View source for L-09-122, Calculation 0900354.301, Rev. 0, Flaw Evaluation for N6A and C Nozzle to Safe End Welds.

{{Adams
| number = ML092650791
| issue date = 04/25/2009
| title = Calculation 0900354.301, Rev. 0, Flaw Evaluation for N6A and C Nozzle to Safe End Welds.
| author name = Gustin H, Herrmann T
| author affiliation = Structural Integrity Associates, Inc
| addressee name = 
| addressee affiliation = FirstEnergy Nuclear Generation Corp, NRC/NRR
| docket = 05000440
| license number = NPF-058
| contact person = 
| case reference number = L-09-122
| document report number = 0900354.301, Rev 0
| document type = Calculation
| page count = 22
}}

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V       Structural Integrity Structural                 Associates, Inc.
Integrity Associates,        Inc.      File No.: 0900354.301 File No.: 0900354.301 Project No.: 0900354 0900354 CALCULATION PACKAGE CALCULATION              PACKAGE                      Project Quality Quality Program:
Program: MIZl Nuclear Nuclear [] D Commercial Commercial PROJECT     NAME:
PROJECT NAME:
Perry Plant Flaw Evaluation Evaluation CONTRACT CONTRACT NO.:
55107920, Revision 55107920,  Revision 3 CLIENT:
CLIENT:                                            PLANT:
PLANT:
FirstEnergy Nuclear rirstEuergy   Nuclear Operating   Co.'
Operating Co;              Perry Perry Nuclear Nuclear Power Power Plant.
Plant CALCULATION TITLE:
CALCULATION         TITLE:
Flaw  Evaluation  for Flaw Evaluation for N6A N6A and  C Nozzle and C Nozzle to  Safe End to Safe End Welds Welds Document        Affected                                       Project Project Manager Manager                Preparer(s)
Preparer(s) &
Revision Document          Pages Affected        Revision Description             Approval                     Checker(s)
Revision Description              Approval                    Cbecker(s)
Revision         Pages                                        Signature & Date           Signatures & Date Signature & Date            Signatures & Date 0
A-i 1- 9 1-9 A-I - A-3 A-3 Initial Issue
                                                                                                        -I *.      -
B-I-B-i   - B-8 B-8                                     "JI/~
H. L. Gustin                T. J. Herrmann T. J. Herrmann 4/25109 HLG 4/25/09                  TJH 4/25109 TJH    4/25/09 JI/~
H. L. Gustin HLG 4/25/09 HLG    4/25109 Page 1 of 11  11 F0306-01RO F0306-01RO

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                                                      .Table Table of Contents

==1.0    INTRODUCTION==
/STATEMENT OF PROBLEM!
INTRODUCTION/STATEMENT                                   PROBLEM/ OBJECTIVE                               ..........................
OBJECTIVE ...............................                3 2.0    TECHNICAL APPROACH OR METHODOLOGY TECHNICAL                                                                         .............................................
METHODOLOGY ....................................................                            3 3.0    ASSUMPTIONS ASSUMPTIONS / DESIGN DESIGN INPUTS ..................                                 .................................
                                                                          ................. :.....................................................     :... 3 4.0    FLAW CHARACTERIZATION CHARACTERIZATION .........................................
                                                                                                               '.......................................... 4 5.0    C  ALC ULA TIO N S .........................................................................................................
CALCULATIONS          .........................................................................................................           5
         . 6.0     STRUCTURAL EVALUATION STRUCTURAL      EVALUATION ..................................................................................
                                                                  .............................................................................             6

==7.0    CONCLUSION==
S CONCLUSIONS AND DISCUSSIONS                                 ................................................................
DISCUSSIONS .......................................................................                        7 8.0    REFEREN CES .............................
REFERENCES      .........................................................           .............................................. 8
:~ ...............................................................................
APPENDIX A INSPECTION 

==SUMMARY==

==SUMMARY==
SHEETS FROM [4] .......................................
                                                                                                             ..................................        A-i A-I PC-CRACK OUTPUT APPENDIX B PC';'CRACK                             ..................................................................................
OUTPUT ..................................................................................                   B-I B-l List of Figures Figure 1. Path 1 Through-Wall Axial Stress (psi) ..............................................................
                                                                                 .................................................................... 9 Figure 2. Center-Cracked Center-Cracked Plate Fracture Mechanics                                       ............................................
Mechanics Model ..................................................                     10 Figure 3.
: 3. Crack Growth Growth Through 200 Cycles ,....................................................................... 111..............................
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==1.0         INTRODUCTION==
/STATEMENT OF PROBLEM!
INTRODUCTION/STATEMENT                          PROBLEM/ OBJECTIVE The N6 A, and C nozzle to safe end welds at Perry are dissimilar metal welds connecting     connecting the low alloy alloy steel nozzle forgings to the Alloy 600 safe ends. The welds are Alloy 821182                             [1, 2]. These 82/182 weld metal [1,2].
welds were previously ultrasonically inspected in 2001,                                   acceptable per IWB-3500 2001, and all results were acceptable            IWB-3500 criteria, requiring no further evaluation.
evaluation. The welds were re-examined during the current     current refueling refueling re-examination identified two flaw indications (on each in the N6-A weld and in (RO12). This re-examination outage (ROI2).
the N6-C weld) in the Alloy 182 material which were detennined  determined to slightly exceed exceed the flaw acceptance acceptance standards of standards      IWB-3514-2 [3,4].
ofIWB-3514-2                    of these flaw indications
[3, 4]. Both ofthese                                determined to be subsurface indications were detennined            subsurface connection to the inside surface of the welds. They were classified as fabrication-indications with no connection indications related defects which had not grown in the intervening intervening period, but were  were re-sized re-sized due to enhancements enhancements in evaluation.
data acquisition and evaluation.
The purpose of this calculation calculation is to evaluate evaluate the identified flaw indications per the requirements of        of IWB-3600, to demonstrate demonstrate that these indications do not affect the structural structural adequacy adequacy of the nozzle to safe end welds.
2.0         TECHNICAL APPROACH APPROACH OR METHODOLOGYMETHODOLOGY mechanics-based evaluation of the flaws is perfonned A fracture mechanics-based                                      performed per the requirements ofIWB-3600 of IWB-3600 considering weld residual stresses present in the welds following the application of a mechanical  mechanical stress improvement process improvement     process (MSIP).
(MSIP). The observed observed flaws are assumed to be growing  growing due to a fatigue crack growth mechanism.
mechanism. The resulting resulting flaws after projected growth during the next 10 year      year inspection inspection period are evaluated evaluated to demonstrate that all structural criteria are maintained.
maintained.
3.0         ASSUMPTIONS ASSUMPTIONS / DESIGN INPUTS
: 1. A composite flaw was assumed,
: 1.                                                                   through-wall dimension and greatest assumed, combining the greatest through-wall eccentricity of the two reported eccentricity              reported flaws and assuming a full 360 degree circumferential circumferential crack length.
This hypothetical hypothetical flaw conservatively conservatively bounds the evaluation evaluation of all of the reported flaws.
: 2. In a previous calculation     performed by SI [1],
calculation perfonned            [1], finite element analysis oftheof the nozzle-safe nozzle-safe end welds was perfonned performed to determine detennine the weld residual stresses present in the welds following the application of a mechanical           improvement process (MSIP) in 1992. The bounding residual mechanical stress improvement                                                       residual stress distribution is shown in Figure 1, taken     from taken*from     [1]. Note  that  in that distribution, which is shown from the inside surface towards the outside (from left to right), the residual stress following MSIP varies from compressive compressive to tensile (perpendicular (perpendicular to the plane of the crack) through the thickness of the weld. In the present calculation, calculation, the weld residual stress is conservatively conservatively taken to be the maximum tensile from that distribution, and is considered considered     to  be a constant   membrane membrane stress across the weld weld File No.: 0900354.301 0900354.301                                                                                           Page 33 of 11 11 Revision: 0 F0306-01 F0306-01

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secondary stress which is not limited by the ASME thickness. Weld residual stress is a steady state secondary calculation such as that which follows, residual stress acts only as aa Code. In a fatigue crack growth calculation mean stress. Weld residual stresses have no effect on cumulativecumulative usage calculations. Therefore, no update to the calculated update            calculated cumulative cumulative usage factor (CUF) is needed to demonstrate ASME Section III code compliance.
: 3. The N6 nozzles are assumed to experience
: 3.                                         experience stress cycles due to plant start-ups and shut downs, and due to system operation in the RHR mode. RHR cycles are assumed to occur twice as frequently as start-up/shut down cycles, and to have the same magnitude. Over the ten year period from the inspection in 2019, the estimated number of such current refueling outage until the next scheduled inspection combined combined cycles is assumed to be less than 100 (49 cycles     cycles reported from 2001 through April 2008
[5]). For additional additional conservatism conservatism in the event that the number of cycles increases significantly significantly from that assumed, calculations are carried out to 200 cycles.
: 4. Crack growth is calculated from the current refueling outage until the next time the N6 nozzles with
         , reported flaw flaw indications indications are scheduled scheduled to be re-examined re-examined (10(10 year inspection inspection interval).
: 5. In the following, all applied stresses are modeled as membrane stresses (i.e., constant magnitude across the wall thickness). This is very conservative since the stress combination combination PL+PB+Q PL+PB+Q includes significant includes   significant bending stresses in the PB and Q terms, and treating bending stresses as membrane membrane is   is conservative.
conservative.
: 6. Since all reported reported flaws are subsurface subsurface with no connection to the weld inside surface or to the coolant chemistry, the intergranular intergranular stress corrosion corrosion crack (IGSCC) growth mechanism is not active. This mechanism requires reactorreactor water chemistry to be present in the crack.
7..,  The fatigue
: 7. "The              crack growth fatigue crack     growth law law for for Austenitic  Material in Air was taken from ASME Section Austenitic,Material                                    Section XI, Appendix C [3]. Since the flaws are subsurface
      , Appendix                                         subsurface and not wetted, the air law is appropriate.
: 8. TheThe value of of Sm used used in in the the calculations calculations is for the Alloy 182 material.
4.0          FLAW CHARACTERIZATION CHARACTERIZATION A total A   total of of 88 flaws flaws were     identified in were identified    in the the Reference Reference [4]
[4] inspection  reports.
inspection reports.
N6A - Flaw Indication Indication 1:1:
Length: 1.5",
Length:     1.5", Through    wall dimension:
Through wall     dimension: 0.35", Separation Separation from from outside outside surface: 0.3" 0.3" N6A - Flaw Indication 2:
Length: 1.2",
Length:           Through wall 1.2", Through     wall dimension:
dimension: 0.2", Separation     from outside Separation from    outside surface:  0.3" surface: 0.3" N6A - Flaw Indication 3:
Length: 2.0",
Length:           Through wall 2.0", Through     wall dimension:
dimension: 0.15",    Separation from 0.15", Separation         outside surface:
from outside   surface: 0.4" 0.4"
, File No.: 0900354.301 0900354.301                                                                                         Page 4 of 1111 Revision: 0 F0306-01' F0306-0J:

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N6A N6A -- Flaw      Indication 4:
Flaw Indication        4:
Length: 0.85",
Length:               Through wall 0.85", Through         wall dimension:                  Separation from 0.15", Separation dimension: 0.15",                        from outside      surface: 0.35" outside surface:     0.35" N6C -- Flaw N6C               Indication 1:
Flaw Indication        1:
Length:             Through wall Length: 1.9",Through 1.9",                       dimension: 0.1",
walldimension:                 Separation from 0.1", Separation       from outside      surface: 0.5" outside surface:     0.5" N6C -- Flaw N6C               Indication 2:
Flaw Indication        2:
Length: 3.7",
Length:             Through wall 3.7", Through               dimension: 0.25",
wall dimension:                  Separation from 0.25", Separation        from outside      surface: 0.3" outside surface:    0.3" N6C -- Flaw N6C               Indication 3:
Flaw Indication        3:
16.6", Through Length: 16.6",
Length:               Through wall        dimension: 0.3",
wall dimension:                Separation from 0.3", Separation       from outside      surface: 0.35" outside surface:    0.35" N6C -- Flaw N6C               Indication 4:
Flaw Indication        4:
Length: 1.9", Through wall dimension:
Length:     1.9",  Through       wall   dimension: 0.2",        Separation from 0.2", Separation               outside surface:
from outside       surface: 0.35" 0.35" From    the review From the     review of ofall all of   the above ofthe   above indications,        there are indications, there      are two    subsurface flaws two subsurface                requiring further flaws requiring      further evaluation [4],
evaluation      [4], which which will      be identified will be                 furthermore as identified furthermore          as Flaw Flaw I1 and     Flaw 2.
and Flaw     2. One One ofofthese        located in these isis located     in the the N6A    weld,    and   one  is  located    in the   N6C   weld. These     flaws   are N6A weld, and one is located in the N6C weld. These flaws are characterized as follows:  characterized      as follows:
Flaw 1 (N6A):
Flaw       (N6A):
1.5", Through Length: 1.5",
Length:             Through wall        dimension: 0.35",
wall dimension:                  Separation from 0.35", Separation                outside surface:
from outside      surface: 0.3" 0.3" Flaw 22 (N6C):
Flaw       (N6C):
Length:
Length: 16.6",       Through wall 16.6", Through               dimension: 0.3",
wall dimension:        0.3", Separation Separation from        outside surface:
from outside      surface: 0.35" 0.35" From the From                          indications, aa single identified indications, the 88 identified                                 worst case single worst            flaw was case flaw           determined that was determined              bounds all that bounds    all of ofthe the flaw flaw indications     for  future   inspections.       This  was   done    in  consideration indications for future inspections. This was done in consideration of future UT technology of  future   UT   technology improvements which improvements         which could       result in could result          identifying additional in identifying                    connected flaws additional connected                  (such as flaws (such     as occurred occurred fromfrom thethe 2001 data 2001    data to    currerit dimensions).
to current   dimensions).
The   inspection summary The inspection                    sheets for summary sheets         for these   flaws [4]
these flaws     [4] are    attached as are attached         Appendix A.
as Appendix       A.
5.0 5.0          CALCULATIONS CALCULATIONS The SI The   SI fracture     mechanics program fracture mechanics                       pc-CRACK [6]
program pc-CRACK              [6] was was used used to    perform the to perform     the crack    growth calculations.
crack growth      calculations.
The   bounding flaw The bounding       flaw from from thethe flaw characterizations above (see assumption 1) was taken as:
flaw   characterizations       above     (see  assumption       1) was  taken   as: Length:
Length:
16.6",  through     wall  dimension:       0.35",    Separation     from 16.6", through wall dimension: 0.35", Separation from outside surface: 0.3".outside    surface:   0.3".
This   flaw was This flaw    was used used as    the starting as the                point for starting point     for the   fatigue crack the fatigue      crack growth      calculation. The growth calculation.        The center-cracked center-cracked plate model was used to represent the flaw geometry for the crack growth calculation. This plate  model     was   used   to  represent     the  flaw  geometry       for  the  crack   growth     calculation. This is is illustrated illustrated in Figure in  Figure 2. This model
: 2. This             treats the model treats      the modeled modeled flawflaw as    infinitely long as infinitely    long inin the  depth direction (into the the depth     direction   (into   the page page in in Figure    2). This   model    effectively     represents     the  assumed      full Figure 2). This model effectively represents the assumed full circumferential flaw. circumferential       flaw.
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Reference Reference [2 page 2] gives the maximum                     experienced at the weld as PL+PB+Q=55.03 maximum stresses experienced                             PL+PB+Q=55.03 ksi for the Inconel material. This is conservatively conservatively used to bound the stress magnitude associated  associated with the startup-shutdown and RHR cycles.
For the purposes of the fatigue crack growth calculation, the Kmax is taken as {PL+PB+Q+RESIDUAL}
{PL+PB+Q+RESIDUAL}
and the Kmin is taken as RESIDUAL.
RESIDUAL. The value of residual stress chosen is consistent with assumption 5; all ail stresses are conservatively conservatively treated as membrane membrane stresses. Referring to Figure 1,        1, the applicable applicable residual residual stress used was for the post MSIP normal operating operating cases(MSIP cases(MSIP OFF, NOP2), where the assumed valued in this analysis is tensile, and axially oriented, i.i. e., normal to the crack face.
assumed The pc-CRACK crack growth results are shown in Figure 3, and the output is included in Appendix B.
For the anticipated number of bounding bounding cycles expected to occur from 2009 to 2019, only a minimal amount amount     of growth  is predicted predicted to occur, even under the very conservative conservative set of assumptions assumptions contained herein. The resulting throughwall through wall dimension oftheof the bounding flaw after 100 cycles is 0.366",
corresponding corresponding to less than 0.02"0.02" growth. This meets the acceptance acceptance criteria ofIWB-3641 ofIWB-3641 [3].
6.0          STRUCTURAL EVALUATION STRUCTURAL           EVALUATION The presence presence of flaws will reduce the amount of wall thickness in the weld that is available to carry load.
The existing existing flaw in nozzle nozzle N6A has an area of: [Flaw 1]: Length (1.5)    (1.5) x Throughwall Throughwall dimension        (0.35) dimension (0.35)
   = 0.53 in2 *. The existing flaw in nozzle N6C has an area of [Flaw 2]: Length (16.6)         (16.6) x Throughwall Throughwall dimension (0.3) =  = 4.98 in2 .*
The cross sectional           of the weld without sectional area ofthe          without flaws is A=     t(OR2-IR A=1t(OR    -IR22)=T(49.87-33.78)=50.55
                                                                                  ):::::1t(49.87-33.78):::::50.55 in2 [7]. So So the reported reported flaws in N6A represent represent approximately 1%    1% of the total area ofthe of the weld. The flaw in N6C represents 9.9%
9.9% of the total area. Removing that amount of material in either      either weld would increase the stress in the remaining material by the same %.      %. All ASME Allowable Allowable stress limits as reported in [2]     [2]
continue to be met after projected projected flaw growth up to an increase of more than 25%. Even if                  the ifthe conservatively evaluated conservatively    evaluated full circumferential                        27E(5.8125 + 0.55) = 14.63 in2 were used, circumferential flaw of 0.366 x 21t(5.8125 this would be 29 % of the area section, section, with a projected             of less than 0.02", significant margin is projected growth ofless provided provided    to primary   stress limits.              .
The primary membrane                intensities at the Alloy 82/182 safe end to nozzle weld are reported in [8],
membrane stress intensities                                                                               [8], ..
sheet 13 of 18 to be 11158 psi for normal and upset conditions.
conditions. The same page notes that any bending    bending stress intensities are very small. The allowable allowable stress intensity intensity for the Inconel material is reported on the same page as 23300 23300 psi. The primary stress intensity intensity ratio (Pm+Pb)/Sm is then equal   equal to 0.48. The largest observed largest                                     approximately 16 inches, and the circumference observed flaw has a length of approximately                                 circumference of the component component at the flaw location is approximately approximately 44 inches, so the ratio of flaw length to circumference circumference is 0.36, which will be rounded to 0.4. Referring to ASME Section XI, 1989          1989 Edition, Table IWB-3641-5, IWB;.3641-5, it may be seen that for a stress ratio of 0.48 (i.e.,
(i.e., less than 0.6) and a flaw length/circumference length/circumference of 0.4, the allowable allowable end of interval flaw depth (2a for a subsurface subsurface flaw) is 0.6 alt.a/t. This value is much greater than File No.: 0900354.301 0900354.301                                                                                               Page 6 of 11   11 Revision: 0 F0306-01O F0306*01

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IntegrityAssociates, Structurallntsgrity that of that          limiting flaw the limiting ofthe             flaw of                           Therefore, the 0.366/1.2=0.305. Therefore, of 6.366/1.2=0.305.                                     flaw is limiting flaw the limiting              acceptable by is acceptable  by the the methods methods ofIWB-3641.
QfIWB-3641.
The   evaluation methods The evaluation                 contained in methods contained          Sections 5.0 in Sections       and 6.0 5.0 and   6.0 are are consistent     with the consistent with         methods and the methods    and requirements      of ASME     Section   XI,  IWB-3600 requirements of ASME Section XI, IWB-3600 and Appendix C. and Appendix       C.
7.0

==7.0         CONCLUSION==
S AND CONCLUSIONS             AND DISCUSSIONS DISCUSSIONS presence of The presence The               ofthe   two reported the two              subsurface fabrication reported subsurface                    defects and fabrication defects          their projected and their              growth due projected growth           to fatigue due to   fatigue does       reduce the not reduce does not                 capacity of the capacity           welds in the welds ofthe           in N6A N6A and                 Code [3]
below Code and CC below                  allowable. The
[3] allowable.          limiting flaw The limiting     flaw shows no shows                      growth in significant growth no significant                     through wall the through in the                  direction, as wall direction,       compared to as compared      to the the 2001  results as 2001 results   as re-re-evaluated last October [5]. This supports the conclusion that the observed indications are in fact evaluated    last October    [5]. This   supports  the   conclusion   that  the   observed    indications  are  in  fact defects. The fabrication defects.
fabrication                                     projected out evaluation isis projected The evaluation                    out for  more than for more           10 years, than 10            allowing the years, allowing        station to the station    to maintain the maintain        current 10 the current    10 year year inspection    interval. All inspection interval. All Code    margins are Code margins       are maintained.
maintained.
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8.0

==8.0       REFERENCES==
REFERENCES
: 1. SI Calculation
: 1. Calculation 0800439.306R0, 0800439.306RO, Residual Heat   Removal/Low Pressure Core Injection (RHRfLPCI)
Heat RemovallLow                            (RHR/LPCI)
Nozzle, N6, ID Repair Weld Residual + MSIP Analysis.
: 2. CB&I Stress Report "238" "238" BWR Vessel" Vessel" Section S-13 sheet 2. SI  File Number 0800439.216 SIFile          0800439216
: 3. ASME Section XI, 1989 Edition and 2001 Edition with Addenda Addenda through 2003
: 4. GE Flaw Inspection Reports APR-09-209-7 APR-09-209-7 (weld IB13-N6A-KB) 1B13-N6A-KB) and ARP-09-209-9 ARP-09-209-9 (weld IB1B 13-13-N6C-KB). SI File 0900354208 0900354.208
: 5. SI Calculation Calculation 0800439.307R1, 0800439.307Rl, Evaluation Evaluation of fabrication defects in N6A and C Nozzle to Safe Safe End Welds.
: 6. SI Program   "pc-CRACK for Windows", version 3.1-98348 Program "pc-CRACK                              3.1-98348
: 7. CB&I Drawing N6 Nozzle Nozzle Forging Forging (RHR-LPCI MODE),"*CBI MODE),"CBI VPF No. 3521-257, 3521-257, Rev. 1, June 1973 1973 SI File 0800439.208 0800439.208
: 8. CB&I Stress Report "238" "238" BWR Vessel" Vessel" Section Section D-13 sheet 13.
13.
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Path 1 Axial StressesStresses (SY)         (SY) 4*0000 60000
                 ,GOOW 40000 2 0000
                                                                                                                         -+-Ilon-"",air
_     NCPl 0                                                                                                _CO   Cod Ca ldl  I I
I                                                                                                          --MSgPO#4 M IP O"
                                                                                                                         -!t"- 1IiI ' POf'
                -20000
                                                                                                                         - - NCP2
                                                                                                                         -..,- (;.0 Id I
                     -o00
                -. 0 000
                -8"000 0          0,2       04 04 I
0.4 00.3 1I           L2 14 DMtIll  from W.Jd 044mw kms    VAN 111 M ' 5I.IIrbee Isaw    Surw* On.) ft .)
Figure 1. Path 1 Through-Wall Through-Wall Axial Stress        Stress (psi)
(PSi)
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a =C. .
1             1             1 L. ra b ..
                                         ~
1t            I..a~
                              -  ~I REQUIRED REQUIRED INPUTS:
INPUTS:
b:   plate half width b: plate       vvidth maxim.un crack a:a: maxinm                   (8max << 0.91b) depth (a.
cmck depth             O.9b)
I ,                         ,F Figure 2.
Figure 2. Center-Cracked        Fracture Mechanics Plate Fracture Center-Cracked Plate           Mechanics Model Model No.: 0900354.301 File No.:
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4, Structu'to';,r        As  SSWer oiates:Ic 5?
brack Gnrwt
                         ,.: <!;          0,1V92                                                 -
092881 01866'
____    i~~;~;~.'1:1/2           i~L2~A~        I      *j-:     4 A2-                                                            -A
                                               -~:__  _
V.-.,>
0     20        40    60     80        l~oo" .120 '140         160       &#xfd;18  200 Figure 3-Crack Gr,owth Through 200 Cycles File No.: 0900354.301                                                        '-  -'                        ..---
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APPENDIX APPENDIX A A
INSPECTION INSPECTION 

==SUMMARY==

==SUMMARY==
SHEETS SHEETS FROM FROM [41
[4]
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HITACHI I I HrrACHI                                                      Austenitic Piping Austenitic                         Piping Flaw Flow Evaluation Sheet                             Sheet 1'nI#Kt: I'eny k*ct:       Pe"y Unit l 1 MIWcIID:    1813-N6A-KB
                                         ~uidID: 18ll-N6A-1<8                                                   EllamOalo BurnDatagbemt:   ....: Af'-09-209O7 APR-09-Z09-07 Inidkcag Indication:: 1   I                                                            S1ugData SIIIng   0aI0 .Anet:   . . . : N/A N/A tfIII8a:d B!IImIfIIt                                                                         tfIIIIIlIIf        B!IIKIIfIIt Felw l/mwh Wall .                0.346 o.J46            0.35                                          .,. nominal.
                                                                                                                      "rTrmbtd-                      LlZ 1.12               Ll 1.1 FEA.L&Wt T.                    1.53             :.5 L5                                         .,.-.1.
T'10mmu,,.                       LZO 1.20               1.2 L2 Swfab      pSmWen"'r =               0333 0.333            03 0.3 rm*M 20IB SectUion II,. 2001 fdIIIon, AS#E SedIan ASHE                                  200A      Mdua AddIi.da TABLE RIB-3514-2 TAMKE                AMWMf USMIo6 UOInch IWB-351WAuanIIIc,...,                 1.$0 hkid NomhII NW*W ~-I-w:. ThkbWU - IngevIc oA           SuSum%       SitMm %             Surbe                S.ljdam %
all
                                                                      ~"                               SUrfDcII" 0.00           10.48 10.118 sut.urfDce "
10.118 10.48                 -
SUbIIII1'ucI "
o.os 0.05 0.10 0.10 10.60 lQ.60 10.88 10.B8 10.60 10,88 lOBS 10.91 10.91Y 10.91 V 0.15 0.15           10-96 10.98            10.9e 10.98                 -                      -
0,20 020            1126 11.26            11.26 1LZ6                  ~                 .
0.25 .         11.38 11.J8            11.38 11.J8                  ~
0.30 o.JO 0.35 o.J5.
11.58 1LS8 11.76 1L76 11.58 1LS8 1176 1L76 0.40 0.110          11.96 11.96            11.96                 ~
0.45 0.50 12.46
                                                                   ,-12.08 1234 12.34 12 l2.D8 1234 1Z.34               -                     --
Allowed Alk9d                   AIIclwed A10w.d 10.91                  1091
* 10.91 a0 0-       0.175 0.175 value--
oil value 011               0.117 0.117 Y-        1.000 v-        LOOO Row is Subsurface Flow     Subsurface Alowed oft AIowed     afts=     10.9%
10.996 a/t=
oft-      14.6%
11&.6'16 COMM~ft ASME Secio Xlroun            run circumferential in orientation.
Indicatin is circurnfenIntia In Flaw Is W=Cmcpzb.b orientation rformed In           xd T"
a*y         S-35,4-L.
wfth WA-3200 -tpe w4 M E29.             E29.
mw"W71"~
Subsurface bsu ce Planar Planar faw flow per IYIA-33ZO IWA-3320,* 1Y14-3320-1 WW,.3320-1 By: ~An:.:::d~re"-!*ROChoI=~~_-=.:::;..--...:._
EvoIuotedLevdQW By:                 ROC9064 Dote                    9* JReviewed                         By.                         Earnest Caon LeveI:..::.II Levet 11_ __                       Date 31Z912OO9 Dote:  3/29/2009      ILevek                        LeYeI:.:::III III_ __                         Date 3/2912009 Dote: 3/29/2009 Poge 22 of 255 vwow3Nr0i File        0900354.301 No.: 0900354.301                                                                                                                                                         Page A-2 of A-3 A-3 File No.:   0900354.301                                                                                                                                                        Page A-2 of Revision: 0 F0306-01 RO F0306-0IRO

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V StructuralIntegrityAssociates, Inc.
I                                                                                 Austenitic Aust..nitic Piping             Piping 8'                 HITACHI HMCH Pn&#xa5;Kt: Perry Unit 1 Flow        Evaluation Sheet Flaw Evaluation                         Sheet WedO.       1813-N6C-KB WiIId /0: l81J-N6C-KB                                                   flIIm   00fa st.t: APR-09-209-09 S amDataght:          APR.()9.2Q9-09 dkxcatmw: 3 1ndIcaIIon:                                                                5IIInf 00fa Sh      Data st.t: ,set:NiA W/A lMm4t             I1JmIr1I.                                                          ffIIIIIrCIIf       ~
flow T1nugIt
                       "'-               VAN Throup. !MIl-           0.31              0.3 0.3                                         "r'--"-
Trwnab .               1.12              1.1 U
FlwLmVO
                            ".,   un,tII T         1655 16.55            15.6 16.6                                      '"Trnmansd.
T'-.d.                    .20 L20               U 12 S rk swa.s.pauCfIMT-        $.-
                                           "SdPwa     0.34             0.35 0.35 A.SME   e an 16 260     . Mm.. 263 Dddmda ASHE 5K1Ion ICI, 2G01 EIIIIan. ZOD3 MdIndo TABLE                    AudimVk SbIIIt.
IW-3S1*2 AuDIItIc TABU! 1W8-:J514.2                      Sbwk UO 1.0LOh      Mo Muh lnd IndI NoIIIInai     Thdma - "-"Ice
                                                                                                                   'YIIIcIIr.a    kmnvko oA all 0.00 0.0 0.05 0.10 0.15 sufam'%
s..tac."
10.48 10AS 10.0 10.60 10.88 10.88 10.88 10.98 sthusagtm SUIsurfaa "
10.48 l0A8 10.0 lQ.60 10.8 10.88 10.98 10.98 Srk"e %
s..tac."
10.50 10.s0 SuLmtxfos S 10.50 10.s0VV 1126 1126             1126 1126              -
0.20 025             1llS 11.38            IUS 11.38 0.30            1258 11.58            11.58 11.58 0.35            1176 11.76            1.76 11.76              -
0.40            11.96 11.96            11.96 11.96              -
0.45 o.so 0,50 12.06 12.oa 12.34 12.34 12.08 12.08 12.34 l2.34 Aflavd Alwed AIbwd              AIkMecI 10.0 10.s0             10.50 10.s0 a=
0=        0L150 0.150 011vake:-            009 a/lvuIue-V.
0.009 1.000 V_         LOOO Flow is Flaw   isSubsurface Subsurface Allowed alt-AlawedaJt-           10.5%
10.5" aIt-aft -      12.5%
125" law b-wuMhCtm FlalrIsUl'      ....... by by Tallie TOM@    MW'-3m1-1W8-351W.
_>mIOl F.*dvm om    ASHE ecn ru itASI4E                         ngifoedm-acodn   1110                    WA-U andA t 11W""3200       andASTliirm. n IndIaItian is                  In SubSwdoC     Planar flaw Pona   Haw WDel' 1W""3320
                                                !#A-3320 , 1W""332G-l rWA-3320-1 jEvaluated
                  &#xfd;Mouated By.            RadIal Andre' Rodid By AandrW
().A..,'
tl          /.....77 Ch'                       Revee By:
ReIIiewed     Bly.______           ~~
Levek 11 level: II                       Date:
Data: 3/28/2009 3/28/2009       IILevek                    l8ve/; III III                        Daft  3/28/2009 Date: 3/28/2009 Pogoi23Of24 Z3 Of Z4 P,6=OC         -3fERIO File No.:   0900354.301 No.: 0900354.301                                                                                                                                              Page A-3 of A-3 File Revision: 0 F0306-01RO0 F0306-01RO

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APPENDIX B APPENDIXB OUTPUT PC-CRACK OUTPUT 0900354.301 File No.:
File  No.: 0900354.301 0900354.301                                     Page B-B-11 of B-8 B-8 Revision:
Revision: 0 F0306-OIRO F0306-01RO

lJ     Structurallntegfity Associates, Inc.
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Structura~
pc-CRACK pc-cv=
VersioD (C) Copyri9ht (C) structural IDteg:ity t=
Copyright 'et fo%"
fazt Windows Version 3.1-98348 3.1-90345 Integrity ~soci Windows
                                                                                              '54 - 'S8 "ge Amsociates.
                                                                                                    . . .s, IDc.
Inc.
3315 2215 ~deDA*laden EXpressway.
Expressway, Suite  S~ite 24  24 Saa San Jose, Jose, CA  CA 98118-1557 95115-1537 Voice:         405-970-0200 408-878-8200 Fax:
Fam:          40B-978-8ge4 408-978-5944 E~i~:
E-uail:        pccrack szuctint.cc=
pccrackistructiAt.CaD Linear Elastic              Fractuxe Mechanics Date: Mon nate:       Hon Apr oe     0   17:22:12 2009 17:22:13 Input Data ;md Input               and lI.esul"s Results f"ile:
rile:       F._PLP=.LrK PY_PLPlIQ.LlM 0900354: Pe%ry

==Title:==
0800354:
Titl.:                        Przzy )IEA NeA and  and NGCNeC rlawFlaw Evaluation Cases:
Load Cases:
Stress Stress CoefficieDts Coefficient*s Case ID                                          CO                     C1 Cl                   C2               C3 C2     Type Type Unit lfembr ODit      membrane......                         10 10                        o0                 o0                o0   Coeff Residual lI.e .. idual CoConzat
                                    .... "                       20                        o0                 o0                 o0  Caeff Coeff
                              ------ Through Wall
                             ------ThEough          Wall Stre  Stresses....es for Load CaDeD    Cases With Stre       ... Coef&#xa3;-------
Stress   Coeff -------
Wall
                            .al~
Depth Depth c......
Case Unitt M*uabr UDi    Heoabr         lI.eaidual C Residual Case Ca**
0.0000 0;0000                      10 10                       20 0.0200 0.0301)                     10 10                       20 o.oeoo 0.0600                      10 10                       21) 20 0.0900 0.1)900                     10 10                       20 20 0.1200                     10 10                        20 20 0.1500                      10 10                       20 0.1300 0.1800                     10 10                       20 20 0.2100 0:2100                     I0 10                       20 20 0.2400 0.2"1)0                    10 10                       20 20 0.2700                     10 10                       20 20 0.3000                      10 10                       20 20 Crack Model:
Crack       HDde~: CenterCeaner Cracked Cracked Plate  P~ate UnderUDder Renowe
                                                                                        ~e Tension               Stress T ..... ion Stres   ..
Crack Parameters:
Para.e~e%D:
Plate Plate      Halt     Width:
Bal&#xa3; Width:               o.eooo 0.6000 Crack      depth:
Crack depth:                          0.2000 0.3000 Co CD     == RmAote      Tension Re.ote Tenaion St~eD5    Stress All
                ~l a~hez other stress          coe&#xa3;ficieutD are neglected.
B~zeDS coefficients                        Deg1ccted~
                                  --------------~-----StreBs    -- Stress          IDte .... ity Factor-Intensity                        -
Factor--------------------
Crack Crack                  Case Case                      Case C:ase size Siae         Unit    MeHmbr UDit Hembr            Residual Re .. idua~ C   c:
0.0060               1.37302 1.27302                2.74604 2.74604 Paqe: 1 Page:
File No.:
No.: 0900354.301 0900354.301                                                                                                                     Page Page B-2 B-2 of B-8 ofB-8 Revision: 0 F0306-OIRO F0306*0IRO

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Associates, Inc.
0.0120           1.942011 1.94209            3.88417 3.18417 0.01110 0.0150           2.27926 2.37926           4.7&IIS3 4.7 853
: 5. 49695 0.0240            2.74848 Z.74548            5~49US
: 6. 14906 0.0300 0.0200           2.01745 3.07453            6.14906 0.0360 0.0260           3.37018 2.23015            e.74026 15.740315 0.0420           3.64303
: 2. 64202         7. 25605 7.2860S 0.0480 0.04110          3.B9804 2.59804            7.7960B
                                                             '1.7960B 0.OS40 0.0540            4.U8n 4.12869            8.2'1'73B 8.27725 0.0600            4.36752 4.28752            8.73503 B.72502 0.0660            4.SBf45 4.5845             9.1'1291 9.17291 0.0720 0.0720            4.79701 4.79701            9.59403 0.07!\)
0.0750           5.00041 5.00041            10.0008 10.0005 0.OB4\)
0.0540           5.111763 5.19763            10.3952 10.3953 0.0900                2951 5.311951
: 5.                   10.779 0.0960 0.0960           5.57675 5.57675           '11.1535 11.1525 0.1020 0.1020           5.75n5 5.75995            11.5199 0.1080 0.1050           5.9311414 5.92964            11.5792 11.!793 0.1140           8.11628 6.11E211           12.2326 0.1200           6-29028 6.2902e            12.5806 12.SII06 0.1260 0.12150               6.462 8.462           12.924 0.1320 0.1220           8.6217a 6.631711           12.2626 13.2U6 0.13BO 0.1250           6.79992            13.59911 13.5995 0.1440            li.!l6671 6.96671            13.9334 0.1600 0.1500              7.U24 7.1324          14.2648 14.2645 0.1560 0.lS60            7.29724           14.5945 14.8945 0.1620 0.1620           7-48146 7.4U46             14.9229 14.9229 0.1650 0.1680           7.e2527 7.62527            15.2505 15.2505 0-1740 0.1740           7.788ell 7_75889            15.5779 15.S778 0.1500 0.1800            7.1152S1 7.95251             15.905 IS. 905 0.1560 0.1860            5.11622 1I.11ea2          16.2326 111.2326 0.1920 0.1920              .m20052 B.2B053           16.5611 16.sell 0.1950 0.1980              . 44521 B.44531           16.5906 16.81106 0.2040 0.2040           8. 81084           17.2217 B.U084            17.2217 0.2100            B.77732 0.77722           17.5546 17.SS46 0.21150 0.2160              8.114U 8.9449          17.5898 17.81!98 0.2220 0.2220            9.11379           18.2276 18.2276 0.2280 0.2250            9.28416 1I.2B4115         16.5692 18.5683 0.2340              9.4562 9.45152         18.9124 18.91%4 0.2400            9.62009 9.630011          19.2602 0.2460 0.%4150           9.80602 9.B0602             19.612 0.2520              9.9842 9.9B42          19.96584 19 .11684
: 0. 2550 0.2580            10.1648 10.164B           20.3296 20.32S15 0.2640 0.21540           10.2481 10.3481           20.6962 0.2700            10.5242 10.5342           21.06B4 21.0684 0.2760 0.27110           10.7225 10.7235           21.4469 21.44159 0.2520 0.2B20              10.916 10.lIle           21.822 0.2880 0.2550            11.1121 11.1121           22.2242 0.2940            11.2121 11.3121           22.6241 22.11241 0.2000 0.3000            11.5161           23.0222 23.0322 Crack Growth        Lawa:
Gr~h Lawn:
               , L .... ID:
Law     ID:     Sect XI hus Sect          Aus Air Air, Model:
Hadel:         ASHE Section XI     XI -- anstenitic     stainless steel agstenibic abainleas           in air environment steel in     enyiro~t da/dX = C - 10^F
* 5 k dKI3.2 where S == 1.0 1.0                          for for   R << 0 1.0 + 1.8
                          = 1.0      1.6 ** R   II        fDr for   0 << II < 0.79 3 <
                             -42.5 +
                          = -43.5    + 57.97 ** a3        fDr for   0.79 < a3 < 11 0.'19 F  =
r = code specified specified       func*ion function         t14umeratuxe of temperature P~age:  2 P'"'I": 2 File No.: 0900354.301                                                                                        Page B-3 ofB-8 of B-8 Revision: 0 F0306-OIRO F0306-OIRO

t>
V Structurallntsgrity Associates, Inc.
StructuralIntegrityAssociates, Inc.
dR =
dK   = J:.aa FmaR - l.'tm:i1l lad, a
A = = ltIaill rain         !/ ~Kmax wbe~e:
where:
C C
* 10~rl OF      =
                                      =      ,.840ae-010 1.Bt03e-010
                  ~.
is fo~for ~     the CUE~eA~ly currently             8elec~ed Selected uni~.      units       of:
farce: Up fa~ce:         kip length; ;Lach length:         inch
                    ~empera~w:e:
temperature:                    550.
550.00000000 FFahrenheit
                                                                       ..hr..ah.. .i~
material           Fracture Toughness Ric:
Material Ka~e~~a1           ID:
MD: Alloy l8Z        182 Depth                          RIC lac 0.0000              Z00.0000 200.0000 0.8000 O.SOOO              Z00.0000 eOO.OOClO 1.0000 1.0000              Z00.0000 eoo.OOOO 1.5000 1.5000              200.0000 eoo.OOOO Inltial Ini~~al           crack .i.e:
crack    siuze                  0. *1780 Cl.1750 Man. crack a~.e=
Max.                  sire=                          [.3000 0.3000 Number of blocl
                !lumber             blockse  ..,=                                1 PrzLn      incrtement of blocit='
P:d.,,~ .iz>=_nu                        block-                   11 Cycl ....
Cycles                 C   .. l.c.
Calc.           Pr.iD~
Print      Crk. <Ont.
CEIl.. Gzw.              Kat..
Mat.
Subblock SubbJ.ock                       !Ti_
                                                 /Time                  incre.
incZ'e~          incre. Law il1c:re. !.a"                         ttIc KIc Per:ryl p.,rryl                          200 200                    11               1          Sect Sec~     Xr ,us XI  Au .. Air hE Alloy Al.l.oy 182 182 lma                                             lain Subblock SubbJ.ock                                       C.....
Case ID baa ID Scale Seal.. ract.or Factor              C ltIain
                                                                                                                     .. oe ID Scale Case           Scal.. ract.or Factor Pe*ryl Perry!                             Residual llesidu.a1 Conat  Const                 1.6000 1.5000        Residual lleaidua1 Conet Const           1.&000 1.5000 Unit.
tJD:L     Membrane Co ltc.brAfte                   5.5000 6.5000 er..
Crack cIL gronh 9Z~b rresults:  ...,ul.tts:
Total TDt. ..l Subblock Subblock Cycles ... Cycles                                                                                            D..Dn Cycl
                    /Tie
                    /TDIr!. /Tlime Cycle ..
                                   /TDIr!.                        mos                 b  in lRain       Del~
DeltaK          R R
DaDn ID ..Dt.
                                                                                                                               /DaDt              Da 0..      ..
a   a/thk
                                                                                                                                                               .. /t-hIL Bl.DCIL:
Block:                1 7
1                 1 6.      64e+001
                                                      ~.64e+OCl1          22.34e+001
                                                                              .34e+001         4.20e+001 4.30 ..+001     0.25 0.3S       .39e-005 7.39   .. -00&   7.29e-005 7.39.. -005   0.17S1 0.1751   0.29 0.29 22                2 6.       GSe+O01 6.1!.5e+ClCll       2.
2.3S a5e+001
                                                                                    .. +001    4. 20e+001 4.30 .. +001    0.28 0.35    7. 3ge-00S 7.39e-005       7.29.,-00S 7.29e-005 7
o .17S1 0.1751   0*.29 0.29 3                      6.
3 6.6S    68e+001
                                                              .. +001     2.
2.3& 28e+001
                                                                                    ..+001     4.30e*001 4.20 .. +001    0.25 0.3S     7.40e-006 7.40.. -00&        .40c-005 7.40 .. -005  0.1752   0.29 0.29 4..
55 4 6. 65e+001 5
G.e5e+001 52 aE.I!S -5es+001
                                                              .. +OOl 2.
2.35 35e+001 2.25e+001
                                                                                    ..+001 2.35..+001
: 4. 30e.001 4.30 ..+001 4.20e+001 4.30 ..+001 0.25 0.35 0.28
                                                                                                                       '1.41.,-005 7.41e-008 7.41e-005 7.41   .. -005 7.41e-005 7.41.. -005 7.41 .. -005 7.4le-005 0.17532 0.1'1113 0.1784 0.29 0.29 0.25                                   0.1'54   0.29 0.29 6                6a E.ESe+001 E.E5e+001           22.25.,+001
                                                                              .25e+001         4.20e+001 4.30 ..+001     0.28 0.25    7.42e-005
: 7. 42e-005       7.42.. -005 7.42e-005     0-1754 0.1754   0.29 0.29 "7
7                 '17 6.65e+001             2.35e+001 2.35.,+001          4.21e+001       0.25 7
E.65e+00l                                4.ale+001       0.35    7..42e-005 43.,-00S     7.4te-005 7.43 .. -00S  0.1755 0.17S5   0.29 0.29 8II               B G.E6e+001 6.E6e+OO1           2.25e+001 2.35.,+001          4.21e+001 4.31.,+001      0.25    7.42e-005
: 7. 43e-005       7.43e-005 7.43.. -005 0.3S                                   0.1756   0.29 0.29 9                  9 6.66e+001              2.
2.35 25e+001
                                                                                    .. +001    4. 81e+001      0.25    7.44e-005        7.44e-005     0-1757 9                9 6. 66e+00l                                   ".31 ..+001     0.35    7.4'1.,-005      7.44 .. -005  0.1'15'1 0.29 0.29 10                 10 6. 66e+001               2.
10                 10 6.E6e+001                 2. 35e+001 35e+001        4.21e+001 4.21 .. +001    0.25 0.3S    ?4e--005
                                                                                                                       .7.4Se-005       7.45e-005 7.45 .. -005  0.1'57 0.1757 0.29 0.29 11                 11 6.96e+001                2.35e+001            4. 21e+001      0.25    7.48e-005        7.45e-005 11                 11 6.e6e+001                 2.35 .. +001        4.31"+001       0.35    7. 45e-005       7.45.. -005   0.1758 0.29 0.29 Pa.ge: 23 Page:
File No.: 0900354.301                                                                                                                                           Page B-4 of    B-8 ofB-8 Revision: 0 F0306-01RO F0306*01RO

tJ Structural V      Structural Integrity Integrity Associates, Associates, Inc.      Inc.
12       12 12  6.664+001 6.6&..+001    2.:5&+001 2.3&.+001    4.21:+001 4.31.,+001   0.25 0.3S     7.46:-006 7.46.,-00S    7. tee-005 0.1789 7.456-ODS         o .118!i  0.29 0.2~
13       12 13  a.66.+001 6.660:+001    2.35e+001 2.<I&e+001   4.21.+001 4.31e+00l    0.25 0.3a   7.46.-00 7.4<<1e-00&    7. Ue-005 0.17 7.406-0D            O.11e6  0.29 0.29 14      14 14  6.67.+001 6.<<1'1.+001   2.384+001 2.3S.+001    4.210-001 4.31.+001    0.23 0.35   7.47?-005
                                                                                  'I. 47e-OO&   7 ** 7 .. -005 0.17e 7.47.-005          O.11E    0.29 0.251 ll5     18 15  6.6?7+001 6.67 .. +001  2&#xfd;25e+O01 2;3& .. +001 4.31a+001 4.81e+001    0.38 0.3&   7.45e-005
                                                                                  'I.4I1e-00&   7.4I1e-008 0.1761 7.45e-008         0.1'161   0.29 0.2!'
16       16 18  6.67+4001 6.6'1.+001    2.38e+001 2.3&.+001    4.22.+001 4.112.+001   0.25 0.3S   7.48#-00
                                                                                  'I.4Ie-OO&    7.411 .. -005 0.1762 71.45.-00G        0.1'162   0.29 0.29 17       17 17  6.67.e+001 6.6'1.+001    2.33e+001 2.3& .. +001 4.22.*001 4.32e+001    0.25 0.3S   7.49.-005
                                                                                  '1.4h-00&     7.4ge-008 0.1762 7.49c-00O         0.1'163   0.29 0.29 ll!      18 18  6.67.+001 6.6'1.+001    2.26.+001 Z.36.+001    4.:22+001 t.32.+001    0.25 0.3&   7.50.-005 7.50e-005    7.50D-00O 7.50.-005 0.1762 0.17e3     o .2~
0.29 19       19 19  6.67.+001 6.6'1 .. +001 2.36.+001 2.315e+00l   4.22+001 4.32 ..+001  0.25 0.35    7.30e-005
                                                                                  'I.SO ..-005  7.50.-005 7.60e-005 0.1764 0'.1'164  0.29 0.2~
20       20 ZO  6.686+001 6.611..+001   2.36e+001 2.315 ..+001 4.22.+001 4.32e+001    0.28 0.3S  7.51e-005
                                                                                  '1.51e-005    7.51e-005 0.1768 7.81.-005        0.1'1e8   0.29 0.29 Zl       21 21  6.680+001
: 6. 68e+OOl    2.36C+001 2.<l15e+00l  4.22+001 4.32e+001    0.28 0.3S  7.82.-005
                                                                                  '1.5Ze-005   7.52C-005        0.1766 7.52e-005 0.1'166          0.29 0.29 22       ZZ 22  6.680+001 6.118.. +001  2.360+001 2.<l15e+00l  4.32C+001 4.3Z.,+001   0.25 0.35  7.52e-005
                                                                                  '1.52 ..-005  7.52 .. -005 0.1766 7.82r-005        0.1'166   0.29 0.29 Z2      22 23  6.68.&#xf7;001 6.118.+001    2.26e+001 2.36e+00l    4.22w.001
                                                             *. :I%e+001  0.25 0.3S   7.532-005
                                                                                  '1.52.-005    7 .. 53.. -005 0.17e7 7.52e-005         0.1'111'1  0.211 0.29 Zt      24 Zt  6.68.+001 6.1111.+001   2.36e+001 Z.26"+001    4.32c+001 4.3Z .. +001 0.38 0.3S  7.54e-00 7.&4e-00&     7.54e-005 0.176a 7.84c-005         O.l'1ee   0.29 0.2~
25      25 Z5  6.69%e001 II. 6ge+OOl   2.36e+001 2.26..+001   4.22e+001 4.33e+001    0.25 0.35  7.54e-005
                                                                                  '1.S4e-00S   7.54e-005 7.5te-005 0.1769 0.1769    0.29 0.29 26      26 26  6.69.+001 1I.6ge+001    2.26e+001 2.3I1e+OO1   4.32e+001 4.2ae+001    0.25 0.35   7.553-005 7.55..-005   77.65e-005  O55e-003 0.1769 0.17U     0.29 0.29 Z7      87 Z7  6.696+001
: 6. 6ge+001    2.36e+001 2.36"+001    4.23e+001
                                                             *. 33e+001   0.23 0.35  7.56.-005
                                                                                  'I.&6e-005   7.56.-00O 7.S6e-005 0.177    0.17'1  0.20 0.30 Zll      28 Z8  6.69e+001
: 6. 6ge+00l    2.369+001 Z.315"+001   4.22e+001 4.33.,+001   0.25 0.35  7.56.-005
: 7. 56e-005   7.86.-00O 7.Slie-005 0.17710.17'11   0.30 0.30 2!1      29 29  6.69.+001 8.l!!Ie+001   2.36e+001 2.36"+001    4.33e+001 4.33e+OOl    0.28 0.3&  7.57e-005
: 7. 57e-005    7.57.e-005 7.57e-005 0.1772 0.1'1'12  0.30 0.30 30       20 ao  6.69e4001 e.<<Ige+001    2.26e+001 2.36e+OOl    4.22.e001 4.33.,+001   0.235 0.3&  7.7e-005
: 7. 57e-005    7.57e-005 0.1772 7.57c-005        0.1'172   0.20 0.30 31       21 a1  6.70e&#xf7;001 41.'10..+001  2.36e+001 z.<lee+OOl   4.22c+001
                                                             ".33.,+001   0.25 0.35  7.588-005 7.SlIe-005    7.588-005
                                                                                                '1.58e-005 0.17720.1'173   0.20 0.30 32       az 6.?Oe+001 32                             4.3ae+00l 0.28 2.26..+001 4.33e+001 11.'10..+001 2.36.+001                  0.3& 7.59.-005
                                                                                  '1.5Pe-005   7.59.-00D 7.SP .. -005 0.1774 0.1174    0.20 0.30 33      23 33  4.70.+001 6.70e+001     2.36e+001 2.311.,+001  4.3e.0&#xf7;01
                                                             *. 33.,+001  0.38 0.35   7.59e-003
                                                                                  '1.5ge-005   7.59e-00D        0.1775 7 .5P.,-005 0.1'1'1&       0.20 0.30 at      34 34  6.7.e+001 6.70..+001    2.37.+001 2.3'1"+001   4.34e+001 4.<14.,+001  0.23 0.3&   7.60e-005 7.IIOe-005   7.6-G-DOS 7.60e-005 0.1778 0.177&    0.20 0.<10 35       25 35  6.70e+001 6.70.. +001   2.27.+001 2.37e+001    4.34O+001 4.34.,+001   0.35 0.35  7.61.-005
                                                                                  '1. 61e-005   7.61D-005 7.61e-005 0.1776 0.1776    0.20 0.30 36       26 36  6.70e&#xf7;001 6.70.+001     2.27.+001 2.:n.+001    4.24O+001 4.34,,+001   0.25 0.35  7.61.-005
                                                                                  '1.61,,-005   7.61e-005 7.61e-005 0.1277 0.17'17   0.20 0.30 37       21 37  6.71.4001 e.71e+001 2.37.+001 2.27e+001    4.34e&#xf7;001
                                                             ".34.,+001   0.235 0.3e  7.62.-00 7.112e-00e   7.62.-0DS 7.6Z .. -008 0.1778 0.1'1711  0.20 0.30 ae       28 38  6.71.+001 6.71e+00l 2.37.+001 Z.37"+001    4.24e&#xf7;001 4.34.,+001   0.25 0.35 0.35 7.62.-DOS
: 7. 63e-005 7.62e-005 7-62r005 7.63,,-005 0.1779 7-62e-005 0.17'19   0.30 0.30 39       29 39  6.71e+001 6.71 ..+001 2.27.e+001 2.37"+001    4.24e+001 4.34.,+001    0.35   7. 63e-005    7.63e-005 0.17'790.1779    0.20 0.30 40       40 40  6.71e+001 2.37.+001 6.71e+001     2.37",+001*  4.24+001
                                                             ".34.,+001   0.25 0.3e  7.645-005 7.64e-005    7.64.-005 7.64e-005 0.178    0.1711  0.20 0.30 41      41 tl  6.71.+001 6.'11e+001 2.37e+001 2.37"+001    4.24a+001 4.3.,,+001   0.23 0.35   7.685-005 7.IISe-OOS   7.65.-00D 7.6Se-005 0.1781 0.1'1111  0.30 0.<10 42      42 fo2 6.'12e+001 2.37.+001 6.72.+001     2.37e+001    4.25.+001
                                                             ".35.+001    0.25 0.35   7.65e-005
                                                                                  '1.ESe-OOS   7.65.-005 7.65.. -005 0.1782 0.17112   0.20 0.30 43      49 41  6.72.+001 6.'I2e+00l 2.27.+001 2.37",+001   4.25D+001
                                                             ".35.,+001   0.25 0.35  7.66e-005 77.66,,-005 7.66e-00O 7.66.. -005      0.1'1112 0.30 0.1782      0.30 4t      44 4t  6.72*+001     2.37.+001 6.72,,+001 2.37e+00l       4.25e+001
: 4. 35e+00l   0.25 0.35     .67e-005 7.e7e-005    7.67.-00O 7.67e-005        0.-1782 0.1''183  0.30 0.30 45      45 45  6.72e+001     2.37e+001 6.72 .. +001 2.<17..+001   4.25e+001 4.3Se+001    0.35 0.35  7.67e-005
: 7. 67e-005   7.67e-005 7.67.,-005       0.178*
0.1784    0.20 0.30 46       46 46  6. 72e+001 2.27.+001 6.72.&#xf7;001     2. 37e+001   4.25e&#xf7;001
                                                             ".35.,+001   0.25 0.35  7.66.-005 7.6I1e-005   7.68.-00O 7.68.. -005     0.1788 0.1785     o.ao 0.20 4?      47 47  6.72..+001 2.3.4+001 6.72.+001     2.<17..+001  4.25*+001
: 4. 35e+001   0.25 0.3e  7.69.-005 7.. ege-00:' 7.69e-00O 7.69.. -005     0.1788 0.1785     o.ao 0.20 48      48 48  6.73 ..+001 2.376+001 6.732.001     2.37';'+001  4.25e+001
                                                             ".3Se+001    0.25 0.3S  7.69e-005 7.69.,-005   7.69.-00O 7.6ge-005       0.1786 0.1786    0.20 0.30 foB     49 411 6.'13.+001 2.27.-+001 6.72.4001     2.37.,+001   4.25e+001 4.35,,+001   0.25 0.35  7.70&-005 7.70.-005     7.70.-00D 7.70e-005       0.17e7 0.1787    0.20 0.30 50       50 50  6.732+001 6.73.. +001 2.38.&#xf7;001 Z.<l8e+00l   4.25c&#xf7;001
                                                             ".35.. +001  0.25 0.35  7.71.-00D 7.71.,-00:'  7.71.-00D 7.71e-005       0.1788 0.17118 0.30 0.30 51      51 51  6.73,,+001 2.32e+001 6.72e+001     2.38e+001    4.36.+001 4.36e+OO1    0.35 0.35 7.7.e-005 7.71e-005    7.71.-00O 7.71.. -005     0.1789 0.1789 0.200.30 52      52 52  6.73.+001     2.38.+001 6.73e+001 2.38e+001        4.26.+001
                                                             *. 3E.,+001  0.25 0.35  7.72.-005
: 7. 72e-005   7.72e-00S 7.72e-005       0.1789 0.1'189 0.30 0.30 e3      8a sa  E.73e+OOl 2.38e&#xf7;001 6.72.+001     Z.3ee+001    4.36.4001 4*.3I1e+001  0.23 0.<1& 7.73e-0O3 7.73..-005   7-72.-00S 7.73e-005         0.179 0.179 0.20 0.30 54      54 54  6.74.+001
: 6. 74e+001 2.28e+001
: 2. <l8e+001  4.36e+001 4.36.,+001   0.35 0.35   7.73e-005 7.73.. -005  71.7.-00D 7.73e-005       0.1791 0.1191 0.200.30 55      55 55  6.74.4001     2.3.e+001 e.74e+OOl z.<le ..+OOl     4.26e+001
                                                             *. 36e+001   0.235 0.35   7.74e-005 7.74..-005    7.74.-00O 7.74e-005       0-1792 0.1712    0.20 0.30 SCi     56 56  6.74 ..+001 2.28.+001 6.74.+001     2.38e+00l    4.36e+001 4.36 .. +001 0.25 0.3S   7.75e-005 7.75..-005   7.75e-006 7.75.. -005     0.1792 0.11112   0.30 0.30 57       57 57  6.74.+001 6.74.,+001* 2.28e4001 2.38"+001    4.26.&#xf7;001 4.360:+001   0.25 0.35   7.76.-005
: 7. 76e-005   7.76.-00D 7.7600-005      0.1792 0.1'193   0.20 0.30 58      58 58  6.74.+001 E.740:+001 2.328+001 2.38e+aOl    4.24.+001
                                                             *. 36.,+001  0.35 0.35   7.76.-005 7.76.. -005  7.76.-005 7.76e-00S       0.1794 0.17114   0.20 0.3a 59       59 59  6. 75e+001 2.38.+001 6.75e+001     2.311 ..+001 4.26a+001 4.36e+001   0.35 0.35  7.77.-005 7.7700-005   7.77e-00S 7.77.,-00&      0.1795 0.1795    0.30 0.30 60       eo 60   6.75.+001 E.75e+001 2.38e+001 2.311e+001   4.27.+001 4.37.,+001   0.35 0.35  7.7.e-005 7.78e-005    7.785-008 7.78e-005       0.1798 0.17P&    0.30 0.30 61   6.73.4001 e.75e+001 2.28.e001 2.3I!"+001   4.372e001
                                                             *. 37e+001   0.25  7.78e-005      7.75e-005        0.1796     0.20 61       III                                         0.35  77.7ee-005      7.7Be-005        0.17Pti    0.30 62      62 E2  6.75e4001
: 6. 75e+001 2.38.+001 2.3e ..+001  4.27w&#xf7;001 4.37,,+001   0.25 0.35    7..7?9-005 7ge-005  7.79.-00D 7.7ge-005       0.1797 0.1797    0.20 0.20 62 63       62 63  6.75c4001     2.38.+001 6.75e+OOl Z.2e,,+001       4.37e+001 4.37,,+001   0.25 0.35   ?.SOr-OD5 7.eO,,~005 7.-0B-005 7.BOe-005       0.1798 0.179B    0.20 0.30 64 64       64 lit 6.75e+001     2.36.+001 6.76e+OOl 2.3e"+001        4.27e+001 4.37 ..+001  0.25 0.3e  7.80e-005
: 7. BOe-005   7.50.-005 7.BOe-005       0.1799 0.1'1911  0.20 0.30 65 65       65 65  6.76e+001 2.28.+001 6.76e+001     2.311.+0Dl   4.27.+001 4.37",+001   0.25 0.35  7.815-005
                                                                                  '1.81,,-005  7.81.-00O 7.Bl.,-005       o.nn 0.1799     0.20 0.30 66 66       66 66  6.76.+001 6.'lh+OOl 2.39.+001 2.3ge+001    4.27.D+001
: 4. 31e+001   0.35 0.3S  7.82.-005
                                                                                  '1.U,,-005   7.826-00O 7.8200-005          0.18 0.111   o.ao 0.20 67 67       67 67  6.76.4001     2.39e+001 6.'l6e+001 2.3ge+01)l      4.27e+001 4.31.,+001   0.25 0.35  7.82.-005
                                                                                  '1. 82e-005  7.82c-005 7.82",-005      0.1801 0.1801     o.ao 0.20 68 68      68 68  6.76.4001 6.760:+001 2.29.+4001 Z.2ge+OOl    4.28e0&#xf7;01 4.38.,+001   0.25 0.35  7.12e-005
: 7. 83e-00S   7.852-005 7.83e-005       0.1802 0.1802    0.20 0.30 69 6!1     69 69  6.776+001
: 6. 76e+00l 2.39e+001       ".38",+001 0.35 2.3ge+OD1 4.28i+001       0.35 7.84.-005
                                                                                  '1.84 ..-005 ?.84.-00S 7 .. 84e-00S    0.1803 0.1803    0.20 0.30 70 70      70 70  6.77.4001 2.39*.001 4.28e+001 0.35 7.84.-005 7-5640-005 6.7'1e+001 2. 3ge+001 4.38e+00l 0.35 '1.84 ..-005 7:84",-005                  0.1802 0.11103   0.30 0.30 71 71      71 71  6.77.+001 6.7'1 ..+001 2.29e+001
: 2. 3ge+001 4.28.+001 4.38.,+001 0.235 0.35 7.25-005
                                                                                  '1. 85e-005 7.85C-00D 7.85.,-005      0.1804 0.11104   0.30 0.30 72 72      72 72  6.77 ..+001 2.39e+001 6.77a+001                  4.a8e+OO1 0.25
: 2. 3ge+001 4.29.+001              7.86.,-005 7.86.-00D 0.35 '7.86-005        7.8600-005      0.1808 0.1805    0.30 0.30 72 7a      72 13  6.77e+001 2.29e"001 6.77.+001     2. 3ge+001 4.38.+001 4.38.,+001 0.25 0.35 7.87.-005
: 7. 87e-005 7.87.-00O 7.117",-005     0.1806 O.lllOti  0.30 0.30 P",p: 40 Page. 4 File  No.: 0900354.301 File No.:  0900354.301                                                                                                        Page Page B-5 B-5 of B-8 ofB-8 Revision: 00 Revision:
F0306-01RO F0306*01RO

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                                          ..e.78.+001 6.77.+001                .. +1)1)1 2.39o+001        4.38     ..+001 4.28.+0D1        0.25 7.811 0.35           .. -005 7.IIBe-005 7 .8o-005       0.11107 0.1807   0.30 0.20 2.39O+001         4.38.4001 78 "70         6.78.+001 2.3ge+001 16 8.7I1e+001 78                     2.29.+001        4.311    .. +001 4.39+0OG1        0.25 7.119 0.35           .. -005 7.111
: 7. t9.-00             ..-005 7.530-005       0.111011 0.1808   0.30 77 77     77   0.78.&#xf7;001 2.3ge+00l 71 1I.7IIe+001         2.29e4001        4.1ge+001 4.29eD001        0.35 7.119     .. -005 7.11ge-005
: 7. e9.-00       7.590-005       0.11109 0.1809   0.30 0.30 711 78     "711 8.711.+001 6.78e.001 2.39.+001 2.29o+001        1I.3h+00l 4.290+001        0.3S   7.90.-005 7.90 0.25 7.90.-005               ..-005 7.900-005          0.1111 0.181  0.30 0.20 79 79     71 79 41.711   .. +001 2.3ge+00l 6.78.+001         2.39o+001        4.lh+00l 4.39e+001        0.35 7.91      .. -005 7.91e-005
: 7. 91-005       7.910-005          0.1111 0.181  0.30 0.20 110 50     80 6.711..+001 2.39 .. +001 80                                      1I.3h+00l 4.39.c001        0.25 7.
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                                                            .. +001   4.39     .. +001  0.25 7.92 0.35  7.92e-005.. -005 7.I2e-005 7.92e-005       0.1812    0.30 Il III    81 6.79e+001 6.79em001         2. 404+001        4.29e+001                                                          0.20 B2 112    112 82 Ii.  "7ge+001 2.40 6.79.+001                ..+1)01 2.40e+001        4.39     ..+001 4.29a+001        0.3S  7.932-005        7.93 0.23 7. 93e-005 7.-920-00C   .. -005   0.1813 0.1812   0.30 0.20 82 113         6.7ge+001 113 6.79.&#xf7;001 2.40.o001 02                     2.40.,+00i       4.3ge+OOl 4.39.+001        0.35 G. 23 7.94.,-005
: 7. 94e-00G    7.911.,-005 7.940-005       O.lB14 0.1814   0.30 0.30 1111 54     84 8.7ge+001 114  6.79e.001 2.40e+OOl 2.40e+001        4.3ge+00l 4.409+001        0.35  7. 94e-005 7.94e-005 0.25 7.94.,-005        7.94.-005       0.11114 0.1814   0.30 0.30 as 85     85 85   e. 7ge+001 2.40 6.79e+001                .. +001 2.40.+001        4.40,,+001 4.40e+001        0.25 7.
0.35       95e-005 7.95e-005 7.95e-005        7.950-005       0.11115 0.1815   0.30 0.30 118 86     a8 6.7""+001           2.40e+00l 6.590+001 2.40.+001                '.110,,+001 4.40O+001        0.35 7. 98e-005 7.96 7.960-005              .. -005 7.96.-005       O.lele 0.1816   0.30 0.30 117 57     87 8.IIOe+001           2.40e+OOl       4.40     .. +001  0O.35 7.96 0.35 7.        .. -005 7.98 96r-005           .. -005 7.96e-005        0.11117 0.1817   0.30 0.20 6.80c+001 2.40e+001                 4.40O+001 58 liB    88   6.80.4001 2 80 6.110..+001           .* 0 .. +001 2.40a+001        11.110.,+001 4.40&sect;o001        0.3S  7.97 ..-00& 7.97.,-005
: 0. 35 7.970-005        7.97C-005        0.18111 0.1815   0.30 09 B9 119         6.80.*001 Z.40 89 6.110..+001                .. +001 2.40.+001        11.110   .. +001 4.400+001        0.3S 0.25 7.911
: 7.       ..-005 7.98 980-005           .. -005 7.990-005        0.1818 0.118    0.30 gO 90     90   6.80.&#xf7;001 2.40e+001 90 6.110..+001         2.40e+001        .... Oe+OOl 4.40C+001              7. 9ge-00& 7.1111 0.35 7.990-005                .. -005 7.990-005        0.1819   0.30 91 91     91 6.110    .. +001 2.40 6.810+001                .. +001 2.40.+001        44.40oe001
                                                                         .* 0..+001     0.35  7.99 0.25 7.        .. -00& 7.91 990-005           .. -005 7.990-005          0.182  0.30 92 92     1112 6.81G+001 2.40.+001 92 6.111.+001          2.40a+001        11.110   ..+001 4.410*001              11 .. 00.-00& 8.00.-005 0.35 S.000-005         8.000-005       D.U21 0.1821   D.30 0.20 92 93     93 8.111 93          .. +00'1 2.40 6.81.+001                .. +1)1)1 2.40.+001        4.111    ..+001 4.41.&#xf7;001        0.35 0.25 8.01.. -00& 5.01O-005 a.01O-005        II.Ol .. -00S   0.11122 O.Izz    0.30 94
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                                                                         .* 1.+DOl      0.35 11.02.,-005 5.020-005        II.OZ  .. -D05 5.02.-005       0.1822    0.30 0.20 96 96     96 96 6.111    .. +001 2.40.,+001 6.82.+001         2.410+001        4. 41 .. +DOl 4.41c+001        0.35 0.35 8.030-005         B.D3e-D05 B.03e-006 S.02.-005              0.lB24 0.1824   0.30 97
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                              !19         .. +001 2.41 6.82.&#xf7;001                .. +001 2.41.+001        4. II l ..+D 0 1 4.41e+001        0.35  B.05.. -005 8.05 0.25 8.050-005               .. -D05 5.050-005       D.1112S 0.1826   0.30 0.20 100 100    100 6.112e+001 10D    6.82.+001 2,41e+001 2.41.+001        4.41     .. +001 4.410+001        D.35 0.3,5 8.06 8.00e-005.. -005 8.06  .. -0D5 5.06o-005       D.IBZ7 D.1827   D.30 0.20 101                                                                0.25 101    1D1 101 6.112     ..+001 2.
6.82.+001             41 .. +DOl 2.41o+001        II.U     ..+001 4.421a001        0.35 11.07     .. -005 8.07
                                                                                                 .07e-008            .. -0D5 8.070-005       0.18Z8 0-.18z   0.30 102    IDZ    6.520+001 2.41 102 6.82.+001                   ..+001 2.41.+001        4.42,,+001 4.420+001        0.35  8.07 .. -005 1I.07 0.25 8.070-005               .. -0D5 8.07.-00C       D.1829 0.1829   0.30 0.20 102 103    102 6.8ie+OD1 ID3    6.502+001 2.41e+0012. 41e+OOI       4.U     .. +00l 4.42e+001              8.0Ile-005 1I.08e-DD5 0.35 8.080-005         8.080-003          D.183 0.182  0.30 0.20 104    104 6.113e+001 6.832+001 2.41.+0012.41 ..+001     4.U      ..+00l 4.42eG001        0.25 1I.0ge-005 0.3S  8.09e-005 8.0ge-005 a.09.-005          D.lS3 0.152  0.31 0.21 105 105    ID5 105 6.                    2.41 ..+0Dl 83.. +0D1 2.41.+001 6.08.+001                           4.42 4.420001.. +001        S.10..-005 B.l0 0.35 8.10o-005                .. -0D5 a.1G.-005       D.1831 0.1821   0.31 106    106 6.83 1D6           .. +001 6.82.4001 2.41e+0012.41 ..+001     4.42.,+001 4.42e+001        0.35 8.10o-005         B.I0e-OD5 B.I0.,-005 8.100-005             0.11132 0.1822   0.31 107    107 6.113.,+001 10-:                     2.41e+00l 6-.803e01 2.41.+001                4.tZe+OOl 4.42.&#xf7;001              8. lle-OOS 8.11.-005 0.35 5.11e-005         8.11e-OD5       D.1113a 0.1032   0.31 105 108    105 6.84.+001 1011   6.84 .. +001 2.tl.,+OOl 2.41.+001        11 .* 2.. +001 4.42e+001         0.35  8.12.,-005 5.12.-005 0.25 8.12.-005         B.12.. -D05     D.1824 0-1824   0.31 0.21 109 109    IDII   6,B440+001 2.41 109 6.840+001                   .. +001 2.41.+001        4.U 4.4.+001 .. +OD1  0.385 11.12 D.35           .. -00& B.ll
                                                                                                 .120-005             .. -OOS 5.120-005       D.1B34 0.1834   0.31 110    llD    6.114oo+D01 2.41 110 6.84.&#xf7;001                   .. +001 2.41e+001        4.43 .. +0Dl 4.42oe001         0.25 8.12 D.3S  8.12e-005..-005 8.13e-DD5 5.120-005       0.lB3S 0.1823   0.31 111 111           6.84 .. +001 2.41 111 6.84e+001                   .. +001 2.42o+001        4.43.. +0D1 4.42e&#xf7;001         0.25 8.
0.3S       14e-005 11.14 8.14.-00s              ..-005 8.14.-DOS       0.1II3S 0.1826   0.31 0.21 112    112    CI.84..+001 2.42e+00l 112 6.8054001            2.42.+001        .... 3.. +0Dl 4.420+001         0.35 II.
0.35        15e-005 II.
8.1-00S              15.. -0D5 5.15-00D5       0.1837 C.1537    0.31 0.21 112 113    113    6.B5a+00l 2.42e+00l 112 6.85.001             2.42.+001        4. 43 .. +0Dl 4.423e001         0.35  5.15.-005 8.16e-OD5 0.25 8.1Se-00S         8.15.-005       0.1838 0.183S    0.31 114           6.118e+00l 2.
114 6.850+001 lU                           42.,+llOl 2.42.+001        4.113 .. +0Dl 4.43.&#xf7;001         0.25 B.16 0.36  8.16.005 .. -006 8.16  .. -006 5.16.-00C       0.1839 0.1829    0.31 115 115    115    CI.S5e+001 2.
115 6.a85.001                42 .. +0ll1 2.42.+001        4."3.,+OD1 4.43e+001         0.325 8.17 0.35  8.17-00S ..-005 1I.17.,-D05 5.17o-005       0.1839 0.1829    0.31 0.21 116 116*          6. II 5e+00 1 2.42 116 6.85.e001 116                             .. +001 2.42.+001        4. 43 ..+0Dl 4.432&#xf7;001         0.25 8.
0.35        18e-00S 8.1B 8.18.-005              .. -005 S.18o-005          0.184  0.31 117    11I 6.115e+001 2.42 .. +0ll1 11'1                                      4 .* 3.. +001     0.25 B.le 0.35  8.180-005.. -005 8.1B  .. -D05 5.18C-005       D.lSU 0.1841    0.31 1i1    118 6.a55+001 2.42e+001                   4.442a001 1111          6.B5a+00l 2.42 118 6.86*4001                   .. +001 2.42.+001        4.44 4.44.4001.. +001  0.3S 0.25 8.19 5.19.-005.. -005 8.11  .. -D05 8.19.-005       0.1842 0.1542    0.31 0.21 119 11111  119    6.86e+D01 2.42 11111 6.864+001                 .. +001 2.42.+001        4.44 ..+001 4.44c4001         0.36 0.25 8.20.005          B.20e-D05 8.20e-005 8.20G-00S              D.1843 0.1842    0.31 0.21 120 1%0    120    6.116e+001 2.42 12D 6.864+001                   .. +001 2.42.+001        ".44 4.44e+001..+001   0.35 11.21 8.21.-00G        II. Zl .. -DOII
                                                                                                       .. -005 5.21.-00D       D.1843 0.1843    0.31 0.31 121 121    121    6.116e+OD1 2.42e+00l 121 6.86.+001            2.42e+001        4. 44 ..+D01 4.44e+001         0.35 8.21.-005
: 8. 21e-005 8.21        ..-DD5 8.21C-005       0.1844 D.1844    0.31 122 122           6.86e+001 2.42 122 6.86e+001 122                             ..+001    4.44 ..+D01       0.3,  B.220-003 D.35 5.22e-005
: 8. 22e-005 11.22       ..-005    D.11145 2.42.+001        4.44&+001         0.35                   5.22.-005       0.1545    0.31 0.31 122 123    122    6.86e+001 2.42.+001 123 6.874+001            2.42e+001        4 .***+001 4.44.+001         0.35 8.23.. -005 8.22        ..-005 8.22e-005       D.184e 0.1846    0.31 0.21 124 124           6. 87..+D01 2.42 124 6.87.+001 124                             .. +001 2.42.+001        4. 44 .. +D01 4.44.+001         0.35  8.24e-00& 8.2"e-OD5 0.25 8.24.-005         8.24a-005       D.IB47 0.1847    0.31 0.21 125 125    125    6. 87.. +DOl 2.42 125 6.07e+001                  .. +0Dl 2.42e+001        4 .....+001 4.445.001         0.35  B.24e-00& 8.24 0.25 8.24e-005               .. -DD5 5.24.-005       0.1848 D.1S48    0.31 126 126    126    6.117 .. +D01 2.
126 6.874+001                42 ..+DDl 2.42e+001        4.45.,+001 4.45B+001         D.35 0.25 8. 25e-005 8.25.-005 8.25r-005        B.25..-005      0.1848 D.1848    0.31 0.31 0.1049 127 127    127    6.117.+001 2.U.+00l 127 6.87.+001            2.43&+001        4.45,,+ODl 4.45a+001         0.25 8.26 D.3S  8.26.-005..-005 8.26.-005 B.26e-DD5       0.1849    D.31 0.21 125 12B    128 6.88.+001 128                      2 6.87e+00l 2.432+001 .* 3..+001     1I.1I5e+001       0.3S B.27.,-00S 0.35                   8.27.. -D05 8.27e-005 8.27.-005                0.1058 O.lBS   D.31 0.21 4.45.+001 129 121    129 129 6.88.+001            2. 44e+OOl 6.IIB ..+001 2.43.+001             4.45e+001 4.45.+001         0.35 0.35  8.27 8.270-005..-00S  8.27e-OD5 8.27.-005       D.18S1 0.1851    D.31 0.21 130 130    120 13D 6.85.+001 6.88.. +001 2.42.+001
: 2. 44e+ll01      '.45,,+001 4.45e+001         0.3S 8.211 0.25  8.28.-00S..-005 1I.211.,-D05 5.25.-005       0.1852 0.1852    0.31 0.21 121 131    121    6. 88.. +D01 2.42.4001 131 6.88.4001            2.U.,+001        4 ** 5.. +001     0.3S 8.29..-005 0.23                   8.2I1e-D05 8.29e-005 8.29.-005              0.11153 0.1852    0.31 0.21 122                                              4.45.+001 la!    122    6.118.+001 2.4324001 132 6.90.+001            2.Ue+001         4.45e+001 4.45e+001         D.3S 8.30.,-005 0.25  6.30-00G5        8.30e-D05 8.300-005       D.1SS3 0.1852    0.31 0.21 122    122 6.89.+001 2.432+001                                                                            0. 1854 121    133 6.118 .. +001 2.Ue+00l                4.45..-+001 4.45ao001         0.35 8.31 0.35  8.31o-005        8.3101-005
                                                                                                       ..-005 B.2l1-005        0.1854    0.31 0.21 134 1311   13.
124 6.59.+001            2 .....+0ll1 e.IIge+OOl 2.43e+001               4.46.. +0D1 4.46e+001         0.25  11.31..-005 8.310-005 0.35 8.21.-005         8.31e-OD5       0. 1855 0.1855    0.31 0.21 125 126    135 6.89e+002 125    6.1111..+001 2-42e+001 2.Ue+OO1         4.46e+001 4.1I~.. +ODl            11.32.,.-005 B.22.-005 D.3S 8.32V-005 0.25                   8. 32.. -DDS    0.11156 0.1856    0.31 0.21 Paq.. : 55 Page:
File No.: 0900354.301 0900354.301                                                                                                                    Page Page B-6 of B-8 B-8 Revision: 0 F0306-01 RO F0306-0IRO

l)      StructuralIntegrityAssociates, V Structurallntegr;ty          Associates, Inc.          Inc.
136 126        Ii. 8ge+001 2.43.,+001 136 6.e89e+001 12e                                  4.46 .. +001 2.432+001 4.46r001           0.25 8.33~-005 0.35  8.23-005        8.33e-005 8.22e-005        0.1115'1 0.1857 0.1557   0.31 0.21 0.21 2.42:+001 4.468+001          0.25 8.342       -O2   B.24 e008 137 127 128  137     6.59.4001 2.43,.+001 6.lIt.,+001 13'1 6.89e+001 128                   2.42.+001      4.46,.+001 4.46+001      0.35 8.34,.-005 0.35  e.348-005       B.34,.-005 5.24e-005        0.185'1 0.1858   0.31 0.21 1311 129  13B   1i.8t..+0*01 2.43 129 6.89.+D01              ..+001 4.46.c001 2.43e+001      *. 46 ..~001  0.35 8.34,.-005 8.35.-005       8.8  ...-005 5.248-005        0.11158 0.1853   C.31 0.21 129 140  1~9 140   6.89.+001 6.90.+001      2.43  ..+001 2.42e+001      *. 46.,+001 4.46.+001     0.25 8.aSe-00s 0.35  8.36.-005       8.~5e-005 8.26r-005        0.18S~
0.188  C.31 0.31 140 141  140 141   6.tO..+001 6.90e+001      2.43  ..+001 2.42e+001      *. 46 .. +001 4.46e+001     0.25 11.36 0.35         ..-005 8.37.-005       8.36.,-005 5.37.-DOS         0.18E 0.1861   0.31 0.21 141 141  141 142   0.90 .. +001 6.90e+001      2.43   ..+001 2.44e+001      4.40 ..+001 4.474e+001    0.32 11.37 0.35         ..-005 8.37r-005       II. 37e-00S S.27-005         O.leel o.1e86   0.31 0.21 142; 142  142 142   6.90..+001 6.90.+001      2.44.,+001 2.44e+001      4:4'7,,+001 4.47e+001     0.25 8.37 0.35         ..-005 8.38.-005   O   8.37    .. -005
                                                                                                      .28e-005       0.1862 0.1862   0.31 0.31 143 144  143 144   11.90..+001 6.90e&#xf7;001      22.44e+001
                                                   .....+001    4.47 .. +001 4.47.+001     0.25 1I.3e 0.35         ..-001i 8.39.-00        15.alle-005 5.23.-00         0.1863 0.1863   0.31 144 145  144 148   41.90.. +001 6.910+001      2.44  ..+001 2.44e"001      4.47 ..+001 4.47.+001     0.35  1I.3h-005 0.25 8.40.-005        11.31.,-005 8.40.-DOS        0.11U13 0.1864   0.3i 0.21 145 146  145 146   6.111 .. +001 6.91e+001      2.44e+001 2.44.+001      4.41.,+001 4.47e4001     0.35 0.23 8.40    ..-005 8.41-005        !l.40.,-005 8.41.-005        0.le64 0.18648  0.31 0.21 146 147  146 147   6. tl .... 001 O.91+001       22.44.+001
                                                   .....+001    4.41.,+001 4.47.+001     0.28 lI.n 0.35         ..-OOIi 8.41.-DOS       8.41 5.41.-00.. -005  0.1865 0.1865   0.31 0.31 147 148  141 148   6.111 .. +001 6.91e+001      2.44  .... 001 2.44""001      4.47.,+001 4.47e+001     0.25 8.41 0.35         ..-005 8.42.-005       !l.n    .. -005 8.42.-DOS        0.186e 0.1887   0.31 0.21 148 149  14B 149   6.91   .. +001 6.91.+001     2.44   .... 001 2.448+001      4.47 ..+001 4.47a+001     0.28 8.U 0.35         .. -001i 8.4.e-00        B.42.,-005 89,42-005        0.186'1 0.1868   0.31 0.21 149 150  149 140   6.91 .. +001 6.92.+001      2.44   ..+001 2.44e+001      4.41 .. +001 4.487+001     0.28 lI.n 0.3S         ..-005 8.44.-00D       15.n.,-005 8.44.-00D       0.186B 0.1868   0.31 0.21 150 151  150 181   6.tZ .. +001 6.92e+001      2.44  ..+001 2.44e+001      4.4Be+001 4.48.+001     0.38 11.44 0.35         ..-005 8.48.-005       B.n     .. -005 8.4%e-005        0.1116a 0.1889   0.31 0.21 1152 III 151 151   0.92 ..+001 6.92.+001      2.44  ..+001 2.44e+001      4.48 .. +001 4.48.e001     0.35 0.35  1I.4l1e-001i 8.45e-00D       8.t5    .. -005 8.46.-005        0.le61 0.187  0,31 0.21 152 152  152 152   6.92..+001 6.92e+001      2.44  ..+001 2.44e+001      4.4B,,+001 4.48.+001     0.25 1I.4Se-00S 0.35  8.46.-00D       8.45    .. -005 B.46e-00O          0.18'1 0.1871   0.31 0.21 153 154  I53 154   6.12 ..+001 6.92e4001      2.44  ..+001 2.44e+001      ** 411.,+001 4.488+001     0.25 B.U 0.35         ..-OOS 8.47e-00        B.46    .. -005 8.47.-005        0.18'11 0.1872   C.31 0.21 15.
154  IS.
154   6.tZe+001 6.92.+001       2.44 ..+001 2.44e+001      *. 4B ..+001 4.48e+001     0.28 8.47 0.35         ..-005 8.48.-005       8.t7.-005 8.487-005        0.11172 0.1872   0.31 0.21 155 156  155 158   li.la.,+OOl 6.93.+001       2.44 ..+001 2.454e+001     4.48 .. +001 4.48e+001     0.35  11.48  ..-005 0.25 8.49.-DOS        8.t15   .. -005 8.49.-D0S        0.18'13 0.1872   0.31 0.21 156 151  IS6 157   6.93   .. +001 6.93e+001      2.45  ..+001 2.45e+001      4.4B ..+001 4.48.+001     0.35  8.49 0.25 8.49.-00..-005   8.U.,-00S 8.49.-005        0.11173 0.1874   C.31 0.31 157 156  15'1 158   6.93.. +001 6.93.+001      2.45  ..+001 2.45e+001      4.48 ..+001 4.49.+0O1     0.35 0.25 B.4h-005 8.40.-005       8.49 8.50.-00.. -005  0.1874 0.1875   0.31 0.31 1511 159  158 159   lI.t2.+001 6.9  2+001     2.45  ..+001 2.45.4001      4.4te+001 4.49.+001     0.25 8.50 0.35         ..-005 8.51e-00        B.50.-005 8.51.-005        0.18'15 0.1878   0.21 0.31 159 160  159 160   6.ta.,+001 6.94.+001      2.45  ..+001 2.45e+001      t.49 .. +001 4.49e+001     0.3S 0.32  8.51.,-005 8.82.-00D       B.51    .. -005 5.5l2-005        0.18'1&#xa3; 0.1877   0.31 0.21 160 161  160 161   11.94  ..+001 6.94e+001      2.45  .. +001 2.45e+001      ".49.. +001 4.49e+001     0.25 8.52.,-005 0.35  8.53.-00D       8.5Z    .. -005 8.52.-005        0.18'17 0.1878   0.31 0.31 161 162  161 161   6.94 ..+001 6.94.+001      2.45.,+001 2.45.+001      4.4t..+001 4.49.+001     0.25 0.25 8.53    ..-005 8.532-005       B.53    .. -00S 0.82.--0S        0.111711 0.1879   0.31 0.21 UZ 162  16Z 162   lI.t4 ..+001 6.94.+001      2.45  .. +001 2.45e+001      4.411 .. +001 4.49c001      0.25 8.5a.,-005 0.35    8.54.-00      II.Sa   .. -005 8.524-005        0.18'19 0.1879   0.31 0.31 In164  163 164   6.94 ..+001 6.94.+001      2.45  .. +001 2.45.+001      4.411.+001 4.49e+001     0.28 11.54.,-005 0.35  8.55.-008       B.5  .... -005 8.58.-005        0.18'19 0.188  0.31 0.21 1U164  164 168   6.94 ..+001 6.98.+001      2.45  .. +001 2.458+001      4.49.+001 4.49.*001     0.32 S.5l1e-005 0.311 8.56.-00        8.55e-00S 8.66.-D-0          O.lSe 0.1881   0.31 0.31 us 166  US 166   6.9Se+00l 6.95e+001      2.45  .. +001 2.45.+001      4.4h+001 4.509+001     0.35 0.32  8.56   ..-005 8.57.-DOS       B.S6    .. -005 8.57.-005        0.1881 0.1882   0.31 0.21 166 167  IE6 167   6.95.+001 6.9,.+4001     2.45e+001 2.45e+001      4.50 .. +001 4.50e+001     0.35  8.57.,-005 0.23 8.57.-005        B.57.-005 8.57.-0D         0.1882 0.1883   0.31 0.21 167 168  16'1 168   E.9Se+00l 6.95e+001      2.45  .. +001 2.45e+001      4.50 .. +001 4.50e+001     0.35  8.57.,-005 0.35 8.5.e-005        B.57 8.588-0D.. -005  0.18S3 0.1884   0.31 0.31 16e 169  168 169   6.9Se+00l 6.956+001      2.45  .. +001 2.45e+001      ".50 .. +001 4.50e+001     0.35 a.58 0.35         .. -005 8.59.-005       8.SB    .. -005 80.9.-005        0.11184 0.1885   0.31 0.21 169 170  169 170   6.9&..+001 6.96.+001      2.45  .. +001 2.46.4001      4.50 .. +001 4.50e+001     0.25 8.5h-00S 0.35  8.60.-005       8.59    .. -005 8.60.-005        0.1885 0.1885   0.31 0.31 170 171  l-?O 111   6. 96e+00l 6.96.+001      2.46  ..+001 2.46.+001      4.50 .. +001 4.50e+001     0.26 8.60.,-005 0.35  5.61.-005       8.6il   .. -005 8.61.-005        0.1885 0.1886   0.31 0.31 I'll 171  I'll 171   6. 96e+00l 6.96+4001      2.46  .. +001 2.46.+001      4.50 .. +001 4.50+.0O1     0.26 8.61 0.35         .. -005 8.61.-DOS       8.61    .. -005S 8.61.--0        o .18se 0.1887   0.31 172 172  172 172   II. 96e+00l 6.96.+001      2.45  .. +001 2.46.+001      4.50 .. +001 4.560+001     0.25 8.61 0.35         .. -005 8.62.-005       11.61 8.62.-00.. -0011 0.11187 0.1888   0.31 0.31 173 174  173 174   E.II6e+OOl 6.96.+001      2.46  .. +001 2.46e+001      4.50 .. +001 4.51e+001     0.25 S.62 0.35         .. -005 8.62.-005       8.62    .. -005 8.62.-00D        0.1888 0.1889   0.31 0.31 174 178  174 175   6.116e+00l 6.97.+001      2.4fi .. +00l 2.46e+001      4.51 .. +001 4.518+001     0.35 0.25 8.63.-005 8.64.-00D       lI.n    .. -005 8.64.-005        0.1889 0.189  0.31 0.21 175 176  1'15 176   6.9'1""001 6.97e+001      2.46  .. +001 2.46e+001      4.51 .. +001 4.S1.+001     0.:15 0.38 8. 64e-005 8.6.4-005       B.64e-005 8.654-005         0.189 0.1891   0.31 0.32 1711 177  176 177   1I.9'1e+00l 6.97.+001      2.45e+OOl 2.46.+001      4.51 .. +001 4.51.+001     0.311 0.25 lI.fiSe-OOIi 8.66.-00D       8.65e-005 B.66.-00D        0.18111 0.1893   0.32 0.32 17'1 178  1'7'1 178   ti.9'1 .. +001 6.97.+001      2.46  .. +001 2.46e+001      ** 51 ..+001 4.51c+001     0.35 0.3   8. 66.. -001l 8.66e-005       8.66    ..-005 8.66.-005        o.lUl 0.1892   0.32 0.32 1711 179  178 179   6.97 .. +001 6.97e+001      2.46..+001 2.46e+001       4.51 .. +001 4.51u+001     0.35 S.66e-OOli 0.25  6.67e-005       15.tifi .. -OOS 8.67e-005        0.18t2 0.1892   0.32 0.22 179 180  1'19 180   6. t'1 .. +001 6.987+001      2.46..+001 2.46e+001       4.51.+001 4.S1w+001     0.25 8.67.-005 0.28  8.66.-005       8.6'1 8.678-00.. -005  0.18n 0.1894   0.32 0.32 180 181  180 181   6.t8.. +001 0.98.+001      2.46..+001 2.46.+001       4.51 .. +001 4.82a&#xf7;001     0.23 II.
0.35      68.,-001i 8.69.-005       8.68.,-005 8.69.-DOS        O.lUt 0.1895   0.32 0.22 1111 182  181 182   1I.ge  .. +00l 6.984+001      2.46..+001 2.46e+001       4.S2 .. +001 4.852+001     0.35  1I.61e-001i 0.38 8.70.-005        11.119  .. -0011 B.70.-D05        0.lS9S 0.1896   0.32 0.22 182 182  182 182   6.98  ..,+001 6.98.+001      2.46.,+001 2.46e+001       4.52 .. +001 4.52e.001     o.as 8.70 0.36        ..-005 8.71e-0OS       8.70.,-005 8.71.e-DO        0.1896 0.1897   0.32 0.22 183 184  183 184   6.118 .. +001 6.98e+001      2.46..+001 2.476+001       4.52 .. +001 4.52e+001     0.35 8.71 0.28         ..-005 8.71.-00S       B.'11   .. -005 8.71.-005        0.18117 0.1898   0.32 0.22
                   'lB4 18   184 188   6.98..+001 6.989+001      2.47..+001 2.47.+001       4.52 .. +001 4.52e+001     0.35 8.71 0.35         ..-005 8.72.-005       11.71   .. -005 8.72e-005        0.1898 0.1898   0.32 0.22 1115 186  1811 186   0.11"'+001 6.99.+001      2.47..+001 2.47e+001       4.S2 .. +001 4.52e+001     0.:15 8.n 0.35         ..-005 8.72.-00        8.72.,-0011 8.72.-005        O.lUe 0.1899   0.22 0.22 186 187  IB6 187   6.n..+00l 6.99c+001      2.47..+001 2.47e+001       4.52 .. +001 4.52a+001     0.3S 8.73 0.35        ..-005 0.743-005       8.73    .. -005 8.74.-DOS        0.18U 0.19  0.22 0.32 187 188  1B7 188   6.9te+00l 6.99.+001      2.47 ..+001 2.47e+001       4.S2 .. +001 4.52e+001     0.35 88.74r-005 0.35   .. 74.....,005 11.74.,-005 8.7Se-005           O.H 0.1901   0.32 0.22 11lB 189  188 189   6.99..+001 6.99e+001      2.47..+001 2.47.+001       4.SZ .. +001 4.52.+001     0.25  8.75..-005 0.25 8.76.-005        8.75    ..
8.76.-005  -005  0.1901 0.1902   0.32 0.32 189 190  189 190   6.11,.,+001 7.004+001      2.47 .. +001 2.474+001       4.53.,+001 4.52.&#xf7;001     0.3S 1I.'16e-005 0.35  8.76e-005       8.76.,-005 8.76.-005        0.11102 0.1302   0.32 0.32 190 191  190 191   '1.00  ..+001 7.00e+001      2.47 .. +001 2.47.+001       4.53 .. +001 4.52e+001     0.35 8.7.6 0.35        ..-005 8.77e-00D       8.'16.. -005 8.77.-00D        0.1903 0.1904   0.32 0.22 191 192  li1 191   7.00  .. +001 7.00m+001      2.47 .. +001 2.47.+001       4.53.,+001 4.52L+001     0.35  8.77  ..-005 0.25 8.78e-005        8.'1'1 .. -005 9.77a-005        0.lB04 0.1905   0.32 0.32 192 192  liZ 192   7.00..+001 7.00.+001      2.47 .. +001 2.47e+001       4.53 .. +001 4.52e8001     0.35 8.78 0.25        .. -005 8.79.-005       8.78.. -005 8.79.-006        0.1905 0.1905   0.32 0.32 193    193   7.00..+001     2.47 .. +001    4.53.,+001    0.35 8.7h-005         8.79.. -005      0.1905   0.32 194    194 194   7.00.+001
                                 '1.00.,+001    2.47.+001 2.4'1 .. +001   4.52.&#xf7;001 4.53.,+001    0.25  8.80e-DO5 0.35 8.80   .. -005   8.80.-00D e.'80.. -0oS     0.1906 0.19015  0.32 0.32 US195  195 US    7.01.4001 1.01   .. +001 2.47.+001 2.47 ..+001     4.52e+001 4.S3.. +001   0.28  8.81--005 0.35 8.111  .. -005   8.91.-005 8.81.. -005      0.1907 0.1907   0.22 0.32 196 196   196 196   7.01e+001 7.01   ..+001  2.47.+001
: 2. 47 ..+1101   4.54e&#xf7;001 4.S.e+00l     0.25  8.81.-005 0.35 8.81.. -005      8.81.-005 B.81..-005       0.1908 0.190e   0.32 0.32 197 197    197 19'1  7.01e+001
                                 '1.01 .. +001  2.47e+001 2.47..+001. 4.54e&#xf7;001 4.54 .. +001  0.25  8.82e-005 0.35 11.112.. -00:1   8.82.-00D 11.112.. -005    0.1909 0.190'   0.32 0.32 Paq  .. : t6 a.ge:
File No.: 0900354.301 0900354.301                                                                                                           Page B-7 of B-8 Revision: 0 F0306-OIRO F0306-0IRO

e V       Structurallntegr;ty Structural              Associates, Inc.
IntegrityAssociates,           Inc.
1ge     190 '7.010+001 2.43e+00I.
UII 1.61,+002                 *. U.,+llOl 0.238 2.45e+llOl *.54u+001                     8.83e-OD5 0.291 8.S3e-005 B.82e-O00 0.3& 8.92e-003             0.191 0.22 0.32 199 199     199 7.01*+001 199 '7.01e+00l 2.4$e+00I.
2.4!1e+lllll 4.Ste+00l 0.88 4.54e+001         8.8te-005 B-64e-005 0.35 8.84e-005  8.84e-005 0.1912 0.1911 0.32 0.32 4
200 200     200 '7.0Z.. +001 2.48e ZOO I.OZe+0O1    2.4!1e+Olll  4.5t.,+001 0.23 001. 4.54e+001    0.3S e.85e-008  0.55c-005 0.91i2 e.8Se-005 8.88e-OD5 0.191Z 0.22 0.32 End of PC-CRAM Output.
Page: I7 Paqe:   '7 File  No.: U0U0354.3U1 Hle No.:    0900354.301                                                                                    Page B-8 Page       ofB-8 B-8 of B-8 Revision:
Revision: 00 F0306-OIRO F0306-OIRO}}