ML16189A218

From kanterella
Jump to navigation Jump to search
BWR Vessel and Internals Project - Vessel Internals Inspection Summaries for Fall 2015 Outages
ML16189A218
Person / Time
Site: Dresden, Peach Bottom, Fermi, PROJ0704  
Issue date: 06/29/2016
From:
Electric Power Research Institute
To:
Document Control Desk, Office of Nuclear Reactor Regulation
Shared Package
ML16189A235 List:
References
Download: ML16189A218 (66)


Text

(

I

\\

J i

\\,

\\ __

I 1,

~I

\\_,

\\~,;

(

)

BWR Vessel and Internals Project Vessel Internals Inspection Summaries for Fall 2015 Outages June 2016 1

Plant

1. Dresden Unit 2
2. Fermi Unit 2
4. Peach Bottom Unit 3 END Table of Contents 2

3 20 49 66

/

i

\\,

Plant: Dresden Unit 2 Components in BWRVIP Scope Core Spray Piping Reactor Internals Inspection History Date or fuspection Summarize the Following fuformation:

Frequency of Method fuspection Results, Repairs, fuspection Used Replacements, Reinspections 1980s to UT, VT-1 IEB 80-13 (1 MIL) VT-1 of piping and D2R14 (lMIL) welds in annulus. fudications observed at one lower elbow to riser weld (3P4c) and two collar to shroud pipe welds (3 and 4P8a) in 1995. All flaw lengths verified with UT. Full structural margins met on all three flawed welds for additional cycle. No repairs performed.

3/1998 UT, GE CSI-2000 fuspected with EVT-1 D2R15 0.0005" supplement for unqualified welds (P8a EVT and P4d). Identified three previously unidentified flaws (1P5, 2P8a and 3P4d) for a total of six flaws. All flaws were analyzed for two additional cycles of operation with no repairs required.

Previously identified flaws were determined to be of the same or less extent than originally sized. 1P5 and 2P8a were not visually verified.

10/2000 EVT-1 Core Spray Piping: P8a and P4d, D2R16 EVT-1 @all four locations. Previous indications have been found on the Core Spray Elbow to Collar on the 260° Downcomer. The results of the 1999 measurements compared with the two previous 1998 indications are as follows.

It appears that the Collar indication has not changed, while the indication on the elbow is larger this year than was seen in 1998. The noted crack growth was bounded by the previous flaw evaluation and the BWRVIP-18 crack growth value.

10/2001 UT, GE CSI-2000 inspected a complete D2R17 EVT-1 Target Set and a sample of P4 welds. No new flaws. Growth within Fracture Mechanics Evaluation predictions.

Performed EVT-1 ofundemonstrated welds.

3

10/2003 EVT-1, Excessive grinding exam of l-4P4a and b D2Rl8 VT-1 (VT-1). Undemonstrated l-4P8a and P4d(EVT-1). Flaws are unchanged.

11/2005 UT, GE CSI-2000 inspected all demonstrated D2Rl9 EVT-1 welds. Previous flaws re-sized, growth within flaw evaluation and BWRVIP-18 predictions. EVT-1 all undemonstrated welds. No new flaws identified.

EVT-1 25% (2) piping bracket assembly welds. NRI.

11/2007 EVT-1 EVT-lofpiping welds Pl, P2, P3 P8a, D2R20 P8b and 25% of P4a, P4b, P4c and P4d in accordance with BWRVIP-18. Rls for previous indications in 3P4d, 3P8a, 4P8a.

11/2009 EVT-1 EVT-lof all Pl, P2, P3 and 25% of P4a D2R21

& b piping welds in accordance with BWRVIP-18. NRI.

Performed Core Spray Lower Sectional Replacement on all four lines. Welds P4c & d, P5, P6, P7, P8a & band P9 all replaced. One P9 weld was examined after the old pipe was removed with no relevant indications. The other three P9 welds were destroyed by the EDM cut and could not be inspected.

10/2011 EVT-1 EVT-lof all Pl, P2, P3 and 25% ofP4a D2R22

& b piping welds. NRI.

EVT-1 on piping attachment welds on all four piping braces VT-lNT-3 Core Spray Lower Sectional Replacement (all 4 lines)

- VT-1 ofbolting, keepers, ratchet springs, latch springs, lateral pins, and keepers. NRI

- VT-3 of repair hardware. NRI 11/2013 EVT-1 EVT-lof all Pl, P2, P3 and 25% of P4a D2R23

& b piping welds. NRI.

11/2015 EVT-1 EVT-1 of all Pl, P2, P3 and 25% of P4a D2R24

& b piping welds. NRI.

4

(

\\

\\

"/

J f

' _)

Core Spray Sparger Vessel ID Brackets 1980s to pres en 3/1998 D2R16 10/2001 D2R17 11/2005 D2R19 11/2009 D2R21 11/2013 D2R23 11/2015 D2R24 4/1994 D2R15 3/1998 D2R16 VT-lNT-3 VT-1 (1 MIL)

EVT-1, MVT-1 EVT-1, VT-1 EVT-1, VT-1 EVT-1, VT-1 EVT-1, VT-1 VT-1 VT-1 MVT-1 5

Core Spray Lower Sectional Replacement (all 4 lines)

- VT-1 of bolting, keepers, ratchet springs, latch springs, lateral pins, and keepers. NRI

- VT-3 ofrepair hardware. NRI.

IEB 80-13 (1 MIL) VT-1 of spargers and tee-boxes. No indications found.

Future inspections per BWRVIP-18.

End caps, cover plates and tee box branch welds were EVT-1 examined (OD). All sparger connections and bracket welds were MVT-1 examined.

NRI.

Complete Target Set and 50% of S3 welds. No Indications recorded.

EVT-1 100% Sl; S2; S4. NRI.

VT-1 50% S3. NRI.

VT-1 100% (12) SB. NRI.

EVT-1 100% S4. NRI.

VT-1 50% S3. NRI.

VT-1100% (12) SB. NRI.

S 1 and S2 structurally replaced by bracket as part of lower sectional replacement.

EVT-1 100% S4. NRI.

VT-1 50% S3. NRI.

VT-1100% (12) SB. One RI identified in heat affected zone of the 260° bracket. Indication acceptable for one cycle.

VT-1 of 260° bracket. Previous indication inspected with no change.

Section XI inspections of jet pump riser brace, dryer, feedwater sparger, core spray, and surveillance capsule holder brackets, performed once per interval.

No indications noted.

Inspected Core Spray Brackets per BWRVIP recommendations. NRI.

b I

10/2000 D2R17 10/2003 D2R18 11/2005 D2R19 11/2007 D2R20 11/2009 D2R21 10/2011 D2R22 VT-1 VT-3 EVT-1 EVT-1, VT-1 EVT-1, VT-1 EVT-1 VT-3 EVT-1 VT-1 EVT-1 VT-1 VT-3 6

100% (6) Surveillance Capsule Brackets.

NRI.

100% ( 6) Guide Rod Attachments. NRI.

EVT-1100% (4) Dryer Lugs. NRI.

EVT-1 100% (4) Dryer Lugs. NRI.

Eight feedwater sparger end-brackets VT-1, NRI.

Eight Core Spray piping bracket welds, EVT-1, NRI.

- EVT-1 100% (8) feedwater sparger end bracket to vessel attachments. NRI.

- VT-1 100% (8) feedwater sparger end bracket lug. NRI.

- EVT-1 100% (8) feedwater sparger end bracket pin tack weld. NRI.

- VT-1 feed water sparger repair at 240°.

RI. Hole in the weld of the repaired nozzle. Accepted as-is.

- EVT-1 25% (2) core spray piping bracket to vessel attachments. NRI.

- EVT-1 100% ( 4) steam dryer wall support lugs. NRI.

- EVT-1 and VT-3 of25% of Core Spray piping brackets (2). NRI

- EVT-1 100% (8) feed water sparger end bracket pin and nut. RI, some wear identified at pin head to bracket interface on three pins. One nut not tight against shoulder.

-EVT-1 of25% of Core Spray piping brackets (2). NRI

- VT-1 100% (8) feedwater sparger end bracket pin and nut. RI, some wear identified at pin head to bracket interface on s1xpms.

-EVT-1 of25% of Core Spray piping brackets (2). VT-1 on bolting of 1 of the 2 brackets. NRI

- VT-3 of moisture separator and dryer guide rod attachments. Rls for top cone bent on 200° guide rod and gouge/metal shaving on top cone of 0° guide rod. NRI for attachment welds.

- VT-1 100% (4) dryer wall support lugs.

Gouges noted on 3 of the lugs.

- VT-1 on all surveillance sample holder lower brackets and VT-3 on upper brackets. NRI.

11/2013 EVT-1

- EVT-1 of 25% of Core Spray piping D2R23 VT-1 brackets (2). VT-1 on bolting for 1 of the 2 brackets. NRI

- EVT-1 100% (8) feedwater sparger end bracket to vessel attach. NRI.

- EVT-1 of 200° moisture separator and 0° dryer guide rod top cones. No change to previous Ris.

- VT-1 100% ( 4) dryer wall support lugs.

Gouges and wear marks noted on all of the lugs.

11/2015 EVT-1

- EVT-1 of 25% of Core Spray piping D2R24 VT-1 brackets (2). VT-1 on bolting for 1 of the 2 brackets. NRI

- EVT-1 of 200° moisture separator rJ guide rod top cones. No change to previous Ris.

- VT-1 100% ( 4) dryer wall support lugs.

Gouges and wear marks noted on all of the lugs. One new RI. Indications acceptable for one cycle.

Feedwater Sparger 10/2011 VT-1 Inspected all eight feedwater sparger end D2R22 bracket pins and nuts. RI, some wear identified at pin head to bracket interface on s1xpms.

Performed inspections of spargers, arm welds and t-box welds. RI - gouge on sparger. RI - sparger repair hardware previous indication, no change.

11/2013 VT-1 Inspected all eight feedwater sparger end D2R23 bracket pins and nuts. RI, wear on six of eight brackets at pin to bracket interface.

11/2015 VT-1 Inspected all eight feedwater sparger end D2R24 bracket pins and nuts. RI, wear on six of eight brackets at pin to bracket interface.

\\,_~;

Core Shroud 8/1995 EVT-1, UT Inspections per BWRVIP Guidelines of D2R14 all shroud repair design reliant structures prior to installation of comprehensive repair ( 4 GE designed tie-rod assemblies). Inspection of shroud consisted ofEVT-1 of all ring segment 7

welds (accessible surfaces), EVT-1 of between 43% and 72% of the length of each vertical weld between Hl & H2 from OD surface (ID not accessible), UT of between 30% and 50% of the length of each of the 6 beltline vertical welds, EVT-1 of between 43% and 72% of the length of 2 of the 3 vertical welds between H6 & H7 from OD surface (ID not accessible), and UT of 35% of the length of the remaining vertical weld between H6 and H7.

( *-,

No Reportable Indications.

03/1998 VT-1, Shroud repair hardware inspected per GE D2Rl5 VT-3 recommendations. NRI.

10/1999 UT&EC UT & EC examinations from the ID with D2R16 the TEIDE 2 manipulator on the core shroud vertical welds V14, Vl5, V16, Vl 7, V18, and V19 per the requirements ofBWRVIP-76 for a repaired shroud.

NRI. Coverages are as follows:

V14: 80.1%

V15: 80.1%

V16: 83.4%

V17: 52.6%

-. -y Vl8: 62.8%

V19: 58.0%

10/2001 EVT-1 Exelon performed one sided EVT-1 of all D2R17 vertical welds outside of the beltline with 100% coverage including welds V5, V6, V7, V26, V27 and V28. There were no I

\\

recordable indications.

11/2005 EVT-1, EVT-1 100% (16) Ring Segment Welds D2R19 VT-1 from the OD. NRI. Coverages were 100% except for the following:

V9:

85%

Vll: 95%

\\

~

V20: 0% (inaccessible due to Jet Pump diffuser)

V21: 90%

V24: 0% (inaccessible due to Jet Pump diffuser)

Attempted EVT-1 of shroud vertical welds V29, V30, V31, V32. 0%

8

\\

r *.

\\._,;

/

\\

\\.__,;

( )

_/

\\, ___ )

/

', \\

\\_./

\\__)

I I

-~I

coverage was achieved due to Jet Pump interference.

Performed 10 year shroud tie rod examination of all four tie rods:

- EVT-1 of the clevis pin to verify if bottomed in slot and checking contact area for movement. NRI.

- VT-1 of stabilizer assembly contact between the RPV wall and upper contact, mid support, and lower contact. RI @ 20 and 110 degrees. Accepted as-is.

- VT-1 of retainer devices at lower support, lower spring to tie-rod connection, upper spring jacking bolts and tie rod nut. NRI.

- VT-1 of contact of the stabilizer assembly between the shroud and upper and lower springs. NRI.

- VT-1 of the core plate wedge contact.

NRI.

- Performed UT on the following vertical welds with the percent coverage shown:

V14: 19.9%

Vl5: 85.8%

V16: 90.1%

V17: 35.0%

V18: 84.0% - RI, Accept as-is.

V19: 47.2%

V27: 63.9%

Besides V18, all other welds NRI EVT-1 of welds V05-V07, Vl9, V26, V28, V29 and V3 l. NRI

- Shroud repair hardware inspections at all four locations. NRI.

Two sided EVT-1 on Vl9. NRI One-sided EVT-1 on vertical ring welds Vl, V2, V3, V4, V8, V9, VlO, Vl l, V12, Vl3, V20, V21, V22, V23, V24 and V25. NRI.

One-sided EVT-1 on vertical welds V5, V6, V7, V14, Vl 7, V26, V28, V29, and V31. NRI.

Performed EVT-1 and VT-3 inspections on all four shroud tie rod repairs. NRI.

(

I

(

\\. _/

,_)

,_/

l

)

_/

Shroud Support Top Guide 3/1993 D2R13 811995 D2R14 3/1998 D2Rl5 1011999 D2R16 11/2005 D2R19 1012011 D2R22 1112013 D2R23 8/1995 D2R14 3/1998 D2Rl5 10/2000 D2R16 10/2003 D2R18 UTNT-1 EVT-1, VT-1 NIA EVT-1 EVT-1, VT-3 EVT-1 VT-1 UT VT-1 NIA EVT-1 EVT-1 VT-1 10 Access hole covers proactively replaced with GE mechanical design. UT for radial flaws performed prior to replacement. No indications identified.

EVT-1 ofH8 and H9 for approx 12" at 4 locations of shroud repair hardware attachment areas.

VT-1 of both replacement access hole cover assemblies. No indications identified.

Not fuspected during D2R15 Core Support Structures, Performed EVT-1 of H8 and H9 Welds per BWRVIP-38 requirements. No Recordable fudications fuspected both Shroud Access Hole Cover repairs, NRI.

EVT-1 H8 & H9 from 132-177°. NRI.

VT-3 H9 100% accessible areas. NRI.

EVT-1 top side of H8 & H9 welds at 132-177° and 312-357°. NRI.

Bolted attachment for both Access Hole Covers. NRI.

UT of 10% of the H9 weld. NRI VT-1 of 5 cells. NRI.

VT-1 of all 4 alignment assemblies. NRI.

VT-1 of rim to bottom plate weld at 4 locations. NRI.

No inspections during D2Rl5.

Top Guide Alignment Pins, EVT 90° and 270° and Rim to Lower Plate Weld per BWRVIP-26. No Reportable fudications Top Guide aligner assemblies at 0, 180° and 270° welds (EVT-1) and pin (VT-1),

NRI

I I

\\

' I

~ '

j

\\ __ l<'

I I

r

\\

j I

'- /

\\

'.../

I 11/2005 D2Rl9 11/2007 D2R20 10/2011 D2R22 11/2013 D2R23 11/2015 D2R24 SLC 11/2005 D2R19 11/2007 D2R20 11/2009 D2R21 11/2013 D2R23 Jet Pump Assembly 8/1995 D2R14 EVT-1 Top guide rim weld at 235° on the outboard side of cell 03-30. NRI.

EVT-1 Top guide rim welds, aligner pins and VT-1 sockets at 0° and 90°.

EVT-1 Top guide rim weld was inspected at accessible locations. One RI - a 12" linear indication was identified.

VT-1 The aligner pins and sockets at 180° and 270°. NRI.

EVT-1 Top guide grid beams were inspected from 10% of the cells (18 cells). NRI.

EVT-1 Top guide rim weld indication inspected with no change noted from previous outage.

EVT-1 Top guide rim weld was inspected at accessible locations. No change to previous RI.

VT-1 All four aligner pins and sockets. One RI on aligner block at 90°.

Enhanced Safe end and nozzle examined. NRI.

VT-2 Enhanced Safe end and nozzle examined. NRI.

VT-2 Liquid Safe end and nozzle examined. NRI.

Penetrant UT Safe end and nozzle examined. NRI.

VT-1 UT Hold down beams, beam bolt keepers, lock-plates and retainers; restrainer wedges, stops, and adjusting screws, clamp bolts and keepers; riser brace assemblies, adapters and baffle plate welds, sensing lines and sensing line brackets per various SILS.

Latest inspections were in 1995, with no reportable indications. Inspect 100%

every other (even numbered) outage.

Jet pump beams are UT examined each outage using technique capable of 11

r--,

',,)

I\\

I./

r' I

I I

\\

)

' \\. /

\\

\\ __ )

\\

\\_)

Ci

(

~/

r 1

I

\\.._.J

\\'--./

( )

(

I

"-_J 3/1998 UT, EVT-1 D2R15 01/2000 UT, EVT-1 D2R16 10/2001 UT, EVT-1 D2R17 10/2003 EVT-1 D2R18 11/2005 EVT-1 D2R19 VT-1 VT-3 12 detecting cracking at throat and ears.

One beam found cracked at ear in 1995 and was replaced.

D2Rl 5 Beam UTs, NRI.

Jet Pump Riser Welds RS-1, 2, 3, 4 and 5 OD Inspected on all ten risers. Riser to JP Pair 15/16 has 1-1/2" long crack in elbow RAZ at RS-1. Evaluated for two cycles of operation without repair. NRI all others.

Jet Pump Beams, UT 100% of Beams NRI Riser Brace, Restrainer Bracket, Wedges and Inlet Mixers EVT-1 High/Medium Priority Welds Per BWRVIP-41 sample and inspection requirements. Minor Indications noted.

Jet Pump Beams, UT 100%, NRI Riser Brace Leaf at RPV wall block on JP#9, upper Rb 4 weld cracked.* EVT-1 examined 100% scope expansion, no other indications. Checked and found no set screw gaps. Examined for B-N-2.

Measured known RS-1 crack on riser 15/16. No change in last two cycles.

Replaced all 20 Jet Pump Beams with BWR4 weldless keeper beams Installed 19 Riser Brace Mitigation clamps one Repair on JP#9.

Measured flaw on JP#15/16 RS-1.

Increased from 1 1/2" to 2" length.

Identified pup piece present on JP#5/6, VT-1 100% (20) WD-1. NRI.

VT-3 100% (20) Jet Pump Bream Tooth Engagement. NRI.

VT-1100% (8) Jet Pump Sensing Line Clamps. RI (2). Teeth not fully engaged. Accepted as-is.

EVT-1 30% (3) RS-4, 5. NRI.

EVT-1 50% (5) RS-1, 2, 3. RI on JP 15/16 RS-1. Size confirmed to be 1Y2 ".

VT-1 100% (20) Jet Pump Riser Brace Clamps. RI (8). Teeth on keepers not fully engaged. Accepted as-is.

EVT-1AS-1,2 on Jet Pumps 8, 9, 19 (AS-1 only). NRI

.r--..,

\\

(--.,

r

)

I 11/2007 VT-1 D2R20 EVT-1 VT-3 11/2009 EVT-1 D2R21 VT-1 10/2011 EVT-1 D2R22 VT-1 13 VT-1 Aux. wedge on VS of Jet Pump 11.

NRI.

- VT-1 100% (8) Jet Pump Sensing Line Clamps. RI (7). Teeth not fully engaged. Accepted as-is.

- EVT-1 of six RB-3 welds. NRI

- EVT-1 ofRS-1 weld on JP 15/16. RI on previously identified indication. No change in flaw size.

- Swing gate replaced and 2 aux wedges installed on Jet Pump 19.

- VT-3 of IN-5 bolting sets on 10 JPs.

NRI

- EVT-1 ofMX-1 welds on 10 JPs. NRI

- VT-1 of 5 JP wedges and swing gate keeper tack welds. One RI on JP 15 swing gate keeper degraded tack weld.

Accepted as-is for one cycle.

- VT-1 of ratchets on eight JP Riser Brace clamps and eight JP Sensing Line clamps. Multiple Ris for incomplete ratchet teeth engagement. Accepted as-IS.

- EVT-1 25% (5) RB-4 & 5. NRI

- EVT-1 30% (3 risers) RS-8 & 9. NRI

- EVT-1 JP 15/16 RS-1. Previous indication - No change

- EVT-1 25% (5) MX-3a and 40% (8)

MX-3b.NRI

- VT-1 25% (5) WD-1. NRI

- VT-1 three aux wedges. Minor wear identified on one wedge. Accepted-as-is for one cycle.

- VT-1 on five swing gate keepers/ratchets. One RI for crack in tack weld HAZ and Two Rls for small gap between gate and restrainer bracket.

- VT-1 two sensing line clamps and one sensing line. No change to previous indications.

- Replaced JP 15 swing gate.

- EVT-1 30% (6) RB-3. NRI

- EVT-1 70% (7 risers) RS-8 & 9. NRI

- EVT-1 60% (6 risers) RS-1 & JP 516 RS-la. JP 15/16 RS-1 previous indication - No change

- EVT-1 50% (5 risers) RS-2 & 3. NRI

- EVT-1 30% (3 risers) RS-4 & 5. NRI

~' )

/ -......

(~-,.

\\.__ /

I

\\ j' r"'

'~

,1

(-\\

v

,r '*

'-..../

\\_)

\\.,_)

('

../

\\.___,/'

(

'-...,,)

"'-~:

u

(

\\__)

)

11/2013 EVT-1 D2R23 VT-1 VT-3 11/2015 EVT-1 D2R24 VT-1 Jet Pump Diffuser 8/1995 VT-1 D2Rl4 3/1998 NIA D2Rl5 01/2000 EVT-1 D2R16

- VT-1 75% (15) WD-1. NRI

- VT-1onJP19 aux wedges. NRI

- VT-1 on seven swing gate keeper tack welds or ratchets. One RI for crack in tack weld RAZ (no change from D2R21).

- VT-1 two sensing line clamps. RI for ratchet teeth engagement and clamp movement.

- VT-1 on 5 riser brace mitigation clamps and the jet pump 9 riser brace repair clamp. NRI

- EVT-1 of jet pump 15/16 riser RS-1.

No change to previous RI but better video has concluded the flaw is only 0.875" (previously recorded as 1.5")

- VT-1 on jet pump 2 and 11 sensing line clamps. No change to previous Ris.

- VT-1 25% (5) WD-1. NRI

- VT-1 3 0% of swing gate keeper tack welds. No change to previous RI on JP 2.

- VT-1onJP11and19 aux wedges. No change to previous RI.

- VT-1 of all 20 beam retainer clips. NRI

- EVT-125% (5 jet pumps) MX-1. NRI

- VT-3 25% (5 jet pumps) IN-5. NRI

- EVT-1 of jet pump 15/16 riser RS-1.

No change to previous RI.

- VT-1 on jet pump 2 and 11 sensing line clamps. No change to previous Ris.

- VT-1 25% (5) WD-1. NRI

- VT-1 on JP 19 vessel side aux wedge.

No change to previous RI.

- EVT-1 25% (5 jet pumps) MX-3a and MX3b.NRI

- VT-1 on JP 19 swing gate bolt ratchets.

NRI

-EVT-1 25% (5) RB-4 & 5. NRI Diffuser to baffle plate welds on all 20 jet pumps. No indications.

Not inspected D2R15.

JP Diffuser EVT-1 High/Med Priority welds per BWRVIP-41 sample and inspection requirements. NRI 14

\\

r

\\

I

\\

/

r, 1

,J

(-

\\

\\

)

\\---./

(

/

I I

I..___,,

.'--/

CRD Guide Tubes CRD Stub Tubes In-Core Housing Dry Tubes 1012001 D2R17 1012003 D2R18 1112005 D2R19 1112007 D2R20 1112009 D2R21 1112013 D2R23 811995 D2R14 1012001 D2R17 11/2007 D2R20 811995 D2Rl4 8/1995 D2R14 811995 D2R14 EVT-1 No scope D2Rl 7.

UT,EVT-1 UT examined Jet Pumps# 2, 3, 4, 5, 8, 9, 12, 13, 14, 15, 18 and 19. This completes first 6 Year Inspection Interval. NRI EVT-1 of the last of the Medium Priority 50% sample also completed. NRI.

NIA Not inspected in D2R19.

NIA Not inspected in D2R19.

EVT-1

- 25% (5) DF-1and50% (10) DF-2. NRI

- 50% (10) AD-1, AD-2 and AD-3a. NRI VT-3 VT-3 inspection of 1 jet pump slip joint. NRI VT-1 11 CRD guide tube lower assembly (1 MIL) welds, 2 CRD guide tube upper assembly welds, 4 CRD guide tube alignment ear welds. NRI.

EVT-1, 5% inspected (9) per BWRVIP-47, VT-3 CRGT-1, 2, 3 and pin. NRI.

EVT-1, Inspected 5% (9) of the control Rod VT-3 Guide Tube Welds and Guide Tube and Fuel Support Alignment Pins. VT-3 on the CRGT-1 and AS-GT-ARPIN-1.

EVT-1 of the CRGT-2 and 3. NRI VT-1 (1 14 CRD housing to CRD stub tube MIL) welds, 14 CRD stub tube to RPV bottom head welds, 3 CRD housing tube to housing cap welds. NRI.

VT-1 (1 4 incore guide tube to housing welds, 4

.MIL) incore housing to RPV bottom head welds, 4 incore guide tube stabilizers.

NRI.

VT-1 No indications identified.

Examined every other outage.

15

,.-- \\

I

."\\

(~,

\\ -

J

~, I

,~')

~- _.J

\\_j'

('\\

\\._ I

(~)

\\

/

""'- /

f

\\

\\_j

/ '

(

~)

(J r

' u

-._)

Instrument Penetrations LPCI Coupling Steam Separator/

Shroud Head 10/2000 D2R16 11/2007 D2R20 11/2009 D2R21 10/2011 D2R22 11/2013 D2R23 11/2015 D2R24 NIA NIA 11/2007 D2R20 11/2009 D2R21 10/2011 D2R22 1112013 D2R23 11/2015 D2R24 VT-1 NRI.

VT-1 50% ofSRM and IRM dry tubes inspected. NRI.

VT-1 50% of SRM and IRM dry tubes inspected. NRI.

VT-1 50% of SRM and IRM dry tubes inspected. NRI.

VT-1 One LPRM and 50% of SRM and IRM dry tubes inspected. NRI.

VT-1 50% ofSRM and IRM dry tubes inspected. Four dry tube plungers not fully engaged..

VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI for one missing pin and pin/window wear on multiple shroud head bolts VT-1

- VT-1 Inspected 100% of Shroud Head EVT-1 Bolt Alignment Pins and Windows. RI for pin/window wear on multiple shroud head bolts

- EVT-1 on Steam Separator Guide Rod top cone. RI for cracked tack weld.

Acceptable-as-is.

VT-1

- VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI for pin/window wear on multiple shroud head bolts VT-1

- VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI for pin/window wear on multiple shroud head bolts.

VT-1

- VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI 16

r ~

\\. _/

r *.

I

(

'*- /

i

', /

\\~*

\\... __.I Steam Dryer 11/2005 VT-1 "best D2R19 effort" 11/2007 NIA D2R20 11/2009 "Best D2R21 Effort" VT-1 10/2011 "Best D2R22 Effort" VT-1 11/2013 "Best D2R23 Effort" 17 for pin/window wear on multiple shroud head bolts.

Performed BWRVIP-139 required inspections as well as inspections of high-stress areas as determined by GE models. Internal start-up instrumentation piping was also examined. Several RI, including:

- Four of six gusset feet tip (adjacent to R2 weld), ranging from 7 to 11.5.

Cracking was ground out and rewelded.

Gusset feet extensions were designed and installed to transfer the stress riser to the mid-support ring.

- Several internal strut/supports were identified with cracking. Several were historical from D2Rl8 inspections. No change in the cracking was observed.

These welds are non-structural.

Accepted as-is.

- Vertical guide cracking (2) at 220°.

Both cracks (2.5-5" in length) were stop-drilled.

- Lower instrument line in Bank C observed cracking at the weld.

Performed fracture mechanics analysis and lost parts analysis. Acceptable as-is.

- Interior drain channel cracking (3).

Performed GE analysis. Acceptable as-lS.

- Perforated plate weld cracking.

Performed GE analysis. Acceptable as-lS.

- Perforated plate bowing. Performed GE analysis. Acceptable as-is.

Replaced steam dryer with a new one.

Examined critical components on steam dryer ID and OD after one cycle of operation per GE recommendations. NRI Examined OEM recommended components on OD. Lifting lug at 40° found rotated. Gouge identified on dryer skirt.

Examined OEM recommended components on ID and OD. New Rls

\\

,,r- ~.

)

)

\\

\\

\\__j

{

'~,/

\\..__)

DMWelds Reactor Vessel Cast Austenitic Stainless Steel 11/2015 D2R24 11/2009 D2R21 10/2011 D2R22 11/2013 D2R23 11/2015 D2R24 10/2011 D2R22 11/2013 D2R23 10/2011 D2R22 11/2013 D2R23 VT-1 noted near the trough supports to cross beam welds at 8 locations. No change to previous RI identified on dryer skirt.

"Best Examined trough support attachment Effort" welds on all 52 supports. No change to VT-1 previous Rls.

No inspections in D2R21 UT Inspected six DM welds. NRI.

UT Inspected four DM welds. NRI.

UT Performed manual UT on one (1) IGSCC Category C, twelve (12) IGSCC Category D, three (3) IGSCC Category F and two (2) IGSCC Category E welds.

None of these welds were dissimilar welds. No relevant indications were identified.

UT Inspected vertical welds (18) and the shell to flange weld. One indication identified in shell to flange weld identified as unacceptable per Table IWB-3510-1. Indication has been evaluated in accordance with IWB-3600.

EVT-1

- Examined weld and heat affected zones on four level instrument nozzles. NRI EVT-1 Inspected one of each of the following for License Renewal commitment: fuel support piece; control rod guide tube base; jet pump mixer flange, mixer flare, mixer ring, inlet/mixer nozzle and inlet mixer elbow. NRI.

EVT-1 Inspected one of each of the following for License Renewal commitment: fuel support piece; control rod guide tube base; jet pump mixer flange, mixer flare, mixer ring, inlet/mixer nozzle and inlet mixer elbow. NRI.

18

11/2015 EVT-1 Inspected one of each of the following D2R24 for License Renewal commitment: fuel support piece; control rod guide tube base; jet pump mixer flange, mixer flare, mixer ring, inlet/mixer nozzle and inlet mixer elbow. NRI.

\\

/

,r,

~,

~,

J r

I

' _/

~

' _/

",j

~--;

\\. _:

~I

.........._ _)

  • 19

Plant: Fermi Unit 2 Components in Date or Inspection Summarize the Following Information:

BWRVIP Scope Frequency of Method Inspection Results, Repairs, Inspection Used Replacements, Reinspections Core Shroud RF04 VT-1 (lmil Inspected: 100% ID welds H2, H3, and, (BWRVJP-07/76) wire)

H4; 100% OD welds Hl-H7; accessible areas HS &H9 VT-lNT-3 The only indications identified were two

<1" vertical in orientation above the H2 weld at azimuth 125 degrees. These were evaluated against established flaw screening criteria and found acceptable.

RF05 EVT-1 Inspected approximately 60-70 degrees r'

(1/2mil arc on the core shroud in area of previous

/ -,

wire) indications. H2-H4 inspected on shroud ID, Hl-H7 inspected on shroud OD. No new indications, no change observed in previous indications above H2 weld.

RF06 UT Performed focused phased array UT examination of the H3, H4, HS and H7 welds utilizing GE's universal carousel.

No indication of cracking was identified.

EVT-1 A cursory exam was performed on H-3 weld to confirm UT results for information only. No new indications and no change was observed in the previous indication above H2 weld.

RF07 EVT-1 Reinspected the indication above the H2 weld on the inside of the shroud. No change in appearance. The control rod blade was withdrawn to perform the examination.

RF09 NIA No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support RFlO NIA No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support 20

./

/

\\

I

",1

)

-- \\

Shroud Support (BWRVIP-381*104)

Access Hole Cover (BWRVIP-180)

RF11 NIA RF12 NIA UT RF13 NIA RF14 NIA (10110)

RF15 NIA (04/12)

RF16 NIA (2014)

RF17 NIA (2015)

RF03 VT-3 RF04 VT-lNT-3 RF05 EVT-1 (112 mil) 21 No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support Performed phased array UT examination of the H3, H4, HS and H7 welds from both sides utilizing AREVA's demonstrated technique. No indication of cracking was identified. Inspection coverage exceeded 60% for all welds with coverage spaced around the entire circumference.

No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support.

No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support.

No inspections performed on the Core Shroud. fuspections were performed on the Shroud Support.

No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support.

No inspections performed.

Inspected shroud support gusset welds and H8/H9 in conjunction with jet pump inspections. No indications Inspected areas in conjunction with jet pumps, included were gusset welds H8 and H9. H8 and H9 welds inspected at 0 and 180 degrees with 1 mil wire. No indications.

Inspected sample area 60-70 degree arc plus 180 degrees location on H8, H9, and gussets. No indications.

RF06 VT-3*

  • Inspection performed in conjunction with jet pump inspections.

Approximately 50% of the gussets and H8 and H9 welds were inspected. This was a best effort exam which ranged from MVT-1 to VT-3 depending on camera angle and lighting. No cleaning was performed. No indications identified.

RF07 EVT-1

  • Inspection performed in conjunction with jet pump inspections. Remaining 50% of the gusset welds were inspected.

This was a best effort exam which ranged from EVT-1 to VT-3 depending on camera angle and lighting. (Credited as a n EVT-1 exam) No cleaning was performed or needed. No indications

( '

identified. The H8 and H9 welds were inspected in detail at 0 and 180 Deg.

Azimuth to EVT-1 standards where there were no obstructions.

RF08 EVT-1 The H8 and H9 welds were reinspected to achieve required coverage. 22% of both welds were inspected and included the areas at 0 and 180 degrees as well as adjacent to Jet Pumps 2 and 3.

I Accessible areas on Gussets 1, 3, 11, 12, and 22 were inspected. No indications of cracking identified.

RF09 EVT-1 The H8 and H9 welds were inspected VT-1 adjacent to Jet Pumps 3 and 4(Coverage obtained 1%and8.3%). Accessible

/

'- I areas on Gussets 2 and 15 inspected (90% coverage on each obtained). Both

(

access hole covers were inspected (VT-1). No indications identified.

RFlO EVT-1/

The H8 and H9 welds were inspected VT-1 adjacent to Jet Pump 5(Coverage obtained 1 % and 8.3%). Accessible areas on Gussets 7 and 8 inspected (70/90% coverage obtained @VT-1 quality, EVT-1 not credited, CARD 05-20378). No indications identified.

22

- /

RFll EVT-1 The H8 and H9 welds were inspected at 0 and 180 degrees as well as several other locations. Coverage obtained was 24%

for H8 and 30% for H9. Accessible areas on Gussets 5, 6, 7, 8, 9, 10, 18, and 21 were inspected with 50% to 80%

coverage obtained@EVT-1. No indications identified.

UT A portion of the H9 weld was examined from the vessel outside diameter using a manual technique as required by BWRVIP-104. Approximately 19.6% of weld was examined with no indications.

RF12 EVT-1 Accessible areas on Gussets 4 and 13 were inspected with 55% to 80%

coverage obtained using EVT-1. No indications identified. Both Access Hole covers were inspected per draft BWRVIP

-180 requirements. Cracking identified on 0 degree cover. Reference OE 25794.

RF13 EVT-1 Accessible areas on Gussets 5 and 6 were inspected with 75% coverage obtained using EVT-1. No indications identified.

j The 0 Degree Access Hole cover was reinspected and no additional cracking was identified. No repair installed.

RF14 EVT-1 Accessible areas on Gussets 1, 21, and 22 (10/10) were inspected with 50% - 60% coverage obtained using EVT-1. No indications identified. All 3 welds on the 0 Degree Access Hole Cover were reinspected and no additional cracking was identified.

No repair installed.

RF15 EVT-1 Accessible areas on Gussets 4, 5, 6, 13, (04/12) 16, and 17 were inspected with 50% to 70% EVT-1 coverage obtained. No indications identified. The H8 and H9 welds were EVT-1 visually inspected from the annulus side with combined coverage at several locations of 15.9%

for the H8 weld and 20.5% for the H9 weld. No indications identified.

23

RF16 EVT-1 Accessible areas on Gussets 11 and 12, (2014) as well as the 180° Access Hole Cover were inspected with 90% coverage and no indications were identified. All 3 welds on the 0° Access Hole Cover were re-inspected. No additional cracking was identified and the component was evaluated to be acceptable without repair.

RF17 EVT-1 Accessible areas on Gussets 14, 15, and (2015) 18, were inspected with 35% to 65%

coverage and no indications were identified.

Core Spray Piping each outage VT-1 During RF-01 two small arc strikes were (BWRVIP-18/18-A)

RFOl thru (lmil) identified on loop piping. These have RF04 been reinspected each outage. No change in condition. fuspections performed per IEB 80-013 and SIL 289.

No indication of cracking.

RF05 EVT-1 All welds brushed prior to inspection (1/2mil) using 1/2 mil wire. Remainder of loop VT-1 piping inspected without brushing. No indication of cracking.

RF06 EVT-1 fuspected all welds on both loops of core spray to EVT-1 standards as opposed to BWRVIP-18 requirements ofMVT-1.

Cleaning assessment was performed -

cleaning was not necessary. No indication of cracking.

RF07 EVT-1 fuspected all welds on both loops of core spray to EVT-1 standards. Cleaning assessment was performed - cleaning was not necessary. No indication of cracking.

RF08 EVT-1 fuspected all welds on both loops of core spray to EVT-1 standards. Cleaning assessment was performed, cleaning was not necessary. No indication of cracking.

RF09 EVT-1 fuspected all target welds on both loops of core spray and sample welds on Div 2 to EVT-1 standards. Cleaning assessment was performed, cleaning was 24

not necessary. No indications of cracking.

RFlO EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 2 to EVT-1. Cleaning assessment was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately but generally >80%.

RFll EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 1 to EVT-1. Cleaning assessment was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately

)

but generally >80%.

RF12 EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 1 to EVT-1. Cleaning assessment was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately but generally >55%.

RF13 EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 2 to EVT-1. Cleaning assessment

  • ._)

was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately but generally >55%.

RF14 EVT-1 Inspected all target welds on both loops (10/10) of core spray and rotating sample welds on Div 2 to EVT-1. Cleaning was performed for all locations and welds were hydrolazed or brushed. No indications of cracking. Inspection coverage reported separately but generally >60%.

25

RF15 EVT-1 Inspected all target welds on both loops (4/12) of core spray and rotating sample welds on Div 1 to EVT-1. Cleaning was performed for all locations and welds were brushed. No indications of cracking. Inspection coverage reported separately but generally >60%.

RF16 EVT-1 Inspected all target welds on both loops (2014) of core spray and a rotating sample welds on Div 1 with no indications of cracking observed. Brushing was performed on all locations. Inspection coverage is reported separately in Art. 2, but

'\\

averaged 58%.

RF17 EVT-1 Inspected all target welds on both loops (2015) of core spray and a rotating sample welds on Div 2 with no indications of cracking observed. Brushing was performed on all locations. Inspection coverage is reported separately in Art. 2, but averaged 60%.

Core Spray Sparger each outage VT-1 (1 During RFO 1 one arc strike identified on (BWRVIP-18/18-A)

RF01-RF04 mil) upper CS sparger. Reinspections have not identified any changes. No indication of cracking RF05 VT-1/

1/2 mil wire used for junction box EVT-1 remainder utilized lmil wire. No (1/2mil) indication of cracking.

RF06 EVT-1, Inspected per BWRVIP-18 using EVT-1 MVT-1 for sparger T-box and end caps and MVT-1 for remaining locations. No indications of cracking.

\\

RF07 EVT-1/

Inspected per BWRVIP-18 using EVT-1 VT-1 for sparger T-box welds, end cap welds, drain plug welds, and support brackets and welds, and VT-1 for flow nozzles and tack welds. No indications of cracking identified.

RF08.

EVT-1/

Inspected per BWRVIP-18 using EVT-1 VT-1 for Sl, S2 and S4 welds. Selected S3a, S3b welds inspected using VT-1.

Selected S3c welds as well as selected 26

\\

I

\\

r

(

\\

'"- _)

I

)

J

(

\\.,'

.J 1._.J RF09 EVT-1/

VT-1 RFIO EVT-1/

VT-I RFll EVT-1/

VT-1 RF12 EVT-1/

VT-1 RF13 EVT-1/

VT-1 27 SB bracket welds were inspected using EVT-1 technique. A best effort exam was performed on all accessible areas.

No indications of cracking identified.

Inspected per BWRVIP-18 using EVT-1 for 50% of the SI, S2 and S4 welds and VT-I for 50% of the S3a, S3b and S3c welds on the same spargers. 9 SB bracket welds were inspected using EVT-1 technique. Coverage for specific welds will be reported separately. No indications of cracking were identified.

Inspected per BWRVIP-18 using EVT-1 for 50% of the Sl, S2 and S4 welds and VT-1for50% of the S3a, S3b and S3c welds on the same spargers. 6 SB bracket welds were inspected using EVT-1 technique. Coverage for specific welds will be reported separately but was >

60% for welds and >85% for brackets.

No indications of cracking were identified.

Inspected per BWRVIP-18-A using EVT-1for50% of the SI, S2 and S4 welds on the same spargers. 6 SB bracket welds were inspected using VT-1 technique. Coverage for specific welds will be reported separately but was >

50% for welds and >75% for brackets.

No indications of cracking were identified Inspected per BWRVIP-18-A using EVT-1for50% of the SI, S2 and S4 welds on the same spargers. 6 SB bracket welds were inspected using EVT-1 technique. Coverage for specific welds will be reported separately but was >

40% for welds and >75% for brackets.

No indications of cracking were identified.

Inspected per BWRVIP-18-A using EVT-1for50% of the Sl, S2 and S4 welds on the same spargers. 6 SB bracket welds were inspected using EVT-

1 technique. Coverage for specific welds will be reported separately but was>

50% for welds and >70% for brackets.

No indications of cracking were identified.

RF14 EVT-1/

Inspected per BWRVIP-18-A using (10/10)

VT-1 EVT-1for50% ofthe Sl, S2 and S4 welds on the C and D spargers. 6 SB bracket welds and S3 nozzle welds were inspected using VT-1 technique.

Coverage for specific welds will be reported separately but was > 40% for welds and >60% for brackets. No indications of cracking were identified.

RF15 EVT-1/

Inspected per BWRVIP-18-A using (4/12)

VT-1 EVT-1for50% of the Sl, S2 and S4 welds on the A and B spargers. 6 SB bracket welds inspected using VT-1 technique. Coverage for specific welds will be reported separately but was >

40% for welds and >60% for brackets.

No indications of cracking were identified.

I I

RF16 EVT-1/

Inspected per BWRVIP-18-A using (2014)

VT-1 EVT-1for50% of the Sl, S2 and S4 welds on the A and B spargers. 6 SB bracket welds were inspected using VT-

1. Coverage for specific welds is reported separately in Attachment 2 but was > 40% for most welds and > 60% for most brackets. No indication of cracking I

1, was identified.

RF17 EVT-1/

Inspected 50% of the Sl, S2 and S4 (2015)

VT-1 welds on the A and B spargers using EVT-1 and 6 sparger bracket welds using VT-1. Coverage for specific welds is reported separately in Attachment 2 but averaged 46% for the welds and 50% for the brackets. No indication of cracking was identified.

Top Guide (Rim, etc.)

RF03 VT-lNT-3 Inspected 6 locations (RICSIL 059) and Beams (BWRVIP-26) rim area 0° and 180°. No indications.

(BWRVIP-183) 28

r' \\

I I

I

\\

I I

' )

,\\

i

)

(

/

, __./

I "--

RF04 VT-lNT-3 RF05 VT-1 RF06 VT-1 RF07 VT-1 RF08 VT-1 RF09 VT-1 RFIO VT-lNT-3 RF11 VT-lNT-3 RF12 VT-lNT-3 RF13 EVT-1 RF14 VT-3 (10/10)

RF15 EVT-1 (4/12) 29 fuspected 6 locations (SIL 554) and rim area 0° and 360°. No indications.

fuspected 15 locations (SIL 554). No indications.

fuspected bottom edge of beams at 11 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 8 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 5 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 6 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 2 core locations per SIL 554 and rim area 0° and 90°. No indication of cracking.

fuspected bottom edge of beams at 2 core locations per SIL 554. No indication of cracking. fuspected 90 degree segment of top guide rim (90° - 180°) and no indications were identified.

fuspected intersection and bottom edge of beams at 5 core locations per SIL 554.

No indication of cracking.

fuspected intersection and bottom edge of beams at 5 core locations per BWRVJP-183 utilizing a new visual inspection tool and rim area 0° - 90°. No indication of cracking.

fuspected rim area 0° - 180° with no indications identified.

Inspected intersection and bottom edge of beams at 5 core locations per BWRVJP-183 utilizing a new visual

inspection tool. No indication of cracking. Fabrication related conditions identified on the bottom surface of the plate material at 3 cell locations.

Inspected the rim area 180° - 360° with no indications.

RF16 NIA No inspections performed in RF16.

(2014)

RF17 EVT-1 Inspected intersection and bottom edge (2015) of beams at 9 core cell locations per BWRVIP-183 with no indication of cracking.

Core Plate Rim Bolts, RF05 VT-1 (lmil Inspected 6 core plate bolts located etc. (BWRVIP-25) wire) between 100 and 160 degrees and adjacent area. No indications.

RF06 VT-3 Inspected tops of approximately 20 bolts per SIL 588. No indications identified.

'* /

RF07 VT-3 Inspected tops of approximately 20 bolts

/

per SIL 588. No indications identified.

RF08 VT-3 Inspected tops of approximately 20 core plate bolts (VT-3) per SIL 588. Did not meet BWRVIP requirements. No indications identified.

RF09 NIA No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2003-117 and TJ-2003-01)

RFlO NIA No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2003-117 and TJ-2003-01)

RFll NIA No inspections performed. BWRVIP

  • -,,/

analysis concluded that inspections are not required. (Reference BWRVIP 2006-041 and DD-2006-01)

RF12 NIA No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2006-041) 30

/--,

J

/\\

I

\\

,-' '\\

(

./

)

\\

\\

'-I l _)

(

\\

l...__)

I -.

\\ __ )

cJ 1 \\_;

(_,/

SLC (BWRVIP-27)

RF13 NIA RF14 NIA (10110)

RF15 NIA (4112)

RF16 NIA (2014)

RF17 NIA (2015)

RF04 VT-3 RF05 -RF07 NIA RF08 VT-2*

RF09 VT-2*

RFlO VT-2*

No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2006-041)

No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2006-041) BWRVIP 2010- 243 now requires preparation of a Deviation Disposition by 313112011.

No inspections performed. BWRVIP analysis concluded that inspections are not required. Deviation Disposition DD-2011-01 was submitted to BWRVIP 313012011.

No inspections performed in RF16, as justified by Deviation Disposition DD-2011-01.

No inspections performed in RFl 7, as justified by Deviation Disposition DD-2011-01 Revision 1.

Performed a visual inspection from Reactor penetration to shroud support when access was provided during jet pump beam replacement. No indications.

No inspections performed as access was not provided.

Performed enhanced inspection on nozzle area from inside skirt area, but did not remove mirror insulation box from safe-end. No leakage observed.

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

Performed enhanced inspection on nozzle area from inside skirt area, and removed 31

/'--..

(\\

/

\\

\\

~

(

'., )

(

(_)

\\

~*

( '.

c (j

L G

(

/-'-

\\

\\,_,-'

I

\\

\\

\\_

'J RF11 RF12 RF13 RF-14 (10/10)

RF-15 (4/12)

RF16 (2014)

RF17 (2015) cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*/UT Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed. Performed a manual PDI qualified ultrasonic inspection of the nozzle to safe end weld as well as additional base material of bored material. No indications identified.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

32

r - "

(

I i

\\

( -.

r '

......__ __./

\\._ /

\\...___)

/.

Jet Pump Assembly Each outage VT-1, (BWRVIP-41) examine at VT-3 least 50%

thru RF05 RF06 MVT-1, VT-3 RF07 EVT-1 R_F08 EVT-1 33 Jet pump assemblies are inspected each outage from top to bottom. During RF-04 all (20) hold down beams were replaced as a preventative measure and to avoid performing UT' s on the old style/original beams. Inspections are performed to the recommendations of SIL 551, 574, 465 S-1, andRICSIL 078.

During RF05 one of the 80 restrainer screw tack welds was found to be cracked. This was evaluated and was not repaired during RF05.

Performed inspections to the intent of BWRVIP-41 as well as augmented VT-3 of selected areas on jet pumps 1-10.

Inspections included all High, Medium and Low Priority locations. Inspected RS-1 and RS-2 welds on jet pumps 11-

20. One indication identified on RS-1 weld, 1.75" long. JCO performed prior to start-up. No other new indications identified.

Performed inspections to the intent of BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected areas on jet pumps 11-20.

Inspections included all High, Medium and Low Priority locations. Reinspected previously identified indication on RS-1 weld, 1.75" long that was identified in RF06. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. No other indications or changes in previous indications identified.

Performed reinspections to the intent of BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected areas on jet pumps l& 2.

Inspections included all High, Medium and Low Priority locations. Reinspected previously identified 1.75" long indication on RS-1 weld for Jet Pumps 7&8 that was identified in RF06. No change in indication length or

appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all 20 jet pumps per recommendations of SIL 629 and verified no wedge damage (WD-1) as well as full contact with restrainer

(\\

screws. No damage identified on any

\\ -, *'

location. Reinspected all restrainer screw tack welds with no changes observed.

RF09 EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected areas on Jet Pumps 3 & 4. Inspections included all High, Medium and Low Priority locations. Reinspected previously identified 1. 7 5" long indication on RS-1 weld for Jet Pumps 7 &8 that was identified in RF06. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all 20 Jet Pump Hold Down Beams by UT for BB 1, BB2, and the transition area BB3 using the latest available technique from General Electric. No indications identified on the beams. Reinspected all restrainer screw tack welds, contact area, and wedges after both tack welds on Jet Pump 15 were fo1,rnd cracked. No other damage or indications identified on any I.... __,.!

location. Jet Pump 15 permanently repaired by the installation of an auxiliary spring wedge. (Reference CARD 03-16929)

RFlO EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 4, 5, 6, 7, & 8. Reinspected previously identified 1.75" long indication on RS-1 weld for Jet Pumps 7

& 8 that was identified in RF06. No change in indication length I appearance.

Existing Flaw Evaluation on hand **

prepared by GE referenced as acceptance limit. Reinspected auxiliary spring

'~ -

.I wedge on Jet Pump 15. No other damage or indications identified on any location.

34

' __ )

RFll EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 7, 8, 9, & 10. Reinspected previously identified 1.75" long indication on RS-1 weld for Jet Pumps 7

& 8 that was identified in RF06. No change in indication length I appearance.

Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all Jet Pump wedges after wear was identified on JP2 restrainer bracket. Performed inspection of other welds on Jet Pump 2 as required by BWRVIP-41. Auxiliary spring wedges installed on Jet Pumps 1 and 2 and a slip joint clamp was installed on Jet Pump 2 to restore integrity. No other damage or indications identified.

RF12 EVT-1 Performed reinspections to BWRVIP-41 including EVT -1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 7, 8, 9, 10, 11, & 12.

Reinspected previously identified 1.75"

\\

long indication on RS-1 weld for Jet Pumps 7 & 8 that was identified in RF06.

No change in indication length I appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all 20 Jet Pump Hold Down Beams. Inspected 12 Jet Pump wedges including the wedges and hardware (auxiliary spring wedges and slip joint clamp) installed in RF 11.

No other damage or indications identified.

RF13 EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 7, 8, 9, 10, 13, 14, 15, and 16.

Reinspected previously identified indication on RS-1 weld for Jet Pumps 7 /8 identified in RF06. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected 35

/---,

(\\

r-'

I

\\

\\ ~ __,,

,~

" -- J r',

1

\\

(

(\\ *

..._~ - )

1_~)

(

'-._ I

\\

RF14 EVT-1 (10/10)

RF15 EVT-1 (4/12)

RF16 EVT-1/

(2014)

VT-1 RF17 36 9 Jet Pump wedges. No other damage or indications identified.

Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on most Jet Pumps including RS-8/9 welds on all pumps. Reinspected previously identified indication on RS-1 weld for Jet Pumps 7/8. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit.

fuspected all 20 Jet Pump wedges. Minor movement noted but no other damage or indications identified.

Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 's of selected welds on several Jet Pumps. Reinspected previously identified indication on RS-1 weld for Jet Pumps 7/8. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit.

fuspected all 20 Jet Pump wedges. No movement noted and no damage or indications identified.

Performed EVT-1 exams of selected welds in accordance with BWRVIP-41 Rev. 3 with no indications identified.

VT-1 exams performed on all 20 main wedge assemblies. Wedge wear identified on Jet Pump 06; scope expansion performed with no further relevant indications observed and wedge was evaluated to be acceptable without repair. Growth identified during re-inspection of indication on RS-1 weld for Jet Pumps 07/08. fudication was evaluated to be acceptable for two cycles without repair. Ultrasonic examination of all 20 Jet Pump Hold Down Beams (BBl, BB2 andBB3). No indications identified on the beams.

1\\

(2015)

EVT-1/

Performed EVT-1 exams of selected VT-1 welds with no indications identified. VT-1 exams performed on all 20 main wedge assemblies. Minor wedge rod wear identified on Jet Pump 01; evaluated to be acceptable without repair. Minor wear identified on Jet Pump 02 Auxiliary Wedge, scope expansion performed with no further relevant indications observed and evaluated to be acceptable without repair. Mitigating clamp installed on the RS-1 weld for Jet Pumps 07/08.

Jet Pump Diffuser Each outage VT-3 Diffusers will be sample inspected during (BWRVIP-41) refueling outages.

RF06 MVT-1 BWRVIP-41 on Jet Pumps 1-10 except

,',,---.\\

inaccessible areas. No cracking.

RF07 EVT-1 BWRVIP-41 on Jet Pumps 11-20 except inaccessible areas. No cracking identified. Welds DF-3, AD-1, and AD-2

,~ - \\

are inaccessible for inspection.

RF08 EVT-1 BWRVIP-41 reinspection on Jet Pumps 1 and 2 except inaccessible areas. No cracking identified. Welds DF-3, AD-1, and AD-2 are inaccessible for inspection.

\\

\\

RF09 EVT-1 BWRVIP-41 reinspection on Jet Pumps 3 and 4 except inaccessible areas. No cracking identified. Welds DF-3, AD-1, and AD-2 are inaccessible for EVT-1 I

\\

visual inspection, VT-3 performed. (TJ-2003-02 prepared as justification)

RFlO EVT-1 BWRVIP-41 reinspection of selected DF-1 and DF-2 welds on Jet Pumps 5, 6, 7, & 8. Performed access study for future performance of UT examinations of welds DF-3, AD-1, and AD-2. These welds are inaccessible for visual 1

.J inspection. VT-3 performed. No indications identified (Reference TJ-2003-02)

\\-.......'

RFll EVT-1 B WR VIP-41 reinspection of selected DF-2 welds on Jet Pumps 9 & 10.

37

UT Performed of UT examinations on a portion of a total of 17 DF-3, AD-1, and AD-2 welds using specialized tooling.

These welds are inaccessible for visual inspection. No indications identified (Reference DD-2006-02)

RF12 EVT-1 BWRVIP-41 reinspection of selected DF-1 and 2 welds on Jet Pumps 6, 11, &

12.

UT No UT examinations performed during RF12 due to tooling failures. These welds are inaccessible for visual inspection. (Reference DD-2006-02)

RF13 EVT-1 BWR VIP-41 reinspection of selected DF-1and2 welds on Jet Pumps 7, 13, &

14.

UT No UT examinations performed during RF13 due to tooling failures. These welds are inaccessible for visual inspection. (Reference DD-2006-02) r RF14 EVT-1 BWR VIP-41 reinspection of selected (10/10)

DF-1and2 welds on Jet Pumps 7, 8, 9, and 13-18. No indications identified.

\\. ___,

UT Completed baseline UT examinations on all 20 Jet Pumps Diffuser/Adapter DF-3, AD-1 and AD-2 welds, (60 welds) since

  • ,_)

these welds are inaccessible for visual inspection. Deviation Disposition is no longer needed.

f

\\.,

~I

(

RF15 EVT-1 BWRVIP-41 reinspection of selected

\\._,/

(4/12)

DF-1 and 2 welds on Jet Pumps 10, 19, and 20. No indications identified.

RF16 EVT-1 BWRVIP-41 re-inspection of selected

/

(2014)

DF-1 and 2 welds on Jet Pumps 01, 02, and 11. No indications identified.

RF17 EVT-1 BWRVIP-41 re-inspection of selected (2015)

DF-1 and 2 welds on Jet Pumps 03, 04, and 12. No indications identified.

38

CRD Guide Tube RF04 VT-3 Inspected lower portion of peripheral (BWRVIP-47) guide tubes and stub tubes when access was provided during jet pump hold down beam replacement. No indications identified.

RF07 EVT-1 and Performed best effort exam on CRGT-3 VT-3 as weld was not visible on inside of tube.

CRGT-2 not accessible due to flow and ARPIN was not felt to be accessible. No indications identified.

RF08 EVT-1 and Performed best effort exam on CRGT-3 VT-3 as weld was not visible on inside of tube.

(,~ -\\

CRGT-2 not accessible due to flow and

(

\\

PS/GT-ARPIN was not felt to be accessible. No indications identified.

RF09 EVT-1 and Performed exams on CRGT-1, CRGT-2, VT-3 CRGT-3, and PS/GT-ARPIN at 10 Control Rod Guide Tubes/locations. No indications identified.

( '

RFlO NIA No inspection performed in RFIO.

RF11 NIA No inspection performed in Rl l.

RF12 VT-3 Performed exams on CRGT-1 and PS/GT-ARPIN at 5 Control Rod Guide

~I Tubes/locations. CRGT-2 and CRGT-3 not performed or credited due to high flow conditions. No indications identified.

RF13 NIA No inspections performed in RF13.

\\,/

RF14 EVT-1 and Completed all remaining baseline

\\.._/

(10/10)

VT-3 inspections on the Control Rod Guide Tubes. Inspections performed on ( 4)

CRGT-1, and PS/GT-ARPIN locations and on (9) CRGT-2 and CRGT-3 locations. One manufacturing flaw identified that did not impact the functionality of the component.

RF15 NIA 39

~

I

(---....

I. '

)

(

"-~/

_..-f CRD Stub Tube *

(BWR VIP-4 7)

In-Core Housing *

(BWRVIP-47)

Dry Tube*

(BWRVIP-47)

(4112)

RF16 NIA (2014)

RF17 NIA (2015)

RF04 VT-3 RF04 VT-3 Each outage VT-1 RF06 VT-1 RF07 VT-1 RF08 VT-1 RF09 NIA RFlO VT-1 RF11 VT-1 No BWRVIP required inspections performed in RF 15.

No BWRVIP required inspections performed in RF16.

No BWRVIP required inspections performed in RF 17.

Inspected lower portion of peripheral guide tubes and stub tubes when access was provided during jet pump hold down beam replacement. No indications identified.

Small portion visible during jet pump beam replacement. No indication of degradation.

9of12 tubes found not completely seated. Performed all inspections per SIL 409 and RICSIL 073. No indications of cracking.

Reinspected 12 dry tubes. No change from previous condition. No cracking.

Inspected all 12 original design Dry Tubes. No change from previous conditions identified. No cracking identified.

Inspected all 12 original design Dry Tubes from two sides. No change from previous conditions identified. No cracking identified.

No inspections performed in RF09.

Inspected all 12 original design Dry Tubes from two sides. Linear indications identified on 7 tubes in the collar region above the pressure boundary weld.

Evaluated as acceptable for one cycle of operation. Plan to replace in RF 11.

(Reference CARD 04-25703)

Replaced all 12 Dry Tubes in RFl 1.

Performed baseline VT-1 and verified proper engagement in Top Guide.

40

RF12 NIA No inspections performed in RF12.

RF13 NIA No inspections performed in RF 13.

RF14 NIA No inspections performed in RF14.

RF15 NIA No inspections performed in RF15.

RF16 NIA No inspections performed in RF16.

(2014)

RF17 NIA No inspections performed in RFl 7.

(2015)

Instrument Penet.

  • Each outage VT-3 Inspected jet pump sensing lines and (BWRVIP-49 & 41) brackets each outage.

RF04 VT-3 SLC and peripheral bottom head penetrations inspected. No indications.

RF06 VT-3 Inspected JP sensing lines for pumps 1-

10. No indications.

RF07 VT-3 Inspected JP sensing lines for pumps 11 thru 20 only. No indications.

RF08 VT-3 Inspected JP sensing lines for Pumps 1 &

2 only. No indications.

\\

RF09 VT-3 Inspected JP sensing lines for Pumps 3 &

4 only. No indications.

RFlO VT-1 Inspected JP sensing lines for Pumps 5, 6, 7, 16, & 17. No indications RF11 VT-1 Inspected JP sensing lines for Pumps 6, 7, 16, & 17. No indications.

RF12 VT-1 Inspected JP sensing lines for Pumps 6, 7, 11, 12, 16, & 17. No indications.

RF13 VT-1 Inspected JP sensing lines for Pumps 6, 7, 13, 14, 16, & 17. No indications.

RF14 VT-1 Inspected JP sensing lines for Pumps 6, 7, 15, 16, 17, & 18. No indications.

41

RF15 VT-1 Inspected JP sensing lines for Pumps 6, 7, 16, 17, 19, & 20. No indications.

RF16 VT-1 Inspected JP sensing lines for Pumps 1, (2014) 2, 6, 7, 16, & 17. No indications.

RF17 VT-1 Inspected JP sensing lines for Pumps 3, (2015) 4, 6, 7, 16, & 17. No indications.

Vessel ID Brackets Each outage VT-1/3 Inspect sample population each outage.

(BWRVIP-48)

We have inspected most brackets each outage (core spray, feedwater). Jet pump riser brace, steam dryer support lugs, guide rod brackets and specimen holder brackets are sample inspected. No indications of cracking identified.

RF06 MVT-1 6 feedwater brackets.

All core spray piping brackets.

4 steam dryer brackets 1 guide rod bracket 1 specimen bracket.

No indication of cracking.

RF07 EVT-1 6 feedwater brackets.

All core spray piping brackets.

4 steam dryer brackets 1 guide rod bracket No indication of cracking identified.

RF08 EVT-1 6 feedwater brackets.

All core spray piping brackets.

t I

4 steam dryer brackets 1 guide rod bracket Surveillance holder and Brackets @ 30 az.

No indication of cracking identified.

RF09 EVT-1 6 Feedwater brackets.

4 Core Spray piping brackets.

1 Jet Pump riser brace (Jet Pump 3 and 4)

No indication of cracking identified.

RFlO EVT-1 6 Feedwater brackets.

3 Core Spray piping brackets.

1 Surveillance Holder bracket 4 Steam Dryer Support brackets 4 Steam Dryer Hold Down 1 Guide Rod Bracket 42

1 Jet Pump riser brace (Jet Pump 5 and 6)

No indication of cracking identified.

RFll EVT-1/

No inspections performed in RF-11.

VT-1 RF12 EVT-1/

6 Feedwater Sparger bracket sets.

VT-1 1 Surveillance Holder bracket 4 Steam Dryer Support brackets 1 Guide Rod Bracket 2 Jet Pump riser braces (Jet Pumps 7, 8, 9, & 10)

No indication of cracking identified.

RF13 EVT-1/

No inspections performed in RF-13.

VT-1 RF14 EVT-1/

3 Feedwater Sparger bracket sets.

(10/10)

VT-1 2 Core Spray Piping Brackets 1 Surveillance Holder bracket 4 Steam Dryer Support brackets 1 Guide Rod Bracket 2 Jet Pump riser braces (Jet Pumps 1/ 2, and 11/12)

No indication of cracking identified.

j RF15 EVT-1/

Inspections performed on 3 Feedwater (4/12)

VT-1 Sparger bracket sets and 1 Guide Rod Bracket. No indications identified.

RF16 EVT-1/

Inspection performed on 1 Surveillance (2014)

VT-1 Sample Holder Bracket. No indications identified.

RF17 EVT-1 I 2 Feedwater Sparger bracket sets (four (2015)

VT-I individual brackets) 4 Core Spray Piping Brackets 4 Steam Dryer Support Brackets 4 Steam Dryer Holddown Brackets I Guide Rod Bracket I Jet Pump Riser Brace.

No indication of cracking identified.

LPCI Coupling NIA NIA Fermi does not have a LPCI Coupling Shroud Head RF04 VTNT 16 had indications, 17 replaced during Bolts/Shroud Head RF04.

43

RF05 NIA Remaining bolts replaced (31) during RF05 as a preventative measure. All 48 are now new style.

RF06 VT-3 Bolts 1-24 (of 48). No indication of cracking.

RF07 VT-3 Bolts 25-48 (of 48). No indication of cracking or damage. Springs were left compressed on 20 of the 24 inspected.

RF08 VT-3 Bolts 1-24 (of 48). No indication of cracking or damage RF09 VT-3 Bolts 23 and 25-48 (of 48). No indication of cracking or damage. All retainer springs verified to be functioning properly.

RFlO VT-3 Bolts 1-24 (of 48). Inspected North 113rd of Shroud Head/Separator and 2 lifting lugs. No indication of cracking or damage RF11 VT-3 Inspected Bolts 25-48 (of 48) and inspected Center 113rd of Shroud Head/Separators. No indication of cracking or damage.

RF12 VT-3 Bolts 1-24 (of 48). Inspected South 1;3rd of Shroud Head/Separator and 2 lifting lugs. All mid support ring gussets were inspected and small short cracks were identified on 3 of the 24 gussets. No repairs were required. Ref. OE 25795.

RF13 VT-3 Bolts 25-48 (of 48). Inspected North 113rd of Shroud Head/Separator and 2 lifting lugs. No changes identified in previous indications identified in RF12.

No other indications identified.

RF14 VT-3 Bolts 1-24, 27, 30, & 33 (of 48).

(10/10)

Inspected Center 113rd of Shroud Head/Separator. No changes identified in previous indications and no new indications identified.

44

RF15 VT-3 Inspected Bolts 25-48 and 2 (of 48).

(4112)

Inspected South 1;3rd of Shroud Head/Separator. No changes identified in previous gusset indications and no new indications identified.

RF16 VT-3 Inspected Bolts 1-12 (of 48) and the (2014)

North 113rd of Shroud Head/Separator.

No new indications were identified.

RF17 VT-3 Inspected bolts 13-24 (of 48). Minor pin (2015)

& window wear identified on bolts 21 &

23, evaluated to be acceptable without repair. Replaced bolts 2 & 33 due to their inability to latch. Inspected the Center 1/3rd of the Separator and identified one tie bar with a severed attachment weld on one end. The tie bar was removed to preclude generation of a loose part (technical justification from OEM obtained to support acceptance of one missing tie bar).

Steam Dryer RF09 VT-3 Inspected approximately 1/3 of dryer (RFOl-RF-08 not including hood welds and cover plate previously reported) welds. (Ref. SIL 644) No indications of

)

additional cracking identified.

RFlO VT-1/VT-3 Inspected approximately 50% of dryer including all inner hood vertical welds as recommended in SIL 644, Supplement 1, and Revision 1 ). Several new indications were identified near welds due to new locations being inspected and the change in technique. Indications were noted at base of inner hood vertical welds.

Reference CARD 04-25416 and also OE

  1. 17600. No changes were identified on previously recorded indications.

RF11 VT-lNT-3 Inspected approximately 50% of dryer including all inner hood vertical welds as recommended in SIL 644, Revision 1 and BWRVIP-139. Several new indications were identified near welds due to new locations being inspected and the change in technique. Indications previously noted on hood welds in RF 10 were reinspected and no changes were noticed.

45

RF12 VT-lNT-3 Inspected approximately 50% of dryer including inner hood vertical welds as recommended in BWRVIP-139. Several new small indications were identified near welds due to new locations being inspected and the change in technique and camera angles used. Indications previously noted on hood welds were reinspected and no changes were noticed.

RF13 VT-lNT-3 Inspected approximately 20% of dryer including "F" Bank welds and a sampling of other locations following reinspection guidelines contained in NRC SE to BWRVIP-139. One new indication identified in support ring.

RF14 VT-lNT-3 Inspected approximately 20% of dryer (10/10) including "E" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. No new indications identified.

RF15 VT-lNT-3 Inspected approximately 20% of dryer (4/12) including "D" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. No new indications identified.

RF16 VT-lNT-3 Inspected approximately 20% of dryer (2014) including "C" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. Indication newly identified on interior vane bank weld HE-C-2-1; evaluated to be acceptable without repair.

RF17 VT-lNT-3 Inspected approximately 20% of dryer (2015) including "B" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. Indication on interior vane bank weld HE-C-2-1 identified in RF16 re-inspected with no changes observed. 24 capture plate assemblies 46

installed to cover all tie rod nut washer locations. Vertical drain channel welds preemptively increased from 1/8" to 1/4".

Dissimilar Metal RF-12 UT Performed ultrasonic examinations on 4 Welds BWRVIP Category B DM welds that contain alloy A (Not previously 82/182 using automated PDI qualified reported, reference techniques and procedures. Since >90%

BWRVIP letter 2008-coverage was not obtained on two welds, 089) 2 additional welds were selected and

>90% volume coverage was obtained.

No indications of cracking identified.

RF-13 UT Performed ultrasonic examinations on 5 Category B DM welds that contain alloy

(

82/182 using automated and manual PDI qualified techniques and procedures. No indications of cracking identified.

RF-14 UT Performed ultrasonic examination of 1 (10/10)

Category B DM weld that contained alloy 82/182 using manual PDI qualified technique and procedure. No indications of cracking identified.

RF-15 UT Performed ultrasonic examination of 1 (4/12)

Category B DM weld that contained alloy 82/182 using manual PDI qualified technique and procedure. No indications of cracking identified.

RF16 UT Performed ultrasonic examination of 3 (2014)

Category B DM welds using manual PDI

. _./

qualified technique and procedure. No indications of cracking identified.

RF17 UT Performed ultrasonic examination of 4 I

}

(2015)

Category B DM welds using PDI qualified phased array technique and procedure. No indications of cracking identified.

Bottom Head Drain RF16 RT Deviation Disposition DD-2014-01 Line (BWRVIP-205)

(2014) issued to support not completing radiography on the first elbow and piping immediately downstream of the reactor vessel in RF16. RT was performed on straight piping further downstream with no evidence of flow accelerated corrosion observed.

47

/

  • VT-2 leakage inspections have been and are performed on all RPV Instrumentation Nozzles and Piping Nozzles each refuel outage. An enhanced leakage inspection is performed on all locations to ensure no pressure boundary leakage. Inspections are performed in the annulus area adjacent to the vessel skirt, and are performed under vessel to ensure that any leakage identified is not from welded connections. Flange leakage from CRDM's is recorded, evaluated, and repaired if necessary.

Mirror insulation is opened for SLC safe end inspection and for bottom head inspections but is not removed from other locations unless the leakage source can't be determined.

48

Reactor Internals Inspection History Plant: Peach Bottom Atomic Power Station, Unit 3 Components in Date or Inspection Summarize the Following Information:

BWRVIP Scope Frequency of Method Inspection Results, Repairs, Inspection Used Replacements, Reinspections Core Shroud 1993 VT-1 Enhanced VT-1 (1 mil resolution) (100%

ID of H-3, H4, & V-3) portions OD ofH-1, H-2, H-3, H-4, H-5, H-6, and H-7 Prior to BWRVIP-01, Circumferential Indications on ID ofH-3 and H-4 (Plate side, not ring side)

Short circumferential indications on ID of V-3 weld.

Evaluation of indications showed full structural margins for one operating cycle.

1995 UT Comprehensive UT Baseline of all Category "C" circumferential welds (H-1 through H-7).

Baseline per BWRVIP-01, Rev. 1.

Exams per BWR-VIP Core Shroud NDE Uncertainty and Procedure Standard, dated November 21, 1994.

Indications identified on ID ofH-1, H-3, H-4, and H-5.

Full structural margins calculated using two cycles of crack growth.

' _/

No indications identified on H-2, H-6, and H-7.

1999 UT UT Examination on welds H-3 & H-4.

Re-identified indications on both welds.

Extent of indications within existing structural analysis.

2005 UT Two-sided UT of all 7 horizontal welds

, _ _/

(Hl thru H7) and 4 vertical welds (V3 thru V6). No indications at H2, H7, V4-V6 or ring side of any weld. One minor indication near V3. Indications at Hl, H3, H4, and H5 correlated with those previously identified. One indication at H6 (new). One deep indication at H4.

Characterized as thru-wall. Review of previous data (1995 and 1999) also 49

\\._/

\\ _,/

(

Shroud Support 201S 1993 1997 1999 2001 200S 2009 UT VT-1 VT-1 EVT-1 UT VT-I EVT-1 VT-1 UT VT-1 so characterized indication as thru-wall at that time. EVT-1 on OD surface did not identify any indications.

Comprehensive UT of all 7 horizontal welds (Hl thru H7) and 4 vertical welds (V3 thru V6) per BWRVIP-76 Rev. 1-A.

Recordable indications were found in the Hl, H3, H4, HS, V3, and V6 welds.

Indications indicative of "off-axis" indications were reported in the vicinity of the H4 weld. Core shroud welds H2, H6, H7, V4, and VS had no reportable indications. All welds are acceptable as-is for a 10 year re-inspection interval via a plant specific analysis.

Enhanced VT-1 (1 mil resolution), of portions ofH-8 weld, No indications identified.

VT-1 examination around perimeter of both access hole covers, No indications identified.

VT-1 of both access hole cover bolted repairs. No indications identified.

10 % of weld length of welds H-8 &

H-9 examined.

No indications identified.

10% ofH-9 weld length from vessel O.D.

No indications identified.

VT-1 of both access hole cover bolted repairs. No indications identified.

> 10% ofH-8 weld, betweenjet pump banks, in area of AHCs.

VT-1 of both access hole cover bolted repairs. No indications identified.

Accessible length ofH-9 between 0 and 180 degrees.

No indications identified.

VT-1 of both access hole cover bolted repairs. No indications identified.

,r- \\

I I

\\_ _j

\\ _)

/

\\_j 2011 Core Spray Piping 1980-present 1985 1993 1995 1997 1999 2001 2003 EVT-1 VT-1 (1 mil)

VT-1 (1 mil)

VT-1 (1 mil)

VT-1 (1 mil)

VT-1 EVT-1 VT-1 VT-1 EVT-1 VT-I EVT-1 51

> 10% of weld length for H-8 & H-9 welds, betweenjet pump banks, in area of AHCs. No indications identified Enhanced VT-1 (1 mil resolution) performed on piping and welds each refueling outage per IEB 80-13, Cracking discovered at tee-box to header pipe weld.

Welded repair plates installed on both header tee-boxes.

Cracking identified in downcomer slip joint (weld P-5), evaluation demonstrated structural margin for one operating cycle.

Additional cracking identified in 3 of 4 downcomer slip joint welds (P-5), repair clamps installed on all 4 downcomers to repair flawed welds.

4 Downcomer repair clamps, no indications identified.

All annulus piping welds, no indications identified.

VT-1 Examination of A, B, C & D Downcomer Repair Clamps & both Header Teebox welded repairs.

No indications identified.

All target welds plus 25 % sample of piping butt welds examined.

No indications identified.

EVT-1 of all target welds plus 25%

sample of butt welds examined. No indications identified.

Four downcomer repair clamps.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

('.

\\

(

\\

I

\\

I I

I

~/

' _I

('

'._J

\\

\\,_I

(

,_/

\\_ __ )

2005 2007 2009 2011 2013 2015 Core Spray Sparger 1980-present EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

VT-1 Four down comer repair clamps.

EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

VT-1 Four down comer repair clamps.

EVT-1 Internal core spray piping from N5 nozzles to core shroud replaced eliminating previously installed downcomer and T-box repairs. EVT-1 performed on two hidden thermal sleeve welds with no indications identified.

VT-1, VT-1 and VT-3 of entire core spray line, VT-3 brackets, and clamps after one operating cycle. Visual exams confirmed all repair hardware is in place/ has not changed from "as-installed" condition. No indications recorded.

VT-1 Enhanced VT-1 (1 mil resolution)

(1 mil) performed on piping and welds each refueling outage per IEB 80-13, No indications identified.

52

/

(~

I I

'-./

'-,J Top Guide (Rim, etc.)

1999 2003 2007 2011 2013 2015 1987 1993 EVT-1 VT-1 EVT-1 VT-1 EVT-1 VT-1 EVT-1 VT-1 VT-1 VT-1, EVT-1 UT VT-3 53 Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

No indications identified.

Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

No indications identified.

Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

No indications identified.

Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

~ 1.0" Indication noted on the shroud side of the 136 degree bracket weld Examination performed on the core spray sparger bracket 05 at 136°. No change in the indication as identified during the 2011 inspection.

VT-1 of all (12) sparger support brackets and 60% of core spray nozzle welds, end cap welds, drain plug and welds on "A thru D" nozzles and drains. No change noted on the sparger bracket 05 at 136° from 2011. No other indications identified.

UT examination performed on 40 cells.

No indications identified Visual (VT-3) examination of 9 cells (02-19, 46-11, 42-59, 58-19, 02-39, 10-51, 18-03, 22-03, and 58-35), per SIL 554.

No indications identified.

r\\

1) i f'

I

'_,/

l l

\\_ j

\\_~*

/

\\

\\. _./

~

I

'-.._j 1995 197 6-present 1997 2009 2011 Core Plate (Rim, etc.)

1995 1997 2011 SLC 1997 2003 2007 VT-3 Visual (VT-3) of3 cells (14-23, 22-31, and 46-23) per SIL 554.

No indications identified.

VT-3 VT-3 examination every other refueling outage per Section XI.

No indications identified.

VT-3 Top Guide Grid examined from above, no indications identified.

VT-1 Adjacent aligner pins at 180 and 270 deg.(per VIP-26), no indications identified.

EVT-1 EVT-1 of five top guide cell locations per BWRVIP-183 requirements. No indications identified.

EVT-1 EVT-1 of fourteen top guide cell locations per BWRVIP-183 requirements. No indications identified.

VT-3 VT-3 examination of hold down bolt retainers planned, deferred to 1997.

VT-1 Examined 18 of 34 bolts/retainers from above. No indications identified.

VT-3 Examined 9 of 34 bolts/retainers from above. No indications identified. This satisfies the 25% commitment from the submitted Deviation Disposition UT UT of nozzle to safe end planned for 1997, per BWRVIP recommendations PT&UT PT & UT of nozzle to safe-end weld, no indications identified.

PT Extended dwell time PT of SLC nozzle to safe end weld and entire safe end.

No indications identified.

PT PT of SLC nozzle to safe end weld.

No indications identified.

54

f'

  • I I

\\._/

I

\\, )

(~.

/

\\

,/ \\

\\__)

\\,__ )

'-,J Jet Pump Assembly 2011 UT 1974 to VT-3 present 1981 VT&UT 1997 VT-3 CSVT-1 (MVT-1) 1999 UT 1999 EVT-1 55 UT of SLC nozzle to vessel and nozzle to safe end weld. No indications identified Visual VT-3 of all jet pump components performed every other refueling outage.

No indications identified.

VT and UT examination performed on all 20 hold down beams/

One beam found to be cracked, replaced with new style beam, All beams replaced with new style beam and reduced preload in 1988.

VT-3 all 20 jet pump assemblies (all parts),including CSVT-1 (MVT-1) of 10 riser braces, including all welds. No indications identified.

CSVT-1 (MVT-1) all 10 thermal sleeve to riser elbow welds, plus UT on pumps 1/ 2, 9/10, 13/14 due to indications on thermal sleeve side of these welds.

MVT-1 on welds RS-2 & RS-3 of three risers w/ indications@ 30, 150, and 300 degrees.

Evaluation of indications justified continued operation for part cycle.

Examinations performed on all 20 hold down beams. Reportable indications observed on hold down beam for jet pump

  1. 20. Beam replaced.

No other indications identified.

Examination of high priority Adapter welds on Jet Pumps 1-10.

Reportable indications on welds (AD-3b )

of Jet pumps 2 & 10. BWRVIP-41 evaluation resulted in use-as-is disposition. Expanded examinations to weld AD3b on Jet Pumps 11-20. No other indications identified.

EVT-1 examination of high priority Diffuser Shell to Tailpipe Welds ( DF-2) of Jet Pumps 1-10. No indications identified.

Examination of Riser welds RS-2 & RS-3 of Jet Pump Assemblies 2, 3 & 4.

No indications identified.

2001 EVT-1 Reexamined weld AD-3b on Jet Pumps 2

& 10. indications remain bounded by existing flaw evaluation.

All 20 WD-1 locations examined. 16 high priority and 45 medium priority welds on inlet mixers, diffusers, and riser braces also examined. No indications identified.

,,'~ \\

2003 VT-1 VT-1 of all twenty hold down beam

,~

ratchet lock keepers (replaced in 2001).

VT-1 all twenty WD-1 main wedge locations, since all inlet mixers were removed in 2001, Two auxiliary spring wedges installed in 2001, and the RS-1 repair clamp on JP 1 & 2 and 13 & 14.

No indications identified.

EVT-1 Reexamination of indication at RS-1 weld on JP 9 & 10.

Minimal change in flaw size. Structural reevaluation completed for continued acceptability.

104% of High priority welds completed.

72% of Medium priority welds completed No indications identified.

Indication identified in backing ring below AD-3a weld on JP 18. Structural evaluation found acceptable for continued operation.

2005 UT Two-sided UT of all diffuser and adapter welds (100) from l.D. Identified 4 small OD originating indications associated J

with the AD-3b fillet weld (2 previously ID'd). Structural and leakage evaluation proved acceptability for numerous operating cycles.

VT-1 VT-1 of five main wedges. No wear identified.

56 I

EVT-1 EVT-1of16 medium priority welds. No indications identified.

EVT-1of3 existing indications. No appreciable change in indication size.

2007 VT-1 VT-1 of 10 main wedges and 2 RS-1 riser repair clamps. No indications identified.

EVT-1 EVT-1 of 30 medium and high priority welds, 1 existing RS-1 weld indication and 12 riser brace welds. No growth of existing indication noted. Small indications identified at the RS-1 weld of two risers. Structural and leakage impact evaluations found indications acceptable for continued operation. No other indications identified.

2009 VT-1 VT-1 of 6 main wedges. Minor wear identified on 3 wedges. Expanded scope to examine all 20 main wedges and performed examinations on additional locations (AS-1/2, RS-6/7, RS-8, RS-9, MX-7) on the 3 JPs with identified wear.

Two set screw gaps identified. No additional indications in expanded scope exams. No repair hardware required.

EVT-1 EVT-1 of 31 medium and high priority welds.

3 existing RS-1 flaws were examined.

- 1 existing indication exhibited no growth and was evaluated as acceptable for two cycles of continued operation.

- 1 existing indication exhibited growth and was evaluated as acceptable for

\\.. - '

two cycles of continued operation.

- 1 existing indication was determined to be the toe of the weld. No indication exists.

No other indications identified.

2009 VT-3 VT-3 of two aux spring wedges. No indications identified.

57

2011 2013 VT-1 EVT-1 UT VT-1 EVT-1 EVT-1 58 A VT-1 of the BB-4 regions of all 20 JP hold down beams was performed with no indications identified. VT-1 examinations were performed on the following components with no indications identified: JP 01/02 RS-1 clamp, JP 13/14 RS-1clamp,JP04 MX-7 and JP 10 MX-

7. Recordable indications were identified on 10 JP wedges, 3 wedges were existing wear no change, 2 JPs had new minor wedge wear and 5 had minor rod wear.

EVT-1 of 53 medium and high priority locations

  • 2 existing RS-1 flaws were examined with no change in length
  • Set screw gaps identified on JP 03, 04 and 05 16 Hybrid Group 2 Hold Down Beams were examined no indications identified.

VT-1 of 10 wedge bearing surfaces WD-1 JPOl thru WD-1 JPlO was performed. No relevant change in indications from previous inspection.

EVT-1 of riser elbow to thermal sleeve weld RS-1 (JP 09/10 and JP 19/20).

Previously documented indication was observed with no apparent change in the indication from the previous inspection data.

EVT-1 of jet pumps JPs 03 and 05 vessel side and shroud side set screw gaps.

EVT-1 of JP 04 vessel side set screw gap.

New slight wear identified on the JP 03 SS, JP 03 VS and JP 04 VS belly band set screw interface. Comparison to P3Rl8 exam data identified these components had similar characteristics during the 2011 exam. No other indications identified.

2015 EVT-1, EVT-1 of ( 17) medium and high priority welds. 2 existing RS-1 flaws were examined with no change in length. No other indications identified.

VT-1, VT-1 of (2) riser clamps. No indications observed.

VT-1 often (10) JP main wedges. No new wedge wear was identified; however, wedge rod wear was identified on JP 11, JP12, JP15, and JP20. All previous wedge rod wear on JP09, JP16, JPl 7 and JP19 has not changed.

VT-3, VT-3 of the two (2) auxiliary wedges installed. No wear identified on JP14.

New wear on the JP09 aux. wedge and new wear into the belly band were noted.

The aux. wedge was in the over-travel position and accepted for continued use for one cycle.

EVT-1, A combination ofEVT-1 on the OD and UT UT from the ID on 10 jet pump diffuser/

adapter welds (AD-1, AD-2, DF-1, DF-2, AD3a/b and DF-3):

- UT diffuser scope: JP09, JPlO, JPl 1, JP12 and JP18. Previous indications on JP12 and JP09 AD3b showed small changes in length from 2005. JP18: 2of3 previous indications on AD3a showed no change from 2005. The third indication was not observed/ could not be found. All other welds were inspected SAT.

- EVT-1 diffuser scope: JP02, JP09, JPlO, JP13, JP14, JPl 7, JP18 and JP19.

Previous indication on JP02 AD3b showed no change from 2005. Previous indication on JPlO AD3b showed small change in length from 2005.

All conditions were evaluated as acceptable.

59

Jet Pump Diffuser See Jet Pump Assembly.

CRD Guide Tube 1985 VT-3 VT-3 PSI examination of 4 replacement CRD housings.

1987 VT-3 VT-3 examination of one of replaced housings.

No indications identified.

1991 VT-3 VT-3 examination of housings accessible from fuel cells 26-31and30-27.

No indications identified.

1999 VT-3 VT-3 examination on Guide Tube welds CRGT-1 & Alignment Pin weld (Core Locations: 14-15, 14-31, 14-47, 18-19, 18-27, 18-35, 18-43, 26-11, 34-35, 42-19)

No indications identified.

EVT-1 EVT-1 examination on Guide Tube welds CRGT-2 & 3 (Core Locations:14-15, 14-31, 14-47, 18-19, 18-27, 18-35, 18-43, 26-11, 34-35, 42-19)

No indications identified.

2003 EVT-1 Best effort EVT-1 on Guide Tube welds CRGT-2 & 3 (Core locations: 10-35, 22-27, 22-35, 30-23, 30-31, 30-39, 38-27, 38-31, 38-35, and 42-31) No indications identified.

VT-3 VT-3 examination on Guide Tube welds CRGT-1 & Alignment Pin weld (Core Locations: 10-35, 22-27, 22-35, 30-23, 30-31, 30-39, 38-27, 38-31, 38-35, and 42-31) No indications identified.

2005 EVT-1 EVT-1 on Guide Tube welds CRGT-2 &

3 (Core locations: 22-39, 38-39, 14-35, 46-35, 46-27, 22-23, and 26-11) No indications identified. CRGT-3 (22-39) later disqualified.

60

VT-3 VT-3 examination on Guide Tube welds CRGT-1 & Alignment Pin weld (Core Locations: 22-39, 38-39, 14-35, 46-35, 46-27, 22-23, and 26-11) Alignment pin weld also at 14-27 and 38-23, No indications identified.

CRD Guide Tube 2007 EVT-1 EVT-1 on Guide Tube welds CRGT-2 (cont.)

(Core locations 22-03, 30-15, 42-03, 46-55, 58-39) and CRGT-3 (Core locations 22-03, 30-15, 42-03, 46-55, 58-39). No indications identified.

Verification of CRGT-1 (Core locations 22-03, 30-15, 42-03, 46-55, 58-39) alignment pins and alignment lug welds.

No indications identified.

2009 EVT-1 EVT-1 on Guide Tube welds CRGT-2 (Core locations 14-31, 22-31, 22-59, 30-47, 50-51)

No indications identified.

CRD Stub Tube 1991 VT-3 VT-3 of accessible portions of 12 stub tubes (30-35, 26-35, 22-35, 22-31, 22-27, 26-27, 26-23, 30-23, 34-23, 34-27, 34-31, 30-31).

No indications identified.

In-Core Housing 1991 VT-3 VT-3 of housings accessible from fuel cells 26-31 and 30-27.

No indications identified.

Dry Tube 1997 NIA All Dry Tubes replaced in 1985.

All IRM and SRM tubes replaced w/

Wide Range Monitoring tubes in 1997.

No inspections required.

2015 VT-3 3 spare dry tubes (no WRNM detector installed) at core locations 16-45, 40-21 and 40-45 were found not fully engaged into the top guide. The observed conditions are acceptable as there remains enough insertion into the notches to laterally support the dry tube.

61

Instrument 1976 to PT PT examination performed on all Penetrations present instrument nozzle to safe end welds once per interval, per Section XI.

No indications identified.

1997 PT PT nozzle to safe-end (coupling) & safe-end to pipe welds on 2 nozzles. (N12A &

N12B). No indications identified.

2001 PT PT nozzle to safe-end (coupling) welds on 2 nozzles. (Nl lA & N16A). No indications identified.

Vessel ID Brackets 1976 to VT-1 or VT-1 and VT-3 of all ID bracket welds present VT-3 performed once per interval No indications identified.

1997 VT-1 All 10 Jet Pump riser brace to vessel welds, no indications identified.

1999 EVT-1 EVT-1 examination performed on 8 Core Spray Bracket Pads@ 15, 117, 123, 165, 195, 237, 243 & 345 AZ.

No indications identified.

2001 EVT-1 EVT-1 examination performed on 4 Feedwater Sparger brackets @ 4, 56, 64, and 116 Az., 3 Jet Pump Riser Braces@

90, 120, and 150 AZ., and 2 Steam Dryer Support Brackets @ 4, and 94 AZ. No indications identified.

2003 VT-1 Lower Surveillance Specimen brackets at 30°, 120°, and 300°.

VT-3 Upper Surveillance brackets at 30°, 120°,

and 300°.

Guide Rod brackets at 0° and 180°.

EVT-1 &

Steam Dryer support brackets at 184 ° and VT-3 274°.

EVT-1 Jet Pump riser brace to vessel welds JP 9/10 and JP 13/14.

No indications identified 2005 EVT-1 8 Feedwater sparger bracket welds and 16 jet pump riser brace welds. No indications identified.

62

2007 EVT-1 8 Core Spray pipe support brackets and one jet pump riser brace. No indications identified.

VT-3 4 Steam dryer hold down bracket welds.

No indications identified.

2011 EVT-1 Steam dryer support brackets at 004 °,

094°, 184°and 274° were examined with minor wear and rub marks found. The conditions were evaluated acceptable.

The upper guide rod bracket attachment welds at 0° and 180° were examined with no recordable indications identified.

The feedwater sparger brackets at the 030°, 090°, 150°, 210°, 270° and 330° sparger locations were examined with no recordable indications identified.

The jet pump riser brace to vessel welds for JPs 01/02, 09/10, 11/12 and 13/14 were examined with no recordable indications identified.

2015 EVT-1, Lower and Upper Surveillance Specimen VT-1 Holder (SSH) bracket attachment welds at 30, 120, and 300 degrees were examined.

No indications were noted on the attachment weld on SSH 030 deg. Wear was only identified on the vertical portion of the interface between the SSH and the bracket. The wear is minor and does not impact the bracket or specimen holder.

8 Core Spray pipe support brackets inspected. No indications identified.

LPCI Coupling NI A for this plant Steam Dryer 2003 VT-3 VT-3 of the entire top of the dryer (including all upper tie bars) and the 2 outer bank hoods and cover plates.

VT-1 VT-1 of 5 new central bank upper tie bars (added in 2001 ), 2 stop-drilled indications at the lower guide rod followers, and all GE SIL 644, Supp. 1 locations on outer bank hoods.

No indications identified. All previous repairs were satisfactory.

63

2005 VT-1 Completed all remaining BWRVIP-139 recommended inspections (68 locations).

No indications identified.

2007 VT-1 VT-1 of 23 high stress welds and all upper tie bars. No indications identified 2009 VT-1 Re-examination of six "red" end bank welds, two "green" drain channel welds, and welds on four lifting lugs per BWRVIP-139-A. No indications identified 2011 VT-1-89 Examinations were performed on the end panel plate to cover plate weld, end panel plate to sloped hood plate weld and end panel plate to vain cap plate weld on both the left and right end of bank 6 of the steam dryer. No recordable indications were identified. The lifting rods at 045°,

135°, 225°and 315° were examined with no recordable indications.

2013 VT-1 VT-1 examinations performed on steam dryer seismic brackets (SDSB) at 004°,

094 ° and 184 °. No additional wear was observed from the previous examination.

VT-1 on steam dryer lifting rod assemblies at 45°, 135°, 225° and 315°.

A new indication was noted on the northeast tack weld of the 225° lifting rod.

No recordable indications were identified on the other three lifting rod assemblies.

2015 Replacement As part of the EPU License Amendment Request (LAR), Exelon PBAPS replaced the Original Equipment Manufacturer (OEM) steam dryer with a 3-ring octagonal (Nordic style) Westinghouse dryer.

Steam Separator 2007 VT-1 VT-1 examinations performed on a sample of upper and lower shroud head bolt support ring gussets. No indications identified.

64

2009 VT-1 VT-1 examinations performed on a sample of upper and lower shroud head bolt support ring gussets. No indications identified.

2011 VT-1-89 Examinations were performed at four locations on both the lower support ring gussets and the upper support ring gussets. No recordable indications were identified. Examinations were performed on the separator standpipe tie straps minor historic damage was observed conditions were acceptable. A VT-1 examination was performed on shroud head bolt 07, indicator window and pin wear observed.

As a result, SHB 07 was removed. The four lifting lugs were examined with no recordable indications identified.

2013 VT-1 The four lifting lugs were examined with no recordable indications identified.

2015 VT-1, Examinations were performed on the VT-3 separator standpipe tie straps and all ( 4) lifting lugs. Found several gouges in the base metal of the lifting lug at 67.5 deg and new wear that appears to be historic.

Bent Tie Straps at locations: 78 deg, 95 deg, 15 0 deg, and 311 deg azimuths and a previously removed tie strap at 220 deg.

All observed conditions were acceptable.

Dissimilar Metal 2009 No examinations scheduled.

Welds (BWRVIP-75-A) 2011 No examinations scheduled.

65

2013 UT Examinations performed on 7 IGSCC Category A welds per BWRVIP-75-A.

No recordable indications were identified.

The welds examined were a pipe bend to pipe weld in the RHR system (10-0-23),

the core spray nozzle to safe end weld (14-A-46), a recirculation inlet nozzle to safe end weld (2-BHC-8), 2 RHR pipe to tee welds (10-2DB20-17, and 10-2DD20-

22) and 2 RHR tee to elbow welds (10-2DB20-19 and 10-2DD20-24). The last

( 4) RHR welds identified above were added during P3R19 (Fall 2013) as a result of EPU.

2015 PAUT 2 dissimilar metal welds (3-I-20: Category A and 12-I-2R: Category C) and 1 weld overlay (12-I-lC) were inspected using manual Phased Array UT. Areas ofless than minimum wall thickness allowable limit were discovered on 12-I-2R. The thinned piping and downstream elbow were replaced. A transition stainless steel piece was installed between the valve and the elbow. All other welds were inspected SAT. Additionally, as a result ofEPU, (4) welds were added to the RHR system during P3R20 (Fall 2015). These (4) welds are Category A welds: 10-2DA20-24, 10-2DA20-25, 10-2DC20-l 7, and 10-2DC20-19.

RPV Shell Welds 2015 UT RPV Shell Welds VlA,B,C thru (BWRVIP-05)

V5,A,B,C and circ. weld C6 were examined. The examinations were performed using automated Phased Array UT. Two indications were observed in the circumferential weld exam volume (C-6 shell to flange). The indications are subsurface flaws and allowable IA W Table IWB 3510-1 of ASME XI 2001 Ed, 2003 Ad.

66

(

I

\\

J i

\\,

\\ __

I 1,

~I

\\_,

\\~,;

(

)

BWR Vessel and Internals Project Vessel Internals Inspection Summaries for Fall 2015 Outages June 2016 1

Plant

1. Dresden Unit 2
2. Fermi Unit 2
4. Peach Bottom Unit 3 END Table of Contents 2

3 20 49 66

/

i

\\,

Plant: Dresden Unit 2 Components in BWRVIP Scope Core Spray Piping Reactor Internals Inspection History Date or fuspection Summarize the Following fuformation:

Frequency of Method fuspection Results, Repairs, fuspection Used Replacements, Reinspections 1980s to UT, VT-1 IEB 80-13 (1 MIL) VT-1 of piping and D2R14 (lMIL) welds in annulus. fudications observed at one lower elbow to riser weld (3P4c) and two collar to shroud pipe welds (3 and 4P8a) in 1995. All flaw lengths verified with UT. Full structural margins met on all three flawed welds for additional cycle. No repairs performed.

3/1998 UT, GE CSI-2000 fuspected with EVT-1 D2R15 0.0005" supplement for unqualified welds (P8a EVT and P4d). Identified three previously unidentified flaws (1P5, 2P8a and 3P4d) for a total of six flaws. All flaws were analyzed for two additional cycles of operation with no repairs required.

Previously identified flaws were determined to be of the same or less extent than originally sized. 1P5 and 2P8a were not visually verified.

10/2000 EVT-1 Core Spray Piping: P8a and P4d, D2R16 EVT-1 @all four locations. Previous indications have been found on the Core Spray Elbow to Collar on the 260° Downcomer. The results of the 1999 measurements compared with the two previous 1998 indications are as follows.

It appears that the Collar indication has not changed, while the indication on the elbow is larger this year than was seen in 1998. The noted crack growth was bounded by the previous flaw evaluation and the BWRVIP-18 crack growth value.

10/2001 UT, GE CSI-2000 inspected a complete D2R17 EVT-1 Target Set and a sample of P4 welds. No new flaws. Growth within Fracture Mechanics Evaluation predictions.

Performed EVT-1 ofundemonstrated welds.

3

10/2003 EVT-1, Excessive grinding exam of l-4P4a and b D2Rl8 VT-1 (VT-1). Undemonstrated l-4P8a and P4d(EVT-1). Flaws are unchanged.

11/2005 UT, GE CSI-2000 inspected all demonstrated D2Rl9 EVT-1 welds. Previous flaws re-sized, growth within flaw evaluation and BWRVIP-18 predictions. EVT-1 all undemonstrated welds. No new flaws identified.

EVT-1 25% (2) piping bracket assembly welds. NRI.

11/2007 EVT-1 EVT-lofpiping welds Pl, P2, P3 P8a, D2R20 P8b and 25% of P4a, P4b, P4c and P4d in accordance with BWRVIP-18. Rls for previous indications in 3P4d, 3P8a, 4P8a.

11/2009 EVT-1 EVT-lof all Pl, P2, P3 and 25% of P4a D2R21

& b piping welds in accordance with BWRVIP-18. NRI.

Performed Core Spray Lower Sectional Replacement on all four lines. Welds P4c & d, P5, P6, P7, P8a & band P9 all replaced. One P9 weld was examined after the old pipe was removed with no relevant indications. The other three P9 welds were destroyed by the EDM cut and could not be inspected.

10/2011 EVT-1 EVT-lof all Pl, P2, P3 and 25% ofP4a D2R22

& b piping welds. NRI.

EVT-1 on piping attachment welds on all four piping braces VT-lNT-3 Core Spray Lower Sectional Replacement (all 4 lines)

- VT-1 ofbolting, keepers, ratchet springs, latch springs, lateral pins, and keepers. NRI

- VT-3 of repair hardware. NRI 11/2013 EVT-1 EVT-lof all Pl, P2, P3 and 25% of P4a D2R23

& b piping welds. NRI.

11/2015 EVT-1 EVT-1 of all Pl, P2, P3 and 25% of P4a D2R24

& b piping welds. NRI.

4

(

\\

\\

"/

J f

' _)

Core Spray Sparger Vessel ID Brackets 1980s to pres en 3/1998 D2R16 10/2001 D2R17 11/2005 D2R19 11/2009 D2R21 11/2013 D2R23 11/2015 D2R24 4/1994 D2R15 3/1998 D2R16 VT-lNT-3 VT-1 (1 MIL)

EVT-1, MVT-1 EVT-1, VT-1 EVT-1, VT-1 EVT-1, VT-1 EVT-1, VT-1 VT-1 VT-1 MVT-1 5

Core Spray Lower Sectional Replacement (all 4 lines)

- VT-1 of bolting, keepers, ratchet springs, latch springs, lateral pins, and keepers. NRI

- VT-3 ofrepair hardware. NRI.

IEB 80-13 (1 MIL) VT-1 of spargers and tee-boxes. No indications found.

Future inspections per BWRVIP-18.

End caps, cover plates and tee box branch welds were EVT-1 examined (OD). All sparger connections and bracket welds were MVT-1 examined.

NRI.

Complete Target Set and 50% of S3 welds. No Indications recorded.

EVT-1 100% Sl; S2; S4. NRI.

VT-1 50% S3. NRI.

VT-1 100% (12) SB. NRI.

EVT-1 100% S4. NRI.

VT-1 50% S3. NRI.

VT-1100% (12) SB. NRI.

S 1 and S2 structurally replaced by bracket as part of lower sectional replacement.

EVT-1 100% S4. NRI.

VT-1 50% S3. NRI.

VT-1100% (12) SB. One RI identified in heat affected zone of the 260° bracket. Indication acceptable for one cycle.

VT-1 of 260° bracket. Previous indication inspected with no change.

Section XI inspections of jet pump riser brace, dryer, feedwater sparger, core spray, and surveillance capsule holder brackets, performed once per interval.

No indications noted.

Inspected Core Spray Brackets per BWRVIP recommendations. NRI.

b I

10/2000 D2R17 10/2003 D2R18 11/2005 D2R19 11/2007 D2R20 11/2009 D2R21 10/2011 D2R22 VT-1 VT-3 EVT-1 EVT-1, VT-1 EVT-1, VT-1 EVT-1 VT-3 EVT-1 VT-1 EVT-1 VT-1 VT-3 6

100% (6) Surveillance Capsule Brackets.

NRI.

100% ( 6) Guide Rod Attachments. NRI.

EVT-1100% (4) Dryer Lugs. NRI.

EVT-1 100% (4) Dryer Lugs. NRI.

Eight feedwater sparger end-brackets VT-1, NRI.

Eight Core Spray piping bracket welds, EVT-1, NRI.

- EVT-1 100% (8) feedwater sparger end bracket to vessel attachments. NRI.

- VT-1 100% (8) feedwater sparger end bracket lug. NRI.

- EVT-1 100% (8) feedwater sparger end bracket pin tack weld. NRI.

- VT-1 feed water sparger repair at 240°.

RI. Hole in the weld of the repaired nozzle. Accepted as-is.

- EVT-1 25% (2) core spray piping bracket to vessel attachments. NRI.

- EVT-1 100% ( 4) steam dryer wall support lugs. NRI.

- EVT-1 and VT-3 of25% of Core Spray piping brackets (2). NRI

- EVT-1 100% (8) feed water sparger end bracket pin and nut. RI, some wear identified at pin head to bracket interface on three pins. One nut not tight against shoulder.

-EVT-1 of25% of Core Spray piping brackets (2). NRI

- VT-1 100% (8) feedwater sparger end bracket pin and nut. RI, some wear identified at pin head to bracket interface on s1xpms.

-EVT-1 of25% of Core Spray piping brackets (2). VT-1 on bolting of 1 of the 2 brackets. NRI

- VT-3 of moisture separator and dryer guide rod attachments. Rls for top cone bent on 200° guide rod and gouge/metal shaving on top cone of 0° guide rod. NRI for attachment welds.

- VT-1 100% (4) dryer wall support lugs.

Gouges noted on 3 of the lugs.

- VT-1 on all surveillance sample holder lower brackets and VT-3 on upper brackets. NRI.

11/2013 EVT-1

- EVT-1 of 25% of Core Spray piping D2R23 VT-1 brackets (2). VT-1 on bolting for 1 of the 2 brackets. NRI

- EVT-1 100% (8) feedwater sparger end bracket to vessel attach. NRI.

- EVT-1 of 200° moisture separator and 0° dryer guide rod top cones. No change to previous Ris.

- VT-1 100% ( 4) dryer wall support lugs.

Gouges and wear marks noted on all of the lugs.

11/2015 EVT-1

- EVT-1 of 25% of Core Spray piping D2R24 VT-1 brackets (2). VT-1 on bolting for 1 of the 2 brackets. NRI

- EVT-1 of 200° moisture separator rJ guide rod top cones. No change to previous Ris.

- VT-1 100% ( 4) dryer wall support lugs.

Gouges and wear marks noted on all of the lugs. One new RI. Indications acceptable for one cycle.

Feedwater Sparger 10/2011 VT-1 Inspected all eight feedwater sparger end D2R22 bracket pins and nuts. RI, some wear identified at pin head to bracket interface on s1xpms.

Performed inspections of spargers, arm welds and t-box welds. RI - gouge on sparger. RI - sparger repair hardware previous indication, no change.

11/2013 VT-1 Inspected all eight feedwater sparger end D2R23 bracket pins and nuts. RI, wear on six of eight brackets at pin to bracket interface.

11/2015 VT-1 Inspected all eight feedwater sparger end D2R24 bracket pins and nuts. RI, wear on six of eight brackets at pin to bracket interface.

\\,_~;

Core Shroud 8/1995 EVT-1, UT Inspections per BWRVIP Guidelines of D2R14 all shroud repair design reliant structures prior to installation of comprehensive repair ( 4 GE designed tie-rod assemblies). Inspection of shroud consisted ofEVT-1 of all ring segment 7

welds (accessible surfaces), EVT-1 of between 43% and 72% of the length of each vertical weld between Hl & H2 from OD surface (ID not accessible), UT of between 30% and 50% of the length of each of the 6 beltline vertical welds, EVT-1 of between 43% and 72% of the length of 2 of the 3 vertical welds between H6 & H7 from OD surface (ID not accessible), and UT of 35% of the length of the remaining vertical weld between H6 and H7.

( *-,

No Reportable Indications.

03/1998 VT-1, Shroud repair hardware inspected per GE D2Rl5 VT-3 recommendations. NRI.

10/1999 UT&EC UT & EC examinations from the ID with D2R16 the TEIDE 2 manipulator on the core shroud vertical welds V14, Vl5, V16, Vl 7, V18, and V19 per the requirements ofBWRVIP-76 for a repaired shroud.

NRI. Coverages are as follows:

V14: 80.1%

V15: 80.1%

V16: 83.4%

V17: 52.6%

-. -y Vl8: 62.8%

V19: 58.0%

10/2001 EVT-1 Exelon performed one sided EVT-1 of all D2R17 vertical welds outside of the beltline with 100% coverage including welds V5, V6, V7, V26, V27 and V28. There were no I

\\

recordable indications.

11/2005 EVT-1, EVT-1 100% (16) Ring Segment Welds D2R19 VT-1 from the OD. NRI. Coverages were 100% except for the following:

V9:

85%

Vll: 95%

\\

~

V20: 0% (inaccessible due to Jet Pump diffuser)

V21: 90%

V24: 0% (inaccessible due to Jet Pump diffuser)

Attempted EVT-1 of shroud vertical welds V29, V30, V31, V32. 0%

8

\\

r *.

\\._,;

/

\\

\\.__,;

( )

_/

\\, ___ )

/

', \\

\\_./

\\__)

I I

-~I

coverage was achieved due to Jet Pump interference.

Performed 10 year shroud tie rod examination of all four tie rods:

- EVT-1 of the clevis pin to verify if bottomed in slot and checking contact area for movement. NRI.

- VT-1 of stabilizer assembly contact between the RPV wall and upper contact, mid support, and lower contact. RI @ 20 and 110 degrees. Accepted as-is.

- VT-1 of retainer devices at lower support, lower spring to tie-rod connection, upper spring jacking bolts and tie rod nut. NRI.

- VT-1 of contact of the stabilizer assembly between the shroud and upper and lower springs. NRI.

- VT-1 of the core plate wedge contact.

NRI.

- Performed UT on the following vertical welds with the percent coverage shown:

V14: 19.9%

Vl5: 85.8%

V16: 90.1%

V17: 35.0%

V18: 84.0% - RI, Accept as-is.

V19: 47.2%

V27: 63.9%

Besides V18, all other welds NRI EVT-1 of welds V05-V07, Vl9, V26, V28, V29 and V3 l. NRI

- Shroud repair hardware inspections at all four locations. NRI.

Two sided EVT-1 on Vl9. NRI One-sided EVT-1 on vertical ring welds Vl, V2, V3, V4, V8, V9, VlO, Vl l, V12, Vl3, V20, V21, V22, V23, V24 and V25. NRI.

One-sided EVT-1 on vertical welds V5, V6, V7, V14, Vl 7, V26, V28, V29, and V31. NRI.

Performed EVT-1 and VT-3 inspections on all four shroud tie rod repairs. NRI.

(

I

(

\\. _/

,_)

,_/

l

)

_/

Shroud Support Top Guide 3/1993 D2R13 811995 D2R14 3/1998 D2Rl5 1011999 D2R16 11/2005 D2R19 1012011 D2R22 1112013 D2R23 8/1995 D2R14 3/1998 D2Rl5 10/2000 D2R16 10/2003 D2R18 UTNT-1 EVT-1, VT-1 NIA EVT-1 EVT-1, VT-3 EVT-1 VT-1 UT VT-1 NIA EVT-1 EVT-1 VT-1 10 Access hole covers proactively replaced with GE mechanical design. UT for radial flaws performed prior to replacement. No indications identified.

EVT-1 ofH8 and H9 for approx 12" at 4 locations of shroud repair hardware attachment areas.

VT-1 of both replacement access hole cover assemblies. No indications identified.

Not fuspected during D2R15 Core Support Structures, Performed EVT-1 of H8 and H9 Welds per BWRVIP-38 requirements. No Recordable fudications fuspected both Shroud Access Hole Cover repairs, NRI.

EVT-1 H8 & H9 from 132-177°. NRI.

VT-3 H9 100% accessible areas. NRI.

EVT-1 top side of H8 & H9 welds at 132-177° and 312-357°. NRI.

Bolted attachment for both Access Hole Covers. NRI.

UT of 10% of the H9 weld. NRI VT-1 of 5 cells. NRI.

VT-1 of all 4 alignment assemblies. NRI.

VT-1 of rim to bottom plate weld at 4 locations. NRI.

No inspections during D2Rl5.

Top Guide Alignment Pins, EVT 90° and 270° and Rim to Lower Plate Weld per BWRVIP-26. No Reportable fudications Top Guide aligner assemblies at 0, 180° and 270° welds (EVT-1) and pin (VT-1),

NRI

I I

\\

' I

~ '

j

\\ __ l<'

I I

r

\\

j I

'- /

\\

'.../

I 11/2005 D2Rl9 11/2007 D2R20 10/2011 D2R22 11/2013 D2R23 11/2015 D2R24 SLC 11/2005 D2R19 11/2007 D2R20 11/2009 D2R21 11/2013 D2R23 Jet Pump Assembly 8/1995 D2R14 EVT-1 Top guide rim weld at 235° on the outboard side of cell 03-30. NRI.

EVT-1 Top guide rim welds, aligner pins and VT-1 sockets at 0° and 90°.

EVT-1 Top guide rim weld was inspected at accessible locations. One RI - a 12" linear indication was identified.

VT-1 The aligner pins and sockets at 180° and 270°. NRI.

EVT-1 Top guide grid beams were inspected from 10% of the cells (18 cells). NRI.

EVT-1 Top guide rim weld indication inspected with no change noted from previous outage.

EVT-1 Top guide rim weld was inspected at accessible locations. No change to previous RI.

VT-1 All four aligner pins and sockets. One RI on aligner block at 90°.

Enhanced Safe end and nozzle examined. NRI.

VT-2 Enhanced Safe end and nozzle examined. NRI.

VT-2 Liquid Safe end and nozzle examined. NRI.

Penetrant UT Safe end and nozzle examined. NRI.

VT-1 UT Hold down beams, beam bolt keepers, lock-plates and retainers; restrainer wedges, stops, and adjusting screws, clamp bolts and keepers; riser brace assemblies, adapters and baffle plate welds, sensing lines and sensing line brackets per various SILS.

Latest inspections were in 1995, with no reportable indications. Inspect 100%

every other (even numbered) outage.

Jet pump beams are UT examined each outage using technique capable of 11

r--,

',,)

I\\

I./

r' I

I I

\\

)

' \\. /

\\

\\ __ )

\\

\\_)

Ci

(

~/

r 1

I

\\.._.J

\\'--./

( )

(

I

"-_J 3/1998 UT, EVT-1 D2R15 01/2000 UT, EVT-1 D2R16 10/2001 UT, EVT-1 D2R17 10/2003 EVT-1 D2R18 11/2005 EVT-1 D2R19 VT-1 VT-3 12 detecting cracking at throat and ears.

One beam found cracked at ear in 1995 and was replaced.

D2Rl 5 Beam UTs, NRI.

Jet Pump Riser Welds RS-1, 2, 3, 4 and 5 OD Inspected on all ten risers. Riser to JP Pair 15/16 has 1-1/2" long crack in elbow RAZ at RS-1. Evaluated for two cycles of operation without repair. NRI all others.

Jet Pump Beams, UT 100% of Beams NRI Riser Brace, Restrainer Bracket, Wedges and Inlet Mixers EVT-1 High/Medium Priority Welds Per BWRVIP-41 sample and inspection requirements. Minor Indications noted.

Jet Pump Beams, UT 100%, NRI Riser Brace Leaf at RPV wall block on JP#9, upper Rb 4 weld cracked.* EVT-1 examined 100% scope expansion, no other indications. Checked and found no set screw gaps. Examined for B-N-2.

Measured known RS-1 crack on riser 15/16. No change in last two cycles.

Replaced all 20 Jet Pump Beams with BWR4 weldless keeper beams Installed 19 Riser Brace Mitigation clamps one Repair on JP#9.

Measured flaw on JP#15/16 RS-1.

Increased from 1 1/2" to 2" length.

Identified pup piece present on JP#5/6, VT-1 100% (20) WD-1. NRI.

VT-3 100% (20) Jet Pump Bream Tooth Engagement. NRI.

VT-1100% (8) Jet Pump Sensing Line Clamps. RI (2). Teeth not fully engaged. Accepted as-is.

EVT-1 30% (3) RS-4, 5. NRI.

EVT-1 50% (5) RS-1, 2, 3. RI on JP 15/16 RS-1. Size confirmed to be 1Y2 ".

VT-1 100% (20) Jet Pump Riser Brace Clamps. RI (8). Teeth on keepers not fully engaged. Accepted as-is.

EVT-1AS-1,2 on Jet Pumps 8, 9, 19 (AS-1 only). NRI

.r--..,

\\

(--.,

r

)

I 11/2007 VT-1 D2R20 EVT-1 VT-3 11/2009 EVT-1 D2R21 VT-1 10/2011 EVT-1 D2R22 VT-1 13 VT-1 Aux. wedge on VS of Jet Pump 11.

NRI.

- VT-1 100% (8) Jet Pump Sensing Line Clamps. RI (7). Teeth not fully engaged. Accepted as-is.

- EVT-1 of six RB-3 welds. NRI

- EVT-1 ofRS-1 weld on JP 15/16. RI on previously identified indication. No change in flaw size.

- Swing gate replaced and 2 aux wedges installed on Jet Pump 19.

- VT-3 of IN-5 bolting sets on 10 JPs.

NRI

- EVT-1 ofMX-1 welds on 10 JPs. NRI

- VT-1 of 5 JP wedges and swing gate keeper tack welds. One RI on JP 15 swing gate keeper degraded tack weld.

Accepted as-is for one cycle.

- VT-1 of ratchets on eight JP Riser Brace clamps and eight JP Sensing Line clamps. Multiple Ris for incomplete ratchet teeth engagement. Accepted as-IS.

- EVT-1 25% (5) RB-4 & 5. NRI

- EVT-1 30% (3 risers) RS-8 & 9. NRI

- EVT-1 JP 15/16 RS-1. Previous indication - No change

- EVT-1 25% (5) MX-3a and 40% (8)

MX-3b.NRI

- VT-1 25% (5) WD-1. NRI

- VT-1 three aux wedges. Minor wear identified on one wedge. Accepted-as-is for one cycle.

- VT-1 on five swing gate keepers/ratchets. One RI for crack in tack weld HAZ and Two Rls for small gap between gate and restrainer bracket.

- VT-1 two sensing line clamps and one sensing line. No change to previous indications.

- Replaced JP 15 swing gate.

- EVT-1 30% (6) RB-3. NRI

- EVT-1 70% (7 risers) RS-8 & 9. NRI

- EVT-1 60% (6 risers) RS-1 & JP 516 RS-la. JP 15/16 RS-1 previous indication - No change

- EVT-1 50% (5 risers) RS-2 & 3. NRI

- EVT-1 30% (3 risers) RS-4 & 5. NRI

~' )

/ -......

(~-,.

\\.__ /

I

\\ j' r"'

'~

,1

(-\\

v

,r '*

'-..../

\\_)

\\.,_)

('

../

\\.___,/'

(

'-...,,)

"'-~:

u

(

\\__)

)

11/2013 EVT-1 D2R23 VT-1 VT-3 11/2015 EVT-1 D2R24 VT-1 Jet Pump Diffuser 8/1995 VT-1 D2Rl4 3/1998 NIA D2Rl5 01/2000 EVT-1 D2R16

- VT-1 75% (15) WD-1. NRI

- VT-1onJP19 aux wedges. NRI

- VT-1 on seven swing gate keeper tack welds or ratchets. One RI for crack in tack weld RAZ (no change from D2R21).

- VT-1 two sensing line clamps. RI for ratchet teeth engagement and clamp movement.

- VT-1 on 5 riser brace mitigation clamps and the jet pump 9 riser brace repair clamp. NRI

- EVT-1 of jet pump 15/16 riser RS-1.

No change to previous RI but better video has concluded the flaw is only 0.875" (previously recorded as 1.5")

- VT-1 on jet pump 2 and 11 sensing line clamps. No change to previous Ris.

- VT-1 25% (5) WD-1. NRI

- VT-1 3 0% of swing gate keeper tack welds. No change to previous RI on JP 2.

- VT-1onJP11and19 aux wedges. No change to previous RI.

- VT-1 of all 20 beam retainer clips. NRI

- EVT-125% (5 jet pumps) MX-1. NRI

- VT-3 25% (5 jet pumps) IN-5. NRI

- EVT-1 of jet pump 15/16 riser RS-1.

No change to previous RI.

- VT-1 on jet pump 2 and 11 sensing line clamps. No change to previous Ris.

- VT-1 25% (5) WD-1. NRI

- VT-1 on JP 19 vessel side aux wedge.

No change to previous RI.

- EVT-1 25% (5 jet pumps) MX-3a and MX3b.NRI

- VT-1 on JP 19 swing gate bolt ratchets.

NRI

-EVT-1 25% (5) RB-4 & 5. NRI Diffuser to baffle plate welds on all 20 jet pumps. No indications.

Not inspected D2R15.

JP Diffuser EVT-1 High/Med Priority welds per BWRVIP-41 sample and inspection requirements. NRI 14

\\

r

\\

I

\\

/

r, 1

,J

(-

\\

\\

)

\\---./

(

/

I I

I..___,,

.'--/

CRD Guide Tubes CRD Stub Tubes In-Core Housing Dry Tubes 1012001 D2R17 1012003 D2R18 1112005 D2R19 1112007 D2R20 1112009 D2R21 1112013 D2R23 811995 D2R14 1012001 D2R17 11/2007 D2R20 811995 D2Rl4 8/1995 D2R14 811995 D2R14 EVT-1 No scope D2Rl 7.

UT,EVT-1 UT examined Jet Pumps# 2, 3, 4, 5, 8, 9, 12, 13, 14, 15, 18 and 19. This completes first 6 Year Inspection Interval. NRI EVT-1 of the last of the Medium Priority 50% sample also completed. NRI.

NIA Not inspected in D2R19.

NIA Not inspected in D2R19.

EVT-1

- 25% (5) DF-1and50% (10) DF-2. NRI

- 50% (10) AD-1, AD-2 and AD-3a. NRI VT-3 VT-3 inspection of 1 jet pump slip joint. NRI VT-1 11 CRD guide tube lower assembly (1 MIL) welds, 2 CRD guide tube upper assembly welds, 4 CRD guide tube alignment ear welds. NRI.

EVT-1, 5% inspected (9) per BWRVIP-47, VT-3 CRGT-1, 2, 3 and pin. NRI.

EVT-1, Inspected 5% (9) of the control Rod VT-3 Guide Tube Welds and Guide Tube and Fuel Support Alignment Pins. VT-3 on the CRGT-1 and AS-GT-ARPIN-1.

EVT-1 of the CRGT-2 and 3. NRI VT-1 (1 14 CRD housing to CRD stub tube MIL) welds, 14 CRD stub tube to RPV bottom head welds, 3 CRD housing tube to housing cap welds. NRI.

VT-1 (1 4 incore guide tube to housing welds, 4

.MIL) incore housing to RPV bottom head welds, 4 incore guide tube stabilizers.

NRI.

VT-1 No indications identified.

Examined every other outage.

15

,.-- \\

I

."\\

(~,

\\ -

J

~, I

,~')

~- _.J

\\_j'

('\\

\\._ I

(~)

\\

/

""'- /

f

\\

\\_j

/ '

(

~)

(J r

' u

-._)

Instrument Penetrations LPCI Coupling Steam Separator/

Shroud Head 10/2000 D2R16 11/2007 D2R20 11/2009 D2R21 10/2011 D2R22 11/2013 D2R23 11/2015 D2R24 NIA NIA 11/2007 D2R20 11/2009 D2R21 10/2011 D2R22 1112013 D2R23 11/2015 D2R24 VT-1 NRI.

VT-1 50% ofSRM and IRM dry tubes inspected. NRI.

VT-1 50% of SRM and IRM dry tubes inspected. NRI.

VT-1 50% of SRM and IRM dry tubes inspected. NRI.

VT-1 One LPRM and 50% of SRM and IRM dry tubes inspected. NRI.

VT-1 50% ofSRM and IRM dry tubes inspected. Four dry tube plungers not fully engaged..

VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI for one missing pin and pin/window wear on multiple shroud head bolts VT-1

- VT-1 Inspected 100% of Shroud Head EVT-1 Bolt Alignment Pins and Windows. RI for pin/window wear on multiple shroud head bolts

- EVT-1 on Steam Separator Guide Rod top cone. RI for cracked tack weld.

Acceptable-as-is.

VT-1

- VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI for pin/window wear on multiple shroud head bolts VT-1

- VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI for pin/window wear on multiple shroud head bolts.

VT-1

- VT-1 Inspected 100% of Shroud Head Bolt Alignment Pins and Windows. RI 16

r ~

\\. _/

r *.

I

(

'*- /

i

', /

\\~*

\\... __.I Steam Dryer 11/2005 VT-1 "best D2R19 effort" 11/2007 NIA D2R20 11/2009 "Best D2R21 Effort" VT-1 10/2011 "Best D2R22 Effort" VT-1 11/2013 "Best D2R23 Effort" 17 for pin/window wear on multiple shroud head bolts.

Performed BWRVIP-139 required inspections as well as inspections of high-stress areas as determined by GE models. Internal start-up instrumentation piping was also examined. Several RI, including:

- Four of six gusset feet tip (adjacent to R2 weld), ranging from 7 to 11.5.

Cracking was ground out and rewelded.

Gusset feet extensions were designed and installed to transfer the stress riser to the mid-support ring.

- Several internal strut/supports were identified with cracking. Several were historical from D2Rl8 inspections. No change in the cracking was observed.

These welds are non-structural.

Accepted as-is.

- Vertical guide cracking (2) at 220°.

Both cracks (2.5-5" in length) were stop-drilled.

- Lower instrument line in Bank C observed cracking at the weld.

Performed fracture mechanics analysis and lost parts analysis. Acceptable as-is.

- Interior drain channel cracking (3).

Performed GE analysis. Acceptable as-lS.

- Perforated plate weld cracking.

Performed GE analysis. Acceptable as-lS.

- Perforated plate bowing. Performed GE analysis. Acceptable as-is.

Replaced steam dryer with a new one.

Examined critical components on steam dryer ID and OD after one cycle of operation per GE recommendations. NRI Examined OEM recommended components on OD. Lifting lug at 40° found rotated. Gouge identified on dryer skirt.

Examined OEM recommended components on ID and OD. New Rls

\\

,,r- ~.

)

)

\\

\\

\\__j

{

'~,/

\\..__)

DMWelds Reactor Vessel Cast Austenitic Stainless Steel 11/2015 D2R24 11/2009 D2R21 10/2011 D2R22 11/2013 D2R23 11/2015 D2R24 10/2011 D2R22 11/2013 D2R23 10/2011 D2R22 11/2013 D2R23 VT-1 noted near the trough supports to cross beam welds at 8 locations. No change to previous RI identified on dryer skirt.

"Best Examined trough support attachment Effort" welds on all 52 supports. No change to VT-1 previous Rls.

No inspections in D2R21 UT Inspected six DM welds. NRI.

UT Inspected four DM welds. NRI.

UT Performed manual UT on one (1) IGSCC Category C, twelve (12) IGSCC Category D, three (3) IGSCC Category F and two (2) IGSCC Category E welds.

None of these welds were dissimilar welds. No relevant indications were identified.

UT Inspected vertical welds (18) and the shell to flange weld. One indication identified in shell to flange weld identified as unacceptable per Table IWB-3510-1. Indication has been evaluated in accordance with IWB-3600.

EVT-1

- Examined weld and heat affected zones on four level instrument nozzles. NRI EVT-1 Inspected one of each of the following for License Renewal commitment: fuel support piece; control rod guide tube base; jet pump mixer flange, mixer flare, mixer ring, inlet/mixer nozzle and inlet mixer elbow. NRI.

EVT-1 Inspected one of each of the following for License Renewal commitment: fuel support piece; control rod guide tube base; jet pump mixer flange, mixer flare, mixer ring, inlet/mixer nozzle and inlet mixer elbow. NRI.

18

11/2015 EVT-1 Inspected one of each of the following D2R24 for License Renewal commitment: fuel support piece; control rod guide tube base; jet pump mixer flange, mixer flare, mixer ring, inlet/mixer nozzle and inlet mixer elbow. NRI.

\\

/

,r,

~,

~,

J r

I

' _/

~

' _/

",j

~--;

\\. _:

~I

.........._ _)

  • 19

Plant: Fermi Unit 2 Components in Date or Inspection Summarize the Following Information:

BWRVIP Scope Frequency of Method Inspection Results, Repairs, Inspection Used Replacements, Reinspections Core Shroud RF04 VT-1 (lmil Inspected: 100% ID welds H2, H3, and, (BWRVJP-07/76) wire)

H4; 100% OD welds Hl-H7; accessible areas HS &H9 VT-lNT-3 The only indications identified were two

<1" vertical in orientation above the H2 weld at azimuth 125 degrees. These were evaluated against established flaw screening criteria and found acceptable.

RF05 EVT-1 Inspected approximately 60-70 degrees r'

(1/2mil arc on the core shroud in area of previous

/ -,

wire) indications. H2-H4 inspected on shroud ID, Hl-H7 inspected on shroud OD. No new indications, no change observed in previous indications above H2 weld.

RF06 UT Performed focused phased array UT examination of the H3, H4, HS and H7 welds utilizing GE's universal carousel.

No indication of cracking was identified.

EVT-1 A cursory exam was performed on H-3 weld to confirm UT results for information only. No new indications and no change was observed in the previous indication above H2 weld.

RF07 EVT-1 Reinspected the indication above the H2 weld on the inside of the shroud. No change in appearance. The control rod blade was withdrawn to perform the examination.

RF09 NIA No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support RFlO NIA No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support 20

./

/

\\

I

",1

)

-- \\

Shroud Support (BWRVIP-381*104)

Access Hole Cover (BWRVIP-180)

RF11 NIA RF12 NIA UT RF13 NIA RF14 NIA (10110)

RF15 NIA (04/12)

RF16 NIA (2014)

RF17 NIA (2015)

RF03 VT-3 RF04 VT-lNT-3 RF05 EVT-1 (112 mil) 21 No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support Performed phased array UT examination of the H3, H4, HS and H7 welds from both sides utilizing AREVA's demonstrated technique. No indication of cracking was identified. Inspection coverage exceeded 60% for all welds with coverage spaced around the entire circumference.

No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support.

No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support.

No inspections performed on the Core Shroud. fuspections were performed on the Shroud Support.

No inspections performed on the Core Shroud. Inspections were performed on the Shroud Support.

No inspections performed.

Inspected shroud support gusset welds and H8/H9 in conjunction with jet pump inspections. No indications Inspected areas in conjunction with jet pumps, included were gusset welds H8 and H9. H8 and H9 welds inspected at 0 and 180 degrees with 1 mil wire. No indications.

Inspected sample area 60-70 degree arc plus 180 degrees location on H8, H9, and gussets. No indications.

RF06 VT-3*

  • Inspection performed in conjunction with jet pump inspections.

Approximately 50% of the gussets and H8 and H9 welds were inspected. This was a best effort exam which ranged from MVT-1 to VT-3 depending on camera angle and lighting. No cleaning was performed. No indications identified.

RF07 EVT-1

  • Inspection performed in conjunction with jet pump inspections. Remaining 50% of the gusset welds were inspected.

This was a best effort exam which ranged from EVT-1 to VT-3 depending on camera angle and lighting. (Credited as a n EVT-1 exam) No cleaning was performed or needed. No indications

( '

identified. The H8 and H9 welds were inspected in detail at 0 and 180 Deg.

Azimuth to EVT-1 standards where there were no obstructions.

RF08 EVT-1 The H8 and H9 welds were reinspected to achieve required coverage. 22% of both welds were inspected and included the areas at 0 and 180 degrees as well as adjacent to Jet Pumps 2 and 3.

I Accessible areas on Gussets 1, 3, 11, 12, and 22 were inspected. No indications of cracking identified.

RF09 EVT-1 The H8 and H9 welds were inspected VT-1 adjacent to Jet Pumps 3 and 4(Coverage obtained 1%and8.3%). Accessible

/

'- I areas on Gussets 2 and 15 inspected (90% coverage on each obtained). Both

(

access hole covers were inspected (VT-1). No indications identified.

RFlO EVT-1/

The H8 and H9 welds were inspected VT-1 adjacent to Jet Pump 5(Coverage obtained 1 % and 8.3%). Accessible areas on Gussets 7 and 8 inspected (70/90% coverage obtained @VT-1 quality, EVT-1 not credited, CARD 05-20378). No indications identified.

22

- /

RFll EVT-1 The H8 and H9 welds were inspected at 0 and 180 degrees as well as several other locations. Coverage obtained was 24%

for H8 and 30% for H9. Accessible areas on Gussets 5, 6, 7, 8, 9, 10, 18, and 21 were inspected with 50% to 80%

coverage obtained@EVT-1. No indications identified.

UT A portion of the H9 weld was examined from the vessel outside diameter using a manual technique as required by BWRVIP-104. Approximately 19.6% of weld was examined with no indications.

RF12 EVT-1 Accessible areas on Gussets 4 and 13 were inspected with 55% to 80%

coverage obtained using EVT-1. No indications identified. Both Access Hole covers were inspected per draft BWRVIP

-180 requirements. Cracking identified on 0 degree cover. Reference OE 25794.

RF13 EVT-1 Accessible areas on Gussets 5 and 6 were inspected with 75% coverage obtained using EVT-1. No indications identified.

j The 0 Degree Access Hole cover was reinspected and no additional cracking was identified. No repair installed.

RF14 EVT-1 Accessible areas on Gussets 1, 21, and 22 (10/10) were inspected with 50% - 60% coverage obtained using EVT-1. No indications identified. All 3 welds on the 0 Degree Access Hole Cover were reinspected and no additional cracking was identified.

No repair installed.

RF15 EVT-1 Accessible areas on Gussets 4, 5, 6, 13, (04/12) 16, and 17 were inspected with 50% to 70% EVT-1 coverage obtained. No indications identified. The H8 and H9 welds were EVT-1 visually inspected from the annulus side with combined coverage at several locations of 15.9%

for the H8 weld and 20.5% for the H9 weld. No indications identified.

23

RF16 EVT-1 Accessible areas on Gussets 11 and 12, (2014) as well as the 180° Access Hole Cover were inspected with 90% coverage and no indications were identified. All 3 welds on the 0° Access Hole Cover were re-inspected. No additional cracking was identified and the component was evaluated to be acceptable without repair.

RF17 EVT-1 Accessible areas on Gussets 14, 15, and (2015) 18, were inspected with 35% to 65%

coverage and no indications were identified.

Core Spray Piping each outage VT-1 During RF-01 two small arc strikes were (BWRVIP-18/18-A)

RFOl thru (lmil) identified on loop piping. These have RF04 been reinspected each outage. No change in condition. fuspections performed per IEB 80-013 and SIL 289.

No indication of cracking.

RF05 EVT-1 All welds brushed prior to inspection (1/2mil) using 1/2 mil wire. Remainder of loop VT-1 piping inspected without brushing. No indication of cracking.

RF06 EVT-1 fuspected all welds on both loops of core spray to EVT-1 standards as opposed to BWRVIP-18 requirements ofMVT-1.

Cleaning assessment was performed -

cleaning was not necessary. No indication of cracking.

RF07 EVT-1 fuspected all welds on both loops of core spray to EVT-1 standards. Cleaning assessment was performed - cleaning was not necessary. No indication of cracking.

RF08 EVT-1 fuspected all welds on both loops of core spray to EVT-1 standards. Cleaning assessment was performed, cleaning was not necessary. No indication of cracking.

RF09 EVT-1 fuspected all target welds on both loops of core spray and sample welds on Div 2 to EVT-1 standards. Cleaning assessment was performed, cleaning was 24

not necessary. No indications of cracking.

RFlO EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 2 to EVT-1. Cleaning assessment was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately but generally >80%.

RFll EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 1 to EVT-1. Cleaning assessment was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately

)

but generally >80%.

RF12 EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 1 to EVT-1. Cleaning assessment was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately but generally >55%.

RF13 EVT-1 Inspected all target welds on both loops of core spray and rotating sample welds on Div 2 to EVT-1. Cleaning assessment

  • ._)

was performed, cleaning was necessary for selected locations and welds were brushed. No indications of cracking.

Inspection coverage reported separately but generally >55%.

RF14 EVT-1 Inspected all target welds on both loops (10/10) of core spray and rotating sample welds on Div 2 to EVT-1. Cleaning was performed for all locations and welds were hydrolazed or brushed. No indications of cracking. Inspection coverage reported separately but generally >60%.

25

RF15 EVT-1 Inspected all target welds on both loops (4/12) of core spray and rotating sample welds on Div 1 to EVT-1. Cleaning was performed for all locations and welds were brushed. No indications of cracking. Inspection coverage reported separately but generally >60%.

RF16 EVT-1 Inspected all target welds on both loops (2014) of core spray and a rotating sample welds on Div 1 with no indications of cracking observed. Brushing was performed on all locations. Inspection coverage is reported separately in Art. 2, but

'\\

averaged 58%.

RF17 EVT-1 Inspected all target welds on both loops (2015) of core spray and a rotating sample welds on Div 2 with no indications of cracking observed. Brushing was performed on all locations. Inspection coverage is reported separately in Art. 2, but averaged 60%.

Core Spray Sparger each outage VT-1 (1 During RFO 1 one arc strike identified on (BWRVIP-18/18-A)

RF01-RF04 mil) upper CS sparger. Reinspections have not identified any changes. No indication of cracking RF05 VT-1/

1/2 mil wire used for junction box EVT-1 remainder utilized lmil wire. No (1/2mil) indication of cracking.

RF06 EVT-1, Inspected per BWRVIP-18 using EVT-1 MVT-1 for sparger T-box and end caps and MVT-1 for remaining locations. No indications of cracking.

\\

RF07 EVT-1/

Inspected per BWRVIP-18 using EVT-1 VT-1 for sparger T-box welds, end cap welds, drain plug welds, and support brackets and welds, and VT-1 for flow nozzles and tack welds. No indications of cracking identified.

RF08.

EVT-1/

Inspected per BWRVIP-18 using EVT-1 VT-1 for Sl, S2 and S4 welds. Selected S3a, S3b welds inspected using VT-1.

Selected S3c welds as well as selected 26

\\

I

\\

r

(

\\

'"- _)

I

)

J

(

\\.,'

.J 1._.J RF09 EVT-1/

VT-1 RFIO EVT-1/

VT-I RFll EVT-1/

VT-1 RF12 EVT-1/

VT-1 RF13 EVT-1/

VT-1 27 SB bracket welds were inspected using EVT-1 technique. A best effort exam was performed on all accessible areas.

No indications of cracking identified.

Inspected per BWRVIP-18 using EVT-1 for 50% of the SI, S2 and S4 welds and VT-I for 50% of the S3a, S3b and S3c welds on the same spargers. 9 SB bracket welds were inspected using EVT-1 technique. Coverage for specific welds will be reported separately. No indications of cracking were identified.

Inspected per BWRVIP-18 using EVT-1 for 50% of the Sl, S2 and S4 welds and VT-1for50% of the S3a, S3b and S3c welds on the same spargers. 6 SB bracket welds were inspected using EVT-1 technique. Coverage for specific welds will be reported separately but was >

60% for welds and >85% for brackets.

No indications of cracking were identified.

Inspected per BWRVIP-18-A using EVT-1for50% of the SI, S2 and S4 welds on the same spargers. 6 SB bracket welds were inspected using VT-1 technique. Coverage for specific welds will be reported separately but was >

50% for welds and >75% for brackets.

No indications of cracking were identified Inspected per BWRVIP-18-A using EVT-1for50% of the SI, S2 and S4 welds on the same spargers. 6 SB bracket welds were inspected using EVT-1 technique. Coverage for specific welds will be reported separately but was >

40% for welds and >75% for brackets.

No indications of cracking were identified.

Inspected per BWRVIP-18-A using EVT-1for50% of the Sl, S2 and S4 welds on the same spargers. 6 SB bracket welds were inspected using EVT-

1 technique. Coverage for specific welds will be reported separately but was>

50% for welds and >70% for brackets.

No indications of cracking were identified.

RF14 EVT-1/

Inspected per BWRVIP-18-A using (10/10)

VT-1 EVT-1for50% ofthe Sl, S2 and S4 welds on the C and D spargers. 6 SB bracket welds and S3 nozzle welds were inspected using VT-1 technique.

Coverage for specific welds will be reported separately but was > 40% for welds and >60% for brackets. No indications of cracking were identified.

RF15 EVT-1/

Inspected per BWRVIP-18-A using (4/12)

VT-1 EVT-1for50% of the Sl, S2 and S4 welds on the A and B spargers. 6 SB bracket welds inspected using VT-1 technique. Coverage for specific welds will be reported separately but was >

40% for welds and >60% for brackets.

No indications of cracking were identified.

I I

RF16 EVT-1/

Inspected per BWRVIP-18-A using (2014)

VT-1 EVT-1for50% of the Sl, S2 and S4 welds on the A and B spargers. 6 SB bracket welds were inspected using VT-

1. Coverage for specific welds is reported separately in Attachment 2 but was > 40% for most welds and > 60% for most brackets. No indication of cracking I

1, was identified.

RF17 EVT-1/

Inspected 50% of the Sl, S2 and S4 (2015)

VT-1 welds on the A and B spargers using EVT-1 and 6 sparger bracket welds using VT-1. Coverage for specific welds is reported separately in Attachment 2 but averaged 46% for the welds and 50% for the brackets. No indication of cracking was identified.

Top Guide (Rim, etc.)

RF03 VT-lNT-3 Inspected 6 locations (RICSIL 059) and Beams (BWRVIP-26) rim area 0° and 180°. No indications.

(BWRVIP-183) 28

r' \\

I I

I

\\

I I

' )

,\\

i

)

(

/

, __./

I "--

RF04 VT-lNT-3 RF05 VT-1 RF06 VT-1 RF07 VT-1 RF08 VT-1 RF09 VT-1 RFIO VT-lNT-3 RF11 VT-lNT-3 RF12 VT-lNT-3 RF13 EVT-1 RF14 VT-3 (10/10)

RF15 EVT-1 (4/12) 29 fuspected 6 locations (SIL 554) and rim area 0° and 360°. No indications.

fuspected 15 locations (SIL 554). No indications.

fuspected bottom edge of beams at 11 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 8 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 5 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 6 core locations per SIL 554. No indication of cracking.

fuspected bottom edge of beams at 2 core locations per SIL 554 and rim area 0° and 90°. No indication of cracking.

fuspected bottom edge of beams at 2 core locations per SIL 554. No indication of cracking. fuspected 90 degree segment of top guide rim (90° - 180°) and no indications were identified.

fuspected intersection and bottom edge of beams at 5 core locations per SIL 554.

No indication of cracking.

fuspected intersection and bottom edge of beams at 5 core locations per BWRVJP-183 utilizing a new visual inspection tool and rim area 0° - 90°. No indication of cracking.

fuspected rim area 0° - 180° with no indications identified.

Inspected intersection and bottom edge of beams at 5 core locations per BWRVJP-183 utilizing a new visual

inspection tool. No indication of cracking. Fabrication related conditions identified on the bottom surface of the plate material at 3 cell locations.

Inspected the rim area 180° - 360° with no indications.

RF16 NIA No inspections performed in RF16.

(2014)

RF17 EVT-1 Inspected intersection and bottom edge (2015) of beams at 9 core cell locations per BWRVIP-183 with no indication of cracking.

Core Plate Rim Bolts, RF05 VT-1 (lmil Inspected 6 core plate bolts located etc. (BWRVIP-25) wire) between 100 and 160 degrees and adjacent area. No indications.

RF06 VT-3 Inspected tops of approximately 20 bolts per SIL 588. No indications identified.

'* /

RF07 VT-3 Inspected tops of approximately 20 bolts

/

per SIL 588. No indications identified.

RF08 VT-3 Inspected tops of approximately 20 core plate bolts (VT-3) per SIL 588. Did not meet BWRVIP requirements. No indications identified.

RF09 NIA No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2003-117 and TJ-2003-01)

RFlO NIA No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2003-117 and TJ-2003-01)

RFll NIA No inspections performed. BWRVIP

  • -,,/

analysis concluded that inspections are not required. (Reference BWRVIP 2006-041 and DD-2006-01)

RF12 NIA No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2006-041) 30

/--,

J

/\\

I

\\

,-' '\\

(

./

)

\\

\\

'-I l _)

(

\\

l...__)

I -.

\\ __ )

cJ 1 \\_;

(_,/

SLC (BWRVIP-27)

RF13 NIA RF14 NIA (10110)

RF15 NIA (4112)

RF16 NIA (2014)

RF17 NIA (2015)

RF04 VT-3 RF05 -RF07 NIA RF08 VT-2*

RF09 VT-2*

RFlO VT-2*

No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2006-041)

No inspections performed. BWRVIP analysis concluded that inspections are not required. (Reference BWRVIP 2006-041) BWRVIP 2010- 243 now requires preparation of a Deviation Disposition by 313112011.

No inspections performed. BWRVIP analysis concluded that inspections are not required. Deviation Disposition DD-2011-01 was submitted to BWRVIP 313012011.

No inspections performed in RF16, as justified by Deviation Disposition DD-2011-01.

No inspections performed in RFl 7, as justified by Deviation Disposition DD-2011-01 Revision 1.

Performed a visual inspection from Reactor penetration to shroud support when access was provided during jet pump beam replacement. No indications.

No inspections performed as access was not provided.

Performed enhanced inspection on nozzle area from inside skirt area, but did not remove mirror insulation box from safe-end. No leakage observed.

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

Performed enhanced inspection on nozzle area from inside skirt area, and removed 31

/'--..

(\\

/

\\

\\

~

(

'., )

(

(_)

\\

~*

( '.

c (j

L G

(

/-'-

\\

\\,_,-'

I

\\

\\

\\_

'J RF11 RF12 RF13 RF-14 (10/10)

RF-15 (4/12)

RF16 (2014)

RF17 (2015) cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*/UT Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed. Performed a manual PDI qualified ultrasonic inspection of the nozzle to safe end weld as well as additional base material of bored material. No indications identified.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

VT-2*

Performed enhanced inspection on nozzle area from inside skirt area, and removed cover on the mirror insulation box for the safe-end for direct inspection. No leakage observed.

32

r - "

(

I i

\\

( -.

r '

......__ __./

\\._ /

\\...___)

/.

Jet Pump Assembly Each outage VT-1, (BWRVIP-41) examine at VT-3 least 50%

thru RF05 RF06 MVT-1, VT-3 RF07 EVT-1 R_F08 EVT-1 33 Jet pump assemblies are inspected each outage from top to bottom. During RF-04 all (20) hold down beams were replaced as a preventative measure and to avoid performing UT' s on the old style/original beams. Inspections are performed to the recommendations of SIL 551, 574, 465 S-1, andRICSIL 078.

During RF05 one of the 80 restrainer screw tack welds was found to be cracked. This was evaluated and was not repaired during RF05.

Performed inspections to the intent of BWRVIP-41 as well as augmented VT-3 of selected areas on jet pumps 1-10.

Inspections included all High, Medium and Low Priority locations. Inspected RS-1 and RS-2 welds on jet pumps 11-

20. One indication identified on RS-1 weld, 1.75" long. JCO performed prior to start-up. No other new indications identified.

Performed inspections to the intent of BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected areas on jet pumps 11-20.

Inspections included all High, Medium and Low Priority locations. Reinspected previously identified indication on RS-1 weld, 1.75" long that was identified in RF06. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. No other indications or changes in previous indications identified.

Performed reinspections to the intent of BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected areas on jet pumps l& 2.

Inspections included all High, Medium and Low Priority locations. Reinspected previously identified 1.75" long indication on RS-1 weld for Jet Pumps 7&8 that was identified in RF06. No change in indication length or

appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all 20 jet pumps per recommendations of SIL 629 and verified no wedge damage (WD-1) as well as full contact with restrainer

(\\

screws. No damage identified on any

\\ -, *'

location. Reinspected all restrainer screw tack welds with no changes observed.

RF09 EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected areas on Jet Pumps 3 & 4. Inspections included all High, Medium and Low Priority locations. Reinspected previously identified 1. 7 5" long indication on RS-1 weld for Jet Pumps 7 &8 that was identified in RF06. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all 20 Jet Pump Hold Down Beams by UT for BB 1, BB2, and the transition area BB3 using the latest available technique from General Electric. No indications identified on the beams. Reinspected all restrainer screw tack welds, contact area, and wedges after both tack welds on Jet Pump 15 were fo1,rnd cracked. No other damage or indications identified on any I.... __,.!

location. Jet Pump 15 permanently repaired by the installation of an auxiliary spring wedge. (Reference CARD 03-16929)

RFlO EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 4, 5, 6, 7, & 8. Reinspected previously identified 1.75" long indication on RS-1 weld for Jet Pumps 7

& 8 that was identified in RF06. No change in indication length I appearance.

Existing Flaw Evaluation on hand **

prepared by GE referenced as acceptance limit. Reinspected auxiliary spring

'~ -

.I wedge on Jet Pump 15. No other damage or indications identified on any location.

34

' __ )

RFll EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 7, 8, 9, & 10. Reinspected previously identified 1.75" long indication on RS-1 weld for Jet Pumps 7

& 8 that was identified in RF06. No change in indication length I appearance.

Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all Jet Pump wedges after wear was identified on JP2 restrainer bracket. Performed inspection of other welds on Jet Pump 2 as required by BWRVIP-41. Auxiliary spring wedges installed on Jet Pumps 1 and 2 and a slip joint clamp was installed on Jet Pump 2 to restore integrity. No other damage or indications identified.

RF12 EVT-1 Performed reinspections to BWRVIP-41 including EVT -1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 7, 8, 9, 10, 11, & 12.

Reinspected previously identified 1.75"

\\

long indication on RS-1 weld for Jet Pumps 7 & 8 that was identified in RF06.

No change in indication length I appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected all 20 Jet Pump Hold Down Beams. Inspected 12 Jet Pump wedges including the wedges and hardware (auxiliary spring wedges and slip joint clamp) installed in RF 11.

No other damage or indications identified.

RF13 EVT-1 Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on Jet Pumps 7, 8, 9, 10, 13, 14, 15, and 16.

Reinspected previously identified indication on RS-1 weld for Jet Pumps 7 /8 identified in RF06. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit. Inspected 35

/---,

(\\

r-'

I

\\

\\ ~ __,,

,~

" -- J r',

1

\\

(

(\\ *

..._~ - )

1_~)

(

'-._ I

\\

RF14 EVT-1 (10/10)

RF15 EVT-1 (4/12)

RF16 EVT-1/

(2014)

VT-1 RF17 36 9 Jet Pump wedges. No other damage or indications identified.

Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 and VT-3's of selected welds on most Jet Pumps including RS-8/9 welds on all pumps. Reinspected previously identified indication on RS-1 weld for Jet Pumps 7/8. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit.

fuspected all 20 Jet Pump wedges. Minor movement noted but no other damage or indications identified.

Performed reinspections to BWRVIP-41 including EVT-1 's as well as augmented VT-1 's of selected welds on several Jet Pumps. Reinspected previously identified indication on RS-1 weld for Jet Pumps 7/8. No change in indication length or appearance. Existing Flaw Evaluation on hand prepared by GE referenced as acceptance limit.

fuspected all 20 Jet Pump wedges. No movement noted and no damage or indications identified.

Performed EVT-1 exams of selected welds in accordance with BWRVIP-41 Rev. 3 with no indications identified.

VT-1 exams performed on all 20 main wedge assemblies. Wedge wear identified on Jet Pump 06; scope expansion performed with no further relevant indications observed and wedge was evaluated to be acceptable without repair. Growth identified during re-inspection of indication on RS-1 weld for Jet Pumps 07/08. fudication was evaluated to be acceptable for two cycles without repair. Ultrasonic examination of all 20 Jet Pump Hold Down Beams (BBl, BB2 andBB3). No indications identified on the beams.

1\\

(2015)

EVT-1/

Performed EVT-1 exams of selected VT-1 welds with no indications identified. VT-1 exams performed on all 20 main wedge assemblies. Minor wedge rod wear identified on Jet Pump 01; evaluated to be acceptable without repair. Minor wear identified on Jet Pump 02 Auxiliary Wedge, scope expansion performed with no further relevant indications observed and evaluated to be acceptable without repair. Mitigating clamp installed on the RS-1 weld for Jet Pumps 07/08.

Jet Pump Diffuser Each outage VT-3 Diffusers will be sample inspected during (BWRVIP-41) refueling outages.

RF06 MVT-1 BWRVIP-41 on Jet Pumps 1-10 except

,',,---.\\

inaccessible areas. No cracking.

RF07 EVT-1 BWRVIP-41 on Jet Pumps 11-20 except inaccessible areas. No cracking identified. Welds DF-3, AD-1, and AD-2

,~ - \\

are inaccessible for inspection.

RF08 EVT-1 BWRVIP-41 reinspection on Jet Pumps 1 and 2 except inaccessible areas. No cracking identified. Welds DF-3, AD-1, and AD-2 are inaccessible for inspection.

\\

\\

RF09 EVT-1 BWRVIP-41 reinspection on Jet Pumps 3 and 4 except inaccessible areas. No cracking identified. Welds DF-3, AD-1, and AD-2 are inaccessible for EVT-1 I

\\

visual inspection, VT-3 performed. (TJ-2003-02 prepared as justification)

RFlO EVT-1 BWRVIP-41 reinspection of selected DF-1 and DF-2 welds on Jet Pumps 5, 6, 7, & 8. Performed access study for future performance of UT examinations of welds DF-3, AD-1, and AD-2. These welds are inaccessible for visual 1

.J inspection. VT-3 performed. No indications identified (Reference TJ-2003-02)

\\-.......'

RFll EVT-1 B WR VIP-41 reinspection of selected DF-2 welds on Jet Pumps 9 & 10.

37

UT Performed of UT examinations on a portion of a total of 17 DF-3, AD-1, and AD-2 welds using specialized tooling.

These welds are inaccessible for visual inspection. No indications identified (Reference DD-2006-02)

RF12 EVT-1 BWRVIP-41 reinspection of selected DF-1 and 2 welds on Jet Pumps 6, 11, &

12.

UT No UT examinations performed during RF12 due to tooling failures. These welds are inaccessible for visual inspection. (Reference DD-2006-02)

RF13 EVT-1 BWR VIP-41 reinspection of selected DF-1and2 welds on Jet Pumps 7, 13, &

14.

UT No UT examinations performed during RF13 due to tooling failures. These welds are inaccessible for visual inspection. (Reference DD-2006-02) r RF14 EVT-1 BWR VIP-41 reinspection of selected (10/10)

DF-1and2 welds on Jet Pumps 7, 8, 9, and 13-18. No indications identified.

\\. ___,

UT Completed baseline UT examinations on all 20 Jet Pumps Diffuser/Adapter DF-3, AD-1 and AD-2 welds, (60 welds) since

  • ,_)

these welds are inaccessible for visual inspection. Deviation Disposition is no longer needed.

f

\\.,

~I

(

RF15 EVT-1 BWRVIP-41 reinspection of selected

\\._,/

(4/12)

DF-1 and 2 welds on Jet Pumps 10, 19, and 20. No indications identified.

RF16 EVT-1 BWRVIP-41 re-inspection of selected

/

(2014)

DF-1 and 2 welds on Jet Pumps 01, 02, and 11. No indications identified.

RF17 EVT-1 BWRVIP-41 re-inspection of selected (2015)

DF-1 and 2 welds on Jet Pumps 03, 04, and 12. No indications identified.

38

CRD Guide Tube RF04 VT-3 Inspected lower portion of peripheral (BWRVIP-47) guide tubes and stub tubes when access was provided during jet pump hold down beam replacement. No indications identified.

RF07 EVT-1 and Performed best effort exam on CRGT-3 VT-3 as weld was not visible on inside of tube.

CRGT-2 not accessible due to flow and ARPIN was not felt to be accessible. No indications identified.

RF08 EVT-1 and Performed best effort exam on CRGT-3 VT-3 as weld was not visible on inside of tube.

(,~ -\\

CRGT-2 not accessible due to flow and

(

\\

PS/GT-ARPIN was not felt to be accessible. No indications identified.

RF09 EVT-1 and Performed exams on CRGT-1, CRGT-2, VT-3 CRGT-3, and PS/GT-ARPIN at 10 Control Rod Guide Tubes/locations. No indications identified.

( '

RFlO NIA No inspection performed in RFIO.

RF11 NIA No inspection performed in Rl l.

RF12 VT-3 Performed exams on CRGT-1 and PS/GT-ARPIN at 5 Control Rod Guide

~I Tubes/locations. CRGT-2 and CRGT-3 not performed or credited due to high flow conditions. No indications identified.

RF13 NIA No inspections performed in RF13.

\\,/

RF14 EVT-1 and Completed all remaining baseline

\\.._/

(10/10)

VT-3 inspections on the Control Rod Guide Tubes. Inspections performed on ( 4)

CRGT-1, and PS/GT-ARPIN locations and on (9) CRGT-2 and CRGT-3 locations. One manufacturing flaw identified that did not impact the functionality of the component.

RF15 NIA 39

~

I

(---....

I. '

)

(

"-~/

_..-f CRD Stub Tube *

(BWR VIP-4 7)

In-Core Housing *

(BWRVIP-47)

Dry Tube*

(BWRVIP-47)

(4112)

RF16 NIA (2014)

RF17 NIA (2015)

RF04 VT-3 RF04 VT-3 Each outage VT-1 RF06 VT-1 RF07 VT-1 RF08 VT-1 RF09 NIA RFlO VT-1 RF11 VT-1 No BWRVIP required inspections performed in RF 15.

No BWRVIP required inspections performed in RF16.

No BWRVIP required inspections performed in RF 17.

Inspected lower portion of peripheral guide tubes and stub tubes when access was provided during jet pump hold down beam replacement. No indications identified.

Small portion visible during jet pump beam replacement. No indication of degradation.

9of12 tubes found not completely seated. Performed all inspections per SIL 409 and RICSIL 073. No indications of cracking.

Reinspected 12 dry tubes. No change from previous condition. No cracking.

Inspected all 12 original design Dry Tubes. No change from previous conditions identified. No cracking identified.

Inspected all 12 original design Dry Tubes from two sides. No change from previous conditions identified. No cracking identified.

No inspections performed in RF09.

Inspected all 12 original design Dry Tubes from two sides. Linear indications identified on 7 tubes in the collar region above the pressure boundary weld.

Evaluated as acceptable for one cycle of operation. Plan to replace in RF 11.

(Reference CARD 04-25703)

Replaced all 12 Dry Tubes in RFl 1.

Performed baseline VT-1 and verified proper engagement in Top Guide.

40

RF12 NIA No inspections performed in RF12.

RF13 NIA No inspections performed in RF 13.

RF14 NIA No inspections performed in RF14.

RF15 NIA No inspections performed in RF15.

RF16 NIA No inspections performed in RF16.

(2014)

RF17 NIA No inspections performed in RFl 7.

(2015)

Instrument Penet.

  • Each outage VT-3 Inspected jet pump sensing lines and (BWRVIP-49 & 41) brackets each outage.

RF04 VT-3 SLC and peripheral bottom head penetrations inspected. No indications.

RF06 VT-3 Inspected JP sensing lines for pumps 1-

10. No indications.

RF07 VT-3 Inspected JP sensing lines for pumps 11 thru 20 only. No indications.

RF08 VT-3 Inspected JP sensing lines for Pumps 1 &

2 only. No indications.

\\

RF09 VT-3 Inspected JP sensing lines for Pumps 3 &

4 only. No indications.

RFlO VT-1 Inspected JP sensing lines for Pumps 5, 6, 7, 16, & 17. No indications RF11 VT-1 Inspected JP sensing lines for Pumps 6, 7, 16, & 17. No indications.

RF12 VT-1 Inspected JP sensing lines for Pumps 6, 7, 11, 12, 16, & 17. No indications.

RF13 VT-1 Inspected JP sensing lines for Pumps 6, 7, 13, 14, 16, & 17. No indications.

RF14 VT-1 Inspected JP sensing lines for Pumps 6, 7, 15, 16, 17, & 18. No indications.

41

RF15 VT-1 Inspected JP sensing lines for Pumps 6, 7, 16, 17, 19, & 20. No indications.

RF16 VT-1 Inspected JP sensing lines for Pumps 1, (2014) 2, 6, 7, 16, & 17. No indications.

RF17 VT-1 Inspected JP sensing lines for Pumps 3, (2015) 4, 6, 7, 16, & 17. No indications.

Vessel ID Brackets Each outage VT-1/3 Inspect sample population each outage.

(BWRVIP-48)

We have inspected most brackets each outage (core spray, feedwater). Jet pump riser brace, steam dryer support lugs, guide rod brackets and specimen holder brackets are sample inspected. No indications of cracking identified.

RF06 MVT-1 6 feedwater brackets.

All core spray piping brackets.

4 steam dryer brackets 1 guide rod bracket 1 specimen bracket.

No indication of cracking.

RF07 EVT-1 6 feedwater brackets.

All core spray piping brackets.

4 steam dryer brackets 1 guide rod bracket No indication of cracking identified.

RF08 EVT-1 6 feedwater brackets.

All core spray piping brackets.

t I

4 steam dryer brackets 1 guide rod bracket Surveillance holder and Brackets @ 30 az.

No indication of cracking identified.

RF09 EVT-1 6 Feedwater brackets.

4 Core Spray piping brackets.

1 Jet Pump riser brace (Jet Pump 3 and 4)

No indication of cracking identified.

RFlO EVT-1 6 Feedwater brackets.

3 Core Spray piping brackets.

1 Surveillance Holder bracket 4 Steam Dryer Support brackets 4 Steam Dryer Hold Down 1 Guide Rod Bracket 42

1 Jet Pump riser brace (Jet Pump 5 and 6)

No indication of cracking identified.

RFll EVT-1/

No inspections performed in RF-11.

VT-1 RF12 EVT-1/

6 Feedwater Sparger bracket sets.

VT-1 1 Surveillance Holder bracket 4 Steam Dryer Support brackets 1 Guide Rod Bracket 2 Jet Pump riser braces (Jet Pumps 7, 8, 9, & 10)

No indication of cracking identified.

RF13 EVT-1/

No inspections performed in RF-13.

VT-1 RF14 EVT-1/

3 Feedwater Sparger bracket sets.

(10/10)

VT-1 2 Core Spray Piping Brackets 1 Surveillance Holder bracket 4 Steam Dryer Support brackets 1 Guide Rod Bracket 2 Jet Pump riser braces (Jet Pumps 1/ 2, and 11/12)

No indication of cracking identified.

j RF15 EVT-1/

Inspections performed on 3 Feedwater (4/12)

VT-1 Sparger bracket sets and 1 Guide Rod Bracket. No indications identified.

RF16 EVT-1/

Inspection performed on 1 Surveillance (2014)

VT-1 Sample Holder Bracket. No indications identified.

RF17 EVT-1 I 2 Feedwater Sparger bracket sets (four (2015)

VT-I individual brackets) 4 Core Spray Piping Brackets 4 Steam Dryer Support Brackets 4 Steam Dryer Holddown Brackets I Guide Rod Bracket I Jet Pump Riser Brace.

No indication of cracking identified.

LPCI Coupling NIA NIA Fermi does not have a LPCI Coupling Shroud Head RF04 VTNT 16 had indications, 17 replaced during Bolts/Shroud Head RF04.

43

RF05 NIA Remaining bolts replaced (31) during RF05 as a preventative measure. All 48 are now new style.

RF06 VT-3 Bolts 1-24 (of 48). No indication of cracking.

RF07 VT-3 Bolts 25-48 (of 48). No indication of cracking or damage. Springs were left compressed on 20 of the 24 inspected.

RF08 VT-3 Bolts 1-24 (of 48). No indication of cracking or damage RF09 VT-3 Bolts 23 and 25-48 (of 48). No indication of cracking or damage. All retainer springs verified to be functioning properly.

RFlO VT-3 Bolts 1-24 (of 48). Inspected North 113rd of Shroud Head/Separator and 2 lifting lugs. No indication of cracking or damage RF11 VT-3 Inspected Bolts 25-48 (of 48) and inspected Center 113rd of Shroud Head/Separators. No indication of cracking or damage.

RF12 VT-3 Bolts 1-24 (of 48). Inspected South 1;3rd of Shroud Head/Separator and 2 lifting lugs. All mid support ring gussets were inspected and small short cracks were identified on 3 of the 24 gussets. No repairs were required. Ref. OE 25795.

RF13 VT-3 Bolts 25-48 (of 48). Inspected North 113rd of Shroud Head/Separator and 2 lifting lugs. No changes identified in previous indications identified in RF12.

No other indications identified.

RF14 VT-3 Bolts 1-24, 27, 30, & 33 (of 48).

(10/10)

Inspected Center 113rd of Shroud Head/Separator. No changes identified in previous indications and no new indications identified.

44

RF15 VT-3 Inspected Bolts 25-48 and 2 (of 48).

(4112)

Inspected South 1;3rd of Shroud Head/Separator. No changes identified in previous gusset indications and no new indications identified.

RF16 VT-3 Inspected Bolts 1-12 (of 48) and the (2014)

North 113rd of Shroud Head/Separator.

No new indications were identified.

RF17 VT-3 Inspected bolts 13-24 (of 48). Minor pin (2015)

& window wear identified on bolts 21 &

23, evaluated to be acceptable without repair. Replaced bolts 2 & 33 due to their inability to latch. Inspected the Center 1/3rd of the Separator and identified one tie bar with a severed attachment weld on one end. The tie bar was removed to preclude generation of a loose part (technical justification from OEM obtained to support acceptance of one missing tie bar).

Steam Dryer RF09 VT-3 Inspected approximately 1/3 of dryer (RFOl-RF-08 not including hood welds and cover plate previously reported) welds. (Ref. SIL 644) No indications of

)

additional cracking identified.

RFlO VT-1/VT-3 Inspected approximately 50% of dryer including all inner hood vertical welds as recommended in SIL 644, Supplement 1, and Revision 1 ). Several new indications were identified near welds due to new locations being inspected and the change in technique. Indications were noted at base of inner hood vertical welds.

Reference CARD 04-25416 and also OE

  1. 17600. No changes were identified on previously recorded indications.

RF11 VT-lNT-3 Inspected approximately 50% of dryer including all inner hood vertical welds as recommended in SIL 644, Revision 1 and BWRVIP-139. Several new indications were identified near welds due to new locations being inspected and the change in technique. Indications previously noted on hood welds in RF 10 were reinspected and no changes were noticed.

45

RF12 VT-lNT-3 Inspected approximately 50% of dryer including inner hood vertical welds as recommended in BWRVIP-139. Several new small indications were identified near welds due to new locations being inspected and the change in technique and camera angles used. Indications previously noted on hood welds were reinspected and no changes were noticed.

RF13 VT-lNT-3 Inspected approximately 20% of dryer including "F" Bank welds and a sampling of other locations following reinspection guidelines contained in NRC SE to BWRVIP-139. One new indication identified in support ring.

RF14 VT-lNT-3 Inspected approximately 20% of dryer (10/10) including "E" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. No new indications identified.

RF15 VT-lNT-3 Inspected approximately 20% of dryer (4/12) including "D" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. No new indications identified.

RF16 VT-lNT-3 Inspected approximately 20% of dryer (2014) including "C" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. Indication newly identified on interior vane bank weld HE-C-2-1; evaluated to be acceptable without repair.

RF17 VT-lNT-3 Inspected approximately 20% of dryer (2015) including "B" Bank welds and a sampling of other locations following reinspection guidelines contained in BWRVIP-139-A. Indication on interior vane bank weld HE-C-2-1 identified in RF16 re-inspected with no changes observed. 24 capture plate assemblies 46

installed to cover all tie rod nut washer locations. Vertical drain channel welds preemptively increased from 1/8" to 1/4".

Dissimilar Metal RF-12 UT Performed ultrasonic examinations on 4 Welds BWRVIP Category B DM welds that contain alloy A (Not previously 82/182 using automated PDI qualified reported, reference techniques and procedures. Since >90%

BWRVIP letter 2008-coverage was not obtained on two welds, 089) 2 additional welds were selected and

>90% volume coverage was obtained.

No indications of cracking identified.

RF-13 UT Performed ultrasonic examinations on 5 Category B DM welds that contain alloy

(

82/182 using automated and manual PDI qualified techniques and procedures. No indications of cracking identified.

RF-14 UT Performed ultrasonic examination of 1 (10/10)

Category B DM weld that contained alloy 82/182 using manual PDI qualified technique and procedure. No indications of cracking identified.

RF-15 UT Performed ultrasonic examination of 1 (4/12)

Category B DM weld that contained alloy 82/182 using manual PDI qualified technique and procedure. No indications of cracking identified.

RF16 UT Performed ultrasonic examination of 3 (2014)

Category B DM welds using manual PDI

. _./

qualified technique and procedure. No indications of cracking identified.

RF17 UT Performed ultrasonic examination of 4 I

}

(2015)

Category B DM welds using PDI qualified phased array technique and procedure. No indications of cracking identified.

Bottom Head Drain RF16 RT Deviation Disposition DD-2014-01 Line (BWRVIP-205)

(2014) issued to support not completing radiography on the first elbow and piping immediately downstream of the reactor vessel in RF16. RT was performed on straight piping further downstream with no evidence of flow accelerated corrosion observed.

47

/

  • VT-2 leakage inspections have been and are performed on all RPV Instrumentation Nozzles and Piping Nozzles each refuel outage. An enhanced leakage inspection is performed on all locations to ensure no pressure boundary leakage. Inspections are performed in the annulus area adjacent to the vessel skirt, and are performed under vessel to ensure that any leakage identified is not from welded connections. Flange leakage from CRDM's is recorded, evaluated, and repaired if necessary.

Mirror insulation is opened for SLC safe end inspection and for bottom head inspections but is not removed from other locations unless the leakage source can't be determined.

48

Reactor Internals Inspection History Plant: Peach Bottom Atomic Power Station, Unit 3 Components in Date or Inspection Summarize the Following Information:

BWRVIP Scope Frequency of Method Inspection Results, Repairs, Inspection Used Replacements, Reinspections Core Shroud 1993 VT-1 Enhanced VT-1 (1 mil resolution) (100%

ID of H-3, H4, & V-3) portions OD ofH-1, H-2, H-3, H-4, H-5, H-6, and H-7 Prior to BWRVIP-01, Circumferential Indications on ID ofH-3 and H-4 (Plate side, not ring side)

Short circumferential indications on ID of V-3 weld.

Evaluation of indications showed full structural margins for one operating cycle.

1995 UT Comprehensive UT Baseline of all Category "C" circumferential welds (H-1 through H-7).

Baseline per BWRVIP-01, Rev. 1.

Exams per BWR-VIP Core Shroud NDE Uncertainty and Procedure Standard, dated November 21, 1994.

Indications identified on ID ofH-1, H-3, H-4, and H-5.

Full structural margins calculated using two cycles of crack growth.

' _/

No indications identified on H-2, H-6, and H-7.

1999 UT UT Examination on welds H-3 & H-4.

Re-identified indications on both welds.

Extent of indications within existing structural analysis.

2005 UT Two-sided UT of all 7 horizontal welds

, _ _/

(Hl thru H7) and 4 vertical welds (V3 thru V6). No indications at H2, H7, V4-V6 or ring side of any weld. One minor indication near V3. Indications at Hl, H3, H4, and H5 correlated with those previously identified. One indication at H6 (new). One deep indication at H4.

Characterized as thru-wall. Review of previous data (1995 and 1999) also 49

\\._/

\\ _,/

(

Shroud Support 201S 1993 1997 1999 2001 200S 2009 UT VT-1 VT-1 EVT-1 UT VT-I EVT-1 VT-1 UT VT-1 so characterized indication as thru-wall at that time. EVT-1 on OD surface did not identify any indications.

Comprehensive UT of all 7 horizontal welds (Hl thru H7) and 4 vertical welds (V3 thru V6) per BWRVIP-76 Rev. 1-A.

Recordable indications were found in the Hl, H3, H4, HS, V3, and V6 welds.

Indications indicative of "off-axis" indications were reported in the vicinity of the H4 weld. Core shroud welds H2, H6, H7, V4, and VS had no reportable indications. All welds are acceptable as-is for a 10 year re-inspection interval via a plant specific analysis.

Enhanced VT-1 (1 mil resolution), of portions ofH-8 weld, No indications identified.

VT-1 examination around perimeter of both access hole covers, No indications identified.

VT-1 of both access hole cover bolted repairs. No indications identified.

10 % of weld length of welds H-8 &

H-9 examined.

No indications identified.

10% ofH-9 weld length from vessel O.D.

No indications identified.

VT-1 of both access hole cover bolted repairs. No indications identified.

> 10% ofH-8 weld, betweenjet pump banks, in area of AHCs.

VT-1 of both access hole cover bolted repairs. No indications identified.

Accessible length ofH-9 between 0 and 180 degrees.

No indications identified.

VT-1 of both access hole cover bolted repairs. No indications identified.

,r- \\

I I

\\_ _j

\\ _)

/

\\_j 2011 Core Spray Piping 1980-present 1985 1993 1995 1997 1999 2001 2003 EVT-1 VT-1 (1 mil)

VT-1 (1 mil)

VT-1 (1 mil)

VT-1 (1 mil)

VT-1 EVT-1 VT-1 VT-1 EVT-1 VT-I EVT-1 51

> 10% of weld length for H-8 & H-9 welds, betweenjet pump banks, in area of AHCs. No indications identified Enhanced VT-1 (1 mil resolution) performed on piping and welds each refueling outage per IEB 80-13, Cracking discovered at tee-box to header pipe weld.

Welded repair plates installed on both header tee-boxes.

Cracking identified in downcomer slip joint (weld P-5), evaluation demonstrated structural margin for one operating cycle.

Additional cracking identified in 3 of 4 downcomer slip joint welds (P-5), repair clamps installed on all 4 downcomers to repair flawed welds.

4 Downcomer repair clamps, no indications identified.

All annulus piping welds, no indications identified.

VT-1 Examination of A, B, C & D Downcomer Repair Clamps & both Header Teebox welded repairs.

No indications identified.

All target welds plus 25 % sample of piping butt welds examined.

No indications identified.

EVT-1 of all target welds plus 25%

sample of butt welds examined. No indications identified.

Four downcomer repair clamps.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

('.

\\

(

\\

I

\\

I I

I

~/

' _I

('

'._J

\\

\\,_I

(

,_/

\\_ __ )

2005 2007 2009 2011 2013 2015 Core Spray Sparger 1980-present EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

VT-1 Four down comer repair clamps.

EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

EVT-1 Four Header Tee Box strong back repair plate welds.

EVT-1 of all target welds plus 25%

sample of butt welds. No indications identified.

VT-1 Four down comer repair clamps.

EVT-1 Internal core spray piping from N5 nozzles to core shroud replaced eliminating previously installed downcomer and T-box repairs. EVT-1 performed on two hidden thermal sleeve welds with no indications identified.

VT-1, VT-1 and VT-3 of entire core spray line, VT-3 brackets, and clamps after one operating cycle. Visual exams confirmed all repair hardware is in place/ has not changed from "as-installed" condition. No indications recorded.

VT-1 Enhanced VT-1 (1 mil resolution)

(1 mil) performed on piping and welds each refueling outage per IEB 80-13, No indications identified.

52

/

(~

I I

'-./

'-,J Top Guide (Rim, etc.)

1999 2003 2007 2011 2013 2015 1987 1993 EVT-1 VT-1 EVT-1 VT-1 EVT-1 VT-1 EVT-1 VT-1 VT-1 VT-1, EVT-1 UT VT-3 53 Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

No indications identified.

Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

No indications identified.

Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

No indications identified.

Examination performed on all Sparger Pipe welds.

Examination performed on all Brackets, Drains and 50 % of Nozzles.

~ 1.0" Indication noted on the shroud side of the 136 degree bracket weld Examination performed on the core spray sparger bracket 05 at 136°. No change in the indication as identified during the 2011 inspection.

VT-1 of all (12) sparger support brackets and 60% of core spray nozzle welds, end cap welds, drain plug and welds on "A thru D" nozzles and drains. No change noted on the sparger bracket 05 at 136° from 2011. No other indications identified.

UT examination performed on 40 cells.

No indications identified Visual (VT-3) examination of 9 cells (02-19, 46-11, 42-59, 58-19, 02-39, 10-51, 18-03, 22-03, and 58-35), per SIL 554.

No indications identified.

r\\

1) i f'

I

'_,/

l l

\\_ j

\\_~*

/

\\

\\. _./

~

I

'-.._j 1995 197 6-present 1997 2009 2011 Core Plate (Rim, etc.)

1995 1997 2011 SLC 1997 2003 2007 VT-3 Visual (VT-3) of3 cells (14-23, 22-31, and 46-23) per SIL 554.

No indications identified.

VT-3 VT-3 examination every other refueling outage per Section XI.

No indications identified.

VT-3 Top Guide Grid examined from above, no indications identified.

VT-1 Adjacent aligner pins at 180 and 270 deg.(per VIP-26), no indications identified.

EVT-1 EVT-1 of five top guide cell locations per BWRVIP-183 requirements. No indications identified.

EVT-1 EVT-1 of fourteen top guide cell locations per BWRVIP-183 requirements. No indications identified.

VT-3 VT-3 examination of hold down bolt retainers planned, deferred to 1997.

VT-1 Examined 18 of 34 bolts/retainers from above. No indications identified.

VT-3 Examined 9 of 34 bolts/retainers from above. No indications identified. This satisfies the 25% commitment from the submitted Deviation Disposition UT UT of nozzle to safe end planned for 1997, per BWRVIP recommendations PT&UT PT & UT of nozzle to safe-end weld, no indications identified.

PT Extended dwell time PT of SLC nozzle to safe end weld and entire safe end.

No indications identified.

PT PT of SLC nozzle to safe end weld.

No indications identified.

54

f'

  • I I

\\._/

I

\\, )

(~.

/

\\

,/ \\

\\__)

\\,__ )

'-,J Jet Pump Assembly 2011 UT 1974 to VT-3 present 1981 VT&UT 1997 VT-3 CSVT-1 (MVT-1) 1999 UT 1999 EVT-1 55 UT of SLC nozzle to vessel and nozzle to safe end weld. No indications identified Visual VT-3 of all jet pump components performed every other refueling outage.

No indications identified.

VT and UT examination performed on all 20 hold down beams/

One beam found to be cracked, replaced with new style beam, All beams replaced with new style beam and reduced preload in 1988.

VT-3 all 20 jet pump assemblies (all parts),including CSVT-1 (MVT-1) of 10 riser braces, including all welds. No indications identified.

CSVT-1 (MVT-1) all 10 thermal sleeve to riser elbow welds, plus UT on pumps 1/ 2, 9/10, 13/14 due to indications on thermal sleeve side of these welds.

MVT-1 on welds RS-2 & RS-3 of three risers w/ indications@ 30, 150, and 300 degrees.

Evaluation of indications justified continued operation for part cycle.

Examinations performed on all 20 hold down beams. Reportable indications observed on hold down beam for jet pump

  1. 20. Beam replaced.

No other indications identified.

Examination of high priority Adapter welds on Jet Pumps 1-10.

Reportable indications on welds (AD-3b )

of Jet pumps 2 & 10. BWRVIP-41 evaluation resulted in use-as-is disposition. Expanded examinations to weld AD3b on Jet Pumps 11-20. No other indications identified.

EVT-1 examination of high priority Diffuser Shell to Tailpipe Welds ( DF-2) of Jet Pumps 1-10. No indications identified.

Examination of Riser welds RS-2 & RS-3 of Jet Pump Assemblies 2, 3 & 4.

No indications identified.

2001 EVT-1 Reexamined weld AD-3b on Jet Pumps 2

& 10. indications remain bounded by existing flaw evaluation.

All 20 WD-1 locations examined. 16 high priority and 45 medium priority welds on inlet mixers, diffusers, and riser braces also examined. No indications identified.

,,'~ \\

2003 VT-1 VT-1 of all twenty hold down beam

,~

ratchet lock keepers (replaced in 2001).

VT-1 all twenty WD-1 main wedge locations, since all inlet mixers were removed in 2001, Two auxiliary spring wedges installed in 2001, and the RS-1 repair clamp on JP 1 & 2 and 13 & 14.

No indications identified.

EVT-1 Reexamination of indication at RS-1 weld on JP 9 & 10.

Minimal change in flaw size. Structural reevaluation completed for continued acceptability.

104% of High priority welds completed.

72% of Medium priority welds completed No indications identified.

Indication identified in backing ring below AD-3a weld on JP 18. Structural evaluation found acceptable for continued operation.

2005 UT Two-sided UT of all diffuser and adapter welds (100) from l.D. Identified 4 small OD originating indications associated J

with the AD-3b fillet weld (2 previously ID'd). Structural and leakage evaluation proved acceptability for numerous operating cycles.

VT-1 VT-1 of five main wedges. No wear identified.

56 I

EVT-1 EVT-1of16 medium priority welds. No indications identified.

EVT-1of3 existing indications. No appreciable change in indication size.

2007 VT-1 VT-1 of 10 main wedges and 2 RS-1 riser repair clamps. No indications identified.

EVT-1 EVT-1 of 30 medium and high priority welds, 1 existing RS-1 weld indication and 12 riser brace welds. No growth of existing indication noted. Small indications identified at the RS-1 weld of two risers. Structural and leakage impact evaluations found indications acceptable for continued operation. No other indications identified.

2009 VT-1 VT-1 of 6 main wedges. Minor wear identified on 3 wedges. Expanded scope to examine all 20 main wedges and performed examinations on additional locations (AS-1/2, RS-6/7, RS-8, RS-9, MX-7) on the 3 JPs with identified wear.

Two set screw gaps identified. No additional indications in expanded scope exams. No repair hardware required.

EVT-1 EVT-1 of 31 medium and high priority welds.

3 existing RS-1 flaws were examined.

- 1 existing indication exhibited no growth and was evaluated as acceptable for two cycles of continued operation.

- 1 existing indication exhibited growth and was evaluated as acceptable for

\\.. - '

two cycles of continued operation.

- 1 existing indication was determined to be the toe of the weld. No indication exists.

No other indications identified.

2009 VT-3 VT-3 of two aux spring wedges. No indications identified.

57

2011 2013 VT-1 EVT-1 UT VT-1 EVT-1 EVT-1 58 A VT-1 of the BB-4 regions of all 20 JP hold down beams was performed with no indications identified. VT-1 examinations were performed on the following components with no indications identified: JP 01/02 RS-1 clamp, JP 13/14 RS-1clamp,JP04 MX-7 and JP 10 MX-

7. Recordable indications were identified on 10 JP wedges, 3 wedges were existing wear no change, 2 JPs had new minor wedge wear and 5 had minor rod wear.

EVT-1 of 53 medium and high priority locations

  • 2 existing RS-1 flaws were examined with no change in length
  • Set screw gaps identified on JP 03, 04 and 05 16 Hybrid Group 2 Hold Down Beams were examined no indications identified.

VT-1 of 10 wedge bearing surfaces WD-1 JPOl thru WD-1 JPlO was performed. No relevant change in indications from previous inspection.

EVT-1 of riser elbow to thermal sleeve weld RS-1 (JP 09/10 and JP 19/20).

Previously documented indication was observed with no apparent change in the indication from the previous inspection data.

EVT-1 of jet pumps JPs 03 and 05 vessel side and shroud side set screw gaps.

EVT-1 of JP 04 vessel side set screw gap.

New slight wear identified on the JP 03 SS, JP 03 VS and JP 04 VS belly band set screw interface. Comparison to P3Rl8 exam data identified these components had similar characteristics during the 2011 exam. No other indications identified.

2015 EVT-1, EVT-1 of ( 17) medium and high priority welds. 2 existing RS-1 flaws were examined with no change in length. No other indications identified.

VT-1, VT-1 of (2) riser clamps. No indications observed.

VT-1 often (10) JP main wedges. No new wedge wear was identified; however, wedge rod wear was identified on JP 11, JP12, JP15, and JP20. All previous wedge rod wear on JP09, JP16, JPl 7 and JP19 has not changed.

VT-3, VT-3 of the two (2) auxiliary wedges installed. No wear identified on JP14.

New wear on the JP09 aux. wedge and new wear into the belly band were noted.

The aux. wedge was in the over-travel position and accepted for continued use for one cycle.

EVT-1, A combination ofEVT-1 on the OD and UT UT from the ID on 10 jet pump diffuser/

adapter welds (AD-1, AD-2, DF-1, DF-2, AD3a/b and DF-3):

- UT diffuser scope: JP09, JPlO, JPl 1, JP12 and JP18. Previous indications on JP12 and JP09 AD3b showed small changes in length from 2005. JP18: 2of3 previous indications on AD3a showed no change from 2005. The third indication was not observed/ could not be found. All other welds were inspected SAT.

- EVT-1 diffuser scope: JP02, JP09, JPlO, JP13, JP14, JPl 7, JP18 and JP19.

Previous indication on JP02 AD3b showed no change from 2005. Previous indication on JPlO AD3b showed small change in length from 2005.

All conditions were evaluated as acceptable.

59

Jet Pump Diffuser See Jet Pump Assembly.

CRD Guide Tube 1985 VT-3 VT-3 PSI examination of 4 replacement CRD housings.

1987 VT-3 VT-3 examination of one of replaced housings.

No indications identified.

1991 VT-3 VT-3 examination of housings accessible from fuel cells 26-31and30-27.

No indications identified.

1999 VT-3 VT-3 examination on Guide Tube welds CRGT-1 & Alignment Pin weld (Core Locations: 14-15, 14-31, 14-47, 18-19, 18-27, 18-35, 18-43, 26-11, 34-35, 42-19)

No indications identified.

EVT-1 EVT-1 examination on Guide Tube welds CRGT-2 & 3 (Core Locations:14-15, 14-31, 14-47, 18-19, 18-27, 18-35, 18-43, 26-11, 34-35, 42-19)

No indications identified.

2003 EVT-1 Best effort EVT-1 on Guide Tube welds CRGT-2 & 3 (Core locations: 10-35, 22-27, 22-35, 30-23, 30-31, 30-39, 38-27, 38-31, 38-35, and 42-31) No indications identified.

VT-3 VT-3 examination on Guide Tube welds CRGT-1 & Alignment Pin weld (Core Locations: 10-35, 22-27, 22-35, 30-23, 30-31, 30-39, 38-27, 38-31, 38-35, and 42-31) No indications identified.

2005 EVT-1 EVT-1 on Guide Tube welds CRGT-2 &

3 (Core locations: 22-39, 38-39, 14-35, 46-35, 46-27, 22-23, and 26-11) No indications identified. CRGT-3 (22-39) later disqualified.

60

VT-3 VT-3 examination on Guide Tube welds CRGT-1 & Alignment Pin weld (Core Locations: 22-39, 38-39, 14-35, 46-35, 46-27, 22-23, and 26-11) Alignment pin weld also at 14-27 and 38-23, No indications identified.

CRD Guide Tube 2007 EVT-1 EVT-1 on Guide Tube welds CRGT-2 (cont.)

(Core locations 22-03, 30-15, 42-03, 46-55, 58-39) and CRGT-3 (Core locations 22-03, 30-15, 42-03, 46-55, 58-39). No indications identified.

Verification of CRGT-1 (Core locations 22-03, 30-15, 42-03, 46-55, 58-39) alignment pins and alignment lug welds.

No indications identified.

2009 EVT-1 EVT-1 on Guide Tube welds CRGT-2 (Core locations 14-31, 22-31, 22-59, 30-47, 50-51)

No indications identified.

CRD Stub Tube 1991 VT-3 VT-3 of accessible portions of 12 stub tubes (30-35, 26-35, 22-35, 22-31, 22-27, 26-27, 26-23, 30-23, 34-23, 34-27, 34-31, 30-31).

No indications identified.

In-Core Housing 1991 VT-3 VT-3 of housings accessible from fuel cells 26-31 and 30-27.

No indications identified.

Dry Tube 1997 NIA All Dry Tubes replaced in 1985.

All IRM and SRM tubes replaced w/

Wide Range Monitoring tubes in 1997.

No inspections required.

2015 VT-3 3 spare dry tubes (no WRNM detector installed) at core locations 16-45, 40-21 and 40-45 were found not fully engaged into the top guide. The observed conditions are acceptable as there remains enough insertion into the notches to laterally support the dry tube.

61

Instrument 1976 to PT PT examination performed on all Penetrations present instrument nozzle to safe end welds once per interval, per Section XI.

No indications identified.

1997 PT PT nozzle to safe-end (coupling) & safe-end to pipe welds on 2 nozzles. (N12A &

N12B). No indications identified.

2001 PT PT nozzle to safe-end (coupling) welds on 2 nozzles. (Nl lA & N16A). No indications identified.

Vessel ID Brackets 1976 to VT-1 or VT-1 and VT-3 of all ID bracket welds present VT-3 performed once per interval No indications identified.

1997 VT-1 All 10 Jet Pump riser brace to vessel welds, no indications identified.

1999 EVT-1 EVT-1 examination performed on 8 Core Spray Bracket Pads@ 15, 117, 123, 165, 195, 237, 243 & 345 AZ.

No indications identified.

2001 EVT-1 EVT-1 examination performed on 4 Feedwater Sparger brackets @ 4, 56, 64, and 116 Az., 3 Jet Pump Riser Braces@

90, 120, and 150 AZ., and 2 Steam Dryer Support Brackets @ 4, and 94 AZ. No indications identified.

2003 VT-1 Lower Surveillance Specimen brackets at 30°, 120°, and 300°.

VT-3 Upper Surveillance brackets at 30°, 120°,

and 300°.

Guide Rod brackets at 0° and 180°.

EVT-1 &

Steam Dryer support brackets at 184 ° and VT-3 274°.

EVT-1 Jet Pump riser brace to vessel welds JP 9/10 and JP 13/14.

No indications identified 2005 EVT-1 8 Feedwater sparger bracket welds and 16 jet pump riser brace welds. No indications identified.

62

2007 EVT-1 8 Core Spray pipe support brackets and one jet pump riser brace. No indications identified.

VT-3 4 Steam dryer hold down bracket welds.

No indications identified.

2011 EVT-1 Steam dryer support brackets at 004 °,

094°, 184°and 274° were examined with minor wear and rub marks found. The conditions were evaluated acceptable.

The upper guide rod bracket attachment welds at 0° and 180° were examined with no recordable indications identified.

The feedwater sparger brackets at the 030°, 090°, 150°, 210°, 270° and 330° sparger locations were examined with no recordable indications identified.

The jet pump riser brace to vessel welds for JPs 01/02, 09/10, 11/12 and 13/14 were examined with no recordable indications identified.

2015 EVT-1, Lower and Upper Surveillance Specimen VT-1 Holder (SSH) bracket attachment welds at 30, 120, and 300 degrees were examined.

No indications were noted on the attachment weld on SSH 030 deg. Wear was only identified on the vertical portion of the interface between the SSH and the bracket. The wear is minor and does not impact the bracket or specimen holder.

8 Core Spray pipe support brackets inspected. No indications identified.

LPCI Coupling NI A for this plant Steam Dryer 2003 VT-3 VT-3 of the entire top of the dryer (including all upper tie bars) and the 2 outer bank hoods and cover plates.

VT-1 VT-1 of 5 new central bank upper tie bars (added in 2001 ), 2 stop-drilled indications at the lower guide rod followers, and all GE SIL 644, Supp. 1 locations on outer bank hoods.

No indications identified. All previous repairs were satisfactory.

63

2005 VT-1 Completed all remaining BWRVIP-139 recommended inspections (68 locations).

No indications identified.

2007 VT-1 VT-1 of 23 high stress welds and all upper tie bars. No indications identified 2009 VT-1 Re-examination of six "red" end bank welds, two "green" drain channel welds, and welds on four lifting lugs per BWRVIP-139-A. No indications identified 2011 VT-1-89 Examinations were performed on the end panel plate to cover plate weld, end panel plate to sloped hood plate weld and end panel plate to vain cap plate weld on both the left and right end of bank 6 of the steam dryer. No recordable indications were identified. The lifting rods at 045°,

135°, 225°and 315° were examined with no recordable indications.

2013 VT-1 VT-1 examinations performed on steam dryer seismic brackets (SDSB) at 004°,

094 ° and 184 °. No additional wear was observed from the previous examination.

VT-1 on steam dryer lifting rod assemblies at 45°, 135°, 225° and 315°.

A new indication was noted on the northeast tack weld of the 225° lifting rod.

No recordable indications were identified on the other three lifting rod assemblies.

2015 Replacement As part of the EPU License Amendment Request (LAR), Exelon PBAPS replaced the Original Equipment Manufacturer (OEM) steam dryer with a 3-ring octagonal (Nordic style) Westinghouse dryer.

Steam Separator 2007 VT-1 VT-1 examinations performed on a sample of upper and lower shroud head bolt support ring gussets. No indications identified.

64

2009 VT-1 VT-1 examinations performed on a sample of upper and lower shroud head bolt support ring gussets. No indications identified.

2011 VT-1-89 Examinations were performed at four locations on both the lower support ring gussets and the upper support ring gussets. No recordable indications were identified. Examinations were performed on the separator standpipe tie straps minor historic damage was observed conditions were acceptable. A VT-1 examination was performed on shroud head bolt 07, indicator window and pin wear observed.

As a result, SHB 07 was removed. The four lifting lugs were examined with no recordable indications identified.

2013 VT-1 The four lifting lugs were examined with no recordable indications identified.

2015 VT-1, Examinations were performed on the VT-3 separator standpipe tie straps and all ( 4) lifting lugs. Found several gouges in the base metal of the lifting lug at 67.5 deg and new wear that appears to be historic.

Bent Tie Straps at locations: 78 deg, 95 deg, 15 0 deg, and 311 deg azimuths and a previously removed tie strap at 220 deg.

All observed conditions were acceptable.

Dissimilar Metal 2009 No examinations scheduled.

Welds (BWRVIP-75-A) 2011 No examinations scheduled.

65

2013 UT Examinations performed on 7 IGSCC Category A welds per BWRVIP-75-A.

No recordable indications were identified.

The welds examined were a pipe bend to pipe weld in the RHR system (10-0-23),

the core spray nozzle to safe end weld (14-A-46), a recirculation inlet nozzle to safe end weld (2-BHC-8), 2 RHR pipe to tee welds (10-2DB20-17, and 10-2DD20-

22) and 2 RHR tee to elbow welds (10-2DB20-19 and 10-2DD20-24). The last

( 4) RHR welds identified above were added during P3R19 (Fall 2013) as a result of EPU.

2015 PAUT 2 dissimilar metal welds (3-I-20: Category A and 12-I-2R: Category C) and 1 weld overlay (12-I-lC) were inspected using manual Phased Array UT. Areas ofless than minimum wall thickness allowable limit were discovered on 12-I-2R. The thinned piping and downstream elbow were replaced. A transition stainless steel piece was installed between the valve and the elbow. All other welds were inspected SAT. Additionally, as a result ofEPU, (4) welds were added to the RHR system during P3R20 (Fall 2015). These (4) welds are Category A welds: 10-2DA20-24, 10-2DA20-25, 10-2DC20-l 7, and 10-2DC20-19.

RPV Shell Welds 2015 UT RPV Shell Welds VlA,B,C thru (BWRVIP-05)

V5,A,B,C and circ. weld C6 were examined. The examinations were performed using automated Phased Array UT. Two indications were observed in the circumferential weld exam volume (C-6 shell to flange). The indications are subsurface flaws and allowable IA W Table IWB 3510-1 of ASME XI 2001 Ed, 2003 Ad.

66