ML20343A259

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Supplement to Proposed License Amendment Request to Revise the Millstone Unit 2 Technical Specifications for Steam Generator Frequency
ML20343A259
Person / Time
Site: Millstone Dominion icon.png
Issue date: 12/08/2020
From: Mark D. Sartain
Dominion Energy Nuclear Connecticut
To:
Document Control Desk, Office of Nuclear Reactor Regulation
References
20-328B
Download: ML20343A259 (44)


Text

Dominion Energy Nuclear Connecticut, Inc.

5000 Dominion Boulevard, Glen Allen, VA 23060 Dominion Dominion Energy.com Energy December 8, 2020 U.S. Nuclear Regulatory Commission Serial No.: 20-328B Attention: Document Control Desk NRA/SS: RO Washington, DC 20555-0001 Docket No.: 50-336 License No.: DPR-65 DOMINION ENERGY NUCLEAR CONNECTICUT, INC.

MILLSTONE POWER STATION UNIT 2 SUPPLEMENT TO PROPOSED LICENSE AMENDMENT REQUEST TO REVISE THE MILLSTONE UNIT 2 TECHNICAL SPECIFICATIONS FOR STEAM GENERATOR INSPECTION FREQUENCY By letter dated October 8, 2020 (ADAMS Accession No. ML20282A594), Dominion Energy Nuclear Connecticut (DENG) submitted a proposed license amendment request (LAR) to the Nuclear Regulatory Commission (NRC) in accordance with 10 CFR 50.90, to revise Millstone Power Station Unit 2 (MPS2) Technical Specification (TS) 6.26, "Steam Generator (SG) Program," Item d.2. The LAR reflected a proposed change to the required SG tube inspection frequency from every 72 effective full power months (EFPM), or at least every third refueling outage, to every 96 EFPM. Because MPS2 has an 18-month operating cycle, a 96 EFPM frequency essentially requires the inspection to be performed every fifth refueling outage. The NRC staff concluded that additional information was needed to enable the NRC to .proceed with its detailed technical review regarding the acceptability of the proposed LAR.

On November 20, 2020, a teleconference was held between the NRC staff and DENG to discuss the information delineated as necessary to assess the acceptability of the proposed amendment. Based on these discussions, DENG decided to supplement the LAR by providing a revised SG Integrity Condition Monitoring and Operational Assessment (CMOA) for MPS2 Refueling Outage 24 (2R24). A submittal date of December 10, 2020 was agreed upon for the LAR Supplement.

Per communication dated November 20, 2020 (ADAMS Accession No. ML20325A376),

the NRC formally provided DENG an opportunity to supplement the proposed LAR discussed above.

It should be noted that the attachment to this LAR Supplement supersedes the LAR Attachment 3 (submitted in DENG letter dated October 8, 2020) in its entirety. The revised

. MPS2 SG CMOA for 2R24 attached to this LAR Supplement demonstrates that the SG structural and accident induced leakage performance criteria would be met during the five-cycle operating period (i.e. preceding MPS2 Refueling Outage 2R29 in fall 2024), for existing and potential degradation mechanisms. For the two existing degradation mechanisms observed at MPS2 (fan bar wear and foreign object wear), the LAR Supplement attachment justifies there is reasonable assurance that the structural integrity performance criterion will be met for a five-cycle operating period. The conclusions of the no significant hazards evaluation and the environmental considerations evaluation have not changed based on the revised MPS2 SG CMOA attached to this LAR Supplement.

Serial No. 20-328B Docket No. 50-336 Page 2 of 3 Should you have any questions or require additional information, please contact Shayan Sinha at (804) 273-4687.

Respectfully,

~

Mark D. Sartain Vice President- Nuclear Engineering and Fleet Support COMMONWEALTH OF VIRGINIA )

)

COUNTY OF HENRICO )

The foregoing document was acknowledged before me, in and for the County and Commonwealth aforesaid, today by Mr. Mark D. Sartain, who is Vice President - Nuclear Engineering and Fleet Support of Dominion Energy Nuclear Connecticut, Inc. He has affirmed before me that he is duly authorized to execute and file the foregoing document in behalf of that company, and that the statements in the document are true to the best of his knowledge and belief.

<r-+'h

_ _ day of Pult#1ber Acknowledged before me this_(::'.) , 2020.

My Commission Expires: / 2-/31 b1 7

Commitments contained in this letter: None

Attachment:

Revised Millstone Unit 2 Steam Generator Integrity Condition Monitoring and Operational Assessment, Refueling Outage 2R24

Serial No. 20-328B Docket No. 50-336 Page 3 of 3 cc: U.S. Nuclear Regulatory Commission Region I 2100 Renaissance Blvd, Suite 100 King of Prussia, PA 19406-2713 R. V. Guzman NRC Senior Project Manager U.S. Nuclear Regulatory Commission One White Flint North, Mail Stop 08 C2 11555 Rockville Pike Rockville, MD 20852-2738 NRC Senior Resident Inspector Millstone Power Station Director, Radiation Division Department of Energy and Environmental Protection 79 Elm Street Hartford, CT 06106-5127

Serial No. 20-3288 Docket No. 50-336 ATTACHMENT REVISED MILLSTONE UNIT 2 STEAM GENERATOR INTEGRITY CONDITION MONITORING AND OPERATIONAL ASSESSMENT REFUELING OUTAGE 2R24 DOMINION ENERGY NUCLEAR CONNECTICUT, INC.

MILLSTONE POWER STATION UNIT 2

Serial No. 20-3288 Docket No. 50-336 Attachment, Page 1 of 40 Millstone Unit 2 Steam Generator Integrity Condition Monitoring and Operational Assessment Refueling Outage (2R24)

December 2020 Revision 1 1

Serial No. 20-328B Docket No. 50-336 Attachment, Page 2 of 40 Record of Revisions Revision Date Description Issued to Dominion Energy Millstone 0 April 2017 Unit 2 in support of return to Mode 4 power following 2R24 This revision updates the Operational Assessment to evaluate an interval of five operating cycles between steam generator inspections. Technical 1 December 2020 content changes are limited to Section 6 (Operational Assessment) of the report. Deterministic evaluation of foreign object wear beyond the 2R24 RFO for newly identified foreign objects has been deleted because those foreign objects were verified to be removed. Minor consistency changes are made as appropriate throughout the rest of the document.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 3 of 40 Table of Contents

1. Executive Summary ............................................................................................... 4
2. Introduction/ Background ...................................................................................... 5
3. Scope of Activities, Evaluated Degradation Mechanisms, Tube Plugging ............. 6 3.1 Scope of Activities ............................................................................................... 6 3.2 Evaluated Degradation Mechanisms ................................................................... 8 3.3 Tube Plugging ..................................................................................................... 8
4. Inspection Results ................................................................................................ 11 4.1 Channel Head inspections ................................................................................. 11 4.2 Primary Side Tube Inspections .......................................................................... 11 4.3 Secondary Side Inspections .............................................................................. 15 4.4 Summary ........................................................................................................... 17
5. Condition Monitoring Assessment. ....................................................................... 18 5.1 Condition Monitoring Conclusion ....................................................................... 18
6. Operational Assessment ...................................................................................... 23 6.1 Fan Bar Wear .................................................................................................... 23 6.2 Foreign Object Wear .......................................................................................... 26 6.3 Potential Degradation Mechanisms ......................................................... 30 6.4 Leakage Performance Criteria ........................................................................... 31 6.5 Secondary Side Internals Degradation .............................................................. 31 6.6 Operational Assessment Conclusion ................................................................. 31
7. Conclusions .......................................................................................................... 31
8. References ........................................................................................................... 32 ATTACHMENT 1 LPT SG25 ....................................................................................... 33 ATTACHMENT 2 LPT SG26 ....................................................................................... 36 3

Serial No. 20-328B Docket No. 50-336 Attachment, Page 4 of 40

1. Executive Summary This document evaluates the Millstone Unit 2 steam generator (SG) as-found condition (condition monitoring assessment) and the anticipated condition during the next operating period (operational assessment). This evaluation is based on the inspection activities performed in SG25 and SG26 during the 2R24 refueling outage. The condition monitoring (CM) assessment concludes that none of the three SG Program performance criteria (structural integrity, operational leakage, or accident induced leakage) were exceeded during the operating period prior to 2R24. The operational assessment (OA) concludes that there is reasonable assurance that operation of the Millstone Unit 2 SGs throughout the operating period preceding the next examination (up to five fuel cycles) will not cause any of the three performance criteria to be exceeded.

Revision 1 of this report amends the 2R24 OA to evaluate an interval of five operating cycles between SG inspections. Two degradation mechanisms were identified during the 2R24 SG inspections, structure wear (fan bar) and foreign object wear. No new locations of structure wear were identified during the 2R24 SG inspections. Additional calculations were performed which evaluate the projected growth at fan bar wear locations previously identified. Four new locations of foreign object wear were identified during the 2R24 SG inspections. Foreign objects attributed to be the cause of the foreign object wear at each location were confirmed to be removed following secondary side FOSAR (foreign object search and retrieval) activities, arresting the progression of the foreign object wear. The revised OA concludes that there is reasonable assurance that operation of the Millstone Unit 2 SGs throughout the operating period preceding the next examination (up to five fuel cycles) will not cause any of the three performance criteria to be exceeded. The current plant Technical Specifications do not allow for inspection intervals greater than three cycles for plants with SG tubes fabricated with Alloy 690 material.

Dominion Energy has submitted a license amendment request to change this requirement to allow a maximum of five cycles between inspections.

This evaluation was performed in accordance with the following Millstone and industry requirement documents:

  • Millstone Unit 2 Technical Specifications {TS 6.26)
  • Dominion Energy SG Condition Monitoring and Operational Assessment (CMOA) procedure (Ref. [8.21)
  • April 201 O Interim Guidance on the IAG (Ref. [8.9])

Descriptions of specific SG activities performed during 2R24, and the degradation mechanisms targeted by the inspection program are provided in Section 3.0.

Key findings:

  • Tube Degradation o The only tube degradation mechanisms detected were fan bar wear and foreign object wear o No degradation exceeded the 40 % TW technical specification plugging criteria o No indications of lattice support wear were reported
  • Foreign Objects o A variety of foreign objects were located and removed from the SG secondary side o Some foreign objects could not be removed, but these objects were deemed benign 4

Serial No. 20-328B Docket No. 50-336 Attachment, Page 5 of 40

  • Tube Plugging o Plugging was not required or performed during the 2R24 outage
  • Secondary Side Inspections o Identified no concerns relative to long-term performance and reliability
2. Introduction / Background NEI 97-06 was developed to provide the industry with guidance and standards for assessing the structural and leakage integrity of steam generator tubes and to provide the basis for plant specific SG integrity programs. NEI 97-06 and the Millstone Unit 2 Technical Specifications (TS 6.26) establish three specific steam generator performance criteria:
  • Structural Integrity - Margin of 3.0 against burst under normal steady state power operation and a margin of 1.4 against burst under the most limiting design basis accident. Additional requirements are specified for non-pressure accident loads.
  • Accident Induced Leakage - Leakage shall not exceed the value assumed in the limiting accident analysis (150 GPO per SG).

This Technical Evaluation constitutes a condition monitoring and operational assessment of each tube degradation mechanism identified during the 2R24 primary and secondary side inspections. The CM assessment is performed to verify that the condition of the tubes, as reflected by the inspection results, meets the above performance criteria. Indications of degradation, if found, are evaluated to confirm that the safety margins against leakage and burst were not exceeded at the end of the previous operating cycle. The results of the condition monitoring evaluation are used as a basis for the OA which demonstrates that the anticipated performance of the steam generators, including any degraded tubes remaining in service, will not exceed the performance criteria for leakage and tube burst during the next operating period.

A pre-outage Degradation Assessment (Ref. [8.4]) was performed to identify existing degradation mechanisms as well as degradation mechanisms which could potentially occur in the near term within the Millstone Unit 2 steam generators. The assessment also identified the appropriate inspection scope, techniques to be utilized during the subject inspection, and applicable detection and sizing information for the identified degradation mechanisms. The 2R24 inspections were performed in accordance with the Degradation Assessment.

All of the acquired eddy current data was analyzed by two independent analysis paths: manual primary analysis and secondary computerized analysis (ZETEC RevospECT). All results were passed through a resolution process. Any discrepancies between the two analysis teams were resolved by a third team of analysts (primary and secondary resolution analysts). The BWXT Lead Level Ill coordinated the analysis process and provided additional' analysis expertise as required. The Dominion Energy ET Level Ill and an Independent Qualified Data Analyst (IQDA), a role defined within the EPRI PWR SG Examination Guidelines (Ref. [8.5]), served in oversight roles. The inspections were performed per the requirements of Ref. [8.5] and all inspection techniques utilized for degradation detection and/or sizing were qualified per these guidelines.

The Millstone Unit 2 Analysis Reference Manual (Ref. [8.6]), updated and approved prior to commencement of the inspection, served as the principal guidance document for data evaluation. As with past practice, Millstone Unit 2-specific examination technique specification sheets (ETSS) were used in conjunction with Ref. [8.6] to summarize instructions relative to acquisition and analysis setups and analysis screening parameters.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 6 of 40 The naming convention of the steam generators in this report has been changed from what has been used in recent outages. The naming convention has been inconsistent in the past and this has caused some confusion among the various Dominion Energy and vendor organizations. In recent outages, the steam generators have been called SG1 and SG2 in the various reports including the CMOA. The steam generators are now designated as SG25 (formerly SG1) and SG26 (formerly SG2). These designations are consistent with the original manufacturing naming convention.

3. Scope of Activities, Evaluated Degradation Mechanisms, Tube Plugging Scope of Activities The SG activities planned for 2R24 were described in the Degradation Assessment (Ref. [8.4]) and are summarized below.

3.1.1 Primary Side The following primary side activities were performed in SG25 and SG 26 during the 2R24 outage.

  • Visual examination of both channel heads (as-found I as-left), specifically including the divider plate/ tubesheet interface, and previously installed tube plugs.
  • Eddy current bobbin probe and rotating +Point' probe examinations as described in Table 3-
1. Table 3-1 provides a breakdown of the actual number of primary side tube examinations performed during the outage including additional tests necessary to bound foreign objects and to address unresolved bobbin indications. Table 3-1 also summarizes the results of the examination.

3.1.2 Secondary Side The following secondary side activities were performed in SG25 and SG26 during the 2R24 outage.

  • Chemical cleaning of the secondary side using AREVA's Deposit Minimization Treatment (DMT) process
  • High pressure sludge lancing.
  • Post-sludge lancing visual examination of top-of-tubesheet annulus and no-tube lane to assess as-left material condition and cleanliness, and to identify and remove any retrievable foreign objects (FOSAR).
  • Visual investigation of accessible locations having eddy current indications potentially related to foreign objects, and removal of retrievable foreign objects.
  • Steam drum visual inspections to evaluate the material condition and cleanliness of key components such as moisture separators, drain systems, and interior surfaces.

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Serial No. 20-3288 Docket No. 50-336 Attachment, Page 7 of 40 Table 3-1 Millstone 2R24 ECT Summary SG25 SG26 Total Number of Installed Tubes 8523* 8523 17046 Number of Tubes In Service Prior to 2R24 8504 8510 17014 Number of Tubes Inspected F/L w/Bobbin Probe** 8504 8510 17014 Previously Pluaaed Tubes 19* 13 32 Number of Tubes Incomplete w/Bobbin Probe due to Obstruction 0 0 0 Number of Exams with +Point' (Total) 2623 2702 5325

  • Hot Leq Tubesheet TSH +3/-3 Periphery 1256 1269 2525
  • Hot Leq Tubesheet PTE 1 0 1
  • Hot Leq Tubesheet 01 HTSH 3 7 10
  • Hot Leq Tubesheet PLP Bounding 18 49 67
  • Cold Leq Tubesheet TSC +3/-3 Periphery 1245 1253 2498
  • Cold Leq Tubesheet 01 CTSC 0 4 4
  • Cold Leq Tubesheet TSC +10/-3 11 0 11
  • Cold Leg Tubesheet PLP Bounding 22 30 52
  • Hot Leq Special Interest 34 39 73
  • U-Bend Special Interest 7 5 12
  • Cold Leg Special Interest 6 11 17
  • Hot Leq Additional RPC 20 22 42
  • Cold Leq Additional RPC 0 13 13 Tubes with Max FB Wear > 40 % 0 0 0 Tubes with Max FB Wear >20% but <40% 0 0 0 Tubes with Max FB Wear <20% 2 2 4 Tubes with Max SVI /VOL/ WAR> 40 % 0 0 0 Tubes with Max SVI /VOL/ WAR>20% but <40% 1 13 14 Tubes with Max SVI /VOL/ WAR<20% 0 2 2 Total Tubes Pluaaed as a Result of this Inspection 0 0 0
  • One tubesheet location in SG25 (R57 C156) was not drilled in the cold leg tubesheet. The hot leg hole for this tube was plugged with a welded plug. Although this location was never tubed, it is included in the counts of installed tubes and plugged tubes.
    • A number of tubes were examined in hot leg / cold leg segments to achieve full length coverage.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 8 of 40 3.2 Evaluated Degradation Mechanisms Prior to this outage, only fan bar wear and foreign object wear had been identified in the MPS2 SGs, therefore these degradation mechanisms were the only mechanisms classified in the DA (Ref. [8.4])

as "existing." As discussed in Ref. [8.41, one other mechanism was classified as "potential" (lattice support wear). It is primarily "existing" and "potential" damage mechanisms that were targeted by the 2R24 inspection.

It is a requirement of the Millstone SG program that all tube locations identified as currently experiencing (i.e., "existing") or potentially susceptible to degradation (i.e., "potential"), be examined with qualified NOE techniques within specific time periods. These periods are prescribed in TS 6.26.d.2. The first inspection period of the MPS2 SGs had a duration of 144 EFPM and ended after the 2R20 outage. The second inspection period has a duration of 120 EFPM and started during Cycle

21. This was the third steam generator inspection in the second inspection period but was the second inspection of each SG.

Table 3-2 summarizes the examinations performed to date and their compliance with the inspection period requirements. For example, in the table an entry of 200 indicates that "200%" of the tubes were examined within the second period. More succinctly, it means that each tube was examined at least twice within the given period. As shown in the table, all tubes were inspected at least four times time during the first period. In addition, all in-service tubes have already been inspected twice during the second inspection period thus meeting the minimum sampling requirements for the second inspection period.

3.3 Tube Plugging Based on the inspection results, tube plugging was not required or performed during the 2R24 outage.

Table 3-3 provides a summary of the MPS2 tube plugging to date.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 9 of 40 Table 3 Summary of SG Inspection Sampling Through the 2R24 Outage (TS 6.26)

FOWear Lattice Support Wear FB Wear Degradation Mechanism (potential) (potential) (potential)

Location Affected TSH toTSC Support Intersections FB Intersections Number of Tubes in Susceptible Region 8,523 8,523 8,523 Principal ECT Probe for Detection Bobbin1A1 Bobbin Bobbin Steam Generator SG25 SG26 SG25 SG26 SG25 SG26 SG EFPM Outage Date Since CUMULATIVE SAMPLE EXAMINED (PERCENT)

Period Start 2R12 Oct-94 0.0 29 28 29 28 29 28 Mid Cycle 13 Jun-97 6.0 100 53 100 53 100 53 2R13 Apr-00 16.0 153 153 153 2R14 Mar-02 35.8 200 200 200 2R15 Oct-03 52.7 253 253 253 2R16 Apr-05 68.6 300 300 300 (mid-period) 2R17 Oct-06 84.8 2R18 Apr-08 101.3 400 353 400 353 400 353 2R19 Oct-09 116.9 2R20 Apr-11 133.0 500 453 500 453 500 453 (last in period) 2R21 Oct-12 5.0 2R22 Apr-14 21.1 100 100 100 2R23 Oct-15 37.5 100 100 100 2R24 Apr-17 54.0 200 200 200 200 200 200 A) FO and FO wear detection is augmented with secondary side visual exams and top of tubesheet (TTS) +Point/Array probe sampling.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 10 of 40 Table 3 Millstone SG Tube Plugging Attributes Preservice Oct-94 May-97 Jun-00 Feb-02 Oct-03 Apr-05 Oct-06 Apr-08 Oct-09 Apr-11 Oct-12 DATE 2R11 2R12 MCO13 2R13 2R14 2R15 2R16 2R17 2R18 2R19 2R20 2R21 SG EFPY 0.0 1.3 1.8 2.6 4.3 5.7 7.0 8.4 9.8 11.1 12.4 13.7 SGID 25 26 25 26 25 26 25 26 25 26 25 26 25 26 25 26 25 26 25 26 25 26 25 26 FO Wear ?,40 %TW 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2 0 0 0 0 0 0 0 Unretrieved FO with or 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 2 0 0 10 11 0 0 w/o Wear <40 %TW FOWear<40 %TW 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5 0 0 0 0 0 0 0 w/o FO Present Lattice Support Wear 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

& Fan Bar Wear lnspectability 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Other 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Sub-Total 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 8 2 0 0 10 11 0 0 TOTAL 1 0 0 0 0 0 0 0 10 0 21 0 Apr-14 Oct-15 Apr-17 Oct-18 Total per DATE 2R22 2R23 2R24 2R25 SG SG EFPY 15.1 16.4 17.8 SGID 25 26 25 26 25 26 25 26 25 26 Total Plugging by Category FO Wear .:=:,40 %TW 0 0 0 0 0 0 2 0 2 FO Wear>40 %TW Unretrieved FO with or Unretrieved FO with or 0 0 0 0 0 0 11 13 24 w/o Wear <40 %TW w/o Wear <40 %TW FO Wear <40 %TW FO Wear <40 %TW 0 0 0 0 0 0 5 0 5 w/o FO Present w/o FO Present Lattice Support Wear Lattice Support Wear 0 0 0 0 0 0 0 0 0

& Fan Bar Wear & Fan Bar Wear lnspectability 0 0 0 0 0 0 0 0 0 lnspectability Other 0 0 0 0 0 0 1 0 1 Other Sub-Total 0 0 0 0 0 0 0 0 19 13 TOTAL 0 0 0 0 32 D SG Inspected 10

Serial No. 20-328B Docket No. 50-336 Attachment, Page 11 of 40

4. Inspection Results This section provides the results of both the primary and secondary side inspections performed during the 2R24 outage. In general, only the specific results that relate to the condition monitoring assessment and the operational assessment will be discussed herein. The implications of these results with respect to the CMOA are discussed in Sections 5.0 and 6.0, respectively.

4.1 Channel Head inspections The hot and cold leg channel heads stay well welds and divider plate welds were visually examined in SG25 and SG26 prior to the installation of eddy current probe manipulators. The examination revealed no evidence of divider plate or staywell weld degradation, and no foreign objects were identified.

Plug visual examinations were performed on all previously installed plugs in SG25 and SG26. No indications of plug degradation, leakage, or misplacement were identified.

4.2 Primary Side Tube Inspections The primary side inspection scope was performed, and a brief tally of the number of indications reported is provided in Section 3.1.1 and Table 3-1. Results of potential significance to SG integrity are discussed in this section. Table 4-1 identifies all indications of tube degradation identified during the 2R24 examination.

4.2.1 lnspectability Issues No indications of signal interference prevented the effective examination of tube regions planned for examination during 2R24.

4.2.2 Geometric Discontinuities Dents (DNTs), bulges (BLGs), and tubesheet overexpansions (OXPs and OVRs) result in elevated residual stresses and, in susceptible tube materials, have been implicated in the development of stress corrosion cracking (SCC). Although SCC is not considered to be a potential degradation mechanism in the MPS2 A690TT tubing, sampling inspections of these geometric discontinuities with

+Point probes were performed during 2R24. None of these examinations revealed tube degradation associated with the discontinuities.

4.2.3 Fan Bar Wear The primary examination technique for fan bar wear detection and sizing is the bobbin coil probe (ETSS 96041.3). A total of four fan bar wear indications in four tubes were reported during the examination; two indications in each SG (Table 4-1). All four have been reported during previous outage inspections 11

Serial No. 20-328B Docket No. 50-336 Attachment, Page 12 of 40 Table 4 2R24 Tube Degradation Summary Depth Axial Circ Maximum Reported Signal Present Foreign Length Length Depth Prior Initially Prior to Current Object In-Situ Plugged &

SG Row Col Location ETSS (in) (in) 2R24 Outage Reported Outage? Cause Remaining? Tested? Stabilized?

12%TW Fan Bar 25 40 155 F06-1.76" 96041.3 3.15* N/A 13%TW 2R14 Yes N/A No No 2R23 Wear 14%TW Fan Bar 25 140 93 F08- 0.66" 96041.3 3.15* N/A 19%TW 2R14 Yes N/A No No 2R23 Wear NDD Foreign 25 92 143 TSH+l0.91" 27901.1 0.24 0.37 23%TW 2R24 Yes No No No 2R23 Object Wear 27%TW Foreign 26 28 5 TSC+21.65" 27901.1 0.28 0.43 25%TW 2R15 Yes No No No 2R22 Object Wear 25%TW Foreign 26 29 4 TSC+22.2" 27901.1 0.27 0.43 26%TW 2R18 Yes No No No 2R22 Object Wear 8%TW Fan Bar 26 37 120 F07- 0.83" 96041.3 3.15* N/A 12%TW 2R15 Yes N/A No No 2R22 Wear 11%TW Foreign 26 44 5 TSC+17.91" 27902.1 0.43 0.38 10%TW 2R20 Yes No No No 2R22 Object Wear 24%TW Foreign 26 59 10 TSC+ 17.33" 27901.1 0.38 0.43 23%TW 2R15 Yes No No No 2R22 Object Wear 20%TW Foreign 26 98 143 TSH+8.76" 27901.1 0.33 0.37 20%TW 2R18 Yes No No No 2R22 Object Wear 15%TW Fan Bar 26 99 80 F06+1.28" 96041.3 3.15* N/A 13%TW 2R15 Yes N/A No No 2R22 Wear 12%TW Foreign 26 118 41 TSH+12.81" 27902.1 0.48 0.37 12%TW 2R18 Yes No No No 2R22 Object Wear 24%TW Foreign 26 119 42 TSH+12.97" 27903.1 0.38 0.43 29%TW 2R18 Yes No No No 2R22 Object Wear NDD Foreign 26 122 123 TSH+2.53" 27901.1 0.33 0.54 34%TW 2R24 No No No No 2R22 Object Wear 22%TW Foreign 26 123 46 TSH+18.15" 27903.1 0.23 0.37 25%TW 2R15 Yes No No No 2R22 Object Wear 26%TW Foreign 26 124 45 TSH+19.27" 27903.1 0.38 0.32 31%TW 2R18 Yes No No No 2R22 Object Wear NDD Foreign 26 124 123 TSH+l.77" 27901.1 0.38 0.43 36%TW 2R24 No No No No 2R22 Object Wear 32%TW Foreign 26 125 48 TSH+ 19.53" 27903.1 0.33 0.43 36%TW 2R15 Yes No No No 2R22 Object Wear NDD Foreign 26 125 122 TSH+l.36" 27902.1 0.53 0.37 23%TW 2R24 No No No No 2R22 Object Wear 34%TW Foreign 26 126 49 TSH+19.97" 27903.1 0.49 0.48 39%TW 2R15 Yes No No No 2R22 Object Wear 29%TW Foreign 26 128 107 TSH+0.06" 27901.1 0.28 0.37 26%TW 2R20 Yes No No No 2R22 Object Wear

. Conservative assumed length  :

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 13 of 40 4.2.4 Foreign Objects and Foreign Object Wear One of the most significant potential threats to tube integrity found during 2R24 was foreign object (FOs). This section provides a discussion of the FO degradation mechanism for 2R24.

A comprehensive approach was applied to foreign objects or foreign object wear during 2R24. The BWXT Loose Parts Tracker (LPT) database contains information on foreign objects detected by either eddy current or by visual examination techniques during 2R24. Prior to the 2R23 examination, the AREVA Foreign Objects Tracking System (FOTS) database for the Millstone Unit 2 SGs was used to develop a list of any foreign object locations that required evaluation during the examination. Based on history and the potential for wear, the appropriate examination scope was planned and documented in the DA.

The +Point' probe was used to perform a 50% examination of the outer 6 rows of the hot and cold leg periphery and open tube lane. Since foreign objects normally contact more than a single tube, the

+Point' probe examination provided an improved probability of detecting foreign objects or foreign object wear within this band. Due to the tube spacing in the tri-pitch steam generator, few foreign objects are capable of traveling more than a few rows into the tube bundle. The cross flow velocity of the incoming feedwater, and consequently the potential for foreign object wear, is also highest within this zone. Compared to the bobbin exam, the +Point examination provides a significant improvement in the probability of detection of foreign objects that are most likely to cause wear and FO wear within this region.

During the 2R24 examination, any new confirmed Possible Loose Part (PLPs), PLP related indications, or new FO wear indications reported by the eddy current examination were investigated by the Secondary Side Inspection (SSI) crew as far as possible and any new objects identified by SSI within the tube bundle region were tested by the +Point' eddy current technique. When possible the FO's were removed by FOSAR. The combined examinations were coordinated through the use of the LPT database. Some of the foreign objects identified during this inspection are shown in Figure 4-1 while Figure 4-2 shows foreign objects that were removed.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 14 of 40 Figure 4-2 -Foreign Objects Retrieved Attachment 1 and 2 contain a full listing of the historical and emergent foreign object items addressed in SG 25 and SG26, respectively, during 2R24. A wide range of cases were addressed as will be presented below.

4.2.5 Summary of Foreign Object Wear A comprehensive program was defined for detection of foreign objects and foreign object wear. This program consisted of planned examinations for known locations, a 50% examination of the outer six rows with the +Point' probe, a 100% bobbin coil examination, bounding examinations with +Point',

SSI of the top of tubesheet annulus and bundle periphery and FOSAR as required.

Per Table 4-1, SG 25 had one tube wear location that was newly detected with a wear depth of 23% in tube R92 C143, located approximately 11" above the hot leg tubesheet.

  • A review of previous bobbin data indicates that this wear has been present in this tube since 1997; however, this was the first time that a +Point probe had been used at this location.
  • One tube adjacent to this tube, R90 C143, and a tube adjacent to that tube but not adjacent to the worn tube, R89 C144, both contained PLP indications at a similar elevation to the wear indication on R92 C143, but neither:tube had any indications of wear identified by +Point' coil.

A review of previous +Point' and bobbin data in these two tubes indicates that this loose part has been present at this location since 2008.

  • A review of the location by SSI confirmed the presence of the part between R90 C143 and R89 C144. However, it could not be accessed for removal.
  • Since the wear indication has been present since 1997, and the nearby PLP has been present since 2008 with no movement or initiation of wear in the associated tubes, this object does not represent a threat to tube integrity over the next five cycles.

Also per Table 4-1, SG 26 had 12 previously reported foreign object wear locations with no significant change in sized depth from 2R22. SG 26 also reported three new wear locations in tubes R122 C123 (34% TW), in R124 C123 (36% TW) and in R125 C122 (23%tw). None of these locations had an indication of a foreign object and FOSAR found no part at any of these locations.

14

Serial No. 20-328B Docket No. 50-336 Attachment, Page 15 of 40 With no growth continuing in the historical foreign object wear locations and no part at the new foreign object wear locations, these tubes do not represent a threat to tube integrity over the next five cycles.

The combination of the 100% bobbin coil examination of the full tube bundle, the +Point' examination of the outer six rows of the periphery and open tube lane and the SSI examination of the tubesheet annulus and periphery, there is reasonable assurance that there are no currently existing parts within the tube bundle high flow region that could threaten tube integrity over the next five cycles.

4.2.6 Inspection Result Classification Category The inspection results from SG 25 and SG26 were classified as category C 1 per Section 3. 7 of the Examination Guidelines (Ref [8.5]) with respect to fan bar wear. Specifically, there were no fan bar wear indications equal to or greater than 40 %TW and no previously reported fan bar wear indications grew more than 10%TW since the last inspection (Table 4-1). Less than 5% of the inspected tubes were degraded by fan bar wear.

Similarly, the inspection results for SG 25 and SG 26 were classified as C1 with respect to foreign object wear. Specifically, there were no foreign object wear indications equal to or greater than 40

%TW and no previously reported foreign object wear indications grew more than 10%TW since the last inspection (Table 4-1). Less than 5% of the inspected tubes were degraded by foreign object wear.

4.3 Secondary Side Inspections Secondary side structures and material conditions must be evaluated to assess any potential impact on SG tube integrity. Any foreign objects, or degradation of internals that could produce foreign objects, are important because tube integrity could be impacted. Visual examinations were performed during this outage to develop the information needed for the evaluation. FOSAR results of potential significance to tube integrity were discussed above in Section 4.2.4. This section provides an overall summary of observations made during the secondary side examination.

4.3.1 Steam Drum A visual examination of steam drum components was performed in SG25 and SG26. In the areas examined, sludge accumulation was light, with a harder underlying crystalline coating of sludge noted.

Due to water clarity issues following refill after DMT, visual inspection of the U-bend structures (arch bars, J-tabs and fan bars) was not possible. Sludge deposits on the primary and secondary moisture separators were light and tightly adhering. Very little deposit was removed from these surfaces when rubbed with a gloved hand. The primary separators examined were in good condition with no evidence of material degradation. The curved arm assemblies within the primary separators were inspected and found to be in good condition. The edges of the steam outlet to the assemblies were sharp, indicating no noticeable flow assisted corrosion. Evidence of early stage flow assisted corrosion of the secondary moisture separators was noted. Severe degradation of these separators can eventually lead to the introduction of loose parts that may migrate to the tube bundle. However, based on limited operational wear observed through 2R24, significant structural degradation is not expected to occur over the next five cycles of operation. This condition should be monitored during future outages.

15

Serial No. 20-3288 Docket No. 50-336 Attachment, Page 16 of 40 Typical separator baseplate Separator baseplate with early stage flow assisted corrosion 4.3.2 Top of Tubesheet Cleanliness Post-lancing visual examinations in SG25 and SG26 identified no loose sludge in the annulus at the top of tubesheet. The no-tube lane and staywell regions were clear as well. The blowdown flow holes in the tubesheet showed no evidence of flow induced erosion. Due to the application of DMT, a total of 2608 pounds of deposit was removed from SG 25 and a total of 2584 pounds of deposit ""'.as removed from SG 26 (See Table 4-2). The 1st support lattice, shroud, and shroud support components examined were in good condition. Jacking studs showed no indication of movement between the shell and shroud. (See Figure 4-4) 16

Serial No. 20-328B Docket No. 50-336 Attachment, Page 17 of 40 Table 4-2 DMT Deposit Removal Quantities Fe Step Pass Step Cu Step LVRs/FVR TOTALS Magnetite Removed (lbs) 1442 291 213 16.1 1963 SG 25 Cu Removed (lbs) 0.6 3.3 11.6 0.7 16.2 Lancing (lbs) 629 Total (lbs) 2608.2 Magnetite Removed (lbs) 1442 291 213 16.1 1963 Cu Removed (lbs) 0.6 3.3 11.6 0.7 16.2 SG 26 Lancing (lbs) 605.5 Total (lbs) 2584.7 Grand Total (lbs) 5192.9 There was a light dusting of sludge noted in the annulus of both SGs. Discoloration of the outer surface of most tubes was noted. This was attributed to the application of DMT, and does not represent a deleterious condition. The no-tube lane and staywell area was clean and the blowdown flow holes showed no evidence of erosion. The 1st support lattice, shroud, and shroud support components examined were in good condition with no evidence of material degradation. Jacking studs showed no indication of movement.

4.4 Summary Consistent with expectations documented in the DA (Ref. [8.41), the only conditions of potential significance to SG integrity identified during the 2R24 SG examinations were secondary side foreign objects, foreign object tube wear, and fan bar tube wear. The significance of these findings with respect to the condition monitoring assessment and operational assessment are discussed in the sections that follow.

Figure 4 Lower Bundle Components 17

Serial No. 20-328B Docket No. 50-336 Attachment, Page 18 of 40

5. Condition Monitoring Assessment The condition monitoring (CM) assessment is an evaluation of tube structural and leakage integrity during the operating period since the last inspection. The CM is based on current inspection results.

As discussed in Section 4.0 and presented in Table 4-1, the modes of tube degradation detected were foreign object wear and fan bar wear. The sizing techniques used to determine the dimensions of the flaws listed in Table 4-1 are also identified in the table. The sizing performance of the techniques, along with the reported flaw dimensions were used to evaluate the structural integrity of the tubes.

A review of the screening guidance of Ref. [8. 7] provides the basis for concluding that non-pressure accident loads are not limiting for MPS2 degradation located beyond the constraint of the tubesheet.

The reference states that circumferential degradation and the circumferential component of volumetric degradation is limiting with respect to non-pressure loads and advises that non-pressure loads are not significant contributors to burst for tubes with flaws that are below the top tube support and which are less than 270° in circumferential extent, or for flaws located on the tube flanks within the u-bend (e.g.,

fan bar wear). All flaws identified during this outage meet this criteria and therefore it is appropriate to use the EPRI Flaw Handbook (Ref. [8.10]) methods, which consider pressure loading only, to establish the structural limits for all of the MPS2 tube degradation identified.

To perform the CM for fan bar wear and foreign object wear, the limiting degradation size must be compared with an appropriate structural integrity limit which accounts for the material property uncertainty, model uncertainties and NOE sizing uncertainties. Since the circumferential extent of all of the indications listed in Table 4-1 can be shown to be <135°, it is appropriate to use the EPRI Flaw Handbook (Ref. [8.1 O]) "Part-Throughwall Axial Volumetric Degradation" flaw model to evaluate the CM limit. Using this model as implemented by the EPRI FHC (Ref. [8.1 O]), CM limit curves were developed in the Degradation Assessment [8.4] for each flaw type and sizing ETSS.

Figures 5-1 through 5-4 provide the CM limit curves for flaws sized with ETSSs 96004.3, 27901.1, 27902.1, and 27903.1 respectively. The CM curves represent the structural performance criteria derived by conservatively accounting for material property uncertainties, model uncertainties, and NOE depth sizing uncertainties. The uncertainties were combined using Monte Carlo techniques as described in Ref. [8.7].

The figures also display the length and depth of each flaw. Because each flaw plotted in Figures 5-1 through 5-4 lies below the CM limit curve, it is concluded that the structural performance criteria set forth in the MPS2 Technical Specifications was not exceeded by any of the evaluated flaws. This also provides reasonable assurance that none of these flaws would have leaked under accident conditions.

j No primary-to-secohdary SG tube leakage was reported during the previous qperating period; therefore, the operational leakage performance criteria was not exceeded durirg the operating period preceding this outag~. \

5.1 Condition Monitoring Conclusion Based upon the evaluations documented in this report, all degradation identified during the 2R24 inspection satisfied condition monitoring requirements for SG tube structural and leakage integrity.

Further, the conditions observed during 2R24 also serve to validate the conclusions of all previous outage operational assessments with respect to projected compliance with technical specification SG performance criteria. Specifically, the 2R24 findings are consistent with the assumptions, expectations, and projections documented in previous operational assessments.

18

Serial No. 20-3288 Docket No. 50-336 Attachment, Page 19 of 40 Figure 5-1 Acceptance Limits for Fan Bar Wear ETSS 96041.3 100 _! _l____l__i __ ].~ -i--,- i__J __:_c-7 I___ L_J-:--;-.-!--! I i ~~-~--~- I I I_~~-~~~---~-~~~ - ~ ~ -  :=-:_J_I__ :

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 20 of 40 Figure 5-2 Acceptance Limits for Foreign Object Wear ETSS 27901.1 100 J_ _I __ I =r:::] _ _ l _1 t_i=:=_, _L_

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 21 of 40 Figure 5-3 Acceptance Limits for Foreign Object Wear ETSS 27902.1 100 J___J_[ L_J_l-l--1--,-__* _I ~ ~ - - - - ~ - - .... I f - .-,

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Serial No. 20-3288 Docket No. 50-336 Attachment, Page 22 of 40 Figure 5-4 Acceptance Limits for Foreign Object Wear ETSS 27903.1 100 I I I I

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 23 of 40

6. Operational Assessment The operational assessment (OA) must demonstrate that the structural integrity performance criteria will not be exceeded prior to the next scheduled examination in either of the Millstone Unit 2 SGs. The MPS2 technical specifications limit the period between inspections to a maximum of three fuel cycles for an individual SG. Hence, this amended OA supplemented with the LAR evaluates the limiting operating interval (i.e., five fuel cycles) for both SGs based upon the current outage primary and secondary side inspection results. Per Table D-1 of the Degradation Assessment [8.4], the expected operating interval between 2R24 and 2R29 will be 78 EFPM or 6.5 EFPY. For this analysis, the five-cycle inspection interval will be conservatively assumed to be 7.0 EFPY.

Given the superior resistance of the A690TT tube material to corrosion and anticipated continued diligence in chemistry monitoring and control, there is minimal near term threat of corrosion initiation.

Consistent with Ref. [8. 7], this operational assessment addresses degradation mechanisms known to exist in the MPS2 steam generators including fan bar wear and foreign object wear, as well as relevant potential degradation mechanisms such as lattice support wear, tube-to-tube wear, and thinning.

The first two subsections below assess future fan bar wear and foreign object wear against the structural performance criteria. The third subsection assesses future compliance with accident induced and operational leakage performance criteria and the fourth subsection considers secondary side internals degradation.

6.1 Fan Bar Wear For the purposes of this OA, future fan bar wear can be grouped into two categories:

  • Wear that currently exists in in-service tubes, whether detected during 2R24 or not
  • Wear which will initiate during the next five fuel cycles.

Because wear which has already initiated will continue to grow, it is assumed to be more limiting in the future than wear which has not yet initiated. This evaluation will focus on wear flaws that have already initiated. This requires consideration of NOE sizing uncertainty, NOE probability of detection (POD), and the rate of future wear flaw growth.

6.1.1 Beginning of Cycle (BOC) Fan Bar Wear Depth The beginning of cycle fan bar wear depth is an upper bound estimate of the depth of wear left in-service prior to the next operating interval. This value accounts for the fact that NOE techniques have an imperfect probability of detection, and must account for known flaws left in service following the tube inspection. Consistent with Ref. [8.7], Table 8-1, the most limiting BOC fan bar wear depth to be used in*

this analysis will be the largest flaw left in service. In the technique qualification program (ETSS 96041.3) all flaws ranging in depth from 4 %TW to 90 %TW were detected. Due to the high POD for fan bar wear detection, undetected flaws are not an issue for structural integrity.

The deepest fan bar wear indication returned to service measured 19%TW with a bobbin probe. As shown in Table A-1 of the Degradation Assessment [8.4], the NOE (Non-Destructive Examination) sizing parameters for the bobbin technique (ETSS 96041.3) are a slope of 0.99 and an intercept of 2. 73% TW.

Using the slope and intercept, a best estimaternal depth of 21.5% TW (19 x 0.99 + 2. 73) is obtained for an indication with a measured depth of 19% TW.

23

Serial No. 20-328B Docket No. 50-336 Attachment, Page 24 of 40 A standard error of 3.36% TW is the uncertainty associated with this technique. Further adjusting this value upward to an upper 95th percentile gives an NOE uncertainty of 5.53% TW (3.36 x 1.645). Adding this uncertainty to the best estimate value of 21.5% TW yields a bounding real depth of 27% TW (21.5 +

5.5) for indications returned to service.

6.1.2 Fan Bar Wear Growth Table 6.1 below provides wall loss measurement data for each MPS2 SG tube exhibiting structural wear to date.

Table 6.1: SG Tube Wall Loss Measurement Data Percent Through Wall Each Outage Row Column SIG 2R14 2R15 2R16 2R18 2R20 2R22 2R23 2R24 40 155 1 9 9 11 11 12 13 140 93 1 9 9 12 12 14 19 37 120 2 6 9 9 8 12 99 80 2 11 11 15 15 13 Only four tubes, (two in each SG), have any recorded wear at support structures and all four wear indications are minor fan bar wear. No wear has been detected at the lattice grid support. Fan bar wear was first detected in SG25 during 2R14 (March 2002) and in SG26 during 2R15 (October 2003).

Apparent growth rates of indications without prior detection could represent a detection issue and not a growth rate issue. In other words, these indications could have existed during previous examinations at degradation depths below detectability or the reporting threshold, making growth rate estimates erroneously high. Additionally, the sample of tubes exhibiting fan bar wear is too small to be statistically significant. Short cycle lengths can generate large NOE measured growth rates, simply because actual growth rates are small in comparison to the NOE sizing variability. Table 6.1 above provides wall loss measurement data for each MPS2 SG tube exhibiting structure wear to date.

In some instances, the effects of NOE sizing variability is evidenced by the apparent negative growth rates. Therefore, it is more reliable to establish growth rates by trending the progression of the degradation over multiple inspections.

24

Serial No. 20-328B Docket No. 50-336 Attachment, Page 25 of 40 A summary of the growth rates for fan bar wear is provided in Table 6.2. The highest average growth rate observed between the two MPS2 SGs over the time from first detection to the most recent inspection was 0.74% TW/EFPY. While the inspection results of the MPS2 SGs support the use of a 0.74% TW/EFPY growth rate value, the following evaluation of the 2R24 CMOA will assume 3% TW/EFPY. This wear rate is conservative and easily bounds the wear observed in the small sample of tubes that exhibit fan bar wear.

Table 6.2 - Fan Bar Wear Growth Rates SG Row Col Location Maximum Size When First Average Growth Depth 2R24 Detected Rate Since Detection 1 40 155 F06 13%TW 9% TW(2002) 0.30% per EFPY 1 140 93 F08 19%TW 9% TW (2002) 0.74% per EFPY 2 37 120 F07 12%TW 6% TW (2003) 0.50% per EFPY 2 99 80 F06 13%TW 11 % TW (2003) 0.17% per EFPY MPS2 utilizes an 18-month operating cycle. A 96-month operating interval will result in a maximum of four outages without SG examinations being performed (i.e. an inspection every fifth refueling outage). MPS2 has averaged 1.371 EFPY per operating cycle. Conservatively assuming 1.4 EFPY per operating cycle and applying a growth rate of 3.0% TW/EFPY over a five-cycle bounding inspection interval of seven EFPY, gives a total growth of 21.0% TW (3.0% x 7 EFPY) until the next planned inspection. Further applying this total growth to the bounding depth of 27% TW gives a projected 2R29 depth of 48% TW (27

+ 21.0) for indications detected and returned to service during the 2R24 outage.

The allowable real depth Structural Limit (SL) for fan bar wear with a bounding length of 3.20" is 50.2%

TW as shown in the ETSS 96041.3 OD Axial Thinning Evaluation found in Appendix C of the 2R24 DA (Reference 8.6). The projected real depth of 48.0 % TW was calcu.lated with various conservatisms (as described above), and is within the allowable real depth of 50.2% TW; therefore, there is reasonable assurance that the structural integrity, operational leakage, or accident induced leakage .performance criterion will be met for this mechanism for the five cycles of operation (at which time, another inspection and OA will be performed).

  • 25

Serial No. 20-328B Docket No. 50-336 Attachment, Page 26 of 40 6.2 Foreign Object Wear Foreign object wear is the primary degradation mechanism of concern at Millstone Unit 2 based on previous plugging history. Although several new foreign object wear indications were reported during the 2R24 outage, many foreign objects were visually confirmed and removed. Many of these foreign objects were in locations where tube degradation is possible.

The 2R24 inspection scope for foreign objects and associated wear was extensive and included both visual and eddy current inspections. Visual inspections included both the annulus and no-tube lane at the top of the tubesheet in both steam generators. These visual inspections included looks into the tube bundle at all peripheral and no-tube lane locations. The eddy current examinations included full length bobbin probe examinations of all tubes, 50% rotating probe examinations of an approximate six tube deep periphery at the top of tubesheet (+/- 3 in) in both legs, and bounding rotating probe examinations of potential foreign object associated indications. All evidence of foreign objects and foreign object wear was tracked and evaluated in the BWXT Loose Parts Tracker (LPT), and objects were retrieved where possible. Tubes adjacent to irretrievable foreign objects with a potential to cause tube wear have been stabilized and plugged during past outages. Migration of those foreign objects that remain is unlikely due to the tri-pitch design of the steam generator tubing and is evidenced by noting past examination history which indicates no apparent change in location following initial detection (except for FO movement that is attributed to waterlancing, which would not be performed without an associated primary side inspection).

Consequently, no foreign objects capable of causing tube degradation are known to remain adjacent to in-service tubes. This aggressive ECT and FOSAR campaign has significantly reduced the potential for future foreign object wear. With these extensive inspections and subsequent part removal, there is reasonable confidence that no parts capable of causing significant tube degradation remain in the tube bundle.

Despite the extensive inspections and removal of multiple parts, the OA still has to consider the potential for tube degradation from parts remaining in the bundle or potentially entering the bundle during the next inspection interval. For the purposes of the OA, the discussion of foreign objects and associated wear will be segregated into the following categories:

1) foreign object wear without evidence of a part present,
2) eddy current PLPs (Potential Loose Parts) without wear,
3) foreign objects known to have remained in the steam generators, and
4) foreign objects that may enter the steam generators.

As discussed previously, the SG work activities performed during this refueling outage included secondary side visual inspections of the steam drum and upper tube bundle in SG25 and SG26. These examinations identified no foreign objects, or any conditions which could credibly generate foreign objects, capable of impacting tube integrity.

Based upon the following discussions, there is reasonable assurance that operation of SG25 and SG26 for five cycles will not generate foreign object wear flaws which exceed the structural integrity, operational leakage, or accident induced leakage performance criteria.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 27 of 40 6.2.1 Foreign Object Wear with No Part Present The four new foreign object (FO) wear indications (maximum depth 36 % TW) identified during 2R24 were confirmed to have no foreign object remaining in the vicinity. A summary of the growth rates for new foreign object wear indications is provided in Table 6.3. Without the objects in-place continued degradation is not possible. Consequently, none of the new flaws in in-service tubes pose a future tube integrity threat.

Table 6.3 New Foreign Object Wear Depth Reported Maximum Prior Delta SG Row Col Location ETSS Depth 2R24 Outage Cause EFPY Foreign NDD 26 122 123 TSH+2.53" 27901.1 34%TW Object 2.74 2R22 Wear Foreign NDD 26 124 123 TSH+l.77" 27901.1 36%TW Object 2.74 2R22 Wear Foreign NDD 26 125 122 TSH+l.36" 27902.1 23%TW Object 2.74 2R22 Wear Foreign NDD 25 92 149 TSH+l0.91" 27901.1 23%TW Object 1.975 2R23 Wear The OA must also consider the growth of foreign object wear indications identified and left in service.

Historical foreign object wear indications where the foreign objects had been previously removed were re-sized during 2R24 and were left in service. All of these historical indications are in SG 26. A summary of the growth rates for historical foreign object wear indications is provided in Table 6.4. Some variation in sizing can be expected from one inspection to the next. As expected, these indications exhibited virtually no growth as compared with previous outage sizing and considering technique sizing variability and uncertainty.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 28 of 40 Table 6.4 Historical Foreign Object Wear Indications Depth Reported Delta %TW Maximum Prior %TW Delta Growth SG Row Col Location ETSS Depth 2R24 Outage Cause Growth EFPY perEFPY Foreign 27%TW 26 28 5 TSC+21.65" 27901.1 25%TW Object -2 2.74 -0.7 2R22 Wear Foreign 25%TW 26 29 4 TSC+22.2" 27901.1 26%TW Object 1 2.74 0.4 2R22 Wear Foreign 11%TW 26 44 5 TSC + 17.91" 27902.1 10%TW Object -1 2.74 -0.4 2R22 Wear Foreign 24%TW 26 59 10 TSC +17.33" 27901.1 23%TW Object -1 2.74 -0.4 2R22 Wear Foreign 20%TW 26 98 143 TSH +8.76" 27901.1 20%TW Object 0 2.74 0 2R22 Wear Foreign 12%TW 26 118 41 TSH + 12.81" 27902.1 12%TW Object 0 2.74 0 2R22 Wear Foreign 24%TW 26 119 42 TSH + 12.97" 27903.1 29%TW Object 5 2.74 1.8 2R22 Wear Foreign 22%TW 26 123 46 TSH + 18.15" 27903.1 25%TW Object 3 2.74 1.1 2R22 Wear Foreign 26%TW 26 124 45 TSH + 19.27" 27903.1 31%TW Object 5 2.74 1.8 2R22 Wear Foreign 32%TW 26 125 48 TSH + 19.53" 27903.1 36%TW Object 4 2.74 1.5 2R22 Wear Foreign 34%TW 26 126 49 TSH +19.97" 27903.1 39%TW Object 5 2.74 1.8

\

2R22 Wear Foreign 29%TW 26 128 107 TSH +0.06" 27901.1 26%TW Object -3 2.74 -1.1 2R22 Wear 28

Serial No. 20-328B Docket No. 50-336 Attachment, Page 29 of 40 6.2.2 Eddy Current PLPs without Wear Thirty-two (32) cases of eddy current PLPs without wear were reported during the 2R24 inspections. Some of the PLPs were newly reported while others had been reported in previous outages. For some of the newly reported PLPs, reviews of the previous eddy current results showed that the suspected part was present in a previous outage(s), but was not reported. The eddy current PLPs with history (either previously reported or previously present based on lookup) were deemed acceptable based on their presence over multiple cycles without causing any detectable wear and will continue to be monitored during future SG inspections. Some of the PLP locations near the periphery of the bundle were visually inspected.

Locations with no v.isual evidence of a part were considered acceptable based on the confirmed absence of a part. All PLP indications were further dispositioned as either PLM (monitor), PLR (part removed), or PLS (signal with no part observed). Based on these analyses, all eddy current PLP locations were acceptable for the next five cycles of operation.

6.2.3 Foreign Object Wear from Parts Remaining in the Steam Generators Tables 2-8 and 2-9 of the Degradation Assessment [8.4] identified known parts remaining in SG25 and SG26 respectively. During 2R24, these locations were re-examined using eddy current and/or visual inspections to confirm that the part was still present and that no wear was caused by these parts. Each of these parts have been monitored for at least four cycles of operation with no noted changes in tube wear.

It is reasonable to expect similar results following five operating cycles before the next steam generator inspection campaign. Parts newly identified during the 2R24 steam generator inspection campaign remaining in SG25 and SG26 had no associated tube wear noted and have all been dispositioned as presenting no risk to tube degradation. Attachments 1 and 2 of this document summarize the results of those inspections which show there is reasonable assurance that operation of SG25 and SG26 for five operating cycles with these parts remaining will not generate foreign object wear flaws which exceed the structural integrity, operational leakage, or accident induced leakage performance criteria.

6.2.4 Foreign Objects That May Enter the Steam Generators No foreign. objects capable of causing tube degradation were known to remain in the MPS2 steam generators following the 2R24 inspection activities. Based on the discussion presented in section 6.2.1 above, there is evidence to conclude that continued wear at tube locations where foreign objects have been removed is not credible. '

Foreign objects may enter the steam generator tube bundle at any time during an operating cycle and cause wear on the tubes. Dominion Energy performs eddy current and visual inspections to identify objects and retrieve them; however, this cannot preclude foreign object events. Industry operating experience proves that wear from foreign objects initially leads to low level leakage. The MPS2 primary-to-secondary leakage monitoring program implemented is capable of identifying leakage at very low levels. If such leakage is identified, MPS2 TSs and procedures require a unit shutdown when necessary to avoid the potential of tube rupture or exceeding the leakage performance criteria.

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Serial No. 20-3288 Docket No. 50-336 Attachment, Page 30 of 40 Historical findings and current FOSAR and eddy current examinations provide reasonable assurance that operation until the next planned inspection will not generate foreign object wear that exceeds the SG structural integrity performance criteria (SIPC). In the unlikely event that significant degradation does occur, primary to secondary leakage monitoring procedures in place at MPS2 provide a high degree of confidence of safe unit shutdown without challenging the SIPC or leakage performance criteria.

6.3 Potential Degradation Mechanisms DAs have been performed per the SG Program described in MPS2 TS 6.26. As previously noted, there have been only two degradation mechanisms detected in the MPS2 SGs, (i.e., wear at the tube bundle U-bend support structures or fan bar and wear caused by foreign objects).

Two additional degradation mechanisms are considered to have the potential to occur in the future. These degradation mechanisms are lattice support wear and tube-to-tube wear. Tube thinning adjacent to support structures was also identified as a degradation mechanism with a low likelihood of initiation and progression.

6.3.1 Lattice Support Wear Tube wear has been detected on other B&W replacement steam generators at the lattice support structures. However, no tube wear has been detected as lattice support wear at MPS2 in nearly 30 years of operation and is unlikely to initiate and rapidly progress to an unacceptable depth during the interval between inspections.

6.3.2 Tube-to-Tube Wear Tube-to-tube wear has been reported at Palisades Nuclear Plant, both units at the San Onofre Nuclear Generating Station (SONGS), and several of the replacement Once Through Steam Generators (OTSGs).

Although the OTSG experience is not relevant to MPS2 due to the different design, the Palisades and SONGS experiences have potential applicability to MPS2. The tube-to-tube wear reported at Palisades is believed to be related to tubes having less than the nominal gap from one tube to the other. The SONGS experience was caused by fluid elastic instability in the U-bend region. However, neither of these conditions are known to exist in MPS2 SGs and no tube-to-tube wear has been detected at MPS2.

6.3.3 Thinning Thinning is a general term used to describe two different SG damage mechanisms. The first is a wastage mechanism resulting from the use of phosphate-based secondary chemistry controls. This mechanism has not been observed in plants that do not use phosphate chemistry (such as MPS2) and is therefore not a threat to the MPS2 SGs. The other is a type of thinning observed in Westinghouse Model 51 SGs caused by acid-sulfate crevice conditions within cold leg deposits. Under modern chemistry control regimes, this mechanism is unlikely to develop because sulfate limits are very low and resulting crevice pH is typically not acidic.

The other mechanisms evaluated in previous DAs were concluded to have a very low likelihood of initiation and progression.

Based upon the following discussions, there is reasonable assurance that operation of SG25 and SG26 for five cycles will not generate any potential degradation mechanisms which would exceed the structural integrity, operational leakage, or accident induced leakage performance criteria.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 31 of 40 6.4 Leakage Performance Criteria No tube leakage was reported during the previous operating cycle. As discussed above, no degradation is expected to exceed SG tube structural integrity limits during the next inspection interval in either SG25 or SG26. Further, no degradation of the type, that can result in throughwall penetration while still meeting structural integrity limits (i.e., cracking), is expected. As a result, there is reasonable assurance that the accident induced leakage performance criteria and operational leakage performance criteria will not be exceeded during the operating period prior to the next SG tube inspection in either of the MPS2 SGs.

6.5 Secondary Side Internals Degradation No degradation of secondary side internals which could impact tube integrity prior to the next examination was identified during the 2R24 SG secondary side inspections. There were no reported difficulties during the insertion of sludge lance equipment into the secondary side hand holes. Therefore, it can be concluded that wrapper drop has not occurred. The eddy current examination performed during 2R24 revealed no indication of missing support structures. The absence of secondary side structural degradation provides a high level of confidence that tube degradation caused by secondary support deterioration will not occur in any of the steam generators prior to the next inspection in each SG. A visual examination of internal components in SG25 and SG26 in the upper bundle and steam drum revealed no degradation and none is expected for the foreseeable future. Consequently, there is no expected degradation mechanism of secondary side components that could threaten tube integrity prior to the next inspection. These findings support an interval of five operating cycles before the next SG secondary side inspection.

6.6 Operational Assessment Conclusion Based upon the evaluations above, there is reasonable assurance that the structural and leakage performance criteria will not be exceeded prior to the next planned inspection in either of the MPS2 SGs; supporting an inspection interval of five operating cycles until 2R29.

7. Conclusions As indicated by the results of the current outage primary side and secondary side examinations, the Millstone Unit 2 steam generators continue to satisfy the structural and leakage integrity requirements delineated in the Dominion Energy SG Program and MPS2 technical specifications. Specifically, no degradation exceeding the performance criteria was identified during this or any previous MPS2 SG inspection.

This evaluation has demonstrated that there is reasonable assurance that operation of the MPS2 SGs for up to five fuel cycles between inspections will not cause the structural or leakage integrity performance criteria to be exceeded. In addition, the absence of conditions which challenge the SG program performance criteria validates prior outage operational assessment assumptions and conclusions regarding structural and leakage integrity.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 32 of 40 8.0 References 8.1 Dominion Fleet Administrative Procedure, "Steam Generator Program," ER-AP-SGP-101, Revision 11 8.2 Dominion Fleet Administrative Procedure, "Steam Generator Condition Monitoring and Operational Assessments," ER-AP-SGP-103, Revision 6 8.3 NEI, "Steam Generator Program Guidelines," NEI 97-06, Rev. 3, January 2011 8.4 Dominion Engineering Technical Evaluation ETE-MP-2017-1015, "Millstone Unit 2 Steam Generator Integrity Degradation Assessment (2R24)", Revision 0, 2/23/2017 8.5 EPRI, "Pressurized Water Reactor Steam Generator Examination Guidelines: Revision 7,"

1013706, October 2007 8.6 Unit 2 Steam Generator Eddy Current Data Analysis Reference Manual U2-24-SIP-REF01, Revision 8, April 2017 8.7 EPRI, "Steam Generator Integrity Assessment Guidelines: Revision 3," 1019038, November, 2009 8.8 EPRI, "Steam Generator Integrity Assessment Guidelines: Revision 4," 3002007571, June 2016 8.9 EPRI, "Interim Guidance Regarding Steam Generator Integrity Assessment Guidelines, Revision 3", SGMP-IG-09-03, November 2009 8.10 EPRI, "SGMP: SG Degradation Specific Management Flaw Handbook, Revision 2," 3002005426, October 2015 8.11 EPRI Software, "Steam Generator Management Program: Flaw Handbook Calculator (SGFHC) for Excel 201 O v1 .O", 3002003048, June 2014 32

Serial No. 20-328B Docket No. 50-336 Attachment, Page 33 of 40 ATTACHMENT 1 LPT SG25 33

Serial No. 20-328B Docket No. 50-336 Attachment, Page 34 of 40 SG25 PLP / Foreign Objects Detected in 2R24 Ref Affected Tube ECT History/

Description 2R24 Results/Disposition ID Locations Results Change?

ECT: No PLP or wear in bounding tubes R30 C97 Newly No PLP SSI: Part could not be R31 C98 detected, Newly or wear removed but likely 2521 Detected Metal R32 C97 on present in Screen bounding Part dis12ositioned to system tubes remain in the SG based on TSC + 0" previously 12revious engineering assessment of metal screen R41 C160 R42 C159 R40 C159 ECT: PLPs detected with R43 C158 Location no wear Historical Weld PLP unchanged 2522 Slag R41 C158 No Wear since (2R20 FK7) R44 C157 2R16 SSI: Part confirmed to be R42 C157 in same location TSH +1" R24 C101 ECT: PLPs detected in R23 C102 Location Historical Weld four tubes with no wear R24 C103 PLP unchanged 2523 Slag R25 C102 No Wear since (2R20 FK1) 2R14 SSI: Part confirmed to be in same location TSC +0" R119 C66 ECT: No PLP or wear in Historical R121 C66 Location bounding tubes Tubes unchanged 2524 Weld Slag R120 C67 plugged since (2R20 FK48) in 2R20 SSI: Part confirmed to be 2R20 TSC +0" in same location R78 C141 ECT: No PLP or wear in R76 C141 Location bounding tubes Historical Weld Tubes unchanged 2525 Slag R77 C142 plugged since (2R20 FK21) in 2R18 SSI: Part confirmed to be 2R18 TSC +0" in same location 34

Serial No. 20-328B Docket No. 50-336 Attachment, Page 35 of 40 Ref Affected Tube ECT History/

Description 2R24 Results/Disposition ID Locations Results Change?

Newly R92 C27 detected, ECT: PLPs detected with Rectangular no wear R94 C27 PLP but likely 2526 Metallic Object No Wear present in (2R20 FK26) system TSH + O" SSI: Part removed previously ECT: PLPs detected with R109 C40 no wear Machine PLP Newly 2527 R110 C41 Shaving No Wear detected R111 C40 SSI: Part removed PLPs newly detected, ECT: PLPs detected with but no wear present in PLP history back to SSI: Part could not be Historical R89 C144 removed 2528 Wear on 2008 Metallic Object R90 C143 adjacent WAR tube newly Part dis1;2ositioned to detected, remain in the SG based on but histo[Y back to 2008 with present no change back to 1997 ECT: PLP with no wear; R36 C5 characterized as weld R42 C5 splatter conforming to tube ECT PLP PLP Detected surface

- R44 C5 in 2R20 (2R20 FK26) No Wear 01H +2" SSI: Location not accessible ECT: INRs re1;2orted in 1, same location as 1;2revious PLPs with no wear; R122 C43 previously characterized ECT PLP R121 C42 PLP Detected as weld splatter

- No Wear in 2R20 (2R20 FK30) conforming to tube surface 01H +2" SSI: Location not accessible Note: ET inspections were performed following first FOSAR campaign.

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Serial No. 20-328B Docket No. 50-336 Attachment, Page 36 of 40 ATTACHMENT 2 LPT SG26 36

Serial No. 20-3288 Docket No. 50-336 Attachment, Page 37 of 40 SG26 PLP / Foreign Objects Detected in 2R24 Ref Affected Tube ECT History/

Description 2R24 Results/Disposition ID Locations Results Change?

R32 C5 No PLP ECT: No PLP or wear in R33 C4 or wear affected and bounding tubes Flexitallic Newly 261 on Gasket detected bounding TSH +1" tubes SSI: Part removed.

R82 C19 R83 C18 No PLP ECT: No PLP or wear in R83 C20 or wear Flexitallic Newly affected and bounding tubes 262 R84 C19 on Gasket detected R85 C20 bounding tubes SSI: Part removed.

TSH +O" R121 C114 R122 C113 R122 C115 R123 C112 No PLP ECT: No PLP or wear in R123 C114 or wear affected and bounding tubes Flexitallic Newly 263 on Gasket R124 C111 detected bounding R124 C113 tubes SSI: Part removed.

R125 C112 TSH +1" 37

Serial No. 20-328B Docket No. 50-336 Attachment, Page 38 of 40 Ref Affected Tube ECT History/

Description 2R24 Results/Disposition ID Locations Results Change?

R135 C104 R136 C103 No PLP ECT: No PLP or wear in R136 C105 or wear affected and bounding tubes.

Newly 264 Wire on R137 C104 detected bounding tubes SSI: Part removed.

TSH +0" R125 C98 R126 C97 No PLP ECT: No PLP or wear in R127 C98 or wear affected and bounding tubes Flexitallic Newly 265 on Gasket R128 C97 detected bounding tubes SSI: Part removed.

TSH +0" R138 C99 No PLP ECT: No PLP or wear in (in annulus) or wear affected and bounding tubes Newly 266 Rust slag on detected bounding TSH +0" tubes SSI: Part removed.

ECT: No PLP or wear in affected and bounding tubes R19 C104 No PLP R20 C103 SSI: Removal not attempted Sludge or wear Newly 267 Rock'or R21 C104 on detected Scale bounding Part dis1;1ositioned to remain in tubes the SG based on sludge rock TSH +1" characterization. Sludge rocks or scale do not lead to tube degradation based on OPEX.

38

Serial No. 20-3288 Docket No. 50-336 Attachment, Page 39 of 40 Ref Affected Tube ECT History/

Description 2R24 Results/Disposition ID Locations Results Change?

ECT: No PLP or wear in associated lanes No PLP or wear Sludge SSI: Characterization 268 - in - identified observed features Rocks associate as likely relating to sludge lanes rocks on the tubesheet ECT: No PLP or wear in No PLP Two tubes bounding tubes; originally Historical R38 C81 or wear plugged in affected tubes already Flexitallic R40 C81 269 on 2R18. Gasket plugged Gasket bounding no longer (2R22 FK8) TSH +0" present.

tubes SSI: Gasket no longer present.

Object has been monitored ECT: PLPs reported closer to R93 C138 since 2000 the periphery. Part appears to Historical R94 C137 have moved. No wear in the PLP with no wear.

Nut vicinity 2610 C95 C138 Part moved 1 (2R22 No Wear row closer to FK22) the periphery, TSH +0" SSI: Part not monitored likely as a visually result of waterlancing R97 C144 R98 C143 R94 C143 R96 C141 Eight tubes ECT: No PLPs or wear in Historical R95 C144 plugged in bounding tubes Flexitallic R96 C143 PLP 2R20; 2611 Gasket R97 C142 No Wear Location (2R22 unchanged SSI: Gasket confirmed to be in FK10) R93 C144 same location since 2R22 R95 C142 R98 C141 TSC +0" 39

Serial No. 20-328B Docket No. 50-336 Attachment, Page 40 of 40 Ref Affected Tube ECT History/

Description 2R24 Results/Disposition ID Locations Results Change?

R24 C67 ECT: No PLP or wear in Rectangular R26 C67 PLP affected and bounding tubes Newly 2612 Metallic No Wear detected Object TSH +0" SSI: Part removed.

ECT: No PLP or wear in affected and bounding tubes R20 C65 No PLP SSI: Part could not be R22 C65 or wear removed Sludge Newly 2613 on Rock detected bounding TSH +0" Part disQositioned to remain in tubes the SG based on sludge rock characterization. Sludge rocks do not lead to tube degradation based on OPEX R66 C157 R67 C156 R68 C155 ECT: PLPs reQorted in same R69 C156 Unchanged location with no wear; Historical characterized as weld splatter R72 C155 PLP since initial

- ECT PLP conforming to tube surface R75 C154 No Wear detection in (2R22 FK4) 2R20 R78 C153 R81 C152 SSI: Location not accessible 01H +2" R18 C165 INR ECT: INRs reQorted in same R19 C166 No Wear location as Qrevious PLPs with Location Historical R20 C165 unchanged no wear; characterized as

- ECT PLP R17 C166 since irJitial weld splatter conforming to

' (2R22 FK6) detectioh in tube surface R16 C167 2R20 SSI: Location not accessible 01C +2" Note: ET inspections were performed following first FOSAR campaign.

40