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20697-10 (3/30/06) A CALCULATION SUMMARY SHEET (CSS) AREVA Document Identifier 32-9049384-000 NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY Title ENGINEERING EVALUATION OF INSURGE/OUTSURGE TRANSIENTS PREPARED BY: REVIEWED BY: METHOD: Z DETAILED CHECK E0 INDEPENDENT CALCULATION NAME Todd Sorensen NAME Tomas Straka SIGNATURE j, SIGNATURE TITLE Engineer I DATE / TITLE Principal Eng DATE 4 '- e/3 D COST REF. TM STATEMENT: CENTER 41324 PAGE(S) 16 REVIEWER INDEPENDENCE ___ NAME B. Djazmati PURPOSE AND SUMMARY OF RESULTS: Purpose (Rev. 000): This document is a non-proprietary version of AREVA NP Document 32-9045275-001. The proprietary information removed from 32-9045275-001 is indicated by a pair of square brackets " ( )." The geometry and operating condition are Dominion Power proprietary. The purpose of this evaluation is to assess the effect of the insurge and outsurge transients on the Surge Nozzle Structural Weld Overlay (SWOL). The severity of the insurge/outsurge transients for the Surge Nozzle Structural Weld Overlay requires elastic-plastic analysis. Since the time required for the elastic-plastic analysis is significant, the analysis cannot be completed before the plant restart. The purpose of this evaluation is to assess the effect of the insurge and outsurge transients on the North Anna Surge Nozzle Structural Weld Overlay and provide assurance for safe operation of the plant for a limited number of cycles. A complete re- analysis including the insurge and outsurge transients is scheduled to be completed by the end of 2007. Conclusion: It is judged that II Heat ups and Cool downs with total of I I cycles of these insurge and outsurge transients are acceptable. Please note that a detailed ASME Section III code analysis is planned to provide a detailed evaluation of the complete number of cycles by the end of 2007. THE DOCUMENT CONTAINS ASSUMPTIONS THAT MUST BE VERIFIED PRIOR TO USE ON THE FOLLOWING COMPUTER CODES HAVE BEEN USED IN THIS DOCUMENT: SAFETY-RELATED WORK CODENERSIONIREV CODENERSION/REV F1 YES Z NO AREVA NP Inc., an AREVA and Siemens company Page I of 16

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Page 1: A CALCULATION SUMMARY SHEET (CSS)

20697-10 (3/30/06)

A CALCULATION SUMMARY SHEET (CSS)AREVA

Document Identifier 32-9049384-000NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

Title ENGINEERING EVALUATION OF INSURGE/OUTSURGE TRANSIENTS

PREPARED BY: REVIEWED BY:

METHOD: Z DETAILED CHECK E0 INDEPENDENT CALCULATION

NAME Todd Sorensen NAME Tomas Straka

SIGNATURE j, SIGNATURE

TITLE Engineer I DATE / TITLE Principal Eng DATE 4 '- e/3 D

COST REF. TM STATEMENT:CENTER 41324 PAGE(S) 16 REVIEWER INDEPENDENCE ___

NAME B. Djazmati

PURPOSE AND SUMMARY OF RESULTS:

Purpose (Rev. 000):

This document is a non-proprietary version of AREVA NP Document 32-9045275-001. The proprietary information removedfrom 32-9045275-001 is indicated by a pair of square brackets " ( )." The geometry and operating condition areDominion Power proprietary. The purpose of this evaluation is to assess the effect of the insurge and outsurge transients onthe Surge Nozzle Structural Weld Overlay (SWOL).

The severity of the insurge/outsurge transients for the Surge Nozzle Structural Weld Overlay requires elastic-plastic analysis.Since the time required for the elastic-plastic analysis is significant, the analysis cannot be completed before the plant restart.The purpose of this evaluation is to assess the effect of the insurge and outsurge transients on the North Anna Surge NozzleStructural Weld Overlay and provide assurance for safe operation of the plant for a limited number of cycles. A complete re-analysis including the insurge and outsurge transients is scheduled to be completed by the end of 2007.

Conclusion:

It is judged that II Heat ups and Cool downs with total of I I cycles of these insurge and outsurge transients are acceptable.Please note that a detailed ASME Section III code analysis is planned to provide a detailed evaluation of the completenumber of cycles by the end of 2007.

THE DOCUMENT CONTAINS ASSUMPTIONS THATMUST BE VERIFIED PRIOR TO USE ON

THE FOLLOWING COMPUTER CODES HAVE BEEN USED IN THIS DOCUMENT: SAFETY-RELATED WORK

CODENERSIONIREV CODENERSION/REV F1 YES

Z NO

AREVA NP Inc., an AREVA and Siemens company Page I of 16

Page 2: A CALCULATION SUMMARY SHEET (CSS)

NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUT SURGE TRANSIENTS

A R EVA DOCNUME BER LANT_____ 32-9049384-000 Noh Anna Units & 2 NON-PROPRETARY

RECORD OF REVISIONS

Prepared by: I. Sorensen

Reviewed by: T. Stiuaka

Date: 04/2007 Page 2

Date: 04/2007

Page 3: A CALCULATION SUMMARY SHEET (CSS)

NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAYA ENGINEERING EVALUATION OF INSURGE/OUISURGE TRANSIENTS

A R E V A 1OCU , , N MB,, m l 2N,32-9049384-000 Noth Anna Units & 2N-PROPRIETARY

TABLE OF CONTENTS

RECORD OF REVISIONS .......................................................................................................... 2

1. PURPOSE .................................................................................................................. 6

2. ANALYTICAL METHODOLOGY ...................................................................................... 6

3. KEY ASSUMPTIONS ............................................................................................................. 64. SEVE RITY ASSE SSMIENT OF ADDITIONAL INSURGE/OUTSURGE

TRANSIENTS ............................................................................................................................... 7

5. NOZZLES COMIPARISON ..................................................................................................... 7

5 .2 .1 T ran sien ts .... .. .... ... . ... ... .. ... ... . .... . . .. . .. .. .. ........ ... .. ..... .. ..... 1

51. .2 E xtern al L oads.. ........ ........ ...... .... ..... . ........... ..............-.... ..... 11

5 .3 M A T E R IA L S .......... .... ............... .. ... ......... .. ...... ..... ........... ... ... 1

6. EVALUATION OF NOZZLE DIFFERENCES ................................................................ 13

7. RESULTS SUMMARY/CONCLUSION OF STRESS ANALYSIS ................................. 14

8. RESULTS SUMMARY/CONCLUSION OF FRACTURE MECHANICS ..................... 159. REFERENCES ................. ................................................................................................... -16

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

Prepared by: T. SorensenReviewed by: T. Straka

Date: 04/2007Date: 04/2007

Page 3

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGEJOUISURGE TRANSIENTS

AR EVA DOCUMIENT NUMBER PANN

32-9049384-000 North Anna Units 1 & 2 NON-PROPRIETARY

LIST OF TABLES

Table 5.1-1 Geometry Comparison ..-..................... ... 7........-....... 7

Table 5.2-1 Insurge/Outsurge Transient Comparison...........................11

Table 5.2-2 DC Cook Unit I External Loads -................ 12

Table 5.2-3 DC Cook Unit 2 External Loads ........................ 12

Table 5.2-4 North Anna External Loads ............. ... 12

Table 5.3-1 Material Comparison........................................ 13

Prepared by:. I.. SorensenReviewed by: T. Straka

Date: 04/2007

Date: 04/2007

Page 4

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUISURGE TRANSIENTS

A R EVA DOCUbMEN NUMBER PANITE

32-9049384-000 North Anna Units I & 2 NON-PROPRIETARY

LIST OF FIGURES

Figure 5.1-1

Figure 5.1-2

Figure 5.1-3

Model ofDC Cook Unit I Smuge Nozzle............................. 8

Model of DC Cook Unit 2 Surge Nozzle.............................9

Model of'North Anna Unit I and 2 Surge Nozzle .. . ..................... 10

... ...................... .. ....... ................................ .: ........... ............. .......... .. .

Prepared by: T. Sorensen

Reviewed by: T. Straka

Date: 04/2007

Date: 04/2007

Page 5

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGFOUTSURGE TRANSIENTS

AREVA DOCI NUME PLANON-PROPRIETARY

32-9049384-000 North Anna Units 1 & 2

1. PURPOSE

The purpose of'this evaluation is to assess the effect of the insurge and outsuige transients on the SurgeNozzle Structural Weld Overlay (SWOL).

Due to severity of the insurge/outsutge transients, the Surge Nozzle Structural Weld Overlay requireselastic-plastic analysis. Since the time required for the elastic-plastic analysis is significant, theanalysis cannot be completed before the plant restart- The purpose of this evaluation is to assess theeffect of the insurge and outsurge transients on the North Anna Surge Nozzle Structural Weld Overlayand provide assurance for safe operation of' the plant fox a limited number of' cycles. A complete re-analysis including the insurge and outsutge transients is scheduled to be completed by the end of 2007.

2. ANALYTICAL METHODOLOGY

The insurge and outsurge transients will only impact the secondary and fatigue criteria and crackgrowth analysis. The SWOL was sized to meet the requirements of Code Case N-740-1 (Reference 7).The sizing calculation ensures the SWOL is capable of transferring the loads between the piping andnozzle. Therefore, the SWOL meets all the primary requirements defined by the ASME Code. Bydefinition, the insurge and outsurge transients will not affect the primary stresses and therefore theprimary Code requirements are not affected by the addition of these transients

The general methodology for the evaluation of the unanalyzed transients on ASME code criteria ate:

1) Evaluate the severity of the transients based on temperature and pressure difference betweenstarting and ending time point, flow rates, number of occurrences, temperature gradients and otherfactor's affecting stresses usage factors and ratcheting.

2) If transients are found to be severe, evaluation of their impact on ASME criteria will be performedusing comparison to similar surge nozzle geometries subjected to similar loads.

3) Reconcile the design and transient differences between the North Anna surge nozzles and the DCCook nozzles. Nozzle dimensions that impact stresses in the overlaid region ate: nozzle insidediameter, nozzle outside diameter, weld overlay thickness, thermal sleeve thickness and placement,head thickness, head radius. Loads that impact the stresses are transients and external loads..Finally, materials must be compared for' their physical properties and allowable limits.

3. KEY ASSUMPTIONS

There are no major assumptions for this calculation. Minor Assumptions are noted where applicable.

... .. ... .. ... . .../ ...... .. . . . . . ..... ... ... . .

Prepared by: T. Sorensen Date: 04/2007 Page 6

Reviewed by: T. Straka Date: 04/2007

Page 7: A CALCULATION SUMMARY SHEET (CSS)

NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUISURGE TRANSIENTS

AR EVA DOCUMEN NU•MB•E PN PIn1 32-9049384-000 North Anna Units 1 & 2 NON-PROPRIETARY

4. SEVERITY ASSESSMENT OF ADDITIONAL INSURGEIOUTSURGETRANSIENTS

Upon review of Reference 1, it was concluded that the additional insuige/outsuige transients ate of'severe nature and would affect secondary stresses, fatigue and possibly other applicable ASMEcriteria.

5. NOZZLES COMPARISON

DC Cook Units 1, 2 surge nozzles were selected because they ae neatly identical to the North AnnaUnits 1, 2 surge nozzles. The DC Cook surge nozzles were analyzed in detail to the ASME Section HIcode and reported in Reference 2 and Reference 3.

5.1 GEOMETRY

Ihe following table summarizes key geometrical dimensions of DC Cook Unitl, DC Cook Unit2 andNorth Anna surge nozzles. Compared ae dimensions that ate significant for stresses..

Table 5.1-1 Geometry Comparison

Prepated by: T. Sorensen

Reviewed by: 1. Straka

Date: 04/2007Date: 04/2007

Page 7

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NORTH ANNA UNITS l&2, PRESSURIZER SURGE NOZZLE WELD OVERLAYA ENG.INEERING EVALUATION O1F INSURGE/OUTSURGE. TRANSIENTS

A R EV DOCUMEN NU.dBEA nP1 32-9049384-000 North Anna Units I & 2 NON-PROPRIETARY

Figure 5.1-1 Model of DC Cook Unit I Surge Nozzle... " " :" " . : .... .. ... ....... .. ..... ... .i': ! • I T :: • ....... .. ........ ...... ......... :". . i" " ............... ..... ...

Prepared by: I, Soiensen

Reviewed by: I. Sthaka

Date: 04/2007

Date: 04/2007

Page 8

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUTSURGE TRANSIENT'S

AREVA DOCUME MER ANNON-PROPRETARY

1 _ 1 32-9049384-000 North Anna Units 1 & 2 N

Figure 5.1-2 Model of DC Cook Unit 2 Surge Nozzle

....... .... ....... .... ............. : .... ......... ................ :.-.: ...... .... ........ ....... ...

Prepared by: r.. SorensenReviewed by: I. Straka

Date: 04/2007Date: 04/2007

Page 9

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NORTH ANNA UNIT'S l&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUTSURGE TRANSIENTS

AR EVA DOCLUeT•lMhd• PITIETAR

32-9049384-000 Noith Anna Units I & 2 NON-PROPRIETARY

Figure 6.1-3 Model of North Anna Unit 1 and 2 Surge Nozzle

Prepared by: 1. SorensenReviewed by: T. Straka

Date: 04/2007Date: 04/2007

Page 10

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGEIOUTSURGE TRANSIENIS

AREVA DOCMI NUMBER ANNON-PROPRIETARY

1 _ 1 32-9049384-000 North Anna Units I & 2 N

5.2 LOADS

The following is comparison of loads applied on DC Cook Unit 1, DC Cook Unit 2 and North Annapressmizer surge nozzles..

5.2.1 Transients

The following is a tabulation of'the insuwge/outsurge transients comparison between DC Cook Unit 1,2 and the North Anna Units 1, 2 pressurizer surge nozzles..

Tam3le 5.2-1 InsurgelOutsurge Transient Comparison

5.2.2 External Loads

The following tabulation shows a comparison for the external loads between DC Cook Unit 1, 2 andNorth Anna Units 1, 2 pressurizer surge nozzle.

Dead Weight (DW) and DBE loads are not considered here. DW does not contribute to the stressintensity ranges. DBE is not considered since it is a Faulted condition load and therefore is not requiredfor the Primazy + Secondry Stress Intensity check and fatigue.......

Prepared by: T.. SorensenReviewed by: T.. Straka

Date: 04/2007

Date: 04/2007

Page 11

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUAIION OF INSURGE/OUISURGE TRANSIENTS

AR EVA 24 4-0t Anna Units 12 NON-PROPRIETARY32-9049384-000 Noitla Anna Units I & 2

/I**"-

Table 5.2-2 DC Cook Unit I External Loads

Table 5.2-3 DC Cook Unit 2 External Loads

J

Table 5.2-4 North Anna External Loads

2

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

-I

Prepaied by: T. Sorensen

Reviewed by: T. StakaDate: 04/2007Date: 04/2007

Page 12

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUISURGE TRANSIENTS

AREVA DOCUMET NUM PLANTNON-PROPRIETARY

32-9049384-000 North Anna Units I & 2

5.3 MATERIALS

Connections of' materials of dissimilar physical properties such as thermal expansion, Young'smodulus, specific heat, thermal conductivity and density would affect secondary stresses. In addition,stress allowable limits will affect the ASME criteria.

The following table shows a comparison of the materials used for DC Cook Unit 1, 2 and North AnnaUnits 1, 2 surge nozzles.

Table 5.3-1 Material Comparison

6. EVALUATION OF NOZZLE DIFFERENCES

1) Geometry: A review of geometrical differences indicates that all three nozzles configurations. aevery similar. Parameters critical for' stresses such as OD and ID at the overlaid region are nearlyidentical. The only diffeience between North Anna Units 1, 2 and DC Cook Units 1, 2 is at theminimum safe end ID that differs within ( ).. The overlay thicknesses have minor variations.. This willproduce an insignificant impact on stresses, and subsequently any crack growth that-may occur.. Other -variations are also judged to have negligible effects on stresses.

2) Transients: .There is..one similar transient between DC Cook Units 1, 2 and North Anna Units 1, 2.The insurge/outsurge off . deltaI occurs( htimes for both DC Cook Units.. North Anna experiences

Prepared by: T. Sorensen

Reviewed by: T.. Straka

Date: 04/2007

Date: 04/2007

Page 13

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF 1NSURGEIOUISURGE TRANSIENTS

AR EVA DOCUMEN INUMBER P1 ANT

1 32-9049384-000 North Anna Units 1 & 2 N RY

( ]occurrences.. This is the most severe and bounding transient fox all the plants. This transient is moresevere fox DC Cook Units I and 2 since the average temperature gradient is larger, the pressure changedining instuge/outsuige is significantly higher and finally, the flow rate is significantly higher. Due tothese increased severities, DC Cook surge nozzles are expected to experience noticeably higherstresses and its ranges.

3) External Loads: There is a wide spread of external loads between each unit, however, there isrelatively small contribution of' external loads to stresses and usage factor since duringinsmuge/outsurge, there is no stratification load. (It must be pointed out that stratification loads havebeen considered for the North Anna PRZ Surge nozzle analysis, Reference 6). The thermal expansionis assumed to have a small contribution to fatigue and stresses since the insurge/outsurge is a relativelyshort event (small variation of thermal expansion load) that happens at the beginning of heat up andend of cool down.. Finally, it is very unlikely that OBE will consistently happen during theinsurge/outsuige. Therefore, the OBE will not affect stress ranges due to the insurge/outsurge events.

4) Materials: The materials for the head and surge nozzle of North Anna Unit 1 &2 are not the sameas at D. C. Cook UI. The difference in Young's modulus is about( )and the difference in coefficientof thermal expansion is about ( J. It is judged that this difference will cause some impact on stresses,but the impact on stresses and usage is judged to be of low significance that will not invalidate thisconservative comparison evaluation. Since the materials for the head and sunge nozzle of'North AnnaUnit 1 &2 are the same as for D.. C. Cook U2, the stresses and usage factor are comparable.

The pipe and elbow material for North Anna Units I and 2 is different compared to D. C.. Cook U1 andU2.. However, all the materials are ( 3 and the differences in the properties areinsignificant.

7. RESULTS SUMMARYICONCLUSION OF STRESS ANALYSIS

It is shown that DC Cook Units 1, 2 surge nozzles are comparable to North Anna Units 1, 2 surgenozzles.. Conservative analyses for- DC Cook Units 1 and 2 qualified the overlaid nozzles to allapplicable requirements of the ASMIE code as indicated in conclusions of both documents, Reference 2and Reference 3. It is expected that using the same level of conservatism as for the DC Cookcalculations, North Anna surge nozzle analysis would yield lower, or at worst case, comparable results..The maximum increase of' usage factor for( I heat up and cool down transients with total( 3instuge/outsurges pet Reference 3 for DC Cook U2 is T 3 Ihe contribution of the insurge/outsungeas a sub-cycle is( J. The maximum increase of usage factor prorated forL. heat up and cool downtransients with total( Jinsurge/outsurges per Reference 2 for DC Cook UI is .. . I The proratedcontribution of the insurge/outsurge as a sub-cycle is ( 3. The main difference in the usage factor isthe level of conservatism. DC Cook U2 was first of'a kind, thus more conservatisms were used. Themaximum usage calculated for North Anna surge nozzle without the additional insurge/outsutgetransients is [ . per Reference 6. Considering usage factor of ( 3 per Reference 10 of the un-overlaid original nozzle for full amount of design transient cycles to account for cycles spent, it is clear-that the total( ) usage factor will not exceed the allowable limit. In addition, there is..no.impact on prirmarystress magnitudes and limits..

Prepared by: T. Sorensen Date: 04/2007 Page 14

Reviewed by: T. Straka Date: 04/2007

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NORTH ANNA UNITS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUI.SURGE TRANSIENTSA R EVA Pxtrni LmE ANAREV DMUENT UMURnAMNON-PROPRIETARY

32-9049384-000 North Anna Units 1 & 2

The above comparison, the small contribution of the insuige/outsurge transients to fatigue, and the lowfatigue usage calculated for the North Anna Analysis, provide the justification for accepting a smallnumber of the un-analyzed transients.. Since two insurge/outsurge events are considered for heat upsand two insuige/outsurge events are considered fox cool downs per- Reference 10, conservatively, it isjudged that number of plant restart shall be limited t4( I heatups and cooldowns combined with a totalof( ) cycles of these insurge/outsurge transients. This number of' events can be imposed on theoverlaid pressurizer surge nozzle with no impact to safety of North Anna Units 1, 2 without detailedanalyses of these events performed. Please note that a detailed analysis is planned to provide a detailedevaluation of the complete number of cycles by the end of 2007.

8. RESULTS SUMMARYICONCLUSION OF FRACTURE MECHANICS

For the limited number- of proposed cycles, ( )heatups and cooldowns combined with( ) cycles ofinsurge/outsutrge transients), the amount of crack growth is expected to be very small. Based on thefiacture mechanics analyses performed to assess crack growth at the surge nozzles at DC Cook Units1, 2 (References 8 & 9), thel Iheatups and cooldowns combined with( . cycles of insurge/outsurgetransients contributed no more than ') of crack growth. A similar, amount of crack growth isexpected at North Anna which is similar to the DC Cook units, as demonstrated by the comparison inSection 6.0. This amount of' ciack growth is much less than the value currently calculated for- theremaining life of the North Anna surge nozzle. The crack growth analysis was performed consideringthe existence of a postulated flaw. Post-weld overlay NDE inspection of the surge nozzle wasperformed for the outer )of the original pipe thickness as per the requirements of ASME CodeCase N-740 and no indications were found.. Therefore, for the limited period of time for which thisjustification is performed, it is assured that the weld overlay thickness is more than adequate toaccommodate any potential crack growth due to the heatup/cooldown and insuige/outsurge transients.

Prepared by: I. Sorensen

Reviewed by: T. Straka

Date: 04/2007

Date: 04/2007

Page 15

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NORTH ANNA UNIIS 1&2, PRESSURIZER SURGE NOZZLE WELD OVERLAY

A ENGINEERING EVALUATION OF INSURGE/OUTSURGE TRANSIENTS

AREVA DOCUM NUMBE ANON-PROPRETARY

1_ 1 32-9049384-000 North Anna Units 1 & 2 N

9. REFERENCES

1

2

3

4

5

6

7

8

9

10

AREVA Document 38-9034638-002, "Required Engineering Input for North Anna PressurizerWeld Overlays, North Anna Power Station Units I & 2."

AREVA Document 32-9028843-001, "DC Cook Unit 1 Pressurizer Surge Nozzle WeldOverlay Analysis."

AREVA Document 32-9011982-002, "DC Cook 2 Pressurizer-Surge Nozzle Weld OverlayAnalysis."

AREVA Document 32-9022616-005, "DC Cook Unit 1 Pressurizer Nozzle Design Transient."

AREVA Document 32-9015165-000, "Flow in DC Cook Surge Line"

AREVA Document 32-9038239-000, "North Anna Units 1&2, Pressurizer Surge Nozzle WeldOverlay Analysis."

AREVA Document 32-9034323-003, "North Anna Units 1&2, Pressurizer Surge Weld OverlaySizing Calculation-Surge Nozzle."

AREVA Document 32-9012181-001, "DC Cook Unit 2 Pressurizer Surge Nozzle WeldOverlay Crack Growth Evaluation"

AREVA Document 32-9028241-000, DC Cook Unit 1 Pressurizer Surge Nozzle Weld OverlayCrack Growth Evaluation."

AREVA Document 38-9046827-000, "Additional Engineering Input for North AnnaPressurizer Surge Nozzle Weld Overlays, North Anna Power Station Units I & 2;"

Prepared by: T.. SorensenReviewed by: I.. Straka

Date: 04/2007 Page 16

Date: 04/2007