service level D pc-CRACK output file Casel (ASME).pcf pc-CRACK input file to evaluate crack growth using ASME Code for FCGlaw Casel (ASME).rpt pc-CRACK main output file using ASME Code for FCG law Casel (N-809).pcf pc-CRACK input file to evaluate crack growth using Code Case N-809 forFCG law easel (N-809).rpt pc-CRACK main output file using Code Case N-809 for FCG law Case2 (N-809).pcf pc-CRACK input file to evaluate crack growth of Case 2 using Code Case N -809 for FCG law Case2 (N -809).rpt pc-CRACK main output file of Case 2 using Code Case N-809 for FCG law Case3 (N-809).pcf pc-CRACK input file to evaluate crack growth of Case 3 using Code Case N -809 for FCG law Case3 (N-809).rpt pc-CRACK main output file of Case 3 using Code Case N-809 for FCG law Case4 (N-809).pcf pc.;.CRACK input file to evaluate crack growth of Case 4 using Code Case N -809 for FCG law Case4 (N -809).rpt pc-CRACK main output file of Case 4 using Code Case N-809 for FCG law Rainflow.exe Rainflow program to determine number of cycles using rainflow cycle counting technique TC102.txt Rainflow input file to determine number of cycles TC102.out Rainflow output file to determine number of cycles Report No. 1600539.401RO A-3

Report No. 1600539.401RO APPENDIXB PC-CRACK OUTPUT FILES B-1 !S} Slnlc:tum Integrity Associates. Inc!'

LevelA.rpt pc-CRACK 4. 2 CS Version Control No. 4. 2. 0. 0 Beta Structural Integrity Associates, Inc. WHYT. structint. com pccrack@structint. com Date: 11/11/2016 11: 02 Input Data read from C: \\Users\\mfong\\Documents\\01. Project\\05. DCPP\\1600539\\Alloi*Tabl e Fla11 Size\\LevelA. pcf Analysis Title : LevelA Units Selected : US Customary Linear Dimensions - inches Stress - ks i Load - kips Temperature - deg F Time - hours Jic - in-lbs/in"2 Analysis Type: ASME Secti on XI HIB-3640 (2004) Crack Geometry Orientation : Circumferential Crack Depth = Crack Length = Pipe Geometry 0.3400

8. 0000 Nominal Pipe Size =

14. 0000 Outer Diameter =

14. 0000 Wal l Thickness =

1. 4200 Servi ce Level : A The allm*1able f l aN size is determined using Tables Stresses Pm =

Pb = 6. 1900 (safety factor = 0.1100 (safety factor = Pe = 11.9180 K (Residual Stress) = Naterial: Stai nl ess Steel Flux >rel d Flow Stress

0. 0000 45.1500 Number of Warnings in Inputs: 0 Analysis Resul ts 2.7000) 2.3000)

Failure Mode per Screening Criteria: EPFM (Class 1 screening rules used) Table C-5310-1 used Stress Ratio Z factor 1/ circumference = all01*1able a/t

0. 3637 1.4300 0. 181 9

0. 7 50 0 (Combined Loading)

!/Circumference All01*1able a/t 0.0000 0.7500 0.1000 0.7500 0.2000 0. 7500 0.3000 0.6918 0.4000 0.5527 Report No. 1600539.401RO B-2 l)slnlctunrlllllegrlty Associates. Inc.*

0. 5000

0. 6000 0.7500 Table C-531 0- 5 used Stress Ratio Z factor 0.4854 0.4482

0. 4382 1/ circumference =

a l lm*rable a/t

0. 5293

1. 4300 0.1819

0. 7500 (Hernbr ane Loading) 1/Circumference AlloHabl e a/t

0. 0000 0. 7500 0.1000 0. 7500

0. 2000 0.7500

0. 3000 0.7383

0. 4000

0. 6689

0. 5000 0.5748 0. 6000

0. 5177

o. 7500 0.4707 Note: Allo\\*Tabl e crack s i ze is cal culated based on the fai l ure mode indicated by the screening criteri a \\*lhi ch is based on the input crack size Number of Runtime Warnings: 0

- - End of pc-CRACK output ***

Report No. 1600539.401RO B-3 S} Stnu:tutallntegrlty Associates. Inc.*

LeveiB.rpt pc-CRACK 4. 2 CS Version Control No. 4. 2. 0. 0 Beta Structural Integrity Associates, Inc. \\-1\\*TVl. structint. com pccrack@structint. com Date: 11/11/2016 11:02 Input Data read from C: \\Users\\mfong\\Documents\\01. Project\\05. DCPP\\1600539\\AlloHable Fla>l Size\\LevelB. pcf Analysis

Title:

LevelB Units Selected: US Customary Linear Dimensions - inches Stress - ksi Load - kips Temperature - deg F Time - hours Jic - in-lbs/in'2 Analysis Type: ASME Section XI IWB-3640 (2004) Crack Geometry Orientation: Circumferential Crack Depth = Crack Length = Pipe Geometry

0. 3400

8. 0000 Nominal Pipe Size =

14. 0000 Outer Diameter = 1 4. 0000 Wall Thickness =

1. 4200 Service Level : B The alloNabl e fla\\*1 size is determined using Tables Stresses Pm =

Pb =

6. 6100 (safety factor =

0. 6700 (safety factor =

Pe = 12.5110 K (Residual Stress) = Naterial: Stainless Steel Flux Held FloH Stress

0. 0000 45.1500 Number of \\*larnings in Inputs: 0 Analysis Results

2. 4000)

2. 0000)

Fail ure Mode per Screening Criteria: EPEM (Class 1 screening rul es use d) Table C-5310-2 used Stress Ratio Z factor 1/ circumference = allo,;able a/t

0. 4287

1. 4300 0.1819

0. 7500 (Combined Loading) 1/Circumference AlloHable a/t 0.0000 0.7500 0.1000 0.7500

0. 2000

0. 7500

0. 3000

0. 6611 0.4000

0. 5326

0. 5000 0.4641

0. 6000

0. 4341

0. 7500

0. 4198 Report No. 1600539.401RO B-4 S)Stnu:funrlllllegrlty Associates. Inc:'

Table c-531a-5 used Stress Ratio Z factor 1 / circumference = all01*1able a/t a. sa24

1. 43aa a.18 19 a. 75aa (}lembrane Loading) 1/Circumference Allowable a/t

a. aaaa a.75aa a.laaa

a. 7saa a. 2oao

0. 7500

a. 30ao 0. 749a 0.4aoa

a. 7a66 a. 5oao

0. 6071 0. 6000

0. 54 73 a.750a

a. 4976 Note: Allo\\oTable crack size is calculated based on the failure mode indicated by the screening criteria which is based on the input crack size Number of Runtime ~*larnings: 0

- - End of pc-CRACK output ***

Report No. 1600539.401RO B-5 SJstroc:tutal Integrity Associates. Inc!'

LeveiC.rpt pc-CRACK 4. 2 CS Version Control No. 4. 2. 0. 0 Beta Structural Integrity Associates, Inc. HVTW. s tructint. com pccrack@structint. com Date: 11/11/201 6 11:02 I nput Data read from C: \\Users\\mfong\\Document s\\01. Project\\05. DCPP\\1600539\\Allo"labl e Fla" Size\\LevelC. pcf Analysis

Title:

LevelC Units Selected : US Customary Linear Dimensions - inches Stress - ks i Load - kips Temperature - deg F Time - hours Jic - in-l bs/in"2 Anal ysis Type: ASME Secti on XI I\\"15-3640 (2004) Crack Geometry Orientation : Circumferential Crack Depth = Crack Length = Pipe Geometr y

0. 34 00

8. 0000 Nominal Pipe Size =

14. 0000 Outer Diameter =

14. 0000

\\"I all Th ickness =

1. 4200 Service Level : C The allowable flaw size is determined using Tables Stresses Pro=

Pb =

6. 6100 (safety factor =

0. 8900 (safety factor =

Pe = 12.6860 K (Residual Stress) = Materi al : Stainless Steel Fl ux Held Flow Stress

0. 0000 45. 1500 Number of Warnings in I nputs: 0 Analysis Results

1. 8000)

1. 6000)

Fail ure Mode per Screening Criteria: EPE11 {Class 1 screening rules used) Table C-5310-3 used Stress Rat i o Z factor 1/ cir cumference = allo1-1abl e a/t

0. 4887

1. 4300 0.1819 0. 7 50 0 (Combined Loading) 1/Circumference AlloHabl e a/t

0. 0000 0.7500

0. 1 000 0.7500

0. 2000 0. 7500 0.3000

0. 6968

0. 4000

0. 5659

0. 5000 0.4936

0. 6000 0. 4525

0. 7500

0. 4302 Table C-5310-5 used Report No. 1600539.401RO B-6

Stress Ratio Z factor 1/ circumference = alloHable a/t 0.3766

1. 4300 0.1619

0. 7500 (Membrane Loading) 1/Circumference AlloHable a/t

0. 0000

0. 7 500

0. 1 000

0. 7 500 0.2000

0. 7 500

0. 3000 0.7500

o. 4000 0.7500

0. 5000

0. 7346

0. 6000 0.6606 0.7500

0. 6232 Note : All oNable crack size is calculated based on the failure mode indicated by the screening criteria \\-Jhich is based on the input crack size Number of Runtime l'larnings : 0

- - End of pc-CRACK output ***

Report No. 1600539.401RO B-7 I} Slnlctutallllletlrlly Associates. Inc.*

LeveiD.rpt pc-CRACK 4. 2 CS Version Control No. 4. 2. 0. 0 Beta Structural Integrity Associates, Inc. \\>lNVl. structint. corn pccrack@structint. com Date: 11/11/2016 11:02 Input Data read from C: \\Users\\mfong\\Do;;,uments\\01. Project\\05. DCPP\\1600539\\Allm*lable FlaH Size\\LevelD. pcf Analysis

Title:

LevelD Units Selected: US Customary Linear Dimensions - inches Stress - ksi Load - kips Temperature - deg F Time - hours Jic - in-lbs/in'2 Analysis Type: ASME Section XI I\\"IB-3640 (2004) Crack Geometry Orientation: Circumferential Crack Depth = Crack Length = Pipe Geometry 0.3400

8. 0000 Nominal Pipe Size =

14. 0000 Outer Diameter =

14. 0000 Wall Thickness =

1. 4200 Service Level: D The allov1able fla\\-1 size is determined using Tables stresses Pm =

Pb = 6. 6100 (safety factor =

1. 0300 (safety factor =

Pe = 12.8040 K (Residual Stress) = Naterial: Stainless Steel Flux Held FloH Stress

0. 0000 45.1500 Number of Warnings in Inputs: 0 Analysis Results

1. 3000)

1. 4000)

Failure Mode per Screening Criteria: EPFM (Class 1 screening rules used) Table C-5310-4 used Stress Ratio Z factor 1/ circumference = a l lo1;able a/t

0. 5316

1. 4300 0. 1819

0. 7500 (Combined Loading)

!/Circumference Allo;~able a/t

0. 0000 0.7500 0.1000

0. 7500

0. 2000 0.7500

0. 3000

0. 7215

0. 4000

0. 6052

0. 5000

0. 5215

0. 6000 0.4747 0.7500 0.4379 Table C-5310-5 used Report No. 1600539.401RO B-8

Stress Ratio Z factor 1 / circumference = allo>~able a/ t

0. 2722

1. 4300 0.1819 0. 7500 (Membrane Loading~

!/Circumference Allo>~able a/t

0. 0000

0. 7500 0.1000

0. 7500

0. 2000

0. 7500

0. 3000 0. 7500

0. 4000

0. 7500

0. 5000

0. 7500

0. 6000

0. 7500 0.7500

0. 7139 Note: AlloNable crack size is cal culated based on the failure mode indicated by the screening criteria vrhich is based on the input crack size Number of Runtime ~*larnings: 0

- - End of pc-CRACK output ***

Report No. 1600539.401RO B-9 e Stnlctutallnlegrlty Associates, Inc.*

Casel (ASME).rpt pc-CRACK 4. 2 CS Version Control No. 4. 2. 0. 0 Beta Structural Integrity Associates, Inc. \\-1\\ol\\*1. structint. corn pccrack@structint. com Date: 03/14/2017 09:08 Input Data read from C: \\Users\\mfong\\Documents\\01. Project\\05. DCPP\\1600539\\304 Crack Gro1*1th\\Support Files_ 304 \\pc-CRACK\\Crack Grm*lth _ris e time 360 _sec 450\\Casel (ASME).pcf Analysis

Title:

Diablo Canyon Units Selected: US Customary Linear Dimensions - inches Stress - ksi Load - kips Temperature - deg F Time - hours Analysis Type: Crack GroHth (LEFM) Crack Gr01*1th Calculation Method - Cycle/Time Stepping Maximum Number of Load Blocks = 100 Block Print Interval = 1 Crack Model: 309-Semi-Elliptical Cir cumferential Crack in Cylinder on the Inside Surface (Chapuliot) Crack Depth, a = 0.34 0 0 Half Crack Length, c =

4. 0000

~/all Thickness, t = 1.4200 Inside Radius, Ri =

5. 5800 Aspect ratio allo\\-1ed to vary Maximum a/t = 0.8 Crack Depth Print Increment for SIF Tabulation = 0. 1 Maximum Aspect Ratio (c/a) for SIF Tabulation = 20 Aspect Ratio Increment for SIF Tabulation = 1 Total Load Cases: 6 Load Case 1: Pres Type: Stress Coefficients Input by User Coefficient CO =

Coefficient Cl = Coefficient C2 = Coefficient C3 = 1.87 09 -0.2827 0.2616 -0.1113 Load Case 2: Thermal max Type: Stress Coefficients Input by User Coefficient CO = Coefficient Cl = Coefficient C2 = Coefficient C3 = Load Case 3: DW 21.0140 -7 8.0730 69.4980 -20.254 0 Type: Stress Coefficients Input by User Coefficient CO = Coefficient Cl = Coefficient C2 = Coefficient C3 = 0.1130 0. 0000

0. 0000

0. 0000 Load Case 4: CrkFacePressure Type: Stress Coefficients Input by User Coefficient CO =

Coefficient Cl = Coefficient C2 = Coefficient C3 =

1. 0000

0. 0000

0. 0000 0. 0000 Report No. 1600539.401RO B-10

!S) Sttuctum lnlefrlty Associates. Inc!'

Load Case 5: Thermal min Type: Stress Coefficients Input by User Coefficient CO = Coefficient Cl = Coefficient C2 = Coefficient C3 = -32.0170 62.2440 -46.5710 12. 1 530 Load Case 6:Residual 70 Type : Stress Coefficients Input by User Coefficient CO = Coefficient Cl = Coefficient C2 = Coefficient C3 =

30. 3706

-227. 2910 289.2005 -88. 6581 Total Load Sub-Blocks: 8 Load Sub-Block # 1 Load Sub-block Name: Thermal_Fatigue 100 Maximum Load Case Multiplier Load Case ID

2. 2350 Pres

1. 0000 D\\*1

1. 0000 Thermal max

2. 2350 CrkFacePressure

1. 0000 Residual 70 Ninimum Load Case Multiplier Load Case ID

2. 2350 Pres 1.oooo m1

1. 0000 Thermal min

2. 2350 CrkFacePressure

1. 0000 Residual 70 Growth Law: TableDADN Cycles/Time: 876 Calc. Interval: 1 Print Interval: 876 Load Sub-Block # 2 Load Sub-block Name: Thermal_Fatigue 72 Maximum Load Case Multiplier Load Case ID

2. 2350 Pres

1. 0000 Dl'l

2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 6800 Thermal max Minimum Load Case Multiplier Load Case ID

2. 2350 Pres

1. 0000 Dl'l 2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 6800 Thermal min Gro1*1th Law : TableDADN Cycles/Time: 876 Cal c. Interval: 1 Print Interval: 876 Load Sub-Block # 3 Load Sub-block Name: Thermal_Fatigue 45 Naxirnum Load Case Multiplier Load Case ID

2. 2350 Pres

1. oooo m1

2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 3950 Thermal max Minimum Load Case Multiplier Load Case ID 2. 2350 Pres Report No. 1600539.401RO B-11 l}

Stnu:tui'BI llllegrlty Associates, fnc.*

1. 0000 2.2350 1.0000

0. 3950 GroHth LaH: TableDADN Cycl es/Time: 1752 Cal c. Interval: 1 Print Interval: 17 52 Load Sub-Block # 4 CrkFacePressure Residual 70 Thermal min Load Sub-b l ock Name: Thermal _Fatigue 34 Maximum Load Case Multiplier Load Case ID

2. 2350 Pres

1. 0000 DW

2. 2350 CrkFacePressure

1. 0000 Res i dual 70 0.2800 Thermal max Minimum Load Case Multiplier Load Case ID 2.2350 Pres

1. 0000 DW

2. 2350 CrkFacePressure 1. 0000 Residual 70 0.2800 Thermal min GroHth La~n TableDADN Cycles/Time: 5256 Calc. I nterval : 1 Print I nterval: 5256 Load Sub-Block # 5 Load Sub-b l ock Name: Thermal_Fatigue 22 Maximum Load Case Multiplier Load Case ID

2. 2350 Pres

1. 0000 01'1 2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 1550 Ther mal max Minimum Load Case Multipl ier Load Case ID

2. 2350 Pres

1. 0000 Dl'l 2. 2350 CrkFacePressure

1. 0000 Residual 70 0.1550 Thermal min GroHth La~n TableDADN Cycles/Time: 10512 Calc. Interval: 1 Pri nt Interval: 10512 Load Sub-Bl ock # 6 Load Sub-b l ock Name : Thermal_Fatigue 9 Maximum Load Case Mul tipl ier Load Case ID

2. 2350 Pres

1. 0000 D\\'1

2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 0650 Thermal max Minimum Load Case Mul tipl ier Load Case I D

2. 2350 Pres

1. 0000 D\\*1 2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 0650 Thermal min GroHth La1;: TableDADN Cycles/Ti me: 876 Calc. Interval : 1 Pri nt Interval : 876 Load Sub-Block # 7 Report No. 1600539.401RO B-12 SJstnu:tutal Integrity Associates, Inc.*

Load Sub-block Name : Thermal_Fatigue 4 Haxi mum Load Case Hul tiplier Load Case ID

2. 2350 Pres

1. 0000 D\\"1

2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 0200 Thermal max Ninimum Load Case Multiplie r Load Case ID

2. 2350 Pres

1. 0000 Del 2. 2350 CrkFacePr essure

1. 0000 Residual 70

0. 02 00 Thermal min Gro1-1th La1-1: Tabl eDADN Cycles/Time: 876 Calc. Interval: 1 Print Interval: 876 Load Sub-Block # 8 Load Sub-block Name: SCC Maximum Load Case Hultipli er Load Case ID 2. 2350 Pres

1. 0000 D\\"1

2. 2350 CrkFacePressure

1. 0000 Residual 70

1. 0000 Thermal max GrO\\;th Law: sec Cycles/Time: 730 Calc. Interval: 1 Pri nt Interval: 730 Material Library Option -

Default Material : 13 Diabl o Canyon Stainless Steel 2: ASME Austenitic Steel in Air Table (da/dn-DK) No. of R ratios in the tables = 12 R Ratio =

1. OOOE-20 Delta K da/dn 1. OOOE-03

1. OOOE-20 0.1000

1. 670E-1 3 1 0.0000

6. 630E- 07 20.0000 6. 530E-06

30. 0000 2. 490E-05

40. 0000 6. 430E-05

50. 0000

1. 340E-04

60. 0000

2. 450E-04 70.0000

4. 080E- 04 80.0000 6.340E-04

90. 0000

9. 340E- 04 100. 0000

1. 320E-03 R Ratio =

0.1000 Delta K da/dn 1. OOOE-03

1. OOOE-30 0.1000

1. 980E-13

10. 0000 7. 880E-07 20.0000

7. 760E-06

30. 0000

2. 960E-05 40.0000

7. 650E-05

50. 0000

1. 600E-04 60. 0000

2. 910E-04 70.0000

4. 850E- 04

80. 0000

7. 530E-04

90. 0000 1.110E-03 100. 0000

1. 570E-03 Report No. 1600539.401RO B-13 l}

Stnu:lutalllllegrlly Associates. Inc.*

R Ratio =

0. 2000 Delta K da/dn

1. OOOE- 03

1. OOOE-30 0.1000 2.300E-13

10. 0000 9. 14 OE-07 20.0000

9. OOOE- 06

30. 0000

3. 430E-05 40.0000 B. B60E-05

50. 0000

1. B50E- 04

60. 0000

3. 3BOE-04 70.0000

5. 620E-04 BO. 0000 B. 730E- 04 90.0000

1. 290E-03 100. 0000

1. B20E- 03 R Ratio =

0. 3000 Delta K da/ dn l. OOOE-03 l. OOOE-30 0.1000 2.610E-l3 10.0000

1. 040E-06 20.0000

1. 020E-05

30. 0000

3. 900E-05 40.0000

1. OlOE-04

50. 0000 2.100E-04 60.0000 3.B40E-04 70.0000 6.390E- 04 80. 0000 9. 930E-04

90. 0000

1. 4 60E-03 100. 0000 2.070E-03 R Ratio =

0. 4000 Delta K da/dn

1. OOOE- 03 1. OOOE-30 0.1000 2.920E-13 10. 0000 1.160E-06 20.0000 1.150E-05 30.0000

4. 370E-05 40. 0000 1.130E-04

50. 0000

2. 360E-04 60. 0000

4. 31 0E- 04 70.0000 7.160E- 04 BO. 0000 1.110E-03 90. 0000

1. 640E- 03 100. 0000 2. 320E-03 R Ratio =

0. 5000 Delta K da/dn

l. OOOE- 03 1. OOOE-30 0.1000 3. 240E-13

10. 0000 1. 290E- 06 20.0000

1. 270E-05 30.0000 4. B40E-05 40. 0000 1.250E-04

50. 0000

2. 610E-04 60. 0000 4.770E-04

70. 0000

7. 930E-04 BO. 0000 1. 230E- 03 90.0000

1. B20E- 03 100.0000

2. 570E- 03 R Ratio =

0. 6000 Delta K da/ dn

1. OOOE-03 1. OOOE-30

0. 1000 3.550E-13 10.0000

1. 410E- 06 20.0000 1.390E-05

30. 0000

5. 310E-05 40.0000

1. 370E-04 5 0.0000 2. B70E-04

60. 0 000

5. 230E-04 Report No. 1600539.401RO B-14 l}slnlctunrlhllegrlty Associates. Inc.*

70.0000

8. 700E-04 80.0000 1. 350E- 03

90. 0000

1. 990E-03 100. 0000

2. 820E-03 R Ratio =

o. 7000 Delta K da/dn

1. OOOE- 03

1. OOOE-30 0.1000

3. 870E-13 1 0. 0000 1. 540E-06

20. 0000 1. 520E- 05

30. 0000

5. 780E-05 40.0000

1. 490E-04

50. 0000 3. 120E-04 60.0000

5. 7 00E-04

70. 0000

9. 470E-04

80. 0000

1. 4 70E-03

90. 0000 2. 170E-03 100. 0000

3. 070E-03 R Ratio =

0. 7900 Delta K da/dn

1. OOOE-03 1. OOOE-30 0.1000 4.150E-13 10. 0000

1. 650E- 06 20. 0000

1. 630E- 05

30. 0000

6. 2 10E-05 40.0000

1. 600E-04

50. 0000 3. 350E-04

60. 0000

6. ll OE-04

70. 0000

1. 020E-03

80. 0000 1. 580E- 03

90. 0000 2. 330E-03 100. 0000 3. 300E-03 R Ratio =

0. 8000 Delta K da/dn 1. OOOE- 03

1. OOOE-30 0.1000

5. 040E-13

10. 0000

2. 010E- 06

20. 0000

1. 980E-05

30. 0000

7. 530E-05 40.0000

1. 950E-04

50. 0000

4. 060E-04

60. 0000

7. 420E- 04

70. 0000

1. 230E-03 80. 0000

1. 920E- 03

90. 0000 2. 830E-03 100. 0000

4. OOOE- 03 R Ratio =

0. 9000 Delta K da/dn

1. OOOE-03 1. OOOE-30 0.1000

1. 470E-12 10. 0000 5. 850E-06

20. 0000 5. 760E- 05

30. 0000 2. 200E- 04 40.0000 5. 680E-04 50. 0000

1. 190E-03 60.0000

2. 160E-03 70.0000

3. 600E-03 80. 0000

5. 590E-03

90. 0000 8. 240E-03 100. 0000

0. 0117 R Ratio =

0. 9990 Delta K da/dn 1. OOOE-03

1. OOOE-30

9. 999E+03 1. OOOE-30 No. of Data in the KI C Table = 2 Report No. 1600539.401RO B-15 l)slnlctuiVI IJJtegrlty Associates. 1nc.*

Crack Depth 0.0000

2. 0000 KIC 200.0000 200.0000 Stress Corrosion Crack GrO\\*lth Equation C =

2. 420E-07 2.1810 K Threshold =

0. 0000 Stress Corrosion Cracking (SCC) Crack GroHth LaH The Crack Gro~<th Rate in/h (or rn/h) is given by:

da/dt = c * (Krnax) 'n Hhere c, n = empirical constants da/ dt = 0 for Krnax < K Threshold messages/Warnings: Soluti on for Ri/t of 0. 2 and 0. 5 Hill be used Number of Warnings in Inputs: 0 ANALYSIS RESULTS - STRESS INTENSITY FACTORS Load Case # 1 : Pres

Crack Dimensions ------------

K at tips a/t c/a c/a = 11.7647

0. 3400

4. 0000

0. 2394 11.7647

2. 2330 0.7366

0. 4400 5.1765

0. 3099 11.7647

2. 6731

0. 8553

0. 5400 6.3529

0. 3803 11.7647 3.1092

0. 9668

0. 6400

7. 5294

0. 4507 11.7647

3. 6043

1. 0759 0. 7400 8. 7059

0. 5211 11.7647 4.1356 1.1 831 0.8400

9. 8824

0. 5915 11.7647

4. 6826

1. 2884

0. 9400 11.0588

0. 6620 11.7647 5. 3761 1.4035

1. 0400 12.2353

0. 7324 11.7647 6.1159

1. 5205 c/a =

12.7647

0. 3400

4. 3400

0. 2394 12.7647

2. 2445

0. 7129 0. 4400

5. 6165

0. 3099 12.7647

2. 6914 0.8275

0. 5400 6. 8929 0.3803 12.7647 3.1352 0.9349 0. 6400 8.1694

0. 4507 12.7647

3. 64 05

1. 0388

0. 7400 9.4459 0. 5211 12.7647 4.1837 1.14 02 0.8400

10. 7224

0. 5915 12.7647

4. 7436 1.2394

0. 9400 11.9988 0. 6620 12.7647 5. 4398

1. 3444

1. 0400 13.2753

0. 7324 12.7647 6.1805

1. 4500 c/a =

13.7647

0. 3400

4. 6800

0. 2394 13.7647 2.2544

0. 6927 0. 4400

6. 0565

0. 3099 13.7647

2. 7070 0.8037 0.5400 7.4329

0. 3803 13.7647 3.1575

0. 9076

0. 6400 8.8094

0. 4507 13.7647

3. 6715

1. 0071 0.7400

10. 1859

0. 5211 13.7647 4.2248 1.1035

0. 8400

11. 5624 0.5915 13.7647 4.7957 1.1976

0. 9400 12.9388

0. 6620 13.7647 5.4942 1.2938

1. 0400

14. 3153

0. 7324 13.7647 6.2357

1. 3897 c/a =

14.7647

0. 3400

5. 0200

0. 2394 14.7647

2. 2629 0. 67 53 Report No. 1600539.401R~

B-16 e Stnlctural Integrity Associates, Inc!'

0. 4400 0.5400 0.6400

0. 7400 0.8400 0.9400 1.0400

6. 4965 7. 9729

9. 4494

10. 9259 12.4024 13.8788

15. 3553 c/a=

15.7647

0. 3400 0.4400 0.5400 0.6400

0. 7400 0.8400 0.9400 1.0400

5. 3600

6. 9365

8. 5129 10.0894

11. 6659 13.2424

14. 8188

16. 3953 c/a =

16.7647 0.3400 0. 4400

0. 5400 0.6400

0. 7400

0. 8400 0.9400 1.0400

5. 7000 7. 3765 9. 0529

10. 7294 12.4059

14. 0824 15.7588 17.4353 c/ a =

17. 7 64 7 0.3400 0.4400

0. 54 00

0. 64 00

0. 7400 0.8400

0. 9400

1. 04 00

6. 0400

7. 8165 9. 5929

11. 3694 13.1459

14. 9224 16.6988 18.4753 c/a=

18.7647 0.3400 0.4400 0.5400

0. 64 00 0.7400 0.8400

0. 94 00

1. 0400

6. 3800

8. 2565

10. 1329

12. 0094 13.8859 15.7624 17. 6388 19.5153 c/a =

19.7647

0. 3400 0. 4400

0. 5400

0. 6400

0. 7400 0. 8400 0.9400

1. 04 00

6. 7200

8. 6965

10. 6729 12.6494 14.6259 16.6024 18.5788 20.5553 Load Case # 2: Thermal max

0. 3099

0. 3803 0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099 0. 3803

0. 4507

0. 5211

0. 5915 0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324 14.7647 14.7647 14.7647 14.7647 14.7647 14.7647 14.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 16.7647 16. 7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 17.7647 17.7 647 17.7647 17.7647 17.7647 17. 7647 17.7647 17.7647 18.7647 18.7647 18.7647 '

18.7647 18.7647 18.7647 18.7647 18.7647 19.7647 19.7647 19.7647 19. 7647 19.7647 19.7647 19.7647 19.7647

Crack Dimensions - -----------

c/a = 11.7647

0. 3400

0. 44 00

0. 5400

0. 6400

0. 7400

0. 8400 0.9400

4. 0000 5.1765

6. 3529 7. 5294

8. 7059

9. 8824

11. 0588 a/t c/a

0. 2394

0. 3099 0.3803

0. 4507

0. 5211

0. 5915

0. 6620 11.7647 11.7647 11.7647 11.7647 11.7647 11.7647 11.7647 Report No. 1600539.401RO

2. 7205 3.1767

3. 6983

4. 2604 4.8407

5. 5413

6. 2834

2. 2703

2. 7324 3. 1935

3. 7216

4. 2914

4. 8800

5. 5823

6. 3251 2.2748

2. 7378 3.2000

3. 7293

4. 3005

4. 8905

5. 5969

6. 3443

2. 2781

2. 7412 3.2033

3. 7324

4. 3032 4.8929

5. 6035

6. 3562 2. 2811

2. 7443 3.2063

3. 7352 4. 3057

4. 8950

5. 6094

6. 3669 2.2838 2.7470 3.2089

3. 7377 4. 3079

4. 8969

5. 614 7 6.3765

0. 7831

0. 8840 0.9797 1.0718 1.1614

1. 2501

1. 3376

0. 6600

0. 7651 0. 8634

0. 9558 1.0441

1. 1299

1. 2120 1.2921

0. 6267

0. 7265 0. 8198

0. 9072

0. 9908

1. 0718 1.14 88

1. 2238

0. 5915

0. 6856 0.7736

0. 8562

0. 9350 1.0115 1.0841 1.1549

0. 5599 0.6491 0.7324

0. 8105

0. 8852 0. 9576

1. 0263

1. 0933 0.5316

0. 6162

0. 6954

0. 7695 0.8404

0. 9091 0.9744

1. 0380 K at tips

10. 5427

9. 3196

7. 7110 6. 0985 4.4077

2. 6295 0.8437

7. 6160

8. 5825

9. 3948 1 0.1096 10.7358 11.2786 11.7745 B-17 e

Slnll:tunrlllllegrlly Associates. Inc.*

l. 0400 12.2353 cia=

12. 7647 0.3400 0.4400 0.5400 0.6400

o. 7400 0.8400 0. 9400 1.0400

4. 3400

5. 6165

6. 8929 B. 1 694 9.4459 10.7224

11. 9988 13.2753 cia=

13. 7647 0.3400 0.4400 0. 5400

0. 6400 0. 7400

0. 8400

0. 9400

l. 04 00

4. 6800

6. 0565 7.4329 B. 8094 10.1859

11. 5624

12. 9388

14. 3153 cia=

14.7647

0. 34 00 0.4400

0. 54 00

0. 64 00

0. 7400 0.8400

0. 9400

l. 0400

5. 0200

6. 4965

7. 9729

9. 4494

10. 9259 12.4024 13.8788 15.3553 cia =

15.7647 0.3400 0.4400 0.5400 0.6400

0. 7400 0.8400 0.9400 1.0400

5. 3600

6. 9365 B. 5129 10.0894

11. 6659 13.2424

14. 81 88 16.3953 cia =

16.7647

0. 3400

0. 4400 0.5400

0. 6400

0. 7400 0. 84 00

0. 94 00

l. 04 00 5. 7000 7.3765 9. 0529 10.7294 12.4059 14. 0824 15.7588 17. 4353 cia=

17.7647

0. 3400

0. 4400 0.5400

0. 64 00

0. 7400 0.8400 0.9400 1.0400

6. 0400

7. 8165 9.5929

11. 3694

13. 1459

14. 9224 16. 6988 18.4753 cia =

18.7647 0.3400 0.4400

0. 5400

0. 64 00

0. 7400 0.8400

6. 3800 B. 2565 10.1329

12. 0094 13.8859 15.7624

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099 0.3803

0. 4507

0. 5211

0. 5915

0. 6620 0.7324 0.2394

0. 3099

0. 3803

0. 4507

o. 5211

0. 5915

0. 6620

0. 7324 0. 2394

0. 3099

0. 3803 0.4507

0. 5211 0. 5915

0. 6620

0. 7324

0. 2394

0. 3099

0. 3803 0.4507

0. 5211

0. 5915

0. 6620

0. 7324 0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620 0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915 11.7647 12.7647

12. 764 7 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 14. 7647 14.7647 14.7647 14.7647 14.7647 14.7647 14. 7647 14.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15. 7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.764 7 16.7647 17. 7647 17.7647 17.7647 17. 7647 17.7647 17. 7647 17.7647 17.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.7647 Report No. 1600539.401RO

-l. 0736

10. 6143

9. 4159

7. 8257 6.2284 4.5428

2. 7579

0. 9352

- l. 0198 10.6755

9. 4 982

7. 9237

6. 3393

4. 6583

2. 8676 1. 0135

- 0.9738 10.7284

9. 5693 B. 0084 6.4353

4. 7582

2. 9625

l. 08 11

-0.9340

10. 7746

9. 6314 8. 0824 6.5190

4. 8454 3. 0453 1.1402

-0.8993 10.7979

9. 6516 8.0975

6. 5299

4. 8525

3. 0492

1. 1387

-0. 9098 10.8135

9. 6595 B. 0964

6. 5212

4. 8387

3. 0327 1.1217

- 0. 9312 10.8275 9. 6665 B. 0954

6. 5135 4.8263

3. 0178 12.1977 7. 4073 B. 3584 9.1632 9.8660 1 0.4800

11. 0139 11.4945

11. 9073

7. 2290 B. 1669 B. 9652 9. 6577 10.2613 10.7876

11. 2551 11.6591

7. 0748 B. 0013 B. 7940 9.4776 10. 0723

10. 5920 11.0482 11. 4445

6. 9402 7. 8568 B. 6446

9. 3204

9. 9072

10. 4212 10.8675 11.2571 6.5957 7.4684 B. 2193 B. 8627

9. 4211

9. 9105 1 0.3343 10.7048

6. 2245 7.0480

7. 7566 B. 3638 B. 8908

9. 3526

9. 7526 10.1022 5.8928

6. 6724

7. 3432

7. 9181 B. 4170 B. 8542 B-18

!S)s~roc:tum Integrity Associates, 1nc.*

0. 9400

1. 0400 17.6388 1 9.5153 c/a =

19.7647 0. 3400 0.4400 0.5400 0.6400

0. 7400 0. 6400 0. 9400 1.0400 6.7200

6. 6965 1 0.6729 12.6494

14. 6259 16.6024 16.5788

20. 5553 Load Case # 3: DW

0. 6620

0. 7324

0. 2394

0. 3099 0.3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324 18.7647 18.7647 19.7647 19.7647 19.7647 19.7647 19.7647 19.7647 19.7647 19.7647

Crack Dimensions ------------

c/a= 11.7647 0.3400 0. 4400 0.5400 0. 6400

0. 7400

0. 6400

0. 9400

1. 04 00 4. 0000 5.1765

6. 3529

7. 5294

8. 7059 9.8824 11. 0588

12. 2353 c/ a =

12. 7 64 7

0. 34 00 0.4400

0. 5400 0.6400 0. 7400 0.8400 0.9400 1.0400

4. 34 00

5. 6165

6. 8929

8. 1694 9.4459

10. 7224 11.9988 13.2753 c/a =

1 3.7 647

0. 3400 0.4400 0. 5400 0.6400 0. 7 400 0.6400 0.9400

1. 0400

4. 6800 6. 0565 7. 4329

8. 8094 10.1859 11.5624

12. 9368 1 4. 3153 c/a =

14.7647 0.3400 0.4400 0.5400

0. 6400 0. 7400 0.8400 0.9400

1. 0400

5. 0200 6.4965

7. 9729 9.4494

10. 9259 12.4024

13. 87 68

15. 3553 c/a =

15. 7647

0. 3400 0.4400 0. 5400 0. 6400

0. 7400 0.8400 0.9400

1. 0400 5. 3600

6. 9365

8. 5129 10. 0894 11.6659 13.2424 14. 81 88 16.3953 c/a =

16.7647 0.3400

5. 7000 a/t c/a 0.2394

0. 3099 0.3803 0.4507

0. 5211

0. 5915

0. 6620

0. 7324 0.2394 0.3099 0.3803 0.4507 0. 5211 0.5915 0. 6620

0. 7324 0. 2394

0. 3099

0. 3803 0.4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915 0. 6620

0. 7 324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7 324

0. 2394 11.7647 11.7647 11.7647 11.7647 11.7 647 11.7647 11.7647 11.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7 647 13.7647 13.7 647 14. 7647 14.7647 14.7647 14.7647 14.7647 14.7647 14.7647 14.764 7 15.7647 15.7647 15.7647 15.7647 15.764 7 15.7647 15.7647 15.7647 16.7647 Report No. 1600539.401RO 1.1066

- 0. 9502 10. 8401

9. 6728 8. 0945

6. 5065

4. 8151 3. 0045

1. 0931

-0.9673 9.2329

9. 5638

5. 5946 6.3348

6. 9717 7.5175

7. 9911

8. 4062

8. 7657 9.0800 K at tips 0.1382 0.1662

0. 1 941

0. 2257

0. 2596

0. 294 9

0. 3394

0. 3871

0. 1389 0.1673 0.1957 0.2260

0. 2626 0.2987 0.3434

0. 3912 0. 1395 0.1683

0. 1971

0. 2299 0.2653

0. 3020 0.3469 0. 3947 0. 1400 0.1691 0.1983

0. 2316

0. 2676 0.3048 0.3498

0. 3977 0.1405 0.1699

0. 1 993

0. 2330 0.2695

0. 3073 0.3524 0.4003 0.1408

0. 0446 0. 0519

0. 0587

0. 0654

0. 0720 0.0785

0. 0857

0. 0930

0. 0432

0. 0502

0. 0568

0. 0632

0. 0694

0. 0755 0.0620

0. 0686

0. 0420 0.048 7

0. 0551

0. 0612

0. 0671 0.0729 0.0789

0. 0846

0. 04 09 0. 04 7 5

0. 0537

0. 0595 0. 0652 0. 0707

0. 0762

0. 0816 0.0400

0. 0464

0. 0524

0. 0581

0. 0635

0. 0688

0. 0738 0.0788

0. 0380 B-19 SJstnlctuiVI llllefrlly Associales, Inc!'

0. 4400

0. 5400

0. 6400

0. 7400 0.8400 0.9400

1. 0400 7. 3765

9. 0529 10. 7294 12.4059

14. 0824 15.7588

17. 4353 c/a =

17.7647

0. 3400 0.4400 0.5400 0.6400 0. 7400 0.8400

0. 9400

1. 0400

6. 0400

7. 8165 9.5929

11. 3694 13.145 9 14. 9224 16.6988 18.4753 c/a =

1 8.7647

0. 3400 0.4400 0.5400 0.6400

0. 7400 0.8400

0. 9400

1. 0400 6.3800

8. 2565 10.1329

12. 0094 13.8859 15.7624 17.6388

19. 5153 c/a =

19.7647 0.3400 0.4400 0.5400 0. 6400

0. 7400 0.8400

0. 9400 1. 0400 6.7200 8. 6965 10.6729 12.64 94 14.6259 16. 6024 18.5788

20. 5553

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099 0.3803 0.4507 0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099 0.3803 0.4507

0. 5211

0. 5915 0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 17.764 7 17.7647 17.764 7 17.7647 17.7647 17.7647 17.7647 17.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.7647 19.7647 19.7647 19.7647 19.7647 19. 7647 19.7647 19.7647 19.7647 Load Case # 4: CrkFacePressure Crack Dimensions - - ----------

cia= 11.7647 0.3400 0.4400

0. 5400

o. 6400

0. 7400 0. 8400 0.9400 1.0400

4. 0000

5. 1765

6. 3529

7. 5294

8. 7059

9. 8824

11. 0588 12.2353 c/a =

12. 7647 0.3400 0.4400 0.5400

0. 6400 0. 7400 0.8400 0. 9400 1.0400 4. 3400 5. 6165 6. 8929

8. 1694 9.4459

10. 7224

11. 9988 13. 2753 c/a=

13.7647 0.3400 0.4400 0.5400

o. 6400 0.7400 0.8400 0.9400

4. 6800

6. 0565

7. 4329

8. 8094 10. 1859 11. 5624

12. 9388 a/t

c/a

0. 2394

0. 3099

0. 3803

0. 4507

o. 5211

0. 5915

0. 6620 0.732 4

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394 0.3099

0. 3803 0.4507

0. 5211

0. 5915

0. 6620 11.7647 11.7647 11. 7647 11.7647 11.7647 11.7647 11. 7647 11.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 Report No. 1600539.401RO

0. 1702 0. 1997

0. 2335 0.2701 0.3079

0. 3533

0. 4015 0.1410 0.1704

0. 1999

0. 2337 0.2702

0. 3081 0. 3537

0. 4023 0. 1412 0. 1706 0.2001 0.2339 0.2704

0. 3082

0. 3541

0. 4029 0.1413 0.1708 0. 2003 0.2340 0. 2705 0.3083

0. 3544

0. 4036 0.0440

0. 04 97 0. 0551

0. 0602 0. 0652

0. 0700

0. 074 6 0. 0358 0.0416 0.0469 0.0520

o. 0568

0. 0615

0. 0660

0. 0704

0. 0339 0.0393 0. 0444

0. 04 92 0. 0538

0. 0583

0. 0625

0. 0667

0. 0322

0. 0374 0. 0422

0. 0467

0. 0511 0. 0553

0. 0594

0. 0633 K at tips

1. 2229

1. 4 708

1. 7176

1. 9977

2. 2989 2_. 6099

3. 0039

3. 4258

1. 2292 1.4808

1. 7319

2. 0176

2. 3254

2. 6436

3. 0393

3. 4618

1. 2345 1.4894

1. 7441

2. 034 7 2.3481

2. 6725

3. 0695 0. 3950

0. 4592

0. 5197 0.5791 0.6375

0. 6951

0. 7 583

0. 8227

0. 3823

0. 4442

0. 5024

0. 5589

0. 6142

0. 6684 0.7259

0. 7840

0. 3714

0. 4313 0.4876 0. 5417

0. 5942

0. 6455

0. 6982 B-20

1. 0400

14. 3153 c/a=

14.7647 0. 3400 0.4400 0.5400 0.6400 0. 7400 0.8400 0. 9400

1. 0400 5.0200

6. 4 965 7. 9729 9. 4494 10.9259 12.4024 13.8788

15. 3553 c/a=

15.7647 0.3400 0. 4400 0.5400 0.6400 0.740 0

0. 84 00

0. 94 00

1. 04 00 5. 3600 6.9365

8. 5129 1 0. 0894 11.6659 13.2424 14.8188

16. 3953 c/a =

16. 7647 0. 3400 0. 44 00 0. 5400 0. 64 00

0. 7400 0.8400 0. 94 00 1.0400

5. 7000

7. 3765

9. 0529 10. 7294 12. 4059 14. 0824 15. 7588 17. 4353 c/a =

17.7647 0. 34 00 0. 4400

0. 54 00 0. 6400 0. 7400 0. 8400

0. 94 00

1. 0400 6. 040 0 7. 8165 9. 5929 11. 3694 13.1459 14. 9224 16. 6988 18.4753 c/a =

18. 7647 0. 3400 0.4400 0.5400 0.6400

0. 7400 0.8400 0. 9400

1. 0400 6. 3800 8. 2565 10.1329 12. 0094 13.8859 15.7624 17.6388 19. 5153 c/a =

19.7647 0. 3400 0.4400 0. 5400 0.6400

0. 7400 0.8400 0. 9400 1.0400

6. 7200

8. 6965 10.6729 12. 6494

14. 6259

16. 6024 18.5788 20.5553 Load Case # 5: Thermal min

0. 7324 0.2394 0. 3099 0.3803 0.4507

0. 5211 0. 5915

0. 6620

0. 7324 0. 2394

0. 3099 0. 3803 0. 4507

0. 5211

0. 5915 0. 6620 0. 7324 0.2394

0. 3099 0.3803 0. 4507

0. 5211 0. 5915 0.6620

0. 7324 0.2394

0. 3099 0. 3803

0. 4507

0. 5211

0. 5915 0. 6620

0. 7324

0. 2394 0. 3099

0. 3803 0. 4507

0. 5211 0. 5915 0. 6620

0. 7324

0. 2394 0. 3099

0. 3803 0. 4507

0. 5211

0. 5915

0. 6620 0. 7324 13.7647 14. 7647 14.7647 14. 7647 14.7647 14. 7647 14.7647 14.7647 14.7647 15.7647 15. 7647 15.7647 15. 7647 15.7647 15.7647 15. 7647 15. 7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 16. 7647 16.7647 17.7647 1 7.7647 17.7647 17.7647 17.7647 17.7647 17. 7647 17.7647 1 8. 7647 18.7647 18. 7647 1 8.7647 18.7647 1 8. 7647 18. 7647 1 8. 7647 19. 7647 19.7647 19.7647 19. 7647 19. 7647 19.7647 19.7647 19.7647

- ----------- Crack Dimensions - - - - -------- c/a= 11.7647 0.3400 0.4400

4. 0000 5. 1765 a/t c/a 0. 2394 0. 3099 11.7647 11.7647 Report No. 1600539.401RO

3. 4 925 1. 2392

1. 4967 1.7546 2.0494 2.3677 2.6974 3. 0956 3. 5191 1.2432

1. 5032

1. 7638 2. 0623

2. 384 9

2. 7192 3. 1184 3. 5423

1. 2457

1. 5062

1. 7674 2. 0665

2. 3899

2. 7250 3.1266 3. 5531

1. 24 7 5

1. 5081 1.7692 2. 0683

2. 391 5

2. 7264 3.1303

3. 5598 1.2491 1.5098

1. 7709

2. 0698 2. 3929

2. 7276 3. 1336

3. 5658

1. 2506 1.5113

1. 7724 2. 0712 2.394 1 2. 7287 3. 1 366 3. 5 712 0.7509

0. 3620

0. 4202 0.4748 0. 5267 0. 5769 0. 6258

0. 6743

0. 7223

0. 3537 0. 4105

0. 4636 0. 5137

0. 561 8

0. 6085 0. 6534 0.6973

0. 3359 0.3897 0. 4402 0. 4876

0. 5330

0. 5772 0. 61 92

0. 6603 0. 3170 0. 3678 0. 4154 0. 4 602

0. 5030 0. 5447

0. 5844 0. 6231 0. 3001 0. 3482

0. 3933

0. 4356

0. 4762

0. 5157

0. 5532 0. 5899

0. 2849

0. 3306 0.3734 0.4136 0. 4521

0. 4896

0. 5252 0. 5601 K at tips

- 26. 5825 - 12. 0951 -28.9648 -13. 8389 B-21 IJStntctunrlllllegrlty Associales.tnc.*

0. 5400 0.6400 0. 7400

0. 8400 0.9400 1.0400

6. 3529

7. 5294

8. 7059 9.8824

11. 0588 12.2353 c/a=

12.7647 0.3400 0.4400 0.5400 0.6400

0. 7400 0.8400

0. 9400

1. 0400

4. 3400

5. 61 65 6.8929

8. 1694 9.4459 10.7224 11.9988 13.2753 c/a=

13.7647 0.3400

0. 4400 0.5400

0. 6400

0. 7400 0. 8400 0. 9400

1. 0400

4. 6800 6. 0565

7. 4329

8. 8094 10.1859 11.5624

12. 9388 14. 3153 c/a =

14.7647 0.3400

0. 4400

0. 5400 0.6400

0. 7400 0.8400

0. 9400 1.0-ioo 5.0200 6.4965 7.9729

9. 44 94 10.9259 12.4024 13.878 8 15.3553 c/a=

15.7647 0.3400 0.4400 0.5400

0. 6400

0. 7400

0. 8400

0. 9400 1.0400 5.3600

6. 9365

8. 5129 10.0894 11.6659 13.2424

14. 8188 16.3953 c/a =

16.7647

0. 3400 0. 4400

0. 5400

0. 6400

0. 7400 0.8 400

0. 9400

1. 0400

5. 7000

7. 3765

9. 0529

10. 7294 12.4059

14. 0824 15.7588

17. 4353 c/a =

17. 7647 0.3400

0. 4400 0.5400

0. 6400 0. 7400 0. 8400 0. 9400 1.0400 6.0400

7. 8165 9.5929 11.3694 13.1459

14. 9224

16. 6988 18.4753 c/a =

18.7647 0.3400

6. 3800

0. 3803

0. 4507 0. 5211

0. 5915 0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394 0. 3099

0. 3803 0. 4507

0. 5211

0. 5915

0. 6620 0.7324

0. 2394 0.3099 0.3803 0.4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099 0. 3803

0. 4507

0. 5211

0. 5915 0. 6620 0.7324

0. 2394

0. 3099

0. 3803 0.4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620 0.7324 0.2394 11.7647 11. 7647 11.7647 11.7647 11.7647 11.7647 1 2.7 647

12. 7 647 12.764 7 12. 7647 1 2. 764 7 12.7647 12.7647 12.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13. 7647 14.7647 14. 7647 14.7647 14.7647 14.7647 14.7647 14.7647 14.7647 15.7647 15.7647 15.7647 15. 7647 15.7647 15.7647 15.7647 15.7647 16.7647 16.7647 16. 7647 16.7647 16.7647 16.7647 16.7647 16.7647 17.7647 17. 7647 17.7647 17. 764 7 17.7647 17. 7647 17.7647 17. 7647 18.7647 Report No. 1600539.401RO

-30.8671 -15.3982 -33.0917 -16.8576 -35.3854 -18.2262 -37.5765 -19.5069 -40.7151 -20. 8232 -43.9229 -22.0875 - 26.7336 - 11.7348 -29.1903 - 1 3.4319 -31. 1682 -14.952 1 -33.4846 -16. 3603 - 35.8740 -17.6730 -38.1566 -18.8996 -41.2803 -20.1244 - 44.4571 -21.2935 -26.8627 -11.4270 -29.3829 -13.0840 - 31. 4255 -14.5708 -33. 8204 - 1 5.9353 -36.2916 -17. 2 002 -38.6524 -18.3805 -41.7633 -19.5271 -44.9136 - 20. 6150 - 26.9744 -11.1608 -29.5495 -12.7832 -31.6479 - 14.241 2 - 34.1108 -15.5678 - 36. 6527 -16.7915 - 39. 0811 -17.931 8 - 42.1810 -19.0108 -45.308 4 -20. 0283 ' - 27. 0719 -10.9284 - 29.6949 -12.5206 - 31.8421 -13.9534 - 34. 3643 -15. 2469 - 36.9679 -16.4346 -39.4554 -17. 5400 -42. 5456 - 18.5599 -45.6530 -19.5160 - 27.1270 -10. 3818 -29.7552 -11.8951 -31. 9058 -13.2573 - 34. 4334 -14.4850 -37. 0434 -15.6110 -39.5374 -16.6587 - 42. 6516 -17.6199 -45.7838 -18.5197 - 27.1670 -9.7974 -29.7891 - 11.2255 - 31. 9312 -12.5111 - 34.4499 -13. 6696 -37.0517 -14.7322 -39. 5383 - 15.72 10 -42.6832 - 16.6281 -45.8498 -17.4772 - 27.2027 -9.2753 B-22 l} Slnlctunrllntegrtty Associates, Inc.*

0 0 4400 Oo5400 Oo6400 Oo7400 0 0 8400 0 0 9400

1. 0400 8 0 2565 10 o1329 12 0 0094 13 0 8859 15o 7624 17o6388 1 9 0 5153 c/a=

1 9o7647 Oo3400 Oo4400 Oo5400 0 0 6400 0 0 7400 Oo8400 0 0 9400

1. 0400 6o 7200 8 0 6965 1 0 0 6729 12o6494 14o6259 16o6024 18o5788 20 0 5553 Load Case # 6: Residual 70 Oo3099 Oo3803 Oo4507 Oo 5211 0 0 5915 0 0 6620 Oo7324 0 0 2394 0 0 3099 Oo3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 18 o7647 18o7647 18o7647 18o7647 18 o764 7 18o7647 18o7647 19o 7647 19o 7647 19 o 7647 19 o 7647 19 o 7647 190 7647 19o 7647 19 o 7647

Crack Dimensions ---------- --

c/a = 11 0 764 7 Oo3400 Oo4400 Oo5400 0 0 6400 Oo 7400 Oo8400 Oo9400 1.0400 4 0 0000 5 o1 765 6 0 3529 7 0 5294 8 0 7059 9o8824 110 0588 12 0 2353 c/ a = 12 o 7 64 7 Oo3400 Oo4400 Oo5400 0 0 6400 Oo 7400 Oo 8400 Oo9400 1.0400 4o3400 50 61 65 6 0 8929 8 0 1 694 9o4459 10 0 7224 11o 9988 13o2753 c/a = 13o7647 Oo 3400 Oo 4400 Oo5400 0 0 6400 Oo 7400 Oo8400 0 0 9400

1. 0400 4 0 6800 6 0 0565 7 0 4329 8 0 8094 1 0 0 1859 110 5624 12 0 9388 14 0 3153 c/a =

14o7647 Oo3400 0 0 4400 Oo5400 Oo 6400 0 0 7400 Oo8400 0 0 9400

1. 0400 5o0200 6 0 4965 7 0 9729 9 0 4494 1 0 0 9259 12o4024 13 0 8788 15 0 3553 c/a =

15o7647 Oo 3400 Oo 4400 Oo5400 Oo 6400 Oo 7400 0 0 8400 0 0 9400 50 3600 6 0 9365 8 0 5129 10 0 0894 11 o 6659 1 3 0 2424 14o8188 a/t c/a Oo2394 0 0 3099 0 0 3803 0 0 4507 Oo 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 Oo 4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 Oo3803 Oo 4507 Oo 5211 Oo 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 Oo4507 Oo 5211 0 0 5915 Oo 6620 0 0 7324 0 0 2394 0 0 3099 Oo3 803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 11.7647

11. 7647 11.7647

11. 7647 110 7647 11 o7647 11o 7647 11.7 647 12o7647 12o7647 12o7647 12o7647 12o7647 12 0 7647 12 0 7647 12 0 764 7 13o7647 13 0 7647 13 0 7647 13 0 7647 1 3 o7647 1 3o 7 64 7 13o7647 13o7647 14o7647 14o7647 14o7647 14 0 7647 14o7647 14o7647 1 4 o7 647 14o7647 150 7647 15o 7647 15o7647 15o7647 15o7647 15o 7647 15o 7647 Report No. 1600539.401RO

-29 0 8193 -10o 6273 - 31o 9538 -11. 8443 - 34o4646 -1209411 -37 0 0590 -13 0 9471 - 39o5392 -14 o8832 -42 0 7114 -15 0 7419 -45 0 9087 -16o 5458 -27 0 2348 - 8 0 8060 - 29o8464 -1 0 0 0896 -31.9742 -1102 451 - 34o4779 -12 o2864 -37 0 0657 -13o2414 -39 0 5399 -14 o1302 -42 0 7367 -14 0 9455 -45o 961 6 -15 0 7087 K at tips - 2 0 0065 -8 o7549 -14 0 8487 -190 87 1 6 -23 0 4902 -25 0 3235 -25 0 8381 -24 o1401 -1.9747 -8 0 7415 -140 8700 -1 9 0 9535 -23 0 6582 - 25 0 5922 -26 o1467 - 24 0 4566 - 1.9475 -8 0 7301 -14o8881 - 20 0 0236 -23 0 8018 - 25 0 8219 -26o 4105 - 24 0 7271 - 1. 9239 - 8 0 7202 - 14 0 9039 - 20 0 0841 -23 0 9259 - 26o0205 -26o 6385 - 24 0 9609 -1.9034 - 8 0 7116 -14o9176 -20 o1370 - 24 0 0343 - 26o 1939 -26 o 8376 10o0647 1 0o 9714 110 5877 12 0 0109 12 o2739 12 0 4025 12 0 3642 12 0 2159 9o8426 10 o7673 11.4176 110 8728 12 01682 12o331 6 12o3464 12 0 2571 9 0 6528 10 0 5930 11 o 2722 11 o 7547 1 2 0 0779 12 0 2 71 0 12 0 3312 12 0 2923 9o 4887 1 0 0 4422 11.1465 11 0 6526

11. 9998 1 2 0 2186 12 0 3181 1203227 9 0 3454 10 0 3105

11. 0368 11.5634 110 931 6 12 01728 12 0 3067 B-23 e

structunri/Riegrlly Associates. Inc.*

1. 0400 16.3953 c/a =

16.7647 0.3400

0. 4400

0. 5400 0.6400

0. 7400 0.8400 0.9400 1.0400

5. 7aoo

7. 3765

9. a529 10.7294 12.4059

14. a824 15.7588 17.4353 c/a =

17.7647 0.3400

0. 4400 0.5400

0. 6400 0.7400

a. 84aO a.94aa

1. 04aO 6.a400

7. 81 65

9. 5929 11.3694 13. 1459 14. 9224

16. 6988 18.4753 c/a =

18.7647

0. 3400 a.44aO a. 5400 a.64aO

a. 74aa a.84aa

0. 940a

1. a4aO 6. 38aa

8. 2565 1a. 1329

12. aa94 13.8859 15.7624 17.6388

19. 5153 c/a =

1 9.7647 0.3400

a. 44aa 0.540a

0. 6400

a. 74aa a.8400

a. 94 oa

1. 04 00

6. 7200

8. 6965 1a. 6729 12.6494

14. 6259

16. 6a24 18.5788

20. 5553

a. 7324

a. 2394

a. 3a99 0.3803 0.4507

0. 5211

a. 5915

a. 6620

0. 7324

a. 2394

a. 3099

a. 38a3

a. 4507

a. 5211

a. 5915

a. 662a

a. 7324

0. 2394

a. 3a99

a. 3803

0. 45a7

a. 5211

a. 5915

a. 662a a. 7324

0. 2394

a. 3099

a. 3803 0. 4507

a. 5211

a. 5915

a. 662a

a. 7324 CRACK GROWTH ANALYSIS RESULTS Total Subblock cycl es

/ Time Bl ocks: 876. ooao 17 52. aaaa Cycl es / Time 876. aaoo 876. aaaa 35a4. aaaa 1752. aaaa 876a. ooao 5256. oaoa

1. 927E+a4

1. 051E+a4

2. 015E+04 876. 0000 2.1a2E+04 876. oaoo 2.175E+a4 730.aaao Blocks:

2. 263E+04 876.aooa Kmax 13.3166 22.2013

9. 3a91

19. 9642 6.28a8 17.6278

4. 9315

16. 7391 3. 6677 15.6694

2. 8a63 14.8762

2. 3758 14.4795 9. 6651 24.a186

6. 5663 25. 6694 15.7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 17.7647 17.7647

17. 764 7

17. 764 7 17.7647 17. 7647 17.7647 17.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.764 7 18.7647 19.7647 19.7647 19.7647 19.7647 1 9.7647 19.7647 19.7647 19.7647 Kmin

-24. a236

a. 24 7 9

-16. a772

4. 6a55

- 8.4624

8. 6234

- 5. 5164 1a. 30aa -2.1154

12. a961

0. 3811 13.3777

1. 6296

14. 0184

- 3a. 3149 -0. 6622 Report No. 1600539.401RO -25.1651 -1.9027 -8.7283 - 14.9531 -20.1863 -24. 0904 - 26.2478 -26. 9a7a -25.2465 -1. 9a71 -8.7503 -14.9914 - 20. 2309 - 24.1287 - 26.267a -26.9378 - 25.2901 -1.9110 -8.7699 -15. a256 - 20. 2707 - 24. 1629 -26.2841 -26.9653 -25. 3291 -1.9145 -8.78 76 -15. a564 - za. 3065 - 24.1937 - 26.2995 - 26. 990a - 25. 3642 DeltaK 12.3492 8. 8895

9. 813a 1a. 51a6 11.0175 11.3732

11. 6a81

11. 7429 11.7914

8. 3891 9.26a6

9. 919a 10.3973 1 0.7330 1a. 9546

11. a819

11. 1277

7. 942a 8. 7671

9. 39a4

9. 8432 1a.161a 10.3708 1a. 4913 1a. 5347 7.54a2 8. 3235

8. 9153

9. 3452

9. 6469

9. 8461

9. 96a5 1 a. aa17 DaDn

/ DaDt 37.3403 5.125E-a5 21.9534

9. a55E-06 25.3863

1. 435E-05

15. 3588

3. 915E-a6 14.7432 2.387E-06

9. aa44

9. a22E-07 1 0.4479 7.661E-07

6. 4391

3. 344E-a7

5. 7831 1.088E-07

3. 5733

5. 454E-08 2.4252

7. 751E-09 1.4985 1.105E-08 0. 7462

2. 9a2E-10 0.4611 2.20aE-24

3. 4a8E-a5

2. 482E-a4 36. 8812 4.92aE-05 26. 3317

1. 619E-05 B-24 Crack Dimensions

0. 384 6

4. 0068

0. 3972

4. a1a 1

0. 4014

4. 0116

0. 4054

4. a134

a. 4065

4. 0139 a. 4 065

4. a139 a. 4065

4. 0139 0.4373

4. 1 887 a.4813

4. 2a11 a/t c/a 0.2708 10.418 1

a. 2797 1 a. a965 a.2826 9. 9951

0. 2855

9. 9001

a. 2 863

9. 8736

0. 2863

9. 8735 0. 2863 9.8735

0. 3079 9.5791 0. 339a

8. 7279 S)stmcturaiiRtefrlly Associates, Inc.*

2. 351E+04 876.0000 2.526E+04 1752. 0000

3. 051E+04 5256. 0000 4. 103E+04

l. 051E+04 4. 190E+0 4 876.0000 4. 27 8E+04 876.0000

4. 351E+04 730.0000 Blocks:

3. 1881 22.8492 0. 6951 20. 0569 - 0.2117 18.8789 -1.1985 17.6022 -1.9093 16.6841 -2.2647 16.2250 5.1764 26.0047

4. 438E+04 4. 526E+04 876.0000

2. 4621

27. 3602 876.0000

-1. 852E-04 4. 701E+04 1752.0000 5. 227E+04 5256. 0000 6. 27 8E+04

l. 051E+04 6. 366E+04 876.0000 6. 453E+04 876.0000 6. 526E+04 730.0000 Blocks:

6. 614E+04 876.0000 6. 701E+04 876.0000

6. 877E+04 1752.0000 7. 402E+04 5256.0000

8. 453E+04

1. 051E+04

8. 541E+04 876.0000

8. 629E+04 876.0000

8. 702E+04 730.0000 Blocks:

24. 0231

-1.9542 20.9366 -2.7420 19. 6883 -3. 5997

18. 3362

-4.2176 17.3638 -4.5266 16.8776

2. 3110 27.0185 0. 0220 28.2466

-1.9361

24. 6568

-3. 6800

21. 4 634

-4. 3825 20. 1706 -5.1476 18. 7702 -5. 6989 17. 7632 -5. 9745 17. 2597 0. 2023 27. 7422

8. 789E+04 876.0000

-8. 031E-04

27. 8324

8. 877E+04 876.0000

9. 052E+04 17 52. 0000 9.578E+04 5256.0000

l. 063E+05

l. 051E+04

1. 072E+05 876.0000

l. 080E+05 876.0000

l. 088E+05 730.0000 Blocks:

-1.9706 24.2975 -3. 7281 21.1570 -4.4367 19. 8873 -5.2082 18. 5113 -5.7640 17.5216 - 6.0419 17.0269 0. 1616 27.3819

1. 096E+05 876. 0000

-9. 560E-04 27.4504 l.lOSE+OS 876.0000 l.l23E+05 1752.0000 -1.9877 23. 9735 -3. iS98 20. 8835 -21.7783

4. 5509

-13. 7848

9. 3535

-10.4773 11.2940 - 6.8814 13.4039 -4.2924

14. 9235

-2.9979 15. 6833 -33.7303 -1.4152 -24. 5612

4. 3302

-16.2236

9. 5011

-12.8588

11. 5851

-9.2004 13.8509 -6.5663 15.4829 -5.2492 lq.2989 -35. 94"04 -1.9471 -26.3968

4. 1329

-17.8905

9. 5438

-14.4579 11.7245 -10. 7255

14. 0952

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11. 6009

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1. 558E-06 10.2656

1. OOOE-30 7. 5849 5.655E-07 5. 6830

1. OOOE-30 4.1984 9.210E-08

2. 3832

1. OOOE-30

l. 7606

l. 787E-08 0. 7333

l. OOOE-30 0.5417 5. 441E-24

8. 732E-06

2. 952E-04 36.1924

4. 623E-05 28.7754 2.170E-05 24.5610 l.OOOE-30 19.6929 8.305E-06 14.2694

l. OOOE-30 11.4355

l. 913E-06 10.1168

1. OOOE-30 8.1033 6.972E-07

5. 6007

1. OOOE-30

4. 4852 l.140E-07

2. 3487

l. OOOE-30

l. 8809 2.158E-08

0. 7227

1. OOOE-30 0.57B7 9.018E-24

l. 504E-06

3. 208E-04

35. 9624

4. 527E-05 30.1937 2.543E-05

24. 4 606 1. OOOE-30 20.5239 9.342E-06 14.2105

l. OOOE-30 11.9196 2. 173E-06 10.0754

l. OOOE-30 B.4461 7.943E-07 5. 5778

l. OOOE-30 4.6749 l.303E-07 2. 3391

l. OOOE-30 1. 9605 2. 420E-08

0. 7197

l. OOOE-30

0. 6032 l.29BE-23

7. 419E-09 3. 399E-04 36.4210

1. OOOE-30 29. 6324

2. 391E-05 24.7752 1. OOOE-30 20.1367 B. 82l.E-06

14. 393B

1. OOOE-30 11.6935

2. 046E-06 10.2051 1. OOOE-30 8. 2863

7. 471E-07

5. 6496

l. OOOE-30 4.5866 l.224E-07 2.3692 l.OOOE-30

l. 9234 2.2B7E-OB

0. 7290

l. OOOE-30

0. 591B l. lSBE-23

4. 543E-09

3. 303E-04 36.B3BB l.OOOE-30 29.1116 2. 255E-05

25. OSBO 1. OOOE-30 19.7845 B. 365E-06 14.5578

l. OOOE-30 11.4894

l. 935E-06 B-25 0. 4933

4. 206B

0. 4973 4.2095

0. 4 973

4. 2124 0. 4973

4. 2134 0. 4973 4. 2134 0.4973 4. 2134 0.5040 4.430B

0. 5459

4. 4479

0. 5502 4.4551

0. 5502 4.45BS 0. 5502

4. 4 621

0. 5502

4. 4633

0. 5502

4. 4 634

0. 5502

4. 4634

0. 5512 4. 7017

0. 591B

4. 721B 0. 591B

4. 7300

0. 591B 4. 733B

0. 591B 4. 73BO

0. 591B

4. 7394

0. 591B

4. 7394

0. 591B 4. 7394

0. 591B

4. 9921

0. 5959

5. 0131

0. 5959 5.0208

0. 5959 5.0244

0. 5959

5. 02B3

0. 5959 5.0296

0. 5959

5. 0297

0. 5959 5. 0297 0. 5959 5.2748

0. 5993

5. 2945 0. 5993

5. 3019

0. 5993

5. 3053 0. 3474

8. 5274

0. 3502

8. 4651

0. 3502

8. 4 710

0. 3502 B. 4730

0. 3502 B. 4730 0. 3550 B. 7905 0. 3B44 B. 147B 0. 3B75 B. 0973

0. 3B75 B. 1034 0.3B75 8.1101

0. 3B75 8.1122

0. 3B75 B.1123 0.3B75 B.1123

0. 3BB2 B. 5293

0. 4167

7. 9793

0. 4167

7. 9932 0.4167 7. 9996

0. 4167 B. 0067

0. 4167 B. 0090

0. 4167 B. 4361 0. 4197 B. 4125

0. 4197 B. 4255 0. 4197 B.4315 0. 4197 B. 43Bl 0. 4197 B. 4403 0.4197 B. 4403

0. 4197 B. 4403 0.4197 B.B516

0. 4220 B. B347

0. 4220 B. B469 0.4 220 B. B526 S)stnu:turatllllegrlly Associates. Inc.*

1.175E+OS 5256. 0000

1. 280E+OS

1. 051E+04

1. 289E+OS 876.0000

1. 298E+OS 876.0000

1. 305E+OS 730. 0000 Blocks:

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1. 314E+OS 876. 0000

-8. 016E-04

27. 1130

1. 323E+OS 876.0000 1.340E+OS 1752.0000

1. 393E+05 5256.0000

1. 498E+05

1. 051E+04

1. 507E+OS 876.0000

1. 515E+OS 876.0000

1. 523E+05 730.0000 Blocks:

-2. 0025

23. 6872

-3.7876 20.6420 -4.5075 19.4114 -5. 2909 18.0768 -5.8552

17. 1168

-6.1374

16. 6367 0.1254 26.7610

1. 532E+OS 876.0000

-1. 514E-04 26.8117

1. 540E+OS 876.0000

1. 558E+OS 1752.0000

1. 610E+OS 5256. 0000

1. 716E+05

1. 051E+04

1. 724E+OS 876.0000

1. 733E+OS 876.0000

1. 740E+OS 730.0000 Blocks :

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1. 749E+OS 876.0000

-2. 790E-04 26.5412 1. 758E+OS 876.0000

1. 775E+OS 1752.0000

1. 828E+05 5256.0000

1. 933E+OS

1. 051E+04 1. 942E+05 876.0000

1. 951E+OS 876.0000

1. 958E+OS 730. 0000 Blocks:

10 -2.0276 23.2024 -3.8349 20.2332 -4. 5639

19. 0337

-5. 3569 17.7323 -5.9281 16.7959 -6.2137

16. 3277 0.1014 26.2564

1. 967E+OS 876.0000

-8.111E-04 26.2964

1. 975E+05 876.0000

1. 993E+OS 17 52. 000 0

2. 045E+OS 5256.0000 2.lSlE+OS 1. 051E+04

-2. 0390 22.9948 -3. 8559 20.0583 -4. 5887 18.8721 -5. 3859 17.5849 -14.7954 11.4925 -10.9659 13.7737 -8.2085 15. 4166 -6. 82 98 16.2380 -37.2131 -1.5359 -27.3136 4.2159 -18.4922 9.3341 -14.9324 11. 3977 -11.0621

13. 6411

-8.2754 15.2566 -6.8820 16.0644 -37. 5493 -1.4218 -27.5547

4. 2416

-18.6491 9. 2817 -15. 0554 11.3140 -11.1483

13. 5232

-8. 3352 15.1142 -6. 9286 15. 9097 -37. 8552 -1.3177 -27.7742

4. 2660

-18.7920

9. 2355

-15. 1675 11.2394 -11.2270 13.4179 -8. 3898 14.9866 -6. 9711 15. 7710 -38.1351 -1.2220 -27.9750

4. 2891

-18.9229 9.1943 -15.2701 11.1725 -11.2990 13. 3229 Report No. 1600539.401RO

10. 3210

1. OOOE-30 8.1420 7. 063E-07

5. 7137

1. OOOE-30 4. 5068

1. 157E-07

2. 3961

1. OOOE-30

1. 8899 2.171E- 08

0. 7373

1. OOOE-30

0. 5815

1. 039E-23 3. 398E-09

3. 218E-04 37.2123

1. OOOE-30 28.6488 2. 139E-05 25.3111

1. OOOE-30 19.4713

7. 974E-06 14.7045

1. OOOE-30 11.3079

1. 840E-06 10.4248

1. OOOE-30

8. 0137

6. 713E-07

5. 7711

1. OOOE-30

4. 4358

1. 098E-07

2. 4202

1. OOOE-30

1. 8602

2. 072E-08

0. 7447

1. OOOE-30 0.5724 9.405E-24

2. 613E-09 3.142E-04 37. 5492

1. OOOE-30 28.2336

2. 038E-05

25. 5393

1. OOOE-30 19.1901

7. 635E-06 14.8369

1. OOOE-30 11.1449 1.758E-06

10. 5185

1. OOOE-30 7.8984 6.410E-07 5. 8230

1. OOOE-30 4.3720 1.048E-07 2.4419 l.OOOE-30

1. 8334

1. 986E-08

0. 7 514

1. OOOE-30

0. 5641

8. 573E-24

2. 070E-09

3. 07 SE-04

37. 8550

1. OOOE-30 27.8589

1. 950E-05 25.7466

1. OOOE-30 18.9363

7. 337E-06 14.9571

1. OOOE-30 10.9977 1.686E-06 10.6036 l.OOOE-30 7.7943 6. 144E-07

5. 8701

1. OOOE-30

4. 3144

1. 004E-07

2. 4616

1. OOOE-30

1. 8093

1. 910E-08

0. 7574 l.OOOE-30 0.5567 7.867E-24 1. 644E-09

3. 014E-04 38.1343

1. OOOE-30 27.5184

1. 872E-05

25. 9360

1. OOOE-30 18.7056

7. 074E-06 15. 0670

1. OOOE-30 10.8639

1. 623E-06

10. 6814

1. OOOE-30

7. 6996

5. 909E-07

5. 9131

1. OOOE-30

4. 2620

9. 650E-08 B-26

0. 5993 5.3090 0.5993

5. 3102 0.5993

5. 3102

0. 5993

5. 3102

0. 5993 5.5485

0. 6023

5. 5673

0. 6023

5. 5743 0. 6023 5.5775 0. 6023

5. 5811

0. 6023 5. 5822 0. 6023 5. 5822 0. 6023 5. 5822 0. 6023 5.8146 0. 6049

5. 8325 0. 6049

5. 8392 0.6049

5. 8423 0.6049

5. 8456

0. 604 9 5.8468

0. 6049 5.8468

0. 6049 6.0739

0. 6073

6. 0910

0. 6073

6. 0974 0. 6073

6. 1004

0. 6073

6. 1036

0. 6073 6. 104 7 0.6073 6.104 7

0. 6073

6. 104 7 0.6073

6. 3272

0. 6095

6. 3436

0. 6095

6. 3498

0. 6095 6. 3526 0. 6095 6. 3557

0. 6095

6. 3567

0. 4220 8.8588

0. 4220 8.8608 0.4220 8.8608

0. 4220 8. 8608

0. 4220

9. 2585 0. 4241 9.2438 0.4241 9.2554 0.4241

9. 2607 0.4241 9.2666 0.4241 9.2685 0.4241

9. 2685 0.4241 9. 2685 0.4241 9. 6544

0. 4260

9. 6415 0. 4260

9. 6526

0. 4260

9. 6577

0. 4260

9. 6632

0. 4260

9. 6651

0. 4260

9. 6651

0. 4260

9. 6651 0. 4260 10.0406

0. 4277

10. 0289

0. 4277

10. 0395

0. 4277

10. 0443

0. 4277 10.0497

0. 4277

10. 0514

0. 4277

10. 0514

0. 4277

10. 0514

0. 4277 10.4177

0. 4293 10.4071

0. 4293 10.4173 0.4293

10. 4220

0. 4293 10.4271

0. 4293 10.4287 IJStroctural lRieflrlly Associates. Inc!'

2.159E+05 2.168E+05 2.175E+05 Blocks: 876. 0000 876.0 000 730.0000 11 -5. 9601 16. 6587 -6.2472 16.1956

0. 0914 26.0375 2. 18 4E+05 876. 0000

-2. 097E- 03 26.0737 2.193E+05 876. 0000

2. 210E+05 17 52. 0000

2. 263E+05 5256. 0000

2. 368E+05

1. 051E+04

2. 377E+05 876. 0000

2. 386E+05 876. 0000 2. 393E+05 730.0000 Blocks:

12 -2. 0502 22. 8059 -3.8757 19. 8992 -4.6120 18.7252 -5.4130 17.4510 -5.9898 16.5340 -6.2783 16. 0756 0. 0821 25.8370

2. 402E+05 876. 0000

-2. 232E-03 25.8690 2. 410E+05 876.0000

2. 428E+05 1752. 0000 2. 4 81E+05 5256. 0000

2. 586E+05

1. 051E+04

2. 594E+05 876. 0000

2. 603E+05 876. 0000

2. 610E+05 730.0000 Blocks:

13 -2. 0595

22. 6324

-3. 8931 19. 7531 -4. 6327 18. 5902 -5.4372 17.3280 -6.0165 16.4196 -6.3062 15.9654

0. 0750 25.6514

2. 619E+05 876.0000

-2. 496E-03 25.6805

2. 628E+05 876.0000

2. 646E+05 1752.0000 2.698E+05 5256.0000

2. 803E+05

1. 051E+04 2. 812E+05 876.0000

2. 821E+05 876.0000

2. 828E+05 730.0000 Blocks:

14 -2.0683 22. 4726 -3. 9093

19. 6185

-4.6519 18.4660 -5.4596 17.2148 -6. 0413 16.3143 -6. 3321 15.8641 0. 0686 25.4797

2. 837E+05 876.0000

-1. 636E-03

25. 5056

2. 84 6E+05 876. 0000

2. 863E+05 1752.0000

2. 916E+05 5256. 0000 3. 021E+05

1. 051E+04 3. 030E+05 876.0000 3. 038E+05 876. 0000

-2. 0754 22. 3243 -3. 9234 19. 4938 -4. 6689 18. 3508 -5.4797 17. 1098 -6. 0636 16.2167 -6.3555 15. 7701 -8.4398 14.8714 -7.0101 15.6456 -38.3930 -1.1338 -28.1602

4. 3111

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4. 3320

-19.1543 9.1242 -15.4516 11.0570 -11.4264 13.1580 -8.5281 14.6709 -7.0790 15.4273 -38.8500 -0.9751 -28.'4881

4. 3519

-19.2570

9. 0939

-15.5320

11. 0066

-11.4827

13. 0856

-8. 5671

14. 5827

-7.1093

15. 3313

-39. 0535 -0. 9033 -28.6339

4. 3710

-19.3516

9. 0662

-15.6061

10. 9601

-11.5343

13. 0187

-8.6026

14. 5010

-7. 1367 15.2422 Report No. 1600539.401RO 2. 4797 l.OOOE-30

1. 7873

1. 843E-08

0. 7630

1. OOOE-30 0. 5499 7.260E-24

1. 312E-09

2. 960E-04 38. 3909

1. OOOE-30 27. 2075 1.804E-05 26. 1100

1. OOOE-30 18.4949 6. 840E-06 15.1680

1. OOOE-30 10.7417

1. 566E-06 10.7529

1. OOOE-30 7.6131

5. 700E-07

5. 9526

1. OOOE-30

4. 2142 9. 303E- 08 2. 4963 l.OOOE-30

1. 7672

1. 784E-08

0. 7681 1. OOOE-30 0.5438

6. 736E-24

1. 036E-09

2. 910E-04 38.6278

1. OOOE-30 26.9206

1. 742E-05 26.2708 l.OOOE-30 18.3004 6.629E-06 15.2613 1. OOOE-30 10.6289

1. 515E-06 10. 8189

1. OOOE-30

7. 5332

5. 512E-07

5. 9892

1. OOOE-30 4. 1700 8.991E-08

2. 5116 1. OOOE-30

1. 7487

1. 730E-08

0. 7728 1. OOOE-30 0.5381 6.276E-24

8. 506E-10 2. 865E-04 38.8475

1. OOOE-30 26.6556 1.686E-05 26.4198 l.OOOE-30 18.1207 6. 438E-06 15.3477 l.OOOE-30

10. 524 6

1. 4 69E-06 10.8801 l.OOOE-30 7. 4594

5. 342E-07

6. 0231

1. OOOE-30 4. 1291 8.709E-08

2. 5258

1. OOOE-30

1. 7316

1. 681E-08

0. 7772 1. OOOE-30 0.5328 5.871E-24

7. 018E-10 2. 823E-04 39. 0519

1. OOOE-30 26.4088 1.635E-05 26. 5585

1. OOOE-30 17.9533 6.264E-06 15. 4282

1. OOOE-30 10. 427 5 1. 427E-06 10. 9371

1. OOOE-30 7. 3907 5.187E-07 6. 0546

1. OOOE-30

4. 0911

8. 452E- 08

2. 5390

1. OO OE-30

1. 7156

1. 636E-08 0. 7812

1. OOOE-30 0. 5279

5. 512E-24 B-27 0. 6095

6. 3568

0. 6095

6. 3568 0.6095 6.5750

0. 6116

6. 5908 0. 6116 6. 5968

0. 6116

6. 5995

0. 6116 6. 6025

0. 6116

6. 6035 0. 6116

6. 8180 0. 6134 6. 8332 0. 6134

6. 8390

0. 6134 6.8417

o. 6134

6. 8446

0. 6134 6. 8455 0. 6134 6. 8455 0. 6134

6. 8455

0. 6134 7. 0565 0. 6151

7. 0713

0. 6151 7. 0769

0. 6151 7. 0795

0. 6151 7. 0823

0. 6151 7. 0832

0. 6151

7. 0832

0. 6151

7. 0832 0. 6151

7. 2910

0. 6166

7. 3053 0. 6166 7.3108 0.6166

7. 3133 0.6166 7.3160 0.6166 7.3169

0. 6166

7. 3169

0. 6166 7. 3169 0.4293

10. 4287 0. 4293 10.4287 0. 4293 10.7868 0. 4307 10. 7770 0.4307 10. 7868 0.4307 10. 7913 0. 4307 10. 7962 0. 4307 10.7978 0. 4307 10. 7978 0. 4307 10.7978

0. 4307 11.1484 0.4320 11.1400 0.4320 11.1495 0. 4320 11. 1538

0. 4320 11.1585

0. 4320 11.1601 0. 4320 11.1601

0. 4320 11.1601

0. 4320 11.5040

0. 4332 11.4964 0. 4332

11. 5055 0. 4332 11.5097

0. 4332 11. 5143

0. 4332 11.5158 0. 4332 11. 5158 0. 4332 11.5158 0. 4332

11. 8535 0. 4342 11. 8471 0. 4342 11.8560

0. 4342 11.8601 0. 4342 11.8645

0. 4342 11.8659

0. 4342 11.8660 0. 4342 11.8660

!S)s~mr:tumt llflegrlty Associates, Inc.*

3. 046E+05 Blocks: 730.0000 15

0. 0642 25.3194

3. 054E+05 S76. 0000

-1. 510E-03

25. 3434

3. 063E+05 676.0000 3.0BlE+05 1752.0000 3. 133E+05 5256. 0000

3. 23BE+05

1. 051E+04

3. 24 7E+05 676.0000

3. 256E+05 676.0000

3. 263E+05 730.0000 Blocks:

16 -2. 0626 22.1669 -3.9371 19.3762 -4. 6653 16.244 1 -5.4966 17.0126 -6.0647 16.1263 -6.3776

15. 6631

0. 0596 25.1703

3. 272E+05 676.0000

-1.270E-03 25.1923

3. 2BlE+05 676.0000

3. 29BE+05 1752.0000

3. 351E+05 5256. 0000

3. 456E+05

1. 051E+04

3. 465E+05 676.0000

3. 4 73E+05 676.0000

3. 4BlE+05 730.0000 Blocks:

17 - 2. 0693 22. 0569 -3.9496 19.2705 -4.7004 18.1446 -5. 51 66 16.9220 -6.1044 16.0421 -6.3963

15. 6021 0.0557

25. 0307

3. 4B9E+05 676.0000

-1. 936E-04

25. 0506

3. 49BE+05 676.0000

3. 516E+05 1752.0.000

3. 56BE+05 5256. 0000 3. 673E+05

1. 051E+04

3. 6B2E+05 676.0000

3. 691E+05 676.0000

3. 69BE+05 730.0000 Blocks:

16 - 2.0947 21. 9368 - 3. 9611 19.1695 -4.7140 1 8. 0514 -5. 5327 16.6372 -6. 1223

15. 9632

- 6.4171 15.5262

0. 0530 24.6993

3. 707E+05 876.0000

-6. 572E-04

24. 9165

3. 716E+05 876. 0000 3.733E+05 1752.0000 3.7B6E+05 5256. 0000

3. 891E+05

1. 051E+04

3. 900E+05 676.0000

3. 90BE+05 676.0000

3. 916E+05 730. 0000 Blocks:

19 - 2.1012

21. 6266

- 3.9726 19.0754 -4.7276 17.9645 - 5.5469 16.7561 -6. 1401 15.6897 - 6.4357

15. 4556 0. 0492 24.7765

-39.2442 -0.6362 -26.7706

4. 3691

-19.4405 9.0409 -15.6756 10.9172 -11.5629 12. 9566 - B. 6361

14. 4255

-7.1627 15.1596 -39. 4227 - 0.7730 -26.6966

4. 4064

-19.5236

9. 0175

-15.7406 10.6775 -11.6283

12. 6993

- B. 6673

14. 3552

-7.16 69 15.0631 -39.5694 - 0.7133 -29. 01 60

4. 4230

-19.6009 B. 9959 -15.6010 10.6405 -11.6703

12. 8455

- B. 6961 14.2693 - 7.2090

15. 0112

-3 9. 7479 -0.6572 -29.1317 4.4386 -19. 6749 6.9759 -15. 6569

10. 6061

-11.71 06

12. 7955

- 8.7241 14.2260 -7.2306 14.9443 Report No. 1600539.401RO

6. 061E-10

2. 7B5E-04 39.2427 1. OOOE-30 26.1796

1. 5BBE-05 26.6660

1. OOOE-30 17.7978 6.105E-06 15.5034

1. OOOE-30 10.3373

1. 3B9E-06 10. 9903 1. OOOE-30

7. 3268

5. 045E-07 6.0640

l. OOOE-30 4.0556 B.218E-OB

2. 5514 1. OOOE-30

1. 7006

1. 596E-OB

0. 7650

1. OOOE-30 0.5233 5.193E-24 5.160E-10

2. 749E-04 39. 4214

1. OOOE-30

25. 9653

1. 54 6E-05 26.6093 l.OOOE-30

17. 6524

5. 959E-06

15. 5738

1. OOOE-30 10.2529

1. 354E-06

11. 04 02

1. OOOE-30

7. 2671 4. 916E-07 6.111 6.

l.OOOE-30 4. 0227 B. 003E-OB

2. 5629 1. OOOE-30

1. 6669

1. 55BE-OB

0. 7686

1. OOOE-30

0. 5191

4. 907 E-24

4. 447E-10

2. 716E-04 39.5692

1. OOOE-30 25.7639

1. 506E-05 26.9232

1. OOOE-30 17.5157 5.B22E-06

15. 6399

1. OOOE-30 10.1736 1.322E- 06 11.0670

1. OOOE-30

7. 2:].09

4. 796E-07

6. 1 376

1. OOOE-30

3. 9916

7. B05E-OB 2. 5738

1. OOOE-30

1. 6739

1. 524 E-0B

0. 7919

1. OOOE-30 0.5150 4.649E-24

3. 999E-10

2. 685E-04 39. 7472 l.OOOE-30 25.5757

1. 470E-05

27. 0305 1. OOOE-30 17.3660 5. 695E-06 15.7022 l.OOOE-30 10. 0995

1. 292E-06 11.1311

1. OOOE-30 7. 1564

4. 6B6E-07

6. 1 620

1. OOOE-30

3. 9626

7. 622E-OB

2. 5640

1. OOOE-30

1. 6617

1. 4 92E-OB

0. 7951

1. OOOE-30 0.5113 4.417E-24 3. 401E-10

2. 656E-04 B-28

0. 6166

7. 5217 0.6161 7.5356 0.6161

7. 5410 0.616 1

7. 5434 0.616 1

7. 5461 0. 616 1

7. 5469 0. 618 1 7.5469 0. 616 1

7. 5469 0.6161 7. 7490

0. 6194 7. 7626

0. 6194 7. 7676

0. 6194 7.7702

0. 6194

7. 7727

0. 6194

7. 7736

0. 6194

7. 7736

0. 6194

7. 7736

0. 6194

7. 9732

o. 6207 7. 9664

0. 6207

7. 9915

0. 6207 7.9936

0. 6207

7. 9963

0. 6207

7. 9971 0. 6207

7. 9971

0. 6207

7. 9971

0. 6207 B. 1943

0. 621 9 8. 2072

0. 621 9 B.2122

0. 6219 B. 2145

0. 6219 6.2169

0. 6219 6.2176

0. 6219 B. 2176 0.6219 6.2178

0. 62 1 9 B. 4126

0. 4342 12.1961

0. 4353 12.1920

0. 4353 12.2007 0. 4353 12.2046

0. 4353 12.2069 0. 4353 12.2103 0. 4353 12.2103

0. 4353 12.2103

0. 4353 12. 5373

0. 4362

12. 5319

0. 4362 12.5403

0. 4362 12.5441

0. 4362 12.5463 0. 4362 12.5497

0. 4362 12.54 97

0. 4362 12.5497

0. 4362 12.8719 0. 4371 12.6674 0. 4371 12.6756 0. 4371 12.6793

0. 4371 12.8634 0. 4371 12.6647

0. 4371 12.6647

0. 4371 12.6647 0.4371 13.2025 0.4379

13. 1 976 0.4379 13.2056 0. 4379 13.2095 0.4379 13.2134 0.4379 13.2147 0.4379 13.2147

0. 4379 13.2147

0. 4379 13.5264 e

StnlctuiWI lllletJrlly Associates, Inc.*

3. 924E+05 876. 0000

-2.160E- 03 24.7948

3. 933E+05 876.0000

3. 951E+05 1752.0000

4. 003E+05 5256. 0000 4.10BE+05

1. 051E+04 4.117E+05 876.0000 4.126E+05 876.0000 4.133E+05 730. 0000 Blocks:

20 -2. 1082 21.7221 -3.9846 18.9873 -4.74 16 17.8832 -5.5648

16. 6841

-6.1575 15.8210 -6.4539 15.3894

0. 0447

24. 6611 4.142E+05 876. 0000

-1.222E-03

24. 6770 4.151E+05 876.0000 4. 16BE+05 17 52. 0000

4. 221E+05 5256. 0000

4. 326E+05 1. 051E+04

4. 335E+05 876.0000

4. 344E+05 876. 0000

4. 351E+05 730.0000 Blocks:

21 - 2. 1127 21.6223 - 3.9940

18. 9035

-4.7529 17.8059 -5.5782

16. 6137

-6.1724 15.7556 -6.4695 15.3265

0. 0429 24. 5510

4. 360E+05 876. 0000

- 5. 027E-04

24. 5659

4. 368E+05 876.0000

4. 386E+05 17 52. 0000

4. 43BE+05 5256.0000

4. 544E+05

1. 051E+04

4. 552E+05 876.0000

4. 561E+05 876.0000 4. 56BE+05 730. 0000 Blocks:

22 -2.1172 21.5282 -4.0029 18. 8244 -4.7 638 17.7329 -5.5910 16.5473 -6.1867 15.6939 -6.4845 15.2672

0. 0412 24.4468

4. 577E+05 876.0000

-2. 764E-03 24.4622

4. 586E+05 876.0000

4. 603E+05 1752.0000 4. 656E+05 5256. 0000

4. 761E+05

1. 051E+04

4. 770E+05 876.0000

4. 779E+05 876.0000

4. 786E+05 730.0000 Blocks:

23 -2. 1239 21.4404 -4. 0137 18.7506 -4.7762 17.6648 -5. 6051 16.4854 -6.2021

15. 6364

- 6. 5005 15.2 119

0. 0367 24.3493

4. 795E+05 876.0000

-1. 513E-03

24. 3621

4. 803E+05 876.0000

-2.1274 21.3557 -39. 8985 -0.60 43 -29.2399

4. 4539

-19.7455 8.9574 -15.9144 10.7741 -11.7498 12.7488 -8.7512 14.1707 -7.2519 14.8817 -40.0387 -0.5536 -29.3403

4. 4685

-19.81 05

8. 9399

-15.9651 10.7437 -11.7850 12.7044 -8.7753

14. 1162

-7.2704

14. 8221

-40.1716 -0. 5055 -29.4355

4. 4824

-19.8722

8. 9236

-16.0132 .10. 7152 -11.8185 12.6626 -8.7982

14. 0649

-7.2880 14.7660 - 40.3010 -0.4603 -29.5285

4. 4957

-19.9330 8. 9085 -16.0611 10.6887 -11.8522

12. 6237

-8. 8218 14.0170 -7.3066

14. 7136

-40.4204 -0.4165 -29.6140

4. 5087 Report No. 1600539.401RO

39. 8964

1. OOOE-30 25.3991

1. 437E-05 2 7. 1318

1. OOOE-30 17.2682 5.579E-06 15.7609

1. OOOE-30 10.0299

1. 264E-06 11.1728

1. OOOE-30

7. 1092

4. 584E-07

6. 1850

1. OOOE-30 3.9353 7.454E-08

2. 5937

1. OOOE-30

1. 6503

1. 463E-OB

0. 7981

1. OOOE-30 0. 5078

4. 20BE-24

2. 759E-10 2. 629E-04

40. 037 5

1. OOOE-30 25.2307

1. 406E-05 27.2275

1. OOOE-30 17.1539

5. 469E-06

15. 8165

1. OOOE-30

9. 9636

1. 23BE-06 11. 2121

1. OOOE-30

7. 0622

4. 488E-07

6. 2068

1. OOOE-30

3. 9093

7. 296E-08

2. 6029

1. OOOE-30

1. 6394

1. 435E-08

0. 8009

1. OOOE-30

0. 5044

4. 015E-24

2. 525E-10

2. 603E-04 40.1711

1. OOOE-30

25. 0714

1. 377E-05 27. 3183

1. OOOE-30 17.0458 5.367E-06

15. 8692

1. OOOE-30

9. 9009

1. 214E-06 11.2495 l.OOOE-30

7. 0178

4. 399E-07

6. 2275

1. OOOE-30 3.8847 7.149E-OB

2. 6115

1. OOOE-30

1. 6291

1. 409E-OB

0. 8035

1. OOOE-30

0. 5013

3. 839E-24

2. 306E-10

2. 579E-04 40.2982 l.OOOE-30 24.9224

1. 350E-05 27.4046

1. OOOE-30 16.9446 5.272E-06

15. 9193

1. OOOE-30

9. 8421 1.192E-06 11.2850

1. OOOE-30 6.9762 4. 317E-07

6. 24 71

1. OOOE-30 3.8617 7.013E-08

2. 6197

1. OOOE-30

1. 6194 1. 385E-OB

0. 8061

1. OOOE-30 0.4983 3.6BOE-24

1. 791E-10

2. 557E-04 40.4189 l.OOOE-30 24.7786

1. 325E-05 27.4866

1. OOOE-30 16.8470 5.182E-06 B-29 0. 6230

8. 4254

0. 6230

8. 4303

0. 6230

8. 4325

0. 6230 8.4349

0. 6230 8.4357

0. 6230 8. 6287

0. 6240

8. 6410

0. 6240

8. 6458

0. 6240

8. 6480

0. 6240

8. 6503

0. 6240

8. 6511

0. 6240

8. 6511 0. 6240

8. 6511

0. 6240

8. 8422

0. 6250

8. 8542

0. 6250 8.8589

0. 6250 B. 8611

0. 6250

8. 8634

0. 6250

8. 8641

0. 6250

8. 8641

0. 6250

8. 8641

0. 6250

9. 0534

0. 6260 9. 0652

0. 6260 9. 0698

0. 6260

9. 0719

0. 6260

9. 0742 0. 6260

9. 0749

0. 6260

9. 0749

0. 6260

9. 0749

0. 6260 9.2625

0. 6269 9.2741

0. 6269 9.2786

0. 4387 13. 5237

0. 4387 13.5315

0. 4387

13. 5351

0. 4387 13.5389

0. 4387 13.5402

0. 4387 13. 5402

0. 4387 13.5402

0. 4387 13. 8500

0. 4395 13.8468

0. 4395 13.8545

0. 4395 13.8580 0.4395 13.8618 0.4395 13.863 0

0. 4395 13.8630

0. 4395 14.1692 0.4402 14.1663 0.4402 14.1739 0.4402 14.1773

0. 4402 14. 1810 0.4402 14. 1822

0. 4402 14.1822

0. 4402 14. 1822

0. 4402 14.4850

0. 4408 14.4810

0. 4408 14.4884

0. 4408 14.4917

0. 4408 14.4954 0.4408 14.4965

0. 4408 14.4966 0.4408 14.4966

0. 44 08 14.7962

0. 4415 14.7943 0.4415

14. 8015 l}Stntcturatlnferrlty Associates. Inc.*

4 o 821E+05 1752 o 0000 4 o 873E+05 5256 o 0000 4 o 979E+05 1o 051E+04 4 o 987E+05 8760 0000 4 o 996E+05 8760 0000 5o 003E+05 730o 0000 Blocks: 24 -4 0 0213 18o6795 -4 0 7855 17 o5992 -50 6163 16o 4257 -6o 2145 15 0 5810 -6o 5136 15o1586 0 0 0359 24 0 2551 5o 012E+05 876o 0000 -20 733E-03 24 0 2683 5o 021E+05 876 0 0000 5o 038E+05 1752 o 0000 5o 091E+05 5256 o 0000 5 o196E+05 10 051E+04 5o 205E+05 876 o 0000 5o 214E+05 876o 0000 5o 221E+05 730 0 0000 Blocks: 25 -2 o1328 21.2762 -4 0 0304 18 0 6128 - 4o7961 17o5376 -50 6285 1 60 3697 - 6o2279 15o5290 -6o 5276 15 01086 0 0 0328 24o1665 5o 230E+05 876o0000 -3o 067E- 03 24o1785 5o 238E+05 876o 0000 5o 256E+05 1752 o 0000 5o 309E+05 5256 o 0000 5o 414E+05

1. 051E+04 5o 422E+05 876o 0000 5o 431E+05 876o 0000 5o 439E+05 730 0 0000 Blocks:

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21. 1274

- 4 0 0453 18o4879 -4 0 8139 1704224 -5o6494 16o2649 - 6 0 2510 15o4317 -6 0 5519 15 0 0151 0 0 0273 23 0 9796 5o 665E+05 876o0000 -2o875E-03 23 0 9893 5o 674E+05 876o 0000 5o691E+05 175200000 5o 744E+05 5256o 0000 -2 o1455 21.0321 -4 0 0536 18o4038 -4 0 8236 17o3414 -19o9883 8 0 8940 -16o1041 10 0 6632 -11.8820 12o5862 -8 0 8421 13o 9708 -7 0 3221 14 0 6632 -40o 5368 -Oo3751 -29 0 6976 4o5210 -2 0o0428 8 0 8806 -16o1469 10o6394 -110 9120 12 0 5511 - 8 0 8629 13 0 9276 -7o3383 14 0 6159 -40o6470 - 0 0 3354 -29 0 7766 4 0 5330 -2 0 0 0941 8 0 8678 -16o1871 10o6167 -11.9401 12o5176 - 8o8822 13o8863 -7 0 3533 14o5707 -40o7511 - 002971 -29 0 8511 4o5445 -20 o1423 8 0 8557 - 16o2247 10 0 5950 -11 o9662 12 o4855 -8 0 9000 13o8468 -7 0 3669 14o5274 -40o8469 -002622 -29 0 9195 4 0 5480 - 20o1870 8 0 8304 -16o2600 10 0 5565 Report No. 1600539.401RO 15 o 9669

1. OOOE-30 9o 7855 1.171E-06 11.3187

1. OOOE-30 6 o 9360 4 o 239E-07 6 o 2658

1. OOOE-30 3 o 8395 6 o 883E- 08 2 o 6276

1. OOOE-30

1. 6101

1. 363E-08 0 o 8085

1. OOOE-30 Oo4954 3o531E-24

1. 706E-10 2 o 536E-04 40 o 5341

1. OOOE-30 24 o 6434 10 301E-05 27 o 5648

1. OOOE-30 16o7552 5o098E-06 l 6o 0123

1. OOOE-30 9 o 7322 1.151E-06 110 3508

1. OOOE-30 6o8983 4o166E-07 6 o 2836

1. OOOE-30 3o8186 6o 763E-08 2 o 6350

1. OOOE-30

1. 6014

1. 341E-08 0 o 8108 10 OOOE-30 0 o 4927 3 o 395E-24

1. 400E-10 2 o 515E-04 40o6439 l.OOOE-30 24 o 5139 10 278E- 05 27 o 6394 10 OOOE-30 16o6673 5o019E-06 16 o 0556 10 OOOE-30 9 o 6811 1.132E-06 110 3815 10 OOOE-30 6o8621 4o097E-07 6 o 3005 1o OOOE-30 3o7986 6o649E-08 2 o 6422

1. OOOE-30

1. 5930

1. 321E-08 0 o 8130

1. OOOE-30 Oo4901 3o269E-24

1. 215E-10 2 o 496E-04 40o 7488 l.OOOE-30 24 o 3897 1o 257E-05 27 o 7106 10 OOOE-30 16o5829 4o943E- 06 16o 0970

1. OOOE-30 9o 6322 1.115E-06 11o 4108

1. OOOE-30 6o8274 4o031E-07 6 o 3168

1. OOOE-30 3o 7794 6o541E-08 2 o 6490

1. OOOE-30

1. 5849

1. 302E-08 0 o 8151 1o OOOE-30 Oo4877 3o152E-24 9 o 365E-11 20 473E-04 40o 8440

1. OOOE-30 24 o 2515 1o 234E-05 27 o 7740 10 OOOE-30 16o4840 4o854E-06 16 o1334

1. OOOE-30 9 o 5735

1. 093E-06 11o 4364

1. OOOE-30 6o 7849 3o951E- 07 B-30 0 0 6269 9o2807 0 0 6269 9o2829 0 0 6269 9 0 2836 0 0 6269 9 0 2837 0 0 6269 9 0 2837 Oo 6269 9o4696 0 0 6277 9 0 4810 0 0 6277 9o 4855 0 0 6277 9o 4875 0 0 6277 9 0 4897 0 0 6277 9 0 4904 0 0 6277 9o 4904 0 0 6277 9 0 4904 0 0 6277 9 0 6748 0 0 6286 9 0 6860 0 0 6286 9 0 6904 0 0 6286 9 0 6924 0 0 6286 9 0 6945 Oo 6286 9o 6952 0 0 6286 9 0 6953 0 0 6286 9o 6953 0 0 6286 9 0 8782 0 0 6293 9o8892 Oo 6293 9 0 8936 0 0 6293 9 0 8955 Oo 6293 9 0 8977 Oo 6293 9 0 8983 Oo 6293 9 0 8983 0 0 6293 9 0 8983 Oo 6293 10o0799 0 0 6300 10o0908 Oo 6300 10 0 0950 0 0 6300 10o0969 0 0 6300 10 0 0990 0 0 4415 14o8048 Oo4415 14o8083 Oo4415 14 0 8095 0 0 4415 14 0 8095 Oo 4415 14 0 8095 Oo 4415 15 o1061 Oo4421 15 0 1033 Oo4421 15 0 1104 Oo4421 15 0 1136 Oo4421 1501171 Oo 4421 15 0 1182 Oo4421 15 o1183 Oo4421 15 o1183 Oo4421 15 0 4120 Oo4426 15o4099 Oo4426 15o4169 Oo4426 15 0 4201 Oo4426 15 0 4235 Oo4426 15o 4246 Oo4426 15 0 424 6 Oo4426 15o4246 0 0 4426 15o 7157 Oo4432 150 7145 Oo4432 15o 7214 0 0 4432 150 7245 Oo4432 15o7278 0 0 4432 15 o7289 Oo 4432 150 7289 Oo4432 15 0 7289 0 0 4432 16o0175 Oo4437 16o0172 Oo4437 16 0 0239 0 0 4437 16 0 0270 Oo4437 16o 0303 l)s~ruc~um lllleflrlty Associates. Jnr:.*

5. 84 9E+05 1. 051E+04

5. 858E+05

5. 866E+05

5. 874E+05 Blocks:

5. 882E+05

5. 891E+05 876.0000 876.0000 730.0000 28 876. 0000 876.0000 5. 909E+05 1752.0000

5. 961E+05 5256. 0000

6. 066E+05

l. 051E+04

6. 07 5E+05

6. 084E+05

6. 091E+05 Blocks:

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6. 293E+05

6. 301E+05

6. 309E+05 Blocks:

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6. 326E+05 876.0000 876.0000 730.0000 30 876. 0000 876. 0000

6. 344E+05 17 52. 0000

6. 396E+05 5256. 0000

6. 501E+05

1. 051E+04

6. 51 0E+05

6. 519E+05

6. 526E+05 Blocks:

6. 535E+05

6. 544E+05 876.0000 876.0000 730. 0000 31 876.0000 876. 0000

6. 561E+05 1752. 0000

6. 614E+05 5256. 0000

6. 719E+05

1. 051E+04

6. 728E+05 876.0000

-5. 6605 16.1896 - 6. 2630

15. 3611

-6.5642 14.9468 -0. 0168 23. 5559 -0. 0176

23. 5321

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4. 4 615

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10. 3560

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12. 8495 Report No. 1600539.401RO

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l. OOOE-30

3. 7557 6.408E- 08 2.6549

l. OOOE-30

l. 5749

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0. 8169

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1. OOOE-30

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3. 5005

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16. 611 3 0.4437 1 6.6265

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17. 1751 0.4437 17.1887 0.4437 17. 1940 0.4437 17.1964

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0. 4437 17.1999 e

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8. 495 8

-12.1225 10.0071 -9. 0434

11. 0954

-7.5038

11. 6395

-41.0391 -0.2089 -30. 0905

3. 6245

-20.3392

7. 0380 Report No. 1600539.401RO 27.7941

1. OOOE-30 13.6757

2. 621 E- 06

16. 1451 1. OOOE-30

7. 9433

5. 906E-07

11. 4446

1. OOOE-30

5. 6302 2.135E- 07

6. 3354

1. OOOE-30 3.1166

3. 463E-08 2. 6568

1. OOOE-30

1. 3070 6. 905E-09

0. 8175

1. OOOE-30 0. 402 1

2. 507E-24

0. 0000

1. 610E-04 40.8752

1. OOOE-30 19. 9037

6. 427E-06 27.7951

1. OOOE-30

13. 5321

2. 532E-06 16.1457 l.OOOE-30

7. 8599

5. 704E- 07 11.4451

1. OOOE-30 5.5711 2.062E-07

6. 3357

1. OOOE-30 3.0839 3.344E- 08

2. 6569 1. OOOE-30

1. 2933

6. 669E-09

0. 8175

1. OOOE-30 0.3979 2.479E-24 0. 0000

1. 575E- 04 40.8 7 66

1. OOOE-30 1 9.7014 6.214E-06 27. 7961

1. OOOE-30 1 3.3946 2. 448E-06 16.1463 l.OOOE-30

7. 7801

5. 515E-07 11.4455

1. OO OE-30

5. 5145 1. 994E-07

6. 3359

1. OOOE-30

3. 0526

3. 234E- 08 2.6570 l.OOOE-30

1. 2801

6. 448 E-09

0. 8175

1. OOOE-30

0. 3939

2. 453E-24

0. 0000

1. 54 1E-04 40. 8780 l.OOOE-30 19.5076 6.014E-06

27. 7971 1. OOOE-30 13.2630

2. 369E- 06 1 6.1468

l. OOOE-30

7. 7037

5. 338E-07

11. 4459

1. OOOE-30

5. 4604

1. 930E-07

6. 3361

1. OOOE-30

3. 0226 3.130E-08

2. 6571

1. OOOE-30 1.2676 6.24 1E-09 0.8176 l.OOOE-30

0. 3900

2. 428E-24

0. 0000

1. 509E-04 40.8794

1. OOOE-30 1 9.3217

5. 827E- 06 27. 7980

1. OOOE-30 13.1367

2. 296E-06 16.1474 l.OOOE-30

7. 6303 5. 172E-07 B-34

0. 6300 12.1680

0. 6300 12.1690

0. 6300

12. 1702 0. 6300 12. 1705

0. 6300 12.1705

0. 6300 12.2893

0. 6300 12.2950

0. 6300 12.2972

0. 6300 12.2982 0. 6300 12.2993 0. 6300 12.2996 0. 6300

12. 2996

0. 6300 12.2996

0. 6300

12. 4158

0. 6300

12. 4212

0. 6300

12. 4234

0. 6300

12. 4243

0. 6300

12. 4254

0. 6300 12.4257

0. 6300 12.5394

0. 6300 12.5446

0. 6300 12.5467 0. 6300 12.5476

0. 6300 12.5487

0. 6300 12.5490

0. 6300

12. 6602

0. 6300 12.6653

0. 6300 12.6673

0. 6300

12. 6683 0.4437 19.3144 0. 4437 19. 3160 0.4437 1 9.3178 0.4437 19. 3184 0.4437

19. 3184 0.4437

19. 3184 0. 4437 19.5070 0.4437

19. 5159 0.4437 19.51 95

0. 4437 1 9. 5211 0.4437 1 9. 5228 0.4437

19. 5233 0.4437 19. 5233 0.4437 19.5233 0.4437 19.7077

0. 4437 1 9.7163 0.4437 19.7197

0. 4437 19.7213

0. 4437

19. 7229 0.4437

19. 7235 0. 4437 19. 7235 0. 4437

19. 7235 0. 4437

19. 9039

0. 4437 1 9.9122 0.4437

19. 9155 0.4437 1 9. 9170 0.4437 19.9186

0. 4437

19. 9191 0. 4437

19. 9191 0.4437

19. 9191 0.4437 20. 0957

0. 4437 20.1038

0. 4437 20.1070 0.4437 20.1085 l)stntctuiVI llllegrtty Associates. Inc:'

9.442E+05 5256.0000 9. 54 7E+05

1. 051E+04

9. 556E+05 876.0000

9. 564E+05 876. 0000

9. 572E+05 730.0000 Blocks:

45 9.5 81E+05 876. 0000 9.589E+05 876. 0000

9. 607E+05 17 52. 0000

9. 659E+05 5256. 0000

9. 764E+05

1. 051E+04

9. 773E+05 876.0000

9. 782E+05 876.0000

9. 789E+05 Blocks:

9. 798E+05

9. 807E+05 730.0000 46 876. 0000 876.0000

9. 824E+05 17 52. 0000

9. 877E+05 5256. 0000 9. 982E+05

1. 051E+04 9. 991E+05 876. 0000 1. OOOE+06

1. 001E+06 Blocks:

1. 002E+06

1. 002E+06 876.0000 730. 0000 47 876.0000 876.0000

1. 004E+06 1752.0000

1. 009E+06 5256. 0000

1. 020E+06

1. 051E+04

1. 021E+06 87 6. 0000 1. 022E+06 1. 022E+06 Blocks:

l. 023E+06 876.0000 730. 0000 48 876. 0000 1.024E+06 876. 0000

1. 026E+06 1752.0000 1. 031E+06 5256. 0000

1. 042E+06

1. 051E+04

-4.9583 13. 8233 -5.7913 12. 9057 -6.3911 12.2453 -6. 6910

11. 9150

-0.1652 18.9437 -0.1655 18.9361 -2.2978 16.6063 -4. 1969 14.5329 -4. 9632 13.6957 -5.7961 12.7866 -6.3958 12.1322 -6. 6956 11.8051 - 0.1707

18. 7734

-0. 1709 18.7662 - 2. 3029 16. 4574 -4. 2017 14. 4026 -4.9679 13. 5730 - 5. 8006 12. 6720 -6. 4002 12. 0235 -6. 7000 11. 6993 - 0.1760 18. 6095 - 0. 1762

18. 6027

-2. 3079 16. 3141 -4.2063 14.2772 -4. 9724 13. 4548 -5. 8050 12.5617 - 6. 4045 11.9189 -6. 7043 11.5975 -0.1811 18. 4516 -0. 1813 18. 4450 -2. 3126 16. 1759 -4.2108 14.1563 -4. 9767 13.3409 -5.8093

12. 4554

-16.4045 8.4149 -12.1276

9. 9118

-9. 0483 10.9898 -7. 5086 11. 5287 -41.0461 -0.2070 -30. 0967

3. 5910

-20. 3447 6.9731 -16.4098 8. 3372 -12.1326

9. 8203

-9.0530 10.8883 -7.5132

11. 4223

- 41.0528 - 0. 2051 -30.1026 3. 5588 -20. 3500

6. 9106

-16.4148

8. 2625

-12. 1373

9. 7324

-9.0576 10. 7908 -7.5177 11.3200 -41.0593 -0. 2033 -30.1084 3.5278 -20.3551 6. 8504 -16.4197 8.1906 -12.1419

9. 64 76

-9.0619 10. 6968 -7. 5220 11.2215 -41. 0655 -0. 2016 -30.1139 3. 4979 -20. 3601 6. 7924 -16.4243 8. 1213 -12.1463

9. 5660 Report No. 1600539.401RO 11. 44 62

1. OOOE-30 5. 4084 1.870E-07 6. 3 3 63

1. OOOE-30

2. 9939

3. 033E- 08 2. 6572

1. OOOE-30

1. 2555 6. 047E-09 0.8176 l.OOOE-30

0. 3863

2. 404E-24

0. 0000

1. 479E-04 40.8806

1. OOOE-30 19.1431 5. 651E-06 27.7989 l.OOOE-30 13.0153 2. 226E-06 16. 14 79

1. OOOE-30 7. 5598 5. 016E-07 11.4466 l.OOOE-30

5. 3585

1. 814E-07 6.3365 l.OOOE-30 2. 9662 2. 941E-08

2. 6572

1. OOOE-30

1. 2439

5. 865E-09 0.8176 l.OOOE-30

0. 3827

2. 380E-24

0. 0000

1. 450E-04 40.8819

1. OOOE-30 18. 9714

5. 486E-06 27.7997

1. OOOE-30 12.8986 2.161E-06 16.1484

1. OOOE-30

7. 4921

4. 869E-07 11.4469

1. OOOE-30

5. 3105 1. 761E-07

6. 3367

1. OOOE-30 2. 9397

2. 855E-08

2. 6573

1. OOOE-30

1. 2328

5. 694E-09 0.8176 l.OOOE-30

0. 3793

2. 358E-24 0.0000

1. 423E-04 40. 8831 1. OOOE-30 18. 8060

5. 330E-06 27. 8005

1. OOOE-30 12. 7863 2.lOOE-06 16. 1488

1. OOOE-30 7. 4268 4. 731E-07 11.4473

1. OOOE-30 5. 2642

1. 710E-07 6. 3369

1. OOOE-30 2. 9141

2. 774E-08

2. 6574

1. OOOE-30 1. 2220 5. 532E-09 0. 8177 l.OOOE-30 0. 3760

2. 336E-24

0. 0000

1. 396E-04 40.8842

1. OOOE-30 18.6466 5.182E-06 27.8013

1. OOOE-30 12.6780 2. 042E-06 16. 1493

1. OOOE-30 7.3640 4.600E-07 11.4476 l.OOOE-30

5. 2197

1. 663E-07

6. 3371

1. OOOE-30 2. 8894 2.697E-08 B-35 0. 6300 12. 6692 0. 6300 12. 6696

0. 6300

12. 6696

0. 6300

12. 6696

0. 6300 12.7785

0. 6300 12.7835

0. 6300 12. 7854

0. 6300 12.7863

0. 6300 12.7873

0. 6300 12.7876

0. 6300 12.7876 0. 6300 12.7876 0. 6300

12. 8944

0. 6300

12. 8992 0. 6300 12. 9011 0. 6300 12.9020 0. 6300 12. 9029

0. 6300 12. 9032 0. 6300

12. 9032 0. 6300

12. 9032 0. 6300 13.0080 0. 6300 13. 0126

0. 6300 13. 0145 0. 6300

13. 0153

0. 6300

13. 0162

0. 6300

13. 0165

0. 6300

13. 0165 0. 6300

13. 0165

0. 6300 13.1193 0. 6300 13. 1239

0. 6300 13. 1257 0. 6300 13.1265 0.6300 13.1273

0. 6300 13.1276 0. 4437 20.1100 0.4437 20.1105

0. 4437 20.1105 0. 4437 20.1105 0.4437 20.2835 0.4437 20.2914 0.4437 20.2945 0. 4437 20.2959

0. 4437 20.2974

0. 4437 20. 2979 0.4437 20,2979 0.4437 20. 2979

0. 4437 20.4 674 0.4437 20.4751 0.4437 20.4781

0. 4437 20.4794 0. 4437 20. 4809 0. 4437 20.4814 0.4437 20.4814

0. 4437 20. 4814 0. 4437 20. 6477 0.4437 20. 6551

0. 4437 20.6580

0. 4437 20. 6593 0. 4437 20. 6608 0.4437 20.6612 0. 4437 20.6612 0. 4437 20. 6612 0. 4437 20. 8244 0. 4437 20.8316

0. 4437 20. 8345 0. 4437 20.8358 0.4 4 37

20. 8372 0. 4437 20. 8376

!l} Slntctunrl hltetJrlly Assoclales, Inc.*

1. 043E+06

1. 044E+06 Blocks:

1. 045E+06

1. 046E+06 876.0000 876.0000 730.0000 49 876.0000 876.0000

1. 048E+06 1752. 0000

1. 053E+06 5256. 0000

1. 063E+06 1. 051E+04

1. 064E+06

1. 065E+06

1. 066E+06 Bl ocks:

1. 067E+06

1. 068E+06 876.0000 876.0000 730.0000 50 876.0000 876.0000

1. 069E+06 1 752.0000

1. 075E+06 5256.0000 1. 085E+06 1. 051E+04

1. 086E+06

1. 087E+06

1. 088E+06 Bl ocks:

1. 089E+06 1. 089E+06 876.0000 876.0000 730.0000 51 876.0000 876.0000

1. 091E+06 1752.0000

1. 096E+06 5256. 0000 1.107E+06

1. 051E+04 1. 1 08 E+06 1. 1 09E+06 1.109E+06 Bl ocks:

1.110E+06 1.111E+06 87 6.0000 876.0000 730.0000 52 876.0000 87 6.0000 1.113E+06 1752.0000

1. 11 8E+06 5256.0000 1.129E+06

1. 051E+04 1.130E+06 876.0000 1.130E+06 876.0000

-6.4087 11.8 1 80 -6.7084 11.4993 -0.1860 18. 2992 - 0. 1 862 18.2929 -2. 3172 16.042 6 -4. 2151

14. 03 97

-4. 9810 1 3. 2310 -5. 81 34 12. 3528 -6.4 127 11.7206 -6. 7124 11. 4046 -0.1907 18.1520 - 0. 1 90 9 18.1460 -2.321 6

15. 9138

-4.21 93

13. 9270

-4. 9850

13. 1249

-5.81 7 3 12.2537 -6.4 1 66 11.6266 -6. 71 62 11.31 31 - 0.1953 18.0098 -0. 1 955 1 8.0040 - 2.3259 15.7893 -4.2233 13.8 1 81 -4.9889 1 3. 0223 -5.82 11

12. 1579

- 6.4203 11.5358 -6. 71 9 9

11. 22 4 7

-0.1997 17.8722 - 0.1999 17.8666 -2.3301

15. 6689

-4.22 72

13. 7128

-4. 9927

12. 9230

-5.8248

12. 0652

-6.4239 11.4478 -6.7235 11. 1391 -9. 0662

10. 6063

-7.5261 11.1265 -41.0715 -0.2000 - 30.1192 3.4691 - 20.3648

6. 7364

-1 6. 4289

8. 0544

-12.1506 9.4872 - 9. 0702 10.5189 -7.5301 11.0348 - 41.0773 - 0. 1984 - 30.1244 3. 4412 -20.3694

6. 6823

-16.4332 7. 9897 - 12.1547 9. 4111 -9.0742 10.4346* - 7.5339 10.9463 - 41. 0829 -0.1968 -30. 1294

3. 41 43

-20.3738

6. 6301

-16.4374

7. 9273

- 12.1587 9. 3375 -9.0780 10. 3530 - 7.5376 10.8607 -41.0883 - 0.1953 - 30.1342 3.3883 -20.378 1 6.5795 -16.4415 7. 8669 -12. 1 625 9. 2664 - 9.0817 10.2741 - 7.5412 10.7780 Report No. 1600539.401RO

2. 6575

1. OOOE-30

1. 2117

5. 37 9E- 09

0. 8177 1. OOOE-30 0. 3728 2.316E-24

0. 0000

1. 371E-04 40. 8853

1. OOOE-30 18.4928 5.042E- 06 27.8020

1. OOOE-30 12.5735

1. 987 E-06 1 6.14 97

1. OOOE-30 7. 3033

4. 47 6E- 07 11.4479 l.OOOE-30 5.1767 1. 618E-07

6. 3372 1. OOOE-30

2. 8656

2. 625E- 08

2. 6575

1. OOOE-30

1. 2017

5. 234 E- 09

0. 8177

1. OOOE-30

0. 3698

2. 296E-24

0. 0000

1. 348E- 04 40. 8864

1. OOOE-30 18.3443 4. 910E-06

27. 8027 1. OOOE-30

12. 4 726

1. 935E- 06 1 6.1501

1. OOOE-30

7. 2447 4. 359E- 07

11. 44 82 1. OOOE-30 5.1351

1. 576E- 07 6.337 4 l.OOOE-30 2.8426 2.5 5 6E- 08

2. 6576

1. OOOE-30 1.1921

5. 097 E- 09

0. 8177

1. OOOE-30

0. 3668

2. 276E-24

0. 0000 1. 325E- 04 40.8874 l.OOOE-30 18.2008

4. 7 84 E- 06 27.8034 1. OOOE-3 0 12.3750

1. 885E- 06 16.1505 1. OOOE-30 7.1880 4.247 E-07

11. 4485

1. OOOE-30

5. 0950

1. 536E- 07

6. 3376

1. OOOE-30

2. 8204

2. 491E- 08

2. 6577

1. OOOE-30 1.1827

4. 966E-09 0. 8177

1. OOOE-30

0. 3639

2. 2 58 E-24 0.0000 1. 303E- 04 40.8884

l. OOOE-30 1 8. 0619 4. 665E- 06 27. 804 1

1. OOOE-30 12.2806 1. 838E-06

16. 1509

1. OOOE-30

7. 1332 4. 14 1E-07

11. 4488

1. OOOE-30

5. 0562

1. 497E- 07

6. 3377

1. OOOE-30

2. 7989

2. 429E- 08

2. 6577

1. OOOE-30 1.1737

4. 842E- 09

0. 8178

1. OOOE-30 0.3611 2.240E-24 B-36 0. 6300

13. 1 2 7 6

0. 6300 13. 1276

0. 6300 13. 2286

0. 6300

13. 2330

0. 6300 13.2347

0. 6300

13. 2355

0. 6300 13.2364

0. 6300 13.2366

0. 6300 1 3.2366

0. 6300 13.2366 0. 6300 13.3358

0. 6300 13.3401 0. 6300 13.3418 0. 6300 13.3426

0. 6300 13.3434

0. 6300 1 3. 3 4 37

0. 6300

13. 3437

0. 6300 13.3437 0. 6300

13. 4 411 0. 6300 13.4453

0. 6300 13.4470

0. 6300 13. 4477

0. 6300 13.4485

0. 6300 13.4488

0. 6300 13.5446

0. 6300 13.5487

0. 6300

13. 5503 0. 6300 13.551 1

0. 6300

13. 5518

0. 6300 1 3.552 1

0. 6300 13.552 1 0. 6300

13. 5521 0.4437 20. 8376 0.4437 20.8376

0. 4437 20.9979 0.4437 21.0049 0.4437

21. 0076 0.4437

21. 0089 0.4437

21. 0102 0.4437

21. 0107

0. 4437 21. 01 07 0.4437 21. 01 07

0. 4437 21.168 1 0.4437

21. 1749 0. 4437 2 1. 1776 0.4437

21. 17 88 0.4437 21.1801

0. 4 43 7

21. 1 806 0.4437 21.1806 0.4437

21. 1806 0.4437 21.335 3 0.4437

21. 3419 0.4437

21. 344 5 0.4437 21.34 57

0. 4437 21.3470 0.4437 21.3474 0. 4437 21.347 4 0.4 437

21. 347 4

0. 4437 21.4995 0.4437 21.5060 0.4437 21.5086 0. 4437

21. 5097 0.4437 21.5110 0.4437 21.5114

0. 4437

21. 5114 0.4437 2 1.5114 e

Stlllatul'lfl Jntegrlly Associates, Ina.*

1. 131E+06 Blocks:

1. 132E+06

1. 133E+ 06 730. 0000 53 876.0000 876.0000 1.135E+06 1752.0000

1. 14 OE+06 5256. 0000 1.150E+06

1. 051E+04

1. 151E+06

1. 152E+06 1. 153E+06 Blocks:

1.154E+06

1. 155E+06 876.0000 876.0000 730. 0000 54 876.0000 876. 0000 1.156E+06 1752.0000 1.162E+06 5256.0000

1. 172E+06

1. 051E+04

1. 173E+06 1.174E+06 1.175E+06 Blocks:

1.176E+06 1.176E+06 876. 0000 876.0000 730. 0000 55 876. 0000 876. 0000

1. 178E+06 1752. 0000 1.183E+06 5256. 0000

1. 1 94E+06

l. 051E+04 1.195E+06 1.196E+06

1. 1 96E+06 Blocks:

1.197E+06 876.0000 876.0000 730. 0000 56 876.0000 l.l98E+06 876.0000

1. 200E+06 1752.0000 1. 205E+06 5256. 0000

1. 216E+06

1. 051E+04

1. 217E+06 876.0000

1. 218E+06 730.0000 Blocks:

57 -0.2040 17.7389 -0. 2042 17.7336 - 2.3341 15.5523 - 4.2310

13. 6107

-4. 9964 12. 8269 -5. 8284 11.9755 -6.4274

11. 3627

-6.7269

11. 0563

-0.2081 17.6098 - 0. 2083 17.6047 - 2. 3380

15. 4393

- 4. 2346

13. 5119

-5. 0000 12.7338 -5. 831 9 11.8886 -6. 4308 11. 2802 -6. 7303 10.9760 -0.2122 17.4846 - 0.2 123 17.4797 - 2. 3417 15. 3298 -4.2382 13.4160 -5. 0035

12. 6434

-5. 8352 11.8042 -6.4 34 1 11.2002 -6.7335 10. 8981 -0. 2161 17. 3632 -0.2162 17. 3584 - 2. 3454 15. 2234 - 4. 24 16 13.3230 - 5. 0068 12.5558 -5. 8385 11.7224 -6.4373 11.1225 -6.7367

10. 8226

-0.2199 17.2452 -41.0935 -0. 1938 - 30. 1388 3. 3631 - 20.3823

6. 5306

-16.4455

7. 8083

-12.1663

9. 1974

-9.0852 10.1977 - 7.5447 10.6978 -41.0986 -0.1924 -30.1434 3.3386 - 20.3863

6. 4 832

-16.4493

7. 7516

-12.1699 9. 1307 -9. 0887 10. 1236 -7.5481

10. 6201

-41.1035 -0. 1911 -30.1478 3. 31 49 -20.3902 6.4372 -16.4530 7. 6967 -12. 1734

9. 0659

-9. 0920

10. 0518

-7. 5514 10.5448 -41.1083 -0. 1897 -30.1520

3. 2919

-20. 3940

6. 3925

-16.4566

7. 6433

-12.1768

9. 0030

-9. 0953

9. 9821

-7.5546 10.4717 Report No. 1600539.401RO

0. 0000

1. 282E-04 40. 8894

1. OOOE-30 17.9274

4. 551E-06 27.8048

1. OOOE-30 12.1892

1. 793E- 06 16.151 3

1. OOOE-30 7. 0801

4. 040E-07

11. 44 90

1. OOOE-30

5. 0186

1. 461E-07 6. 3379

1. OOOE-30

2. 7781 2. 369E-08 2. 657 8 1. OOOE-30 1.1650

4. 725E-09

0. 8178

1. OOOE-30 0. 3585

2. 222E-24 0. 0000

1. 261E-04 40.8903

1. OOOE-30

17. 7971

4. 443E-06

27. 8054

1. OOOE-30 12.1007

1. 751E-06 16. 1517

1. OOOE-30 7.0287 3.944E-07 11.4493

1. OOOE-30 4. 9821 1.426E-07

6. 3380

1. OOOE-30

2. 7 579

2. 313E-08

2. 6579 1. OOOE-30

1. 1565 4. 612E-09

0. 817 8

1. OOOE-30

0. 3559

2. 206E-24 0. 0000 1. 242E-04 40.8912

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4. 9468

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6. 3381

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40. 8921

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17. 54 81

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11. 9315 1. 671E-06 16.1524

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6. 9305

3. 765E-07 11.4498

1. OOOE-30 4. 9125

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21. 6710

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0. 4437 22.2812 S) Stnu:tutalllllefrlly Associates. Inc.*

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1. 051E+04

1. 238E+06

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1. 259E+06

1. 051E+04

1. 260E+06 1. 261E+06

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1. 281E+06

1. 051E+04

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1. 287E+06 1752. 0000

1. 292E+06 5256. 0000

1. 303E+06

1. 051E+04

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1. 307E+06 876.0000 876.0000 730. 0000 61 876.0000 876. 0000

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9. 7225

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1. OOOE-30 17.4290 4.147E-06 27. 8072

1. OOOE-30

11. 8505

1. 634E-06 16.1527

1. OOOE-30

6. 8835

3. 682E-07 11. 4500

1. OOOE-30

4. 8792

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11. 4503

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11. 6954 1. 565E- 06

16. 1534 1. OOOE-30

6. 7934 3. 525E-07 11.4505

1. OOOE-30

4. 8153

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1. OOOE-30 17. 0913

3. 888E-06

27. 8089

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11. 6210

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1. OOOE-30 6.7502 3.452E-07 11.4507

1. OOOE-30

4. 7847

1. 248E- 07

6. 3388

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2. 6486

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1. OOOE-30 16.9848 3. 808E-06 27. 8094

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14. 0421

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0. 4437 22.2869 0.4437 22.2892 0.4437 22.2902

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22. 291 3

0. 4437 22.2917 0.4437 22. 2917 0.4437 22.2917

0. 4437

22. 4302 0. 4437 22.4359 0.4437 22. 4381

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22. 5858 0. 4437 22.5869 0. 4437 22.5872 0.4437 22.5872

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22. 8719 SJ Stnn:tuliiiiRiegrlty Associates, Inc.*

1. 309E+06 17 52. 0000

1. 314E+06 5256.0000

1. 325E+06

1. 051E+04 1. 325E+06

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1. 352E+06 1752.0000

1. 358E+06 5256. 0000

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9. 9548

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1. OOOE-30

6. 7081

3. 381E-07 11.4509

1. OOOE-3 0

4. 7549 1.223E-07 6. 3389

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1. 456E+06 876.0000

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1. 051E+04

1. 478E+06

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5. 9099

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7. 0663

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8. 3235

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6. 3393

1. OOOE-30

2. 5702

1. 833E-08

2. 6584

1. OOOE-30

1. 0778

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1. OOOE-30 11.2131

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2. 5557

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2. 6585

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27. 8122

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1. 0543 3. 398E-09 B-40

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0. 6300 14.8361

0. 6300

14. 8392 0.6300 14.8404

0. 6300 14.8409 0.6300 14.8415 0.6300 14.8417

0. 6300 14.84 17

0. 6300 14.8417

0. 6300 14.9191

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14. 9238

0. 6300 14.92 44

0. 6300 14.9246

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15. 0062

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15. 0064

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15. 0064

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15. 0871

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15. 0873

0. 4437 23.4251 0. 4437

23. 4251 0. 4437

23. 4251 0.4437 23.5496

0. 4437 23.5544

0. 4437 23.5563 0.4437 23.5571 0.4437 23.5580 0.4437

23. 5583 0.4437 23. 5584 0.4437 23.5584 0.4437

23. 6813 0.4437

23. 6860 0.4437 23.6879 0.4437 23.6887 0.4437 23.6896 0.4437 23.6899 0.4437

23. 6899 0.4437 23.6899

0.4437

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0. 4437 23.8199 0.4437

23. 9399 0.4437 23.9445 0.4437 23.9462 0.4437 23.9471 0.4437 23.9479 0.4437 23.9482 0. 4437 23.9482 I)

Stnu:tunrlllllegrlty Associates. Inc.*

1o 500E+06

1. 501E+06 Blocks:

lo 502E+06

1. 503E+06 8760 0000 730 0 0000 70 876 o 0000 876 o 0000

1. 505E+06 17 52 o 0000 1 o 510E+06 5256 o 0000

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1. 051E+04

1. 521E+06 876o 0000 1o 522E+06 876o 0000 10 523E+06 730 o0000 Blocks:

71 l o 524E+0 6 876 o 0000 l o 525E+06 876o 0000

1. 526E+06 1752 o 0000 10 532E+06 5256 o 0000 1 o 542E+06 1 0 051E+04

1. 543E+06

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1. 545E+06 Blocks:

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l. 546E+06 876o 0000 876 0 0000 730o 0000 72 876o0000 8760 0000 1.548E+06 l752o0000

l. 553E+06 52560 0000

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l. 051E+04 lo 586E+06 876 0 0000

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l. 019E-04 40 o 9022

1. OOOE-30 16o1370 3 o216E-06 27 o 8135

1. OOOE-30 10 o 9724

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1. OOOE-30 4 o 5177

1. 033E-07 6 o3398 l.OOOE-30 2 o 5009

1. 675E-08 2 o 6586

1. OOOE-30 1.0487 3 o340E-09 0 o 8180 10 OOOE-30 0 o 3227 1o 991E-24 0 0 0000 lo 007E-04 40 o 9028

1. OO OE-30 16o0534 3ol61E-06 27 o 8139 10 OOOE-30 10 o 9155 1.246E-06 16 o1566

1. OOOE-30 6 o3404 2 o807E-07 11 0 4528 1o OOOE-30 4 o 4943

l. 015E-07 6o3399 l.OOOE-30 2o4879 1.646E-08 2 o 6587 l o OOOE-30 lo 0433 3 o 283E-09 Oo 8181

1. OOOE-30 Oo3210 l.980E-24 0 0 0000 9 o 958E-05 40 o 9034 1o OOOE-30 15 o 9716 3 ol09E- 06 27 o 8143 1o OOOE-30 10 o 8599 10 225E-06 16o1568 l.OOOE-30 6o3081 2 0 760E-07 11 0 4530 1 o OOOE-30 4 o 4 714 9 o 982E-08 6 o 34 00 1 o OOOE-30 2 o4752 1.619E-08 2 o 6587 10 OOOE-30

1. 0380 3 o 228E-09 Oo8181 l.OOOE-30 0 o 3194 1o 969E-24 OoOOOO 9o 850E-05 40 o 9040

l. OOOE-30 15 o 8915 3 o 057E-06 27 o 8147

1. OOOE-30 10 o 8055

1. 205E-06 16 ol 571

l. OOOE-30 6 o 2765 2 o 715E- 07 110 4531 1o OOOE-30 4o4490 9 o8l8E- 08 6o3401 l.OOOE-30 2o4628 l.592E-08 2 o 6588 l

o OOOE-30

1. 0328 3 o175E-09 Oo 8181

1. OOOE-30 Oo3l78 1.959E-24 OoOOOO 9 o 744E-05 B-41 0 0 6300 15 0 0873 0 0 6300 15 ol620 0 0 6300 15 ol649 0 0 6300 15 01660 0 0 6300 15o1665 Oo6300 l5o1670 0 0 6300 15 o1672 0 0 6300 15 ol672 0 0 6300 15 ol672 0 0 6300 15 o2411 0 0 6300 15 o2439 0 0 6300 15 o2450 Oo6300 15 0 2455 0 0 6300 l5o2460 0 0 6300 15o2462 0 0 6300 l5 o2462 0 0 6300 l5o2462 0 0 6300 15 0 3192 0 0 6300 15 0 3220 0 0 6300 15o3230 0 0 6300 15 0 3235 0 0 6300 15 o3240 0 0 6300 15 0 3242 0 0 6300 15 0 3242 0 0 6300 15 0 3242 0 0 6300 15 0 3965 0 0 6300 15 0 3992 Oo6300 15o4002 0 0 6300 l5o4007 0 0 6300 15o4012 0 0 6300 l5 o4014 0 0 6300 15 o4014 0 0 6300 15o4014 Oo6300 l5o4729 0 0 4437 23 0 9482 Oo4437 24o0669 0 0 4437 24o0713 Oo4437 24 0 0731 Oo4437 24 0 0739 Oo4437 24 0 0748 Oo4437 24o0750 Oo4437 24 o0750 0 0 4437 24 o0750 0 0 4437 24 o1924 Oo4437 24 ol968 Oo4437 24 o1985 Oo4437 24 o1993 0 0 4437 24o2001 0 0 4437 24o2004 Oo4437 24 0 2004 Oo4437 24o2004 Oo4437 24 0 3164 Oo4437 24 o3207 0 0 4437 24 0 3224 0 0 4437 24 0 3232 0 0 4437 24 o3240 Oo4437 24 o3243 0 0 4437 24 0 3243 Oo4437 24 0 3243 0 0 4437 24o4390 0 0 4437 24o4433 0 0 4437 24 o4449 0 0 4437 24 0 4457 Oo4437 24o4465 Oo4437 24o4468 Oo4437 24 o4468 0 0 4437 24o4468 0 0 4437 24 0 5603 SJs~roc:tutalllllegrlty Associates. Inc.*

Blocks:

1. 589E+06

1. 590E+06 74 876.0000 876.0000

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1. 612E+06 876.0000 876.0000 730.0000 75 876.0000 876.0000

1. 613E+06 1752.0000

1. 619E+06 5256. 0000

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1. 630E+06

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1. 633E+06 876.0000 876.0000 730. 0000 76 876.0000 876.0000

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1. 640E+06 5256.0000

1. 651E+06

1. 051E+04

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1. 653E+06

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1. 655E+06 876.0000 876.0000 730.0000 77 876.0000 876.0000

1. 657E+06 1752.0000

1. 662E+06 5256. 0000

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12. 0063

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8. 0741

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8. 8676

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9. 3025

-41. 1876 -0.1678 Report No. 1600539.401RO 40.9045

1. OOOE-30 15.8 131

3. 008E-06 27.8151

1. OOOE-30 10.7522 1. 186E-06 16.1573

1. OOOE-30 6.2456 2.671E-07 11.4533

1. OOOE-30

4. 4271

9. 659E-08

6. 3402

1. OOOE-30

2. 4507

1. 567E-08

2. 6588

1. OOOE-30 1. 0277 3. 124E-09 0.8181 l.OOOE-30

0. 3162

1. 949E-24

0. 0000 9. 641E-05 40.9051

1. OOOE-30 15. 7363 2.960E- 06 2 7.8 155

1. OOOE-30 10.7000 1.167E-06 16.1575

1. OOOE-30 6.2152 2.628E-07

11. 4534

1. OOOE-30 4.4056 9.505E-08

6. 3403

1. OOOE-30 2.4388 1.542E-08

2. 6588

1. OOOE-30

1. 0227

3. 074E-09

0. 8181

1. OOOE-30

0. 314 7

1. 939E-24

0. 0000

9. 541E- 05 40.9056

1. OOOE-30 15.6611

2. 914E- 06

27. 8158

1. OOOE-30 10.6489 1.148E-06 16.1577

1. OOOE-30 6.1856

2. 587E-07

11. 4536

1. OOOE-30 4.3846 9.356E-08 6.3404

1. OOOE-30

2. 4271

1. 517E-08

2. 6589

1. OOOE-30

1. 0178

3. 026E-09

0. 8181

1. OOOE-30

0. 3132.

1. 929E-24

0. 0000 9.443E-05 4 0. 9062

1. OOOE-30 15.5874

2. 869E-06 27.8162 1. OOOE-30

10. 5987 1.131E-06 16.1579 l.OOOE-30 6.1565 2.547E-07

11. 4537 1. OOOE-30

4. 3639

9. 212E-08 6.3405 l.OOOE-30 2.4157 1.494E-08

2. 6589

1. OOOE-30

1. 0130

2. 979E- 09

0. 8181

1. OOOE-30

0. 3117

1. 920E-24

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1. OOOE-30

15. 5151

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o. 6300 15.4775

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15. 551 0

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15. 5530

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15. 5532

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15. 6232

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15. 6272

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15. 6277 0. 6300 15.6278

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0. 6300 15.7727 0.4437 24. 5644 0. 4437

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24. 5668 0.4437 24.5676 0.4437 24.5679

0. 4437

24. 5679 0.4437

24. 5679 0.4437 24.6802

0. 4437 24.6843 0.4437

24. 6859 0.4437 24. 6866 0.4437 24. 6874 0.4437

24. 6877 0. 44'37

24. 6877 0.4437

24. 6877 0. 4437 24.7988 0.4437 24.8028 0.4437 24.8044

0. 4437 24.8052 0.4437 24.8059

0. 4437 24.8062

0. 4437 24.8062 0.4437 24.9161

0. 4437

24. 9201 0.4437

24. 9217

0. 4437

24. 9224 0.4437 24. 9232

o. 4437 24.9234 0. 4437

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25. 0323

0. 4437

25. 0362 SJstroGtutaiiRlegrlty Associates. 1nc.*

1. 677E+06 876.000 0

1. 679E+06 1752.0000 1. 684E+06 52 56. 000 0 1. 694E+06 1. 051E+04

1. 695E+06 1. 696E+06

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5. 5520 Report No. 1600539.401RO 27.8165

1. OOOE-30

10. 5496

1. 114E-06 16.1581

1. OOOE-30 6.1279 2.509E-07 11. 4539

1. OOOE-30 4. 3437

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1. OOOE-30

6. 0999

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1. OOOE-30 4.3239 8.936E-08 6. 3406

1. OOOE-30 2. 3936

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2. 6590

1. OOOE-30

1. 0037

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1. 081E-06 1 6. 1585 1. OOOE-30

6. 0725

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1. OOOE-30

4. 3044

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6. 3407

1. OOOE-30

2. 3828 1. 428E-08

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1. OOOE-30 0. 9992 2.847E-09 0. 8182

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1. OOOE-30

15. 3066

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1. OOOE-30

10. 4 079

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1. OOOE-30 6.0456 2.399E-07 11.4543

1. OOOE-30

4. 2854

8. 676E-08 6.3408 l.OOOE-30

2. 3722

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0. 8182

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1. OOOE-30 15. 2396

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10. 3624

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1. OOOE-30 6. 0192

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0. 6300 15.7737 0.6300 15.7741

0. 6300

15. 7 746

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0. 6300

15. 9143 0. 6300 15.9167

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0. 6300

15. 9187

0. 6300 15.9187 0. 6300 15.9187

0. 6300 15. 9853

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15. 9876

0. 6300 15.9886 0.6300

15. 9890

0. 6300 15. 9894 0. 6300 15.9896 0.6300

15. 9896

0. 6300

15. 9896

0. 6300

16. 0555

0. 6300 16.0578

0. 6300 16.0588 0. 6300

16. 0592 0.4437

25. 0377

0. 4437 25. 0384

0. 4437 25. 0392 0. 4437 25. 0394

0. 4437 25. 0395 0. 4437

25. 0395

0. 4437 25. 1472

0. 4437 25. 1511 0.443 7 25.1526 0.4437 25. 1533 0. 4437 25.1540 0.4437 25.1543 0.4437 25.1543 0.4437 25.1543 0.4437 25.2609 0. 4437 25.2648 0.4437 25. 2663 0.4437 25.2669 0.4437 25.2677 0.4437 25.2679 0.4437 25.2679 0.4437 25. 2679 0.4437 25.3736 0.4437

25. 3773 0.4437 25.3788 0. 4437 25.3795 0.4437 25.3802 0.4437 25.3804 0.4437 25.3804 0. 4437 25.3804 0.4437 25.4851 0. 4437 25.4888 0.4437 25.4902 0. 4437 25.4909 S)stnu:tura~ Integrity Associates. Inc.*

1. 771E+06 5256. 0000

1. 78 1E+06

1. 051E+04

1. 782E+06

1. 783E+06

1. 784E+06 Blocks :

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1. 786E+06 876.0000 876.0000 730.0000 83 876.0000 876.0000

1. 787E+06 1752.0000

1. 793E+06 5256.0000

1. 803E+06

1. 051E+04

1. 804 E+06

1. 805E+06 1. 806E+06 Blocks:

1. 806E+06

1. 807E+06 876.0000 876.0000 730.0000 84 876.0000 876.0000

1. 809E+06 1752.0000

1. 814E+06 5256.0000

1. 825E+06

1. 051E+04

1. 826E+06

1. 827E+06

1. 827E+06 Blocks:

1. 828E+06

1. 829E+06 876.0000 876.0000 730.0000 85 876.0000 876.0000

1. 831E+06 1752.0000

1. 836E+06 5256. 0000

1. 84 7E+06

1. 051E+04

1. 847E+06

1. 848E+06

1. 84 9E+06 Blocks :

1. 850E+0 6

1. 851 E+06 876.0000 876.0000 730.0000 86 876.0000 876.0000

1. 853E+06 1752.0000

1. 858E+06 5256. 0000

1. 868E+06

1. 051E+04

-5. 0700

10. 9050

-5.8999 10.1813 - 6.4974

9. 6603

-6.7962

9. 3998

-0.2917

15. 0121

-0.2918

15. 0099

-2.4163 13.1644 -4. 3083

11. 5212

-5. 0718 10.8581 -5.9017 10. 1374 -6.4992

9. 6187

-6.7979

9. 3593

-0.2938 14.9482 -0.2938 14.9461 -2.4182 13.1085 -4. 3101 11.4723 -5.0736 10. 8119 - 5. 9034

10. 0944

-6. 5008 9.5778 -6. 7996

9. 3195

-0.2958

14. 8855

-0.2959 14.8834 -2. 4201

13. 0535

- 4. 3119

11. 4242

-5.0753 10.7666 -5. 9051

10. 0521

-6. 5025

9. 5377

-6.8012

9. 2805

-0. 2978

14. 8239

-0. 2978 14. 8218 -2. 4219

12. 9995

-4. 3137 11.3769 - 5.0770 10.7221 -5. 9067

10. 0105

-16.5244

6. 6384

-12.2408

7. 8195

-9. 1565

8. 6698

-7.6144

9. 0950

-41.2009 -0.1641 -30.2345

2. 8467

-20.4674

5. 5280

-16.5264

6. 6098

-12. 2426

7. 7858

- 9.158 3

8. 6325

- 7.6161

9. 0558

-41.2034 -0. 1634 - 30. 2367 2. 8346 - 20.4694

5. 5045

-16.5283

6. 5817

-12. 2444

7. 7527

- 9.1600

8. 5958

- 7.6178 9.0174 -41.2 059 -0.1627 -30.2389

2. 8227

-20.4714

5. 4815

- 1 6.5301

6. 5541

-12.2461

7. 7202

-9.1616

8. 5598

-7.6194

8. 9796

-41.2083 -0.1620 -30.2411

2. 8110

-20. 473 3 5.4588 -16.5320

6. 5270

-12.2479

7. 6883 Report No. 1600539.401RO 11.454 4

1. OOOE-30

4. 2666

8. 551E- 08

6. 3408

1. OOOE-30

2. 3619

1. 387E-08

2. 6591

1. OOOE-30 0.9905

2. 765E-09

0. 8182

1. OOOE-30 0.3048 1.875E-24

0. 0000

8. 905E-05 40.9091

1. OODE-30 15.1739

2. 625E- 06 27.8 1 82

1. ODOE-30 10.3177

1. 035E- 06 16.1591

1. OOOE-30

5. 9932

2. 331E-07 11.4546

1. OOOE-30 4.2482 8.430E-08

6. 3409

1. OOOE-30

2. 3517

1. 367E-08 2. 6591

1. OOOE-30 0.9862

2. 726E-09

0. 8182

1. OOOE-30

0. 3034

1. 867E-24

0. 0000

8. 823E-05 40.9096

1. ODOE-30 15.1094

2. 588E-06

27. 8185

1. ODOE-30 10.2738

1. 020E- 06 16.1593 1. OOOE-30

5. 9677

2. 299E-07 11.4547

1. OOOE-30

4. 2302

8. 312E-08

6. 3410

1. OOOE-30 2. 3417

1. 34 8E-08

2. 6591

1. OOOE-30

0. 9820

2. 688E-09

0. 8182 1. OOOE-30

0. 3022 1. 858E-24 D. 0000

8. 742E- 05 40.9100

1. OOOE-30 15.0461

2. 553E- 06

27. 8188

1. OOOE-30 10.2308

1. 006E-06 16.1595

1. OOOE-30

5. 9427

2. 267E-07 11.4548

1. OOOE-30

4. 2125 8.198E-08

6. 3411

1. OOOE-30

2. 3319

1. 330E-08 2. 6592 1. OOOE-30

0. 9779

2. 651E-09

0. 8182

1. OOOE-30

0. 3009

1. 850E-24

0. 0000

8. 663E-05 40.9105

1. OOOE-30

14. 9838

2. 518E-06 27.8191

1. OOOE-30 10.1885

9. 927E-07 1 6.1596

1. OOOE-30 5. 9182

2. 236E-07 11.4549

1. OOOE-30 4.1950

8. 087E-08

6. 3411

1. OOOE-30

2. 3222

1. 312E-08 B-44

0. 6300 16.0596

0. 6300 16.0598

0. 6300 16.1251

0. 6300 16.1274

0. 6300 1 6.1283

0. 6300 16. 1287

0. 6300 16.1291

0. 6300 16.1293

0. 6300 16.1293 0. 6300 16.1293

0. 6300

16. 1939

0. 6300

16. 1962

0. 6300

16. 1971

0. 6300 16.1975 0. 6300 16.1979 0.6300 16.198 1

0. 6300 16.1981

0. 6300 16.198 1

0. 6300 16.2622 0. 6300 16.264 4

0. 6300 16.2653

0. 6300 1 6.2657

0. 6300 16.2661

0. 6300 16.2663

0. 6300

16. 3298

0. 6300 16.3320

0. 6300 16.3329

0. 6300 16.3333

0. 6300

16. 3337

0. 6300 16.3338 0.4437 25.4916 0.4437 25.4918 0.4437 25.4918

0. 4437 25.4918 0.4437

25. 5955 0.4437 25.5991 0.4437 25. 6006

0. 4437

25. 6012

0. 4437 25.6019

0. 4437

25. 6021 0.4437

25. 6021

0. 4437 25.6021

0. 4437 25.7048 0. 4437 25.7084

0. 4437 25.7098 0.4437 25.7105

0. 4437

25. 7112 0.4437 25.7114

0. 4437 25.7114 0.4437 25.7114 0.4437 25. 8131

0. 4437 25. 8167

' 0.4437 25.8181

o. 4437 25.81 87

0. 4437 25.8194 0. 4437 25.8196

0. 4437 25.8196 0. 4437 25.8196 0.4437

25. 9204 0.4437

25. 9239 0.4437

25. 9253

0. 4437

25. 9259 0.4437 25.9266

0. 4437 25.9268

1. 869E+06

1. 870E+06

1. 871E+06 Blocks:

1. 872E+06

1. 873E+06 876.0000 876.0000 730. 0000 87 876.0000 876.0000

1. 874E+06 1752. 0000

1. 880E+06 5256.0000

1. 890E+06

1. 051E+04

1. 891E+06 1. 892E+06

1. 893E+06 Blocks:

1. 893E+06 1. 894E+06 876.0000 876.0000 730.0000 88 876. 0000 876. 0000

1. 896E+06 1752.0000

1. 901E+06 5256. 0000

1. 912E+06

1. 051E+04

1. 913E+06

1. 914E+06

1. 914E+06 Blocks:

1. 915E+06

1. 916E+06 876.0000 876. 0000 730.. 0000 89 876.0000 876.0000

1. 918E+06 1752.0000

1. 923E+06 5256. 0000

1. 934E+06

1. 051E+04

1. 935E+06

1. 935E+06 1. 936E+06 Blocks:

1. 937E+06

1. 938E+06 876. 0000 876.0000 730.0000 90 876.0000 876.0000

1. 940E+06 1752. 0000

1. 945E+06 5256.0000

1. 955E+06

1. 051E+04

1. 956E+06 876.0000

1. 957E+06 876.0 000

-6.5041 9.4982 -6.8028

9. 2421

-0.2997 14.7633 -0.2998 14.7613 -2.4238 12. 9464 -4. 3154 11. 3305 -5.0787 10.6783 -5. 9084 9. 9696 -6. 5057

9. 4595

-6.8044 9.2044 -0. 3016 14.7038 -0.3017 14.7018 -2. 4255 12.8943, -4.3171

11. 2849

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10. 5930

-5. 9115

9. 8900

-6. 5088 9. 3839 - 6.8075 9.1309 -0. 3054 14.5878 -0.3054 14.5859 -2. 4290

12. 7926

-4.3204 11. 1959 -5. 0835 10. 5 515 -5. 9131

9. 8512

-6. 5103

9. 34 71

-6. 80 90

9. 0950

-9.1633 8.5244 - 7.6210

8. 9424

-41.2107 -0.1614 -30.2432

2. 7996

-20.4752

5. 4365

-16.5337 6. 5004 -12.2495

7. 6569

-9.1649 8.4896 -7.6226

8. 9059

-41.2131 -0.1607 -30. 2453

2. 7883

-20.4771

5. 4146

-16.5355

6. 4742

-12.2512 7. 6260 -9. 1665 8. 4554 -7. 6242 8. 8701 -41.2154 -0. 1601 -30.2473

2. 7772

-20.4789

5. 3931

-16.5373 6. 4485 -12.2529

7. 5957

-9.1681

8. 4218

-7.6257 8. 8348 -41.2176 - 0. 1594 -30.2493 2. 7663 -20. 4807

5. 3719

-16.5390 6. 4232 -12.2545

7. 5659

-9. 1696

8. 3887

-7.6272

8. 8002 Report No. 1600539.401RO 2. 6592

1. OOOE-30

0. 9738

2. 615E-09

0. 8182

1. OOOE-30

0. 2996

1. 842E-24 0. 0000

8. 586E- 05 40.9109

1. OOOE-30 14.9227

2. 484E-06 27.8194

1. OOOE-30 10.1469 9.794E- 07 16. 1598

1. OOOE-30 5.8940 2.206E- 07 11.4551

1. OOOE-30 4.1779 7.978E- 08

6. 3412

1. OOOE-30

2. 3128

1. 294E-08

2. 6592

1. OOOE-30 0. 9699 2.580E-09

0. 8182

1. OOOE-30

0. 2984

1. 834E-24

0. 0000

8. SllE-05 40.9113

1. OOOE-30

14. 8625

2. 451E-06

27. 8197

1. OOOE-30 10.1060 9. 664E- 07 16.1600

1. OOOE-30 5. 8703 2. 177E-07 ll. 4552

1. OOOE-30 4.16ll 7. 873E- 08 6. 3413

1. OOOE-30

2. 3034

1. 277E-08 2. 6592

1. OOOE-30 0.9660 2.546E-09

0. 8182

1. OOOE-30 0. 2972

1. 826E-24

0. 0000.

8. 437E- 05 40.9ll8 l.OOOE-30 14. 8034

2. 419E-06 27.8200

1. OOOE-30 10.0658 9.538E- 07

16. i602

1. OOOE-30 5.8469 2.149E- 07 ll. 4553 1. OOOE-30 4.1446

7. 770E-08

6. 3413 1. OOOE-30

2. 2943

1. 260E-08

2. 6593

1. OOOE-30

0. 9621

2. 513E- 09

0. 8182

1. OOOE-30

0. 2960

1. 819E-24 0. 0000

8. 365E-05 40.9122

1. OOOE-30 14.7453

2. 388E-06 27. 8203

1. OOOE-30 10.0263 9.415E-07 16.1603

1. OOOE-30

5. 8240 2.121E-07 11. 4554

1. OOOE-30 4.1283

7. 670E-08

6. 3414

1. OOOE-30 2.2853 1.244E-08

2. 6593 1. OOOE-30 0.9583 2.480E-09

0. 8182 1. OOOE-30

0. 2949 1. 8llE-24 B-45

0. 6300 16.3338

0. 6300 16.3338 0. 6300 16.3968

0. 6300 16.3989

0. 6300

16. 3998 0. 6300 16.4002

0. 6300 16.4006

0. 6300 16. 4007 0. 6300 16. 4007

0. 6300 16.4007 0. 6300 16.4631

0. 6300 16.4653

0. 6300 16.4661

0. 6300 16.4665 0. 6300 16.4669

0. 6300 16.4670 0.6300 16.4671 0. 6300 16. 4671

0. 6300 16. 5289

0. 6300 16.5310

0. 6300 16.5319

0. 6300

16. 5322

0. 6300 16.5326

0. 6300 16.5328

0. 6300 16.5328 0. 6300 16.5328 0. 6300 16.5941

0. 6300

16. 5962 0. 6300 16.5970

0. 6300 16.5974

0. 6300 16.5978

0. 6300 16.5979

0. 63 00 16.5979 0.4437 25.9268 0. 4437

25. 9268 0.4437 26.0267 0.4437 26.0302 0.4437 26. 0316 0.4437 26. 0322

0. 4437

26. 0328 0. 4437

26. 0331 0.4437

26. 0331 0. 4437 26.0331

0. 4437 26.1321 0.4437 26. 1355 0. 4437 26.1368 0. 4437 26.1374 0. 4437 26.1381 0.4437

26. 1383 0.4437 26.1383 0.4437 26.1383 0.4437 26.2365 0.4437 26.2399 0.4437 26. 2412 0.4437 26.2418 0.4437 26. 2424 0.4437 26.2426 0.4437 26.2426 0.4437 26.2426 0. 4437 26.3400 0. 4437 26.3433 0. 4437 26.3446 0.4437 26.3452 0. 4437 26.3458

0. 4437 26.3460 0.4437 26. 3460 0.4437 26.3460 S)Stntctrua~ltrlefrlly Associates. Inc.*

1. 958E+06 Blocks:

1. 959E+06

1. 960E+06 730. 0000 91 876.0000 876.0000

1. 961E+06 1752.0000

1. 967E+06 5256.0000

1. 977E+06

1. 051E+04

1. 978E+06

1. 979E+06

1. 980E+06 Blocks:

1. 980E+06

1. 981E+06 876.0000 876.0000 730.0000 92 876.0000 876.0000

1. 983E+06 1752.0000

1. 988E+06 5256.0000

1. 999E+06

1. 051E+04

2. OOOE+06

2. 001E+06

2. 001E+06 Blocks:

2. 002E+06

2. 003E+06 876.0000 876.0000 730.0000 93 876.0000 876. 0000

2. 005E+06

'1752. 0000

2. 010E+06 5256. 0000

2. 021E+06

1. 051E+04

2. 022E+06

2. 023E+06 Blocks:

2. 024E+06

2. 025E+06 876.0000 876.0000 730.0000 94 876.0000 876.0000 2.027E+06 1752.0000

2. 032E+06 5256.0000

2. 042E+06

1. 051E+04

2. 043E+06 876.0000 2. 044E+06 876.0000

2. 045E+06 730.0000 Blocks:

95 -0. 3072

14. 5312

-0.3073 14.5293 -2.4308 12.7430 -4. 3220

11. 1525

-5.0851 10.5106 -5.9146

9. 8130

-6. 5118

9. 3109

-6.8104

9. 0598

-0.3090 14.4755 -0. 3090 14.4 737 -2.4324 12.6943 -4.3236 11.1098 -5.0867 10.4703 -5.9161

9. 77 55

-6. 5133 9. 2752 -6.8119 9. 0251 -0. 3108 14. 4208 -0. 3108

14. 4190

-2. 4341 12.6463 -4. 3251 11.0678 -5.0882 10. 4308 -5.9176

9. 7385

-6.5147 9.2402 -6.8133

8. 9910

-0. 3125

14. 3669

-0. 3125

14. 3651

-2.4357

12. 5990

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10. 3918

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9. 7022

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8. 9574

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2. 7556

-20. 482 5

5. 3511

-16. 5406

6. 3983

-12.2560 7. 5366 -9.1711

8. 3562

-7.628 7

8. 7661

-41.2221 -0.1582 -30.2533

2. 7450

-20. 4 842

5. 3306

-16.5423

6. 3738

-12.2576

7. 5078

-9.1726

8. 3243

-7.6301

8. 7325

-41.2242 -0.1576 -30.2552 2.7347 -20.4859

5. 3105

-16.5439

6. 34 97

-12.2591

7. 4 794

-9.1741

8. 2928

-7.6316

8. 6995

-41.2263 -0.1570 -30.25 71

2. 7244

-20.4876

5. 2906

-16.5455

6. 3260

-12.2607

7. 4515

-9.1755

8. 2618

-7.6330

8. 6670 Report No. 1600539.401RO

0. 0000

8. 295E-05 40.9126

1. OOOE-30 14.6881

2. 358E-06 27.8206

1. OOOE-30 9.9874 9.295E-07 16.1605

1. OOOE-30

5. 8014

2. 094E-07 11.4555

1. OOOE-30 4.1123

7. 572E-08 6.3415 1.000E-30 2.2764 1.228E-08

2. 6593

1. OOOE-30 0.9546 2.449E-09

0. 8183

1. OOOE-30 0.2937 1.804E-24 0.0000

8. 225E-05 40.9130

1. OOOE-30

14. 6319

2. 328E-06 27.8208 1. OOOE-30

9. 9492 9. 178E-07 16.1606

1. OOOE-30

5. 7792

2. 068E-07 11.4556

1. OOOE-30 4.0966 7.477E-08

6. 3415

1. OOOE-30

2. 2677

1. 213E-08

2. 6593

1. OOOE-30 0.9510 2.418E-09

0. 8183

1. OOOE-30

0. 2926

1. 797E-24

0. 0000 8.158E-05 4 0. 9134

1. OOOE-30 14.5766 2. 299E-06

27. 8211

1. OOOE-30

9. 9116

9. 064E-07 16.1608

1. OOOE-30 5.7574 2.042E-07 11.4558

1. OOOE-30

4. 0811

7. 384E-08

6. 3416

1. OOOE-30

2. 2591 1.198E-08

2. 6594

1. OOOE-30 0.9474 2.388E-09 0.8183 l.OOOE-30 0.2915

1. 790E-24 0.0000

8. 091E-05 40.9138

1. OOOE-30 14.5221

2. 271E-06

27. 8214 1. OOOE-30 9.8746 8.953E-07 16.1610

1. OOOE-30

5. 7358

2. 017E-07 11.4559

1. OOOE-30

4. 0658

7. 294E-08 6.3416

1. OOOE-30

2. 2507 1.183E-08

2. 6594

1. OOOE-30

0. 9438

2. 359E-09

0. 8183

1. OOOE-30

0. 2904

1. 7 83E-24

0. 0000

8. 026E-05 B-46 0. 6300 16.6587

0. 6300

16. 6608

0. 6300

16. 6616

0. 6300 16.6619

0. 6300

16. 6623

0. 6300

16. 6625

0. 6300 16.6625

0. 6300 16.7228 0.6300 16.7248 0.6300 16.7256 0.6300 16.7260

0. 6300 16.7264 0.6300 16.7265

0. 6300 16.7265

0. 6300 16.7863

0. 6300 16.7883

0. 6300 16.7891

0. 6300 16.7894

0. 6300 16.7898 0. 6300 16.7899

0. 6300 16.7900

0. 6300 16.8492

0. 6300

16. 8512

0. 6300 16.8520

0. 6300

16. 8524

0. 6300 16.8528

0. 6300 16.8529

0. 6300 16.8529 0.6300 16.8529

0. 6300 16.9117

0. 4437 26.4425

0. 4437 26.4458 0.4437 26.4471 0.4437 26.4477

0. 4437 26.4483 0.4437 26.4485

0. 4437 26.4485

0. 4437 26.4485 0. 4437 26.5442

0. 4437 26.5474

0. 4437 26.5487

0. 4437 26.5493

0. 4437 26.5499

0. 4437 26.5501

0. 4437 26.6450

0. 4437 26.6482

0. 4437 26.6495

0. 4437 26.6500

0. 4437 26.6507 0.4437

26. 6509 0.4437 26.6509

0. 4437 26.6509 0.4437 26.7450

0. 4437 26.7481

0. 4437 26.7494

0. 4437 26.7499

0. 4437 26.7506

0. 4437 26.7508

0. 4437 26.844 1

(>stntctum /Rtefrlty Associates. Inc~

2. 046E+06 876.0000 2.047E+06 876.0000

2. 048E+06 1752.0000

2. 054E+06 5256. 0000

2. 064E+06

1. 051E+04

2. 065E+06

2. 066E+06

2. 067E+06 Blocks :

2. 068E+06

2. 068E+06 876.0000 876.0000 730.0000 96 876.0000 876.0000

2. 070E+06 1752.0000

2. 075E-1'06 5256. 0000

2. 086E+06

1. 051E+04

2. 087E+06

2. 088E+06

2. 088E+06 Blocks:

2. 089E+06 876.0000 876.0000 730.0000 97 876.0000

2. 090E+06 876. 0000

2. 092E+06 17 52. 0000

2. 097E+06 5256. 0000 2.108E+06

1. 051E+04 2. 109E+06 2. 109E+06 2. 110E+06 Blocks:

2.111E+06 2.112E+06 876.0000 876.0000 730. 0000 98 876.0000 876.0000 2.114E+06 1752.0000

2. 119E+06 5256. 0000 2.129E+06

1. 051E+04 2.130E+06

2. 131E+06 2.132E+06 Blocks:

2.133E+06 2. 134E+06 876. 0000 876.0000 730.0000 99 876.0000 876.0000 -0. 3142 14.3121 -2.4373 12. 5525 -4.3281

10. 9858

-5.0911

10. 3535

-5. 9204

9. 6664

-6.5175 9.1717 -6.8161

8. 9244

-0. 3159 14.2616 -0. 3159 14.2599 -2.4389

12. 5068

-4.3296 10.9457 -5.0926 10.3157 -5.9218

9. 6311

-6.5189 9.1383 -6.8175 8.8918 -0.3175 14. 2101 -0.3176 14.2085 -2.4404

12. 4617

-4. 3311

10. 9063

-5.0940 10.2786 - 5. 9232

9. 5964

-6. 5203

9. 1053

-6. 8188

8. 8598

-0. 3192

14. 1595

-0. 3192 14.1578 -2.4420 12.4173 -4. 3325 10.8674 -5. 0954

10. 2419

-5.9246

9. 5622

-6.5216 9.0729 -6. 8201 8.8282 -0.3208 14.1096 -0.3208 14.1080 -2. 4435 12.3736 -41. 2284 -0.1564 -30.2590 2. 7144 -20.4893 5.2711 -16.5471 6.3027 -12.2621

7. 4240

-9.1770 8.2313 -7.6344

8. 6350

-41.2305 -0. 1559 -30.2608

2. 7045

-20.4909

5. 2519

-16.5 486

6. 2797

-12.2636 7.3969 -9.1784

8. 2013

-7.6357

8. 6036

-41.2325 -0.1553 -30.2626

2. 694 7

-20.4925

5. 2330

-16.5502 6.2570 -12.2650

7. 3702

-9.1797 8.1718 -7.6371

8. 5726

-41.2345 -0.1548 -30.2644

2. 6851

-20.4941 5.2143 -16.5517 6.2348 -12.2665

7. 3440

-9.1811 8.1427 -7. 6384

8. 5420

-41.2365 -0.1542 -30.2661

2. 6757 Report No. 1600539.401RO 4 0. 9142

1. OOOE-30 14.4685 2.243E-06 27.8216

1. OOOE-30

9. 8381

8. 844E-07

16. 1611

1. OOOE-30

5. 714 7

1. 992E-07 11. 4560

1. OOOE-30

4. 0508

7. 205E-08 6.3417 l.OOOE-30 2. 2424 1.169E-08

2. 6594

1. OOOE-30

0. 9404

2. 330E-09

0. 8183

1. OOOE-30

0. 2893

1. 776E-24

0. 0000

7. 963E-05 40.9146

1. OOOE-30 14.4157

2. 217E-06

27. 8219 1. OOOE-30

9. 8023

8. 738E-07 16.1613

1. OOOE-30

5. 6938

1. 968E-07 11.4561 l.OOOE-30

4. 0361

7. 119E-08

6. 3418

1. OOOE-30

2. 2342

1. 155E-08

2. 6594

1. OOOE-30

0. 9369

2. 302E-09

0. 8183

1. OOOE-30 0.2883

1. 769E-24

0. 0000

7. 900E-05 40.9149

1. OOOE-30

14. 3638 2.190E-06

27. 8222

1. OOOE-30

9. 7669

8. 635E-07 16.1614

1. OOOE-30

5. 6733 1. 945E-07

11. 4562

1. OOOE-30

4. 0215

7. 035E-08

6. 3418

1. OOOE-30

2. 2262 1.141E-08

2. 6595

1. OOOE-30 0. 9336

2. 275E-09

0. 8183

1. OOOE-30

0. 2872

1. 762E-24

0. 0000

7. 839E-05 40. 9153

1. OOOE-30 14.3126 2.165E-06 27.8224

1. OOOE-30

9. 7321

8. 534E-07 16.1615

1. OOOE-30

5. 6531

1. 922E-07

11. 4563

1. OOOE-30

4. 0072

6. 952E-08 6.3419 l.OOOE-30

2. 2183

1. 128E-08

2. 6595

1. OOOE-30 0.9302 2.248E-09

0. 8183

1. OOOE-30

0. 2862

1. 756E-24

0. 0000

7. 77 9E-05 40.9157

1. OOOE-30 14.2622 2.140E-06 27.8226

1. OOOE-30

9. 6979

8. 435E-07 B-47

0. 6300 16.9137

0. 6300 16.9144

0. 6300 16.9148

0. 6300 16.9152

0. 6300 1 6.9153

0. 6300 16.9153

0. 6300 16.9736

0. 6300 16.9756 0. 6300 16.9763 0.6300 16.9767

0. 6300

16. 9771

0. 6300

16. 9772

0. 6300

16. 9772

0. 6300 16.9772

0. 6300

17. 0351

0. 6300 17.0370

0. 6300 17.0377

0. 6300 17.0381

0. 6300 17. 0385

0. 6300 17. 0386

0. 6300 17.0386

0. 6300 17.0960

0. 6300 17.0979

0. 6300 17.098 7

0. 6300 17.0990

0. 6300

17. 0994

0. 6300

17. 0995

0. 6300 17.0995

0. 6300

17. 1565 0. 6300 17.1583

0. 6300 17.1591

0. 4437 26.8472

0. 4437 26.8485

0. 4437

26. 8490

0. 4437 26.8496

0. 4437 26.8498

0. 4437 26.8498 0. 4437 26.8498

0. 4437 26.9424

0. 4437 26.9455

0. 4437 26.9467

0. 4437 26.9473

0. 4437 26.9479

0. 4437 26.9481

0. 4437 26.9481 0. 4437 26.9481

0. 4437

27. 0399

0. 4437

27. 0430

0. 4437

27. 0442

0. 4437 27.0447

0. 4437

27. 0453

0. 4437

27. 0455

0. 4437

27. 0455

0. 4437 27.0455

0. 4437 27.1367

0. 4437 27.1397

0. 4437 27.1409

0. 4437 27.1414

0. 4437 27.1420

0. 4437 27.1422

0. 4437 27.2326

0. 4437 27.2356 0.4437 27.2368 S) Slruc:tural lllletJrlly Associates. Inc.*

2.135E+06 1752.0000 -4. 3339 - 20.4956 16.1617 1. OOOE-30 0. 6300 0. 4437 10.8292

5. 1960

5. 6332

1. 900E-07 17.1594 27.2373

2. 141E+06 5256. 0000

-5. 0968 -16.5532 11.4564

1. OOOE-30

0. 6300 0.4437 10.2059

6. 2128

3. 9931

6. 872 E-08 17. 1598 27.2379

2. 151E+06

1. 051E+04

- 5. 9259 -12.2679 6.3419 1. OOOE-30

0. 6300 0.4437

9. 5286

7. 3181

2. 2104 1.115E-08 17.1599 27.2381 2.152E+06 876.0000

-6.5229 -9.1824

2. 659 5

1. OOOE-30

0. 6300

0. 4437 9.0410 8.1140

0. 9270

2. 222E-09 17.1599 27.23 81 2.153E+06 876.0000

-6.8214 -7.6397

0. 8183

1. OOOE-30 0.6300 0.4437

8. 7972

8. 5119

0. 2852

1. 749E-24 17.1599 27.2381 2.154E+06 730. 0000

-0.3223 0. 0000 0. 6300 0. 4437

14. 0604

7. 720E-05 1 7.2165 27.3279 Blocks:

100

2. 155E+06 876.0000

- 0. 3224 -4 1. 2384 40.9160 1. OOOE-30

0. 6300 0.4437 14.0589

- 0. 1537 14. 2 125 2.115E-06 17.2183

27. 3308

2. 155E+06 876.0000

-2 ;44 50 -30.2678 27.8229

1. OOOE-30

0. 6300 0.4437

12. 3305

2. 6664

9. 664 1

8. 339E-07 17.2190 27.3320 2.157E+06 1752.0000

-4. 3353 - 20. 4972

16. 1618 1. OOOE-30

0. 6300 0.4437 10.7915 5.1779

5. 6136 1. 878E-07 17.2194

27. 3325 2. 1 62E+06 5256. 0000

- 5. 0981 -16.5546 11.4565

1. OOOE-30

0. 6300 0.443 7 10.1704 6.191 2 3.9792

6. 793E- 08 1 7.2197 27.3330

2. 173E+06

1. 051E+04

-5. 9273 - 12. 2692

6. 3420

1. OOOE-30

0. 6300 0.4437

9. 4954

7. 2927

2. 2027 1. 102E- 08 17.2198 27.3332

2. 174E+06 876.0000

- 6.5242 -9.1838

2. 6595

1. OOOE-30

0. 6300 0. 4437

9. 0095

8. 0858

0. 9237

2. 197E-09 17.2198

27. 3332 2.175E+06 876.0000

- 6. 8227 -7.6410 0.8183

1. OOOE-30

0. 6300

0. 4437 8. 7665 8.4823 0.2842

1. 743E-24 17.2198

27. 3332 2. 175E+06 730.0000

- 0. 3239

0. 0000 0. 6300 0. 4437

14. 0120

7. 662E-05 17.2760

27. 4223 Maximum number of blocks reached. The analysis terminated.

Number of Runtime Warnings : 2

- - Runtime \\*larning: The c u rrent value of R(-1.2640) is less than the first value of R(l.OOOE-20) in the da/dn-DeltaK table. The first value of R(l.OOOE-20)

Hill be used

- - Runtime \\*larning: The current value of R(49.1815) is greater than the l ast value of R(0.9990) in the da/dn-DeltaK table. The last value of R(0.9990) >Till be used
  - End of pc-CRACK output ***

Report No. 1600539.401RO B-48 lJStntctum Integrity Associates, Inc.*

Casel (N-809).rpt pc-CRACK 4. 2 CS Versi on Control No. 4. 2. 0. 0 Beta St ructural Integrit y Associates, Inc. HWN. str uct int. corn pccrack@structint. c orn Date: 03/14/2017 09:09 Input Data read from C: \\ Users\\mfong\\ Documents\\01. Project \\05. DCPP\\1600539\\304 Crack Gro;rth\\Support Fil es _304 \\pc-CRACK\\Crack Grm; t h _ r i se t i me 360 _sec 450\\Casel (N-809). pcf Anal ysi s Title : Diablo Ca nyon Uni ts Selected : US Cus t omary Linear Dimensions - inches Stress - ksi Load - kips Temperature - deg F Time - hours Anal ysi s Type : Crack Gro;rth (LEFH) Crack Gro;rth Calculation Nethod - Cycl e/Time St epping Naximum Number of Load Blocks = 100 Bl ock Print I nterval = 1 Cr ack Hodel : 309-Semi-Elliptical Ci rcumferenti a l Crack in Cyl inder on t he I nside Su rface (Chapuliot) Cr ack Depth, a =

0. 3400 Hal f Crack Length, c =

4. 0000 Wall Thi c kness, t =

1. 4200 Insid e Radius, Ri =

5. 5800 Aspect rat io allowed to vary

!1aximum a/t = 0. 8 Crack Depth Print Increment for SIF Tabulati on = 0. 1 !1aximum Aspect Ratio (c/a) for SIF Ta bul ation = 20 Aspect Ratio I ncrement fo r SI F Tabulat ion = 1 Total Load Cases: 6 Load Case 1: Pres Type : Stress Coefficients Input by Us er Coefficient CO = Coef fici ent Cl = Coef fi cient C2 = Coe f f i c i ent C3 =

1. 8709

- 0.2827 0. 2616 - 0. 1113 Load Case 2: Thermal max Type : St ress Coefficients Input by User Coeffi c i ent CO = Coefficient Cl = Coefficient C2 = Coefficient C3 = Load Case 3: Dl'l 21.0140 -78. 0730 69.4980 - 20.2540 Type : Stress Coeffi cients I nput by User Coeffi c i ent CO = Coeffi cient Cl = Coef f i cient C2 = Coeffi c i ent C3 =

0. 1130 0. 0000 0. 0000

0. 0000 Load Case 4 : CrkFacePressure Type: Str ess Coeffici ents Input by User Coefficient CO =

Coeffi c i ent Cl = Coefficient C2 =

1. 0000 0. 0000 0. 0000 Report No. 1600539.401RO B-49

!l}Btnu:tutW llflegrlty Associates, Inc.*

Coefficient C3 = 0 0 0000 Load Case 5: Thermal min Type: Stress Coefficients Input by User Coefficient co = Coefficient Cl = Coefficient C2 = Coefficient C3 = -32o0170 62o2440 -46o5710 12 0 1530 Load Case 6:Residual 70 Type: Stress Coefficients Input by User Coefficient CO = Coefficient C1 = Coefficient C2 = Coefficient C3 = 30o3706 -227 0 2910 289 o2005 -88 0 6581 Total Load Sub-Blocks: 8 Load Sub-Block # 1 Load Sub-block Name: Thermal_Fatigue 100 Maximum Load Case Multiplier Load Case ID 2o2350 Pres 10 0000 DW 1o 0000 Thermal max

2. 2350 CrkFacePressure 1o 0000 Residual 70 Minimum Load Case Multiplier Load Case ID 2 o2350 Pres

1. 0000 DW

1. 0000 Thermal min 2 o 2350 CrkFacePressure

1. 0000 Residual 70 Grmo~th LaH: TableDADN Cycles/Time: 876 Calc o Interval: 1 Print Interval: 876 Load Sub-Block # 2 Load Sub-block Name: Thermal_Fatigue 72 Haximum Load Case Multiplier Load Case ID 2o2350 Pres 1o 0000 DW 2 o 2350 CrkFacePressure

1. 0000 Residual 70 0 o 6800 Thermal max Minimum Load Case Multiplier Load Case ID 2o2350 Pres 10 0000 DW 2 o 2350 CrkFacePressure 1o 0000 Residual 70 0 o 6800 Thermal min Grm;th LaH: TableDADN Cycles/Time: 876 Calc o Interval: 1 Print Interval : 876 Load Sub-Block # 3 Load Sub-block Name: Thermal_Fatigue 45 Maximum Load Case Multiplier Load Case ID 2 o2350 Pres 1o 0000 DW 2 o 2350 CrkFacePressure 1o 0000 Residual 70 0 o 3950 Thermal max Minimum Load Case ~lul tiplier Load Case ID Report No. 1600539.401RO B-50

!S}Stnlr:tunrllntegrlly Associates. Inc.*

2. 2350

1. 0000

2. 2350

1. 0000 0. 3950 GroHth La~r: TableOADN Cycles /Time: 17 52 Calc. Interval: 1 Print Interval: 1752 Load Sub-Block # 4 Pres OW CrkFacePressure Residual 70 Thermal min Load Sub-block Name: Thermal_Fatigue 34 Maximum Load Case Nultiplier Load Case IO

2. 2350 Pres

1. 0000 OW 2. 2350 CrkFacePressure

1. 0000 Residual 70 0.2800 Thermal max Hinirnum Load Case Nultiplier Load Case IO 2. 2350 Pres

1. 0000 DW

2. 2350 CrkFacePressure

1. 0000 Residual 70 0.2800 Thermal min GroHth La1*1: TableDADN Cycles/Time: 5256 Calc. Interval: 1 Print Interval: 5256 Load Sub-Block # 5 Load Sub-block Name: Thermal_Fatigue 22 Naximum Load Case Nul tiplier Load Case IO

2. 2350 Pres

1. 0000 ow

2. 2350 CrkFacePressure

1. 0000 Residual 70 0.1550 Thermal max t-linimwn Load Case Nultiplier Load Case IO 2. 2350 Pres

1. 0000 0\\'7

2. 2350 CrkFacePressure

1. 0000 Residual 70 0.1550 Thermal min Grol'lth Law: TableDADN Cycles/Time : 1 0512 Calc. Interval: 1 Print Interval : 10512 Load Sub-Block # 6 Load Sub-block Name: Thermal_Fatigue 9 Maximum Load Case Multi pli er Load Case IO 2. 23 5 0 Pres

1. 0000 DW 2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 0650 Thermal max Hinimum Load Case Multipli er Load Case IO 2.2350 Pres

1. 0000 0\\*7

2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 0650 Thermal min Grm*rth Law: TableOADN Cycles/Time: 876 Calc. Interval : 1 Print Interval: 876 Report No. 1600539.401RO B-51 I}

Slnlr:tum Integrity Associates. Inc.*

Load Sub-Block # 7 Load Sub-block Name: Thermal_Fatigue 4 Naxirnurn Load Case Hultiplier Load Case ID

2. 2350 Pres

l. 0000 DW

2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 02 00 Thermal max Minimum Load Case Hul tiplier Load Case ID

2. 2350 Pres

l. 0000 DW

2. 2350 CrkFacePressure

1. 0000 Residual 70

0. 02 00 Thermal min GroHth LaH:.TableDADN Cycles/Time: 876 Calc. Interval: 1 Print Interval : 876 Load Sub-Block # 8 Load Sub-block Name: SCC Maximum Load Case Multiplier Load Case ID

2. 2350 Pres

l. 0000 DW

2. 2350 CrkFacePressure

1. 0000 Residual 70 1. 0000 Thermal max Grm*rth Law: SCC Cycles/Time: 730 Calc. Interval : 1 Print Interval: 730 Haterial Library Option -

Default Hate rial: 19 Diablo Canyon : rise time 360 sec Table (da/dn-DK) No. of R ratios in the tables = 11 R Ratio =

1. OOOE-20 Delta K da/dn

1. OOOE-03 1. OOOE-30 1.1000

1. OOOE-30 1.1100

2. 250E-08 10.0000 3. 17 0E-06 20.0000

1. 510E-05

30. 0000

3. 760E-05 40.0000 7.170E-05 50. 0000 1. 190E-04

60. 0000

l. 790E-04 70.0000

2. 530E-04

80. 0000

3. 410E-04

90. 0000

4. 450E-04 100. 0000

5. 640E-04 R Ratio =

0.1000 Delta K da/dn

l. OOOE-03

1. OOOE-30 1.1000

1. OOOE-30 1.1100

2. 270E-08 10.0000 3.190E-06

20. 0000

1. 520E-05

30. 0000

3. 780E-05

40. 0000 7. 210E-05

50. 0000 l.l90E-04

60. 0000

l. 800E-04

70. 0000

2. 540E-04 Report No. 1600539.401RO B-52 S}Stmc:tutalllllegrlty Associates. Inc.*

eo. oooo

3. 430E-04

90. 0000 4.470E- 04 100. 0000

5. 670E-04 R Ratio =

0. 2000 Delta K da/dn 1. OOOE- 03

1. OOOE-30 1.1000

1. OOOE-30 1.1100

2. 280E- 08 1 0. 0000

3. 210E- 06 20.0000

1. 530E- 05 30.0000

3. SOOE-05 40.0000

7. 260E- 05 50. 0000

1. 200E- 04

60. 0000

1. 810E- 04 70.0000

2. 560E- 04 80.0000

3. 450E- 04

90. 0000 4. 500E-04 100. 0000 5. 710E- 04 R Ratio =

0. 3000 Delta K da/dn

1. OOOE- 03 1. OOOE-30 1.1000

1. OOOE-30 1.1100

2. 320E- 08

10. 0000

3. 260E- 06 20.0000

1. 550E-05

30. 0000

3. 860E-05 40.0000 7. 370E-05

50. 0000

1. 220E-04

60. 0000

1. 840E-04 70.0000

2. 600E-04 80.0000

3. SlOE-04

90. 0000 4.570E- 04 100. 0000 5. 790E- 04 R Ratio =

0. 4000 Delta K da/dn 1. OOOE-03

1. OOOE-30

1. 1000

1. OOOE-30

1. 1100 2. 390E-08

10. 0000 3. 370E- 06 20.0000

1. 600E-05

30. 0000

3. 990E-05 40.0000

7. 61 0E-05 50.0000

1. 260E-04

60. 0000

1. 900E-04

70. 0000

2. 680E- 04 80.0000

3. 620E- 04

90. 0000

4. 720E- 04 100. 0000

5. 980E- 04 R Ratio =

0. 5000 Delta K da/dn

1. OOOE-03

1. OOOE-30 1.1000 1. OOOE-30 1.1100

2. 560E-08

10. 0000

3. 600E- 06 20.0000

1. 710E-05 30. 0000 4. 270E- 05 40.0000 8.160E-05

50. 0000

1. 350E-04

60. 0000

2. 030E-04 70.0000

2. 870E-04 80.0000

3. 880E-04

90. 0000

5. 060E- 04 100. 0000

6. 410E-04 R Rati o =

0. 6000 Delta K da/dn

1. OOOE-03

1. OOOE-30 Report No. 1600539.401RO B-53 l)s~n~c~urattntegrlly Associates, Inc!'

1. 1 000

1. OOOE-30 1.1100 2. 940E- 08

10. 0000 4.140E- 06

20. 0000 1. 970E- 05

30. 0000

4. 900E- 05 40.0000 9. 360E- 05

50. 0000

1. 550E- 04

60. 0000

2. 330E-04 70.0000 3. 300E-04 80.0000

4. 450E- 04

90. 0000

5. 810E- 04 1 00. 0000 7. 360E-04 R Ratio =

0. 7000 Delta K da/d n 1. OOOE- 03 1. OOOE-30 1.1000 1. OOOE-30 1.1100

3. 790E- 08 1 0.0000

5. 330E- 06 20.0000 2. 530E- 05

30. 0000

6. 310E- 05 40.0000 1. 21 0E- 04 50.0000

1. 990E- 04 60.0000 3. OOOE- 04

70. 0000

4. 250E-04 80.0000

5. 740E-04

90. 0000

7. 480E- 04 1 00. 0000

9. 480E-04 R Ratio =

0.8000 Del ta K da/dn 1. OOOE-03 1. OOOE-30

1. 1000

1. OOOE-'30 1.1100

5. 680E- 08

10. 0000

7. 980E- 06 20. 0000

3. 800E- 05 30.0000

9. 450E- 05 40.0000

1. 810E-04

50. 0000

2. 980E- 04

60. 0000

4. 500E- 04 70.0000

6. 360E- 04

80. 0000

8. 590E- 04 90. 0000 1.120E-03 1 00. 0000

1. 420E-03 R Ratio =

0. 9000 Delta K da/ dn

1. OOOE-03

1. OOOE-30 1. 1000

1. OOOE-30 1. 1100 9.890E- 08 1 0. 0000 1. 390E-05

20. 0000

6. 61 0E- 05

30. 0000 1. 650E- 04 40.0000

3. 150E- 04

50. 0000

5. 200E- 04 60. 0000

7. 830E- 04 70.0000 1.110E- 03 80.0000 1. 500E-03

90. 0000

1. 950E-03 100. 0000

2. 4 70E-03 R Ratio =

0. 9990 Delta K da/dn

1. OOOE-03

1. OOOE-30

9. 999E+03

1. OOOE-30 No. of Data in the KI C Tabl e = 1 Crack Depth KIC

0. 0000 200. 0000 Stress Corrosion Crack Gr ot*lth Equati on Report No. 1600539.401RO B-54 S)slnlctunrlllllegrlty Associates, Jnc.*

C =

2. 420E-07 2.181 0 K Threshold =

0. 0000 Stress Corrosion Cracking (SCC) Crack GroNth LaH The Crack Gro>Ith Rate in/h (or m/h) is given by:

da/dt = C * (Kmax) 'n \\*lhere c, n = empirical constants da/ dt = 0 for Kmax < K Threshold rnessages/Narnings: Solution for Ri/t of 0. 2 a nd 0. 5 l*lill be used Number of Warnings in Inputs: 0 ANALYSIS RESULTS - STRESS INTENSITY FACTORS Load Case # 1: Pres

Crack Dimensions ----- -------

K at tips a/t c/a c/a = 11.7647 0. 3400

4. 0000

0. 2394 11.7647

2. 2330

0. 7366

0. 4400 5.1765

0. 3099 11. 7647

2. 6731

0. 8553 0.5400 6.3529

0. 3803 11.7647 3.1092 0. 9668 0.6400 7. 5294

0. 4507 11.7647

3. 6043 1.0759

0. 7400 8. 7059

0. 5211 11. 7647 4.1356

1. 1831

0. 8400 9. 8824

0. 5915 11.7647

4. 6826 1.2884 0.9400 11.0588

0. 6620 11.7647

5. 3761

1. 4035

1. 0400 12.2353

0. 7324 11.7647 6.1159

1. 5205 c/a =

12.7647

0. 34 00 4.3400 0.2394 12.7647 2. 2445 0. 7129 0. 4400

5. 6165 0. 3099 12.7647

2. 6914 0.8275

0. 5400

6. 8929 0.3803 12.7647 3. 1352 0. 9349

0. 6400 8.1694

0. 4507 12.7647

3. 6405 1.0388

o. 7400 9. 4459

0. 5211

12. 764 7

4. 1837

1. 1 402 0.8400

10. 7224

0. 5915 12.7647 4. 7436

1. 2394 0.9400 11.9988

0. 6620 12.7647

5. 4398

1. 3444 1.0400 13. 2753

0. 7324 12.7647 6. 1805

1. 4500 c/a =

13.7647 0.3400

4. 6800 0. 2394 13.7647

2. 2544

0. 6927 0.4400 6. 0565 0. 3099 13.7647

2. 7070

0. 8037

0. 5400 7.4329 0. 3803 13.7647 3.1575 0.9076

0. 6400 8. 8094 0.4507 13.7647 3. 6715

1. 0071

0. 7400 10.1859

0. 5211

13. 7647 4. 224 8 1.1035 0. 8400 11.5624

0. 5915 13.7647 4. 7957 1.1976 0.9400 12.9388

0. 6620 13.7647 5. 4942

1. 2938 1.0400 14. 3153

0. 7324 13.7647 6.2357

1. 3897 c/a =

14. 7647 0.3400

5. 0200 0. 2394 14. 7647

2. 2629

0. 67 53 0.4400

6. 4965 0. 3099 14.764 7

2. 7205 0.7831 0. 5400

7. 9729

0. 3803 14.7647 3.1767 0.8840 0.6400 9. 4494 0. 4507 14.7647

3. 6983 0. 9797 0.7400 10.9259

0. 5211 14.7647

4. 2604 1.0718 0.8400 12.4024

0. 5915 14.7647 4.8 407 1.1614 0.9400 13.8788 0. 6620 14.7647

5. 54 1 3

1. 2501 Report No. 1600539.401RO B-55 S)slnlctutalllllegrlty Associates. Inc.*

1.0400 15.3553 c/a = 15.7647 0.3400 0.4400 0.5400 0.6400

0. 7400 0.8400 0.9400 1.0400

5. 3600

6. 9365 8.5129 10.0894

11. 6659 13.2424 14.8188 16.3953 c/a =

16.7647 0.3400

0. 4400

0. 5400

0. 6400

0. 7400 0.8400

0. 94 00

1. 0400

5. 7000

7. 3765

9. 0529

10. 7294 12.4059

14. 0824 15.7588 17.4353 c/a =

17.7647 0. 3400

0. 44 00

0. 5400

0. 64 00

0. 7400

0. 84 00

0. 9400

1. 0400

6. 0400

7. 8165

9. 5929

11. 3694 13.1459

14. 9224

16. 6988 18. 4753 c/a=

18.764 7

0. 3400

0. 44 00

0. 5400

0. 64 00

0. 7400

0. 8400

0. 9400

1. 0400

6. 3800

8. 2565

10. 1329 12. 0094 13.8859 15.7624

17. 6388 19. 5153 c/a =

19.7647

0. 3400

0. 4400 0.5400 0.6400

0. 7400

0. 8400

0. 9400 1.0400 6. 7200

8. 6965

10. 6729 12.6494

14. 6259 16.6024 18.5788

20. 5553 Load Case # 2: Thermal max

0. 7 324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

o. 7324

0. 2394 0. 3099

0. 3803 0.4507

0. 5211

0. 5915

0. 6620 0. 7324 0. 2394

0. 3099

0. 3803 0.4507

0. 52 11

0. 5915

0. 6620

0. 7324

0. 2394 0.3099

0. 3803 0.4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394 0.3099 0.3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324 14.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.764 7 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647 16.7647

16. 7647 17.7647 17.7647 17.7647 17.7647

17. 7 647 17.7647 17.7647 17.7647 18.7647 18.7647 18.7647 18.764 7 18.7647 18.7647 18.7647 1 8.7647 1 9.7647 19.7647 1 9.7647 19.7647 19.7647 19.7647 19.7647 19.7647 Crack Dimensions ------------

c/a = 11.7647 0.3400 0.4400

0. 5400 0.6400

0. 7400

0. 8400

0. 9400

1. 04 00

4. 0000 5.1765

6. 3529

7. 5294

8. 7059 9.8824

11. 0588 12.2353 c/a =

12.7647

0. 3400

0. 44 00 4.3400

5. 6165 a/t c/a

0. 2394

0. 3099 0.3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099 11.7647 11.7647 11.764 7 11.7647 11.7647 11.7647 11.7647

11. 7647 12.7647 12.7647 Report No. 1600539.401RO 6.2834 2.2703

2. 7324 3.1935

3. 7216

4. 2914 4. 8800

5. 5823

6. 3251 2.2748

2. 7378

3. 2000

3. 7293 4. 3005 4.8905

5. 5969 6.3443 2.2781

2. 7412

3. 2033

3. 7324

4. 3032 4.8929

5. 6035

6. 3562

2. 2811

2. 7443

3. 2063

3. 7352

4. 3057 4.8950

5. 6094

6. 3669 2.2838

2. 7470 3.2089

3. 7377

4. 3079

4. 8969

5. 6147

6. 3765

1. 3376

0. 6600

0. 7651

0. 8634

0. 9558

1. 0441 1.1299

1. 2120

1. 292 1

0. 6267

0. 7265

0. 8198

0. 9072

0. 9908 1.0718 1.1488

1. 2238

0. 5915

0. 6856

0. 7736

0. 8562 0. 9350

1. 0115

1. 0841 1.1549

0. 5599

0. 6491

0. 7324

0. 8105

0. 8852

0. 9576

1. 0263

1. 0933 0. 5316

0. 61 62

0. 6954

0. 7695

0. 8404

0. 9091 0.9744 1.0380 K at tips

10. 5427 9.3196 7. 7110

6. 0985

4. 4077

2. 6295

0. 8437

-1.0736

10. 6143

9. 4159

7. 6160

8. 5825

9. 3948 10.1096 10.7358 11.2786 11.7745 12.1977 7. 4073 8.3584 B-56 lJ Stmctumlllllefrlly Associates. Inc.*

0.5400 0 0 6400 0 0 7400 0. 8400 0.9400

1. 0400 6.8929 8.1694 9 0 4459 10.7224

11. 9988 13.2753 c/ a =

13. 7 64 7 0. 3400 0 0 4400

0. 5400 0.6400

0. 7400 0.8400 0. 9400 1.0400 4 0 6800 6 0 0565 7 0 4329 8 0 8094 10.1859

11. 5624 12 0 9388 14 0 3153 c/a =

14.7647

0. 3400

0. 4400 0.5400 0.6400

0. 7400 0.8400 0 0 9400

1. 0400 50 0200 6 0 4 965 7 0 9729 9.4494 10.9259 12 0 4024 13.8788 15 0 3553 c/a=

15.7647

0. 3400 0.4400 0.5400 0.6400

0. 7400 0.8400 0 0 9400 1.0400 50 3600 6 0 9365 8 0 5129 10.0894

11. 6659 13 0 2424 14 0 8188 16.3953 c/a =

16.7647 0. 3400 0.4400 0.5400 0 0 6400 0.7400 0.8400 0.9400 1.0400 50 7000 7 0 3765 9 0 0529 10 0 7294 12.4059 14 0 0824 15 0 7588 17 0 4353 c/a= 17.7647 0.3400 0 0 4400 0.5400 0 0 6400 0 0 7400 0 0 8400 0 0 9400 1.0400 6 0 0400 7 0 8165 9.5929

11. 3694 13.1459 14 0 9224 16.6988 18.4753 c/a =

18.7647 0.3400 0.4400 0. 5400 0 0 6400 0 0 7400 0.8400 0.9400 1.0400 6 0 3800 8 0 2565 10.1329 12 0 0094 13.8859 15.7624 17.6388 19.5153 c/a= 19.7647 0 0 3400 6.7200 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0.3803 0.4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0.3803 0.4507

o. 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507

o. 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099

0. 3803

o. 4507

0. 5211

0. 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099

0. 3803

0. 4507

0. 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507

0. 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 12.7647 12.7647 12.7647 12.7647 12.7647 12. 7647 13 0 7647 13 0 7647 13. 7647 13.7647 13.7647 13.7647 13.7647 13.7647 14.7647 14. 7647 14.7647 14.7647 14.7647 14.7647 14.7647 14. 7647 15. 7647 15.7647 15.7647 15.7647 15.7647 15.7647 15. 7647 15.7647 16.7647 16.7647 16.7647 16. 7647 16.7647 16.7647 16.7647 16.7647 17.7647 17. 7647 17.7647 17. 7647 17. 7647 17. 7647 17.7647 17.7647 18 0 7647 18.7647 18. 7647 18 0 7647 18 0 7647 18 0 7647 18 0 7647 18.7647 1 9.7647 Report No. 1600539.401RO 7 0 8257 6.2284 4 0 5428 2 0 7579 0 0 9352

-1.0198 10 0 6755 9.4982 7 0 9237 6.3393 4 0 6583 2 0 8676

1. 0135

-0.9738 10.7284 9. 5693 8 0 0084 6.4353

4. 7582 2 0 9625

1. 0811

-0.9340 10.7746 9 0 631 4 8 0 0824 6.5190. 4 0 8454 3.0453 1.1402 -0.8993 1 0. 7979 9 0 6516 8 0 0975 6 0 5299 4 0 8525 3 0 0492 1.1387 -0 0 9098 10 0 8135 9 0 6595 8 0 0964

6. 5212 4 0 8387 3 0 0327 1.1217

-0.9312 10.8275 9 0 6665 8 0 0954 6 0 5135 4 0 8263 3.0178 1.1066 -0 0 9502 10.8401 9.1632 9 0 8660 10. 4800

11. 0139 11.4945

11. 9073 7 0 2290 8. 1669 B. 9652 9. 6577 10.2613 10.7876 11.2551

11. 6591 7 0 0748 8 0 0013 8 0 7940 9. 4776 10 0 0723 10 0 5920 11.0482 11.4445 6.9402 7 0 8568 8.6446 9.3204

9. 9072 10. 4212 10.8675 11.2571 6 0 5957 7.4684 8 0 2193 8 0 8627 9 0 4211 9 0 9105 10 0 3343 10.7048 6 0 2245 7 0 0480 7.7566 8 0 3638 8.8908

9. 3526

9. 7526 10.1022 50 8928 6.6724 7 0 3432 7.9181 8 0 4170 8 0 8542 9 0 2329 9 0 5638 5.5946 B-57

0.4400 0.5400 0.6400 0. 7400 0.8400 0.9400 1.0400

8. 6965

10. 6729 12.6494

14. 6259 i6. 6024 18.5788

20. 5553 Load Case # 3: D\\"1

0. 3099

0. 3803 0. 4507

0. 5211

0. 5915

0. 6620

0. 7324 19.7647 19.7647 19.7647 19.7647 19.7647 19.7647 19.7647

Crack Dimensions ------------

c/a = 11.7647 0.3400 0.4400 0.5400 0.6400

0. 7400

0. 8400 0.9400 1.0400

4. 0000 5.1765

6. 3529

7. 5294

8. 7 059

9. 8 824

11. 0588

12. 2353 c/a=

12.7647 0.3400 0.4400 0.5400 0.6400

0. 7400 0.8400 0.9400

1. 0400 4. 3400

5. 6165 6.8929 8.1694

9. 4459

10. 7224

11. 9988 13.2753 c/a =

13.7647 0.3400 0.4400 0.5400 0. 6400

0. 7400 0.8400 0.9400 1.0400

4. 6800

6. 0565

7. 4329 8.8094 10.1859 11.5624

12. 9388

14. 3153 c/a=

14. 7647 0.3400 0.4400 0.5400 0.6400

0. 7400 0.8400 0.9400

1. 0400

5. 0200 6.4965

7. 9729 9.4494

10. 9259

12. 4024 13.8788

15. 3553 c/a =

15.7647 0.3400

0. 4400 0.5400

o. 6400

0. 7400 0.8400 0.9400 1.0400

5. 3600

6. 9365

8. 5129 10.0894 11.6659

13. 2424

14. 8188 16.3953 c/a =

16.7647 0.3400 0.4400

0. 5400 0. 6400

0. 7400 0.8400 0.9400 5.7000

7. 3765

9. 0529

10. 7294 12.4059

14. 0 824 15.7588 a/t c/a

0. 2394

0. 3099 0. 3803

0. 4507 0. 5211 0.5915

0. 6620 0. 7324 0. 2394

0. 3099 0. 3803

0. 4507 0. 5211

0. 5915

0. 6620

0. 7324 0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324 0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915 0. 6620

0. 7324 0.2394

0. 3099 0. 3803

0. 4507

0. 5211

0. 5915

0. 6620 0. 7324 0. 2394

0. 3099

0. 3803 0.4507

0. 5211

0. 5915

0. 6620 11.7647 11.7647 11.7647 11.7647 p.7647 11.7647 11.7647 11.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 12.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13.7647 13. 7647 14.7647 14.7647 14.7647 14.7647 14.7647 14.764 7 14.7647 14.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 15.7647 16.7647 16.7647 16.7647 16. 7647 16.7647 16.7647 16.7647 Report No. 1600539.401RO 9.6728

8. 0945

6. 5065 4. 8151

3. 0045

1. 0931

- 0.9673 6.3348

6. 9717 7. 5175

7. 9911

8. 4062

8. 7657 9.0800 K at tips 0.1382 0.1662 0.1941

0. 2257

0. 2598

0. 294 9

0. 3394

0. 3871 0.1389 0.1673 0.1957 0.2280

0. 2628

0. 2987

0. 3434

0. 3912 0.1395 0.1683 0.1971 0.2299

0. 2653

0. 3020 0.3469 0.3947 0.1400 0.1691 0.1983 0.2316

0. 2676 0.3048 0.3498

0. 3977 0.1405 0.1699 0.1993

0. 2330

0. 2695

0. 3073

0. 3524 0.4003 0.1408

0. 1702 0. 1 997

0. 2335 0. 2701

0. 3079

0. 3533 0.04 46

0. 0519

0. 0587

0. 0654 0. 0720 0.07 85

0. 0857

0. 0930

0. 0432

0. 0502

0. 0568

0. 0632 0. 0694

0. 07 55 0.0820 0.0886 0.0420 0.0487

0. 0551

0. 0612

0. 0671 0. 0729

0. 0789 0. 0848 0.0409

0. 0475

0. 0537 0. 0595 0. 0652

0. 0707 0. 0762 0.0816 0.0400 0.0464

0. 0524

0. 0581

0. 0635

0. 0688

0. 0738 0.0788

0. 0380

0. 0440

0. 0497

0. 0551

0. 0602

0. 0652

0. 0700 B-58 I.Jstnu:tuta~ llllegrlty Associates. Inc.*

1o 0400 17o4353 c/a = 17 0 7647 Oo3400 Oo4400 Oo5400 0 0 6400 0 0 7400 Oo8400 Oo9400 1.0400 6 0 0400 7 0 81 65 9o5929 11 0 3694 13o1459 14 0 9224 16o6988 18o4753 c/a = 18 o 764 7 Oo3400 0 0 4400 0 0 5400 0 0 6400 Oo 7400 Oo8400 0 0 94 00

1. 0400 6 0 3800 8 0 2565 10 o1329 12 0 0094 13 0 8859 1 5o 7624 17o6388 1 9 0 5153 c/a =

1 9o7647 0 0 3400 Oo4400 0 0 5400 0 0 6400 0 0 7400 Oo8400 0 0 9400 1.0400 6o7200 8 0 6965 10 0 6729 12o6494 14 0 6259 16 0 6024 1 8 o5788 200 5553 0 0 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 Oo 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 Oo 7324 1 6 0 7647 1 7o 7647 17 o7647 1 7o 7647 1 7 0 7647 17o7647 1 7 0 764 7 1 7o 7647 1 7o 7647 1 8o7647 18o 7647 18 o7647 18o7647 1 8o7647 1 8o7647 18o 7647 1 8o7647 1 9o7647 1 9o7647 1 9o7647 1 9o7647 19 o7647 19o7647 19 o 7647 1 9 0 7647 Load Case # 4: CrkFacePressure Crack Dimens i ons -------- ---- c/a = 110 7 647 0 0 3400 Oo4400 Oo5400 0 0 6400 0 0 7400 0 0 8400 Oo9400

1. 0400 4 0 0000 5 o1765 6 0 3529 7 0 5294 8o 7059 9o8824 11.0588 12 0 2353 c/a =

12 o 764 7 0 0 3400 0 0 4400 Oo5400 Oo 6400 Oo 7400 Oo 8400 Oo 9400 1o 0400 4 0 3400 50 6165 6 0 8929 8 o1694 9 0 4459 10 0 7224 11o 9988 13 0 2753 c/a = 13o 7647 Oo 3400 0 0 44 00 0 0 5400 Oo6400 Oo 7400 Oo8400 Oo9400 1.0400 4 0 6800 6 0 0565 7 0 4329 8 0 8094 10 o1859 110 5624 12 o9388 14 0 3153 c/a = 14 o 7647 Oo3400 Oo4400 50 0200 6o4965 a/t c/a 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 Oo7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 Oo 2394 Oo3099 0 0 3803 Oo4507 Oo 5211 0 0 5915 0 0 6620 Oo7324 Oo 2394 Oo3099 11o 7647 11.7647 11 o7647

11. 7 647 11 o7647 110 7647 11.7647 11o7647 12 0 7647 12o7647 12 0 7647 12o7647 12o7647 12 o7647 12o7647 12o 7 647 1 3o7647 1 3o 7 647 1 3o7647 1 3 o7647 1 3o764 7 13 o7647 13o7647 130 7647 14o7647 14 o7647 Report No. 1600539.401RO Oo 4015 Oo1410 0 o1704 0 o1999 0 0 2337 Oo2702 0 0 3081 0 0 3537 Oo 4023 Oo 1 412 Oo1706 0 0 2001 0 0 2339 0 0 2704 0 0 3082 Oo354 1 Oo4029 Ool413 Oo1708 0 0 2003 0 0 2340 0 0 2705 0 0 3083 0 0 3544 Oo4036 Oo0746 0 0 0358 Oo 0416 Oo0469 0 0 0520 0 0 0568 0 0 0615 0 0 0660 0 0 0704 0 0 0339 0 0 0393 0 0 0444 Oo 0492 0 0 0538 0 0 0583 0 0 0625 0 0 0667 Oo 0322 Oo0374 0 0 0422 0 0 0467 0 0 0511 0 0 0553 0 0 0594 0 0 0633 K at tips

1. 2229

1. 4 708

1. 7176 1o 9977 2 0 2989 2 0 6099 3 0 0039 3 0 4258

1. 2292

1. 4808

1. 7319 2 0 0176 2 0 3254 2 0 6436 3 0 0393 3o4618 1 0 2345

1. 4894

1. 744 1 2 0 034 7 2o 348 1 2o6725 3 0 0695 3 o4925

1. 2392 1.4967 0 0 3950 Oo 4592 0 0 5197 0 0 5791 Oo6375 0 0 6951 Oo 7583 0 0 8227 0 0 3823 Oo 4442 0 0 5024 0 0 5589 0 0 6142 0 0 6684 0 0 7259 Oo 7840 Oo 3714 0 0 4313 Oo4876 0 0 5417 0 0 5942 Oo 6455 0 0 6982 Oo7509 0 0 3620 0 0 4202 B-59

Oo5400 Oo6400 0 0 7400 0 0 8400 Oo9400 1.0400 7 0 9729 9 0 4494 10 0 9259 12o4024 13 0 8788 15 0 3553 cia= 15o7647 0 0 3400 0 0 4400 0 0 5400 Oo6400 0 0 7400 Oo8400 Oo9400 1 0 0400 5 0 3600 6 0 9365 8 0 5129 1 0o0894 11o 6659 13 0 2424 14 0 8188 16o 3953 cia = 16 0 7647 Oo3400 Oo4400 Oo5400 Oo6400 0 0 7400 Oo8400 0 0 9400

1. 0400 50 7000 7 0 3765 9o0529 10 0 7294 12o4059 14 0 0824 15 0 7588 17 0 4353 cia =

170 7647 Oo3400 0 0 4400 0 0 5400 0 0 6400 0 0 7400 0 0 8400 Oo9400

1. 0400 6o0400 7o8165 9o5929 11 0 3694 13 o1459 14 0 9224 160 6988 18 o4753 cia=

18o7647 0 0 3400 Oo4400 0 0 5400 Oo 6400 0 0 7400 0 0 8400 Oo9400

1. 04 00 6o3800 8 0 2565 10o1329 12 0 0094 13 0 8859 15o7624 17o6388 19 0 5153 cia=

19o7647 Oo 3400 Oo4400 0 0 5400 0 0 6400 0 0 7400 0 0 8400 Oo9400

1. 04 00 6o7200 8 0 6965 100 6729 12o6494 14 0 6259 16 0 6024 18 0 5788 20o5553 Load Case # 5: Thermal min 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 Oo7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 Oo 5211 0 0 5915 0 0 6620 Oo7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 Oo7324 0 0 2394 Oo3099 Oo3803 0 0 4507 Oo 5211 0 0 5915 0 0 6620 0 0 7 324 Oo2394 Oo3099 Oo3803 Oo4507 Oo 52 11 Oo 5915 0 0 6620 Oo7324 0 0 2394 Oo3099 0 0 3803 0 0 4507 0 0 5211 Oo 5915 0 0 6620 0 0 7324 14 0 7647 14 0 7647 14 0 7647 14 0 7647 14 0 7647 14 0 7647 15 0 7647 15 0 7647 15 0 7647 15 0 7647 15o 7647 15o7647 15 0 764 7 15o7647 160 7647 16o 7647 16o 7647 16o7647 160 7647 16o 7647 1 6o 764 7 1 6 o 7647 17o 7647 17 0 7647 17o7647 17o7647 17 o7 647 17o7647 17o7647 17o7647 18o7647 18o7647 18o7647 18o7647 18o7647 1 8o7647 1 8o7647 18o7647 19 o7 647 19o7647 19o7647 190 7647 19o 7647 1 90 7647 1 9o 7647 190 7647

Crack Dimensi ons ------------

cia = 110 7647 Oo3400 Oo4400 Oo5400 0 0 6400 0 0 7400 Oo8400 Oo9400

1. 04 00 4 0 0000 50 1765 6 0 3529 7 0 5294 8o 7059 9 0 8824 11o 0588 12 0 2353 alt cia Oo2394 Oo3099 Oo3803 Oo4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 llo 7647 11o7647

11. 7647 11o7647 11o7647 11.7647 110 7647 11.7647 Report No. 1600539.401RO 1.7546 2 0 04 94 2 0 3677 2 0 6974 3 0 0956 3o5191

1. 2432 10 5032

1. 7638 2 0 0623 2o3849 2 0 7192 3 01184 3 0 5423

1. 2457

1. 5062

1. 7674 2 0 0665 2o3899 2 0 7250 3 01266 3 0 5531

1. 24 7 5 1o5081

1. 7692 2 0 0683 2 0 3915 2 0 7264 3 o1303 3 0 5598 1.2491 1o 5098

1. 7709 2 o 0698 2 0 3929 2 0 7276 3 o1336 3 0 5658

1. 2506 1.5113

1. 7724 2 0 0712 2o3941 2 0 7287 3 0 1366 3 0 5712 0 0 4748 0 0 5267 Oo5769 0 0 6258 0 0 6743 0 0 7223 0 0 3537 0 0 4105 Oo4636 0 0 5137 0 0 5618 0 0 6085 Oo 6534 0 0 6973 0 0 3359 0 0 3897 0 0 4402 0 0 4876 0 0 5330 0 0 5772 0 0 6192 0 0 6603 Oo3170 Oo 3678 Oo 4154 Oo 4602 0 0 5030 0 0 544 7 0 0 5844 0 0 6231 0 0 3001 Oo3482 0 0 3933 0 0 4356 0 0 4762 0 0 5157 0 0 5532 Oo 5899 Oo2849 Oo3306 Oo3734 Oo4136 0 0 4521 Oo4896 0 0 5252 0 0 5601 K at tips

-26 0 5825 -12 0 0951 -28 0 9648 -13o 8389 -30o8671 - 15o3982 -33 0 0917 -16o8576 - 35 0 3854 -18 0 2262 - 37 0 5765 -19o5069 - 40o 7151 -20 o8232 -43 0 9229 -22 0 0875 B-60 S)stnu:tutalllllegrlty Associates. Inc~

c/a = 12o7647 0 0 3400 Oo4400 0 0 5400 0 0 6400 Oo 7400 Oo8400 Oo9400

1. 0400 4o3400 50 6165 6o8929 8o1694 9o4459 10o 7224 11 0 9988 13o2753 c/a =

13o7647 Oo3400 Oo4400 0 0 5400 Oo 6400 0 0 7400 Oo8400 Oo 9400

1. 0400 4 o6800 6o 0565 7 0 4329 8o8094 10o1859 110 5624 12 0 9388 14 0 3153 c/a=

14o7647 Oo3400 Oo4400 Oo5400 0 0 6400 0 0 7400 Oo8400 0 0 9400 1.0400 50 0200 6 0 4 965 7o9729 9o4494 10 0 9259 12o4024 13 0 8788 15 0 3553 c/a = 15o 7647 Oo3400 0 0 4400 Oo5400 Oo6400 Oo 7400 Oo 8400 Oo 9400

1. 0400 50 3600 6 0 9365 8 0 5129 10 0 0894 110 6659 13 0 2424 14 0 8188 160 3953 c/a =

16o 7647 0 0 3400 Oo4400 Oo5400 0 0 6400 Oo7400 0 0 8400 Oo9400 1.0400 50 70 00 7 0 3765 9 0 0529 100 7294 12o4059 14 0 0824 15o 7588 17 0 4353 c/a= 17o7647 0 0 3400 Oo4400 Oo5400 Oo6400 Oo 7400 Oo8400 Oo9400

1. 0400 6 0 0400 7 0 8165 9o5929 11.3694 13o1459 14 0 9224 16 0 6988 18o4753 c/a =

18o 7647 Oo3400 Oo4400 Oo5400 0 0 6400 Oo7400 Oo8400 Oo9400 6o3800 8 0 2565 10 0 1329 12 0 0094 13o8859 150 7624 17 0 6388 0 0 2394 0 0 3099 0 0 3803 Oo 4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 Oo4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 Oo 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 Oo7324 0 0 2394 0 0 3099 0 0 3803 Oo 4507 0 0 5211 0 0 5915 0 0 6620 0 0 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 Oo 6620 Oo 7324 0 0 2394 0 0 3099 0 0 3803 0 0 4507 0 0 5211 0 0 5915 0 0 6620 12o7647 12o7647 1207647 12 o7647 12o7647 12o7647 12o7647 1207647 13 0 7647 13 o764 7 13 o7647 13o7647 13o7647 13 o7 647 13o7647 13o7647 -26o 7336 -29 o1903 -31.1682 -33o 4846 -35o 8740 -38 o1566 - 41.2803 -44o4571 - 260 8627 -29o3829 -31o 4255 -33 0 8204 -36 0 2916 -38 0 6524 -41.7633 -44 0 9136 14o7647 -26o9744 14o7647 -29o5495 14o7647 ° - 31.6479 14 0 7647 - 34 01108 14o7647 -36o6527 14o7647 -39o0811 14 0 7647 -42 o1810 14o7647 -45o3084 15 o7647 15o 7647 15 o 7647 15 o7647 15o 7647 15o 7647 15o7647 15o 7647 160 7647 16o 7647 16 o 7647 16o 7647 16o 7647 16o 7647 16o 7647 160 7647 17o 7647 17o 7647 17 0 764 7 17 0 764 7 17 0 7647 17 0 7647 17o7647 170 7647 180 7647 18o7647 18o7647 18o7647 18o7647 18 0 7647 18o7647 -27 0 0719 -29o6949 - 31. 8421 -34 0 3643 -36o 9679 -39o4554 - 42 0 5456 - 45o6530 -27 o1270 -29o7552 -31. 9058 - 34 0 4334 -37 0 0434 -39 0 5374 -4 2 0 6516 -4 5o 7838 -27 o1670 -29 0 7891 -31o 9312 -34o4499 - 37o0517 -39 0 5383 - 42 0 6832 - 45o8498 -27 0 2027 -29 0 8193 - 31. 9538 -34 0 4646 -37 0 0590 -39o 5392 -42 0 7114 Report No. 1600539.401RO -110 7348 -13 0 4319 -14 0 9521 -16o 3603 -17o6730 -1 8 0 8996 -20 01244 -210 2935 -110 4270 -13 0 0840 -14 0 5708 -15 0 9353 -17o2002 -18o3805 -19 0 5271 -20 0 6150 -1101608 -12 0 7832 -14o2412 -15o5678 -16o 7915 -17o9318 -19o0108 -20 o 0283 -10 o 9284 -1205206 -13o 9534 -15o2469 -16o4346 -17o5400 -18 o5599 -19 0 5160 -10 o3818 -11.8951 -13o2573 -14o4850 -15o6110 -160 6587 -17o6199 -18o5197 -9 0 7974 -11.2255 -12 0 5111 -13 0 6696 -14 0 7322 -15o7210 -16o 6281 -17o4772 -9o2753 -100 6273 -110 8443 -12o9411 -13 0 9471 -14o8832 -150 7419 B-61

1. 04 00 19. 5153 c/a =

19.7647

0. 3400 0. 4400

0. 5400

0. 6400

0. 7400 O. B400 0.9400 1.0400

6. 7200 B. 6965

10. 6729 12.6494

14. 6259

16. 6024 1B.57BB 20.5553 Load Case # 6: Residual 70 0. 7324 0. 2394 0. 3099 0. 3B03

0. 4507

o. 5211 0. 5915

0. 6620 0. 7324 1B.7647 19.7647 19.7647 19.7647 19.7647 1 9.7647 19.7647 1 9. 7647 19.7647

Crac k Dimensions ------- --- - -

c/a = 11.7647 0.3400 0.4400 0.5400

0. 6400

0. 7400 O.B400 0.9400 1.0400

4. 0000

5. 1 765

6. 3529 7. 5294 B.7059

9. BB24

11. OSBB 12.2353 c/a =

12. 7647 0. 3400

0. 4400

0. 5400 0.6400 0. 7400 O.B400 0. 9400 1. 0400 4. 3400 5. 6165 6. B929 B. 1694 9. 4459 1 0. 7224

11. 99BB 13. 2753 c/a =

13.7647 0.3400

0. 4400

0. 5400 0. 6400

0. 7400 O. B400 0.9400

1. 0400 4. 6BOO

6. 0565 7. 4329 B.B094 10. 1B59

11. 5624 12. 93BB 14. 3153 c/a=

14.7647

0. 3400

0. 4400 0. 54 00 0.6400 0.7400 O. B400 0. 9400

1. 0400

5. 02 0 0 6. 4965

7. 9729

9. 4494

10. 9259 12.4024 13.B7BB 15. 3553 c/a =

1 5.764 7

0. 3400

0. 4400 0. 5400

0. 6400 0.7400

0. B400 0. 9400 1.0400

5. 3600

6. 9365 B. 5129 1 0. OB94 11.6659 13. 2424

14. BIBB 1 6.3953 c/a =

16.7647 0. 3400 0. 4400

5. 7000 7. 3765 a/t c/a 0. 2394

0. 3099 0.3B03

0. 4507

0. 5211 0.591 5 0. 6620 0. 7324

0. 2394 0. 3099

0. 3B03

o. 4507

0. 52 11 0.591 5

0. 6620

0. 7324

0. 2394

0. 3099

0. 3B03 0. 4507 0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099

0. 3B03 0. 4507

0. 5211 0. 5915

0. 6620 0. 7324 0. 2394

0. 3099

0. 3B03 0. 4507 0. 5211

0. 5915

0. 6620

0. 7324

0. 2394

0. 3099 11.7647 11.7647 11.7647 11.7647 11.7647

11. 7647 11. 7647 11.7647 12.7647 12. 7647 12. 7647 12.7647 12.7647 12.7647 12.7647 12.7647 13.764 7 13.7647 13. 764 7 13.7647 13.7647 13. 7647 13.7647 13. 7647 14.7647 14. 7647 14.7647 14.7647 14.7647 14. 7647 14.7647 14. 7647 15.7647 15. 7647 15.7647 15. 7647 15. 7647 15.7647 15. 7647 15.7647 16. 7647 16.7647 Report No. 1600539.401RO

- 45. 90B7 - 16. 545B -27.234B -B. B060 -29. B464 -10. OB96 - 31.9742 -11.2451 - 34. 4779 - 12.2B64 - 37. 0657 -13.2414 - 39. 5399 - 14.1302 - 42.7367 - 14. 9455 -45.9616 -15. 70B 7 K at tips - 2. 0065 -B. 7549 -14.B4B7 - 19. B716 -23. 4902 - 25. 3235 -25. B3Bl -24.1401 - 1.9747 - B. 7415 - 14.B700 - 1 9. 9535 -23. 65B2 - 2 5.5922 - 26. 1467 - 24. 4566 -1.9475 -B. 7301 - 14. BBBl -20. 0236 -23. BOlB - 25. B219 - 26. 4105 - 24. 7271 -1.9239 - B. 7202 - 14. 9039 - 20. OB41 -23. 9259 - 26. 0205 -26. 63B5 - 24. 9609 -1.9034 - B. 7116 -14.9176 - 20.1370 -24.0343 - 26.1939 - 26. B376 - 25.1651 -1.9027 - B. 72B3 1 0. 064 7 10.971 4

11. 5B77

12. 01 09 12.2739 12.4025 12.3642 12.2159 9. B426 10.7673 11.4176 11. B72B 12. 16B2

12. 331 6 12.3464 12.2571 9. 652B 10. 5930 11. 2722

11. 754 7 12.0779 12. 2710

12. 3312 12. 2923

9. 4BB7 10. 4422 11. 1465

11. 6526 11. 999B 12. 2 1 B6 12.31B l 12. 3227 9. 3454 1 0. 3105

11. 036B 11.5634

11. 931 6 12.172B 12. 3067 12. 3492 B. BB95

9. B130 B-62 l)s~tuctura~ llllegrtty Associates. Inc.*

0. 5400 0.6400

0. 7400 0. 8400

0. 9400

1. 0400

9. 0529

10. 7294 12.4059 l4. 0824 15.7588 17.4353 c/a=

17.7647

0. 3400 0. 4400 0.5400

0. 6400

0. 7400

0. 8400

0. 9400

1. 0400

6. 04 00

7. 8165

9. 5929 11.3694 13.1459 l4. 9224 16.6988 18.4753 c/a=

18.7647

0. 3400

0. 4400 0.5400

0. 6400 0. 7400 0.8400

0. 9400

1. 0400 6.3800 8.2565 10. 1329

12. 0094 13. 8859 15. 7624 17.6388

19. 5153 c/a=

19.7647 0.3400

0. 4400

0. 5400

0. 6400 0. 7400

0. 8400 0.9400

1. 0400 6.7200

8. 6965 10.6729 12.6494 l4. 6259 16.6024 18.5788 20.5553

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620 0.7324

0. 2394

0. 3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620

0. 7324

0. 2394 0.3099

0. 3803

0. 4507

0. 5211

0. 5915

0. 6620 0.7324

0. 2394

0. 3099

0. 3803 0. 4507

0. 5211

0. 5915 0. 6620

0. 7324 CRACK GROWTH ANALYSIS RESULTS Total Subblock cycles

/Time Blocks: 876.0000 1752.0000 Cycles /Time 876. 0000 876.0000 3504.0000 1752.0000 8760.0000 5256.0000

1. 927E+04

1. 051E+04

2. 015E+04 876.0000 2.102E+04 876.0000 2.175E+04 730. 0000 Blocks:

2. 263E+04 876.0000

2. 351E+04 876.0000

2. 526E+04 1752.0000

3. 051E+04 5256. 0000 Kmax

12. 6795 22.5711 8. 0544

20. 6290

4. 5690 18.4605

2. 4627 17.8835

0. 8405 16.9135

0. 0566 16.0445

-0. 3322

15. 6087 7.2263 25.2397

3. 727 9 27.0217

0. 2007

24. 1314

-1.7667 21.0280 - 2. 5585 19.7688 16. 7647 16.7647 16.7647 16.7647 16.7647 16.7647 17.7647 17.7647 17.7647 17.7647 17.7647 17.7647 17.7647 17.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18.7647 18. 7647 19.7647 19. 7647 19.7647 19.7647 19.7647 19. 7647 19.7647 19.7647 Kmin -24. 6642 0. 1775 -17.2942

4. 6324

-10.1251

8. 9078

-7.9122 10.8606 -4.8887 12.9546 - 2.3458

14. 3839

-1.0715 15.0978 -32.5773 -1.2049 -24.2559

4. 3319

- 15.9769 9. 5322 - 12.6361

11. 6264 Report No. 1600539.401RO

-14.9531 -20.1863 - 24. 0904 -26.2478 -26.9070 - 25.2465 -1.9071 - 8.7503 -14.9914 -20. 2309 -24.1287 -26. 2670 -26.9378 -25. 2901 - 1.9110 -8.7699 -15.0256 - 20.2707 - 24. 1629 -26.2841 -26.9653 -25.3291 -1.9145 -8.7876 -15.0564 -20. 3065 -24.1937 -26.2995 -26.9900 -25.3642 DeltaK

10. 5106 11.0175

11. 3732 11.6081 11.7429 11.7914

8. 3891 9.2606

9. 9190 10.3973 10.7330 10.9546

11. 0819

11. 1277 7.9420

8. 7671

9. 3904

9. 8432 10.1610

10. 3708 10.4913 10.5347

7. 5402

8. 3235

8. 9153 9. 3452

9. 6469 9.8461

9. 9605 10.0017 DaDn

/DaDt 37.3437 6.146E- 05 22.3936

1. 948E-05 25. 3486 2.574E-05 15.9965 9.282E- 06 14.6941

7. 542E-06

9. 5527 3. 210E-06 10.3749 3. 444E- 06

7. 0229

1. 904E-06

5. 7291

9. 048E-07

3. 9589

8. 648E-07

2. 4025

1. 279E-07 1. 6605

2. 401E-07

0. 7392

1. OOOE-30

0. 5109

1. OOOE-30

1. 808E-05

2. 765E-04 36.3053

5. 769E-05 28.2266 3.278E-05 24.4566

2. 374E-05 19.7995 1.494E-05 14.2102

1. OOOE-30 11.4958

4. 775E-06 10.0775

1. OOOE-30 8.1424

2. 564E-06 B-63 Crack Dimensions

0. 3936

4. 0149

0. 4162 4.0226 0.4295 4.0281 0.4477

4. 0377 0.4572

4. 04 66 0.4573

4. 0468 0.4573

4. 0468

0. 4 723 4.2477 0. 5241

4. 2737

0. 5451

4. 2864

0. 5451

4. 2948

0. 5451

4. 3083 a/t c/a 0.2772 10.1996 0.2931

9. 6643 0.3024

9. 3789 0. 3153

9. 0195

0. 3220

8. 8508

0. 3221 8.8491

0. 3326

8. 9934

0. 3691

8. 1542 0. 3839

7. 8632 0. 3839 7.8786

0. 3839

7. 9033

!S)stmctum hltefrlly Associates, Ina:'

4.103E+04

1. 051E+04 4.190E+04 876.0000 4. 278E+04 876.0000

4. 351E+04 730. 0000 Blocks:

-3. 4208 18.4042 -4.0432 17.4276 - 4.3544 1 6.9395

2. 5134

27. 1432 4. 438E+04 876.0000

-2. 744E-03 28.3680

4. 526E+04 876.0000

4. 701E+04 1 7 52. 0000 5. 227E+04 5256. 0000 6. 278E+04

1. 051E+04 6. 366E+04 876.0000 6. 453E+04 876.0000

6. 526E+04 730.0000 Blocks:

- 1.9475 24.7 518 - 3.6826 21.5379 - 4.3816 20.2347 - 5.1428 1 8. 8221 - 5. 6922 17.8109 -5. 9670 17.3053 0.1659 27.8980

6. 614E+04 876.0000

-2. 1 04E- 03

27. 9501

6. 701E+04 876.0000 6.877E+04 1752.0000

7. 402E+04 5256.0000

8. 453E+04

1. 051E+04

8. 541E+04 876.0000

8. 629E+04 876.0000

8. 702E+04 730.0000 Blocks:

- 1.9635 24.3879 - 3.7151 21.2265 - 4. 4190 1 9.9392 -5.1866 18.5468 -5.7422

17. 5545

-6.0200 17.0586 0.1855 27.4300

8. 789E+04 876.0000

-1.460E-03 27.4980

8. 877E+04 876.0000

9. 052E+04 1752. 0000 9.578E+04 5256. 0000 1. 063E+05

1. 051E+04 1. 072E+05 876.0000

1. 080E+05 876. 0000

1. 088E+05 730. 0000 Blocks:

- 1.9833 24.0057 - 3.7525 20.9049 -4.4639 19.6437 -5. 2393 1 8.2787 - 5. 8000 17.3046 - 6. 0804 16.8177

0. 1596

27. 0502

1. 096E+05 876.0000

- 1. 709E- 03

27. 1 068 1.105E+05 876.0000 1.123E+05 1752.0000 1.175E+05 5256.00 00

1. 280E+05

1. 051E+04

1. 289E+05 876.0000

-2. 0013 23.67 49 -3.7856 20.6265 - 4.5035

19. 3879

- 5.2857 1 8.0465 - 5. 8509 17.0883 -9. 0015 13.8999 -6. 3835

15. 5388

-5. 0745

16. 3583

-35. 8155 -2.0211 - 26. 3121 4.1037 -17. 8399

9. 5499

-14.4221 11.7437 -10.7033 14. 1250 -8.02 41 15.8412 -6. 6845 16_.6993 -36.29 61 -1.8422 - 26.6596 4.1535 -18.0667 9.4816 -1 4.5989

11. 6238

- 10. 8251 13.9484 - 8.1067 15.6262 -6.7476 16.4652 - 36.7882 -1.6787 - 27. 0121 4.1862 -18.2964 9. 3997 -14.7792 11.4968 -10.9523 13.7728 - 8. 1959 15.4151 -6.8176 16.2363 -37.2214 -1.5336 -27. 3227

4. 2172

-18.4988

9. 3305

-14.938 1 11.3880 -11.0644

13. 6216

-8.2743 1 5.2327 Report No. 1600539.401RO

5. 5808 1. OOOE-30

4. 5043 1.107E-06

2. 3403

1. OOOE-30

1. 8889 3.122E-07

0. 7201 1. OOOE-30

0. 5812

1. OOOE-30 1. 806E-06

3. 241E- 04 35.8 128

1. OOOE-30 30.3891

3. 870E- 05 24.3646

1. OOOE-30 20.6480

1. 640E-05 14.1573

1. OOOE-30

11. 9880

5. 213E-06 10.0405

1. OOOE-30

8. 4910

2. 787E-06

5. 5605

1. OOOE-30

4. 6971 1.194E-06

2. 3318

1. OOOE-30

1. 9697

3. 389E- 07

0. 7175

l. OOOE-30 0. 6061 1. OOOE-30

4. 81 0E-09 3.440E-04 36.2940

1. OOOE-30 29.7923 3.702E-05

24. 6961 1. OOOE-30 20.2345

1. 567E-05

14. 3515 1. OOOE-30

11. 7449 4.989E-06 10.1800

1. OOOE-30

8. 3154

2. 669E-06

5. 6385

1. OOOE-30

4. 5984 1.145E- 06 2.3646 l.OOOE-30

1. 9283

3. 244E- 07 0. 7276

1. OOOE-30

0. 5933 1. OOOE-30 6.137E-09 3. 31 6E-04 36.7867 l.OOOE-30 29.1767 3. 532E-05 25.0288

1. OOOE-30 1 9. 8195

1. 497 E- 05 14.5439

1. OOOE-30

11. 5052

4. 772E-06 10. 3154

1. OOOE-30 8.1470 2.557E-06

5. 7130

1. OOOE-30

4. 5058 1.100E-06

2. 3958

1. OOOE-30 1.8895 3.110E-07

0. 7372

1. OOOE-30

0. 5814 1. OOOE-30

4. 419E- 09

3. 216E-04 37.2197 1. OOOE-30 28.6404

3. 387E- 05 25.3214 1. OOOE-30 19.4577

1. 436E-05

14. 7132

1. OOOE-30 11.2960

4. 588E-06 10.4346

1. OOOE-30 7. 9999

2. 462E-06

5. 7787

1. OOOE-30

4. 4249

1. 062E-06

2. 4233

1. OOOE-30

1. 8556

2. 996E-07 B-64

0. 5451

4. 3199

0. 5451 4. 3202

0. 5451

4. 3202 0. 5464

4. 5611

0. 5913

4. 5930

0. 5913 4.6074

0. 5913

4. 6165

0. 5913

4. 6312

0. 5913

4. 6437

0. 5913

4. 6440 0. 5913

4. 6440

0. 5913 4. 8998

0. 5949

4. 9322 0.5949 4. 9460 0.5949 4. 954 7 0.5949

4. 9688 0.5949 4.9808 0. 594 9

4. 9811

0. 594 9

. 4. 9811

0. 5949

5. 2272 0.5989 5. 2582 0.5989

5. 2714 0.5989 5.2797 0.5989 5.2932 0. 5989

5. 3048 0.5989

5. 3050 0.5989

5. 3050 0.5989 5.5433

0. 6024

5. 5730

0. 6024

5. 5856

0. 6024

5. 5936

0. 6024

5. 6066

0. 6024

5. 6178

0. 6024

5. 6180

0. 3839

7. 9247

0. 3839

7. 9252 0. 3839

7. 9252

0. 3848

8. 3477

0. 4164

7. 7679

0. 41 64

7. 7922 0. 4164 7. 8076 0. 4 164

7. 8324

0. 4164

7. 8537

0. 4164

7. 8542

0. 4164

7. 8542

0. 4164

8. 2867 0.4189

8. 2908 0.418 9

8. 3139 0.4189 8.3286 0.4 1 89

8. 3522 0. 4189

8. 3725 0.4189 8. 3730 0.4189

8. 3730 0.4189

8. 7867

0. 4217

8. 7801 0. 4217

8. 8020 0. 4217

8. 8160 0. 4217

8. 8385

0. 4217

8. 8578

0. 4217 8.8582 0.421 7 8.8582

0. 4217 9.2561

0. 4242

9. 2521 0. 4242 9.2730 0. 4242 9.2863

0. 4242

9. 3078

0. 4242

9. 3264

0. 4242

9. 3268 l)s~ruc:tum~ /Rtefrllf Associates, Inc.*

1. 298E+05

1. 305E+05 Blocks:

876.0000 730. 0000 -6.1336

16. 6094 0.1384 26.7159

1. 314E+05 876.0000

-1. 879E-03 26.7634

1. 323E+05 876.0000 1.340E+05 1752.0000

1. 393E+05 5256. 0000

1. 498E+05

1. 051E+04

1. 507E+05 876. 0000

1. 515E+05 876.0000

1. 523E+05 730. 0000 Blocks:

-2.0170 23.3845

-3.8148

20. 3822

-4. 5383 19.1633 - 5.3265 17.8427 -5.8957 16.8985 -6.1804 16.4265 0.1215 26.4183

1. 532E+05 876.0000

-3. 075E-03 26.4594

1. 540E+05 876.0000

1. 558E+05 1752. 0000

1. 610E+05 5256. 0000

1. 716E+05

1. 051E+04

1. 724E+05 876. 0000

1. 733E+05 876.0000

1. 740E+05 730.0000 Blocks:

-2. 0319 23.1273 - 3.8415 20.1660 - 4.5701 18.9644 -5.3635 17.6622 -5. 9363 16.7304 -6.2227 16.2647 0.1066

26. 1518

1. 749E+05 876.0000

-1. 406E-03 26.1857

1. 758E+05 876.0000

1. 775E+05 17 52. 0000

1. 828E+05 5256.0000

1. 933E+05

1. 051E+04

1. 942E+05 876.0000

1. 951E+05 876.0000

1. 958E+05 730.0000 Blocks:

10 -2. 0429 22. 8959 -3.8634

19. 9714

-4.5966 18.7854 -5. 3948 17.4997 -5.9709 16.5792 -6.2590 16.1191

0. 0969

25. 9094

1. 967E+05 876. 0000

-3. 649E-04

25. 9392

1. 975E+05 876.0000

1. 993E+05 17 52. 0000

2. 045E+05 5256.0000 2.151E+05

1. 051E+04 2.159E+05 876.0000 2.168E+05 876.0000 2.175E+05 730. 0000

-2. 0532 22.6874 -3.8836 19.7961 -4. 62 09

18. 6242

-5.4235 17.3533 -6. 0026 16. 4431 -6.2922 15.9880 0.0884

25. 6892

-6.8792 16. 0384 -37. 6064 -1.4034 -27. 5986

4. 2466

-18.6785 9.2711 -15.0791 11.2936 -11.1636 13.4894 -8.3436 15.0729 -6. 9336 15.8648 - 37.9526 -1.2860 - 27.8469 4.2742 -18.8404 9.2196 -15.2062 11.2108 -11.2532

13. 3727

-8.4062 14.9317 -6. 9827 15.7112 -38.2630 -1.1783 -28. 0691 4.3006 -18.9847 9.1742 -15.3190 11.1369 -11.3321 13.2682 -8.4608 14.8048 - 7.0251

15. 5731

- 38.5457 -1.0798 -28.2715

4. 3254

-19.1162 9.1340 -15.4219

11. 0709

-11.4041 13.1743 -8. 5106 14. 6906 - 7.0639 15. 4488 Report No. 1600539.401RO

0. 7456 l.OOOE-30

0. 5709

1. OOOE-30

3. 242E-09

3. 130E-04 37.6045

1. OOOE-30 28.1668 3. 263E-05 25.5816

1. OOOE-30 19.1379 1. 384E-05

14. 8638

1. OOOE-30 11.1111 4. 428E-06 10.5408

1. OOOE-30

7. 8697

2. 379E-06

5. 8372

1. OOOE-30

4. 3533

1. 029E-06

2. 4479

1. OOOE-30

1. 8256

2. 897E-07

0. 7532

1. OOOE-30

0. 5617

1. OOOE-30

2. 439E-09

3. 055E-04 37.9495

1. OOOE-30 27. 7453 3.154E-05 25.8150

1. OOOE-30 18.8531

1. 338E-05

14. 9989

1. OOOE-30 10.9463 4.288E-06 10.6361

1. OOOE-30

7. 7536

2. 306E-06 5. 8897

1. OOOE-30 4.2894 9.997E-07

2. 4 699

1. OOOE-30 1.7988 2.810E-07

0. 7600

1. OOOE-30

0. 5535 1. OOOE-30

1. 834E-09

2. 988E-04 38. 2616

1. OOOE-30 27.3640 3.057E-05 26.0262

1. OOOE-30 18.5953

1. 297E-05 15. 1212

1. OOOE-30 10. 7972 4.164E-06 10.7224

1. OOOE-30 7. 6485

2. 242E- 06 5.9373 l.OOOE-30 4. 2315

9. 737E-07 2. 4898

1. OOOE-30

1. 7745

2. 733E-07

0. 7661

1. OOOE-30

0. 5460

1. OOOE-30

1. 490E-09

2. 928E-04 38.5454

1. OOOE-30

27. 0191

2. 971E-05 26.2183

1. OOOE-30 18. 3620

1. 261E-05 15.2326

1. OOOE-30 10. 6621

4. 053E-06 10.8009

1. OOOE-30

7. 5533 2.184E-06

5. 9806

1. OOOE-3 0 4. 1790

9. 505E-07 2. 5080

1. OOOE-30 1. 7525 2. 664E-07 0. 7717

1. OOOE-30 0. 5392

1. OOOE-30

1. 219E-09

2. 874E-04 B-65

0. 6024

5. 6180

0. 6024

5. 8495 0. 6054

5. 8782

0. 6054

5. 8903

0. 6054 5. 8981

0. 6054

5. 9106

0. 6054 5. 9214 0. 6054

5. 9216

0. 6054 5.921 6 0. 6054 6.14 73

0. 6081 6.1749

0. 6081 6.1867

0. 6081 6.1942 0. 6081

6. 2063 0. 6081 6.2168

0. 6081

6. 2171 0. 6081 6.2171

0. 6081

6. 4375

0. 6105 6. 4643 0.6105 6.4757 0. 6105 6.4830

0. 6105

6. 4948

0. 6105 6. 5050

0. 6105

6. 5053

0. 6105

6. 5053

0. 6105

6. 7211

0. 6127

6. 7471 0. 6127 6.7582

0. 6127

6. 7653

0. 6127 6.7768

0. 6127

6. 7868

0. 6127

6. 7870

0. 6127 6.7870

0. 6127

6. 9986 0. 4242 9.3268

0. 4242

9. 7111

0. 4263

9. 7094 0.4263

9. 7294

0. 4263

9. 7423

0. 4263

9. 7629 0.4263

9. 7808

0. 4263

9. 7812

0. 4263

9. 7812

0. 4263 10. 1539

0. 4283 10. 1537 0. 4283 10.1730

0. 4283 10.1853

0. 4283 10.2053

0. 4283 10.2226

0. 4283

10. 2230

0. 4283 10.2230 0. 4283

10. 5854 0. 4300 10.5878 0. 4300 10. 6064 0.4300 10.6184

0. 4300

10. 6377

o. 4300 10. 6544 0.4300 10.6548 0. 4300 10.6548 0.4300

11. 0083 0.4315 11.0117 0. 4315 11.0298 0. 4315 11.0414

0. 4315

11. 0601 0.4315 11.0764

0. 4315 11.0768

0. 4315

11. 4222 I}

Stnu:tumlltlleflrlly Associates, Ina.*

Blocks: 11 2.184E+05 876.0000 -9.156E-04 25. 7162 2.193E+05 876. 0000

2. 210E+05 1752.0000

2. 263E+05 5256. 0000 2. 368E+05

1. 051E+04

2. 377E+05 876.0000

2. 386E+05 876. 0000

2. 393E+05 730.0000 Blocks:

12 -2. 0639 22.4987 - 3. 9031 19.6376 -4.6441 18.4783 -5.4506 17.2209 -6. 0324

16. 3199

-6. 3233 15.8695

0. 0797 25.4885 2. 4 02E+05 876.0000

-1. 255E-03 25.5124

2. 410E+05 876.0000

2. 428E+05 1752. 0000

2. 4 81E+05 5256. 0000

2. 586E+05

1. 051E+04

2. 594E+05 876.0000

2. 603E+05 876.0000 2. 610E+05 730.0000 Blocks:

13 -2. 0735

22. 3263

-3. 9209 19. 4927 -4. 6652

18. 3450

-5.4753

17. 0999

- 6. 0596 16.2074 - 6. 3517 15.7612

0. 0724

25. 3039

2. 619E+05 876. 0000

-3. 245E-03 25.3261

2. 628E+05 876. 0000 2. 646E+05 1752.0000

2. 698E+05 5256.0000

2. 803E+05 1. 051E+04

2. 812E+05 876.0000

2. 821E+05 876.0000 2. 828E+05 730.0000 Blocks:

14 - 2. 0839 22.1687 -3.9385 19. 3604 -4. 6859

18. 2232

-5.4991

16. 9894

-6. 0856 16.1046 -6. 3789

15. 6623 0. 0644 25.1343

2. 837E+05 876.0000

- 2. 387E-03

25. 1529

2. 846E+05 876.0000

2. 863E+05 1752.0000 2.916E+05 5256.0000

3. 021E+05

1. 051E+04

3. 030E+05 876.0000

3. 038E+05 876. 0000

3. 046E+05 730.0000 Blocks:

15 - 2. 0910 22. 0222 -3. 9527 19.2373 -4. 7030 18.llOO -5. 5194 16.8866 -6.1080

16. 0091

-6.4024 15.5704 0.0600 24.9757

3. 054E+05 876.0000

-1. 056E-03 24. 9922 -38.8058 -0.9896 -28.4580 4.3487 -19.2375

9. 0982

-15.5170 ll. Oll6 -11.4709 13.0896 -8.5570 14.5874 -7.1001

15. 3364

-39.0449 -0. 9061 -28.6294 4.3708 -19.3490 9. 0660 -15.6043 10.9578 -ll. 5321

13. 0124

-8. 5995 14.4933 -7.1332 15.2338 -39.2674 -0. 8289 -28.7892 4.3915 -19. 4532

9. 0370

-15.6861 10.9089 - 11.5897

12. 9421

-8. 6398 14.4074 -7.1648 15.1401 -39.4712 -0.7564 - 28. 9351

4. 4ll5

-19.5479

9. 01 04

-15.7601

10. 8637

-ll.6413 12.8769 -8.6753 14.3276 -7. 1923

15. 0530

-39. 6604 -0.6886 Report No. 1600539.401RO 38.8049

1. OOOE-30 26.7058 2.894E-05 26.3941

1. OOOE-30 18.1500

1. 229E-05 15.3344

1. OOOE-30

10. 5393 3. 954E-06 10. 8729

1. OOOE-30

7. 4667 2.133E-06

6. 0203

1. OOOE-30 4.1313

9. 297E-07

2. 5247

1. OOOE-30

1. 7325 2. 602E-07

0. 7768

1. OOOE-30

0. 5331

1. OOOE-30

9. 736E-10

2. 825E-04 39.0437

1. OOOE-30 26.4 185 2. 825E- 05 26.5559

1. OOOE-30

17. 9555

1. 200E-05

15. 4281

1. OOOE-30

10. 4267 3. 864E- 06

10. 9390

1. OOOE-30

7. 3872 2. 086E- 06

6. 0568

1. OOOE-30

4. 087 5

9. 1 08E-07 2.5400 l.OOOE-30

1. 7141

2. 546E-07

0. 7815

1. OOOE-30 0.5274 l.OOOE-30 7. 897E-10

2. 781E-04 39.2642

1. OOOE-30 26. 1550 2.762E-05 26.7053

1. OOOE-30 17.7772 1.173E-05 15. 5148

1. OOOE-30 10.3234 3.783E-06 ll. 0002

1. OOOE-30

7. 3143

2. 044E-06

6. 0906

1. OOOE-30

4. 04 73

8. 937E-07

2. 5541

1. OOOE-30 1. 6972

2. 4 95E-07

0. 7859

1. OOOE-30 0. 5222

1. OOOE-30 6.117E-10

2. 740E-04 39.4689

1. OOOE-30

25. 9093

2. 704E- 05 26.8440

1. OOOE-30 1 7.6108 1.149E-05

15. 5952

1. OOOE-30 10. 2270

3. 708E-06

11. 0570

1. OOOE-30 7. 2462

2. 005E- 06 6.1219

1. OOOE-30 4. 0097

8. 779E-07

2. 5673

1. OOOE-30

1. 6815

2. 448E-07

0. 7899

1. OOOE-30 0.5174 l.OOOE-30 5. 242E-10

2. 703E-04

39. 6594

1. OOOE-30

25. 6807

2. 650E-05 B-66

0.6147

7. 0240

0. 614 7 7.0348 0. 614 7 7. 0417

0. 614 7

7. 0529

0. 614 7 7. 0627

0. 6147

7. 0629

0. 614 7 7. 0629

0. 614 7

7. 2708

0. 6166 7. 2956

o. 6166

7. 3061 0. 6166 7.3129

0. 6166

7. 3239

0. 6166

7. 3335

0. 6166

7. 3337

0. 6166

7. 3337

0. 6166 7. 5382

0. 6183 7. 5624

0. 6183

7. 5727

0. 6183

7. 5793

0. 6183

7. 5901 0.6183

7. 5995 0. 6183

7. 5997

0. 6183 7. 5997

0. 6183 7. 8011

0. 6198 7.8248

0. 6198 7.8349

0. 6198 7. 8414

0. 6198 "7. 8519

0. 6198 7. 8612

0. 6198

7. 8614

0. 6198

7. 8614 0. 6198

8. 0599

o. 6212

8. 0832 0. 4329 11.4262

0. 4329 11.4437

0. 4329 ll. 4550

0. 4329 11.4733 0. 4329 11.4892

0. 4329 11.4895

0. 4329

11. 8278

0. 4342

11. 8328

0. 4342 11.8498

0. 4342 11.8608

0. 4342 11.8786

0. 4342 11.8942

0. 4342 11.8945 0. 4342 11.8945 0.4342 12.2262

0. 4354

12. 2314 0.4354 12.2480

0. 4354 12.2588

0. 4354 12.2761 0. 4354 12.2914 0.4354 12.2917

o. 4354 12.2917 0. 4354

12. 6175

0. 4365 12.6246

0. 4365 12. 6408

0. 4365

12. 6513

0. 4365

12. 6683

0. 4365

12. 6832

0. 4365

12. 6836

0. 4365

12. 6836 0. 4365

13. 0039 0.4375

13. Oll9

3. 063E+05 876.0000 3.081E+05 1752.0000 3. 133E+05 5256.0000

3. 238E+05

1. 051E+04

3. 24 7E+05 876. 0000

3. 256E+05 876.0000

3. 263E+05 730.0000 Bl ocks:

16 - 2. 0972 21.8863 -3. 9655 19.1232 -4. 7185 18.0049 -5. 5378 1 6.7913 -6.1284

15. 9205

-6.4238 15.4851

0. 0567 24.8279

3. 272E+05 87 6. 0000

-1. 820E- 03 24.8438 3.281 E+05 876. 0000 3. 298E+05 1752.0000

3. 351E+05 5256. 0000

3. 456E+05

1. 051E+04 3. 465E+05 876.0000

3. 473E+05 876.0000

3. 48 1 E+05 730.0000 Bl ocks:

17 - 2.1047

21. 7608

- 3.9789 19.0179 - 4.7344 17.9080 - 5. 5563 16.7033 - 6.1488 15. 8387 - 6.4450 15.4065

0. 0519

24. 6908

3. 489E+05 876.0000

- 6. 271E-04 24.7045

3. 4 98E+05 876.0000

3. 516E+05 17 52. 0000 3.568E+05 5256.0000

3. 673E+05

1. 051E+04

3. 682E+05 876.0000

3. 691E+05 87 6.0000

3. 698E+05 730.0000 Blocks:

18 - 2. 1101 21.6430 - 3. 9900 1 8.9190 - 4.7479 17.81 69 - 5.5723 1 6.6207 -6.1665 1 5.7620 -6.4636 15.3327 0.0495 24.561 7

3. 707E+05 876.0000

- 3. 1 92E- 04 24.5745

3. 716E+05 876. 0000

3. 7 33E+05 1 7 52. 0000 3. 786E+05 5256.0000 3. 891E+05 1. 051E+04

3. 900E+05 876.0000

3. 908E+05 876. 0000

3. 916E+05 730. 0000 Bl ocks:

19 -2.1158

21. 5331

-4.0010 1 8.8268 -4.7611 1 7.7321 -5. 5878 16.5436 -6. 1837

15. 6904

-6. 4816 1 5.2639

0. 0465 24.4408

3. 924E+05 876.0000

- 4.189E-04 24.4528

3. 933E+05 876.0000

-2. 1215

3. 951E+05 17 52. 0000 21.4302

- 4.0116 18. 7404 -29.0704

4. 4304

- 1 9.6355

8. 9860

-15.8285 10.822 1 - 11.6889 12.8 165 - 8.7080 14. 2537 - 7.2175

14. 9723

- 39. 8391 -0. 6253 -29.1986 4. 4483 -19. 71 89

8. 9638

- 15. 8938 10.7838 - 11.7347 12.7609 -8.7397 14.1855 - 7. 2422 14.8978 - 40.0046 - 0.5655 - 29. 3170

4. 4654

-19. 7 955

8. 9431

-15.9536 1 0.7480 -11. 7763

12. 7 088

-8.7682 14.1215 -7. 2642 1 4. 8279 -40. 1609 -0.5093 - 29.4289 4.481 7 -19. 8681 8.9240 -16. 0103 10.7148 -11.8159 12. 6603 -8.7954 1 4. 0619 -7.2852 14.7628 -40.3085 -0.4563 -29. 5346 4. 4972 -19. 9368 8. 9064 Report No. 1600539.401RO 26.9732

1. OOOE-30 17.4559

1. 126E- 05 15.6700

1. OOOE-30

10. 1372 3. 639E- 06 11.1100 1. OOOE-30 7.1829

1. 971E-06

6. 1 512

1. OOOE-30 3.9748 8. 634E-07 2. 5795

1. OOOE-30

1. 6668

2. 405E- 07

0. 7937 1. OOOE-30

0. 5129

1. OOOE-30

4. 635E-1 0 2. 668E-04 39. 8373 1. OOOE-30 25.4692 2. 601E-05

27. 0938

1. OOOE-30 17.3126 1.106E-05 15. 7400

1. OOOE-30 1 0.054 1

3. 576E-06 11. 15 94

1. OOOE-30

7. 1242

1. 94 1 E- 06 6.1785

1. OOOE-30

3. 9424

8. 500E- 07

2. 5910

1. OOOE-30

1. 6533

2. 365E- 07

0. 7972 l.OOOE-30

0. 5087

1. OOOE-30

3. 81 5E-10

2. 636E- 04 40. 0040 l:OOOE-30 25.2700 2. 556E- 05 27.2069 1. OOOE-30 17.1776

1. 087E-05

15. 8055

1. OOOE-30 9.9759 3.517E- 06 11.2057

1. OOOE-30 7. 0689 1. 912E-06 6.2040

1. OOOE-30 3. 9119

8. 375E-07 2.6017 l.OOOE-30

1. 6405

2. 328E- 07 0. 8005

1. OOOE-30

0. 504 8

1. OOOE-30 3. 435E-10

2. 606E- 04 40. 1606 l.OOOE-30 25.0838 2. 514E-05 27.3131

1. OOOE-30 1 7. 051 4

1. 069E- 05 1 5. 8671 1. OOOE-30 9. 9028

3. 4 62E-06 11.2493 1. OOOE-30 7. 0173 1.886E- 06 6.2281

1. OOOE-30

3. 8834

8. 259E-07 2. 6118 1. OOOE-30

1. 6285

2. 294E- 07

0. 8036 1. OOOE-30

0. 5011

1. OOOE-30 3. 005E-10 2. 578E- 04 40.3080 l.OOOE-30 24.9091 2.474E- 05 27.4 131

1. OOOE-30 16.9329

1. 053E-05

15. 9252

1. OOOE-30 9. 8341 3.411E- 06 B-67

0. 6212

8. 0930

0. 621 2 8. 0994 0. 6212 8.1098

0. 6212 8.1189

0. 62 12 8.1191

0. 6212 8.1191

0. 621 2

8. 3150

0. 6226 8.3378

0. 6226

8. 3475

0. 6226

8. 3538 0. 6226

8. 3640

0. 6226 8. 3729

0. 6226 8. 3731

0. 6226 8.3731

0. 6226

8. 5666 0. 6238 8. 5890

0. 6238 8. 5986

0. 6238

8. 604 7

o. 6238

8. 6148 0. 6238 8. 6236 0. 6238

8. 6238

0. 6238

8. 6238 0. 6238 8. 8150

0. 624 9 8. 8371

0. 624 9 8. 8464

0. 6249

8. 8525

0. 6249

8. 8624

0. 6249

8. 8711

0. 6249

8. 8713

0. 6249

8. 8713

0. 6249

9. 0605

0. 6260

9. 0821 0. 6260

9. 0914

0. 6260 9.0973 0.4375 13.0278 0.4375

13. 0381 0. 4375 13.0548 0.4375

13. 0694 0. 4375

13. 0697 0.4375

13. 3851

0. 4384 13.3928

0. 4384 13.4083

0. 4384 13.4 184

0. 4384 13.4348

0. 4384 13.4491

0. 4384 13.4495

0. 438 4 13.4495 0. 4384 13.7603

0. 4393 13. 7694

0. 4393 13.7846

0. 4393 13.7945 0. 4393 13. 8106

0. 4393 13.8247

0. 4393

13. 8251

0. 4393

13. 8251

0. 4393 1 4.131 7 0.4401 1 4.1408

0. 4401 14.1558

0. 44 01 14. 1655 0.4401 1 4. 1813 0. 4401 14.1952 0.4401 14.1955 0.4401 1 4.1955 0.4401 14.4982 0.4409 14.5075 0.4409 14.5223 0.4409

14. 5318 S}Stroctur.ri/Riegrlly Associates. Inc~

4. 003E+05 5256. 0000 4. 108E+05 1. 051E+04 4.117E+05 876. 0000 4.126E+05 876.0000 4.133E+05 730. 0000 Blocks:

20 -4.7737 17.6526 -5.6026 16.4 715 - 6. 2000

15. 6234

-6.4987

15. 1994

0. 0435

24. 3272 4.142E+05 876. 0000

-5.162E- 04

24. 3383

4. 151E+05 876.0000 4.168E+05 1752.0000 4. 221E+05 5256. 0000

4. 326E+05 1. 051E+04

4. 335E+05 876.0000

4. 344 E+05 876.0000

4. 351E+05 730.0000 Blocks:

21 - 2.1269

21. 3334

- 4.0217

18. 6592

-4.7857 17.5778 -5.61 66 16.4037 -6.2154 15.5604 -6.5149 15. 1388

0. 0408

24. 2201

4. 360E+05 876.0000

-2.560E- 04 24.2302

4. 3 68E+05 876.0000

4. 386E+05 1752. 0000 4. 438E+05 5256. 0000

4. 544 E+05

1. 051E+04

4. 552E+05 876. 0000

4. 5 61 E+05 876.0000 4. 568E+05 730.0000 Blocks :

22 -2.13 17 21.2419 -4.0309 18.5826 -4.79 67

17. 5072

- 5.6296

16. 3396

-6.2298

15. 5010

- 6.5299 15.0817 0.0386 24. 1187 4. 577E+05 876.0000 -2. 799E- 03

24. 1294 4. 586E+05 876.00 00

4. 603E+05 1752.0000 4. 656E+05 5256. 0000

4. 761E+05 1. 051E+04

4. 770E+05 876. 0000

4. 779E+05 876.0000

4. 786E+05 730.0000 Bl ocks:

23 -2. 1387

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12. 614 9

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11. 2903

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!S)slnlr:tutalllllegrtty Associates. Inc.*

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!S)Stnn:tum Integrity Associates. Inc.*

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1. 638E-05 27.7897 1. OOOE-30 14.0947 6.971E-06 16.1426

1. OOOE-30 8.1846 2.263E-06 11.4429

1. OOOE-30 5.7985 l.241E-06

6. 3345

1. OOOE-30

3. 2084

5. 435E-07

2. 6564

1. OOOE-30

1. 3454

1. 503E-07 0.8173 l.OOOE-30

0. 4140

1. OOOE-30

0. 0000

1. 712E-04 40.8692

1. OOOE-30 20.4558 1.589E-05 27.7911 1. OOOE-30 13.9031 6.760E-06 16.1434

1. OOOE-30

8. 0735 2.195E-06 11.4434

1. OOOE-30

5. 7199

1. 204E-06

6. 334 8

1. OOOE-30 3.1649 5.271E-07

2. 6565

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1. 3272

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1. OOOE-30

7. 9684 2. 131E-06 11.4440

1. OOOE-30

5. 6456 1.169E-06

6. 3351

1. OOOE-30 3.1239 5.119E-07

2. 6566

1. OOOE-30

1. 3100

1. 416E-07 0.8174 l.OOOE-30

0. 4031

1. OOOE-30

0. 0000

1. 618E-04 40.8730

1. OOOE-30 19.9360 1.499E-05 27.7937

1. OOOE-30

13. 5503

6. 380E-06 16.1449 l.OOOE-30

7. 8688

2. 071E-06 11.4445

1. OOOE-30

5. 5752 1.136E-06

6. 3353

1. OOOE-30

3. 0849

4. 976E-07

2. 6568

1. OOOE-30

1. 2937

1. 376E-07

0. 817 5

1. OOOE-30 0.3981

1. OOOE-30

0. 0000

1. 576E-04 40.8747 l.OOOE-30 19.6959

1. 459E-05 27.7948

1. OOOE-30

13. 3873

6. 208E-06 B-71

0. 6298 11.7952

0. 6298

11. 8013

0. 629 8

11. 8053

0. 6298 11.8118

0. 6298 11.8175

0. 6298

11. 8177

0. 6298 11.8177 0. 6298 11.9441

0. 6298 11.9580

0. 6298

11. 9640

0. 6298 11.9678

0. 6298 11.9741

0. 6298 11.9797

0. 6298 11.9798

0. 6298

12. 1026

0. 6298 12.1161

0. 6298 12.1219

0. 6298 12.1256

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12. 1318

0. 6298 12.1372

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0. 6298 12.2567

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0. 6298 12.2754

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0. 6298 12.4066

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0. 4435 18.7280 0.4435 18.7377 0.4435 1 8.7440

0. 4435 18.7544 0.4435 18.7635 0.4435 18.7637 0.4435 18.7637 0.4435 18.9644 0.4435 18.9866 0.4435

18. 9960

0. 4435

19. 0021 0.4435 19.0121

0. 4435

19. 0209

0. 4435 19.0211 0.4435 1 9.0211

0. 4435 19.2161

0. 4435 19.2376

0. 4435 19.2467

0. 4435 19.2527 0.4435 19.2624 0.4435 19.2710 0.4435 19.2712 0.4435 19.2712 0.4435 19.4607

0. 4435 19.4816 0.4435 19.4905

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19. 5058 0.4435 19.5141

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7. 702E+05 5256. 0000

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l. 051E+04

7. 815E+05

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l. 051E+04

8. 033E+05

8. 042E+05

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8. 242E+05

l. 051E+04 8. 250E+05 8. 259E+05

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l. 0 51E+04

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8. 2011 Report No. 1600539.401RO 16.1455

l. OOOE-30 7. 7743 2.016E-06 11. 4450

l. OOOE-30

5. 5083 l. l06E-06 6. 3356

l. OOOE-30 3. 0480

4. 843E-07 2. 6569

l. OOOE-30

l. 2782

l. 340E-07 0.8175 l.OOOE-30

0. 3933

l. OOOE-30

0. 000 0 l. 536E-04 40.8763

l. OOOE-30 19. 4675

l. 421E-05 27.7959

l. OOOE-30 13.2323 6. 04 7E-06 16.1462

l. OOOE-30

7. 6843 l. 964E-06 ll. 4454

l. OOOE-30

5. 4446

l. 077E- 06

6. 3359

l. OOOE-30

3. 0128

4. 718E-07 2. 6570

l. OOOE-30

l. 2634

l. 305E-07

0. 8175

l. OOOE-30 0. 3887

l. OOOE-30

0. 0000

l. 499E-04 40.8779 l.OOOE-30 19.24 98

l. 385E-05 27.7970

l. OOOE-30 13.0845

5. 896E-06 16. 1468

l. OOOE-3 0

7. 5986

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5. 3840

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6. 3361

l. OOOE-30

2. 9793

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l. OOOE-30 1.2494 l.273E-07 0.8176 l.OOOE-30

0. 3844

l. OOOE-30

0. 0000

l. 464E-04 40.8794

l. OOOE-30 19.0420

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27. 7980

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5. 754E-06 16.1474

l. OOOE-30 7. 5167

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l. OOOE-30

5. 3261

l. 025E-06

6. 3363

l. OOOE-30 2.9473 4.490E-07

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l. 2359

l. 242E- 07 0. 8176 l.OOOE-30

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l. OOOE-30 18. 8432

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l. OOOE-30 12.8085 5. 620E-06 16.1480

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7. 4384

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0. 6298 12.4284 0. 6298

12. 4342

0. 6298

12. 4393 0. 6298

12. 4394

0. 6298 12.4394

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12. 5527

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12. 5651 0. 6298 12.5704

0. 6298 12.5739

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0. 6298 12.5846

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12. 7124

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19. 9814 0. 4435

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0. 4435 20.4095 0. 4435 20.4181 0.4435 20.4256 0. 4435 20. 4258 0.4435 20.4258 0.4435 20.5931 0.4435 20.6114 0.4435

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20. 6327 SJstnn:turalllllefrlty Associates, Jnc.*

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3. 4003

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-12.1553 9.2911 -9.0750 10.3014 Report No. 1600539.401RO

6. 3366

1. OOOE-30

2. 9167 4. 386E-07

2. 6573

1. OOOE-30

1. 2231

1. 213E- 07 0.8176 l.OOOE-30

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27. 8008

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1. OOOE-30 12 o 0035 4 o BSSE-06 1 6 o1513

1. OOOE-30 6o9713 1.577E-06 11 o 44 90 1o OOOE-30 4o9400 8 o656E-07 6 o 3379

1. OOOE-30 2o 7339 3o 792E-07 2 o 6578 1 o OOOE-30 101465 1 o049E-07 Oo817B l.OOOE-30 0 o 3528 1 o OOOE-30 0 0 0000

1. 219E- 04 40o8904 l.OOOE-30 17 o 5122 1 o120E- 05 27 o BOSS 1 0 OOOE-30 11 o904 B 4o766E- 06 16 o1517

1. OOOE-30 6o 9139

1. 54BE-06

11. 4493

1. OOOE-30 4 o 8994 B o 497E-07 6o 3380

1. OOOE-30 2 o 7114 3 o 722E-07 2 o 6579

1. OOOE-30 1.1370

1. 030E-07 0 o 81 78

1. OOOE-30 Oo3499 l.OOOE-30 0 0 0000 1 o1 9BE-04 B-74 0 0 6298 13 0 5111 0 0 6298 13 0 6059 0 0 6298 1 3 0 6163 Oo 6298 13 0 6207 Oo 6298 13 0 6236 0 0 6298 13 0 6283 0 0 6298 13 0 6325 0 0 6298 13 0 6326 0 0 6298 13 0 6326 0 0 6298 13 0 7256 0 0 6298 13o 7358 0 0 6298 13 0 7401 0 0 6298 13 0 7429 0 0 6298 13o 7476 0 0 6298 13o 7516 0 0 6298 13 o 7517 Oo629B 13 o 7517 0 0 6298 13 0 8430 0 0 6298 13o8530 0 0 6298 13 0 8572 0 0 6298 13 0 8600 0 0 6298 13o8645 0 0 6298 13 0 8685 0 0 6298 130 8686 0 0 6298 1 3o 8686 0 0 6298 13 0 9582 0 0 6298 13o96BO 0 0 6298 1 3 0 9722 0 0 6298 13o9749 0 0 6298 13o9794 0 0 6298 13 0 9833 0 0 6298 13 0 9834 0 0 6298 13 o9834 0 0 6298 14 0 0714 Oo4435 21.4525 Oo4435

21. 6030 Oo 4435 21o 61 95 0 0 4435 21.6265 Oo4435

21. 6311 Oo4435

21. 6386 Oo 4435

21. 6452 Oo443 5 21.6454 Oo4435 21.6454 Oo4435 21.7 930 Oo4435 21.8092 Oo 4435 21.8161 Oo4435 210 8205 0 0 4435

21. 8279 0 0 4435 210 8343 0 0 4435 21o 8345 Oo4435

21. 8345 Oo4435 21.9794 Oo4435 21.9953 Oo4435 22 0 0020 Oo4435 22 0 0064 Oo4435 22o0136 Oo4435 22 0 0200 Oo 4435 22 0 0201 Oo4435 22 0 0201 0 0 4435 22 o1624 0 0 4435 22o17BO Oo 4435 22o1846 Oo4435 22 o1 BB9 Oo4435 22 o1960 Oo4435 22 0 2022 Oo4435 22 0 2024 Oo4435 22o2024 Oo4435 22 0 3421 l)s~n~ctunrlllllegrlly Associales, Inc!'

Blocks :

1. 045E+06 lo 046E+06 49 876o0000 876o 0000

1. 048E+06 1752o 0000

1. 053E+06 5256o 0000 lo 063E+06 lo 051E+04 l o 064E+06 876o 0000 l o 065E+06 876o 0000

1. 066E+06 7 30o 0000 Blocks:

50 lo 067E+06 876 0 0000 lo 068E+06 876o0000 lo 069E+06 1752 o 0000

1. 075E+06 5256o 0000 lo 085E+06 lo 051E+04

1. 086E+06 876o 0000 lo 087E+06 876o 0000 lo 088E+06 730 0 0000 Blocks:

51

1. 089E+06 876o 0000

1. 091E+06 1752 o 0000 l o 096E+06 5256 o 0000 l ol07E+06 l o 051E+04 lol08E+06 l ol09E+06 1.109E+06 Blocks:

lo110E+06 lo111E+06 876o 0000 876 o 0000 730o0000 52 876o0000 876o0000 1.113E+06 1752 o 0000 lo118E+06 5256 o 0000 1.129E+06

1. 051E+04 lol30E+06 876 0 0000 lol30E+06 876 0 0000 1.131E+06 730o 0000 Blocks:

53 lo 132E+06 876o 0000 -Oo2138 17 ol844 -2 0 3436 15 0 0681 -4 0 2405 13 0 1852 -5 0 0060 12 0 4227 -So 8380

11. 5952

-6 0 4370

11. 001 8

- 6o7364 l0o7051 -0o2178 17 0 0615 -0 0 2181 17 0 0499 - 2 03477 14 0 9503 - 4 02443 1 3 0 0822 - 50 0097 12 0 3257 -50 84 1 6 11 o5048 -6 o4405 10 0 9160 -6 o 7399 lOo 6216 -0 0 2220 l6 o 9309 -0 0 2223 16 0 9198 -2 0 3516 14 0 8362 -4 0 2480 12 0 9824 - 50 0133 12 0 231 9 - 50 8451 11.4172 -6o4439 l0 o8329 -60 7433 l0o5408 -0 0 2260 l6o8045 - 0 0 2264 l6o7937 -2 0 3554 14 0 7258 -4 0 2515 l2o8858 -50 0168 l 2ol409 -5 0 8485 11o 3324 -6o4472 10 0 7525 -60 7466 10 0 4626 -0 0 2300 l 6o6820 -0 0 2303 l6o6715 -41.1052 -Ool873 -30ol498 3o2588 - 20 0 3926 6o 3267 -l6o 4556 7 0 5625 -l2o1762 8 0 9055 -9 0 0949 9 0 8738 -7 0 5543 l0 o3581 -41.1105 -0 ol BSB -30 ol545 3 0 2333 - 20 0 3968 6 o2772 -l6o4596 7 0 5034 -l2ol799 8 0 8360 -9 0 0985 9o 7968 -7 0 5578 l0o2773 -41.1156 -0ol844 -30 ol 591 3o2086 - 20o4009 6 0 2294 -160 4634 7o4463 -12 ol836 8o7688 -9 ol 020 9 0 7223 -7 0 5612 10 ol991 - 41.1206 -0 ol830 -30 ol635 3 ol 847 - 20o4048 6 ol830 -l6 o4672 7 0 3909 -12 ol871 8 0 7036 -9 ol053 9 0 6501 -7o5645 10 0 1234 - 41.1254 -Ool817 Report No. 1600539.401RO 40o 8914

1. OOOE-30 l7o3717 lo099E-05 27 o 8062

1. OOOE-30 11.8093 4 o 680E-06 l6ol521

1. OOOE-30 6 o 8585

1. 521E- 06 11.4496

1. OOOE-30 4 o 8602 8 o 345E-07 6 o 3382

1. OOOE-30 2 o6897 3 o656E-07 2 o 6580 l o OOOE-30 1.1280

1. 011E-07 0 o 8178

1. OOOE-30 0 o 34 71

1. OOOE-30 0 0 0000

1. 177E-04 40o 8924

1. OOOE-30 17 o 2357

1. OBOE-OS 27 o 8068

1. OOOE-30 11o 7170 4o598E-06 l 6 ol525

1. OOOE-30 6o8049 1.494E-06 11.4499

1. OOOE-30 4 o 8223 8 ol99E-07 6 o 3383

1. OOOE-30 2 o 6688 3 o 592E-07 2 o 6580 l o OOOE-30 1.1192 9 o 934E-08 0 o 8179 l o OOOE-30 0 o 3444

1. OOOE-30 0 0 0000 lo l SBE-04 40o 8933

1. OOOE-30 17 ol04 1

1. 062E-05 27 o 8075

1. OOOE-30 11.6276 4 o 520E- 06 l6 ol529

1. OOOE-30 6o 7530 1.468E-06 llo 4502 lo OOOE-30 4o 7856 8o059E-07 6 o 3385

1. OOOE-30 2 o 6485 3 o 531E- 07 2 o 658 1

1. OOOE-30 1.1106 9o 765E- 08 0 0 8179

1. OOOE-30 0 o 3417

1. OOOE-30 0 0 0000 lo l 39E-04 40o8943 l.OOOE-30 l6o9767 lo044E-05 27 o 8081

1. OOOE-30 llo 5410 4 o 444E-06 16 ol533 lo OOOE-30 6o 7028

1. 444E-06 11o 4504 lo OOOE-30 4 o 7500 7 o 925E- 07 6o 3386

1. OOOE-30 2 o 6288 3 o 4 72E- 07 2 o 6581 lo OOOE-30 1.1024 3 o 322E-25 0 o 8179

1. OOOE-30 0 o 3392 lo OOOE-30 0 0 0000 1.121E-04 40o 8951

1. OOOE-30 l6o 8532

1. 027E-05 B-75 0 0 6298 14 0 0811 0 0 6298 14 0 0852 0 0 6298 14 o0878 0 0 6298 14 0 0922 0 0 6298 14 0 0961 0 0 6298 14 0 0961 0 0 6298 l4o0961 Oo 6298 l4ol826 0 0 6298 l4ol92 1 0 0 6298 14 ol961 0 0 6298 l4ol988 0 0 6298 14 0 2031 0 0 6298 14 0 2069 0 0 6298 14 0 2069 0 0 6298 14 0 2069 0 0 6298 14 0 2920 0 0 6298 14 0 301 3 0 0 6298 1 4 0 3053 0 0 6298 14 0 3078 0 0 6298 14 0 3121 0 0 6298 14 0 3158 0 0 6298 14 0 3159 0 0 6298 14 0 3159 Oo 6298 l4o3995 0 0 6298 l4o4087 0 0 6298 14 o4126 0 0 6298 14 0 4151 Oo 6298 14 0 4193 Oo 6298 l4o4229 0 0 6298 14 0 4229 Oo 6298 14 0 4229 Oo 6298 14 0 5053 Oo 6298 14 0 5143 Oo 4435 2203574 0 0 4435 22 0 3639 Oo4435 22 0 3682 Oo4435 22 0 3751 Oo4435 22 0 3812 0 0 4435 22 0 3814 0 0 4435 22 0 3814 0 0 4435 22o5187 0 0 4435 22 0 5338 Oo4435 22 0 5402 0 0 4435 22 0 5443 Oo4435 22 0 5512 Oo4435 22 0 5571 Oo4435 22 0 5573 Oo4435 22 0 5573 Oo4435 22 0 6923 0 0 4435 22 0 7071 0 0 4435 22 0 7134 Oo 4435 220 7175 0 0 4435 22 0 7242 0 0 4435 22 0 7301 Oo 4435 22 0 7302 0 0 4435 22 0 7302 0 0 4435 22 0 8631 0 0 4435 22 o8776 Oo 4435 22 0 8838 Oo4435 22o8878 Oo4435 22 0 8944 0 0 4435 22 0 9002 Oo 4435 22 0 9002 Oo4435 22 0 9002 Oo4435 23 0 0309 0 0 4435 23 0 0452 l}Stnlr:tutwl Integrity Associates. Inc.*

1. 133E+06 876.0000 1.135E+06 1752.0000 1. 14 0E+06 5256. 0000 1.150E+06

1. 051E+04 1.151E+06

1. 152E+06

1. 153E+06 Blocks:

1.154E+06 1.155E+06 876.0000 876.0000 730.0000 54 876.0000 876.0000 1.156E+06 1752.0000 1.162E+06 5256. 0000 1.172E+06

1. 051E+04 1.173E+06 1.174E+06 1.175E+06 Blocks:

1.176E+06 1.176E+06 876. 0000 876. 0000 730.0000 55 876. 0000 876.0000 1.178E+06 1752.0000 1.183E+06 5256.0000 1. 194E+06 1. 051E+04 1.195E+06 1.196E+06 1.196E+06 Blocks:

1. 197E+06 1.198E+06 876. 0000 876. 0000 730. 0000 56 876.0000 876.0000

1. 200E+06 1752.0000

1. 205E+06 5256. 0000

1. 216E+06

1. 051E+04

1. 217E+06

1. 217E+06 1. 218E+06 Blocks:

1. 219E+06

1. 220E+06 876.0000 876. 0000 730.0000 57 876.0000 876.0000

1. 222E+06 17 52. 0000

- 2. 3591

14. 6187

-4.2550 12.7922 -5. 0201

12. 0528

-5.8517 11.2503 - 6.4504 10. 6746 -6.7498 10.3867 -0. 2338 16. 5632 -0. 2341 16.5530 -2.3627 14.5149 -4. 2584 12. 7014 -5. 0234 11.9673 -5.8549 11.1705 - 6.4535

10. 5989

- 6.7528

10. 3131

-0.2375 16.4478 -0.2378 16.4380 -2.3661 14.4141 -4.2616 12. 6133 - 5.0266 11.8843 -5. 8580 11. 0931 -6.4565

10. 5255

-6.7558

10. 2416

-0.2411

16. 3358

-0.2414 16.3262 -2. 3695 14.3162 -4.2648 12.5276 -5.0297

11. 8037

-5. 8610 11.0179 -6.4595 10.4541 - 6. 7587 10. 1722 -0.2446 16. 2268 -0. 2449 16.2175 -2.3728 14. 2210

_4. 2679 12. 4443

-30.1678 3. 1616 -20. 4086 6. 1381 -16.4708

7. 3373

-12. 1905

8. 6405

-9.1086 9.5802 -7.5677

10. 0500

-41.1301 -0.1804 -30.1720 3.1391 -20.4123 6.0945 -16.4743 7.2853 -12.1938

8. 5793

-9.1118 9. 5123 -7. 5708 9.9787 -41.1347 -0.1791 -30.17 60 3.1173 -20.4159

6. 0522

-16.4777 7.2348 -12.1970

8. 5198

-9.1149 9. 4463 -7. 5738

9. 9096

-41.1391 -0.1779 -30.1799

3. 0962

-20. 4194

6. 0111

-16. 4810 7.1857 -12. 2002

8. 4621

-9.1178

9. 3823

-7.5767 9. 8424 -41.1433 -0.1767 -30.1837 3.0756 -20. 4228 5. 9712

Report No. 1600539.401RO 27. 8087

1. OOOE-30 11.4571

4. 372E-06 16.1536

1. OOOE-30

6. 654 1

1. 420E-06 11.4507

1. OOOE-30 4. 7155

7. 796E-07

6. 3388

1. OOOE-30

2. 6097

3. 415E-07 2. 6582

1. OOOE-30

1. 0944

1. OOOE-30 0.8179 l.OOOE-30 0. 3367

1. OOOE-30

0. 0000 1.103E-04 40.8960

1. OOOE-30 16.7334

1. 011E-05 27.8093

1. OOOE-30 11.3758 4.302E-06 16.1539

1. OOOE-30 6. 6069

1. 398E-06 11.4509

1. OOOE-30

4. 6821

7. 672E-07 6.3389 l.OOOE-30 2. 5912

3. 361E-07

2. 6582 1. OOOE-30 1. 0866

1. OOOE-30

0. 8179

1. OOOE-30

0. 3344

1. OOOE-30

0. 0000

1. 087E-04 4 0.8968

1. OOOE-30 16.6171 9.948E-06

27. 8099

1. OOOE-30

11. 2968

4. 235E-06 16.1543 l.OOOE-30 6. 5610

l. 376E-06 11.4511

1. OOOE-30

4. 6496

7. 553E-07

6. 3390

1. OOOE-30 2. 5733 3. 309E-07

2. 6583

1. OOOE-30

1. 0791

1. OOOE-30

0. 8179

l. OOOE-30

0. 3320

1. OOOE-30

0. 0000

l. 071E-04 40. 8977 l.OOOE-30 16. 5041 9. 797E-06 27.8104

1. OOOE-30 11. 2200 4. 171E-06 16.1546

1. OOOE-30 6.5165 1.355E-06 11.4514

l. OOOE-30 4.6180 7.438E-07

6. 3392

1. OOOE-30

2. 5558 3. 259E-07

2. 6584

1. OOOE-30

l. 0718

1. OOOE-30

0. 8180

1. OOOE-30

0. 3298

1. OOOE-30 0. 0000

1. 055E-04

40. 8984

1. OOOE-30 16.3943 9. 650E-06

. 27.8110

1. OOOE-30 11.1454 4. 108E-06 16.154 9

1. OOOE-30

6. 4732

1. 335E-06 B-76

0. 6298 14. 5181 0. 6298 14.5206

0. 6298 14.5247

0. 6298 14. 5283

0. 62 98

14. 5283

0. 6298

14. 5283 0. 6298

14. 6093

0. 6298 14. 6182

0. 6298

14. 6219

0. 6298 14. 6244

0. 6298 14.6284

0. 6298

14. 6320 0. 6298 14.6320

0. 6298 14.6320

0. 6298 14.7118

0. 6298 14.7205 0. 6298 14. 7242

0. 6298 14. 7266 0. 6298 14. 7306

0. 6298 14.7341

0. 6298 14. 7341 0. 6298

14. 8127

0. 6298 14.8213 0. 6298 14.8249

0. 6298 14. 8273 0. 6298

14. 8312 0. 6298 14.8346 0. 6298 14.8346 0. 6298 14.8346

0. 6298 14. 9121

0. 6298

14. 9206

0. 6298

14. 9242

0. 6298

14. 92 65 0. 4435 23. 0513 0. 4435 23. 0553

0. 4435 23. 0618 0. 4435 23. 0675

0. 4435 23.0675

0. 4435 23.1962 0. 4435 23.2102 0. 4435 23.2162 0.4435 23. 2201 0. 4435

23. 2265 0. 4435

23. 2321 0.4435 23.2321 0.4435 23. 2321 0.4435

23. 3588 0.4435 23. 3727 0.4435 23. 3786 0.4435

23. 3824 0.4435 23. 3887 0. 4435

23. 3942 0. 4435 23. 3942 0.4435 23. 3942 0.4435

23. 5190 0.4435

23. 5327

0. 4435

23. 5385

0. 4435

23. 5423 0. 4435 23. 5485 0. 4435 23. 5539

0. 4435 23.5539 0.4435 23.5539 0. 4435 23. 6769 0.4435 23. 6903

0. 4435 23. 6961

0. 4435

23. 6998 S)stnn:tutalllllefrlly Assor:iales.Jnc.*

1. 227E+06 5256. 0000

1. 237E+06 1. 051E+04 1.238E+06 876.0000

1. 239E+06 876. 0000

1. 240E+06 730.0000 Bl ocks:

58

1. 241E+06 876. 0000

1. 242E+06 876.0000

1. 243E+06 1752. 0000 1. 249E+06 5256.0000

1. 259E+06 1. 051E+04 1.260E+06 876.0000 1.261E+06 876.0000 1.262E+06 730.0000 Blocks :

59 1.263E+06 876. 0000

1. 263E+06 876. 0000

1. 265E+06 1752.0000

1. 270E+06 5256. 0000

1. 281E+06

1. 051E+04 1.282E+06 876.0000

1. 283E+06 876.0000

1. 283E+06 730. 0000 Blocks:

60

1. 284E+06 876.0000 1. 285E+06 876. 0000

1. 287E+06 1752.0000

1. 292E+06 5256. 0000

1. 303E+06

1. 051E+04

1. 304E+06 876.0000

1. 305E+06 876.0000

1. 305E+06 730. 0000 Blocks:

61

1. 306E+06 876. 0000

1. 307E+06 876. 0000

1. 309E+06 17 52. 0000

1. 314E+06 5256. 0000

1. 325E+06

1. 051E+04

-5. 0327 11.7253 -5.8639 10.9448 -6.4623 10.3847 -6.7615 10.1047 -0.2480 16.1209 -0.2483 1 6.111 9 -2.3760 14.1284 -4.2709

12. 3634

- 5. 0356 11.6491 -5.8667

10. 8737

-6.4651 10.3173 -6.7643

10. 0390

-0.2513 16.017 8 -16.4842

7. 1380

- 12.2032 8. 4059 -9.1207

9. 3201

-7.5795

9. 7771

-41.1475 -0.1756 -30.1875 3. 0556 -20. 4261

5. 9323

-16.4874

7. 0915

-12. 2061 8. 3513 -9.1236

9. 2595

-7. 5823

9. 7136

-0.2516 -41.1516 16.0090 - 0.1745 -2.3791 -30. 1911 1 4. 0383.

3. 0361

- 4.2738 -20.4293 1 2. 2845

5. 894 5

- 5.0384 -16.4904 11.5749 7.0464 - 5.8695 -12.2090 10.8045

8. 2982

-6.4678 - 9.1263 10.2516 9. 2006 -6.7 670 -7.5850 9.9751 -0.2546 15.9175

9. 6517

-0.2548 -41.1555 15.9089 -0.1734 -2.382 1 -30.1946 13.9505 3.0171 -4. 2766 - 20.4324 12.2078 5. 8577 -5.0412 - 16.4934 11.5026 7. 0024 - 5.8722 - 12.2118 10.7371 8. 2464 - 6.4704 -9.1290 10.1876 9.1432 -6.7696 -7.5876 9.9129. 9.5915 -0.2577

15. 8197

-0.2580 15.8113 -2. 3850 13.8650 -4.2794 12. 1330 -5.0439

11. 4322

-5.8748

10. 6714

-41.1594 -0.1723 -30. 1980 2.9986 -20.4355

5. 8218

-16.4963

6. 9595

-12.2145

8. 1960 Repoti No. 1600539.401RO 11.451 6

1. OOOE-30

4. 5874

7. 327E-07

6. 3393

1. OOOE-30

2. 5389 3. 210E-07

2. 6584 1. OOOE-30

1. 0647

1. OOOE-30

0. 8180

1. OOOE-30

0. 3276 1. OOOE-30 0. 0000

1. 040E- 04 40.8992

1. OOOE-30 16.2874

9. 509E-06

27. 8115

1. OOOE-30 11.0728 4. 048E-06 1 6.1552

1. OOOE-30 6.431 0 1.31 6E- 06

11. 4518

1. OOOE-30

4. 5576

7. 220E- 07 6. 3394

1. OOOE-30

2. 5224 3. 1 64E- 07 2. 6585

1. OOOE-30

1. 0578 1. OOOE-30

0. 8180

1. OOOE-30

0. 3255 1. OOOE-30 0. 0000 1. 026E- 04 40.9000

1. OOOE-30 16.1835 9.373E- 06

27. 8120 1. OOOE-30 11. 0022 3. 990E-06 16.1555

1. OOOE-30

6. 3900

1. 297E- 06 11.4520

1. OOOE-30

4. 5285 7.117E- 07

6. 3395

1. OOOE-30

2. 5063 3. 118E-07

2. 6585

1. OOOE-30

1. 0510

1. OOOE-30

0. 8180

1. OOOE-30

0. 3234

1. OOOE-30

0. 0000

1. 012E-04 40.9007

1. OOOE-30 16.0822 9. 242E-06

27. 8125

1. OOOE-30

10. 9334

3. 935E- 06 16.1558

1. OOOE-30

6. 3501

1. 279E-06 11.4522

1. OOOE-30 4. 5003

7. 018E-07

6. 3396

1. OOOE-30

2. 4 907

3. 07 5E- 07

2. 6586

1. OOOE-30

1. 0445 1. OOOE-30 0. 8180

1. OOOE-30

0. 3214 1. OOOE-30

0. 0000

9. 983E- 05 40.9014

1. OOOE-30 15.9836 9.115E-06 27.8 130

1. OOOE-30 10. 8664 3.880E-06

16. 1561

1. OOOE-30 6. 3112 1.261E-06 11.4524

1. OOOE-30 4.4727 6.921E- 07

6. 3397

1. OOOE-30

2. 4754

3. 033E-07 B-77

0. 6298 14. 9303

0. 6298

14. 9337 0. 6298

14. 9337 0. 6298 14. 9337 0. 6298

15. 0101

0. 6298 15-. 0184

0. 6298 15.0220

0. 6298 15.0243 0. 6298 15. 0281 0. 6298 15. 0314

0. 6298

15. 0314

0. 6298 15. 0314

0. 6298

15. 1067

0. 6298 15.1149

0. 6298 15.11 84

0. 6298 15.1207

0. 6298 15.1244

0. 6298 15.1277

0. 6298

15. 1277

0. 6298 15.2019 0. 6298 15.2100

0. 6298 15.2135

0. 6298 15.2157

0. 6298 15. 2194

0. 6298 1 5.2227

0. 6298 15.2227

0. 6298 15.2959

0. 6298 15. 3039

0. 6298 15.3073

0. 6298

15. 3095

0. 6298

15. 3131

0. 6298 15.3163

0. 4435 23. 7059

0. 4435

23. 7112 0. 4435 23.7112

0. 4435 23.7112

0. 4435 23. 8325

0. 4435 23.8457 0.4435 23. 8514

0. 4435

23. 8550 0.4435

23. 8610 0.4435 23.8663

0. 4435 23.8663

0. 4435 23. 8663

0. 4435

23. 9859

0. 4435 23.9989

0. 4435

24. 0045

0. 4435 24.0081

0. 4435 24.0140 0.4435

24. 0192 0. 4435

24. 0192

0. 4435 24.0192

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24. 3044

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0. 4435 24.3188 l}slnlctwv~ hllegrtty Associates, Jnc.*

1. 325E+06

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5. 7 527

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5. 6869

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8. 0064

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8. 8770

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2. 6586

1. OOOE-30 1. 0381 1. OOOE-30 0. 81 80

1. OOOE-30

0. 31 94

1. OOOE-30

0. 0000

9. 852E-05 40.902 1

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10. 8011

3. 828E-06

16. 1563

1. OOOE-30 6.2733

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1. OOOE-30 4.4459 6.828E-07

6. 3398

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2. 4 606

2. 992E- 07

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1. OOOE-30

4. 3941 6. 651E-07

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1. 0141

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0. 3120

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15. 3965

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15. 5000

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15. 5000

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!S) SlnlcturaiiRtegrlty Associates. Inc.*

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11. 4554

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!l} Slnll:tutalllllegrlty Associates, Inc~

1. 783E+06

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8. 4227 Report No. 1600539.401RO

0. 8183

1. OOOE-30

0. 2870

1. OOOE-30

0. 0000

7. 825E- 05 40.9135 1. OOOE-30 14.2966

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9. 7202

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4. 0014 5.387E- 07 6. 3416

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27. 8221

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- 20. 4964

5. 06 15

- 1 6.5560 6.0750 -12.2708 7. 1549 -9.1855 7.9329 - 7.6428

6. 3220

- 41.2409 -0.1498 -30.2705 2. 6069 - 20. 5000

5. 0616

- 16.5576

6. 0513

- 12.2723 7.1269 -9. 1 869

7. 9020

-7.6442 8.2895 -41.2430 -0.1492 Report No. 1600539.401RO 40.9152

1. OOOE-30

14. 0611 6. 630E-06

27. 8224 1. OOOE-30

9. 5601

2. 908E-06

16. 1 615

1. OOOE-30 5.5528 9. 454E-07

11. 4563

1. OOOE-30 3.9355

5. 190E-07

6. 3419

1. OOOE-30 2.17 83

2. 275E-07

2. 6595

1. OOOE-30

0. 9135 1. OOOE-30 0. 8163

1. OOOE-30 0. 2611 1. OOOE-30

0. 0000

7. 480E-05 40.9156

1. OOOE-3 0 14.0047

6. 768E- 06 27.8226

1. OOOE-30 9.5216 2.8 62E- 06 1 6. 1617 1. OOOE-30

5. 5305 9. 369E- 07

11. 4564

1. OOOE-30

3. 9198 5.143E- 07

6. 3419

1. OOOE-30 2.1696

2. 254E-07

2. 6595 1. OOOE-30

0. 9098 1. OOOE-30

0. 8183 1. OOOE-30

0. 2799

1. OOOE-30 0. 0000

7. 415E-05 40.9160

1. OOOE-30 13.9492 6.708E- 06

27. 8229

1. OOOE-30 9.4841 2. 856E-06 16.1618

1. OOOE-30 5.5066 9.285E-07 11.4565

1. OOOE-30

3. 9043

5. 097E-07

6. 3420

1. OOOE-30

2. 161 0

2. 234E-07

2. 6595

1. OOOE-30

0. 9062

1. OOOE-30

0. 6183

1. OOOE-30 0.2788 l.OOOE-30

0. 0000

7. 352E-05 40.9164

1. OOOE-30 13.6947 6.649E- 06 27. 8232 1. OOOE-30

9. 44 71

2. 831 E- 06

16. 1620 1. OOOE-30 5. 4671

9. 204E-07 11.4566

1. OOOE-30 3. 8690

5. 053E-07

6. 3421

1. OOOE-30 2. 1526 2.2 15E-07

2. 6596

1. OOOE-30 0. 9027

1. OOOE-30

0. 8183

1. OOOE-30 0.2778

1. OOOE-30

0. 0000

7. 290E- 05 40.9168

1. OOOE-30 13.6410

6. 591E-06 B-84

0. 6296 17.3964

0. 6296 17.3969

0. 6298 17.4006

0. 6298 17.4033

0. 6298 17.4057

0. 629 6 17.4057

0. 629 8 17.4605

0. 6298 17.4664

0. 6298 17.4689 0. 629 8 17.4706

0. 6298

17. 4733

0. 6298 1 7.4756

0. 6296 17.4756

0. 6298 1 7. 5300

0. 6298

17. 5356 0. 6296 17.5383

0. 6296 17.5400

0. 6296 17.5426

0. 6298 17.5450

0. 6296 17.5450

0. 6298 17.5450

0. 6298 17.5966

0. 6298 1 7. 604 7

0. 6298 17.6072

0. 6298 17. 6088

0. 6296 1 7. 6114

0. 6296 1 7.6138 0. 6298 1 7. 6138 0. 6298 17. 61 38

0. 6298 17.6671

0. 6296 17.6729 0. 4435 27. 62 13 0. 4435

27. 6254 0. 4435 27.6260 0. 4435

27. 6323

0. 4435

27. 6361

0. 4435

27. 6361 0. 4435

27. 6361 0. 4435 27.7231

0. 4435 27.7326

0. 4435 27.7366

0. 4435 27.7392

0. 4435 27.7435

0. 4435 27.7472

o. 4435 27.7472

0. 4435 27.7472

0. 4435 27. 6335

0. 4435 27. 6428

0. 4435 27.8468

0. 4435 27.8494

o. 4435

27. 8536 0. 4435

27. 8573 0. 4435 27.6573 0. 4435

27. 6573

0. 4435 2 7. 9428

0. 4435

27. 9521 0.4435

27. 9560

0. 4435 27. 9586

0. 4435 27. 962 6 0. 4435

27. 9665 0.4435

27. 9665 0.4435 27. 9665 0. 4435

26. 0513 0.4435 26.0605 l)s~n~r:tum llllegrlty Associates. Inc.*

1. 960E+06 876.0000

1. 961E+06 1752. 0000

1. 967E+06 5256. 0000

1. 977E+06

1. 051E+04

1. 97BE+06

1. 979E+06 1. 9BOE+06 Blocks:

1. 9BOE+06

1. 9B1E+06 876.0000 876.0000 730.0000 92 876.0000 876.0000

1. 983E+06 17 52. 0000 1. 9BBE+06 5256. 0000

1. 999E+06 1. 051E+04 2. OOOE+06

2. 001E+06

2. 001E+06 Blocks:

2. 002E+06 2. 003E+06 876.0000 876.0000 730. 0000 93 876. 0000 876.0000 2. 005E+06 1752.0000

2. 010E+06 5256. 0000

2. 021E+06 1. 051E+04

2. 022E+06

2. 023E+06 Blocks:

2. 024E+06

2. 025E+06 876.0000 876. 0000 730.0000 94 876.0000 876.0000

2. 027E+06 17 52. 0000

2. 032E+06 5256. 0000

2. 042E+06 1. 051E+04

2. 043E+06

2. 044E+06

2. 045E+06 Blocks :

2. 04 6E+06

2. 04 7E+06 876.0000 876.0000 730.0000 95 876.0000 876.0000

2. 04BE+06 1752.0000

- 2.4490 12.0074 - 4. 3396

10. 5080

-5.1025

9. 9020

-5.9317 9.2437 -6. 5287 B. 7707 -6.8272 B. 5342 -0. 3277 13.6441 -0.3278 13. 6396 - 2. 4505

11. 9617

-4.3410 10.4680 -5. 1039

9. 8643

- 5. 9331

9. 2085

- 6. 5301 8.7373 -6.828 6 B. 5017 -0.3293 1 3.5926 -0. 3295 13.5882 -2. 4521

11. 9166

-4. 3425

10. 4286

- 5. 1053

9. 8271

- 5.9345 9.1739 - 6.5315

8. 7044

-6.8299 B. 4697 - 0. 3310 13.54 19 - 0. 3311 13.5376 -2. 4536 11.8722 -4. 3439

10. 3898

-5.1067 9.7906 - 5. 9359 9.1398 - 6. 5328

8. 6721

- 6. 8312 B. 4382 - 0.3326 13.492 0 -0. 3327 13.4878 -2.4551 11.8286 - 4.3453 10.3516 -30.2724

2. 5969

- 20.5017

5. 0421

-16.5592 6.0280 - 12.2738

7. 0995

-9.1883

7. 8715

-7.6456 B. 2575 -4 1. 24 50 - 0.1486 -30. 2742

2. 5870

-20. 5033

5. 0229

-16.5607

6. 0050

-12.2753

7. 0724

-9.1897 7.8415 -7.6469

8. 2261

-41.2470 -0. 1481 -30.2760

2. 5772

-20.5049 5.0040 -16. 5623

5. 9824

-12. 2767 7.0458 -9.1911 7. 8120 -7.6483 B.1951 -41.2490 -0.1475 -30.27 78 2. 5676 -20. 5065 4. 9853 -16. 5638

5. 9601

-12.2781 7. 0196 -9.1925

7. 7830

-7.6496 8.1646 -41.2510 -0.1470 -30.2796

2. 5582

-20. 5081 4.9670 Report No. 1600539.401RO

27. 8234 1. OOOE-30

9. 4106

2. B07E- 06 16.1621 1. 000E-30

5. 4660 9.124E-07 11.4567

1. OOOE-30 3.8740 5.009E-07 6.3421 l.OOOE-30 2.1 443 2.195E-07

2. 6596

1. OOOE-30 0. 8992

1. OOOE-30

0. 8183

1. OOOE-30 0.2767 l.OOOE-30

0. 0000

7. 230E-05 40.9172 l.OOOE-30 13.7 882

6. 535E-06

27. 8237

1. OOOE-30 9.3747

2. 783E-06 16.1623

1. OOOE-30

5. 4451

9. 046E-07 11. 4568

1. OOOE-30 3. 8593

4. 966E-07

6. 3422 1. OOOE-30 2.1361 2.177E-07

2. 6596

1. OOOE-30

0. 8958

1. OOOE-30

0. 8183

1. OOOE-30

0. 2756

1. OOOE-30

0. 0000 7.170E-05 40. 9176

1. OOOE-30 13.7363 6.479E-06 27.8240

1. OOOE-30 9.3394

2. 759E-06 16.1624

1. OOOE-30

5. 424 6 B. 970E-07 11.4569

1. OOOE-30 3.8447 4.924E-07

6. 3422

1. OOOE-30 2.1281 2. 15BE-07

2. 6596

1. OOOE-30

0. 8924 1. OOOE-30

0. 8184

1. OOOE-30 0. 2746 l.OOOE-30

0. 0000 7.112E- 05 40.9179 l.OOOE-30 13. 6851

6. 425E-06

27. 8242

1. OOOE-30 9.3046 2. 736E-06 16. 1626

1. OOOE-30 5.4044 8.895E-07 11.4570 l.OOOE-30

3. 8304

4. B83E-07 6.3423

1. OOOE-30 2.1202 2.140E-07

2. 6597

1. OOOE-30

0. 8891

1. OOOE-30

0. 8184

1. OOOE-30 0.2736 l.OOOE-30

0. 0000

7. 055E-05 40.9183

1. OOOE-30 13.6348

6. 372E-06 27.8244

1. OOOE-30

9. 2704

2. 714E-06 16.1627

1. OOOE-30

5. 3845

8. B21E-07 B-85

0. 6298 17.6754

0. 6298 17.6770

0. 6298 17.6796

0. 6298 17.6819

0. 6298 17.7349

0. 6298 17.7406

0. 6298 17.7430

0. 6298 17.7446 0. 6298 17.7472

0. 6298 17.7495

0. 6298 17.7495 0. 6298 17.8020

0. 6298 17.8077

0. 6298 17.8101

0. 6298 17.8117

0. 6298 17.8143

0. 6298 17.8166

0. 6298

17. 8166

0. 6298 17.8686

0. 6298 17.8743

0. 6298 17.8767

0. 6298 17.8782 0. 6298 17.8808

0. 6298 17.8830

0. 6298 17.9347

0. 6298 17.9403

0. 6298 17. 9427

0. 6298 17.9442

0. 4435 28.0644 0.4435

28. 0669 0.4435 28.0711

0. 4435 28.0747 0.4435 28.0747 0.4435 28.0747 0.4435 28.1588 0.4435 28. 1679

0. 4435 28.171 8

0. 4435 28.1743 0.4435 28.1784 0.4435 28.1821 0.4435 28.1821

o. 4435 28.1821

0. 4435 28.2655

0. 4435 28.2745 0.4435 28.2783

0. 4435 28.2808

0. 4435 28.2849 0.4435 28.2885 0.4435 28.2885

0. 4435 28.2885 0.4435 28. 3712 0.4435

28. 3802 0.4435 28.3840 0.4435 28.3864 0.4435 28. 3905 0.4435 28.3941 0. 4435 28.3941

0. 4435 28.3941

0. 4435 28.4761 0.4435 28. 4850 0.4435 28.4888

0. 4435 28.4912 l}

Slroc:tural hrlegrtty Associates. Inc.*

2. 054E+06 5256. 0000

2. 064E+06

1. 051E+04

2. 065E+06

2. 066E+06

2. 067E+06 Blocks:

2. 068 E+06

2. 068E+06 876.0000 876.0000 730 0 0000 96 876.0000 876.0000 2. 070E+06 1752.0000

2. 07 5E+06 5256. 0000

2. 086E+06

1. 051E+04

2. 087E+06

2. 088E+06

2. 088E+06 Blocks:

2. 089E+06

2. 090E+06 876 0 0000 876.0000 730.0000 97 876.0000 876.0000

2. 092E+06 1752.0000

2. 097E+06 5256. 0000 2.108E+06

1. 051E+04 2.109E+06 2.109E+06 2.110E+06 Blocks :

2.111E+06 2.112E+06 876.0000 876 0 0000 730.0000 98 876.0000 876.0000 2. 114E+06 1752.0000 2. 119E+06 5256. 0000 2.129E+06

1. 051E+04 2.130E+06

2. 131E+06 2. 132E+06 Blocks:

2.133E+06 2.134 E+06 876. 0000 876. 0000 730.0000 99 876.0000 876.0000 2.135E+06 1752.0000 2.141E+06 5256.0000

2. 151E+06

1. 051E+04

-50 1081 9 0 7546 -50 9372 9.1062 - 6.5341 8 0 6402 - 6.8325 8 0 4072 - 0. 3342 13.4429 - 0 0 3343 13 0 4387 - 2 0 4566 11.7856 - 4 0 3467 10 0 3139 - 5.1095 9 0 7191 -50 9385 9.0731 -6 0 5354 8 0 6088 -6 0 8338 8 0 3767 - 0.3357 13 0 3945 -0 0 3358 13 0 3904 -2 0 4580 11.7432 -4.3481 10.2769 -5.1108 9 0 6842 -50 9398 9 0 0405 -6 0 5367 8 0 5779 -6 0 8351

8. 3466

- 0 0 3373 13.3469 - 0 0 3374 13.3428 - 2 0 4595 11.7015 - 4.3495 10.2404 - 5.1121 9.6499 - 5.9411 9 0 0084 -6.5379 8 0 54 75 - 6.8363 8.3170 - 0 0 3388 13 0 2999 - 0 0 3389 13. 2959 - 2.4609 11.6604 - 4 0 3508 10.2044 -5. 1134 9.6160 - 50 9423 8. 9768 -16.5652 50 9382 -12 0 2795 6 0 9938 -9.1938 7. 7544 - 7 0 6509 8.1346 -41.2529 -0. 1464 -30.2813 2. 5489 -20.5096 4.9489 -16.5667 50 9167 - 12 0 2809

6. 9684

-9.1951 7 0 7262 - 7 0 6522 8.1051 -41.2548 -0. 1459 -30.2830 2 0 5397 -20.5111 4 0 9312 -16.5681 5.8954 -12.2823 6 0 9434 - 9. 1964 7 0 6985 - 7 0 6535 B. 0760 - 41.2567 -0. 1 454 - 30 0 2846 2 0 5307 -20 0 5126 4 0 9136 -16.5695 50 8745 -12 0 2836

6. 9188

-9.1977 7 0 6711 -7.6547 B. 04 73 -41.2586 - 0. 1449 -30.2863 2 0 5218 -20 0 5141 4.8964 - 16.5709 50 8539 -12.2849

6. 8945 Report No. 1600539.401RO 11.4571

1. OOOE-30 3.8164 4.843E-07 6. 3423

1. OOOE-30 2.1124 2.123E-07

2. 6597 1. OOOE-30

0. 8858

1. OOOE-30 0. 8184

1. OOOE-30

0. 2726

1. OOOE-30 0 0 0000

6. 9 99E-05 40. 9186

1. OOOE-30

13. 5852

6. 320E-06 27. 824 7

1. OOOE-30

9. 2367

2. 692E-06 16.1629

1. OOOE-30 5.3650 B. 749E-07 11.4572

1. OOOE-30

3. 8025

4. 803E-07

6. 3424

1. OOOE-30 2.1047 2.lOSE-07

2. 6597

1. OOOE-30

0. 8826

1. OOOE-30 0.8184 l.OOOE-30 0.2716 l.OOOE-30 0 0 0000 6. 945E-05 4 0. 9190

1. OOOE-30 13.5363

6. 269E-06 27.8249

1. OOOE-30

9. 2035

2. 670E-06 16.1630 l.OOOE-30

5. 3457

8. 679E-07 11.4573

1. OOOE-30

3. 7888

4. 764E-07

6. 3425

1. OOOE-30

2. 0971

2. OB8E-07

2. 6597 1. OOOE-30 0.8794 l.OOOE-30

0. 8184

1. OOOE-30 0. 2706 l. OOOE-30 0 0 0000

6. 891E-05 4 0. 9193

1. OOOE-30 13.4882 6.219E-06

27. 8252 1. OOOE-30 9.1708

2. 64BE- 06 16.1631

1. OOOE-30

5. 3267

8. 609E- 07 11.4574

1. OOOE-30 3.7754 4.726E-07

6. 3425

1. OOOE-30

2. 0897

2. 072E-07

2. 6598

1. OOOE-30 0. 8763

1. OOOE-30

0. 8184

1. OOOE-30 0. 2696

1. OOOE-30 0 0 0000

6. 83BE-05 40.9197

1. OOOE-30 13.4408

6. 170E-0 6

27. 8254

1. OOOE-30 9.1386

2. 628E-06 16.1633

1. OOOE-30

5. 3080

8. 542E-07

11. 4575

1. OOOE-30 3.7621 4.689E-07 6.3426 l.OOOE-30

2. 0824

2. OSSE- 07 B-86 0 0 6298 17.9468 0 0 6298 17.9490 0 0 6298 17.9490 0 0 6298 17.9490 0 0 6298 18.0003 0 0 6298

18. 0058 0 0 6298 18 0 0081 0 0 6298 18 0 0097 0 0 6298 18 0 0122 0 0 6298 18. 0144 0 0 6298 18.0144 0 0 6298 18 0 0144 0 0 6298 18 0 0653 0 0 6298 18 0 0708 0 0 6298 18 0 0731 0 0 6298 18.0746 0 0 6298 1 8 0 0771 0 0 6298 18 0 0793 0 0 6298 18 0 0793 0 0 6298 18.0793

0. 6298 18. 1298 0 0 6298 18. 1352 0 0 6298 18.1375 0 0 6298 18.1391 0 0 6298 1 8.14 15 0 0 6298 18.1437 0 0 6298 18.1437 0 0 6298 18.1437

0. 6298 18.1938 0 0 6298 18.1992 0 0 6298 18.2015 0 0 6298 18 0 2030

0. 6298 18 0 2055 0 0 6298 18.2076 0. 4435 28.4953

o. 4435 28 0 4988 0 0 4435 28 0 4988 0. 4435 28.4988 0.4435 2 8.5802 0.4435 28.5890 0 0 4435 28.5927 0 0 4435 28. 5951 0 0 4435 28.5992 0 0 4435 28.6027

0. 4435 28.6027 0 0 4435 28 0 6027 0.4435 28 0 6834 0 0 4435 28 0 6921 0.4435 28 0 6958 0 0 4435 28.6983 0.4435 28 0 7022 0.4435 28 0 7057

0. 4435 28.7057 0. 4435 28 0 7057 0 0 4435 28 0 7858 0 0 4435 28 0 7945 0. 4435 28 0 7982 0.4435 28 0 8006 0.4435 28 0 8045 0.4435 28 0 8080 0. 4435 28 0 8080 0.4435 28.8080 0.4435 28.8875 0.4435 28.8960 0 0 4435 28 0 8997 0.4435 28 0 9021 0.4435 28.9060 0.4435 28.9094 S)Situcturalllllegrlly Associates. Inc.*

2. 152E+06 876. 0000 -6.5391 - 9. 1 989

2. 6598

1. OOOE-30

o. 6298 0. 4435

8. 5175 7. 6442 0. 8732

1. OOOE-30 18.2076 28. 9094

2. 153E+06 876.0000

- 6.8375 - 7.6559 0.8 184

1. OOOE-30

0. 6298

0. 4435 8.2878

8. 01 91 0. 2687 1. OOOE-30 18.2076 28.9094 2. 154E+06 730. 0000

- 0.3402 0. 0000

0. 6298

0. 4435 13.2536

6. 786E- 05 18. 2573 28.9883 Blocks:

100 2. 155E+06 876.0000 -0.3404 -41.2604 40. 9200 1. OOOE-30

0. 6298 0.4435 13.2497

-0.1444 13.3941

6. 122E-06 18.2627 28.9968 2. 155E+06 876.0000

-2.4623 -30. 2879

27. 8256

1. OOOE-30

0. 6298

0. 4435 11. 61 99

2. 5130 9.1068 2. 607E-06 18.2650 29.0005 2. 157E+06 1752.0000

- 4.352 1 -20.5155 1 6. 1 634

1. OOOE-30

0. 6298

0. 4435

10. 1690 4.8794 5.2896 8. 475E-07 18.2664 29.0028 2.162E+06 5256. 0000

- 5. 1147 -16. 5723 11.4576

1. OOOE-30

0. 6298 0.4435 9. 5826

5. 8335

3. 7491

4. 652E-07 18.2689 29.0067 2.173E+06

1. 051E+04

-5.9436 - 12.2862

6. 3426

1. OOOE-30

0. 6298

0. 4435

8. 9457

6. 8705

2. 0751

2. 039E-07 1 8.2710 29.01 01 2.174E+06 876.0000

-6.5404 -9.2002

2. 6598

1. OOOE-30 0. 6298 0. 4435

8. 4879 7. 6177 0.8702

1. OOOE-30 18.2710 29.01 01 2.175E+06 876.0000

-6. 8387 -7.6571

0. 81 84 1. OOOE-30

0. 6298 0. 4435

8. 2590

7. 9913

0. 2678

1. OOOE-30

18. 2710 29.0101 2. 175E+06 730. 0000

- 0.3417 0. 0000

0. 6298

0. 4435 13.2080

6. 735E- 05 18.3203 29.0884 Maximum number of blocks reached. The analysis terminat ed.

Nwnber of Runtime Narnings : 2

- - Runtime l'larning : The current val ue of R( - 1.2640) is l ess than the first value of R(l.OOOE-20) i n the da/dn-Del taK tabl e. The firs t value of R(l.OOOE-20)

Hill be used

- - Runtime l*lar n i ng: The current value of R(3.2249) is greater than the last value of R(0. 9990) i n the da/dn-Del taK t abl e. The l ast value of R(0.9990) will be used
  - End o f pc-CRACK output ***

Report No. 1600539.401RO B-87 SJs~n~c~utVI Integrity Associates, hrc!'}}

v t e Letter Sequence Request
EPID:L-2017-LLR-0092, Flaw Evaluation of Unit 2 Residual Heat Removal Suction Weld Joint (Open)
Initiation Request, Request, Request Acceptance Administration Questions 2 November 2017 Answers Results Approval Other: DCL-24-066, Request to Extend the Nrg Approval of Alternative for Use of Full Structural Weld Overlay, REP-RHR-SWOL
MONTHYEAR2017-05-18 [Table View]

DCL-17-049, Flaw Evaluation of Unit 2 Residual Heat Removal Suction Weld Joint

Text

Dear Commissioners and Staff:

Title:

1.0 INTRODUCTION

7.0 CONCLUSION

8.0 REFERENCES

1.0 INTRODUCTION

7.0 CONCLUSION

8.0 REFERENCES

Title:

Title:

Title:

Title:

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DCL-17-049, Flaw Evaluation of Unit 2 Residual Heat Removal Suction Weld Joint

Text

Dear Commissioners and Staff:

Title:

1.0 INTRODUCTION

7.0 CONCLUSION

8.0 REFERENCES

1.0 INTRODUCTION

7.0 CONCLUSION

8.0 REFERENCES

Title:

Title:

Title:

Title:

Navigation menu

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