JAFP-17-0023, Submittal of the Final Ultrasonic Test Results on the 24-10-130 Weld Overlay

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Submittal of the Final Ultrasonic Test Results on the 24-10-130 Weld Overlay
ML17068A370
Person / Time
Site: FitzPatrick Constellation icon.png
Issue date: 03/09/2017
From: Drews W
Entergy Nuclear Northeast, Entergy Nuclear Operations
To:
Document Control Desk, Office of Nuclear Reactor Regulation
References
JAFP-17-0023
Download: ML17068A370 (39)
v • d • e


Text

JAFP-17-0023 March 9, 2017 U.S. Nuclear Regulatory Commission Document Control Desk Washington, D. C. 20555

Subject:

Submittal of the Final Ultrasonic Test Results on the 24-10-130 Weld Overlay James A. FitzPatrick Nuclear Power Plant Docket No.

50-333 License No.

DPR-59

Reference:

1.

ENOI letter, Proposed Alternative to ASME Code Requirements for Weld Overlay Repair, RR-21 at James A. FitzPatrick Nuclear Power Plant, JAFP-17-0010, dated January 27, 2017

2.

NRC letter, Summary of January 30, 2017, Teleconference with Entergy Nuclear Operations, Inc. Regarding Verbal Authorization for Relief Request RR-21 for the James A. FitzPatrick Nuclear Power Plant (CAC No. MF9128), ML17031A280, dated February 8, 2017

Dear Sir or Madam:

During Refueling Outage R22, an indication was found by ultrasonic testing (UT) examination in A Residual Heat Removal Low Pressure Coolant Injection Loop weld number 24-10-130.

Pursuant to 10 CFR 50.55a(z)(1), James A. FitzPatrick Nuclear Power Plant (JAF) proposed a repair in accordance with Relief Request RR-21 [Reference 1] and included a commitment to submit information to the NRC regarding the results of the Weld Overlay repair. This letter submits results of UT examination of the Weld Overlay.

(1)

Weld Overlay examination results including a listing of indications detected, if any; (2)

Disposition of indications using the standards of ASME Section XI, Subsection IWB-3514-2 and/ or IWB-3514-3 criteria and, if possible, the type and nature of the indications is the final examination report for the Weld Overlay and a listing of the indications detected. The report contains disposition of indications in the Weld Overlay using the acceptance standards of ASME Section XI, Subsection IWB-3514-2 and/or IWB-3514-3 criteria and the type and nature of the indications. A total of eight indications have been dispositioned using ASME Section XI, Subsection IWB-3514-2 and IWB-3514-3 and ASME Section XI Appendix Q (Q-4100(c)). Five laminar flaws were evaluated per ASME Section XI, Subsection IWB-3514-3 and three planar flaws were evaluated per ASME Section XI, Subsection IWB-3514-2.

Entergy Nuclear Northeast Entergy Nuclear Operations, Inc.

James A. FitzPatrick NPP P.O. Box 110 Lycoming, NY 13093 Tel 315-342-3840 William C. Drews Regulatory Assurance Manager - JAF

JAFP-17-0023 Page 2 of 2 (3)

Discussion of any repairs to the weld overlay material and/or base metal and the reason for the repairs; and Prior to the installation of the weld overlay, base material indications were identified in the cast carbon steel valve body during the liquid penetrant testing (PT) examination. Indications in the cast carbon steel valve body beneath the Weld Overlay or within W' of the toe of the Weld Overlay were removed or reduced to an acceptable size to comply with ASME Section XI Code case N-504-4, paragraph (c) and Appendix Q, paragraph Q-2000 and Q-4100.

During installation of the Weld Overlay buffer layers, the detected axial indication in the dissimilar metal weld created a through wall leak. A manual shielded metal arc welding (SMAW) repair patch was applied over the through wall leak and repair of unacceptable indications in buffer layers was performed.

On 2/11/2017, eighteen (18) indications were identified in the Weld Overlay UT examination (Enclosure 2). The weld overlay repair consisted of mechanically removing a 360 degree area on the carbon steel valve side of the weld overlay and an area at top dead center of the stainless steel Tee side of the weld overlay.

The 360 degree repair cavity required reapplication of the temper bead layers due to the depth of the repair cavity. The stainless steel Tee repair required manual reapplication of the ER308L buffer layers. The remaining Alloy 52M was applied via machine Gas Tungsten-Arc Welding (GTAW).

Pages 3 and 4 of Enclosure 1 disposition the remaining indications in the final Weld Overlay after the Weld Overlay repair.

(4)

Description of the examination coverage achieved during the examination of the Weld Overlay. documents the examination coverage achieved during the examination of the final Weld Overlay. Page 7 of Enclosure 1 states the Total Weld Overlay Material coverage was 96.0% and the Total ISi Volume Coverage was 96.1 %.

This letter contains no new regulatory commitments. Should you have any questions, please contact me at (315) 349-6562.

Very truly yours, William C. Drews Regulatory Assurance Manager WCD:mh : :

JAF-17-RHR-130-WOL-R1: Phased Array Ultrasonic Examination Record JAF-17-RHR-130-WOL: Phased Array Ultrasonic Examination Record cc:

USNRC, Region I Administrator USNRC, Project Manager USNRC, Resident Inspector NY SERDA NYPSC

JAFP-17-0023 JAF-17-RHR-130-WOL-R1:

Phased Array Ultrasonic Examination Record (25 pages)

0 0

© Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAMINATION RECORD Examination Data Sheet No.:

Fitz atrick 24-10-130-WOL Re air Calibration Data Sheet Nos.:

See Comments Section Below Date:

02120/2017 Time:

Start: 1806 Finish: 2006 Plant: I J.A. Fltzoatrick Unit: I 1

!Procedure No.:

ISl-UT-126

!Revision:

13 Examination Scans Performed Yes No System:

RHR (Al - Residual Heat Removal IJ.A.F Work Order: 00407344-32 1 Axial CFacina Downstream\\

Component Conflauratlon:

WOL -Valve to Tee

!Weld No.:

124-10*130 COverlavl 2 Axial CFacina Uostreaml Coveraae: I CSee below for coveraae details\\

!Limitations:

100 Confiauration of Comoonent 3 Circumferential CClockwise<1l)

Comoonent Zero Datum:

IX= Too Dead Center I Y = OMW Centerline 4 Circumferential (Counterclockwise<1l)

Weld Overlay Width: 4.0" Norn.

!Weld Overlay Length: 82. 75"

~E_x_a_m_ln_a_t_lo_n~S_u_rf_ac_e_:_O_D~-+~~~~~~~~~~-E_x_a_m_l_n_atl_o~n~A_n=g_le_s~~~~~~~~~~-<Notes:

Temperature: 92'F Thermometer: 271398 Axial L-Wave Circ L-Wave

<*>As viewed facing downstream 0' through 85<><21 0' through 75<><2l (21 Examination angles are generated in 1° increments Examination Sensitlvitv:

47.0 dB 50.0 dB Comments: This report documents the results of the Weld Overlay Material examination and the Pre-Service Inspection. Results: ACCEPTABLE Examination performed to lhe requirements of ASME BP&V Code,Section XI, 2001 Edition wilh 2003 Addenda and the requirements of Relief Request RR-21.

Multiple Recordable Indications were noted wilhln the examination volume of the WOL material. Indications included both laminar and planar flaws.

Five laminar flaws were recorded, all meeting the acceptance criteria ofTable IWB-3514-3 and the conditions imposed on Code Case N-504-4 per RG 1.147 R17.

Three planar flaws were recorded, all meeting the acceptance criteria ofT able IWB-3514-2.

See the Flaw Indication Evaluation Sheets for additional details.

The Weld Base Material (WBM) axial planar flaw originally documented in SI Report No. JAF-17-RHR-130 Is not subject to IWB-3514 acceptance standards, and meels the requirements of Relief Request RR-21. Recorded depth of this axial flaw lying under the overlay material is recorded as 1.20" in deplh.

Examination Coverage Summary:

96.0%: WOL Material Exam Volume 96.1%: PSI/ ISi Exam Volume See the Examination Coverage Sheet for details.

The applicable Calibration Data Sheets are listed below:

JAF-17-CAL-050; JAF-17-CAL-051; JAF-17-CAL-052

// J

//,,f./

Examiner:

Wade Holloway JCh.. [

gff /

Examiner.

N/A

{I SI Reviewer:

Jason J. Halse Entergy Review:

Scott Reed Level:

Level.

el:

III Date:

N/A Date.

N/A Date:

III Date:

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ANll:

Gary Gustafson

~~~~ra~/Jlll-.l!lftdl Date:

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2120/17 N/A 2/20/17 2121/17

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0 CD Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAMINATION RECORD Examination Data Sheet No.:

Calibration Data Sheet Nos.:

Date:

02/20/2017 Time:

Procedure No.:

Sl-UT-126 Revision:

3 J.A.F Work Order: 00407344-32 Weld No.:

24-10-130 Overla anent Dead Center I Y = DMW Centerline Weld Overlay Length: 82.75" Fitz atrick 24-10-130-WOL Re air See Comments Section Below Start: 1806 Finish: 2006 Examination Scans Performed Clockwisel1>

Counterclockwisel1l rE_x_a_m_ln_a_t_lo_n_S~u_rf_ac_e_:_O_D~-t~~~~~_,.-~..,,-,~~-E_x_a_m_l_na_t_lorn~A_n~g_le_s~~~~~~~~~~~Notes :

Yes No Temperature: 92°F Thermometer: 271398 Axial L-Wave Circ L-Wave 111 As viewed facing downstream 0' through 85'121 0' through 75'l21 121 Examination angles are generated in 1° increments Examination Sensltlvl 47.0 dB 50.0 dB Comments: This report documents the resulls of the Weld Overlay Material examination and the Pre-Service Inspection. Results: ACCEPTABLE Examination performed to the requirements of ASME BP&V Code,Section XI, 2001 Edition with 2003 Addenda and the requirements of Relief Request RR-21.

Multiple Recordable Indications were noted within the examination volume of the WOL material. Indications included both laminar and planar flaws.

Five laminar flaws were recorded, all meeting the acceptance criteria ofTable IWB-3514-3 and the conditions imposed on Code Case N-504-4 per RG 1.147 R17.

Three planar flaws were recorded, all meeting the acceptance criteria of Table IWB-3514-2.

See the Flaw Indication Evaluation Sheets for additional details.

The Weld Base Material (WBM) axial planar flaw originally documented in SI Report No. JAF-17-RHR-130 is not subject to IWB-3514 acceptance standards, and meets the requirements of Relief Request RR-21. Recorded depth of this axial flaw lying under the overlay material is recorded as 1.20" In depth.

Examination Coverage Summary:

96.0%: WOL Material Exam Volume 96.1 %: PSI / ISi Exam Volume See the Examination Coverage Sheet for details.

The applicable Calibration Data Sheels are listed below:

JAF-17-CAL-050: JAF-17-CAL-051 : JAF-17-CAL-052 Examiner:

Wade Holloway Examiner:

NIA SI Reviewer:

Jason J. Halse Entergy Review:

Scott Reed

~~~~~.'.:...!:'='---'--""',,.;:'""'-~~~~

ANll:

Gary Gustafson III Date:

2/20/17 N/A Date:

NIA N/A Date:

2120/17 III Date:

2/21 /17 Date:

Page _/_ of _d

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0 CD Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAMINATION RECORD INDICATION DAT A SHEET COMPONET ID: 24-10-130-WOL No.

Angle u

l2 length Wl Wm ax W2 Width MPl MP max MP2 Depth to Depth to Flaw Type Scan Top Bottom Direction 1

o*

74.5 75.7 1.2 0.95 1.1 1.25 0.3 N/A N/A N/A 1.15 N/A Laminar N/A 2

o*

81.5 82 0.5

-0.5

-0.55

-0.6 0.1 N/A N/A N/A 0.77 N/A Laminar N/A 3

o*

68 69.25 1.25

-0.95

-0.9

-0.85 0.1 N/A N/A N/A 0.66 N/A Laminar N/A 4

o*

5.5 6

0.5 1.3 1.35 1.4 0.1 N/A N/A N/A 0.8 N/A Laminar N/A 5

o*

9 10 1

1.35 1.4 1.45 0.1 N/A N/A N/A 0.63 N/A Laminar N/A 6

33*

38 40.5 2.5 0.5 0.55 0.7 N/A 0.76 0.73 0.7 0.59 0.64 Planar OS 7

40*

48.5 50.75 2.25 1.05 1.2 1.35 N/A 0.6 0.56 0.52 0.4 0.46 Planar OS 8

38' 41 41.2 0.2

-0.42

-0.5

-0.58 N/A 1.32 1.3 1.2 0.95 1.04 Planar OS NOlE:

Component Zero Datum: length (X-directlon) =TDC, Width (Y-dlrection) = DMW Centerline Page_..2:_ord

0 CD

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Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAMINATION RECORD Flaw Indication Evaluation Sheet WOL Laminar Flaw Comparison to Acceptance Standards Flaw No.

1 2

3 4

5 ComponentlD: 24-10-130-WOL Flaw Flaw Lengthl'I Lenglhl'I Start End 74.50 75.70 81.5 82 68.00 69.25 5.50 6.00 9.00 10.00 Flaw Length 1.20 0.50 1.25 0.50 1.00 Total Flaw Length Flaw Width

Start 0.95

-0.60

-0.95 1.30 1.35 Flaw Wldth121 End 1.25

-0.50

-0.85 1.40 1.45 Flaw Wldthl21 0.30 0.10 0.10 0.10 0.10 Flaw Area 0.36 0.05 0.13 0.05 0.10 Total Flaw Area'"

Note ltl The length axis of the laminar flaw is parallel to the direction of welding Flaw Depth 1.15 0.77 0.66 0.80 0.63 Note 121 The width axis ol the laminar naw is pecpendlcular to the direction of welding

  • WOL Thickness 131 1.09 1.15 1.15 1.09 1.09 Width dimensions of laminar flaws supplied for the abo1.e calculations are best-effort estimates ASME Code Reallt Accept Accept Accept Accept Accept Linear Dimension Limit Accept Accept Accept Accept Accept Note 131 WOLthickness from UT Thickenss Report 817UT016 is taken as the a""'8ge thickness o\\et Station A (1.147") or Station B (1.093")

Station A from WSI Construction Dwg. 414691 =Location "B" from UT Thickness Report B17UT016.

Station B from WSI Construction Dwg. 414691 =Location "C" from UT Thickness Report 817UT016.

Comments:

Reduction in co1.erage due to laminar flaws is shown on a separate page.

Flaw #'s 1, 4 & 5: Postulated flaws ha1.e 2a dimension of 0.00" (maximum) owing to its proximity to the original material interface Flaw #2: Postulated law has 2a dimension of 0.10" (maximum) is the distance from the bottom of the laminar ftaws to the intersection of the 70" circ scans (CW, CCW).

Flaw #3: Postulated ftaw has 2a dimension of 0.20" (maximum) owing to its proximity to the original material interface Page~of~

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CD Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAMINATION RECORD Flaw Indication Evaluation Sheet WOL Planar Flaw Comparison to Acceptance Standards ComponentlD: 24-10-130-WOL ASME Section XI 2001/03 Table IWB-3514-2 Flaw (S) Depth Depth Flaw WOL Upper(OD)

Flaw Flaw Flaw OD to Top 00 to Bottom Thru*Walt Component Acceptlnc* Flaw Flaw Flaw Boundary Matertal Flaw Flaw No.

film End ~

3a 40:5 2.50 21.E!!!!.

~ ~

ThlckneW11 ThlcknHaA?J 0.59 064 0.05 1.22 1.09 0.03

~ Proxlmlly

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0.01 2.29 Subsurface AusleniUc 0.01 7

46 5 50.75 2.25 0.40 046 0.06 1.22 1.09 0.03 0.01 2.7-4 Subaurtace Au1tenrtic 0.01 41 41.2 0,20 0.95 1 04 0.09 1.22 1.15 0.05 0 22 3.92 Subsurface Austenillc 0.22 Comment WOL Postulated Radial Flaw Obstructed by Laminar Flaws Ftawa#1, 2 and 3 tJ.low,,. the mnlmum Sze poatulalld radlal ftawa which could r111lde within th* obstructed volume.

2

-0.60

-0,50 D.10 o.n 0.87 0.10 1.22 109 005 0.50 457 Subsurface AustenlUc 050 3

...0.95

-0.9 0.10 0.66 086 0.20 1.22 1147 0.10 050 B.72 Subsurface Au1tenitic 0.50 Subsurface Flaw olt%

2.29%

2.74%

3.92%

4.57%

8.72%

Code Allowable

~

B.52%

8.52%

9.07%

1 2. 43~

12.38%

Comment! The Flaw Througll-Wa11 (2a) dimension for asaumed hidden Flaw #2 (0.11 is the d11tance from the bottom of lhe laminar flaws lo the lnlersect1on of the 70* clrc scans (CW, CCW).

The Flaw Througll-Wall {2a) dimension for assumed hidden Flaw #3 (0.'Z'} is the distance flotn the bottom of lhe laminar flaw lo the original material interface.

Thia A!lpteSent* the mHlmum poalula1ed flaw lhroogh-wel dirnan~on. Code eMowabie ~

!tom th* !nsef'Ace eumlnation atand&rds of Tabte IWB-3514-2 Note 111 Nominal lh1cknesa Note Pl WOL lhiekneaa from UTThickensa Report Bt7UTD16 ia taken as the a..erage thickness o..er Station A (1 147") or Station B (1,093"}

Station A from WSI Construction Dwg. 414691

  • Location "B" from UT Thlcknesa Report B17UT016.

Station B from WSI Construction Owg. 41-4691 = Location*~ from UT Thicknesa Report B17UT018.

Page _d of Z t(

Sub1Urfsce Flaw Only

~

1

!!!!Y!!!

Acceptable Acceptabht Acceptable Acceptable Acceptable

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Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAMINATION RECORD Allowable Laminar Flaw Reduction in Coverage Criteria Q-4100 (c)(2)

Awrage Pipe OD:

24.16 From WSI Construction Drawing 414691 Post Machining Awrage WOL OD:

26 43 From WSI Construction Drawing 414691 Awrage Weld Axial Length:

2.43 (DMW width plus 1/2" on each side)

Length ofWOL Exam Volume:

3.68 Awrage as measured from WSI Contours Pipe (OD) Circumference:

75.86 WOL (OD) Circumference:

82.99 10"/0 of Pipe Circumference:

7.59 Largest Permissible Linear Dimension of Any Laminar Flaw 10"/0 of WOL Circumference:

8.30 Weld Surface Area: 184.35 ln 2 Weld lengt x Pipe Circumference 10"/0 of Weld Area: I 18.43 I Maximum Allowed Area of Laminar Flaws 0.69 I Total Combined Area of Laminar Flaws from Laminar Flaw table Total Combined Area (0.69 ln2) is less than 10% of the Average Weld Area (18.43 in2) and is therefore Acceptable Page 5"ar..!!J!

0 CD SS) Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAMINATION RECORD Supporting Data Images The underlying Axial Flaw below the overlay is located at 69" CW (Flow into Tee) as measured from the overlay centerline and at a depth from the overlay surface of 1.20", see screen shot image below.

Page _fE_ of 2 J/

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CD

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Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL-R1 PHASED ARRAY ULTRASONIC EXAM/NATION RECORD Examination Coverage of Weld Overlay Material Volume Weld Overlay Weld Overlay Component Component Weld Overlay Material Coverage Material Coverage Material Coverage Tota/Weld Combined Axial Scanning Circumferential Circumferential Overlay Material Identification Description Facing Upstream & Downstream Coverage Coverage Coverage Clockwise Counterclockwise JAF RHR 24"00 RHR 24-10-130 Valve-to-Tee 97.5%

95.2%

95.2%

96.0%

(Overlay)

Weld Overlay Notes:

1) Calculated volumetric coverage based on the ASME Section XI Code (Appendix Q) required volume.
2) Axial scan coverage based on the required one-directional examination coverage while scanning bi-directionally toward the tee and toward the valve.
3) Percentage of coverage is based on electronically generated area percentages.

Examination Coverage of ASME Code IS/ Volume ASME Section XI ASME Section XI ASME Section XI ASME Section XI Component Component Volume Coverage Volume Coverage Volume Coverage Volume Coverage Total /SI Volume Circumferential Circumferential Identification Description Axial Scanning Axial Scanning Coverage Coverage Coverage Downstream Upstream Clockwise Counterclockwise JAF RHR 24" 00 RHR 24-10-130 Valve-to-Tee 99.9%

66.4%

96.2%

96.2%

96.1%

(Overlay)

Weld Overlay Notes:

1) Calculated volumetric coverage based on the ASME Section XI Code (Appendix Q) required volume.
2) ASME Section XI axial scan coverage based on bidirectional examination from both sides of the weld overlay.
3) Percentage of coverage is based on electronically generated area percentages.

PageJ....or24'

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Structural Integrity Associates Report#: JAF-17-RHR-130-WOL-Rl ULTRASONIC PHASED ARRAY CAL/BRAT/ON RECORD 0

Customer: Entergy I

Calibration Sheet:IJAF-17-CAL-050 Plant/Unit: J.A. Fitzpatrick I Unit 1 I Procedure No:IS1-UT-12S, Rev. 3 ComPOnent/Svstem: 24-10..130 (Overlay) I RHR Valve-to-Tee Weld Overlay Wed!le Manufacturer:

SI Refracted An!lle Verification Model:

100102 Focal Law Measured Index Offset Material:

Rexolite Angle Angle (in)

Velocitv:

2330 (mis) so*

so*

0.40 Wedge Anale:

1s.2*

45*

45*

0.45 Scan Direction:

Axial 30° 30' 0.54 Wedge Nominal OD:

28' Instrument Search Unit lntearal Cable Manufacturer:

Zetec TvDe:

34 Conductor I 38 Gauge Coaxial Model:

OmniScan MX Length:

8' Serial Number:

OMNl-100084 Connectors:

1-Pex Phased Array Module:

OMNl-M-PA32 / 128PR Intermediate Cable PA Module Serial No.:

OMNl*S212 Tvoe: I NIA Software Revision:

1.4R3 Length:

NIA Instrument Settings:

See Next Page Connectors:

N/A Search Unit Manufacturer:

GEIT Element Len!lth:

2.70mm Transmit Model:

115-000-613 Element Width:

1.15mm Transmit Serial Number:

01VW13 Elements IPrlmarv Axlsl:

1S Receive Model:

115-000-613 Elements ISecondarv Axisl:

2 0

Receive Serial Number:

01VW13 Inactive Element - Transmit:

0 Frequency IMHzl:

2.0 Inactive Element - Receive:

0 Calibration Data Flies Focal Law: RHR_28A_2MTRL2x1S_Q..85_N_52mmHP.law Angles Generated: O' through as* (1° Increments)

Wave Mode:

Long~udinal Set-up File: 28 AX 52mm 45-SQ..70.ops Focal Sound Path:

52mm Couplant I Batch Ultragel II / 12325A Calibration Blocklsl:

Sl-24-AX-01 Calibration Reflector Data Comments:

Calibration Reference

%FSH Ref.Gain Wedge Delay Active element checks performed at initial Reflector Ana le and final cal checks.

0.1" Deep SDH ao*

82%

37d8 2.9 µs Intermediate Check: 2120117-1852 O.S" Deep SDH 70° 80%

45d8 0.2 us Reference Block No.: Sl-14-AX-01 1.1"DeepSDH so*

87%

45d8 1.Sus Temperature: 98"F 1.4" Deep SDH 45° 83%

40d8 2.5 us SIN: 271398 1.2" Deep SDH o*

84%

37d8 2.9us Calibration Performed Examiner Level Date-Time Initial:

Wade Holloway/;(/~/

m 2120/17 - 1 SOO Final:

Wade Holloway /~_/ ~~

III 2/20/17 - 2040 SI Reviewed:

Jason J. Halsey /::__ L::P/ _)_ /:/

N/A 2120/17 0

Client Review:

Scott Reed

~.._./x )

/)

III z./z.,/zo17 ANllReview: LAILV c,.,,,...=--..J J.L, A..,,.-x}/ ~

N/A l/z,J,7

( ~

Page _jJ_ of 1:1

55) Structural Integrity Associates Report#: JAF-17-RHR-130-WOL-Rl File Name 28 AX_52mm_ 45-60-70.ops Menu Item

.L Essential Instrument Settir!g File e

rile Fonnnl

-~ctun On @euts ITT Paramclcrs Into Report)

ReadinP Result Selector

!Lisi I Field I A% (Peak Amnliludc In GD.le A)

Ficld2 IA I Position Of Peak Si11na] In Gate A)

UT General St on IO (Dcfoull)

Rlln"C 12.80 Sound Vclocitv 10.2283 in/us LOCKED Pulser Pulser I (Per Focal Law) LOCKED Tx/Rx Modc PE (Per Focal LawT LOCKED Volln"c flioh PW Auto PRF Ontimum Reccin:r ~

I !Per Foa!l I.a" l LOCKED None FW Video Filler Off Averagi!!g I

Rcicct 0

Beam Gain Offset 10.0dll Dcnrn Dela**

I 14.52 us 0

Advanced Points Qt\\'

Auto Sum Gain IAuto (!_n this position t!!£ instrument will set the~-

J>~y Selection DiSnla\\*

IA-S.C Proicclion On Rulers LIT Unit True Dcnth

%Ruler l.incail%1 TCG Off Gate On Cursor On Color Sc.icct IAmnlitudc Stnrt lo/*)

0.0 End I%)

1100.0 Proncrties Source:

INonnal

!'.!obe/Part _ ---

Select Select ISclcCI TX I RX Auto Detect I Off PGM Probe Conlio.uration Scan T-IScclorial Connection P 11 1.a,..

I Auto Prof'TDJTl

!Off

-Gate/Alarm Gate Gale Select IGntcA:

S\\nchro

!Pulse c

Page~of.£i

© Structural Integrity Associates Report#: JAF-17-RHR-130-WOL-RJ ULTRASONIC PHASED ARRAY CAL/BRAT/ON RECORD Customer: Entergy Calibration Sheet: JAF-17-CAL-051 Plant/Unit: J.A. Fitzpatrick I Unit 1 Procedure No: Sl-UT-12S, Rev. 3 Com onent/S stem: 24-10-130 (Overlay) I RHR Valve-lo-Tee Weld Overlay Wedge Manufacturer:

SI Refracted Angle Verification Model:

100102 Focal Law Measured Index Offset Material:

Rexolite Angle Angle (in)

Velocity:

2330 (mis) so*

so*

0.40 Wed11e An11le:

1s.2*

45*

45*

0.45 Scan Direction:

Axial 30*

30*

0.54 Wedae Nominal OD:

28" Instrument Search Unit lntearal Cable Manufacturer:

Zetec Type: I 34 Conductor I 38 Gauge Coaxial Model:

OmniScanMX Lenath: I B'

Serial Number:

OMNl-100084 Connectors:

1-Pex Phased Array Module:

OMNl-M-PA32 / 12BPR lntennedlate Cable PA Module Serial No.:

OMNl-6212 TYoe:

NIA Software Revision:

1.4R3 Length:

NIA Instrument Settlnas:

See Next Page Connectors:

NIA Search Unit Manufacturer:

GEIT Element Len11th:

2.70mm Transmit Model:

115-000-613 Element Width:

1.15mm 0

Transmit Serial Number:

01VW13 Elements (Primary Axis):

1S Receive Model:

115-000-613 Elements (Secondary Axis):

2 Receive Serial Number:

01VW13 Inactive Element - Transmit:

0 FreauencY IMHzl:

2.0 Inactive Element - Receive:

0 Calibration Data Flies Focal Law: RHR 28A_2MTRL2x1S 0-85_N 20mmHP.law Angles Generated: 0° through 85" 11° Increments!

Wave Mode:

Longltudinal Set-up File: 28_AX_20mm 0-80.ops Focal Sound Path:

20mm Couplant I Batch Ultragel II / 12325A Calibration Block(s):

Sl-24-AX-01 Calibration Reflector Data Comments:

Calibration Reference

'loFSH Ref. Gain Wedge Delay Active element checks performed at initial Reflector Angle and final cal checks.

0.1 " Deep SDH so*

84%

40dB 1.1 µs Intermediate Check: 2120117 - 1935 1.2" Deep SDH o*

88%

36dB 1.1 us Reference Block No.: Sl-14-AX-01 Temperature: 98"F SIN: 271398 Calibration Perfonned Examiner Level Date-Time Initial:

Wade Holloway Ill 2120/17 -1S15 Final:

Wade Holloway Ill 2120117 - 2050 SI Reviewed:

Jason J. Halsey N/A 2120117 0

Client Review:

Scott Reed Ill ANllRevlew: &°vqoi"So..J N/A

~1z.

~

Structural Integrity Associates Report#: JAF-17-RHR-130-WOL-Rl e

File Name I

28_~_20mm_0-80.ops Menu Item I

Essential Instrument Setting File File Format Selun IQ.ti Unnuts UT Paramclers lnlo Rev.art)

ReadinP R\\.-suh Selector IList I Field I IA% (Pcnk Amnlitudc In Gate Al Ficld2 IA'" I Position Of Peak Sinn11J In Gale A\\

UT Gcm:ral Slllrt O{DcfuulO Ranee 069 Sound Vclocitv 0.2283 in/us LOCKED PulS4!f Pulser I IPer Focal Law) LOCKED Tx/Rx Mooe PE /Per Focal Law) LOCKED Voltat!.c llii!h PW Auto PRF Ootimum Receiver Receiver I IPcr Focal Lawl LOCKED Filler None Rectifier FW Video Filll.-r Off A\\*---in11 I

Rcicct 0

Ucum Gain Offsc1 0.0 dB 0

Beam Delay 17.81 us Ad,*nnccd Points Of\\.'

I Auto Sum Gain I Aut~~~~s ition the instrument will sci the vtlluc)

Disnlav Selection Disnlav IA*S.C Proicction On Rukrs 1JT Unit True Dc,,lh

%Ruler Lincar t%)

TCG Off Gate On Cursor On Color Select IAmnl1tudc Start Wo}

10.0 End '%)

1100.0 Proncrtics Source Normal Probe/Part Sch..-et Select ISclcct TX I RX Auto Detect I Off PGM Probe Conlirtumtion Scan Tvnc IScctorial Connection P II Laws I

Auto Pro~

I Off Gate/Alarm Gale 0

Gate Select IGal<A.

Svnchro I Pulse Page 2:~of 2q

© Structural Integrity Associates Report#: JAF-17-RHR-130-WOL-Rl ULTRASONIC PHASED ARRAY CAL/BRA TION RECORD Customer: Entergy I

Calibration Sheet:IJAF-17-CAL-052 I

Plant/Unit: J.A. Fitzpatrick I Unit 1 I Procedure No:ISl-UT-126, Rev. 3 I

Component/System: 24-10-130 (Ovenay) I RHR Valve-to-Tee Weld Ovenay Wedae Manufacturer:

SI Refracted Anale Verification Model:

100102 Focal Law Measured Index Offset Material:

Rexolite Angle Angle (In)

Velocity:

2330 (mis) 55' 55' 0.38 Wedge Angle:

16.2° 45*

45*

0.50 Scan Direction:

Circumferential 30' 30*

0.60 Wedae Nominal OD:

28" Instrument Search Unit Integral Cable Manufacturer:

Zetec Type:

34 Conductor I 38 Gauge Coaxial Model:

OmniScanMX Length:

8' Serial Number:

OMNl-100084 Connectors:

1-Pex Phased Array Module:

OMNl-M-PA32 I 128PR Intermediate Cable PA Module Serial No.:

OMNl-6212 Type:

NIA Software Revision:

1.4R3 Lenath:

NIA Instrument Settlnas:

See Next Page Connectors:

NIA Search Unit Manufacturer:

GEIT Element Lenath:

2.70mm Transmit Model:

115-000-613 Element Width:

1.15mm 0

Transmit Serial Number:

01VW13 Elements (Primary Axlsl:

16 Receive Model:

115-000-613 Elements (Secondary Axis):

2 Receive Serial Number:

01VW13 Inactive Element - Transmit:

0 Frequency (MHz):

2.0 Inactive Element - Receive:

0 Calibration Data Flies Focal Law: RHR 28C 2MTRL2x16 Cl-75 N_38mmHP.law Anales Generated: O' lhrouah 75" (1° Increments)

Wave Mode:

Longitudinal Set-uo File: 28 CIRC 1 38mm.ops Focal Sound Path:

38mm Couplant I Batch Uttragel II I 12325A Calibration Blocklsl: Sl-24-CIRC-01 Calibration Reflector Data Comments:

Calibration Reference

%FSH Ref. Gain Wedge Delay Active element checks perfOITlled at initial Reflector Angle and final cal checks.

0.6' Deep SDH 51° 82%

37dB 3.3 µs Intermediate Check: 2120117 - 1800 1.0* Deep SDH 49° 89%

40d8 3.3us Reference Block No.: Sl-14-CIRC-01 1.3" Deep SDH 47° 82%

40dB 3.9us Temperature: 98'F SIN: 271398 Calibration Performed Level Date -Time Initial:

Wade Holloway m

2120117 -1630 Final:

III 2120117 - 2045 SI Reviewed:

N/A 2120117 Client Review:

ANllReview: &Ar1..<?

© Structural Integrity Associates Report#: JAF-17-RHR-130-WOL-Rl e

File Name 2B_CJRC 1_38mm.ops Menu Item Essential Instrument Setting File File Fomuu Sctun On @r.uts UT PW1U11ctcrs Into Rcpon)

ReadinP Result Selector List l Field I A% (Peak Amnlitudc Jn Gare A)

Ficld2 A" (Position Of Peak Si 0 nal Jn Gate A}

UT General 511111 lo (Dcfoull)

Rnn *c 12.70 Sound Vclocit\\.'

10.2283 in/ols LOCKED Pulser Pulser I <Per Focal Law) LOCKED Tx/Rx Mode PE (Per Focnl Law) LOCKED Vollaec Hi*h rw Auto PRF Qntimum Receiver Rccd\\.*cr I CPcr Focul Low) LOCKED Filter None Rectifier FW Video Filler Off Av........ nin11 I

Rcii.-cl 0

Beam Gain Offset 0.0 dB Hi:amDclu

  • I 14 68 us Advanced roints Otv Auto Sum Gain Auto Hn lhis_position the in~mcnt will st:I the value\\

0 Disnlav Selection Oisnla\\'

IA-S.C I

Proicction I On Rulers UT Unit True !Jcnth

%Ruler Lincnr {%l TCG Off Gate On Cursor On Color Select Amnlilude StMtl%)

0.0 End Wo)

IOOO Proocnics Source Nonnal Probe/Part Select Select ISelcctTX / RX AutoDclcct I Off PGM Probe Conffouration ScanT... ~

IScclorial Connection P II Lau*

I Auto Pros!rain jOff Gate/Alarm Gate Gn1eSch..-ct IGulcA:

s~ chro I Pulse 0

Page B of..2:i

JAFP-17-0023 JAF-17-RHR-130-WOL:

Phased Array Ultrasonic Examination Record (10 pages)

0 0

CD

('.t Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL PHASED ARRAY ULTRASONIC EXAMINATION RECORD Examination Data Sheet No.:

Fitz atrick 24-10-130-WOL Calibration Data Sheet Nos.:

See Comments Section Below Date:

02/1 1/2017 Time:

Start: 1128 Finish: 2145 Procedure No.:

Sl-UT-126 Revision:

3 Examination Scans Performed Yes No J.A.F Work Order: 00407344-32 Weld No.:

24-10-130 Overla Dead Center I Y = DMW Centerline Circumferential Counterclockwise(!>

Weld Overlay Length: 82.75" 1--~~~~~~~~~~-r-~~~~~~~~---~_E_x_a_m~in_a_t~lorn~A_n~g~le_s~~~~~~~~~~---1Notes :

Axial L-Wave Gire L-Wave 111 As viewed facing downstream Temperature: 96°F Thermometer: 271396 o* through 85° 121 00 through 75o<21 121 Examination angles are generated in 1° increments Examination Sensitlvi 46.0 dB 48.0 dB Comments:

This report documents the results of the Weld Overlay Material examination for the exam volume depicted in Figure Q-4100-1 of ASME Section XI Appendix Q.

Examination performed to the requirements of ASME BP&V Code,Section XI, 2001 Edition with 2003 Addenda and the requirements of Relief Request RR-21.

Multiple Recordable Indications were noted within the examination volume of the WOL material. Indications included both laminar and planar flaws.

Laminar flaws #1, 2, 3, 4, 6, 7, 8, 9, 10 and 11 exceed the acceplance criteria ofTable IWB-3514-3 and the conditions imposed on Code Case N-504-4 per RG 1.147 R17.

Laminar flaw #5 Is Rejectable based on the maximum postulated planar flaw residing under the obstructed volume exceeding the acceptance criteria of Table IWB-3514-2.

Planar flaw #'s 15 -18 combine together by proximity rules to exceed the acceptance criteria ofTable IWB-3514-2.

~ I wou~-.. I See the Flaw Indication Evaluation Sheets for additional details.

Examination Coverage: Exam volume coverage will be determined using final weld overlay contours following the completion of weld repairs.

The applicable Calibration Data Sheets are listed below:

JAF-17-CAL-047; JAF-17-CAL-048; JAF-17-CAL-049 Examiner:

Wade Holloway Level:

Examiner:

N/A

~~~~~~~-7"7<-~-r"'i'-2""=-=f-::--

S I Reviewer: ~~~~~~~~

el:

Page_/_

III N/A N/A III ofl.Q Date:

2115/17 Date:

N/A Date:

2/15/17 Date:

z..//~/z...,;z Date:

z..&G.bz

)

0 CD

{'.r Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL PHASED ARRAY ULTRASONIC EXAMINATION RECORD INDICATION DATA SHEET COMPONET ID: 24-10-130-WOL Angle u

l2 length Wl Wmax W2 Width MP1 MP max MP2 Depth to Depth to Flaw Type Scan No.

Top Bottom Direction 1

o*

81.5 38 39.25

-0.75

-0.85

-0.95

-0.2 N/A N/A N/A 0.6 N/A Laminar N/A 2

o*

3 7

4

-0.6

-0.65

-0.7

-0.1 N/A N/A N/A 0.43 N/A Laminar N/A 3

O" 6.5 12 5.5 0.2 0.3 0.4 0.2 N/A N/A N/A 0.82 N/A Laminar N/A 4

o*

9 9.6 0.6

-0.125

-0.25

-0.35

-0.23 N/A N/A N/A 0.85 N/A Laminar N/A 5

o*

42.75 45.5 2.75

-0.9

-0.95

-1.0

-0.1 N/A N/A N/A 0.5 N/A Laminar N/A 6

o*

56.5 60.25 3.75

-0.8

-0.85

-0.9

-0.1 N/A N/A N/A 0.54 N/A Laminar N/A 7

o*

61.25 67 5.75

  • 1.2

-1.25

  • 1.3

-0.1 N/A N/A N/A 0.49 N/A Laminar N/A 8

o*

62.2 82.75 20.55

  • 1.05

-1.1

-1.15

-0.1 N/A N/A N/A 0.4 N/A Laminar N/A 9

o*

63.5 63.9 0.4

-0.8

-0.85

-0.9

-0.1 N/A N/A N/A 0.6 N/A Laminar N/A lD o*

67.75 69.25 1.5

-0.75

-0.8

-0.85

-0.1 N/A N/A N/A 0.75 N/A Laminar N/A 11 o*

71 82.75 11.75

-0.85

-0.9

-0.95

-0.1 N/A N/A N/A 0.55 N/A Laminar N/A 12 o*

74.5 75.7 1.2 0.95 1.1 1.25 0.3 N/A N/A N/A 1.15 N/A Laminar N/A 13 33*

38 40.5 2.5 0.5 0.55 0.7 N/A 0.76 0.73 0.7 0.59 0.64 Planar OS 14 40*

48.5 50.75 2.25 1.0S 1.2 1.3S N/A 0.6 0.56 0.52 0.4 0.46 Planar OS 15 35*

81.5 82.75 1.25 0.85 LO 1.15 N/A 0.9 0.87 0.78 0.64 0.74 Planar 05 16 49*

80.1 80.6 0.5 1.1 1.15 1.25 N/A 0.67 0.64 0.6 0.37 0.44 Planar OS 17 25*

78 5.25 10 0.55 0.6 0.7 N/A 1.09 1

0.95 0.88 0.96 Planar 05 18 ss*

78 5.25 10 1

1.1 1.2 N/A 0.68 0.58 0.5 0.3 0.35 Planar OS NOTE:

Indication #'s 15

  • 18 are combined by proximity rules for evaluation.

Page~

of.!S2

0 0

CD

{'.t Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL PHASED ARRAY ULTRASONIC EXAMINATION RECORD Flaw Indication Evaluation Sheet WOL Laminar Flaw Comparison to Acceptance Standards Component ID: 24-10-130-WOL Additional Relief Request Acceptance Standards Flaw Flaw Flaw Flaw Volume ASME Linear Obstructed Flaw Lengthl'I Length

Flaw Wldthl'I Wldthl'I Flaw Flaw Flaw Obstructed WOL Code Dimension Volume No.

Start End Length Start End Width

Ara a Depth by Flaw Thickneos

Result Limit Limit141 1

81.50 38.00 39.25

-0.75

-0.95 0.20 7.85 0.60 NIA 1.15 E

lBO 2

3 4.00

-0.60

-0.70 0.10 0.40 0.43 NIA 1.15 3

6.50 12.00 5.50 0.20 0.40 0.20 1.10 0.82 NIA 1.15 Laminar Flaws# 1, 2, 3, 4, 6, 7, 8, 9, 10, and 11 are 4

9.00 9.60 0.60

-0.13

-0.35 0.23 0.14 0.85 NIA 1.15 combined due to proximity per IWA-3360. The total all!a 6

56.50 60.25 3.75

-0.80

-0.90 0.10 0.38 0.54 NIA 1.15 per IWA-3360 (b) is 81.92 sq. in. This exceeds the 7

61.25 67.00 5.75

-1.20

-1.30 0.10 0.58 0.49 NIA 1.15 Allowable Laminar Area of 7.5 sq. in. of Table IWB-3514-3.

8 62.20 82.75 20.55

-1.05

-1.15 0.10 2.06 0.40 NIA 1.15 Per the conditions imposed on Code Case N-504-4 per 9

63 50 63.90 0.40

-0.80

-0.90 0.10 0.04 0.60 NIA 1.15 RG 1.147 R17, "a) the sum of the laminar flaw length in 10 67.75 69.25 1.50

-0.75

-0.85 0.10 0.15 0.75 NIA 1.15 any direction shall be less than 10% of the O\\ellay". This 71.00 82.75

-0.85

-0.95 0.10 0.55 NIA 1.15 criteria is also exceeded.

1.70 0.000 Total Flaw Area = 64.25in. x 1. 70in.

Total Total Flaw Flaw Width Volume 5

42.75 45.50

-0.90

-1.00 0.10 0.50 1.15 Accept Accept TBD 12 74.50 75.70 1.20 0.95 1.25 0.30 1.15 1.05 Accept Accept TBD Note 111 The length axis of the laminar law is parallel to the direction of welding Note The width axis of !he laminar flaw is perpendicular lo the direction of welding.

Width dimensions or laminar flaws supplied for the abow calculations are best~ffort estimates Note 131 WOL lhickness from UTThickenss Report B17UT015 is taken as the awrage thickness owr Station A (1. 145") or Station B (1.05")

Station A from WSI Construction Dwg. 414691 =Location "B" from UT Thickness Report B17UT015.

Station B from WSI Construction Dwg. 414691 = Localion "C" from UT Thickness Report B17UT015.

Note 1*1 Obstructed Volume Limit not calculated due lo flaws exceeding other acceptance criteria.

Note l*I Total Flaw Area is calculated in accordance with M/A-3360(b).

Pagei arJ.Q

r 0

{J Structural Integrity Associates Report No.: JAF-17-RHR-130-WOL PHASED ARRAY ULTRASONIC EXAMINATION RECORD Flaw Indication Evaluation Sheet WOL Planar Flaw Comparison to Acceptance Standards ComponentlD: 24-10-130-WOL ASME Section XI 2001/03 Table IWB-3514-2 Flaw Sub91.1rfllce CSI Depth Depth Flaw WOL Upper(OO)

Sub*uflce Code Flaw Flaw Flaw Flaw 00 to Top OD to Bottom Thru-Wall Component Acuptanc. Flaw Flaw Flaw Bound Hy Material Flaw Flaw Allowable Only Flaw~ Start End ~

of Flaw

~ !!.

Thlckna.J11 ThlcknuJ11 !

~ elt%

Prcalmltv 1-

  • It%

alt%

~

13 38 40.5 2.50 0.59 0.64 0.05 1.22 1.05 003 001 2.38 Sublurt.ce Austanillc 0.01 2.38%

8.50%

1 48.5 50.75 2.25 0.40 0.46 0.06 1.22 1.05 0.03 0 01 2.86 Subsulface Austenltlc 0.01 2.66%

8.50%

1 15 - 18 78 5.25 10.00 0.30 0.95 0.65 1.22 1.05 0.33 003 J0.95 Subsurface Austenitic 0.03 30.95%

7......

0.92 Comment.: Flaw #'s 15 - 18 combine to represent an area of Indications from 1s* to s.2s* at wrying depths (max O us*) and metal palha that haw to be linked together, WOL Postulated Radlal Flaw Obstructed by Laminar Flaws Flaw1#6 and #12 below are the maiclmum size pollulated nidlal ftaw*w~ch cauld reside within th* obttructed volume,.lllltlng from WOL Laminar Fl*w*#6 and #12.

5

-0.90

  • 1.00 0.10 0.50 0.95 0.45 1.22 1.15 0.23 2.25 19.57 Subsufface Austenilic o.50 19.57%

BAB%

12 0.95 1.25 0.30 1.15 1 15 0.00 1.22 1.05 0.00 a 00 o 00 Subturface Auatenftic 0.00 o 00%

8.43%

Comm*nl: The Flaw Through-Wall (2a) dimensions for assumed hidden Flaws #5 and #12, DAS' and 0.0" respectc\\ely, are the distances rrom the bottom of the lamlnar flaws to the original material interface.

Thi* represents th& maximum postulated naw throog~I dimension.

Note 111 Nominal lhlckness Note

WOL thickness from UTlhickanu Report B17UTU15 ii taken as the &'lerage thlcknesa awr Station A (1.145.) orStation B (1.05"}

Statk>n A from WSI Construction Owg. 414691 =Location "B" ftOm UT Thickness Report B17UTD15.

Station 9 frnm WSI Construc:lion Owg. 414691 = LocaHon "C' from UTlhickneu Report 817UlU15.

Page A of J..Q.

Re suite Acceptable Acceptable

lJ Structural Integrity Associates Report#: JAF-17-RHR-130-WOL ULTRASONIC PHASED ARRAY CALIBRATION RECORD e

Customer: Entergy I

Calibration Sheet:IJAF-17-CAL-047 Plant/Unit: J.A. Fitzpatrick I Unit 1 I Procedure No:IS1-UT-12S, Rev. 3 Component/System: 24-10-130 (Overfay) I RHR Valve-to-Tee Weld Overlay Wedge Manufacturer:

SI Refracted Anale Verification Model:

100102 Focal Law Measured Index Offset Material:

Rexolite Angle Angle (in)

Velocity:

2330 (mis) so*

so*

0.40 Wedae Anale:

1S.2° 45*

45*

0.45 Scan Direction:

Axial 30" 30" 0.54 Wedae Nominal OD:

28" Instrument Search Unit lntearal Cable Manufacturer:

Zetec Type:

34 Conductor I 38 Gauge Coaxial Model:

OmniScan MX Lenath:

8' Serial Number:

OMNl-100084 Connectors:

1-Pex Phased Array Module:

OMNl-M-PA32 / 128PR Intermediate Cable PA Module Serial No.:

OMNl-6212 Type:

N/A Software Revision:

1.4R3 Lenath:

N/A Instrument Settlnas:

See Next Page Connectors:

NIA Search Unit Manufacturer:

GEIT Element Lenath:

2.70mm Transmit Model:

115-000-613 Element Width:

1.15mm Transmit Serial Number:

01VW13 Elements IPrimarv Axisl:

1S 0

Receive Model:

115-000-613 Elements ISecondarv Axisl:

2 Receive Serial Number:

01VW13 Inactive Element - Transmit:

0 Frequency MHz):

2.0 Inactive Element - Receive:

0 Calibration Data Files Focal Law: RHR 28A 2MTRL2x1S 0-85 N 52mmHP.law Anales Generated: 0" throuah 85" (1° Increments)

Wave Mode:

Lang~udinal Set-up File: 28 AX 52mm 45-60-70.ops Focal Sound Path:

52mm Couplant I Batch Ultragel II / 12325A Calibration Blocklsl:

Sl-24-AX-01 Calibration Reflector Data Comments:

Calibration Reference

%FSH Ref. Gain Wedge Delay Active element checks performed at initial Reflector Ana le and final cal checks.

0.1" Deep SDH 80° 80%

39d8 O.S µs Intermediate Check: 2/11/17 -112S, 2100 0.S" Deep SDH 70° 80%

46d8 o.s us Reference Block No.: Sl-14-AX-01 1.1" Deep SDH S0° 80%

45d8 1.Sus Temperature: BO"F 1.4" Deep SDH 45° 80%

42dB 2.5us S/N: 271398 1.2" Deep SDH oo 80%

37dB 1.1 us Calibration Performed Examiner Level Date-Time Initial:

Wade Holloway £//_ /L// /'

III 2/11/17 -1000 Final:

Wade Holloway d/ £L/

llI 2/11/17-2219 SI Reviewed:

Jason J. Halsey ~/?J/" N/A 2/13/17 Client Review:

Scott Reed

'Sc-.-!~)

III z..;,,,,-/,7 0

ANllReview: rAllu r>.. --;o...,..-,.J

,f b::::?

N/A z..1tJ,7 A

Pae(~

g --

~

Structural Integrity Associates Report#: JAF-17-RHR-130-WOL File Name 28 AX 52mm 45-60-70.ops Menu Item Essential Instrument Settine File File Fonnnt Sctun On llnoulS UT Pnramctcrs Into Renart)

Readinl!

Result Selector List I Field I Ao/o lPcak Amnlitudc In Gate A)

Field 2 A" tPosition Of Peak Si,mal In Gate A)

UT General Stort lo (Default)

Ranne 13.00 Sound Vclocitv 10.2283 in/us LOCKED Pulser Pulser I !Per Focal Lawl LOCKED Tx/Rx Mode PE IPer Focal Law) LOCKED Volllll!e Hi*h PW Auto PRF Ontimum

~

I IPcr Focal Law) LOCKED None r

FW Video Filter OIT Avenu?.ine I

Reicct 0

Beam Gain Offset O.OdB 0

Beam Dcluv 15.30 us Advanced PointsOlv I Auto Sum Gain IAulo tin this oosition the instrument will set the value)

Disnlav Selection Disnlnv A-S-C Proiection On Rulers UT Unit True Denth

%Ruler Lincnrl%)

TCG OIT Gate On Cursor On Color Select Amnlitudc Start I%)

0.0 Endt%\\

100.0 Proocrtics Source Nonna]

Probe/Part Select Select ISclccl TX I RX Auto Detect IOIT PGM Probe Conffoumtion Scan Tvoe IScctorinl Connection P II Laws I

Aulo Procm1m IOIT Gate/Alarm Gale Gate Select IGalcA:

Svnchro I Pulse c

Page ~orJ..Q

~

Structural Integrity Associates Report#: JAF-17-RHR-130-WOL e

ULTRASONIC PHASED ARRAY CAL/BRA TION RECORD Customer: Entergy I

Calibration Sheet:IJAF-17-CAL-048 Plant/Unit: J.A. Fitzpatrick I Unit 1 I Procedure No:ISl-UT-126, Rev. 3 Component/System: 24-10-130 (Overlay) I RHR Valve-to-Tee Weld Overlay Wedt1e Manufacturer:

SI Refracted Anale Verification Model:

100102 Focal Law Measured Index Offset Material:

Rexolite Angle Angle (in)

Velocity:

2330 (mis) so*

so*

0.40 Wedge Angle:

1s.2*

45*

45*

0.45 Scan Direction:

Axial 30° 30" 0.54 Wedge Nominal OD:

20*

Instrument Search Unit Integral Cable Manufacturer:

Zetec Tvoe: I 34 Conductor I 38 Gauge Coaxial Model:

OmniScan MX Length:

8' Serial Number:

OMNl-100084 Connectors:

1-Pex Phased Array Module:

OMNl-M-PA32 / 128PR Intermediate Cable PA Module Serial No.:

OMNl-6212 Type:

N/A Software Revision:

1.4R3 Length:

N/A Instrument Settings:

See Next Page Connectors:

N/A Search Unit Manufacturer:

GEIT Element Lent1th:

2.70mm 0

Transmit Model:

115-000-613 Element Width:

1.15mm Transmit Serial Number:

01VW13 Elements (Primary Axis):

16 Receive Model:

115-000-613 Elements (Secondary Axis):

2 Receive Serial Number:

01VW13 Inactive Element - Transmit:

0 Freauencv IMHzl:

2.0 Inactive Element - Receive:

0 Calibration Data Files Focal Law: RHR_28A_2MTRL2x16 0-85_N 20mmHP.law Angles Generated: o* through 85" (1° Increments)

Wave Mode:

Longitudinal Set-up File: 28_AX_20mm_0-80.ops Focal Sound Path:

20mm Couplant I Batch Ultragel II / 12325A Calibration Block(s):

Sl-24-AX-01 Calibration Reflector Data Comments:

Calibration Reference

%FSH Ref. Gain Wedge Delay Active element checks performed at initial Reflector Angle and final cal checks.

0.1* Deep SDH 80° 80%

40dB 1.1 µs Intermediate Check: 2111/17 -1525, 2005 1.2* Deep SDH 0'

80%

45dB 0.9 us Reference Block No.: Sl-14-AX-01 Temperature: 80"F SIN: 271398 Calibration Performed Level Date-Time Initial:

Wade Holloway III 2111/17-0950 Final:

Wade Holloway III 2111/17-2224 SI Reviewed:

N/A 2113/17 c

Client Review:

III z.j-.>/z.,, 7 ANll Review:

N/A z /.1

lJ Structural Integrity Associates Report#: JAF-17-RHR-130-WOL e

File Name 28 AX 20mm 0-80.oos Menu Item I

Essential Instrument Settin~

File File Fonnal SclUD IOn '1nnuts UT Parameters Into Rcnnrt\\

Readin2 Result Selector ILiot I Field I IA% IPcak Amnlitudc In Gate A)

Field 2 IA" lPosition OrPcnk Sil!llal In Gate A)

UT General St wt O <Default)

Rane.c 0.603 Sound Velocitv 0.2283 in/us LOCKED Pulser Pulser 1 IPcr Focal Law) LOCKED Tx/Rx Mode PE IPcr Focal Law) LOCKED Voltas?.e Hi!!h rw Auto PRF On ti mum Receiver Receiver I <Per Focal Law) LOCKED Filter None Rectifier FW Video Filter Off Avc~i n ~

I Rcicct 0

Beam Gain Offset O.OdB 0

Beam Dclav 17.81 us Advanced Points Olv Auto Sum Gain Auto 'In this nosition the instrument wilt set the vaJucl Display Selection Disnlav A-S-C Proicction On Rulers UT Unit True Dcnth

% Ruler Linear lo/o)

TCG Off Gate On Cursor On Color Select IAmnlitudc Stnrt(%)

10.0 Endt%\\

1100.0 Properties Source I Normal Probe/Part Select Select

!Select TX I RX Auto Detect I Off PGM Probe Confi1?.uration Scan T~

ISectoriaJ Connection P II Laws I

Auto J>ron.... m I Off Gate/Alarm 0

Gale Gate Select Gate A:

Svnchro Pulse Page _fl of _j_Q

lJ Structural Integrity Associates Report#: JAF-17-RHR-130-WOL e

ULTRASONIC PHASED ARRAY CAL/BRA TION RECORD Customer: Entergy I

Calibration Sheet:IJAF-17-CAL-049 Plant/Unit: J.A. Fitzpatrick I Unit 1 I Procedure No:ISl-UT-126, Rev. 3 Component/System: 24-10-130 (Overlay) I RHR Valve-to-Tee Weld Overlay Wedge Manufacturer:

SI Refracted An11le Verification Model:

100102 Focal Law Measured Index Offset Material:

Rexolite Angle Angle (in)

Velocitv:

2330 (mis) 55*

55*

0.38 Wed!le An!lle:

16.2° 45*

45*

0.50 Scan Direction:

Circumferential 30" 30° 0.60 Wedae Nominal OD:

28" Instrument Search Unit lntearal Cable Manufacturer:

Zetec Type: I 34 Conductor I 38 Gauge Coaxial Model:

OmniScanMX Lenath:

8' Serial Number:

OMNl-100084 Connectors:

1-Pex Phased Array Module:

OMNl-M-PA32 / 128PR Intermediate Cable PA Module Serial No.:

OMNl-6212 TYoe:

N/A Software Revision:

1.4R3 Length:

N/A Instrument Settinas:

See Next Page Connectors:

N/A Search Unit Manufacturer:

GEIT Element Length:

2.70mm 0

Transmit Model:

115-000-613 Element Width:

1.15mm Transmit Serial Number:

01VW13 Elements (Primary Axis):

16 Receive Model:

115-000-613 Elements (Secondary Axis):

2 Receive Serial Number:

01VW13 Inactive Element - Transmit:

0 Frequency (MHz):

2.0 Inactive Element - Receive:

0 Calibration Data Files Focal Law: RHR 28C 2MTRL2x16 0-75 N 38mmHP.law An11les Generated: o* throuah 75" (1° Increments)

Wave Mode:

Longitudinal Set-uo File: 28_CIRC 1_38mm.ops Focal Sound Path:

38mm Couolant I Batch Ultragel II/ 12325A Calibration Blocklsl:

Sl-24-AX-01 Calibration Reflector Data Comments:

Calibration Reference

%FSH Ref.Gain Wedge Delay Active element checks performed at initial Reflector Angle and final cal checks.

0.6" Deep SDH 51° 80%

39dB 3.1 µs Intermediate Check: 2111/17 -2105, 2146 1.0" Deep SDH 49° 80%

40dB 3.3 us Reference Block No.: Sl-14-CIRC-01 1.3" Deep SDH 47° 80%

41 dB 3.7us Temperature: BO"F S/N: 271398 Calibration Performed Level Date-Time Initial:

Wade Holloway m

2111/17 -1030 Final:

III 2111/17-2213 SI Reviewed:

N/A 2113/17 c

Client Review:

III z:/;J--;;{-~17 ANllReview:

N/A

~ '

fJ Structural Integrity Associates Report #: JAF-17-RHR-130-WOL e

File Name 28 CIRC 1 38mm.oos Menu Item Essential Instrument Sellin~

File Filo Fonnnl Sctun On flnnuts lff Poramcrcrs Jnro Rcnnn1 Read In I!

Result Sclcclor List I Field I A%7Pcak Amplirudc In Gate A)

Ficld2 A" tPosition Of Peak Sit!llnl In Gate Al UT General Stnrt To7Dcfuultl Rant!C 12.710 Sound Velocitv 10.2283 in/ns LOCKED Pulser Pulser I IPor Focal Lawl LOCKED Tx/Rx Mode PE iPcr Focal Lawl LOCKED Vol'"tu>

Hi*h PW Auto PRF 10ntimum Receiver Receiver I tPcr Focul Law) LOCKED Filler None Rectifier FW Video Filter Off AvcnH!inu.

I Rcicct 0

Bcum Gain Offset O.OdB 0

Benm Dclav 14.68 "'

Advanced PointsOtv IAulo Sum Gain lAuto lln this pasition the instrument will set the valucl Dlsolav Selection Disnlav A-S.C Protection On Rulers UTUnil True Denlh

'Y. Rulcr Linear 1*1.T TCG Off Gate On Cursor On Color Select Amnlitudc Startt%)

0.0 Endt%l 100.0 Proocrtics Source Nonntll Probe/Part Sckc:t Select SclcclTX i RX Auto Detect

  • 1off PGM Probe Confinuro.tion Scan Tvnc ISectorioJ Connection P 11 Laws I

AutoP~--

Off Gate/Alarm Gale Gate Select IGnlcA:

Svnchro

-I Pulse Page J!2 of _!S)

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