L-2013-257, Inservice Inspection Plan, Second RAI Reply to Fourth Ten-Year Interval Unit 1 Relief Request No. 5, Revision 0
| ML13235A309 | |
| Person / Time | |
|---|---|
| Site: | Saint Lucie |
| Issue date: | 08/22/2013 |
| From: | Katzman E Florida Power & Light Co |
| To: | Document Control Desk, Office of Nuclear Reactor Regulation |
| References | |
| L-2013-257 | |
| Download: ML13235A309 (21) | |
Text
0 August 22, 2013 FPL.
L-2013-257 10 CFR 50.4 10 CFR 50.55a U. S. Nuclear Regulatory Commission Attn: Document Control Desk Washington, DC 20555 Re:
St. Lucie Unit I Docket No. 50-335 Inservice Inspection Plan Second RAI Reply to Fourth Ten-Year Interval Unit 1 Relief Request No. 5, Revision 0
References:
- 1. FPL Letter L-2013-044 dated February 4, 2013, "Inservice Inspection Plan Fourth Ten-Year Interval Unit I Relief Request No. 5, Revision 0," ML Accession No. ML13046A101.
- 2. NRC email from Siva Lingam to Ken Frehafer dated May 29, 2013, "Request for Additional Information for Relief Request No. 5, "Examination of Cold Leg Dissimilar Metal Welds," at St. Lucie Unit 1 (TAC NO. MF-0675).
- 3. FPL Letter L-2013-232 dated July 30, 2013, "RAI Reply to Fourth Ten-Year Interval Unit 1 Relief Request No. 5, Revision 0," Accession No. ML13219A254.
- 4. NRC email from Siva Lingam to Ken Frehafer dated August 9, 2013St. Lucie, Unit I Relief Request No. 5 - 2nd Round of Requests for Additional Information (RAIs) (TAC No. MF0675), Accession No. ML13221A205.
In Reference 1 above, Florida Power & Light (FPL),
requested relief from the 10CFR50.55a(g)(6)(ii)(F)(4) exception to ASME Code Case N-770-1 that essentially 100%
coverage be achieved for the baseline required volumetric examinations. In Reference 2 above, the NRC submitted a request for additional information (RAI) on the relief request. FPL replied to that RAI via Reference 3. The NRC developed an additional RAI via Reference 4. The reply to this RAI is provided in the attachment to this letter.
Please contact Ken Frehafer at (772) 467-7748 if there are any questions about this submittal.
Sincerely, Eric S. Katzman Licensing Manager St. Lucie Plant Attachment ESK/KWF A047 Florida Power & Light Company n
6501 S. Ocean Drive, Jensen Beach, FL 34957
L-2013-257 Attachment Page 1 of 20 Response to Second Round of NRC Request For Additional Information (RAI) for St. Lucie Unit 1-Fourth Ten-Year Interval (ML13221A205), Relief Request No. 5 Revision 0.
By letter dated February 4, 2013 (Agencywide Documents and Access Management System (ADAMS) Accession No. ML13046A101) with supplement dated July 30, 2013, Florida Power & Light Company (the licensee) requested relief from Title 10, Code of Federal Regulations, Part 50 (10 CFR 50), paragraph 10 CFR 50.55a(g)(6)(ii)(F)(3) and 10 CFR 50.55a(g)(6)(ii)(F)(4) which impose a condition on American Society of Mechanical Engineers (ASME) Code Case N-770-1 requiring essentially 100 percent coverage be achieved for the baseline volumetric examinations of dissimilar metal welds (DMW). The licensee proposed an alternative to the required examination coverage for the eight DMWs at reactor coolant pump (RCP) nozzles at St Lucie Unit I as documented in Relief Request Number 5, Revision 0. To complete its review, the Nuclear Regulatory Commission (NRC) staff requests the following additional information.
NRC RAI-1 In response to RAI-3A (page 5) in the July 30, 2013, submittal, the licensee performed flaw analyses using dissimilar metal weld thickness of 3.2 inches. The licensee stated that this thickness was conservative. However, in response to RAI-3B (page 9), the licensee used a pipe thickness of 2.9 inches. Discuss how the weld thickness was determined (e.g. weld profile taken using zero degree probe, etc.) and why the thickness used is considered to be conservative. Also, are these weld thickness values used in response to RAI 3A and 3B conservative for both welds (RC-121-6-504 or RC-124-7-504)?
Response to RAI-1 The "DMW weld thickness" for RC-121-6-504 or RC-124-7-504 were measured or "as built" as 3.2" - 3.25" for the two DM welds using a zero degree UT probe.
Therefore, using 3.2" as the thickness for flaw growth by PWSCC in the response to RAI-3A (page 5) is conservative. The response to RAI-3B (Page 9) indicated that the "pipe thickness" of 2.9" was used to scale the OD measured length of the missed coverage to an ID length since the UT scanning for axial flaws was primarily on the pipe. Note that the DM weld is thicker than the pipe because the weld transitions to a thicker stainless steel safe end section. The smaller thickness of the pipe was used since the scaling of missed coverage would result in a longer ID missed coverage length. Scaling 3.2" DM weld thickness yields 7.296" missed coverage length, shorter than the 7.416" missed coverage length calculated using the 2.9" pipe thickness. Therefore, it is conservative to use the 2.9" pipe thickness for the missed coverage length calculation.
L-2013-257 Attachment Page 2 of 20 NRC RAI-2 (a) Discuss whether the crack face pressure is included in the flaw growth calculation. If not, provide justification. (b) Provide axial stresses and bending stresses that were used to calculate the growth of the circumferential flaw.
Response to RAI-2 (a)
The flaw growth evaluation assumed 2.5ksi as the crack face pressure.
Response to RAI-2 (b)
The PWSCC flaw evaluation used the St. Lucie Plant bounding axial membrane and bending stresses taken from WCAP-16925-P, Table 3-6 (ADAMS ML092740085). The through wall axial bending stresses are calculated using the maximum bending stress at OD (2.052 ksi) and the ID and OD of the DM weld.
The axial bending and membrane stresses are listed in the table below.
Normalized Axial through-wall Axial Benin membrane Ratio (a/t)
Stress (ksi)
Stress ksi 0.00 1.691 0.286 0.05 1.709 0.286 0.10 1.727 0.286 0.15 1.745 0.286 0.20 1.763 0.286 0.25 1.781 0.286 0.30 1.799 0.286 0.35 1.817 0.286 0.40 1.836 0.286 0.45 1.854 0.286 0.50 1.872 0.286 0.55 1.890 0.286 0.60 1.908 0.286 0.65 1.926 0.286 0.70 1.944 0.286 0.75 1.962 0.286 0.80 1.980 0.286 0.85 1.998 0.286 0.90 2.016 0.286 0.95 2.034 0.286 1.00 2.052 0.286
L-2013-257 Attachment Page 3 of 20 NRC RAI-3 Explain why the weld residual stresses used to calculate the growth of the axial flaw and circumferential flaws did not use the same assumptions for the depth of the internal repair and heat treatment? Specifically, the axial flaw growth calculation used weld residual stresses based on the "50% ID repair with no heat treatment", whereas the circumferential flaw growth calculation used weld residual stresses based on the "25% ID repair with heat treatment".
Response to RAI-3 The axial and circumferential flaw evaluations used the same weld residual stress (WRS) cases, including the "25% ID repair with heat treat" and "50% ID repair with no heat treatment". Although all cases were evaluated for both the axial and circumferential flaw evaluations, only the limiting cases are presented for the RAI response, i.e., 50% repair with no heat treatment case for axial flaw, 25% repair with heat treat for circumferential flaw. Hoop WRS for the axial flaws are all tensile, and heat treatment relaxes the tensile stress. Therefore, 50% ID repair with no heat treatment case is limiting. The axial WRS through-wall profiles for circumferential flaws are either slightly compressive or tensile at the ID. Heat treatment relieves the beneficial compressive stress at the ID, therefore, it is the more limiting case.
L-2013-257 Attachment Page 4 of 20 NRC RAI-4 In RAI-5 A, the licensee was asked for the "as-built" weld geometry. This information is necessary to accurately determine volumetric coverage and beam intensities in the model. The licensee responded by stating that the sketches (included in the initial submittal) are scaled, and that further dimensional information is located in response to question RAI-4 D. However, in the response to RAI-4 D, the information in the table provided by the licensee describes "minimum design thickness," thus it is unclear whether the actual as-built thickness is the value stated in this table. Please clarify and provide the actual (as-built) thicknesses and other as-built geometrical information (such as inside and outside diameter taper and pipe cross sectional dimensions).
Response to RAI-4 The scaled as-built geometry is reflected in the drawings from one circumferential location for each item (the "b" sketch for each configuration). The inside diameter is identified in the both the original submittal and the 1st RAI response (30" ID). The outside circumference that was measured with a tape measure is identified in the table below.
RCP Inlet/Outlet Measured Circumference 1A1 Suction 114.25 1A2 Suction 114.5 11B1 Suction 114.38 1B2 Suction 113.5 1A1 Outlet 113.0 1A2 Outlet 113.0 1B1 Outlet 112.75 1 B2 Outlet 112.5 NRC RAI-5 In RAI-5 B(1), the licensee states that three (3) elements from each probe were tested per ASTM E-1065 for frequency, bandwidth, and pulse duration for the GEIT 115-000-545, 2 x 16 element matrix array probes. Further, the licensee states that center frequencies of 1.59 to 1.65 MHz were found during these tests. The manufacturers design center frequency for this probe is 1.5 MHz.
Please explicitly state the pulse excitation type and duration used during the examinations of Welds RC-121-6-504 and RC-124-7-504.
Response to RAI-5 The pulse excitation type was square wave. The pulse duration was 330 ns.
L-2013-257 Attachment Page 5 of 20 NRC RAI-6 In RAI-5 B(2), the licensee states that both longitudinal and shear wave modes of sound propagation were used during the examinations. When using phased array techniques, in order to properly set the nominal angles for each of these modes of examination, it is standard to apply two different sets of wedges, one set for longitudinal and one for shear wave modes. However, two sets of wedges (along with their dimensions) have not been included in the response. Please clarify which mode (longitudinal or shear) of propagation was being used for the one set of wedges described in the RAI response. Further, clarify and state if the same wedges were being used for the second mode of propagation, or if a second set of wedges was applied. If a second set of wedges was used, please provide dimensional information (similar to that originally requested) for the second set of wedges.
Response to RAI-6 Only one wedge was used for both the longitudinal and shear wave propagation consistent with the qualified procedure. Only one wedge was used in the examination.
NRC RAI-7 In RAI-5 D(3), the licensee was asked for transmit and receive delay values for each of the elements in the phased array probe in order for PNNL to simulate proper beam formation in the component. The licensee responded:
"Not available. These examinations were performed using the WesDyne Intraphase instrument. The Intraphase has an internal proprietary focal law generator based on the essential input parameters defined in the qualified EPRI-DMW-PA-I procedure."
The time delays for element firing are controlled by software and must be validated to ensure the beams are steered and focused correctly. These values are necessary for PNNL to complete the simulation of the examinations using CIVA. The licensee should submit the delay law values as requested. If these are considered WesDyne proprietary, PNNL will treat them as such, and not release this information to any outside party.
Response to RAI-7 The spreadsheets below provide the focal law delays for the longitudinal and shear search units. The transducer is 16 x 2 design, so there are 16 transmitter elements and 16 receive. A '-1" value means the channel is disabled for that function and the "0" value is the reference element for each of the transmit and receive elements. All values (except -1 for "off") are in nanoseconds.
L-2013-257 Aftachment L Wave Focal Law Delays Page 6 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 25L 26L 27L 28L 29L PIR Channel Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay 0
2735.78186
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L-2013-257 Aftachment L Wave Focal Law Delays Page 7 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 30L 31L 32L 33L 34L 3r Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay 2339.93274
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L-2013-257 Aftachment L Wave Focal Law Delays Page 8 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans
_L 36L 37L 38L 39L 40L Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay
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L-2013-257 Aftachment L Wave Focal Law Delays Page 9 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 41L 42L 43L 44L 45L 4E Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay 1522.75143
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L-2013-257 Aftachment L Wave Focal Law Delays Page 10 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans iL 47L 48L 49L SOL 51L Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay
-1 1118.12913
-1 1054.07444
-1 991.056895
-1 929.103015
-1 868.239087
-1
-1 1071.88298
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-1 913.344924
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-1 853.295993
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-1 721.215208
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-1 310.838067
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L-2013-257 Aftachment L Wave Focal Law Delays Page 11 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 52L 53L 54L 55L 56L 5
Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay 808.491361
-1 749.885987
-1 692.449005
-1 636.206329
-1 581.183737
-1 527.406854 778.057267
-1 722.392862
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L-2013-257 Attachment L Wave Focal Law Delays Page 12 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans FL 58L 59L 60L 61L 62L Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay
-1 474.901138
-1 423.691858
-1 373.80408
-1 325.262643
-1 278.092136
-1
-1 460.983286
-1 412.260745
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-1
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-11 427.381066
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L-2013-257 Aftachment L Wave Focal Law Delays Page 13 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 63L 64L 65L 66L 67L V_
Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay 232.316875
-1 187.960879
-1 145.047835
-1 103.601074
-1 63.643434
-1 25.197624 230.06199
-1 187.806163
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-1
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L-2013-257 Attachment L Wave Focal Law Delays Page 14 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 3L 69L 70L Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay
-1 0
-1 0
-1
-1 9.172938
-1 10.802721
-1
-1 17.498165
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-1
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-1 0
32.662007
-1 9.172938
-1 10.802721 39.199099
-1 17.498165
-1 20.834096 44.743843
-1 24.915752
-1 30.039196 49.225344
-1 31.360314
-1 38.358028 52.566259
-1 36.760427
-1 45.724974 54.682112
-1 41.037973
-1 52.06817 55.480542
-1 44.107405
-1 57.3088 54.860459
-1 45.874934
-1 61.360314 52.711115
-1 46.237617
-1 64.127544 48.911074
-1 45.082349
-1 65.505716 43.327081
-1 42.28473
-1 65.379349 35.812818
-1 37.707829
-1 63.621019 26.207549
-1 31.200811
-1 60.089991 14.334643
-1 22.597433
-1 54.630705 0
-1 11.714402
-1 47.071097
L-2013-257 Aftachment S Wave Focal Law Delays Page 15 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 35S 36S 37S 38S 39S PIR Channel Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay 0
0
-1 0
-1 0
-1 0
-1 0
-1 1 118.610054
-1 126.962049
-1 135.197277
-1 143.31348
-1 151.308436
-1 2
227.250589
-1 244.184959
-1 260.889197
-1 277.358508
-1 293.588165
-1 3
325.570065
-1 351.312585
-1 376.715742
-1 401.771926
-1 426.473627
-1 4 413.219452
-1 447.989952
-1 482.31673
-1 516.189095
-1 549.59657
-1 5
489.854406
-1 533.86541
-1 577.333949
-1 620.245987
-1 662.587627
-1 6
555.136712
-1 608.592045
-1 661.412504
-1 713.580473
-1 765.078475
-1 7
608.736598
-1 671.829999
-1 734.203156
-1 795.83465
-1 856.7032
-1 8
650.33466.
-1 723.248419
-1 795.364266
-1 866.656789
-1 937.100693
-1 9
679.623782
-1 762.527414
-1 844.563783
-1 925.703321
-1 1005.91655
-1 10 696.311443
-1 789.360435
-1 881.48169
-1 972.641356
-1 1062.80564
-1 11 700.121115
-1 803.455735
-1 905.811504
-1 1007.1502
-1 1107.43361
-1 12 690.794442
-1 804.538659
-1 917.26268
-1 1028.92388
-1 1139.47955
-1 13 668.092774
-1 792.353291
-1 915.562357
-1 1037.67293
-1 1158.63783
-1 14 631.799028
-1 766.664474
-1 900.457527
-1 1033.12679
-1 1164.62061
-1 15 581.718613
-1 727.258837
-1 871.716171
-1 1015.03494
-1 1157.15913
-1 16
-1 0
-1 0
-1 0
-1 0
-1 0
17
-1 118.610054
-1 126.962049
-1 135.197277
-1 143.31348
-1 151.308436 18
-1 227.250589
-1 244.184959
-1 260.889197
-1 277.358508
-1 293.588165 19
-1 325.570065
-1 351.312585
-1 376.715742
-1 401.771926
-1 426.473627 20
-1 413.219452
-1 447.989952
-1 482.31673
-1 516.189095
-1 549.59657 21
-1 489.854406
-1 533.86541
-1 577.333949
-1 620.245987
-1 662.587627 22
-1 555.136712
-1 608.592045
-1 661.412504
-1 713.580473
-1 765.078475 23
-1 608.736598
-1 671.829999
-1 734.203156
-1 795.83465
-1 856.7032 24
-1 650.33466
-1 723.248419
-1 795.364266
-1 866.656789
-1 937.100693 25
-1 679.623782
-1 762.527414
-1 844.563783
-1 925.703321
-1 1005.91655 26
-1 696.311443
-1 789.360435
-1 881.48169
-1 972.641356
-1 1062.80564 27
-1 700.121115
-1 803.455735
-1 905.811504
-1 1007.1502
-1 1107.43361 28
-1 690.794442
-1 804.538659
-1 917.26268
-1 1028.92388
-1 1139.47955 29
-11 668.092774
-1 792.353291
-1 915.562357
-1 1037.67293
-1 1158.63783 30
-11 631.799028
-1 766.664474
-1 900.457527
-1 1033.12679
-1 1164.62061 31
-1 581.718613
-11 727.258837
-1 871.716171
-1 1015.03494
-1 1157.15913
L-2013-257 Aftachment S Wave Focal Law Delays Page 16 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Ciro Scans 40S 41S 42S 43S 44S 4_r Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay 0
-1 0
-1 0
-1 0
-1 0
-1 0
159.179956
-1 166.92589
-1 174.544123
-1 182.032577
-1 189.389213
-1 196.612032 309.573508
-1 325.30995
-1 340.792969
-1 356.01812
-1 370.981028
-1 385.677397 450.813427
-1 474.78401
-1 498.37816
-1 521.58876
-1 544.408803
-1 566.831388 582.528514
-1 614.974687
-1 646.924881
-1 678.369015
-1 709.297141
-1 739.699445 704.345104
-1 745.50479
-1 786.053201
-1 825.976996
-1 865.262986
-1 903.898253 815.889178
-1 865.995391
-1 915.380077
-1 964.026349
-1 1011.91748
-1 1059.03693 916.787662
-1 976.067036
-1 1034.52047
-1 1092.12726
-1 1148.86688
-1 1204.71894 1006.67081
-1 1075.34211
-1 1143.08968
-1 1209.88876
-1 1275.71473
-1 1340.54314 1085.1741
-1 1163.44668
-1 1240.70515
-1 1316.92056
-1 1392.06376
-1 1466.10607 1151.94079
-1 1240.01315
-1 1326.98911
-1 1412.83514
-1 1497.5178
-1 1581.00375 1206.62352
-1 1304.68174
-1 1401.57007
-1 1497.25036
-1 1591.68449
-1 1684.83438 1248.88695
-1 1357.10326
-1 1464.08562
-1 1569.79114
-1 1674.17688
-1 1777.19987 1278.40973
-1 1396.94117
-1 1514.18456
-1 1630.09218
-1 1744.61633
-1 1857.70884 1294.88713
-1 1423.87423
-1 1551.5296
-1 1677.80069
-1 1802.63474
-1 1925.97877 1298.0324
-1 1437.59804
-1 1575.79904
-1 1712.57805
-1 1847.87741
-1 1981.6391
-1 0
-1 0
-1 0
-1 0
-1 0
-1
-1 159.179956
-1 166.92589
-1 174.544123
-1 182.032577
-1 189.389213
-1
-1 309.573508
-1 325.30995
-1 340.792969
-1 356.01812
-1 370.981028
-1
-1 450.813427
-1 474.78401
-11 498.37816
-1 521.58876
-1 544.408803
-1
-1 582.528514
-1 614.974687
-1 646.924881
-1 678.369015
-1 709.297141
-1
-1 704.345104
-1 745.50479
-1 786.053201
-1 825.976996
-1 865.262986
-1
-1 815.889178
-1 865.995391
-1 915.380077
-1 964.026349
-1 1011.91748
-1
-1 916.787662
-1 976.067036
-1 1034.52047
-1 1092.12726
-1 1148.86688
-1
-1 1006.67081
-1 1075.34211
-1 1143.08968
-1 1209.88876
-1 1275.71473
-1
-1 1085.1741
-1 1163.44668
-1 1240.70515
-1 1316.92056
-1 1392.06376
-1
-1 1151.94079
-1 1240.01315
-1 1326.98911
-1 1412.83514
-1 1497.5178
-1
-1 1206.62352
-1 1304.68174
-1 1401.57007
-1 1497.25036
-1 1591.68449
-1
-1 1248.88695
-1 1357.10326
-1 1464.08562
-1 1569.79114
-1 1674.17688
-1
-1 1278.40973
-1 1396.94117
-1 1514.18456
-1 1630.09218
-1 1744.61633
-1
-1 1294.88713
-1 1423.87423
-11 1551.5296
-1 1677.80069
-1 1802.634741
-1
-1 1298.0324
-1 1437.59804
-1 1575.79904
-1 1712.57805
-1 1847.87741
-1
L-2013-257 Aftachment S Wave Focal Law Delays Page 17 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans is 46S 47S 48S 49S 50S Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay
-1 0
-1 0
-1 0
-1 0
-1 0
-1
-1 203.699074
-1 210.648422
-1 217.458115
-1 224.126497
-1 230.651704
-1
-1 400.103008
-1 414.253724
-1 428.125404
-1 441.71426
-1 455.016335
-1
-1 588.849728
-1 610.457151
-1 631.647022
-1 652.413093
-1 672.748993
-1
-1 769.566257
-1 798.888051
-1 827.655368
-1 855.859171
-1 883.490336
-1
-1 941.869696
-1 979.164726
-1 1015.77073
-1 1051.67554
-1 1086.86694
-1
-1 1105.36829
-1 1150.89537
-1 1195.60208
-1 1239.47279
-1 1282.49182
-1
-1 1259.66326
-1 1313.67982
-1 1366.74873
-1 1418.85056
-1 1469.96584
-1
-1 1404.34971
-1 1467.1103
-1 1528.80091
-1 1589.398
-1 1648.87797
-1
-1 1539.01885
-1 1610.77359
-1 1681.34188
-1 1750.69576
-1 1818.80718
-1
-1 1663.25975
-1 1744.25267
-1 1823.94944
-1 1902.31753
-1 1979.32388
-1
-1 1776.66199
-1 1867.12937
-1 1956.19853
-1 2043.83186
-1 2129.99158
-1
-1 1878.81714
-1 1978.98571
-1 2077.66252
-1 2174.80479
-1 2270.36952
-1
-1 1969.32177
-1 2079.407
-1 2187.91624
-1 2294.8014
-1 2400.01406
-1
-1 2047.77963
-1 2167.98397
-1 2286.53816
-1 2403.38868
-1 2518.48158
-1
-1 2113.80485
-1 2244.31602
-1 2373.11365
-1 2500.1387
-1 2625.33163
-1 0
-1 0
-1 0
-1 0
-1 0
-1 0
196.612032
-1 203.699074
-1 210.648422
-1 217.458115
-1 224.126497
-1 230.651704 385.677397
-1 400.103008
-1 414.253724
-1 428.125404
-1 441.71426
-1 455.016335 566.831388
-1 588.849728
-1 610.457151
-1 631.647022
-1 652.413093
-1 672.748993 739.699445
-1 769.566257
-1 798.888051
-1 827.655368
-1 855.859171
-1 883.490336 903.898253
-1 941.869696
-1 979.164726
-1 1015.77073
-1 1051.67554
-1 1086.86694 1059.03693
-1 1105.36829
-1 1150.89537
-1 1195.60208
-1 1239.47279
-1 1282.49182 1204.71894
-1 1259.66326
-1 1313.67982
-1 1366.74873
-1 1418.85056
-1 1469.96584 1340.54314
-1 1404.34971
-1 1467.1103
-1 1528.80091
-1 1589.398
-1 1648.87797 1466.10607
-1 1539.01885
-1 1610.77359
-1 1681.34188
-1 1750.69576
-1 1818.80718 1581.00375
-1 1663.25975
-1 1744.25267
-1 1823.94944
-1 1902.31753
-1 1979.32388 1684.83438
-1 1776.66199
-1 1867.12937
-1 1956.19853
-1 2043.83186
-1 2129.99158 1777.19987
-1 1878.81714
-1 1978.98571
-1 2077.66252
-1 2174.80479
-1 2270.36952 1857.70884
-1 1969.32177
-1 2079.407
-1 2187.91624
-1 2294.8014
-1 2400.01406 1925.97877
-1 2047.77963
-1 2167.98397
-1 2286.53816
-1 2403.38868
-1 2518.48158 1981.6391
-1 2113.80485
-1 2244.31602
-1 2373.11365
-1 2500.1387
-1 2625.33163
L-2013-257 Aftachment S Wave Focal Law Delays Page 18 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 51S 52S 53S 54S 55S 5(
Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay 0
-1 0
-1 0
-1 0
-1 0
-1 0
237.032002
-1 243.265714
-1 249.351319
-1 255.287041
-1 261.071474
-1 266.70317 468.027854
-1 480.745145
-1 493.164643
-1 505.282894
-1 517.096561
-1 528.602431 692.648575
-1 712.105841
-1 731.114948
-1 749.670217
-1 767.766141
-1 785.397394 910.54
-1 936.99949
-1 962.860332
-1 988.11426
-1 1012.75323
-1 1036.76944 1121.333
-1 1155.062
-1 1188.04247
-1 1220.26318
-1 1251.71318
-1 1282.38178 1324.64397
-1 1365.91383
-1 1406.2867
-1 1445.748
-1 1484.28345
-1 1521.87908 1520.07544
-1 1569.16046
-1 1617.20231
-1 1664.18267
-1 1710.08368
-1 1754.88738 1707.21755
-1 1764.39372
-1 1820.38375
-1 1875.16517
-1 1928.71587
-1 1981.01405 1885.64841
-1 1951.19196
-1 2015.41058
-1 2078.27731
-1 2139.76548
-1 2199.84877 2054.93612
-1 2129.12194
-1 2201.84927
-1 2273.08625
-1 2342.80131
-1 2410.96318 2214.64013
-1 2297.74011
-1 2379.25425
-1 2459.14568
-1 2537.3772
-1 2613.91239 2364.31386
-1 2456.59502
-1 2547.17031
-1 2635.99715
-1 2723.03309
-1 2808.23586 2503.50589
-1 2605.2285
-1 2705.13351
-1 2803.17258
-1 2899.29737
-1 2993.45961 2631.76304
-1 2743.17859
-1 2852.67416
-1 2960.19539
-1 3065.68784
-1 3169.09702 2748.63268
-1 2869.98188
-1 2989.31895
-1 3106.58343
-1 3221.71458
-1 3334.65148
-1 0
-1 0
-1 0
-1 0
-1 0
-1
-1 237.032002
-1 243.265714
-1 249.351319
-1 255.287041
-1 261.071474
-1
-1 468.027854
-1 480.745145
-1 493.164643
-1 505.282894
-1 517.096561
-1
-1 692.648575
-1 712.105841
-1 731.114948
-1 749.670217
-1 767.766141
-1
-1 910.54
-1 936.99949
-1 962.860332
-1 988.11426
-1 1012.75323
-1
-1 1121.333
-1 1155.062
-1 1188.04247
-1 1220.26318
-1 1251.71318
-1
-1 1324.64397
-1 1365.91383
-1 1406.2867
-1 1445.748
-1 1484.28345
-1
-1 1520.07544
-1 1569.16046
-1 1617.20231
-1 1664.18267
-1 1710.08368
-1
-1 1707.21755
-1 1764.39372
-1 1820.38375
-1 1875.16517
-1 1928.71587
-1
-1 1885.64841
-1 1951.19196
-11 2015.41058
-1 2078.27731
-1 2139.76548
-1
-1 2054.93612
-1 2129.12194
-1 2201.84927
-1 2273.08625
-1 2342.80131
-1
-1 2214.64013
-1 2297.74011
-1 2379.25425
-1 2459.14568
-1 2537.3772
-1
-1 2364.31386
-1 2456.59502
-1 2547.17031
-1 2635.99715
-1 2723.03309
-1
-1 2503.50589
-1 2605.2285
-1 2705.13351
-1 2803.17258
-1 2899.29737
-1
-1 2631.76304
-1 2743.17859
-1 2852.67416
-1 2960.19539
-1 3065.68784
-1
-1 2748.63268
-1 2869.98188
-1 2989.31895
-1 3106.58343
-1 3221.71458
-1
L-2013-257 Aftachment S Wave Focal Law Delays Page 19 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans
_S 57S 58S 59S 60S 61S Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay
-1 0
-1 0
-1 0
-1 0
-1 0
-1
-1 272.180747
-1 277.502891
-1 282.668355
-1 287.675968
-1 292.524633
-1
-1 539.797539
-1 550.678699
-1 561.243219
-1 571.488434
-1 581.411832
-1
-1 802.558842
-1 819.245548
-1 835.452784
-1 851.176043
-1 866.41118
-1
-1 1060.15532
-1 1082.90358
-1 1105.00717
-1 1126.45937
-1 1147.25372
-1
-1 1312.25859
-1 1341.33354
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-1 1397.0392
-1 1423.6515
-1
-1 1558.52126
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-1 1662.59625
-1 1695.29574
-1
-1 1798.5766
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-1 1882.54433
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-1 1961.85655
-1
-1 2032.03828
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-1
-1 2258.5012
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-1 2371.41154
-1 2425.61957
-1 2478.29701
-1
-1 2477.5409
-1 2542.50387
-1 2605.82189
-1 2667.46516
-1 2727.40434
-1
-1 2688.7149
-1 2761.74869
-1 2832.97805
-1 2902.36765
-1 2969.88251
-1
-1 2891.56335
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-1 3052.42545
-1 3129.87685
-1 3205.28703
-1
-1 3085.61114
-1 3175.70384
-1 3263.68978
-1 3349.52113
-1 3433.15027
-1
-1 3270.36836
-1 3369.44726
-1 3466.27911
-1 3560.80927
-1 3652.98314
-1
-1 3445.33316
-1 3553.69789
-1 3659.68428
-1 3763.2306
-1 3864.2749
-1 0
-1 0
-1 0
-1 0
-1 0
-1 0
266.70317
-1 272.180747
-1 277.502891
-1 282.668355
-1 287.675968
-1 292.524633 528.602431
-1 539.797539
-1 550.678699
-1 561.243219
-1 571.488434
-1 581.411832 785.397394
-1 802.558842
-1 819.245548
-1 835.452784
-1 851.176043
-1 866.41118 1036.76944
-1 1060.15532
-1 1082.90358
-1 1105.00717
-1 1126.45937
-1 1147.25372 1282.38178
-1 1312.25859
-1 1341.33354
-1 1369.59687
-1 1397.0392
-1 1423.6515 1521.87908
-1 1558.52126
-1 1594.19672
-1 1628.89255
-1 1662.59625
-1 1695.29574 1754.88738
-1 1798.5766
-1 1841.13442
-1 1882.54433
-1 1922.79025
-1 1961.85655 1981.01405
-1 2032.03828
-1 2081.76771
-1 2130.1814
-1 2177.25936
-1 2222.98193 2199.84877
-1 2258.5012
-1 2315.69718
-1 2371.41154
-1 2425.61957
-1 2478.29701 2410.96318
-1 2477.5409
-1 2542.50387
-1 2605.82189
-1 2667.46516
-1 2727.40434 2613.91239
-1 2688.7149
-1 2761.74869
-1 2832.97805
-1 2902.36765
-1 2969.88251 2808.23586
-1 2891.56335
-1 2972.97389
-1 3052.42545
-1 3129.87685
-1 3205.28703 2993.45961
-1 3085.61114
-1 3175.70384
-1 3263.68978
-1 3349.52113
-1 3433.15027 3169.09702
-1 3270.36836
-1 3369.44726
-1 3466.27911
-1 3560.80927
-1 3652.98314 3334.65148
-1 3445.33316
-1 3553.69789
-1 3659.68428
-1 3763.2306
-1 3864.2749
L-2013-257 Attachment S Wave Focal Law Delays Page 20 of 20 Wedge Model: 360-151-057 Delays are the same for Axial and Circ Scans 62S 63S 64S 65S Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay Xmit Delay Rcv Delay 0
-1 0
-1 0
-1 0
-1 297.21333
-1 301.741118
-1 306.107136
-1 310.310607
-1 591.011058
-1 600.283916
-1 609.228376
-1 617.842575
-1 881.153876
-1 895.400461
-1 909.147381
-1 922.391337
-1 1167.38409
-1 1186.84483
-1 1205.63016
-1 1223.73509
-1 1449.42509
-1 1474.35175
-1 1498.42361
-1 1521.63326
-1 1726.97938
-1 1757.63598
-1 1787.25485
-1 1815.8258
-1 1999.7281
-1 2036.39027
-1 2071.829
-1 2106.03076
-1 2267.32995
-1 2310.2848
-1 2351.82847
-1 2391.94351
-1 2529.42035
-1 2578.96603
-1 2626.91166
-1 2673.23527
-1 2785.61059
-1 2842.0556
-1 2896.71182
-1 2949.55171
-1 3035.48813
-1 3099.15046
-1 3160.83596
-1 3220.51163
-1 3278.61526
-1 3349.82119
-1 3418.86487
-1 3485.70679
-1 3514.52998
-1 3593.61262
-1 3670.35145
-1 3744.69983
-1 3742.74611
-1 3830.04364
-1 3914.82124
-1 3997.02472
-1 3962.75503
-1 4058.60868
-1 4151.77332
-1 4242.18622
-1
-1 0
-1 0
-1 0
-1 0
-1 297.21333
-1 301.741118
-1 306.107136
-1 310.310607
-1 591.011058
-1 600.283916
-1 609.228376
-1 617.842575
-1 881.153876
-1 895.400461
-1 909.147381
-1 922.391337
-1 1167.38409
-1 1186.84483
-1 1205.63016
-1 1223.73509
-1 1449.42509
-1 1474.35175
-1 1498.42361
-1 1521.63326
-1 1726.97938
-1 1757.63598
-1 1787.25485
-1 1815.8258
-1 1999.7281
-1 2036.39027
-1 2071.829
-1 2106.03076
-1 2267.32995
-1 2310.2848
-1 2351.82847
-1 2391.94351
-1 2529.42035
-1 2578.96603
-1 2626.91166
-1 2673.23527
-1 2785.61059
-1 2842.0556
-1 2896.71182
-1 2949.55171
-1 3035.48813
-1 3099.15046
-1 3160.83596
-1 3220.51163
-1 3278.61526
-1 3349.82119
-1 3418.86487
-1 3485.70679
-1 3514.52998
-1 3593.61262
-1 3670.35145
-1 3744.69983
-1 3742.74611
-1 3830.04364
-1 3914.82124
-1 3997.02472
-1 3962.75503
-1 4058.60868
-1 4151.77332
-1 4242.18622