$StrwiuralIntegrilyAssociatesSteamGeneratorInlet Nozzle B
UltrasonicExaminationSteam GeneratorB - Inlet NozzleFSWOL . General
Configuraion7.87"5.34"-8.87"NozzleSideReferencePunchMark1.50"SafeEndSideRofefencePunchMarkCode
CaseN-740-2Weld OverlayExamination VolumeA-B-C-DNote: TheInterface
C - DIncludesthe bond andthe heat-affected zonefrom the overlay.The
HAZexterds M20-intothe austenitic weld.S...CodeCaseN-740-2
ISIExaminationVolurneA-B-C-D0Pageof
8ellStrunturalIntegrityAssociatesSteam GeneratorInlet Nozzle B
Uftrasonic ExaminationSteam GeneratorB- Inlet Nozzle FSWOL - Seal
Weld Area Configuration2.76"PagW20VStruduralIntegrity
AssociatesSteam GeneratorInlet Nozzle B
UltrasonicExaminationSteamGeneratorB - Inlet NozzleFSWOL - Seal
Weld Area ConfigurationNozzleSide of DNWeld4.16"6.2rSaft End Side
of DM Weld>t,431118Wto
TDCPa/e30o8VStructuralIntegrityAssociatesSteam GeneratorInlet
NozzleB Ultrasonic ExaminationSteam Generator8 - Inlet
NozzleFSWOLWeld Overlay Axial Acceptance Examination
CoverageAxialWOL Laminar Flaw.0is.Or rExaminaon Coverage100%No
Lambw*lawExam*naonCoverageI
iN'II!\~N~sift-\Omutatb&=0&afA&
1f*VLL4~MkWbftMufu~su~huAWtCam-IFSA?WMUM~fw&biniiu&%b~ftaltCJA?&WPop
4 of$4VStructuralIntegrityAssociatesSteam GeneratorInlet Nozzle B
UltrasonicExaminationSteam GeneratorB - Inlet NozzleFSWOL -
CircumewnalExamination CoverageWeld Overlay Acceptance and PSI /
ISI Examination VolumesCIMUMferentlWVLPlanarFlawExamlnrton
Coverawg.95.9%C~Clwunfe'ntwpel PSI/sExwnlnetonCovmpg.=100%3Wj[~* No
PlanarFlawExaminationCovweWaeNE! Sof
S505O/jVStrucluralIntegrityAssociatesSteam GeneratorInlet NozzleB
UltrasonicExaminationSteam GeneratorB - Inlet Nozzle FSWOLPSI/ISI
Axial Examination Volume Coverage - General
AreaAxialCvrg1I9.ExamintoCoverage.- .7%pap 6 of
a$StructuralIntegrityAssociatesSteam GeneratorInlet Nozzle
BUltrasonicExaminationSteam GeneratorB - Inlet Nozzle FSWOLPSI /IS1
Axial Examination VolumeCoverige- Seal Weld
AreAxIelPS81S/Exomlnaion Coverage -*.6%Page 70f8SructuralIntegrity
AssociatesSteam GeneratorInlet NozzleBUIftisonic ExaminationSteam
GeneratorB.Inlet NozzleFSWOL - Flaw Location PlotPage 8 of
ael"',AMVOuwbal NoerI*yAsC WasSteam Generator "B" Inlet NozzleFSWOL
Scan Plan+(Po.WW")0 SkewAxialF+CfrnCWfWeMCL- I-3eeScan Units at
Right SeeScanLmitsatM WIgt14 Skew Axl4>AzhnulhaRodwwicPiach
M,"110WOIW CuwdwfneSGFMasdSftE"$NQ*53W9'9w.38wScanSeen
ARiahideAriScanScan
Ar;*heAnclaDkoeefnUmbfunftaMeedo"UmbfLhidAxleI0sk-3.61o4.1-2-
to35-Ckrc-Osk-2-to35-3.0Oto -5.0Axial Oak-3.86to4.133-
1t68WClrcOek33-to Or3.0Oto -5.0A)aL Oak-3G.6104.1M' olO1WCkq_ Osk6r
tolO02'3.0to -5.0AoaBLOsk-3.6
to4.1102'tolS6"CirCLOak10frto131383.0Oto -5.0AxdLe1Oek1.6 to4.
1136' to 10rCkqrcl8Osk136'to1O1O3.0 to .5.0AdM-j8Oa1.6
to4A1102'toWCWGl8Oa102-toBO'3.01to-5.0AAdLIBOelc1.610-6.1GO-to
33Ch~cj8OakWto33-3.01to-5.0MA)Wl8Oak1.61o-8.135- to -2-Circ-jSW*36-
to -r3.0to-5.0ClroOsk2-5
to-3.0101ro11(rClrcjSft12.51to-3.010'tollO1yS-Mun.eExambiaonAnglesFocushifonnatonScaning
kicrmntWOL(-10- 0-,+10")10'Intervals50-.100% VWL TAxial0
SkewWOL(25--.75)010"IntervalsProjection0.5.WVM45"5.4r' HPWBMGo5.0"
HPWOL(-10r - (-,+101)10'Intemrs50-.100%
WOLTInAxwsAxial180SkewWOL(25"-.75-)
a10-IntevalsProjection0.5.DetectionI LengtSizing:0.20'WUM45'5.47r
HPSiing Index Axle:0.10V__M60O5.0'
HPWOL(25'-,65)Q10"IntervalsProection 0.5"Data Co'ectionAxis:Circ 0
Skew (CW)WBM45"6.29" HPA*0.040rWUM60'5.0"
HPWOL(25'-,65)Q10-IntervalsProction 0.5"Ciro180Skew
(CCW)VYM45"6.2WHPWBM60"5.0MHPSerialNo.12-326DocketNo.50-338BSteamGeneratorHot
LegSealWeldRepairVStructuralIntegrity Associates,
Inc.PHASEDARRAYULTRASONICEXAMINATIONRECORDExaminationData Sheet
No.:NAPS-SG-B-FSWOL(Informational)CalibrationData Sheet No.:See
CommentsSectionDate:04/10/12Time:0915through1045Plant:NorthAnnaUnit:iProcedureNo.:SI-UT-126Revision:3ExaminationScansPerformedYesNoComponent:DWG
#11715-WMKS-RC-E-1B.2- Steam GeneratorBInletNozzleFSWOL(1)
Axial(FacingDownstream)0n-ComponentConfiguration:Nozzle-to-SafeEndWeldNo.:
WeldN-SE29IN-SummaryN1.R1.15.004(2)
Axial(FacingUpstream)0E]WeldOverlayRegions:Oveday,
OverlaidWeldandBase Material(Outer 25%)Nozzle-to-SafeEnd(3)
Circumferential(ClockwiseFlow(1 )Z01]ExaminationSurface:Surface of
WeldOverlayExaminationAngles(4)
Circumferential(Counterclockwise(Z)10JWeld OverlayThickness:-
0.50InchAxialCircumferentialNotes:00through84000through840Asviewedfacing
downstreamComponentTemperature:70 F(2) Examinationgainsens"was
continuouslyadjusted toExaminationSensitivity:51.0dB12)51.0
dB(21maintain5%to 20% procedurespecifiedbaseline noise.Purposeof
Examinations:1) Todetermine thedetectabilityof theunderlyingaxial
flaws (previouslyleaking through-wallflaws).2) Todetectpotential
conditionsin the DMweldrepairregionwhichmayhave resultedfrom
weldingprocessor from
theunderlyingcrackbeingdrawntowardthedeposited
repairweldmaterialduringwelding. This examinationregionis
outlinedin withreddashed linesbelowright.3)Tointerrogate a
selectedregionof theweld overlaymaterialwhere porositywas
detectedduring in-processPT
examinations.Thisexaminationregionisoutlined in
withbluedashedlinesbelow right.Conclusions:1) The
twounderlyingaxialflaws(previouslyleaking through-wallflaws)are
detectable.2) The repairweldregion(over the
axialflaws)containsneitherdetectablewelding flaws,norevidence
thatthe underlyingcrackhadbeen drawnoutwardby the
depositedduringrepair welding.3) The selectedregion of the
weldoverlay containsalimitedamountof indicationsof porosity,as
describedin thisreport.ApplicableCalibrationDataSheet:NAPS
SG-BWOL(Informational)Examiner:ChadMcDonaldSIReview:JohnJ.
HaydenLevel:IIDate:Level:IIIDate:04/11/1204/11/12FVFPage1 of
11VStructural Integrity Associates, Inc.Locationof Weld
RepairedExamination RegionC"/~c//B$~H~OZ~J-(/7)*- - 7e-roNIE/APage
2of 11!tStructural Integrity Associates, Inc.Locationof Weld
Overlay MaterialExamination Region0~ARIAA/7/.7/80-i9//&~
~'h/fi0,VolAA(*O o.~rcR'IrOiviSAWfENDPage3of 11VStructuralIntegrity
Associates, Inc.ScanIAxialFlaw #1 - LookingCW (Data
acquiredwithfront of wedge13.0" from900Punch Mark)Page 4 of
11VStructuralIntegrity Associates, Inc.Scan 2AxialFlaw #1-
LookingCCW(Dataacquiredwithfront of wedge14.0"
from900PunchMark)SUnletdA-ScanGr.lS:180A:0Bem 49R48.00S:180.00
MainGets PO2-11 1 .83.1Page5 of 11VStructuralIntegrity Associates,
Inc.Scan3AxialFlaw #1- LookingCCW (Data acquiredwithfront of
wedge14.0" from 900PunchMark)sector~iasan GO&S:180k0Beam 47Ft
46.00 S.160.00 Mak C72lowIIs11IOOis b0Page6 of
11VStructuralIntegrity Associates, Inc.Scan5AxialFlaw #2 -
LookingCW(Data acquiredwithfront of wedge14.25"
from900PunchMark)Page7 of 11VStructuralIntegrity Associates,
Inc.Scan6AxialFlaw #2- LookingCCW (Data acquiredwith front of
wedge15.25" from900PunchMark)III0.8083.1wdcoria%con Gri
SlB8OA.O:5m51Rc5000S.180OMahCUKPage 8of 11VStructuralIntegrity
Associates, Inc.Scan 7AxialFlaw #2-
LookingCCW(Dataacquiredwithfront of wedge15.25" from900PunchMark)I
Lh*edA-Scan Gr.tS:160A0:Beam 46It 45.00 S: 180.00 MainGate
P0[110.7383.1S[I13jsectorilulacanrlS.,lBAOkOlea4Sft45.00S:l8000MOkiI101Page
9 of 11VStructural Integrity Associates, Inc.WeldOverlayRegion@
TDCPorosity at 4.5" from TDCnear Safe End edgeof WOLsectorialscan
GrlS:180A:O.Bam33 R32.00S:180.00 MainG1.451SPage 10 of
11VStructuralIntegrity Associates, Inc.WeldOverlayRegion@
TDCPorosity at TDCnear SafeEndedge of WOLNLikedA-ScnGOiS:180A0:Beam
22R:21.00 S:180.00 MainGateP0.1.3683.18IR2-"Page11of
11SerialNo.12-326DocketNo.50-338CSteamGenerator.HotLegCStmctural
IntegrityAssociatesiPHASEDARRAYULTRASONICEXAMINATIONRECORDCustomer:WeldingServicesInc./
DominionExaminationData SheetNo.:NAPS-SG-C-FSWOLCalibrationData
SheetNo.:See CommentsSectionBelow.Exam Start:I04/15/12 -1100I
ExamFinish:1 04/16/12-
1350Plant:INorthAnnaunit:1ProcedureNo.:SI-UT-149Revision:4ExaminationScans
PerformedYesNoComponent: DWG #11715-WMKS-RC-E-1C.2- SteamGenerator
CInletNozzleFSWOL(1) Axial(FacingDownstream)0ElComponent
Configuration:Nozzle-to-SafeEndWeldNo:WeldN-SE29IN-SummaryN1.R1.15.002(2)
Axial(FacingUpstream)0ElCoverage:(See below for
coveragedetails)Limitations: ISeeReportedConditions(3)
Circumferential(Clockwise)09ElComponent ZeroJX=TC, Y=
+0.50"Upstreamfrom1ExaminationSurface:ODSurface(4)
Circumferential(Counterclockwise)0ElDatum
Locations:Nozzle-to-ButterInterfaceDM
WeldWidth:1.59"WOLDiameter:42.2"WOLTemperature:77FExaminationAngles
& ScanSensitivtyData File
NamesAxial0"Axial180'Circ0"Circ180"NAPS-SG-C-FSWOL-AxialOak-3.6
to3.7 -2to 35NAPS-SG-C-FSWOL-ClrcOak 2.6 to-5.2 -2
to35NAPS-SG-C-FSWOL-AxialOak-3.6 to3.733to
69NAPS-SG-C-FSWOL-CircOak2.6 to-5.233 to 68NAPS-SG-C-FSWOL- Axial
Osk -3.6 to3.7 68to 102NAPS-SG-C-FSWOL-CircOak2.6 to-5.2 66to
102NAPS-SG-C-FSWOL-AxialOsk -3.6 to3.7 68to
72NAPS-SG-C-FSWOL-CircOak 2.6 to-5.2100
to138NAPS-SG-C-FSWOL-AxialOsk -3.6 to3.7100 to
136NAPS-SG-C-FSWOL-Circ180sk 2.7to -5.3 -2 to
35NAPS-SG-C-FSWOL-AxialI80sk 1.2to-8.1-2 to 35NAPS-SG-C-FSWOL-
Circ18Oak 2.7 to -5.3 33to 68NAPS-SG-C-FSWOL-Axial180sk1.2 to-6.133
to69NAPS-SG-C-FSWOL-Circ180sk2.7to -5.3 66 to
102NAPS-SG-C-FSWOL-AxialI80sk 1.2 to-6.166
to102NAPS-SG-C-FSWOL-Circ180sk2.7to -5.3100
to136NAPS-SG-C-FSWOL-Axial180sk1.2 to-6.1102
to136Comments:Duringthe examinations,three(3)
flawindicationsweredetected;two (2) WeldOverlay(WOL)planar
flaws,one(1) WOLlaminar flaw.One (1)of the two(2)planar
flawsislocatedoutside the WOLexaminationvolume.Allthree (3)
flawsare acceptableinaccordancewithASMESectionXl,IWB-3514andthe
additionalrequirementsof Relief RequestNI-14-CMP-001.See
theIWB-3514flawcharacterizationandevaluationonthe
followingpages.ExaminationCoverage:Examinationsachieved90.0%coverageof
the requiredvolume of the WeldOverlaymaterialexaminationvolume
forLaminar Flaws.Examinationsachieved96.3%coverageof the
requiredvolume of the WeldOverlaymaterialexaminationvolume
forPlanar Flaws.Examinationsachieved99.8%coverageof the
requiredvolume of thePSI-
ISIexaminationvolume.Examinationsachieved100%coverageof the
susceptiblematerialwithinthe examinationPSI -
ISIexaminationvolume.The applicableCalibrationDataSheets
arelistedbelow:NAPSSGA / C- WOL - 0 AXIAL;NAPSSGA / C- WOL - 180
AXIALNAPS SGA / C - WOL - 0 CIRC;NAPSSGA I C- WOL - 180
CIRCAnalysis:Reviewer:VLevel:mrDate:O/SILevel:Date:PageIof
7Dominion
J&JaA/ANII:Date:Date:StructuralIntegrityAssociatesPHASEDARRAYULTRASONICEXAMINATIONRECORDCustomer:WeldingServicesInc.
/DominionExaminationData
SheetNo.:INAPS-SG-C-FSWOLExaminationCoverageCalculationsComponentlD:NAPS-SG-CWeldOverlayAcAcnranceExaminatidon
Volume -
LaminarFlawsAxialTowardNozzleTotalAreaCoveredAreaPercentWeight1184106690.005AxialTowardSafeEndTotal
AreaCoveredAreaPercentWeight1184106690,00 5CircumferentialCWI
CCWN/ATotal:Weld Overlay Acceotance Examination
Volume.PlanarFlawsAxialTowardNozzleAxialTowardSafeEndCircumferentialCW/
CCWTotalArea11.84TotalArea1184TotalArea1184CoveredArea11.84CoveredArea1184CoveredArea1096CoveredArea6,68CoveredArea672CoveredArea673Percent100,0Percent1000Percent926PSI
- ISI Examination
VolumeAxialTowardNozzleTotalArea673AxialTowardSafeEndTotalArea673CircumferentialCWI
CCWTotalArea6
73Weight0.25Weight025WeightO5Total:Weight0.25Weight025Weight05Total:Weighted
Coverage460Weighted Coverage45.090.0Weighted Coverage25.0Weighted
Coverage250WeightedCoverage46396.3WeightedCoverage248WeightedCmerage250WeightedCoverage5099.8Percent99.3Percent999Percent100Page
2 of 7(CStructuralIntegrity AssociatesPHASED ARRAYULTRASONIC
EXAMINATIONRECORDxiCustomer: WeldingServicesInc./
DominionExaminationData Sheet
No.:NAPS-SG-C-FSWOLWOLPlanarFlawComparisontoAcceptanceStandardsComponentID:NAPSSG-CRaw(S)DepthDepthFlaw
Thnr.Upper(01))SubsurfaceFlawFlawFlawFlawOto
TopO00toBottamWallComponentAcceptanceFlawFlawFlawBoundaryMaterialFlawFlowK%.lEFIII
Lenatm ol
FaanofIFoZTIhicness')Ihikne'aAAlat&pmxroimityI=Adn1411.6010.28.600730970.243.991630.120.017.36SubsurfaceAustenitlc0.017,36%269.870.20.401,281.480.203.991.630.100.2!6.13SubsurfaceAuslenltc0.216A13%Note")
D01WetoT,(nominalthickness)Notel'Thicknessappllcaoleforflaw
acceptance:Reliant upon
thenominalWCLthicknessabovetheDMwetelASMESectionX1(2004)
TableIWB.3514.2(PSI)SubsurfaceCodeFlawAllowableOnlynA~IaeesbflnmEk823%1Acceplable(-2to35')
Axial1801Sxew8.90%1Acceptable(68to72-) AXia0-
SkewWOLLaminarFlawComparison to AcceptanceStandardsASMESectionXl
(2004) TableIWB-3514.3Component ID;NAPSSG-CRelief
ReaumtAccamancaStandardaFlawFlawFlawFlawVolumeASMELinearLaminarObstructedFlawLength")Lengtht"FlawWidthzWidth(2)FlawFlawFlawObstructedWOLCodeDimensionAreaVolumefi.ioniEndLengtlh2WaiWnWidth12AreT
a"1 ~hijhyEa FieThkneanLjjnj,
t12.22In.(19.43In'lt155.2In)Dnat.eFite31018010460280-219-1840350981
530041
63AccentAccectAcceptAccept(100'to136"Axial180')QA-oifl--TotalTotalFlawFlawIEIVolumeNoteIllThelength
axisofthelaminar lawisusuallyparallelto
thedirectionofweldingNote(2)Thewidthaxisofthe
laminarflawisusuallyperpendicularto
thedirectionofweldingWidthdimensionsof laminarflawsaresupplied
fortheabovecalculationsarebest-eflodestimatesWOLPostulatedRadialFlaw
ObstructedbyLaminarFlawsFlawASMESectionXl (2004)Table
IWV514.2(PSI)Subsurface(S)DepthDepthFlawThru.Upper(OD)SubsurfaceCodeFlawFlawFlawFlawFlew00oTopODtoBottomWellComponentAcceptanceFlawFlawFlawBoundaryMatelalFlawFlawAllowableOnlyNOjStarEnLenottof
Flawof Flaw2a.sPThicknkes'
MaalWProximityimyaim04%Y=sWResuDate31.6010.28.601.531.E70.043.991.630.020.001.23Su~surfaceAustenllic0.001.23%8.20%1Acceptaale100to136'ioal180')NoteW"DWeldT,(nominalthickness)Note"nThicknessapplicaole
forflawacceptance* Reliant uponthe nominal WOL thcrn ass alote the
OtwelbData Analyst: 44)ZLevel:IIIDate:o///1DominionLIII:44C.Date:
1k4c~4~'z Page 3 of 7SStructural Integrity AssociatesSteam
Generator - C: Flaw
TablePlanarFlawsDepthtoDepthtoFlawFlawFlowFlawJMQBottmmfFlaw
Thru.No.2LStartEnjd_LenathY
positionFlawMXFlawWall2aAmplitude11601028601f25to2120.730.970.24269.87020402_161.2814802002%Laminar
FlawsFlawFlawFlawFlawFlawLengthll)LengthFlawWidthWidthFlawFlawNo.SrEndLenathS=rtEndWidthDeathAmIlitd3101.80104,60280-2.19-1840351352%Page
4 of
7StructuralIntegrityAssociatesPHASEDARRAYULTRASONICEXAMINATIONRECORDSG
- Charlie:Axial Scan (1800Skew)WOLPlanar Flaw #1-2" to 35"
+1001800SkewICustomer:jWeldingServicesInc./
DominionlExaminationDataSheet No.:NAPS-SG-C-FSWOLWOL PlanarFlaw
#1-2" to 35" +1001800Skew,Flaw #1.,I4.12I,.8.24Page 5 of
7StructuralIntegrity Associates~SG - Charlie:Axial Scan
(00Skew)WOLPlanarFlaw #268" to 72"00SkewWOLPlanarFlaw #268" to 72"
00Skewi'i II.:*-4.--.--1Flaw #2.n__A4I~I- 5Page6of
7VStructuralIntegrity AssociateseWOLLaminarFlaw#3100" to136"
+1000OSkewIF"_-7-_J$- I',.:LLaminarFlaw#3100" to136"
+10000SkewamILs IPage7 of
7ANSteamwGnraatorleNyAssociatesSteamGenerator C Inlet Nozzle
UltrasonicExaminationSteam GeneratorC - Inlet NozzleFSWOL - General
Configuration6.99"5.36"
6.37"NozzleSideReferencePunchMark1.59"aSafeEndSideReferencePunchMarki-*---'-.
. Code CaseN-740-2 WeldOverlayExaminationSiVolume.........
A-B-C-DNote:The interfaceC - D incWdes thebondand
thehea-affectedzone from the overlay.TheHAZ
extenduAntothea-efentcweld.A-B-C-0I1.58"Outer1.03'wNozzleMaU5rielAloySA-NeCIS'*51IuMNP*CSaaNl4.10r'AButtWoADNy8/Safe
EndMAtedellSA-336ChmPage Ior 8SVOuduralItegriy AssmcatesSteam
GeneratorC Inlet NozzleUltrasonicExaminationSteam GeneratorC -
Inlet NozzleFSWOLWeld Overlay Axial Acceptance Examintion
CoverageAxialWOLLa&mniFlawIExmk*atoCovemga90.0%AxalVWOLPlanarRawEr-mbnonCoverye-100%No
LaminarFlwEmaminationCoveragsPage2 of 8!UScturul
IategrityAssociatesSteam GeneratorC Inlet
NozzleUltrasonicExaminationSteam GenratorC - Inlet NozzleFSWOL -
CircumferentielExamination CoverageWeld Overlay Acceptance andPSI
IISIExamination VolimesCircumferetiaWOL PlanarFlawExamkbftn
Coverage.0.3%ChoirenUPSI IS1Examination Coverage.100%7.70"{w*No
Planar Flaw&aimiao ComgPage3of 5Structural Intgdly
AssociatesSteam GeneratorC Inlet NozzleUltrasonic ExaminationSteam
GeneratorC- Inlet Nozzle FSWOLPSI / ISI Axial Examination Volume
CoveragerL2.40"-4.82--pAxial PSI /ISIExamirntion
Coverage.9m.8%NOWOlMatrlwSA-508C13SPwsCCSusc~p//SANtEndMfaterblSA4336/uet1AH5~yA811Page4
of5VSbwtural Ine#ri'AscatSteam GeneratorC Inlet
NozzleUltrasonicExaminationSteam GeneratorC - Inlet NozzleFSWOL -
Flaw Location PlotL.i.IVL LaMh*arW.KO IVLPawIagSA-aNCF3 NP4CC
SUBOdChmnMSIUMPage 5 of 50!Stncural Ifterity AssociatesSteam
Generator"C" Inlet Nozzle FSWOL Scan
Plan+(PMsWV)arrcCWSe.ScanUmiNSat RghtWeldCL- (Negative)SeaScan
Uffts at RItWmAzimuthRefe"noPunch M1.*to IM WMd
CAn/igrn.PosStionSkdSeiEnd S/d0.&226.35w90
5.46"6.3V1805.2V"8.36270"5.48"6.W9"sewScanAxisindex
AxisScanScaAxsndeAxisDkwcffonLisftiUmbfDkconkfUitAxial_0k-3.6
to3.7-2'to 35"CircOak-2to 35T2.6to -5.2Aal
Osk-3.6to3.733'to9CircOak33" to 682.6 to -5.2Axia0sk-3.6
to3.766Wto102"CircOak66to102'2.6 to -5.2AxiaOk-3.6 to3.7100. to
136CIrcN-0100'to136I2.Ato5.2Axlalj80k1.2 to-6.1136'to
100,Circl1801k136'to 100,2.7 to-5.3Axial180$k1.2 to-6.1102"
to66"Cikc180k102" to 662.7 to-5.3Axil180lk1.2 to-.516to
33'Cinv8jOk6Wto 332.7 to -5.3Axialo180k1.2
to.5.13V5to-2"COko_180k35Wto-2"2.7 to -5.3Semp NameExmimaon
AnglesFocus lnommaonScamningncmentsVWOL(-101 --(-.
+10")10'Intervals50-100% VVOLTAxial 0SkewWOL (25--.75')
Q10'IntervalsPrjebm0.5.WBM45"5.47HPWM60"5.0UHPWOL(-10' - 0-.
+101)10.lntervals50-100% WOLTnAxial180 SkewWOL (25'-.75') Q10"
IntervalsPojecon0.5"Detection/ LengthSizhig0.20rWUM
45"5.47HPSizingIndex Axis:0.10WSM605.0,HPWOL(25'-45)
a10'IntervalsProedion0.5.DateColection Axis:Circ 0Skew
(CW)WBM45'6.29'HPAll:0.040'WB605.0HPWOL(25"-AS') @10"
IervalPmjecion0.5.Circ180 Skew(CCW)WBM45'6.29WHP__WBM605.0* HP
