ML18054A949
| ML18054A949 | |
| Person / Time | |
|---|---|
| Site: | Palisades  |
| Issue date: | 08/24/1989 |
| From: | Decker J, Willman S CONSUMERS ENERGY CO. (FORMERLY CONSUMERS POWER CO.) |
| To: | |
| Shared Package | |
| ML18054A948 | List: |
| References | |
| NUDOCS 8909060071 | |
| Download: ML18054A949 (327) | |
Text
{{#Wiki_filter:., PALISADES NUCLEAR PLANT 1989 MIZ-18 EDDY CURRENT SYSTEM QUALIFICATION PROJECT NUMBER 248815222024 CONSUMERS POWER COMPANY ENERGY SUPPLY AND FIELD TECHNICAL SERVICES NDT SERVICES DEPARTMENT 135 WEST TRAIL ST. JACKSON, MICHIGAN 49201 WRITTEN BY~&;~ LEVEL~_ DATE__!!~~ APPROVED BY: .J_ _ DATE~-f'?
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- ACKNOWLEDGEMENTS The following personnel were involved in the development and implementation of this qualification program. Their involvement-has contributed to the successful completion of this project.
- 1. Kelly V. Cedarquist; Senior Engineer, Consumers Power Company, Palisades Nuclear Plant, Plant Projects Dept.
- 2. Blaine L. Curtis, P.E.; Level III Consultant, Allen Nuclear Associates
- 3. Lori A. Leitch, P.E.; General Engineer, Consumers Power Company, Energy Supply Technical Services, Engineering Evaluations Dept. *
- 4. William R. Pavlichko, PhD; Staff Engineer, Consumers Power Company, Energy Supply Technical Services, Engineering Evaluations Dept.
- 5. H. W. Voight, Staff Chemist, Consumers Power Company, Energy Supply Technical Services, Chemistry Dept.
- Tl.ILE MIZ-18 QUALIFICATION REPORT SE.CTlQN BACKGROUND & OBJECTIVES ----*------------------------------- 1.0 APPROACH -------------------------------------------------- 2.0 TECHNICAL DESCRIPTION --------------------------~--~------- 3.0 TECHNIQUE CONFIGURATIONS ---------------------------------- 4.0 TECHNIQUE SPECIFICS --------------------------------------- 5.0
- GUIDELINE FOR ANALYSIS TECHNIQUES ------------------------- 6.0 TECHNIQUE CONCLUSIONS------------~------------------------ 7.0 STATISTICAL ANALYSIS -------------------------------------- 8.0
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- ENERGY SUPPLY TECHNICAL SERVICES NONDESTRUCTIVE TESTING SERVICES DIVISION PALISADES STEAM GENERATORS MIZ-18 TECHNOLOGY UPGRADE 1989
1.0 BACKGROUND
& OBJEQI.I.Y.E.6.
I. BACKGROUND The following background explains the reasoning behind upgrading from the present Zetec MIZ-12 System to the MIZ-18: A) Based on eddy current profilometry results collected from 1981 to 1985, the progression of magnetite denting is continuing at an average rate of 2.0 mils radially per operating cycle on the most severely dented support plates. The problem occurs, in eddy current inspection, when a previously reported flaw indication is associated with an area of denting. The dent response will tend to obscure the flaw indication progressively as the denting increases. The MIZ-12 system has the ability to suppress dent responses up to approximately a 4.0 mil radial dent. After that point the system begins to lose the ability to suppress the dent up to a level of approximately 8.0 mils radially, at which point the system reaches electronic saturation of the instrumentation.. The MIZ-18 system is a digital system and is not restricted by instrumentation voltage limits, input into the tester, as in the MIZ-12 system. This allows for a much needed increased dynamic range for the signal input. With this increased capability, it is apparent that the MIZ-18 system would be capable of handling signal responses from dents more severe than 8.0 mils of radial compression. The ability to implement the MIZ-18 system at Palisades ~as delayed however d~e to the inability of the available analysis software to suppress both the support and dent response simultaneously. For this reason it was necessary to remain with the existing techniques using the MIZ-12 system. Recently, Zetec Inc. has begun marketing analysis software capable of performing the necessary mixing functions to accomplish the simultaneous support and dent suppression. Based upon this, it is now appropriate to attempt to qualify the MIZ-18 system for detection and 0488-010.18B
- Page 2 - 1
- . B) sizing of all of the known defect mechanisms within the Palisades steam generators.
Th~ Palisades plant is currently in the process of changing the data management system, from the corporate mainframe computer system, to a stand alone P.C. based system titled "ISIS-TUBE". One of the advantages of this system is that it makes use of the MIZ-18's digital capabilities to record the final analysis results and transfer this information by computer to the data base .. This eliminates many hand generated steps in the data flow process that increase the possibility of error in the recording of results. A reduction in clerical manpower ~ill be realized which will help in reducing overall inspection costs. C) From an A.L.A.R.A. standpoint the MIZ-18 system offers the potential to reduce overall work time spent on the steam generator platforms. The number of cables run to each platform from the ope~ating station could potentially be reduced by half. The possibility of utilizing a zero-entry positioner with the MIZ-18 is a reality and the probe pushers *could be controlled through the computer. The setup time for the MIZ-18 is less and requires minimal calibrations for the operator, thus reducing the need for personnel on the platforms. For the rotational exams of the sleeves and dented regions, the SM-6 probe pusher is no longer required with the MIZ-18. This, in itself, is a major reduction in man Rem exposure to platform personnel. With the use of the MIZ-18's rotating head probes all of these examinations can be accomplished much the same as the other pull-through techniques. D) During discussions between Consumers Power Company personnel and the Nuclear Regulatory Commission in late 1987, the NRC indicated a need to become more updated in the technology employed in the eddy current inspections of the steam generators at Palisades. Until just recently, as stated in 'A', the mixing technology as needed for Palisades was not available. This limitation now has the potential o'f being eliminated. It appears probable that MI?-18 system could be implemented at
'Palisades and satisfy the concerns of the NRC.
- E) The ability to support an inspection utilizing the MIZ-12 system is becoming increasingly more difficult due to the lack of available equipment. The standard industry equipment has become the MIZ-18 digital system.
0488-010.lBB
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- Consequently none of the major vendors support the older MIZ-12 system. In addition to this, the testing personnel are no lon-ger current on the operation of the older system and would require refresher training.
II. OBJECTIVES This qualification intends to address all the known types of defect indications that exist within the tubing of the Palisades steam generators, and to demonstrate that the MIZ-18 system meets or exceeds the capabi"lities of .the existing MIZ-12 techniques qurrently used at *Palisades. This will be accomplished by sequentially achieving the following objectives: A) Determine the appropriate coil configuration(s) for each type of known flaw geometry.
- 1. Wastage (with and without dents)
- 2. Intergranular attack (with and without dents)
- 3. Circumferential cracking (with and without dents)
- 4. Tube/sleeve defects B) Determine the appropriate test configuration(s) for each type of known flaw geometry.
- 1. Wastage (with and without dents)
- 2. Intergranular attack (with and without dents)
- 3. Circumferential cracking (with and without dents)
- 4. Tube/sleeve defects This objective includes a number of tasks that have been addressed .during earlier work with Zetec Inc. of Issaquah, Washington. In November of 1986 and December of 1987, a study was attempted to determine the abilities of the Zetec enhanced mixing software. This resulted in some improved capabilities in dent suppression over the MIZ-12 system. Since that work was done, Zetec has continued to developed an improved concept in mixing software that could further improve flaw detection and sizing. This will require repeating some of the work done previously but the overall improvements should prove beneficial .
- C) Determine the detection and sizing capabilities of all techniques.
- 1. Bobbin (.540/.560/.580) 0488-010.18B
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- - 2.
3. 4. 5. Multicoil surface riding pancakes (4C4F/8xl) Motorized rotating pancake coil (MRPC) Sleeve examination (rotating axial wound differen-tial and crosswound) Other techniques (Narrow Groove Bobbin Coil, Rotating Axial Wound Differential) D) Determine performance levels of_ selected MIZ-18 techniques compared to accepted MIZ-12 techniques presently approved at Palisades. E) Determine the potential for change in the Palisades data base when the switch is made from the MIZ-12 system to the MIZ-18 system.
-o488-010.18B
Page l ..... 2
- I. APPROACH This qualification is intended to be inclusive for all of the eddy current test methods to be utilized at Palisades. The defect sample matrix '(Attachment 2-A) shall include wastage type flaws with depths from 20% to 100% throughwall with denting levels from .000" to .030" of radial compression.
IGA samples shall include depths from 20% to 100% throughwall with denting levels from . 000" to . 030" of -radial compression. The simulated circumferential-crack samples will range in depth from 20% to 100% throughwall with denting levels ranging from .000" to .010" of radial compression. The sleeve assembly samples shall contain wastage type defects on the parent tube O.D. and I.D. The sleeve shall contain defects on the O.D. only. The probe designs types for this qualification shall include the following:
- A) BOBBIN COIL The bobbin coil presently used in the MIZ-12 analog system is a set of 0.540" diameter coils connected in the differential mode. The coils.are separated 2.5" apart (i.e. 540 SFW) and were spaced at this distance to achieve two functions* on the. analog system:
1.) By separating the coils, the eddy current fields generated by the coils did not influenc~ each other .
. Thus the lobe openings normally seen on the support plates and the dents were dramatically reduced. This reduced the X and Y component respectively, in the support and the dent allowing less signal suppression to be required in the mixing process.
2.) The separation of the coils also reduced the influence of a dent when only one coil was affected independent of the other. There are several limitations to this particular probe. These limitations are as follows: The fill factor of the 0.540" diameter coil in the 0.654" diameter I.D. inconel tubing is only 68% (optimum is 85% to 95%). *This creates two problems: 1) Sensitivity to small volume defects is less because of reduced eddy current coupling to the tube 0488-010.18B
Page 2 - 2
- wall. 2) The signal to noise ratio is decreased because of increased levels of probe motion. The probe motion with the 540 SFW is further increased due to the flexible construction of the probe head.
Some preliminary work has been done with the MIZ-18 utilizing several coi1 designs, one being the 540 SFW probe. It has been determi~ed that the mixing capabilities using the 540 SFW probe were not as good as the close space bobbin coils when utilizing the MIZ-18 digital system. It is also apparent that the fill factor could be increased to improve the detectability level of the probe. Based upon the fact that the body diameter of the 4C4F probe, currently used at Palisades, is 0.560" diameter, it is reasonable that the bobbin coil diameter could be increased to at least 0.560" with minimal number of probe restrictions during in-generator testing due to denting. This would bring the fill factor to 73% which would be an improvement over the 0.540" probe. It would be preferable to increase to a 0.580" diameter coil which would.bring the fill factor to 78%. The 0.580" probe has been used previously at Palisades prior to 1981. A sample of approximately 400 tubes-Was examined in 1988
- with a 0.580" probe with no obstructions encountered.
This would indicate that larger diameter probes could be utilized with a minimal amount of obstructions due to denting. To increase the probe diameter greater than 0.580" would not be feasible due to excessive weld rollover at the tubesheet on some tubes, ovalization in the 90° bends and significant
. levels. of magnetite denting in many tubes.
B) MULTI COIL SURFACE RIDING PANCAKES (4C4F/8Xl) 4C4F The 4C4F probe design is currently used at Palisades for the detection of circumferential cracks and sizing of* intergranular attack (IGA). This design incorporates eight surface riding pancake coils of 0.187" diameter, arranged in two sets of four with each set wired in series. Each set is then connected in a differential mode to the "other set (see figure 2-1) . . This probe is similar in design to an earlier version (the 4 X 4) except the coil sets are spaced 2.5" apart with a flex member between the sets, as opposed to the 1.0" separation on the solid gody 4X4. This allows the 4C4F probe to traverse the 90 bends in the steam generators.
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- The 4C4F technique was qualified on the MIZ-12 System, in 1983, for the detection of circumferential cracking.
However, during the 1983 inspection, the technique detected flaw type indications that had not been detected.* with the &40 SFW probe. After a series of studies, which included pulling tube sections from the steam generator for metallurgical analysis, it was determined that the flaw responses were areas of IGA. The technique was subsequently qualified for detection and sizing of IGA ranging in depth from 30% to 60% of tube wall.in the presence of up to a 4 mil radial dent. The initial study of this probe design for the MIZ-18 upgrade should include, as a minimum, a range of defect types and configurations to establish equivalent detectability and quantification ability of the 4C4F .
- 8.3 FT. NYLON SHAFT
**MAXIMUM COIL O.D.
(*+ .12) . FLEX MEMBER *PROSE O.D.
;:'LEX MEMBER 1
'*"NOMINA~ TUBE I. D.
FRONT COIL SET(4 EA. PANCAKE) J REFERENCED TO . . . REAR COIL SET(4 EA. PANCAKE) FIGURE 2-1 4C4F PROBE 0488-010.18B
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- 8 x 1 The 8 X 1 probe design utilizes 8 separate surf aces riding pancake coils to provid~ a total coverage around the I.D. of the tube wall. These coils are wired in the absolute mode (external reference differential) and function independently. *This technique provides good sensitivity to volumetric type defects and circumferential cracking.
The 8 X 1 technique was first evaluated in 1983 using the MIZ-12 System. With the MIZ-12 System the ability to preform multi-frequency mix suppressions, using the 8 X 1 technique was not possible . . For this reason, it was determined that the 8 X 1 could not be utilized at that time. With the MIZ-18 System, the ability to mix frequencies is possible using the 8 X 1 technique. This technique should b~ evaluated again to determine if any additional benefit could be obtained .
**MAXIMUM COIL O.D.
. 83 FT, NYLON SHAFT (*+ ,12)
FLEX MEMBER *PROSE O.D. FLEX MEMBER
....,.NOMINA~ .TU8E 0. J 1
I. EXTERNAL REFERENCE PANCAKE COILS(8 EA,)
- 0488-010.18B FIGURE 2-2 8Xl PROBE
Page 5 - 2 .~ C) ROTATIONAL PANCAKE COIL (RPC) This technique utilizes a surf ace riding pancake coil that is rotated through the I.D. of the tube while being retracted from the tube. This provides for a helical
- scan of the tube wall. The technique was initially developed for the detection and sizing of flaws ~ 45%
that were no longer.interpretable because of denting. The original technique utilized two EM-3300 single frequency testers. The first unit operated the test pancake coil and the second unit was connected to the locator coil mounted on the probe body. This test system plus the use of the SM-6 rotating probe pusher was the basic set-up used until 1983. At that time the technique remained essentially the same except the EM-3300 units were replaced with the MIZ-12 tester. This technique, although functional, resulted in increased platform time for personnel due to a large number of mechanical failures with the SM-6 probe _pusher units. (See figure 2-3 for probe design) With the introduction of the motorized head probe, in conjunction with the MIZ-18 Remote Acquisition Data Unit
- (RADU), it is possible to physically perform the rotational exams much the same as any pull-through technique. This technique was qualified in December of 1987 for the detection and sizing of volumetric wastage and characterization of circumferential cracking indications (
Reference:
Consumers Power Co., NDT Services 1987 report, "Qualification Report for Dent/Defect Examination using the Zetec MIZ-18 MRPC"). This qualification addressed only the depth accuracy of A.S.M.E. type machined defects. No qualification of this technique was performed on other types of.tube degradation at that time. The software allows for dimensional surf ace measurements of the length and width of the defect area. This feature was demonstrated in the qualification, although the accuracy of this function was not established. This feature should be evaluated to determine the accuracy tolerance of this analysis mode. The MRPC technique was utilized during the 1987 inspection to verify and characterize the circumferential crack indications detected with the 4C4F Technique. The MRPC software has the ability to perform several analysis functions. The software allows for normal phase or amplitude analysis techniques and an additional C-Scan 0488-010.lBB
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- presentation enables the user to graphically dispiay the geometry of the defect indication.
The present qualification of this technique should reassess and incorporate as appropriate the findings of the 1987 Qualification Report in addition to further evaluating the types of defects not previously addressed.
** MAXI MUM COIL 0.0.
(*+.120) .
*PROBE 0.0.
ABSOLUTE PANCAKE COIL
#NOMINAL TUBE I. D*
] tt
.LOW FREQUENCY LOCATOR COIL FIGURE 2-3 ROTATIONAL PANCAKE PROBE D) INSTALLED SLEEVE EXAMINATIONS ROTATIONAL AXIAL WOUND DIFFERENTIAL The sleeves at Palisades are hydraulically expanded leak limiting sleeves inst~lled in 1976 & 1978 by Combustion Engineering Inc. The examination technique was developed to evaluate the tube-sleeve assembly and 3/8 inch with~n each end of the sleeve. The differential coil arrangement provides good phase discrimination between both sleeve and parent tube flaws. This technique was used through 1981 utilizing the EM-3300. In 1983 it was adapted to the MIZ-12 System.
0488-010.18B
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- The technique should be qualified utilizing the MIZ-18 System i.n conjunction with the rotating head motor unit probe. Some prelimina_ry work has been performed with this equipment and the initial findings indicate that the results are comparable to the MIZ-12 method.
(See figure 2-4 for probe design)
- LOCATOR COIL FIGURE 2-4 ROTATIONAL AXIAL WOUND DIFFERENTIAL PROBE 540 - 280 Khz SLOW PULL This technique was developed to locate the sleeve position in relation to the parent tube flaw an quantify the parent tube defect. It is intended to determine the integrity of the parent tube and ensure.that the sleeve has not moved within the parent tube such that the parent tube flaw is located between the expanded regions of the sleeve/tube assembly. The examination is performed using a 0. 540" diameter bobbin probe for detect*ion of the parent tube flaw .
- This examination could also be adapted to the MIZ-18 with minimal qualification work required. The actual
*technique has*not*been altered but the method of collection and recording would be changed.
Page 8 - 2
- CROSS WOUND This technique has not previously been used in the Palisades Steam Generators. The method is used to inspect the sleeve transitions within the sleeve/tube assembly. Some consideration should be given to evaluating this method in order to determine its merits and limitations regarding the Palisades sleeves.
E. OTHER TECHNIQUES NARROW GROOVE BOBBIN COIL This probe design has been utilized by several utilities for improving the detectability of defects in the presence of conductive deposits on the tube O.D. It appears to be more sensitive to smaller volume pit type defects than the standard.size coil. Consideration will be given to incorporating evaluation of this probe design. into this qualification .
- ROTATIONAL AXIAL WOUND DIFFERENTIAL This probe has proven successful in the sleeve assembly examinations.at Palisades and may have.the potential for providing additional information in the characterization and sizing of other types of defect areas. The probe has two attributes that may provide additional information:
- 1) The coils are surface riding, thus the fill factor of
.the coils is not a consideration. This should improve the sensitivity of the coils to smaller volume defects.
- 2) The orientation of the coils is perpendicular to the circumferential cracking known to exist in the Palisades Steam Generators. This technique used in conjunction with the MRPC Technique may have the potential of improving the overall characterization of circumferential defects at Palisades .
0488-010.lfrB
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- STD MATRIX OF TUBE SAMPLES FOR MIZ-18 WASTAGE QUALIFICATION ATTACHMENT 2-A SERIAL DEFECT DENT CIRC AXIAL DEFECT % OF NUMBER LOC . SIZE EXTENT EXTENT DEPTH WALL IN-168 A N/A 0.110 0.110 0.029" 60%
B 2 MILS 0.110 0.110 0.029" 60% c 4 MILS 0.110 0.110 0.030" 63% D 6 MILS 0.110 0.110 0.030" 63% E 8 MILS 0.110 0.110 0.030" 63% F 10 MILS 0.110 0.110 0.028" 58% IN-169 A N/A
- 0.109" 0.109" 0.028" 58%
B 2 MILS *0.109" 0.109" 0.029" 60% c 4 MILS 0.109" 0.109" 0.028" 58% D 6 MILS 0.109" .0.109" 0. 029 ;, 60% E 7 MILS 0.109" 0.109" 0.028" 58% F 10 MILS 0.109" 0.109" 0.028" 58% IN-170 A N/A 0 .109*~ 0.109" 0.029" 59% B 2 MILS 0.109" 0.109" 0.029" 59% c 4 MILS 0.109" 0.109" 0.029" 59% D 6 MILS 0.109" 0.109" 0.029" 59% E 8 MILS 0.109" 0.109" 0.029" 59% F 10 MILS 0.109" 0.109" 0.029" 59% IN-178 A N/A 0.050 0.050" 0'.049" 100% B N/A 0.075 0.075" 0.037" 80% c N/A 0.110 0.110" 0.027" 59% D N/A 0.190 0.190" 0.018" 39% E N/A 0.190 0.190" 0. 009*" 20% F N/A 2.355 0.125" 0.009"ID 20% IN-317 A 2 MILS 0.078" 0.078" 0.038" 76% B 4 MILS 0.078" 0.078" 0.040" 80% c 8 MILS 0.078" 0.078" 0.040" 80% D 10 MILS 0.078" 0.078" 0.032" 64% IN-319 A 4 MILS 0.190" 0.190" 0.012" 25% B 5 MILS 0.190" 0.190" 0.014" 29% c 9 MILS 0.190" 0.190" 0.013" 27% D 11 MILS 0.190" 0.190" 0.012" 25% IN-320 A 2 MILS 0.080" . 0.080" 0.040" 83% B 5 MILS 0.080" 0.080" 0.040" .83% c 8 MILS 0.080" 0.080" 0.038 79% D 10 MILS 0.080" 0.080" 0.036" 75%
Page 2 of 7
- IN-369 A B
c D E 10 10 10 10 10 MILS MILS MILS MILS MILS 0.078" 0.109" 0.187" 0.187" 0.000" 0.078" 0.109" 0.187" 0.187" 0.000" 0.040" 0.030" 0.020" 0.015" 0.000" 80% 60% 40% 30% 0% IN-370 A 15 MILS 0.078" 0.078" 0.040" 80% B 15 MILS 0.109" 0.109" 0.030" 60% c 15 MILS 0.187" 0.187" 0.020" 40% D 15 MILS 0.187" 0.187" 0.015" 30%. E 15 MILS 0.000" 0.000" 0.000" 0% IN-371 A 20 MILS 0.078" 0.078" 0.040" 80% B 20 MILS 0.109" 0.109" 0.030" 60% c 20 MILS 0.187" 0.187" 0.020" 40% D 20 MILS 0.187" 0.187" 0.015" 30% E 20 MILS 0.000" 0.000" 0.000" 0% IN-372 A 25 MILS 0.078" 0.078" 0.040" 80% B 25 MILS 0.109" 0.109" 0.030" 60% c 25 MILS 0.187" 0.187" 0.020" 40% D 25 MILS 0.187" 0.187" 0.015" 30% E 25 MILS 0.000" 0.000" 0.000" 0% IN-373 A 30 MILS 0.078" 0.078" 0.040"' 80% B 30 MILS 0.109" 0.109" 0.030'~ 60% c 30 MILS 0.187" 0.187" 0.020" 40% D 30 MILS 0.187" 0.187" 0.015" 30% E 30 MILS 0.000" 0.000" 0.000" 0% LARGE VOLUME WASTAGE DEFECTS STD SERIAL DEFECT DENT CIRC AXIAL DEFECT % OF NUMBER LOC SIZE EXTENT *EXTENT DEPTH WALL
----------------------------------------------~--------------------------
IN-302 A 2 MILS 0.196" .688" '0.038" 78% B 2 MILS 0.196" .750" 0.030" 61% c 2 MILS 0.196" 1.500" 0.017" 3'5% D 2 MILS 0.196" . 688" 0.010" 20% IN-303 A 2 MILS 0.588" . 813" 0.036" 73% B 2 MILS 0.588" .. 688" 0.028" 57% c 2 MILS 0.588" .688" 0.018" 37% D 2 MILS 0.588" . 813" 0.015" 31% IN-306 A 4 MILS 0.196" .688" 0.040" 82% B 4 MILS 0.196" .750" 0.029" 59% c 4 MILS 0.196" 1. 063" 0.018" 37%
- D 4 MILS 0.196" .*563" 0.011" 22%
Page 3 of 7 Page 4 of 7
- IN-211 A B
c D 10 8 6 N/A MILS MILS MILS 0.375" 0.375" 0.375" 0.375"
.006"
.006"
.006"
.006" 0.030" 0.030" 0.030" 0.032" 63%
63% 63% 67% E 4 MILS 0.375" .006" 0.031" 65% F 3 MILS 0.375" .006" 0.034" 71% IN-212 A N/A 0.375" .006" 0.049" 100% B 11 MILS 0.375" .006" 0.049" 100% c 8 MILS 0.375" .006" 0.049" 100% D 6 MILS 0.375" .. 006" 0.049" 100% E 4 MILS 0.375" .006" 0.049" 100% F 2 MILS 0.375" .006" 0.049" 100%
MATRIX OF TUBE SAMPLES . Page 5 of 7 FOR MIZ-18 IGA QUALIFICATION
- STD SERIAL NUMBER NUMBER OF DENTS DENT SIZE IGA AXIAL DIMENSION IGA CIRCUMFRENTIAL DIMENSION IGA DEPT 1 IN -464 .o N/A 0.20" 0.588" 30%
2 IN -465 1 4 Mil 0.20" 0.588" 40% 1 6 Mil 0.20" 0.588" 40% 1 10 Mil 0.20" 0.588" 40% 1 15 Mil 0. 20" 0.588" 40% 1 20 Mil 0.20" 0.588" 40% 3 IN -466 0 N/A 0.20" 0. 58.8 .. 20% 4 IN -467 1 4 Mil 0.20" 0.588" 50% 1 6 Mil 0.20" 0.588 50% 1 10 Mil 0.20" 0.588 50% 1 15 Mil 0.20" 0.588 50% 1 20 Mil 0.20" 0.588 50% 5 IN -468 0 N/A 0.20" 0.588 60% 6 IN -469 0 N/A 0.20" 0.588 80% 7 IN -470 0 N/A 0.20" 0.588 100% 8 IN -471 0 N/A 0.20" o*. 588" 30% 9 IN -472 0 N/A 0.20" 0.588" 20% 10 IN -473 0 N/A 0.20" 0.588" 40% 11 IN -474 0 N/A 0.20" 0.588" 50% 12 IN -475 0 N/A. 0.20" 0.588" 60% 13 IN -476 0 N/A 0.20" 0.588" 80%. 14 IN -477 0 N/A 0.20" 0.588" 100% 15 IN -382 4 2 Mil 0.20" 0.588" 30% 16 IN -383 4 2 Mil 0.20" 0.588" 20% 17 IN -384 4 2 Mil 0.20" 0.588" 40% 18 IN -385 4 2 Mil. 0.20" 0.588" 50% 19 IN -386 4 2 Mil 0.20" 0.588" 60% 20 IN -387 4 *2 Mil 0.20" 0.588" 80% 21 IN -388 4 2 Mil 0.20" 0.588" 100% 22 IN -389 4 4 Mil 0.20" 0.588" 30% 23 IN -390 4 4 Mil 0.20" 0.588" 20% 24 IN -391 4 4 Mil 0.20" 0.588" 40% 25 IN -392 4 4 Mil 0.20" 0.588" 50% 26 IN -393 4 4 Mil 0.20" 0.588" 60% 27 IN -394 4 4 Mil 0.20" 0.588" 80% 28 IN -395 4 4 Mil 0.20" 0.588" 100% 29 IN -396 4 6 Mil* 0.20 0.588" 30% 30 IN -397 4 6 Mil 0.20 0.588" 20% 31 IN -398 4 6 Mil 0.20 0.588" 40% 32 IN -399 4 6 Mil 0.20 0.588" 50% 33 IN -400 4 6 Mil 0.20 0.588" 60%
- 34 35 36 37 38 39 IN IN IN IN IN IN
-401
-402
-403
-404
-405
-406 4
4 4 4 4 4 6 6 8 8 8 8 Mil Mil Mil Mil Mil Mil 0.20 0.20 0.20" 0.20" 0.20" 0.20" 0.588" 0.588" 0.588" 0.588" 0.588" 0.588" 80% 100% 30% 20% 40% 50%
Page 6 of 7 I I
** 40 41 42 43 44 IN -407 IN -408 IN -409 IN IN
-410
-411 4
4 4 4 4 8 Mil 8 1Mil 8 Mil 10 10 Mil Mil 0.20" 0.20" 0.20" 0.20 0.20 0.588" 0.588" 0.588" 0.588" 0.588" 60% 80% 100%. 30% 20% 45 IN -412 4 10 Mil 0.20 0.588" 40% 46 IN -413 4 10 Mil 0.20 0.588" 50% 47 IN -414 4 10 Mil 0.20 0.588" 60% 48 IN -415 4 10 Mil 0.20 0.588" 80% 49 IN -416 4 10 Mil 0.20 0.588" 100% 50 IN -417 4 12 Mil 0.20 0.588" 30% 51 IN -418 4 12 Mil 0.20 0.588" 20% 52 IN -419 4 12 Mil 0.20 0.588" 40% 53 IN -420 4 12 Mil 0.20 0.588" 50% 54 IN -421 4 12 Mil 0.20 0.588" 60% 55 IN -422 4 12 Mil 0.20 0.588" 80% 56 IN -423 4 12 Mil 0.20 0.588" 100% 57 IN -424 4 15 Mil 0.20 0.588" 30% 58 IN -425 4 15 Mil 0.20 0. 588". - 20% 59 IN -426 4 15 Mil 0.20 0.588" 40% 60 IN -427 4 15 Mil 0.20 0.588" 50% 61 IN -428 4 15 Mil 0.20 ____ o. 588" 60% 62 IN -429 4 15 Mil 0.20 0.588" 80% 63 IN*-430 4 15 Mil 0.20 0.588" 100% 64 IN -431 4 20 Mil 0.20 0.588" 30% 65 IN -432 4 20 Mil 0.20 0.588" 20% 66 IN -433 4 20 Mil 0.20 0.588" 40% 67 IN -434 4 20 Mil 0.20 0.588" 50% 68 IN -435 . 4 20 Mil 0.20 0.588" 60% 69 IN -436 4 20 Mil 0.20 0.588" 80% 70 IN -437 4 20 Mil 0.20 0.588" 100% 71 IN -438 4 25 Mil 0.20 0.588" 30% 72 IN -439 4 25 Mil 0.20 0.588" 20% 73 IN -440 4 25 Mil 0.20 0.588" 40% 74 IN -441 4 25 Mil 0.20 0.588" 50% 75 IN -442 4 25 Mil 0.20 0.588" 60% 76 IN -443 4 25 Mil
- 0.20 0.588" 80%
77 IN -444 4 25 Mil 0.20 0.588" 100% 78 IN -445 4 30 Mil 0.20 0.588" 30% 79 IN -446 4 30 Mil 0.20 0.588" 20% 80 IN -447 4 30 Mil 0.20 0.588" 40% 81 IN -448 4 30 Mil 0.20 0.588" 50% 82 IN -449 4 30 Mil 0.20 0.588" 60% 83 IN'-450 4 30 Mil 0.20 0.588" 80% 84 IN -451 4 30 Mil 0.20 0.588" 100% 85 IN -483 0 NA 0. 01 .. 0.588" 40%
- 0.05" 0.10" 0.20" 0.30" 0.588" 0.588" 0.588" 0.588" 40%
40% 40% 40%
Page 7 of .7
- 86 IN -482 0 NA 0.50" 1.00" 2.00"
- 0. 20" 0.20" 0.588" 0.588" 0.588" 0.070" 0.130" 40%
40% 40% 40% 40% 87 IN -481 .0 NA 0.20" 0.200" 40%. 0.20" 0.260" 40% 0.20" 0.330" 40% 0.20" 0.460" 40% 0.20" 0.588" 40% 88 IN -480 0 NA 0.20" 0.783" 40% 0.20" 0.979" 40% 0.20" 1.175" 40% 0.20" 1. 763 .. .40% 0.20" 2.355" 40% INITIAL TRIAL SAMPLES 89 IN -452 4 2 Mils 0.20" 0.588" 45% 90 IN -453 4 4 Mils 0.20" 0.588" 45% 91 IN -454 4 6 Mils 0.20" 0.588" 45% 92 IN -455 4 8 Mils 0.20" 0.588" 45% 93 IN -456 4 10 Mils 0.20" 0.588" 45% I 94 IN -457 4 12 Mils 0.20" 0. 588'! 45% I 95 IN -458 4 15 Mils 0.20 0.588" 45%
'96 IN -459 4 20 .Mils 0.20 0.588" 45%
97 IN -460 4 25 Mils 0.20 0.588" 45% 98 IN -461 4 30 Mils 0.20 0.588" 45% 99 IN -478 0 NA 0.20 0.588" 45% 100 IN -479 0 NA 0.20 0.588" 45%
Page 1 - 3
- I. DATA ACQUISITION 3.0 TECHNICAL DESCRIPTION The MIZ-18 Data Acquisition System includes the following components (as described in the Zetec Operating Guides):
1- Hewlett-Packard 9000 series 200, Model 236 (HP9836) or Series 300, Model 310, 320, 330, 350 or 360 computer with:
- 1) External Disc Drive and HPIB cable (if required)
- 1) Mbyte RAM (Random Access Memory) as a minimum recommended
- 1) 2-Channel DMA (Direct Memory Access) Controller
- 1) HP GPIO (General Purpose Input/Output) Interface (Address 12) 1- Zetec Data Cartridge Recorder HCD-75Z
- 1) GPIO Interface Cable (50-pin) 1- Zetec MIZ-18 Remote Data Acquisition Unit (RDAU) with:
- 1) MIZ-18 to HPIB Interface unit
- 1) HPIB cable
- 1) 10' Length of MIZ-18 Remote cable
- 1) ~IZ-18 Probe Adaptor (specific to the probe being used)
The Hewlett-Packard desktop computer is used to control and operate all aspects of data acquisition and recording. This hardware is commercially available from Hewlett-Packard and no modifications are made by Zetec. The Data Cartridge Recorder is based on the 3M, HCD-75 digital cartridge recorder and includes an internal power supply and controller as well as a Zetec-designed interface. The recorder uses 600' PRE-FORMATED. but not necessarily CERTIFIED, data cartridges made by 3M under the brand name Scotch (TM) DC 600HC data cartridge. The data is recorded using 16 tracks, each having 4096 1-Kbyte blocks. This provides for the recording of 67.1 Mbytes of data on one cartridge. The MIZ- 18 RDAU provides all primary tester functions including test frequency generation, coil multiplexing, in-phase and quadrature signal digitization and data communication with the Hewlett-Packard computer. This.unit is contained,within a sealed enclosure to prevent inadvertent contamination of the internal power supply an.d other 0488-010.18B
Page 2 - 3
- electronic circuitry. A single probe adaptor is used to connect various types of *test probes to the remote acquisition unit. The selection of the probe adaptor type depends upon the type of test probe(s) being used. Up to 8 individual test coils, such as an 8-coil pancake array, can be driven.
The computer receives data over a differential IEEE-488 bus thorough the MIZ-18 remote cable, which can be extended to 1000 feet. The MIZ-18 to HPIB Interface Unit, located near the computer, provides the necessary interface between the HPIB interface in the computer and the MIZ-18 RDAU. The MIZ-18 RDAU is an addressable device on this bus as are other components. The last. necessary component of the MIZ-18 Acquisition System is the software system. The System Disc is written to disc in machine language (i.e., compiled form). This system has been developed by Zetec under license to Creative Solutions, Inc. using their 32 bit Multi-FORTH(TM) implementation of FORTH. The System Disc will operate on any properly configured
- Hewlett-Packard Series 200 or Series 300 computer. The computer hardware should meet the requirement listed above.
The MIZ-18 interconnections for a 200 Series computer shall be in accordance with figure 3-1. For a-300 Series computer the interconnections shall be in accordance with figure 3-2. A complete explanation of the system set-up can be obtained from the ZETEC SYSTEM DISC 200/300 SERIES OPERATING GUIDE. II. DATA ANALYSIS The MIZ-18 Data Analysis System includes the following components: 1- Hewlett-Packard 9000 series 200, Model 236 (HP9836) or Series 300, Model 310, 320, 330, 350 or 360 computer with:
- 1) External Disc Drive and HPIB cable (if required)
- 1) Mbyte RAM (Random Access Memory) as a minimum recommended
- 1) 2-Channel DMA (Direct Memory Access) Controller
- 1) HP GPIO (General Purpose Input/Output) Interface (Address 12) 1- Zetec Data Cartridge Recorder HCD-75Z
- 1) GPIO Interface Cable (50-pin) 1- HP ThinkJet Graphics Printer (or equivalent) 04R8-010.18B
Page 3 - 3
- 1- System Disc Software (Edition 18.6, Revision 5.2) 1- MIZ-18 Data Analysis Supplement Software (Edition 18.6 Revision 6) 1- MIZ-18 MRPC Data Display Analysis Supplement Software (Edition 18.6 Revision 13) 1- Eventide Expressway Memory Buffer The Hewlett-Packard desktop computer is used to control and operate all aspects of data analysis. The computer controls the data cartridge recorder and transfers data to and from the recorder through the GPIO interface.
The MIZ-18 Data Analysis System is the software system used for the evaluation of the eddy current data. The Data Analysis System is written as a binary supplement to the System Disc in machine language. The Analysis System will load and operate only* as an extension of the MIZ-18 System. The software package provides the evaluator with the additional functions necessary to evaluate previouly recorded data.* The software design provides for all functions to be controlled through function-key closures on the computer keyboard .
- To operate the MIZ-18 Analysis System requires the use of a Security/Enable module. This serialized module system allows the designated Analysis System to load and operate whenever the module is present on a direct HPIB. bus line form the System Processing Unit. This module system allows the user the ability to copy the Analysis System software for back-up purposes. However, only one Analysis System can be operated per module. *
- The information contained in this section was obtained from the ZETEC, MIZ-18 System Disc, 200/300 Series, Edition 18.6, Revision 5, Operating Guide, Section 3.0 0488-010.18B
MIZ-18 INTERCONNECTICJ'J SQHEMATIC (200 SERIES COMPUTER> CREAR VIEW> PRINTER HPTICNALJ BRUSH RECOOOER CCPTICNAU HP. 9836A CCNPUTER ' AN TO lt<<l CAil..£ Ol'IO CAILE HCO 75Z IOPllJ REMOTE w I
-0 0 000 z ' I I 0 0 IXSl'l.AY ORO CAil..£ DA/8 llPTOl,t,LJ HPIB INTER=ACE ..n-11 Toma lfl8 CAILE C04f'UTER
*O MIX.
. tftl CA&.E MIZ-18 REMOTE T!=STER 1-131 2/l/811
MIZ-16 INTERCOONEC:TIOO SCHEMATIC 1300 SERIES Ca.tPlJTERJ CREAR VIEW> IR.ISH IECOODER llllO 13ea.I C<PfllWU . MCl-ITCR cca..mi DISK DRVE U127 rrr:.~ R 0 I MllCI lf'll CMl.E c) ') DISK ORVE U122 KEYIID. a 11'11 CMl.E EXPANDER 100001 IBCIJE 300 w 0 I N 2999
- 0 0 lll'IO OAll.E DAiii IG'JIHtU MZ-'8 TO lftl CAll..E f'RNTER ICPTOIALI Sf'll (00001 300 HCD 75Z r-_J MIZ-111 l£MOTE TESTER 1-m Z/a/11 w
Page 1 - 4 4.0 TECHNIQUE CONEIGURATIONS I. The following techniques shall be configured as described for these selected examinations: A. BOBBIN H!JMBEF:: 1 SAMPLES per* SEC: 400 1:1k t*lAt-1E--: 5E.*3-SLF FPEQUEHCY SEQUENCE PROBE CHAtiHEL :::ELECT
;+ COIL COIL COIL COIL COIL COIL COIL COIL FF:E1~1JEtKY 1 2 3 4 5 6 7' 8 1 E.(nj kHz Im I I I I I I* l l I I I 2 400 kHz I* I I I I I Im I I I I I 3 100 kHz I *I II I I I Ill I I ~ I I 4 rn kHz IIll I I I I I Im I I I I I tlUMBEP: ~1 SAMPLES per SEC: 400 1:)k t*lAME--: 54(1-SLF I
FF:EG!UENCY SEOIJEHCE PF:OBE CHANNEL SELECT l I COIL COIL COIL COIL COIL COIL COIL COIL
;+ FREC!UEt*lC'r' 1 2 8 4 5 6 7' 8 1 5(n3 kHz I*I I I I I I* I I I I I 2 4t10 kHz I* I I I I I Irm I I I I I 3 u:i.:1 kHz I* I I -I *I I I* I I I I I
!iii 4 rn kHz I *I I I I I I Im I I I I I t4Ut*1E:EP: 2 SAMPLES per SEC: 400 NAME--: 540-SLF.
FREQUHICY SEG!UEt4CE PROBE CHRNMEL SELECT COIL COIL COIL COIL COIL COIL COIL COIL
!I FREQIJEMC'r' l 2 3 4 5 6 7 8 l*I I I I I I111 I I I I I l E.0(1 kHz 2 4(1(1 kHz
*1-1 I I I I I I I I I I
- 100 kHz l*I I I I I I Ill I I I I I l!!I 4 10 kHz I El I I I I I I Ei I I [ I I 0488-010.lBB
Page 2 - 4 A. BOBBIN (Continued) r*IUMBEP: ::: SHMPLES per SEC: 4*;113 ok t*1HME--: 5:30-SF/N(; FF:EG!UEHCY SEG!UEHCE PF~OBE CHHNt~EL 3ELECT COIL COIL COIL COIL COIL COIL COIL COIL
;+ FREG!UENC\'
1 2 ::: 4 ~
~* E. 7' 8 Im I I I Bi I I I 1 b[n} kHz Fr I I I I Im I I I Im I I I I 2 40[1 kHz I I I 100 kHz I I I I I I I I I I 4 rn kHz I Im I I I I I Im I I I I I B. 4C4F
- NUMBER: 4
~IHME--: 4C4F FF:EQIJEHC'l 3H!UEt-ICE
;+ FREG!UENC\'
COIL 1 COI'L 2
- RMF'LE3 per 3EC: 400 COIL 3
F'F~OBE COIL 4 CHHNNEL 3ELECT COIL 5 E. ok Cf.ilL COIL 7 COIL 3 1 E.1)(1 kHz
*I I I I I I I I 2 400 kHz 111 I I I I I I I I
- 3 100 kHz
*I I I I I I I I
!Ei 4 10 kHz Ill I I I I I I I I 0488-010.18B
Page 3 - 4
- c. 8Xl NUMBER: 5 NHME--: 8~-::1 FREG!UENC'r' SEG!IJENCE SRt1PLES per SEC: 400 PROBE CHRNNEL SELECT ok COIL COIL COIL COIL COIL COIL COIL COIL
;+ FREC!UEMC'l 1 2 ::: 4 ~*
6 7 8 13 1 30(1 kHz Im I I I
- Im I I* Im I Im I I I
- I Bi I I I I I I I I I Eli I 2 300 kHz 3 10(1 kHz I I I I I I I* I I IE I I I 4 100 kHz [ Im I I I l I I* I E
I I I D. MRPC
- NIJMBEP: 5 t*lRME--: MRPC FREOUEHCY SEC!UEt-lCE
;+ FREC!IJEMCY COIL COIL SRMPLES per SEC: 400 PROBE CHRMNEL SELECT COIL COIL COIL COIL e.
ok COIL COIL
., 4 1 2 3 5 7 8
- 1 400 kHz I I I I I I I I I I I 2 200 kHz IEl -
I I I I I I I I I I s HX1 kHz I *m I I I
- I I I I I I I 4 10 kHz I I I *I I I I II I I 0488-010.18B
Page 4 - 4 E. AXIAL ROTATIONAL (Defect & Sleeve)
~llJMBEF.:: 7 3RMF'LES per SEC: 400 1:1k t*lP.ME--: R>(IRL F.:OTO FREOUEHC'i :::EG!UHlCE PROBE CHRHHEL SELECT COIL COIL COIL COIL COIL COIL COIL COIL
;+ FRE1;iUEHC'r' k 1 II I
40[1 kHz I~ 1 I I 2 I 3 I 4 I I 5 I 6 I I I 7 I 8 I 2 2(1[i kHz I Em I _J I I I I I I I I I
- 3 100 kHz Ie I I I I I I I I I I I 4 10 kHz I ES I I I I I I I I I ml I I F. CROSSWOUND (Sleeve)
- HUMBER: t:
t~AME--: X-~JOLH~D FRE1)1JEHCY SEG!UEt-lCE COIL COIL Sf:IMPLES per SEC: 400 PROBE CHRHHEL SELECT COIL COIL COIL COIL
*~k COIL COIL
;+ FREQUEHC'r' 1 2 8 4 5 6 .
., ~
C*
~1 ~:o kHz
*I I I *I I Ill I Im I I
*I I* I I
*I I .1 E I I 2 rn0 kHz
- 40~3 kHz
*I I I I I 1111 I I I I 4 60(1 kHz
- I I I* I I Ill I I* I I 0488-010.18B
Page 1 - 5 5.0 TEC.Hlil.Q!lE_aEEQIEI.ra I. BOBBIN COIL All bobbin coil examinations shall be configured in the same manner. The 600 Khz (ch-1 & 2) shall be utilized to provide the high frequency I.D. suppression channels. The optimum frequency channel (ch-3 & 4) shall be operated at 400 Khz. A 100 Khz frequency shall be established (ch-5 & 6) to provide for an anti-support mix and also a ch-3,1,5,7 "NEW MIX" that incorporates a 10 Khz frequency (ch-7 & 8) that will also be used as a support locator channel. The data shall be collected with the use of a Zetec 4-D probe pusher. The probe retraction speed shall be between 12" and 14" per second. The retraction speed shall not exceed 14" per second. Each run shall be recorded and the tube identified by its appropriate serial number. The complete sample matrix of tubes shall be examined five times with each individual probe. This process shall be repeated five. times with each probe (5 different probes). The probe serial number shall be recorded on the summary form for each reel of data collected. A sample of the summary form is provided in figure 5.1 II. 4C4F The configuration for the 4C4F examination shall be identical to the Bobbin coil examination with the exception of no absolute channels. The channels will provide the same function for the 4C4F as they*do for the Bobbin examinations. The data shall be collected with the use of a Zetec 4-D probe pusher. For the initial trial samples the data shall be collected at two different speeds. The first set shall be collected at a retraction speed of 6" per second. The second set shall be collected at a retraction speed of between 12" and 14" per second. A determination will then be made to determine the most effective retraction speed for this technique. All subsequent data for this technique will then be collected at that speed. It shall be noted on the summary form at what speed the applicable data was recorded. The complete sample matrix of tubes shall be examined five
- times with each individual probe. This process shall be repeated five times with each probe (5 different probes).
probe serial number shall be recorded on the summary form for each* reel of data collected. A sample of the. summary form is The 0488-010.18B
Page 2 - 5 provided in figure 5.1 . III. 8Xl The configuration for the 8Xl technique shall provide a 300 Khz and a 100 Khz channel for each coil. The data shall be collected with the use of a Zetec 4-D probe pusher. For the initial trial samples the data shall. be collected at two different speeds. The first set shall be collected at a retraction speed of 6" per second. The second set shall be collected at a retraction speed of between 12" and 14" per second. A de*termination shall .then be made to determine the most effective retraction speed for this technique. All subsequent data for this technique will then be collected at this determined speed. It shall be noted on the summary form at what speed the applicable data was recorded. The complete sample matrix of tubes shall be examined five times with eacll*tndividual probe. This process shall be repeated five times with each probe (5 different probes). The probe serial number shall be recorded on the summary form for each reel of dat*a collected. A sample of the summary form is provided in figure 5. 1-. IV. MRPC The configuration for the MRPC shall provide an optimum frequency channel that shall be operated at 400 Khz (ch-1). A 200 Khz channel shall be provided (ch-2) as a supporting or alternate defect detection and sizing channel. A 100 Khz channel shall be provided (ch-3) to establish an anti-support (ch-1,3) mix and to aid defect characterization. Channel (ch-4) will be used for the rotational trigger pulse. A 10 Khz channel (ch-5) shall be used as a low frequency locator channel to determine the location of a defect in relation to a support plate structure. The Zetec 4-D probe pusher shall be used to manipulate the motor-body probe which will rotate the MRPC probe head. The probe shall be rotated at a speed of approximately 220 RPM with a nominal retraction speed of 0.2" per second. The operator shall ensure the coil detects the A.S.M.E. 0.052" diameter 100% defect 4 to 6 times during the scan. The* complete sample matrix of tubes shall ~e examined five times with each individual probe. This process shall be 0488-010.18B
Page 3 - 5 repeated five time~ with each probe (5 different probes). The probe serial number shall be recorded on the summary form for each reel of data collected. A sample of the summary form is provided in figure 5.1. V. AXIAL ROTATIONAL The qualification objectives of this technique are twofold. The first objective is to provide assurance that this technique can provide information utilizing the MIZ-18 system that is at least equivalent to the MIZ-12 system. The frequency selections for this examination are the same as those used previously in the analog system. The Zetec 4-D probe pusher shall be used to manipulate the motor-body probe which will rotate an axial wound differential coil probe head, similar in design to the probe head used with the MIZ-12 system. The probe shall be rotated at a speed of approximately 220 RPM with a nominal retraction speed of 0.2" per second. The operator shall ensure the coil detects the A.S.M.E., 0.052" diameter 100% defect 4 to 6 times during the scan .
- The second objective is to determine the ability of this probe to detect and size areas of IGA. To accomplish this task, the same configuration, rotation and retraction speed as the sleeve examination shall be used. The IGA sample matrix of tubes shall be examined with five different probes with five examinations per probe. The probe serial number shall be recorded on the summary form for each reel of data collected.
A sample of the summary form is provided in figure 5.1. VI. CROSSWOUND The crosswound technique is configured to provide information on both the parent tube and tube/sleeve assembly. A 30 Khz frequency is established for use as a locator channel for the transition areas (ch-1 to ch-4). A 100 Khz frequency is used to detect degradation and is a component of selected mixes (ch-5 to ch-8). The 400 Khz frequency is used to detect degradation and is most sensitive to the parent tube (ch-9 t6 ch-12). A 600 Khz frequency is used to detect degradation and is most sensitive to the sleeve (ch-13 to ch-16) . 0488-010.18B
Page 4 - 5 The data shall be collected with the use of a Zetec 4-D probe pusher. The probe retraction speed shall be between 12" and 14" per second. The retraction speed shall not exceed 14" per second. Each run shall be recorded and the tube identified by its appropriate seria~ number. Each sample tube/sleeve assembly shall be examined five times with each probe. A total of three .different probes shall be used. The purpose of this technique evaluation is to determine if any additional benefit can be obtained by utilizing this technique over the axial wound differential rotational examination currently qualified for the installed sleeves at Palisades .
- OWNER PLANT UNIT
. PALISADES MIZ-18 QUAL CHAN 1 2 3 4 FREQ 600 600 400 400 100 100 NA DATE 01/31/89 SPAN 25 40 52 81 36 5 6 96 7
10 34 123 8 10 S/G NA LEG NA ROT 0 329 126 95 319 280 170 170 TAPE NO. 21 TO COIL 5 1 5 1 5 5 OPER. LVLMIKE KIRK I II OPER. LVL I CHAN M-1 M-2 M-3 M-4 M-5 14 15 16 ASME S/N IN-490 FREQ 35 3157 3157 3157 3157 STD S/N IN-493 SPAN 52 13 13 20 10 SIZE 0.7500.D.X0.048 ROT 124 104 107 105 85 MATERIAL INCONEL 600 COIL 1 PROBE TYPE A-580/SLF MFG/LENGTH ZETEC /83 FT MIZ-18 ACQUISITION EDITION 18.6 REV5.2 PROBE EXT: MFG ZETEC TYPE 4-PIN LENGTH 50 FT PROBE SERIAL I 0107120 PROBE SET # 4 REQUIRED PULL SPEED 12IN/SC MIZ-18 SERIAL # 129 CALIBRATION DUE DATE 6-22-89 DEFECT SET WASTAGE QUALIFICATION ANALYST 11 LEVEL DATE _ / _ / _ ANALYST #2 LEVEL DATE _ / _ / _ ANALYST 13 LEVEL DATE _ / _ / _ ANALYST #4STEVE WELLMAN LEVEL III DATE 04/03/89
- SAMPLE
SUMMARY
FORM (FIGURE 5-1)
Page 1 - 6
- ~GUIDELINE FQR ANALYSIS TECHNIQUES I. PURPOSE The purpose of this guideline is to establish uniform practices in setting up the various dent mixes such that desired phase spreads and signal amplitudes can be consistently obtained.
II. BACKGROUND The "New Mix" function employs a mathematical algorithm which enables the user to emulate the phase relationships of the prime frequency channel selected during "Set Mix". The user can vary certain "New Mix" parameters in order to achieve a "best fit" to the prime channel. As mix parameters are adjusted, improvements in desired propertie9 of the resultant mix can generally be achieved only at the expense of reductions in competing properties. Consequently, the process of setting up a particular _'._'New Mix" is inherently one of. optimization involving the balancing of competing objectives. Specifically, the properties of the resultant mix which are to be optimized include overall phase spread, phase spread between ASME flaw depths, ASME flaw signal amplitudes, and dent residual amplitude. The.phase vs. depth relationship of dent mixes cannot, in general, be accurately represented by the curve :f"itting routine of the MIZ-18 analysis software .. Therefore, once an "optional" mix is established the resultant phase vs. depth relationship must be represented through the use of alternative curve fitting techniques. The characteristic curve of a dent mix can be represented by a 3rd order polynomial. Accordingly, a cubic regression curve for the routine has been selected, with the result that a correlation coefficient' at or near unity for all dent mixes, is obtained, when the phase vs. depth values of the 4 ASME flaws between 80% and 20% are used as data points. If, in setting up the various dent mixes, the phase vs. depth relationships for the 80% through 20% ASME flaws are maintained, in accordance with pre-established values, then the curve fit corresponding to those values will apply to each particular mix. In summary, when using "New Mix" an optional dent mix can be established for each.dent magnitude. The phase vs. depth relationship for each mix can be described by a cubic regression for to the 80%, 60%, 40% and 20% ASME flaws. If pre-established phase vs. ASME flaw depth relationships are maintained, each time a mix is setup for a particular dent magnitude, then the curve corresponding to these phases vs.depth relationships will apply. 0389-010.18B
Page 2 - 6
- III. METHOD A. BOBBIN & 4C4F Four radial dent sizes are used in the MIZ-18 qualification; 4 mil, 8 mil, 11 mil and 15 mil. The mixing process for each dent size is given below. NOTE: Due to lift-off effects of the larger dent sizes, the 4c4F mixes are limited to the support mix and the 4 mil dent mix only.
A two frequency mix is used for the support plate mix. The frequencies, channels and order of selection for this mix are as follows: 400 KHZ: CH 3 100 KHZ: CH 5 Mix configuration: 3-5 A four frequency mix is used for each of the dent mixes. The frequencies, channels a-nd--order of selection for each mix are as follows:
- 400 600 100 10 KHz:
KHz: KHz: KHz: CH CH CH CH 3 1 5 7 Mix configuration: 3-1-5-7 The following are suggested mix settings to establish the necessary phase spreads for the individual mixes. Some variation in each setup is permissible provided a signal to noise ratio maintains a better than 1 to 1 is maintained while preserving acceptable phase discrimination between defect responses. All bobbin, 4C4F, MRPC and axial rotational examinations shall use the ASME defect standard to establish the required evaluation curves. The 8Xl
- examination shall use the circumferential groove standard to establish the required evaluation curves. The phase analysis curves shall established for the 8Xl, MRPC and Axial rotational techniques using the curve fit function available in the MIZ-18 DDA-4 analysis software.
- 1. SUPPORT MIX The support suppression shall be accomplished in the normal mix mode. After sup'pressing the support plate, the dent
.Page 3 - 6
- response shall be rotated horizontal, with the initial flaw response down. The mix curve shall be established using the DDA-4 and the 100%, 60%, and 20% ASME defect responses as set points.
- 2. SUPPORT/DENT MIX The combined support/dent mixes shall be accomplished with the use of the "NEW-MIX" function. After calculating the mix coefficients, the defect response of the ASME 81% defect shall* be rotated to 40 degrees with the initial response down. The curve for each mix shall be selected from the attached curve selections. The most appropriate curve should be selected by comparing actual known ASME defect depths with the published phase vs. depth table.
- 3. SUGGESTED MIXING SEQUENCES
.4_Mi1 Dent (Bobbin & 4c4F) 1-Q@ .ell. ~ ~ 2.Q.% lQ.%
#Saves 3 1 1 1 3 1
#Saves Locations (Nominal) 54-60 18-20 18-20 18-20 60-66 22-24 Amplitude: 2.8 3.7 3.0 2.3 2.4 *5.3 (Typical)
Dent Residual: 0.4 v
!Sf LMil
#Suppressions 1 1
#Suppressed 50 50 Locations (Nominal)
Phase: See 4 mil Dent curve.
.6-MiLD.en:t (Bobbin & OPTIONAL with 4c4F) lil~ 2.~ ~
#Saves 1 6 1
- #Save Locations (Nominal) 102-120 *18-20 54-60 18-20 1207130 22-24
Page 4- 6
- Amplitude: 2.4 (Typical)
Dent Residual: 2.8 1.1 v 2.3 1.9 2.2 5.0 l'.S.E. LMil LMil Suppressions: 1 2 2
#Locations 50-54 180-200 180-200 Phase: See 8 Mil Dent Curve.
1.l__M1~nt (Bobbin)
.8ll 2.Q.~ l~
#Saves 1 8 1
#Save Locations 160-170 18-20 54-60 18-20 160-170 20-24 (Nominal)
Amplitude 1. 2 1. 6 1. 3 1.1 1. 4 3.0 (Typical) Dent Residual: 1.0 v (Typic.al) Iaf 4 Mil .6.._Mil l l Mil
.Suppressions 1 1 1 2
#Suppressed Locations 50-54 120-130 120-130 Phase: See 11 Mil Dent Curve 15 Mi~nt. (Bobbin) l~ .8ll
#Saves 9 1
#Save Locations 180 20 120 20 180-198 22 (Nominal)
Amplitude 1.2 1.5 1. 6 1.5 1.8 3.8 (Typical) Dent Residual 0.8 v Taf .LMil LMil l.LMil lli_Mil
* * #Suppressions: 1 1 1 1 3 0389-010.lBB
Page 5 - 6
- #Suppressed Location's (Nominal) 54 70-80 70-80 70-80 210-240 Phase: See 15 Mil Dent curve NOTE: Use attached "New Mix/Data Analysis Curve Parametric Study Form" to keep track of Saves and Suppressions.
- 4. PROCEDURE (BOBBIN & 4C4F)
- a. Set Mix 1: 400-100 Standard Support Mix Rotation: 4 Mil dent horizontal, up and to left.
Set curve
- b. Set Mix 2: 4 mil dent per ~ethod Rotation: 81% at 40
- c. Set Mix 3: 8 mil dent per method Rotation: 81% at 40°
- d. Set Mix 4: 11 mil dent per method Rotation: 81% at 40°
- e. Set Mix 5: 15 mil dent per method Rotation: 81% at 40°
- f. *Setup CH 3, 400 Khz (1) Rotation: 100% at 40° (2) Set volts: 5 v p-p on 20%
(3) Save/Store to all channels (4) Set curve (5) Store variables
- g. Add Data (1) ASME 100/81/60/42/20/10/TSP Using CH-3 (400 KHz)
(2) 15m/llm/8m/4m dents using Mix 1
- h. Final Report For each of the dent mixes, Mix 2 - Mix 5, measure and report the following data:
(1) Dent residual :Q.=.12 max. volts.record as "RES" in% column (2) Dump Graphics (3) 100%/81/60/42/20/10 flaws (a) Use appropriate Mix curve to evaluate depth. (b) Dump Graphics 0389-010.lBB
Page 6 - 6
- B. (8X1)
The 8X1 technique is functionally 8 separate pancake coils connected in the absolute mode. The circumferential groove calibration standard shall be used for establishing a phase analysis curve for the 300 Khz channels (CH-1 through CH-8). The 300 Khz channels shall be used for flaw sizing utilizing the channel with the greatest amplitude response for phase measurement. A support mix shall be established, combining the 300/100 Khz channels. This mix shall only be used when the primary 300 Khz is not interpretable.
- 1. PROCEDURE (BXl)
- a. Setup CH-1 through CH-8 (1) Rotation: Set probe motion horizontal (2) Set Volts: 5 v p-p on 100%
(3) Save/Store to all channels (4) Set degree curve on CH-1 through CH-8 (5) Store variables
- b. Setup CH-9 through CH-16 (1) Rotation: Set probe motion horizontal (2) Set Volts: 5 v p-p on 100%
(3) Save/Store to all channels (4) {OPTIONAL} Set degree curve on CH-9 through CH-16 This shall. be use for confirmation only. (5) Store variables
- c. Add Data (1) 100%/80/60/40/20 using CH-1 (300 Khz)
- d. Final Report For.the 300 Khz channel (CH-1 through CH-8) which registers the maximum response, measure and. report the following data:
(1) 100%/80/60/40/20 circumferential flaws on calibration standard. (2) Report depth of each flaw (3) On the final report, indicate the number of coils that responded to the defect. This number should be recorded in the extent area of the final report. (4) Dump graphics on reportable indications.
- c. {MRPC)
The MRPC technique utilizes the ASME calibration standard as the setup standard. A nqrmal support mix shall be established using a 400/100 Khz mix. The area sizing, using the clip plot function on the DDA-4, shall be calibrated using the 0.052" diameter through wall.hole. 0389-010.lBB
Page 7 _ 6
- 1.
- PROCEDURE
- a. Setup CH-1 through CH-3 (1) Rotation: Set probe motion horizontal (2) Set Volts: 5 v p-p on the greatest amplitude signal response from the 100% defect.
(3) Save/Store all channels * (4) Establish a degree curve for CH-1 and CH-2 using the p-p measurement. (5) Store variables
- b. Add Data (1) ASME 100%i81/60/42/20/10 using CH-1 (400 Khz)
- c. Final Report (1) ASME 100%/81/60/42/20/10 using CH-1 (400 Khz)
(2) Dump Graphics ASME (3) .Defects-report depth and in extent column report axial and circumferential dimensions. (Example: 125x455) D. (AXIAL ROTATIONAL) The Axial Rotational technique utilizes the ASME calibrations standard as the setup standard. A support plate mix shall be established using the 400/100 Khz channels.
- 1. "PROCEDURE
- a. Setup CH-1 through CH-4
( 1 ). Rotation: Set probe motion .horizontal (2) Set volts: 5 v p-p on 20% (3) Save/Store to all channels (4) Set Curve for CH-1 400 Khz (5) {OPTIONAL} Set Curve for CH-2 & 3 (200 & 100 Khz) (6) Store variables
- b. Add Data (1) ASME 100%/81/60/42/20/10 using CH-1 (400 Khz)
- c. Final Report .
(1) ASME 100%/81/60/42/20/10 using CH-1 (400 Khz) (2) Dump Graphics (3) Reportable indications (4) Dump Graphics 0389-010.lBB
Page 8 - 6
- IV. REPORTING CRITERIA A. Final Report Header UNT MIZ-18 Qualification ANL J. Doe Level II A DAT Mo/Day/Year REL Reel #
DSK (Reel#) .1 (. 2, . 3, etc.) DEF Wastage/Circumferential/IGA PRB 580SLF/MRPC/Axial, etc. B. End a disk with "END" in % Column. C. Flaw Evaluations (1) 1 entry per area, in sequence e.g. Area A, Area B, Area C, etc. (2) Quantifiable Indications Manually enter values if determined from mixes 2-5; otherwise use "Set curve" . (3) Non-quantifiable defects. if flaw is present but non-quantifiable d~e to ambiguous phase, record as. "NQD." NOTE: A best effort m~ be made to quantify. (Use NQD ~s a last resort) (4) No Flaw Indications Enter as "ND" at appropriate location. (5) Flaw Measurement In general, use Max. Rate function (6) Graphics Dump Graphics for each f.l.aH reported: Upper Graphics: Calling Channel Lower Graphics: Mix #1 0389-010.lBB
Curve 1 Page 1 of 27 PALISADES: 4 M!L DENT MlX - 580 BOBB!N 111l0 9121 80 - I '*., 70 I *...
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Curve 2 Page 2 of 27
- 100 912:1 PALISADES:
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.Page 3 of 27
- 100 9121 PALISADES: 8 M!L DENT MIX - 560 BOBBIN 81<!
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Curve 4 Page 4 of 27
- .. me 9121 PALJSADES: 11 MtL DENT MlX - 580 BOBBlN 80 -
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Curve 5 Page 5 of 27
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Curve 6 Page 6 of 27
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Curve 7 Page 7 of 27
- 100 9121 PALlSADE:3:
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Curve 8 Page 8 of 27
- 100 9121 PALISADES: l 1 HIL DENT MI){ - 580 BOBBIN sr 4 80
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Curve 9 Page 9 of 21 PAL!SAOE:3: 8 MrL DENI M!X - 580 BOBB!N ST 4 me I I 90 l I I I 80 I - I I I
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Curve 10 Page 10 of 27
- rn0 Siil PAL!SADES: 8 M[L DENT MIX - 588 BOBBIN ST 2 80
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Curve 11 Page 11 of 2'[
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Curve 12 Page l2 of 21 PAUSADES: l 1 MIL DENT Ml){ - 580 BOBBIN ST 2 rn0 9t:I 80 - \
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Curve 13 Page 13 of 27
- 80 PALISADES: 8 MtL DENT MIX -
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- 37 82 57 68 77 57 97 47 117 32 137 8 18
- 38 82 58 68 78 57 98 46 118 31 138 7 19
- 39 82 59 67 79 56 99 45 119 30 139 5
Curve 14 Page 14 of ~'I PALlSADES: 8 MI:L DENT MlX - 580 BOBBlN ST 2 1El0 9111 80 70 60 50 --- 40 30 20 0 '---"-~-------~........~-------~~~...___..~_._~....__._~--~-------- \ 0 10 20 30 40 50 .i::0 70 :30 90 100 1 l0 120 130 140 150 160
~-; THROUGH WALL l/S, PHASE ANGLE (DE:GF!E:ES)
I
Curve 15 Page 15 of 27
Curve 16 Page 16 of 27
- 100 9121 80 PALISADES: 4 MI:L DENT MIX - 580 BOBBlN ST 4
\ .....
*.\
'\
70 ~ 60 50 I I I l I I I I I '*-*--. k,. . l I l l I I I I 40 *-....... 30 20 ', 10 ~
\\
0 \ 0 10 20 30 40 50 60 70 80 90 1B0 110 120 lSB 140 150 160
% THROUGH WALL VS. PHASE ANGLE 1DEGREES)
I
- 0 0
1
% 0 20 21 41 (I) 40 81 80 60 61 0
63 62 80 81 0 50 50
% 0 100
. 101 39 39
% 0 120 121 27 26
% 0 140 141 9
8 2
- 22
- 42 79 62 62 82 49 102 38 122 25 142 7 3
- 23
- 43 78 63 61 83 49 103 38 123 25 143 6 4
- 24
- 44 77 64 60 84 48 104 37 124 24 144 5 5
- 25
- 45 76 65 59 85 47 105 36 125 23 145 4 6
- 26
- 46 75 66 59 86 47 106 36 126 22 146 3 7
- 27
- 47 74 67 58 87 46 107 35 127 21 147 2 8
- 28
- 48 73 68 57 88 46 108 35 128 21 148 0 9
- 29
- 49 72 69 57 89 45 109 34 129 20 10
- 30
- 50 71 70 56 90 45 110 33 130 19 11
- 31 .
- 51 70 71 56 91 44 111 33 131 18 12
- 32
- 52 69 72 55 92 44 112 32 132 17 13
- 33
- 53 69 73 54 93 43 113 32 133 16 14
- 34
- 54 68 74 54 94 43 114 31 134 15 15
- 35
- 55 67 75 53 95 42 115 30 135 14 16
- 36 82 56 66 76 53 96 41 116 30 136 13 17
- 37 82 57 65 77 52 97 41 117 29 137 12 18
- 38 82 58 65 78 51 98 40 118 28 138 11 19
- 39 82 59 64 79 51 99 40 119 27 139 10
Curve 17 Page 17 of 27
- PALISADES: 8 H!L DENT MlX - 580 BOBBIN sr 2 60 l---l-~-1--+-l----+-~+----'~-!-""'"-+--+~-+-~+--+~-+-~+---+------1
** (1) 18 20 30 (1) .,
40 50 r/J E.1]
% THROUGH l~ALL VS.
f<:; 70 130 (1) % 90 100 110 120 lSB PHASE ANGLE (DEGREES) (1) % r/J 140 150 0 160 I lo (1) % 0
- 20
- 40 61 60 69 80 S8 100 4S 120 31 140 12 1 21
- 41 80 61 68 81 S7 101 4S i 21 30 141 11 2 .
22 *
?-
42 80 52 68 82 S7 102 44 1.,........, 29 142 10
.1..,.
3 . .J 79 63 67 83 S6 103 43 ' ... .., 28 143 9
... :J
- 1 ri7 4
- 24
- 44 78 64 67 84 SS 104 43 124 27 144 8 s
- 2S
- 4S 7E 6S 66 85 55 105 42 125 27 145 7 6 .. 26
- 46 77 66 66 86 54 106 41 126 26 146 5 7
- 27 82 47 ... ~
{ { 67 65 87 54 107 41 127 25 147 4 8
- 28 82 48 76 68 64 88 53 108 40 128 24 148 3 9
- 29 82 49 75 69 64 89 52 109 39 129 23 149 2 10
- 30 82 S0 75 70 63 90 52 110 38 130 22 1S0 1 11 31 82 Sl 74 71 63 91 Sl 111 38 131 21 151 0 12 .
32 82 S2 74 72 62 92 51 112 37 132 20 13
- 33 82 S3 73 73 62 93 S0 113 36 133 19 14 .. 34 82 S4 72 74 61 94 49 114 36 134 18 15 35 82 SS 72 7S 61 9S 49 115 35 135 17 16 36 82 S6 r'
..,, 76 60 96 48 116 34 136 16 17
- 37 82 S7 {' 77 S9 97 47 117 33 137 15 18
- 38 82 58 70 78 S9 98 47 118 32 138 14 19
- 39 82 S9 70 79 58 99 46 119 32 139 13
Curve 18 Page 18 of 27 PALISADES: ll MIL DENT MIX - 580 BOBBIN ST 2 lC0 912! 80
~
I I I
"-*.......... I 70 I 68 I -..
50 *.. 48 I I *- ..... 38 II Il I
! I ' **-.
I *.._ 20 I I I I I *. I II I ........ I I i r* .. 30 I *........ 0 I i I I I I \. E1 18 *21] ~:(j 4i'1 SE* E-0 70 88 98 lflE1 l 313 120 l3B 140 150 380
~ THROUGH W~LL VS. PHASE ANGLE (DEGF!EES'.l I
- Ql 0
- 1 3
.,,, Ql 20
- 21 22
- 23
- 40 41 42 43 l/J 81 80 79 78 60 61 62 63 l/J 64 63 63 62
.,/o 80 81 82 9*3 (1) 52 52 51 51 100 101 102 103 0
42 42 41 41 120 121 122 123 0 31 31 30 29
% Ql 140 141 142 143
*15 14 13 12 4
- 24
- 44 77 64 61 84 50 104 40 124 29 144 11 5
- 25 .. 45 76 65 61 8S S0 10S 40 12S 28 145 10 6 + 26 .. 46 75 66 60 86 49 106 39 126 .,~
.:. I 146 9 7 27 .. 47 74 67 S9 87 49 107 39 127 26 147 8 8 ..* 28 .. 48 73 68 S9 88 48 108 38 128 26 148 7 9 + 29 .. 49 72 69 SB 89 48 109 38 129 2S 149 6 10 .. 30 82 S0 72 70 58 90 47 110 37 130 24 1S0 4 11
- 31 82 51 71 71 57 91 47 111 37 131 -
....:. ;) 151 3 12
- 32 82 52 70 72 S6 92 46 112 36 132 22 1S2 2 13 + 33 82 S3 69 73 S6 93 46 113 36 133 22 1S3 14
- 34 82 S4 68 74 SS 94 45 114 3S 134 21 154 0 15
- 3S 82 SS 68 7S 5S 95 45 115 34 135 20 16 .. 36 82 .. S6 67 76 S4 96 44 116 34 136 19 17 . 37 92 S7 66 77 S4 97 44 117 33 137 18 18
- 38 82 S8 6S 78 S3 98 43 118 33 138 17 19 + 39 82 S9 65 79 S3 99 43 119 ;).:,. 139 16
Curve 19 Page 19 of 27 PALISADES: B M!L DENT MIX - 588 BOBBIN ST 2 HlEl 9121 I 8121 - I 70 I .. I 88 50 I I
**...**~..
48 \ ..***, 38 I ********.. I *J 28 I I I
.1 I *..
i I ...... I 10 0 I I '* 8 10 20 3E1 48 58 E0 0 7[1 138 98 100 110 120 l80 148 150 160
~~ THF.:*'.lLIGH l~ALL VS. PHASE ANGLE .:DEGREES)
I
- (1) 0 1
lo 20
- 21 22 *
(1) 40 41 42 0 81 81 80 lo 60 61 62 (1) 71 71 70 80 81 82 Q) 59 58 57 r. 100 101 102 Q) 43 43 42
- i. Q) 120 28 121 *27 122 26
- r. Q) 140 141 142 r.
12 12 11 2 3 ..* .,-
.:. :i .. 43 80 63 70 83 56 103 41 123 25 143 10 4
- 24
- 44 79 64 69 84 56 104 40 124 24 144 9 5 .. 25 .. 45 79 65 69 85 55 105 40 125 24 145 9 6 .. 26 .. 46 79 66 68 86 54 106 39 126 23 146 8 7
- 27 .. 47 78 67 67 87 53 107 38 127 22 147 7 8
- 28
- 48 78 68 67 88 53 108 37 128 21 148 7 9
- 29 .. . 49 77 69 66 89 52 109 36 129 21 149 6 10
- 30 82 50 77 70 65 90 51 110 36 130 20 150 5 11 .. 31 82 51 76 71 65 91 50 111 35 131 19 151 5 12 32 82 52 76 72 64 92 50 112 34 132 18 152 4 13 .* 33 82 53 75 73 63 93 49 113 33 133 18 153 3 14
- 34 82 54 75 74 6"3 94 48 114 32 134 17 154 3 15 35 82 55 74 75 62 95 47 115 -?
- i~ 135 16 155 2 16
- 36 82 56 74 76 61 96 47 116 31 136 15 156 1 17
- 37 82 57 73 77 61 97 46 117 30 137 15 157 1 18
- 38 82 58 73 78 60 98 45 118 29 138 14 158 0 19
- 39 82 59 72 79 59 99 44 119 28 139 13
Page 21 of' 27
- I I'll!!
91!1 PAL!SADES: 4C4F RNALYS!S CURVE *1 I
/ I"--... **- **........
8til i I ~"-. f"-._ __ 7til I
,./ ...,*~.....
80 ', 50 I ...,*....~ 40 i
/ '*
\
30
/
I \ \.
\\
I \ 20 10 l
/ \
\
I
/ \
(!I 0 10 20 30 40 50 80 70 80 :30 100 110 120 130 140 150 160 170
~' THROUGH WALL VS. PHASE ANGLE rnEGF!EESl I
0 % 0 i. 0 % 0 % 0 % 0 % 0 % 0 % 0 0 23 58 46 95 . 69 82 92 74 115 64 138 47 161 18 3 24 60 47 95 70 82 93 73 116 63 139 46 162 16
.:. 5 25 63 48 94 71 82 94 73 117 63 140 45 163 14 3 8 26 65 49 93 72 81 95 73 118 62 141 44 164 13 4 10 27 68 50 92 T3 81 96 72 119 61 142 43 165 11 5 13 28 70 51 92 74 80 97 72 120 61 143 42 166 9 6 15 29 73 52 91 75 80 98 71 121 60 144 41 167 8 7 18 30 75 53 91 76 80 99 71 1°22 59 145 40 168 6 8 20 31 78 54 90 77 79 100 71 123 59 146 38 169 4 9 23 3,2 80 55 89 78 79 101 70 124 58 147 37 170 2 10 25 33 83 56 89 79 78 102 70 125 S7 148 36 171 0 11 28 34 85 S7 88 80 78 103 69 126 S7 149 35 12 30 35 88 58 88 81 78 104 69 127 S6 150 34 13 33 36 90 S9 87 82 77 105 68 128 SS 151 32 14 35 37 93 60 87 83 77 106 68 129 SS 152 31 1S 38 38 9S 61 86 84 77 107 68 130 S4 153 30 16 40 39 98 62 86 8S 76 108 67 131 S3 1S4 28 17 43 40 99 63 8S 86 76 109 67 132 52 lSS 27 18 45 41 99 64 8S 87 75 110 66 133 Sl 1S6 2S 19 48 42 98 6S 84 88 75 111 66 134 S0 157 24 20 S0 43 98 66 84 89 7S 112 6S 13S S0 1S8 22
- 21 22 53 5S 44 4S 97 96 67 68 83 83 90 74 91 74 113 114 6S 64 136 137 49 48 1S9 160 21 19
Page 22 of 27
- H!ll!l 9t!I Bta I
/
I PALISADES: 4C4F" ANALYSIS CURl/E *2
'- ~
7~ I "'*-, 60 I ~... 50 I .............
\ .....
I l 40 30 .t
/ \.'*
\
\
,' \
20 \ I
'\
10
/ \
/ \
!!J
/ \
0 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 1B0 170
- -; THROUGH WALL VS. PHASE ANGLE (DEGREES)
I 0 % 0 % 0 % 0 % 0 % 0 % 0 % 0 % 0 0 23 58 46 96 69 85 92 75 115 63 138 44 161 16 3 24 60 47 96 70 85 93 7*5 116 62 139 43 162 14 2 5 25 63 48 95 71 84 94 74 '17 61 140 42 163 13 3 8 26 65 49 95 72 84 95 74 118 61 141 41 164 11 4 10 27 68 50 94 73 83 96 73 119 60 142 40 165 9 5 13 28 70 51 94 74 83 97 73 120 59 143 39 166 8 6 15 29 73 52 93 75 83 98 72 121 59 144 38 167 6 7 18 30 75 53 93 76 82 99 72 122 58 145 37 168 4 8 20 31 78 54 92 '77 82 100 71 123 57 146 36 169 3 9 23 32 80 55 92 78 81 101 71 . 124 56 147 34 170 1 10 25 33 83 56 91 79 81 102 70 125 56 148 33 171 0 11 28 34 85 57 91 80 80 103 70 126 55 149 32 12 30 35 88 58 90 81 80 104 69 127 54 150 31 13 33 36 90 59 90* 82 80 105 69 128 53 151 29 14 35 37 93 60 89 83 79 106 68 129 52. 152 28 15 38 38 95 61 89 84 79 107 68 130 52 153 27 16 40 39 98 62 88 85 78 108 67 131 51 154 26 17 43 40 99 63 88 86 78 109 66 132 50 155 24 18 45 41 ,99 64 87 87 77 110 66 133 49 156 23 19 48 42 99 65 87 88 77 111 65 134 48 157 21 20 50 .43 98 66 86 89 77 112 65 135 47 158 20 21 53 44 98 67 86 90 76 113 64 136 46 159 19 2*2 55 45 97 68 86 91 76 114 63 137 45 160 17
P.age 23 of 27
- 11!10 9 C!I 81il J
/
*PALISADES: 4C4r RNALYStS CURVE *3
/
\ .............,
~
7t11 I -...., 6!3 I -.......
~-
50 I ..___
~'-
-'-\
40 I '\._ 30 I "' ~. J ..... 20
\,
10
/ \
l!J
/*
0 10 20 30 40 50 60 70 80 90 100 l10 l20 130 140 150 160 170
% THROUGH WALL VS. PHASE ANGLE (DEGREES)
I 0 % 0 % 0 % 0 % 0 % 0 % 0 % 0 % 0 0 25 63 S0 94 75 81 100 69 . 125 56 150 37 175 9 3 26 6S SI 93 76 80 101 69 126 SS 151 36 176* 7
..,"- 5 27 68 52 92 77 80 102 68 127 54 152 35 177 6 3 8 28 70 S3 92 78 79 103 68 128 54 153 34 178 5 4 10 29 73 S4 91 79 79 104 67 129 53 154 33 179 3 5 13 30 7S S5 91 80 78 10S 67 130 S2 155 32 180 0 6 15 31 78 S6 90 81 78 106 66 131 52 156 31 7 18 32 80 S7 90 B2 77 107 66 132 51 157 30 8 20 33 83 58 89 83 77 108 6S 133 50 158 29 9 23 34 85 59 BB B4 76 109 65 134 50 159 28 10 25 35 8B 60 BB .as 76 110 64 135 49 160 27 11 28 36 90 61 87 86 76 111 64 136 48 161 26 12 30 37 93 62 87 87 75 112 63 137 48 162 25 13 33 38 9S 63 86 BB 7S 113 63 138 47 163 24 14 3S 39 98 64 B6 89 74 114 62 139 46 164 22 15 38 40 99 65 85 90 74 115 62 140 45 165 21 16 40 41 99 66 85 91 73 116 61 141 44 166 20 17 43 42 99 67 84 92 73 117 60 142 44 167 19 18 45 43 98 68 84 93 72 118 60 143 43 168 18 19 48 44 97 69 83 94 72 119 S9 144 42 169 16 20 50 45 97 70 83 95 71 120 S9 145 41 170 lS 21 S3 46 96 71 82 96 71 121 58. 146 40 171 14 22 55 47 95 72 82 97 71 122 SB 147 39 172 13 23 58 4B 95 73 82 98 70 123 57 148 39 173 11 24 60 49 94 74 81 99 70 124 S'S 149 38 174 10
P_age 24 of 27
- ll!ll!!
91!1 8111 I
/
r ,,,_ PALISADES: 4C4F" ANALYSIS CURl/E *4 7111 60 I '"" --,. ~- 50
/
I 40
/ i\'\
\
I\ 30 J \
/
\
\
20
\
I \ \*
\I 10
/ '*
I r\
\\
10 20 30 40 50 60 70 80 80 100 110 120 130 140 150 160 170 Y. THROUGH WALL VS. PHASE ANGLE (DEGREES) I
- (1) 0 0
4 (1) 20 21 74 78 40 41 (1) 92 91 0 60 61 81 81 80 81 0 71 71
% 0 100 101 58 57
% (1) 120 121 39 38
% (1) 140 11 141 9 2 7 3 ,, 22 23 81 85 42 43 91 90 62 63 80 80 82 83 70 69 102 103 56 55 122 123 36 35 142 7 143 5 4 15 24 89 44 90 64 79 84 69 104 55 124 34 144 4 5 19 25 93 45 89 65 79 85 68 105 54 125 33 145 .,'-
6 22 26 96 46 88 66 .78 86 68 106 53 126 31 .146 0 7 26 27 99 47 88 67 78 87 67 107 52 12( 30 8 30 28 99 48 87 68 77 88 66 108 51 128 29 9 33 29 99 49 87 69 77 89 66 109 50 129 27 10 37 30 98 50 86 70 76 90 65 110 49 130 26 11 41 31 97 51 86 . 71 76 91 64 111 48 131 25 12 44 32 97 52 85 72 75 92 64 112 47 1-.,
- ,,_ 23 13 48 33 96 53 85 73 75 93 63 113 46 133 22 14 52 34 95 54 84 74 74 94 62 114 45 134 20 15 56 35 95 SS 84 75 74 95 62 115 44 135 19 16 59 ,..._
36 94 56 83 76 73 96 61 116 43 136 17 17 tl .;J 37 94 57 83 77 73 97 60 117 42 137 16 18 67 38 93 58 82 78 72 98 59 118 41 138 14 1g 70 39 92 59 82 79 72 99 59 119 40 139 12
Page 25 of 27
- 11!11!1 912!
PALISADES: 4G4F ANALYSIS CURVE *5 81il I ............ 70 I -., 60 / ""*.,.
' ...\ . ,...
50 I "\ I \ ... 40 *-.*, 30 j \
\,
J l I I \ 20 I 10 I 1'
\.,*,
\
\
\
10 20 30 40 50 80 70 80 80 100 ~10 l20 l30 140 150 160 170
% THROUGH WALL VS. PHASE ANGLE (DEGREES)
I 0 % 0 % 0 % 0 % 0 % 0 % 0 % 0 % 0 0 20 gs 40 87 60 74 80 61 100 45 120 26 140 1 . 5 21 99 41 86 61 74 81 60 101 44 121 25 141 0 2 10 22 9g 42 86 62 73 82 59 102 43 122 23 14 3 23 99 43 85 63 72 83 59 103 43 123 i..i:.. 4 19 24 g8 44 84 64 72 84 58 104 42 124 21 5 24 25 97 45 84 65 71 85 57 105 41 125 20 6 29 26 96 46 83 66 70 86 56 106 40 126 19 ( 33 27 96 47 82 67 70 87 56 107 39 127 18 8 38 28 gs 48 82 68 69 88 55 108 38 128 16 g 43 29 94 49 81 69 68 89 54 109 37 129 15 10 48 30 g4 50 81 70 68 90 53 110 36 130 14 11 52 31 g3 51 80 71 67 91 53 111 35 131 13 12 57 32 92 52 79 72 66 g2 52 112 34 132 11 13 62 33 92 53 79 73 66 93 51 113 33 . 133 10 14 67 34 91 54 78 74 65 94 50 114 32 134 g 15 71 35 90 55 77 75 64 95 49 115 31 135 8 16 76 36 90 56 77 76 64 96 49 116' 30 136 6 17 81 37 89 57 76 77 63 97 48 117 29 137 5 18 86 38 88 58 75 7,8 62 98 47 118 28 138 3 1g 90 39 88 59 75 7;g 62 99 46 11 9 27 139 2
Page 26 of 27
- l l!l El 91:!1 8111
/
t ~,'*,.... PALISADES: 4G4F ANALYSts CURVE *6
............,a i--,
**r-_
7[;':(
"""' r~
60 Ii '--.... l 1\-.. 50 '* 40 I \\ J
"\\
30 *. 2[1 I \\
\
1 E) I
/ \ ..
i\ I \ ti
\
0 l0 20 30 40 50 60 ?0 80 80 l00 1l0 120 130 l40 150 180 170 180 l90
~-. THROUGH WALL l/S, PHASE ANGLE (DEGREES)
I
- (2) 0 2
0. 4 8 25 26 27 (2) % 96 99 99 50 51 52 (2) 86 85 85 75 76 77 (2) 77 77 77
% (2) 100 101 102 71 70 70
% r/J 125 126 127 62 62 61 150 (2) 151 152 47 46 45
% (2) 175 176 177 21 20 18 3 12 28 98 53 84 78 76 103 70 128 61 153 45 178 17 4 15 29 98 54 84 79 76 104 70 "129 60 154 44 179 16 5 19 30 97 55 84 80 76 105 69 130 60 155 43 180 14 6 23 31 96 56 83 81 76 106 69 131 59 156 42 181 13 7 27 32 96 57 83 82 75 107 69 132 59 157 41 182 11 8 31 33 95 58 82 83 75 108 68 133 58 158 40 183 10 9 35 34 94 59 82 84 75 109 68 134 58 159 39 184 8 10 38 35 94 60 82 85 75 110 68 135 57 160 38 185 7 11 42 36 93 61 81 86 74 111 67 136 57 161 37 186 5 12 46 37 92 62 81 87 74 112 67 137 56 162 36 187 4 13 50 38 92 63 81 88 74 113 67 138 55 163 35 188 2 14 54 39 91 64 80 89 74 114 66 139 55 164 34 189 0 15 58 40 91 65 80 90 73 115 66 140 54 165 33 16 62 41 90 66 80 91 73 116 66 141 54 166 32 17 65 42 90 67 79 92 73 117 65 142 53 167 31 18 69 43 89 68 79 93 73 118 65 143 52 168 30 19 73 44 89 69 79 94 72 119 65 144 52 169 29 20 77 45 88 70 79 95 72 120 64 145 51 170 27 21 81 46 88 71 78 96 72 121 64 146 50 171 26
- 22 23 24 85 88 92 47 48 49 87 87 86 72 78 73 78 74 77 97 98 99 72 71 71 122 123 124 63 63 63 147 148 149 49 49 48 172 173 174 25 24 22
Page 27 of 27
- PALISADES: 4C4F RNALYsrs CURVE *7 911l
/'\* ""-
I -,~' 8lil
/
71il I ~ ...... 60 I
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50 ,, I I'-\.
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40 I '\,
- 30 "
20 I [\\
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- l!J 0
0 10 20 30 0 40 Y. i. 50 0 60 70 80 THROUGH WALL VS. PHASE ANGLE (DEGREES) 0 90 100 110 120 130 140 150 160 170 0 % 0 % 0 I
% 0 i.
Q) Q) 23 92 46 84 69 73 92 65 115 56 138 41 161 16 4 24 96 47 83 70 72 93 64 116 55 139 40 162 14
,;. 8 25 99 48 83 71 72 94 64 117 SS 140 39 163 13 3 12 26 99 49 82 72 72 9S 64 118 S4 141 38 164 11 4 16 27 98 S0 81 73 71 96 63 119 S3 142 37 16S 10 5 20 28 98 51 81 74 71 97 63 120 S3 143 36 166 8 6 24 29 97 52 80 7S 71 98 63 121 S2 144 3S 167 7 7 28 30 96 53 80 76 70 99 62 122 S2 145 34 168 s 8 32 31 9S 54 79 77 70 100 62 123 Sl 146 33 169 4 9 36 32 94 SS 79 78 69 101 62 124 51 147 32 170 2 10 40 33 93 S6 78 79 69 102 61 12S 50 148 31 171 0 11 44 34 92 S7 78 80 69 103 61 126 49 149 30 12 48 3S 91 58 77 81 68 104 60 127 49 150 29 13 52 36 91 59 77 82 68 105 60 128 48 151 28 14 56 37 90 60 76 83 68 106 60 129 47 152 27 15 60 38 89 61 76 84 67 107 59 130 47 153 26 16 64 39 88 62 76 85 67 108 59 131 46 154 ZS 17 68 40 88 63 75 86 67 109 58 132 45 155 23 18 72 41 87 64 75 87 66 110 58 133 45 156 22
- 1g 20 21 76 80 84 88 42 43 44 45 86 86 85 84 65 66 67 68 74 74 73 73 88 89 90 65 91 65 66 66 111 112 113 114 57 57 56 56 134 135 136 137 44 43 42 41 157 158 159 160 21 20 18 17
Page 1 - 7
- I. PURPOSE The following information will describe the findings relating to the specific techniques used in this qualification. This section provides general information in regards to the set-ups and analysis techniques that were ultimately used in the evaluation of the tube samples for the known types of degradation present in the Palisades steam generators.
II. 580 BOBBIN This technique was. initially developed to use a frequency configuration of 800-Khz, 400-Khz, 100-Khz and 10-Khz in both the differential and absolute mode. The initial probe design was a mid-range probe which did not operate satisfactorily at the 800-Khz. These probes were then replaced with a high range probe. This provided an adequate response at the highe~ frequencies but the 100-Khz and 10-Khz channels were not acceptable. Because of this limitation, created by the large frequency range employed, it was necessary to reduce the upper frequency to bring it within the operating range of the mid-range probe. A comparison study was conducted to determine if 600-Khz would provide a sufficiently high frequency to allow for an I. D.
- suppression mix for the denting. This comparison indicated that the ability to suppress the denting was as good with the 600-Khz as with the 800-Khz. This change in-the configuration allowed for the use of a mid-range probe that would give* acceptable characteristics on all of the selected frequencies.
The development of the mixing parameters was found to be best optimized by applying various weighting factors to. the flaw responses on the A.S.M.E. standard and the dent responses. By applying more saves to the 100%, 60% and 20% defect responses than to the other remaining defects, optimization of the phase spread is achieved for the range of A.S.M.E. defects. The number of suppressions that are applied to the support and dent responses also affected this phase spread. A parametric study was conducted to determine the optimum mixing sequence of these parameters to provide the best signal to noise ratio for a given dent size. The outcome of this study is reflected in section 6.0 of this report. NOTE: Attachment-7A of this section contains data from the study. During the development of these mixing techniques, it became apparent that the curve fit routines provided in the Zetec MIZ-18 analysis software were not adequate for developing the correlation curves necessary for this evaluation. Thus, a series of 20 curves. were developed providing a range of correlation curves from which to selecte the qurve which best represented the actual phase/depth relationship. This provided a much improved 0889-001
Page 2 - 7
- accuracy over the curves generated by the MIZ-18 software.
Zetec system currently provides for a 3-point fit curve. When this is utilized calibrating on the 100%, 60% and 20% A.S.M.E. defects, the 80% and the 40% defects do not fall on the curve The line . . It became apparent that a higher order curve fit would provide greater accuracy when attempting to measure defects in this range of depths. Thus a 4 or 5-point cubic regression curve fit was utilized to establish the correlation curves. The MIZ-18 bobbin techniques provided results exceeding the capabilities of the MIZ-12 bobbin technique currently used at Palisades. The MIZ-18 bobbin techniques improved the signal to noise ratio over the analog MIZ-12 system, with the detectability of defect indications in dented regions remaining acceptably consistent in dents from 0-10 mils of radial compression, depending upon the volume of the individual defect. In dented regions above 10 mils radial compression, the ability to consistently detect and quantify the defect areas deteriorates rapidly. A complete statical analysis of the abilities of this technique is provided in section 8.0 of this report. The evaluation of the data indicates that a signal to noise ratio of L 1:1 should be maintained to consistently quantify defect indications. Figure 7-1 and 7-2 provides an example of a defect response. in relation to the residual from the combined support/dent response.
- CH 8 VERT + - CH E. VERT + CHANNEL NO -- MIX+I 2 ST 4 IH- 170 RUt~ 1 XY DISPLi:IY CHANii-==-M"T CHAHS -- *~H-5-7 SPl=IH ----- 2E*
ROTATIO~l - 10E. DEG
) LEFT STRIP CHART cHfiNii-::--3'1----
FREQ ----- 400 kHz SPl=IH ----- 52 ROrnTION - 12E. DEG
- l~
.. J~..;;=;.*""'.**~*~==Jr .................. .
RIGHT STRIP CHART
-cHfiNii-::--1/___ _
FREO ----- 100 kHz
....._1~==-*,--J 1---,,-..,..,,-.,..,.,,.,..-:-:---,,..,,...-,=----=-=""'"""' SPAN -----
59~: l .>. **.** ~~:r~r~!Q~
- 2. 42 VOLTS 6(1 DEG ROTATION - 280 DEG LOC D + 0.0 1
\ -~* COIL*
r
'-----.~~---====I < FREI;) 1 2 8 4 5 E. 7 8
> E.(10 2 4L)(j .* 4 I l HKI E.
! t 10 8
- 0889-001 (DEFECT RESPONSE)
FIGURE 7-1
Page 3 - 7
- - CH ::;:
,~I
\.'Ef':T + - CH S \IERT + CHAt~HEL
~
~ :<:*\
MCI -- Mli<:I+ 2 ST 4 Hl- 170 RUM
~::'*( DI SF'LA'r' CHRNi-::-r:;-2 CHAMS -- :?.-1-5-7 SPAM ----- 25 T
ROTRTI OM - 105 DEG
. LEFT STRIP CHART
\:*-'~\_c;;---; cHi"it.ii-::-~311----
FREQ ----- 400 kHz
*-t.7 '~\ / SPAM -----
- ~~t ~------
1 c:=)............
---==='"'_L..:..:..:..:..
DENT RESIDUAL'"....*................... FREQ 1 2 3 4 5 5 7 8 500 2
~
l 10 8 (SUPPORT/DENT RESIDUAL) FIGURE 7-2
- This indication has a signal to noise ratio of 1.07:1. Thus, the ability to differentiate between the defect indication and the residual noise is within the acceptable ratio. It should be noted the volume of the affected area of the defect directly influences the response to the defect verses the residual of the support/dent mix residual. It is quite possible to have a low volume defect with significant depth.in an area of major denting that would not maintain a ratio of 21:1:
ability to detect and quantify the defect would depend upon the In these areas, the particular geometry of the defect in relation to the support and associated dent and their resultant effect upon the defect signal. The mixing capabilities of the "New-Mix" function incorporated in the DDA-4 software were demonstrated to be repeatable for the selected dent sizes. This mixing technique is *superior to the older mixing concepts used in the MIZ-12 system for two reasons: 1.) The final analysis set-up of the MIZ-12 analog system was dependant upon the calibration of the acquisition system being extremely precise in the phase and gain settings of each frequency module. If these parameters varied from one set-up to another, some fluctuation in the final. analysis signal calibration was experienced. With the MIZ-18 digital system, the final analysis calibration is not dependent upon the phase and gain settings during acquisition. This allows the analyst to
- 6onsistently duplicate the required calibration settings.
0889-001
Page 4 - 7
- 2.) The dynamic range of the MIZ-12 analog system was limited to maximum voltage inputs from the test coil. Thus, once this limit is reached the instrumentation capabilities reach a saturation point and the signal response becomes invalid until the signal voltage comes back within the range of the instrumentation. This *was a major problem in dented regions when the signal response from the dent would reach the saturation point. With the gain settings used for the MIZ-12 inspections this. would typically occur with dents that exceeded approximately 8 mils of radial compression.
With the MIZ-18 digital system, this limitation for all practical purposes is not relevant. The dynamic range of the MIZ-18 system far exceeds the signal voltage ranges from the test coil, thus it does not reach a point of instrumentation saturation. This does not necessarily mean that detectability of defect indications can be achieved in areas of extreme denting. The signal to noise ratio criteria will still apply when evaluating these areas. The 580 bobbin provided acceptable results on wastage, pit and IGA type defects. The ability to quantify these defects can be related back to an acceptable signal to noise ratio. This acceptable ratio was primarily dependant upon the size of the dent involved and the orientation of the defect to the dent. The bobbin coil did not provide acceptable results on the circumferential (simulated crack) samples. This results from the eddy current field generated by the bobbin probe being oriented in the circumferential plane around the tube wall. Thus, the presence of a circumferentially oriented crack will not significantly interrupt the eddy current field. This will cause minimal impedance-changes between the probe to tube interface of the coil. This finding is consistent with previous studies conducted for Palisades and is also consistent with basic eddy current theory. Section 8.0 of this report will provide specific accuracy ranges and levels of detectability for the defect types that were included in this qualification. III. 560 AND 540 BOBBIN Data was collected with both the 560 and 540 bobbin probes. To minimize the time necessary to evaluate and determine the statistical accuracies of both techniques it, was decided the 540 bobbin would be completed initially. If the 580 and 540 bobbin provided acceptable results, the conclusion could be made that the 560 bobbin would be considered qualified .
- The 540 technique was configured and evaluated identically to the 580 bobbin. The findings of this qualification indicate the 540 bobbin probe will perform acceptably. The .findings as stated 0889-001
Page 5 - 7
- above for the 580 bobbin were determined to be applicable to the 540 bobbin.
A slight increase in the overall mean difference in the eddy current reported indications and also a comparable increase in the standard deviation for the overall population of the defects was observed. This would indicate the technique of preference for the bobbin examination would be the .580" diameter probe followed by the .560" and then the .540" diameter. During recent eddy current examinations in the Palisades Steam Generators a sample of approximately 400 tubes were examined using the 0.580" diameter probe. It was determined at that time the 580-SLF probe design could be implemented without a significant number of tubes being blocked by denting. The approach that will be taken for the in-service bobbin examination will be to inspect all required tubes initially with the 580-SLF and to down size to the 560-SLF and then the 540-SLF as required. If the tube will not pass the 0.540" diameter probe, it will be considered blocked. IV. NARROW GROOVE BOBBIN COIL AND 540 280-Khz SLOW PULL After discussions with Zetec and other industry personnel familiar with the application of the narrow groove bobbin coil, it was determined that its application for Palisades was not relevant. This technique was designed for the detection of small pit type defects and not volumetric wastage that is typical of the degradation at Palisades. It has been the experience at Palisades that this pitting condition is not present in the 1 operating steam generators. This has been substantiated by pulled tube.results from as recent as 1984. For this. reasons it was determined the narrow groove bobbin would be dropped from this qualification program. The 540 280-Khz examination was developed to determine if the position of the sleeve had moved in relation to the parent tube defect. In addition, the qualification was also to determine the optimum frequency for detection of the parent tube flaw and phase spread for defect quantification. The initial qualification was performed in 1980 (
Reference:
Consumers Power Co., NDT Services project number 80001-N). The transition to the MIZ-18 does not alter any of the original parameters of the examination, only the method of collection. For this reason it was determined that the 540 280 Khz technique could be implemented using the MIZ-18 system without.further qualification.
- v. 4C4F The same problems arose with the selection of test frequencies and *establishing correlation curves with the 4C4F as with the bobbin examinations. The test coils did not operate well at the 800-Khz, thus a 600-Khz was used as the high frequency
* *suppression channel. A comparison of the resultant mixes 0889-001
Page 6 - 7
- indicated no appreciable difference between using the 800-Khz verses the 600-Khz. The test system was configured using only the differential mode with frequency selections of 600-Khz, 400-Khz, 100-.Khz and 10-Khz. These frequencies were combined to perform a support elimination mix (Mix~l) and a support/dent mix (Mix-2). It was initially thought that additional support/dent mixes would be required depending upon the severity of the denting. However, this was not the case. It became evident the increase in voltage displacement that occurred when the severity of the dent increased was minimal from 4 mils through 10 mils of radial compression. Thus, one dent mix was sufficient to accommodate this range of denting. This resulted from the surface riding capabilities of the' probe design which maintains the minimum amount of lift-off on the probe coils. With dents
> 10 mils the coil voltage response increased rapidly with small increases in dent size. Because of this large voltage increase above 10 mils it was determined that additional mixes would not
*provide.any_additional benefit. A selection of of seven correlation curves, using a 5 point cubic regression curve fit routine was established for the correlation curves.
The probe retraction speed was* evaluated to determine if it would be possible to pull the probe at 12 inches per second verses 6 inches per second. The result of this study indicated the noise level of the probe increased significantly due to the probe chatter at the higher speed. Consequently, the 6 inches per. second pull rate was used. *
- The ability of the 4C4F technique.to consistently quantify volumetric -conditions- is dependent upon "the circumferential
~xtent of the defect. If the defec~ is not of sufficient circumferential extent to cover a minimum of two coil sets, it is probable that each pull of the probe will result in a slightly different signal response. This is due to the orientation of the pancake coil to a slightly different portion of the defect. This limitation is compounded by the complexity of the signal response that is displayed to the analyst. Because of the probe design, the signal response will not react to defect indications in the same manner as the differential bobbin coil probes. With a bobbin coil, the phase is adjusted to cause the phase change of a defect signal to initially move in the down direction. With the 4C4F probe design it is possible for the defect to pass between the leading set of coils, which normally produces the initial response, without being detected thus no initial downward excursion to the signal response would be present. The trailing set of co.ils would then detect the defect with the signal
- displaying an upward excursion only. This type of response is not characteristic of normal defect response. When this is combined with the overall noise level of the surface riding probe, the signal response can become extremely complex and
- inconsistent. An example of this type of problem is shown in figure 7-3 and 7-4. As can be seen by the example,* a significant phase .shift has occurred between the two examinations of the same defect.
0889-001 With figure 7~3 the defect was detected with the leading
Page 7 - 7
- set of coils and the initial excursion is in the downward direction. However, in figure 7-4 the same defect is detected only with the trailing set of coils causing the response to the defect to move in the upward direction which is not characteristic of defect responses from differential probes.
When these indications are combined with the effects of support plates, dents and conductive deposits, it can be extremely difficult to differentiate between these signal responses to determine what is and is not a defect.
- CH 2 VERT + - CH 4 HORZ + CH>MNEL NO -- 2 ST 1 IN- 186 RUN 999 XY DI SPLA'1' CHi'.iN*-::--f-FREQ ----- 400 kHz SPAN ----- 40 ROTATI OH - 334 DEG LEFT STRIP CHAF:T EHi'.it:l*-::--2v-----
FREo ----- 400 kHz SPAt-i ----- 4(1 ROTATION - 3:?.4 DEG I-- RIGHT STRIP CHART
-CHAN*-::--4H" ___ _
- 4. 4 7 VOL TS 44 DEG FREQ -----
1--__,.....,..,,,..,..,.="'""'==-__,..,....,~---,..,,..,,i SPAN ----- DEFECT ROTl=ITI ON - 10 kHz 29 0 DEG RSME 79!~ + 0. 00 S~'STEM COHFIGURATiot' t-iif11"E----_--4c:4-(-r;u-Ar--
..................................... *>*......... II *;)~* CHA~l- 4
~ 6:24:58 PM FE8RUl=IRY 9 1989
................................. ) .......... FREQ 1 2 1;(1(1 1
- iC~l§\ 7 8 100 3 10 4 FIGURE 7-3
- CH 2 VERT + - CH 4 HORZ + CHAHNEL HO -- 2 ST 1 IH- 186 RUN 999
>~Y DISPLAY cHi'.iN*-==--a-FREQ ----- 400 kHz SPAN ----- 40 1-==l ROTATION -
LEFT STRIP CHART 334 DEG cHAN*-::--2;---- FREo ----- 400 kHz SPAl' ----- 40 ROTATION - 384 DEG 1--
.......................... .. RIGHT STRIP CHART 1--
~
-cHi'.iN*-::--.rH" ___ _
FRE1;i ----- 10 kHz 1--------~~--=="" SPAH ----- 29
- 4. 24 . VOL TS 59 DEG DEFECT ROTAT I OH - 0 DEG ASME 7*3~,; + 0. 00
.....................................* ........ .. 4+ of' CHAN- 4
' 6:28:05 PM FE8RUARV 9 1989
.......................................................... f.......... FREQ 1 2 3 4 5 6 7 8 1-"~;::;;g'*g"""-'"'1!-+-!-+-+-i-+--1 I! '"--'1~0~0+.:=<3~_._-l-+-1-4-~
10 4 FIGURE 7-4
Page 8 - 7
- For volumetric defect conditions of varying geometries the consistency of the 4C4F technique is not as good as the standard bobbin coil techniques. This is defined in section 8.0 of this report which describes the statistical accuracies of the 4C4F technique in relation to the other techniques employed in this qualification.
The detection of circumferential (crack) defects with the 4C4F technique was consistent with the qualification for the MIZ-12 system. The technique provides a reliable detectability beginning at approximately 50% of wall. The ability of the 4C4F probe to detect circumferential cracks over the bobbin techniques is due to the orientation of the eddy current fields in relation to the defect.
- The surf ace riding pancake coil creates a circular field around the coil that is sensitive to circumferential indications which will interrupt the eddy current flow. The classification of the defect signal response as a crack indicati.on is based upon the response time of the indication. The'crack indications are of extremely short duration which causes a fast rise time on the signal response.
- The amplitude is related to the number of coils affected. Figure 7-5 is a typical response to a circumferential crack.indication .
- - CH M 2 VERT+ - CH 4 VERT + CHRNt*lEL NO -- MIX* 2 ST 3 IH- 211 RUN
>:'r' DISPLAY CHANi-==11-2 4
CHANS --*2-1-3-4 SPA~l ----- 22 ROTATION - 340 DEG LEFT STRIP CHi:lRT CHANi-::11-2'1--- CHANs -- 2-1-3-4 SPAI~ ----- 22
-=-- ROTATION - 340 DEG Ril3HT STRIP CHi:lRT
-cHANi-::--4V----
FREa ----- 1(1 kHz 1--,--:=:=-.,.,.,,,.~-.=-:=-...,...~ SPRN ----- 80
- 1. 27 \IOL TS 55 DEG CRACK ROTfiTI ot~ - 1133 DEG LOC B + 0. 0
- of' CHAN- 4 10:55:05 PM FEBRUARY 10 1989 COIL*
FREQ 1 2 3 4 5 6 7 8 600
- FIGURE 7-5 0889-001
Page 9 - 7
- VI. 8X1 The design of the 8X1 probe is similar to that of the 4C4F in the construction of the probe head. The difference being the configuration of the coils. The 8X1 has 8 separate absolute coils utilizing an external reference. This design had an improved signal to noise ratio over the 4C4F and the interpretability of the data was much improved over the 4C4F.
The sixteen channels of data acquisition allowed for a support m~x to be preformed for each coil, which minimized the influence of the support plates. The capabilities and limitations of the 8Xl were similar to the 4C4F technique. The same principles apply to the 8Xl as the 4C4F in the ability to size volumetric defects that are of. limited circumferential extent. The individual pancake coils may respond to a slightly different portion of the defect from one inspection to the next with no actual change in the defect. It is possible to approximate the circumferential extent of the defect by determining the number of affected coils. Figure 7-6 illustrates that only one coil set has detected the first. four defects in this t.ube sample. Thus, it can be estimated that the affected areas of these four defects are less than 45 degrees on the circumference . DISF'Li:IY II -- 0 i:l.S.M.E. + 0.0 ST 1 IN- 186 RLIH 999 1 2 3 4 CHll- 1\I CHll- 2V CHll- 3\1 CHll- 4\1 FIGURE 7-6 0889-001
Page 10 - 7
- The statistical analysis indicated a tendency to undercall the depth of the volumetric defect areas and overca.11 the crack indications. This was dependent upon the specific type of defect and the volume of the affected area. A complete statistical analysis of the technique is provided in section 8.0 of this report.
A limitation of this technique is the inability to adequately suppress the horizontal effects of a dent. The response to dents are minimized by the surface riding capabilities of the probe and the fact that each coil responds independently to the dent. The geometry of the defect in relation to the dent is the determining factor in the ability to interpret the indication. The probe retraction speed w*as evaluated to determine if it would be possible to pull the probe at 12 inches per second verses 6 inches per second. The result of this study indicated the noise level of* the probe increased significantly due to the probe chatter at the higher speed. Consequently, the 6 inches per second pull rate was used. The ability of the 8X1 to detect and characterize circumferential crack indications was improved over the 4C4F technique. The level of detectability is approximately 35% through-wall in areas of denting ~ 10 mils of radial compression. Above this denting level the consistency of detectability is undetermined due to the lack of available tube samples. The ability to characterize the crack indications is very similar to the 4C4F technique. A typical crack response is very short in time duration with minimal lobe opening to the signal response. Figure 7-7 is a typical crack response.
- CH 2 VERT + - CH 10 VERT + CHRNNEL HO -- MIX* 3 ST l IH- 205 RUN 2 I'
J XY DISPLRV CHANi-==-ff-3 CHRHS -- 2-10 SPRN ----- 8~)0 ROTRTIOt~ - 2E.9 DEG
- L_
LEFT STRIP CHRRT CHAf:ii-::--2';---- FREQ ----- 810 kHz
-r- SPAt~ ----- 100
{ ROTRTI ml - 252 DEG r RIGHT STRIP CHRRT
-CHANi-==~f0i7 ____
FREQ ----- 100 kHz 1----------~.,,..,.,-1 SPRH -----
\
50 CRACK ROTRTIOH - 121 DEG LOC D + 0.0 S'i'STEM CONFIGURATIOH H"R"M'E--_-:..-3x:-c-o-u-R"C--
- of CHRH- 1E.
9:04:05 RM MRF~CH 1 1989 COIL+I FREQ 1 2 3 4 5 6 7 8 8(U31~ :3 4 301 5E.78 rn0 '3 1B ~ 1 2
*********** ********** * ************ ........... 101 t1:3 4 tt.5 *. nE.
FIGURE 7-7 0889-001
Page ll - 7
- The 8X1 technique provides no additional advantages over the bobbin coil for detection and quantification of volumetric defect
*conditions, i.e. wastage, pitting and IGA. It does, however, of fer some advantages over other techniques for the detection of circumferential cracking conditions. The improved detectability over the 4C4F would indicate the 8Xl to be the examination of choice for the cracking conditions at Palisades. It also allows some advantages for consistency in interpretation of the eddy current data. The 8X1 signal response is much less complicated than the 4C4F technique which reduce the possibility of an incorrect evaluation of a defect signal. Based upon these findings,* the 8Xl technique should be used to supplement the bobbin examination and to replace the 4C4F for the purpose of circumferential crack detection. The statstical analysis of this technique is provided in section 8.0 of this report.
VII. MOTORIZED ROTATING PANCAKE (MRPC) The qualification of this technique was intended to be an extension of a qualification that was initiated in 1987. The objective of this previous qualification was to determine the ability to detect and quantify A.S.M.E. type defects. It was concluded that the technique was equivalent to a previously qualified technique using a pancake probe with a rotating probe pusher. The intent of the present qualification was to further determine the MRPC capabilities in a wider range of defect types and configurations. To fully evaluate this technique; it was determined the present.qualification.would not base any results upon the previous data. This would keep the MRPC data consistent with the other techniques evaluated in this qualification. The *MRPC technique provided better detection of volumetric defects in dented regions than any of the other techniques employed in this qualification. A major area of emphasis for this technique was to determine the detectability of defects .in dented regions when the denting levels exceeded the capabilities of the pull through examinations. The technique was found to be capable of detecting all types of volumetric defects through the complete range of dent samples. These samples included dents
~ 30 mils of diametrical compression. Although the statistical analysis was not complete for this data set at the time of this report, the approximate level of detectability is in the range of 30% to 40%. No approximation of the ability to quantify the flaw depths has been made at this time. Upon completion of the statistical analysis, this report shall be revised to include the accuracies of MRPC technique.
The MRPC technique utilizes a rotating pancake coil inserted into the tube I.D. and rotated at approximately 220 rpm with a nominal pull speed of 0.2" per second. This results in a helical scan of the.tube wall. The signal is then displayed in a C-Scan presentation which can be utilized for defect characterization. 0889-001
Page 12 - 7
- The C-Scan display plots the amplitude of the signal response in relation to the circumferential and axial position of the defect in the tube. This p~ovides a 3-dimensional view of the defect which can be use to characterize the defect according to orientation in the tube and the amount of area affected. Figure 7-8 provides an example of a volumetric wastage defect located just above the support plate. Figure 7-9 is an example of a pit type defect located within the support plate and associated with a dent. Figure 7-10 is a crack type indication with minimal axial extent.
- CH M 2 VERT+ CHAt*lt*lEL tlO -- MIX!! 2 ST 2 Itl- 311 RUt4 CH!=!~l* -- M 2 CHHHS -- 2-3 SF'Ht*l ----- %0 ROTHTI ot4 - 1 DEG
-0 .. 87
+0.87 Mi=!l<: VOL TS '34. 2 l=l>~IAL PITCH ~:9 CIRC PITCH 29 Z ROTATiot4 295
;x; F~OTi:iTI OH 65
- OF SCAHS PO I HTS/SCHt4 43 B0 FIGURE 7-8 WASTAGE DEFECT 0889-001
13 - 7
- I
- CH M 2 VERT+ ST 2 rn- 317 RUH CHRt*HI -- M 2 CHRt*J::: -- 2-8 SPRN ----- 120 E
~
ROTRTION - DEG
~
-1.01 iI J
....... ~~'3~,!!!!j I
+1. 01 MRX VOL TS 11. 7 R~U RL PITCH 4(1 CIRC PITCH 29 2 ROTRTiot~ 296
- ~ ROTRTJot-l 5E.
- OF SCRt*IS PO I t-ITS/SCRt~
49 82
- - CH M 2 VERT+
FIGURE 7-9 PIT TYPE DEFECT CHRNl4EL NO -- MIX* 1 ST 2 IN- 205 RUN CHRN* -- 11 CHRt4S -- 1-8 SPRH ----- 12(1 ROTRTI O~I - 255 DEG
+0.80 MRX VOLTS 11.7 AXIRL PITCH 89 CIRC PITCH 29 2 ROTATION 121 X ROTRTION 52
- OF SCRNS PO ItffS/SCAt4 3'3 81
- 0889:...001 FIGURE 7-10 CRACK TYPE DEFECT
Page 14 - 7
- VIII. ROTATIONAL AXIAL WOUND DIFFERENTIAL The statistical analysis of this technique is not complete as of this date. Upon completion of the analysis the conclusions for this technique will be finalized.
0889-001
ATTACHMENT 7-A Page 1 of 27 PLANT UNIT S/G LEG REEL TO REEL DATE
- MIZ-18 QUAL ST IN- RUN VOLTS DEG
[" NA NA
'* CH# LOCATION LINT ANL NA MIZ-18 QUALIFICATION B. CURTIS II I 11 11 01/30/89 EXTENT DAT 3/01/89 REL #*11 MIZ18 QUAL PRB 580 SLF OSK lS NEW.MIX/DATA ANALYSIS CURVE PARAMETRIC STUDY ANALYSIS CURVE VALUES OF ASME FLAWS AND 107. OD GROOVE FOR CH3<400KHZ> AND MIX1(STANDARD 400/100>
WHERE CURVES ARE ESTABLISHED USING SP1=100, SP2=60, AND SP3=20. 1 490 999 7.68 40 99 3 1007.ASME+ 0.00 5.93 83 76 3 81% ASME+ 0.00 6~12 109 59 3 60%ASME + 0.00 4.90 133 39 3 427. ASME+ 0.00 5.00 153 20 3 . 20% ASME+ 0.00 8.98 149 24 . 3 10%GROOV+
- 0. 00 1 490 999 8.39 30 100 M 1007.ASME+ 0.00 6.05 66 77 M 81% ASME+ 0.00 5.68 87 60 M 607.ASME + 0.00 3.97 105 42 M 42% ASME+ 0.00 3.30 122 21 M 207. ASME+ 0.00 5.83 115 30 M 10%GROOV+ 0.00 RUN 1 : 400-600-100 WITH 1 SAVE ON EACH ASME STD FLAW AND 1 SUPPRESSION ON TSP & 4MIL ONT l 490 999 0.38 247 RES M 2 4M DENT+ 0. 00 (RES IDUAU 490 999 ..,
M <.. CURVE 1: SP1=100;SPZ=60;SP3=20 1.95 39 100 M 2 100%ASME+ 0.00 2.55 40 97 M 2 81% ASME+ 0.00 2.44 63 60 M 2 607.ASME + 0.00
- 1. 90 93 32 M 2 42% ASME+ 0.00 1.86 114 20 M 2 207. ASME+ 0.00 4.06 120 <20 M 2 10%GROOV+ 0.00 M2 CURVE 2: SP1=81;SP2=60;SP3=20 2.55 40 81 M 2 81% ASME+ 0.00 2.44 63 59 M 2 60%ASME + 0.00
- 1. 90 93 35 M 2 42% ASME+ 0.00 1.86
"+
- IUCI 114 20 M 2 120 <20 M 2 207. ASME+ 0.00 10%GROOV+ 0.00 M ....<.. CURVE ::J; SP 1-'-81*; SP2-42; SP3-.:20
..,<.. ,;:)"+ ,,..,... ... ,....
40' OJ
" M 2 0 I /o n;:>J"IC:.T e.00 I"\ .. * ,
- 2. 45 ,...
- 62 67 M 2 oiu r.n;:inc:.n*1,..,...
\U. VJ\U LEVEL
Page 2 of 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG 490 999 UNIT NA 7.
S/G NA LEG NA CH# LOCATION
- 1. 90 93 42 M 2 427. ASME+ 0.00 REEL TO REEL 11 11 DATE 01/30/89 EXTENT 1.87 113 21 M 2 20% ASME+ 0.00 4.06 120 <20 M 2 10%GROOV+ 0.00 M ., CURVE 4:SP1=80;5P2=60;5P3=42 2.55 40 81 M 2 817. ASME+ 0.00 2.44 62 60 M 2 607.ASME + 0.00
- 1. 90 92 42 M 2 427. ASME+ 0.00 1.85 114 33 M 2 207. ASME+ 0.00 4.05 119 31 M 2 107.GROOV+ 0.00 M 2 CURVE 5:SP1=60;SP2=42;SP3=20 2.44 62 60 M 2 607.ASME + 0.00
- 1. 90 92 42 M 2 427. ASME+ 0.00 1.85 114 20 M 2 207. ASME+ 0.00 4.05 11 g <20 M 2 107.GROOV+ 0.00 RUN 2: SAME AS RUN 1 EXCEPT 2 SAVES ON 207. FLAW 1 490 999 0.35 257 RES M 3 4M DENT+ 0 . 00 <RES ID UAL l M3 CURVE 1: SP1=100;SP2=60;SP3=20 2.07 39 97 M 3 1007.ASME+ 0.00
- 2.69 40 100 M 3 2.56 63 60 M 3 2.02 95 31 M 3 2.01 115 20 M 3 4.36 120 <20 M 3 M3 817. ASME+ 0.00 607.ASME + 0.00 427. ASME+ 0.00 207. ASME+ 0.00 107.GROOV+ 0.00 CURVE 2: SP1=81;SP2=60;SP3=20 2.69 40 81 M 3 817. ASME+ 0.00 2.56 63 60 M 3 607.ASME + 0.00 2.02 95 34 M 3 42% ASME+ 0.00 2.01 115 20 M 3 20% ASME+ 0.00 4.36 120 <20 M 3 107.GROOV+ 0.00 M3 CURVE 3: SP1=81;SP2=42;SP3=20 2.69 40 Bl M 3 81% ASME+ 0.00 2.56 63 67 M 3 607.ASME + 0.00 2.02 95 42 M*3 427. ASME+ 0.00 2.01 115 20 M 3 207. ASME+ 0.00 4.36 120 <20 M 3 107.GROOV+ 0.00 M3 CURVE 4: SP1=81;SP2=60;SP3=42 2.69 40 81 M 3 817. ASME+ 0.00 2.56 64 60 M 3 607.ASME + 0.00 2.02 95 42 M 3 427. ASME+ 0.00 2.01 115 33 M 3 207. ASME+ 0.00 4.36 120 31 M 3 107.GROOV+ 0.00 M3 CURVE 5: SP1=60;SP2=42;SP3=20 2.56 64 60 M 3 607.ASME + 0.00 2.02 95 42 M 3 42% ASME+ 0.00
- 2.01 115 20 M 3 20% ASME+ 0.00 LEVEL
Page 3 of 27 PLANT UNIT SIG LEG REEL TO REEL DATE MIZ-18 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG 7. CH# LOCATION EXTENT 490 999 RUN 3: SAME AS RUN 1 EXCEPT 3 SAVES ON 207. FLAW 490 999 0.45 242 RES M 4 4M DENT+ 0. 00 . 490 999 M4 CURVE 1 :SP1=100;SP2=60;SP3=20 2.37 40 100 M 4. 1007.ASME+ 0.00
- 3. 09 40 100 M4 81X ASME+ 0.00 2.91 64 60 M4 607.ASME + 0.00 2.31 96 31 M4 427. ASME+ 0.00 2.34 117 20 M4 207. ASME+ 0.00 5.10 122 <20 M4 107.GROOV+ 0.00 M4 CURVE 2: SP1=81;SP2=60;SP3=20 3.09 40 81 M4 817. ASME+ 0.02
- 2. 91 64 60 M4 607.ASME + 0.00 2.31 96 34 M4 42% ASME+ 0. 00 2.34 117 20 M4 207. ASME+ 0.00 5.10 122 <20 M4 107.GROOV+ 0.00 M4 CURVE 3:SP1=81 ;SP2=42;SP3=20 3.10 40 80 M4 817. ASME+ 0.00 2.92 65 66 M4 607.ASME + 0.00
- 2.31 96 41 2.34 116 21 5.10 122 <20 3.10 40 2.92 64 81 60 M4 M4 M4 M4 M4 M4 42% ASME+ 0.00 20'% ASME+ 0.00 107.GROOV+ 0.00 CURVE 4:SP1=81 ;SP2=60;SP3=42 81% ASME+ 0.00 607.ASME + 0.00 2.32 96 42 M4 42% ASME+ 0 .00 2.32 117 32 M4 207. ASME+ 0.00 5.10 122 31 M4 107.GROOV+ 0 ..00 M 4 CURVE 5: SP1=60;SP2=42rSP3=20 2.92 64 60 M4 607.ASME + 0.00 2.32 96 42 M4 42% ASME+ 0.00 2.32 117 20 M4 207. ASME+ 0.00 5.10 122 <20 M4 107.GROOV+ 0.00 490 999 RUN 4 SAME AS RUN 1 EXCEPT 6 SAVES ON 20% FLAW' 490 999 0.54 217 RES M 4 4M DENT+ 0.00 490 999 M4 CURVE 1: SP1=100;SP2=60;SP3=20 2.76 40 100 M4 1007.ASME+. 0.00 3.59 40 100 M4 81% ASME+ 0.00 3.39 63 60 M4 607.ASME + 0.00
- 2. 72 96 31 M4 427. ASME+ 0.00 2.81 117 20 M4 20'% ASME+ 0.00 6 .11 122 <20 M4 10%GROOV+ 0.00 M4 CURVE 2: SP1=81 ;SP2=60;SP3=20 3.59 40 81 M 4 Bl'Z ASME+ 0.00 LEVEL
Page 4 of 27
- PLANT
. MIZ-18 QUAL ST IN- RUN VOLTS DEG UNIT NA S/G NA LEG NA CH# LOCATION REEL TO REEL 11 11 DATE 01/30/89 EXTENT 490 999 3.39 63 60 M4 60%ASME + 0.00
- 2. 72 96 34 M4 427. ASME+ 0.00 2.81 117 20 M4 207. ASME+ 0.00
- 6. 11 122 <20 M4 10%GROOV+ 0.00 M4 CURVE 3: SP1=81 ;SP2=42;SP3=20 3.59 40 80 M4 81% ASME+ 0.00 3.39 63 67 M4 60%ASME + 0.00
- 2. 72 96 41 M4 42% ASME+ 0.00 2.81 117 <20 M4 20% ASME+ 0.00 6.11 122 <20 M4 107.GROOV+ 0.00 M4 CURVE 4: SP1=81 ;SP2=60;SP3=42 3.59 40 81 M4 817. ASME+ 0.00 3.39 63 60 M4 607.ASME + 0.00
- 2. 72 96 41 M4 427. ASME+ 0.00 2.81 117 34 M4 207. ASME+ 0.00 6.11 122 32 M4 107.GROOV+ 0.00 M4 CURVE 5: SP1=60;SP2=42;5P3=20 3.39 63 60 M4 607.ASME + 0.00
- 2. 72 96 42 M4 42% ASME+ 0.00 2.81 117 20 M4 207. ASME+ 0.00
- 490 999 6.42 123 <20 0.33 M4 82 RES M S 4M 107.GROOV+ 0.00 RUN S NO SAVE ON 107.GRV11SAVE/SUPPRESSION ELSEWHERE DENT+ 0.00 490 999 MS CURVE 1: 5P1=100;SP2=60;SP3=20 1.60 40 99 M s 1007.ASME+ 0.00 2.00 39 97 M s 81% ASME+ 0.00 1 .81 68 59 M 5 601.ASME + 0.00 1.64 102 28 M 5 427. ASME+ 0.00
- 1. 92 114 20 M 5 207. ASME+ 0.00 4.26 115 <20 M 5 107.GROOV+ 0.00 M*5 CURVE 2: SP1=81;SP2=60;SP3=20 2.00 40 81 M S 817. ASME+ 0.00
- 1. 81 68 60 M S 60%ASME + 0.00 1.64 103 30 M 5 427. ASME+ 0.00
- 1. 92 115 20 M 5 207. ASME+ 0.00 4.26 116 <20 M S 10%GROOV+ 0.00 MS CURVE 3: SP1=81 ;SP2=421SP3=20 2.00 40 81 M 5 817. ASME+ 0.00 1.81 68 70 M S 607.ASME + 0.00 1.63 104 40 M S 427. ASME+ 0.00
- 1. 93 11 s <20* M S 207. ASME+ 0.00 4.26 117 <20 M S 107.GROOV+ 0.00 Ms CURVE 4: SP1=81;SP2=60;SP3=42 2.00 40 81 M s 817. ASME+ 0.00 LEVEL
Page 5 of 27 PLANT UNIT S/G LEG REEL TO REEL DATE . MIZ-18 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG % CH# LOCATION EXTENT 490 999 1 .81 68 60 M5 607.ASME + 0.00 1 .64 103 42 M5 42% ASME+ 0.00 1 *. 92 115 37 M5 207. ASME+ 0.00 4.26 116 36 M5 107.GROOV+ 0.00 M5 CURVE 5: SP1=60;SP2=42;SP3=20 1 .81 68 59 M5 607.ASME + 0.00 1.64 103 41 M5 42% ASME+ 0.00*
- 1. 92 115 <20 M5 20% ASME+ 0.00 4.26 116 <20 M5 107.GROOV+ 0.00 RUN 6: 0 SAVE ON 107.;3 SAVE ON 20%; 1 SAV/SUP OTHER 490 999 M5 CURVE 1: SP1=100;SP2=60;SP3=20
- 1. 73 40 100 M5 100%ASME+ 0.00 2.15 40 100 M5 81% ASME+ 0.00 1.88 69 60 M5 60%ASME + 0.00 1.67 106 28 M5 427. ASME+ 0.00
- 1. 98 120 20 M5 20% ASME+ 0.. 00 4.39 121 <20 M5 107.GROOV+ 0.00 M-5 CURVE 2: SP1=81;SP2=601SP3=20
- 2.15 40 80 1.88 69 59 1.67 106 31
- 1. 98 120 <20 4.39 121 <20 2 .*15 4.0 80 M5 M5 M5 M5 M5 M5 81% ASME+ 0.00 607.ASME + 0.00 427. ASME+ 0.00 20% ASME+ 0.00 10%GROOV+ 0.00 CURVE 3: SP 1=81 ; SP2=42; SP3=20 .
M5 81% ASME+ 0.00 1.88 69 70 M5 607.ASME + 0.00 1.67 106 41 M5 42% ASME+ 0.00
- 1. 98 120 <20 M5 20% ASME+ 0.00 4.39 121 <20 M5 107.GROOV+ 0.00 M5 CURVE 4: SP1=~1;SP2=601SP3=42 2.15 40 81 M5 81% ASME+ 0.00 1.88 69 59 M5 607.ASME + 0.00 1.67 106 41 M*5 427. ASME+ 0.00
- 1. 98 120 36 M5 201 ASME+ 0.00 4.39 121 36 M5 107.GROOV+ 0.00 M5 CURVE 5: SP1=60;SP2=421SP3=20 1.88 69 61 M5 60%ASME + 0.00 1.67 106 42 M5 42% ASME+ 0.00
- 1. 95 120 20 M5 207. ASME+ 0.00 4.39 121 <20 M5 107.GROOV+ 0.00 RUN 7: 0 SAV 107.;3 SAVS 20/42%; 1 SAV/SUP OTHER 490 999 0.38 52 RES M 5 4M DENT+ 0.00
- 490 999 M 5 CURVE 1: SP1=100;SP2=60;SP3=20 LEVEL
Page 6 of 27
- PLANT UNIT S/G LEG REEL TO REEL DATE MIZ-18 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG % CH# LOCATION EXTENT 490 999 1. 76 40 100 M5 100%ASME+ 0.00
- 2. 18 40 100 M5 81% ASME+ 0.00
- 1. 95 68 60 M5 60%ASME + 0.00
- 1. 75 104 28 M5 42% ASME+ 0.00 2.04 118 20 M5 20% ASME+ 0.00 4.54 119 <20 M5 10%GROOV+ 0.00 M5 CURVE z: SP1=81 ;SP2=60;5P3=20 2 .18 40 81 M5 81% ASME+ 0.00
- 1. 95 68 60 M5 607.ASME + 0.00
- 1. 75 104 31 M5 427. ASME+ 0.00 2.04 118 20 M5 20% ASME+ 0.00 4.54 119 <20 M5 10%GROOV+ 0.00 M5 CURVE 3: SP1=81 ;SP2=42;SP3=20
- 2. 18 40 81 M5 81% ASME+ 0.00
- 1. 96 68 70 M5 60%ASME + 0.00
- 1. 74 105 42 M5 42% ASME+ 0.00 2.05 118 20 M5 20% ASME+ 0.00 4.54 119 <20 M5 10%GROOV+ 0.00 M5 CURVE 4: SP 1=8*1 ; SP2=60; SP3=42 2 .18 40 81 M5 81% ASME+ 0.00
- 1. 95 68
- 1. 75 104 2.04 118 4.55 119
- 1. 95 . 68 60 42 36 36 60 M5 M5 M5 M5 M5 M5 60%ASME + 0.00 427. ASME+ 0.00 207. ASME+ 0.00 10%GROOV+ 0.00 CURVE 5: SP1=60;SP2=42;5P3=20 607.ASME + 0.00 RUN 8:SAVES- 100/1 ;81/1 ;60/3;42/1 ;20/3;10/0 SUPPRESSIONS: TSP/1 ;4M DNT/1 490 999 0.40 213 RES M 5 4M DENT+ 0.00 490 999 M5 CURVE 1: SP1=1001SP2=60;SP3=20
- 1. 93 40 100 M 5 1007.ASME+ 0.00 2.55 41 97 M*5 81% ASME+ 0.00 2.52 66 60 M 5 60%ASME + 0.. 00
- 2. 1(1) 97 32 M 5 42% ASME+ 0.00
- 2. 19 117 20 M 5 20% ASME+ 0.00 4.82 123 <20 M 5 107.GROOV+ 0.00 M5 CURVE 2: SP1=81 ;SP2=60;SP3=20 2.55 41 81 M 5 817. ASME+ 0.00 2.52 67 60 M 5 60%ASME + 0.00 2.10 96 37 M 5 427. ASME+ 0.00
- 2. 1g 118 20 M 5 207. ASME+ 0.00 4.82 123 <20 M 5 107.GROOV+ 0.00 M5 CURVE 3: SP1=81 ;SP2=42;SP3=20 2.55 41 81 M 5 817. ASME+ 0.00 2.51 67 65 M 5 607.ASME + 0.00 LEVEL
Page 7 of 27 PLANT UNIT SIG LEG REEL TO REEL DATE MIZ-18 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG % CH# LOCATION EXTEIH 490 999 2.11 97 42 M 5 42% ASME+ 0.00
- 2. 18 117 21 M 5 20% ASME+ 0.00 4.83 123 <20 M 5 1.0%GROOV+ 0.00 M 5 CURVE 4: SP1=81;SP2=60;SP3=42 2.55 41 80 M 5 81% ASME+ 0.00 2.51 67 59 M S 60XASME + 0.00 2.11 97 42 M 5 42% ASME+ 0.00 2.18 117 32 M 5 20X ASME+ 0.00 4.83 123 29 M 5 10ZGROOV+ 0.00 M 5 CURVE 5:SP1=60;SP2=42;SP3=20 2.51 67 60 M 5 60%ASME + 0.00 2.11 97 42 M 5 42X ASME+ 0.00 2 .18 117 20 M 5 20% ASME+ 0.00 4.83 123 <20 M 5 10ZGROOV+ 0.00 RUN 9:SAVES- 100/1;81/3;60/3;42/1 ;20/3/10/0 SUPPRESSIONS: TSP /1 ; 4M ONT I 1 490 999 0.48 211 RES M 5 4M DENT+ 0.00
- 490 999 2.18 39 100 2.86 39 100 2.89 62 60 2.38 92 32 2.48 113 20 M5
*M 5 M5 M5 MS M5 CURVE 1 :SP1=100;SP2=60;5Pp=20 100XASME+ 0.00 81X ASME+ 0.00 60%ASME + 0.00 42Z ASME+ 0.00 20X ASME+ 0.00 5.43 118 <20 M5 10%GROOV+ 0.00 M5 CURVE 2: SP1=81;SP2=60;SP3=20 2 ~ 86 39 81 M5 81% ASME+ 0.00 2.89 62 60 M5 60%ASME + 0.00 2.38 92 35 M5 42X ASME+ 0.00 2.48 112 20 M5 20Z ASME+ 0.00 5.43 118 <20 M5 10XGROOV+ 0.00*
M5 CURVE 3: SP1=81 ;SP2=42;SP3=20 2.88 39 80 M*5 81% ASME+ 0.00 2.88 63 65 M5 60%ASME + 0.00 2.39 91 42 M5 42% ASME+ 0.00 2.48 112 21 M5 20% ASME+ 0.00 5.42 118 <20 M5 10%6ROOV+ 0.00 M5 CURVE 4: SP1=81 ;SP2=60;SP3=42 2.88 39 81 M5 SD~ ASME+ 0.00 2.88 63 60 M5 60%ASME + 0.00 2.39 91 42 M5 42% ASME+ 0.00 2.48 112 31 M5 20% ASME+ 0.00 5.42 118 28 M5 10%GROOV+ 0.00 M5 CURVE 5: SP1=60;SP2=42;5P3=20 2.88 63 60 M5 60%ASME + 0.00 2.39 91 42 M5 42% ASME+ 0.00 LEVEL
Page 8 of' 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG 490 999 UNIT NA SIG NA LEG NA
% CH# LOCATION 2.48 112 . 20 M 5 20% ASME+
REEL TO REEL 11 0.00 11 DATE 01 /30/89 EXTENT 5.42 118 <20 M 5 107.GROOV+ 0.00 RUN 10: SAVES=100/l ;81/3;60/3;42/3;20/3;10/1 490 9"99 0.54 251 RES M 5 4M DENT+ 0.00 490 999 M5 CURVE 1: SP1=100;SP2=60;SP3=20 2.44 40 100 M5 1007.ASME+ 0.00 3.20 40 100 M5 81% ASME+ 0.00 3.26 61 60 M5 607.ASME + 0.00 2.60 87 ;)-?... M5 42% ASME+ 0.00 2.47 106 20 M5 20% ASME+ 0.00 5.30 111 <20 M5 107.GROOV+ 0.00 M 5 CURVE 2: SP1=81 ;SP2=60;SP3=20 3.20 40 81 M5 81% ASME+ 0.00 3.26 61 60 M5 607.ASME + 0.00 2.60 87 36 M5 42% ASME+ 0.00 2.47 106 20 M5 20% ASME+ 0.00 5.30 111 <20 M5 107.GROOV+ 0.00
- 3.20 40 81 3.26 61 66 2.60 88 42 2.47 106 20 5.30 111 <20 M5 M5 M5 M5 M5 M5 CURVE 3: SP1=81 ;SP2=42;SP3=20 81% ASME+ 0.00 60%ASME + 0.00 427. ASME+ 0.00 20% ASME+ 0.00 10%GROOV+ 0.00 M5 CURVE 4: SP1=81 ;SP2=60;SP3=42 3.20 40 81 M5 817. ASME+ 0.00 3.26 62 60 M5 607.ASME + 0.00 2.60 87 42 M5 427. ASME+ 0.00 2.47 106 31 M5 20% ASME+ 0.00 5.30 111 28 M5 107.GROOV+ 0.00 M5 CURVE 5: SP1=60;SP2=42;5P3=20 3.26 61 60 M5 607.ASME + 0.00 2.61 87 42 M 5 42% ASME+ 0.00 3.26 61 60 M 5' 607.ASME + 0.00 2.61 87 42 M 5 427. ASME+ 0.00 2.47 106 20 M5 20% ASME+ 0.00 5.30 111 <20 M5 107.GROOV+ 0.00 RUN 11: SAVES: 100/0;81 /1 ;60/1 ;42/1;20/1i10/ 1 SUPP: TSP/1; 4M ONT I 1 1 490 999 0.58 228 RES M 6 4M DENT+ 0.00
- 490 999
- 2. 96 M 6 CURVE 1: SP1=100;5P2=60;5P3=20 41 100 M 6 100%ASME+ 0.00 LEVEL
Page 9 of 27
- PLANT UNIT S/G LEG REEL TO REEL DATE MIZ-i8 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG % CH# LOCATION EXTENT 490 999 3.92 40 97 M6 81% ASME+ 0.00 4.15 55 60 M6 60%ASME + 0.00 3.25 77 31 M6 42% ASME+. 0.00 3.10 94 20 M6 20% ASME+ 0.00 6.63 100 <20 M6 10%GROOV+ 0.00 M6 CURVE 2: SP1=81; SP2=60;SP3=20 3.92 40 81 M6 81% ASME+ 0.00 4.15 55 60 M6 60%ASME + 0.00 3.25 77 35 M6 427. ASME+ 0.00 3.10 94 20 M6 20% ASME+ 0.00 3.10 94 20 M6 20% ASME+ 0.00 6.63 100 <20 M6 10%GROOV+ 0.00 M6 CURVE 3: SP1=81 ;SP2=42;SP3=20
- 3. 92 40 80 M6 81% ASME+. 0.00 4.15 SS 66 M6 60%ASME + 0.00 3.2S 77 41 M6 42% ASME+ 0.00 3.10 94 <20 M6 20% ASME+ 0.00 6.63 100 <20 M6 10%GROOV+ 0.00 .
!. 3.92 40
- 4. lS SS 3.25 77 3.10 94 6.63 100 81 60 42 33 30 M6 M6 M6 M6 M6 M6 CURVE 4: SPl=Bl 1 SP2=60;SP3=42 81% ASME+ 0.00 60%ASME + 0.00 42% ASME+ 0.00 204 ASME+ 0.00 10%GROOV+ 0.00 M6 CURVE 5: SP1=60;SP2=42;SP3=20*
4.15. 55 59 M6 60%ASME + 0.00 3.25 77 41 M6 42% ASME+ 0.00 3.10 94 <20 M6 20% ASME+ 0.00 6.63 100 <20 M6 107.GROOV+ 0.00 RUN 12: SAVES- 100/0;81 /1 ;60/1 ;42/1;20/3;10/1 SUPPRESSIONS: TSP/1; 4M DNT/1 490 999 0.62 226 RES M 6 4M DENT+ 0.00 490 999 M6 CURVE 1: SP1=100;SP2=60;SP3=20 3.20 40 100 M6 1004ASME+ 0.00 4.2S 40 100 M6 817. ASME+ 0.00 4.49 54 59 M6 607.ASME + 0.00 3;59 76 31 M6 42Y. ASME+ 0.00 3.47 98 <20 M6 207. ASME+ 0.00 7.46 100 <20 M6 107.GROOV+ 0.00 M6 CURVE 2: SP1=81;SP2=60;SP3=20 4.2S 39 81 M6 81% ASME+ 0.00 4.49 55 58 M6 60%ASME + 0.00 3.S8 7.6 3S M6 427.ASME + 0.00 3.47 94 20 M6 20% ASME+ 0.00 7.46 100 <20 M6 107.GROOV+ 0.00 LEVEL
Page 10 of 27
- PLANT UNIT SIG LEG REEL TO REEL DATE MIZ-18 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG % CH# LOCATION EXTENT 490 999 M6 CURVE 3: SPl =81; SP2=42; SP3=20 4.25 40 81 M6 81% ASME+ 0.00 4.49 56 66 M6 60%ASME + 0.00 3.58 79 42 M6 42% ASME+ 0.00 3.47 96 20 M6 20% ASME+ 0.00 7.46 101 <20 M6 10%GROOV+ 0.00 M6 CURVE 4: SPl =81; SP2=60;SP3=42 4.25 40 81 M6 81% ASME+ 0.00 4.49 56 60 M6 607.ASME + 0.00 3.58 79 42 M6 42% ASME+ 0.00 3.47 96 33 M6 20% ASME+ 0.00 7.46 101 31 M6 10%GROOV+ 0.00 M6 CURVE 5: SP1=60;SP2=42;SP3=20 4.50 56 60 M6 60%ASME + 0.00 3.58 79 42 M6 427. ASME+ 0.00 3.47 96. 20 M6 207. ASME+ 0.00 7.46 102 <20 M6 10%GROOV+ 0.00 I 0.34 0 RES M6 4M DENT+ 0.00 RUN 13: SAVES- 100/3;81 /1 ;60/1 ;42/1;20/3;10/1 .
- SUPPRESSIONS: TSP/1; 4M DNT/1 I
I I 1 490 999 M6 CURVE 1:SP1=100;SP2=60;SP3=20 1 .97 40 100 M 6 100%ASME+ 0.00 2.52 41 97 M 6 817. ASME+ 0.00 2.13 68 58 M 6 607.ASME + 0.00 1.62 107 30 M 6 42% ASME+ 0.00 1.67 131 <20 M 6 207. ASME+ 0.00 3.68 137 <20 M 6 107.GROOV+ 0.00 M6 CURVE 2: SPl=Bl ;SP2=60;SP3=42 2.52 40 Bl M 6 817. ASME+ 0.00
- 2. 13 66 60 M 6 607.ASME + 0.00
- 1. 62 106 33 M 6 42% ASME+ 0.00 1.67 129 20 M 6 20% ASME+ 0.00 3.68 136 <20 M*6 10%GROOV+ 0.00 M6 CURVE 3: SP1=Bl;SP2=42;SP3=20 2.52 40 81 M 6 81% ASME+ 0.00 2.13 66 68 M 6 60%ASME + 0.00 1.62 106 42 M 6 427. ASME+ 0.00 1.67 130 <20 M 6 20% ASME+ 0.00 3.68 136 <20 M 6 107.GROOV+ 0.00 M6 CURVE 4: SPl=Bl ;SP2=60;SP3=42 2.52 40 81 M 6 81% ASME+ 0.00 2.13 66 60 M 6 601.ASME + 0.00 1 .62 106 42 M 6 42% ASME+ 0.00 1.67 130 35 M 6 20% ASME+ 0.00 3.68 136 33 M 6 107.GROOV+ 0.00 M6 CURVE 5: SP1~60;SP2=42;SP3=20 LEVEL
Page 11 of 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG 490 999 UNIT NA
- 2. 13 66 59 M 6 S/G NA LEG NA CH# LOCATION 607.ASME +
REEL TO REEL 11 0.00 11 DATE 01 /30/89 EXTENT 1 .62 106 42 M 6 427. ASME+ 0.00 1 .67 130 <20 M 6 207. ASME+ 0.00 3.68 136 <20 M 6 10%GROOV+ 0.00 RUN 14: SAVES- 100/3;81/1;60/3;42/1 ;20/3;10/1 SUPPRESS IONS: TSP/1; 4M ONT/1 490 999 0.36 272 RES M 6 4M DENT+ 0.00 490 999 M6 CURVE 1: SP1=100;SP2=60;SP3=20
- 1. 79 39 100 M6 1007.ASME+ 0.00 2.30 41 97 M6 81% ASME+ 0.00 2.02 72 62 M6 607.ASME + 0.00 1.65 108 34 M6 42% ASME+ 0.00 1.65 128 21 M6 20% ASME+ 0.00 3.59 134 <20 M6 107.GROOV+* 0.00 M6 CURVE 2: SP1=81; SP2=60;SP3=20
- 2.30 41 81 2.02 72 61 1.65 109 36 1.65 128 22 3.59 134 <20 M6 M6 M6 M6 M6 M6 817. ASME+ 0.00 607.ASME + 0.00 427. ASME+ 0.00 207. ASME+ 0.00 107.GROOV+ 0.00 CURVE 3*: SP1=81 ;SP2=42;SP3=20
_2 .30 41 80 M6 817. ASME+ 0.00 2.02 72- 67 M6 607.ASME + 0.00 1.65 108 41 M6 427. AS-ME+ 0.00
- 1. 65 128 <20 M6 207. ASME+ 0.00 3.59 134 <20 M6 107.GROOV+ 0.00 M6 CURVE 4: SP1=81 ;SP2=60;SP3=42 2;30 41 81 M6 817. ASME+ 0.00 2.02 72 60 M6 607.ASME + 0.00 1.64 109 42 M6 427. ASME+ 0.00 1.65 128 34 M6 20% ASME+ 0.00 3.59 134 32 M6 10%GROOV+ 0.00 M6 CURVE 5: SP1=60;SP2=42;SP3=20 2.02 72 60 M6 607.ASME + 0.00 1.65 108 42 M6 42% ASME+ 0.00 1.65 128 20 M6 207. ASME+ 0.00 3.59 134 <20 M6 107.GROOV+ 0.00 RUN 15: SAVES- 100/3;81/3;60/3;42/l ;20/3;10/1 SUPPRESSIONS: TSP/1; 4M DNT/1 490 999 0.46 274 RES M 6 4M DENT+ 0.00
- 490 999 M 6 CURVE 1: SP1=100;SP2=60;SP3=20 LEVEL
Page 12 of 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG 1 490 999 UNIT NA 2 .10 40 . 99 SIG NA LEG NA CH# LOCATION REEL TO REEL M 6 100%ASME+ 0.00 11 11 DATE 01/30/89 EXTENT 2.70 41 98 M 6 81% ASME+ 0.00 2.52 70 59 M 6 60%ASME + 0.00 2.06 103 31 M 6 42% ASME+ 0.00 2.02 122 20 M 6 20% ASME+ 0.00 4.37 128 <20 M 6 10Y.GROOV+ 0.00 M 6 CURVE 2: SP1=81 ;SP2=60;SP3=20 2.70 40 81 M 6 817. ASME+ 0.00 2.52 68 60 M 6 60%ASME + 0.00 2.06 100 35 M 6 42Y. ASME+ 0.00 2.01 120 20 M 6 20% ASME+ 0.00 4.37 125 <20 M 6 10%6ROOV+ 0.00 M6 CURVE 3: SP1=81 ;SP2=42;SP3=20 2.70 40 81 M 6 81% ASME+ 0.00 2.52 68 66 M 6 60%ASME + 0.00 2.06 100 42 M 6 42% ASME+ 0.00 2.01 120 20 M 6 207. ASME+ 0.00 4.37 125 <20 M 6 10Y.GROOV+ 0.00 M 6-CURVE 4: SP1=81 ;SP2=60;SP3=42 2.70 40 81 M 6 81% ASME+ 0.00
- 2.52 68 2.06 100 2.01 120 4.37 -125 2.52 68 60 60 42 33 30 M 6 60%ASME + 0.00 M 6 42% ASME+ 0.00 M 6 20% ASME+ 0.00 M 6 10%GROOV+ 0.00 M 6 CURVE 5: SP1=60;SP2=42;SP3=20 M 6 60%ASME + 0.00 2.06 100 42 M 6 427. ASME+ 0.00 2.01 120 20 M 6 20% ASME+ 0.00 4.37 125 <20 M 6 10%GROOV+ 0.00 RUN 16: SAVES-100/3;81/3;60/3;42/3;20/3;10/1 SUPPRESSIONS-TSP/I 1 4M DNT/1 490 999 0.47 0 RES M 6 4M DENT+ 0.00 490 999 M6 CURVE 1: SP1=100;SP2=60;5P3=20 2 .16 39 100 M 6 100%ASME+ 0.00 2.75 41 96 M 6 81% ASME+ 0.00 2.56 71 60 M 6 60%ASME + 0.00 2.12 105 31 M 6 42% ASME+ 0.00 2.07 122 20 M 6 207. ASME+ 0.00 4.45 127 <20 M, 6 10%GROOV+ 0.00 M6 CURVE 2: SP1=81;SP2=60;5P3=20 2.75 40 81 M 6 81% ASME+ 0.00 2.56 70 60 M 6 607.ASME + 0.00 2 .12 104 34 M 6 42% ASME+ 0.00 2.06 122 20 M 6 20% ASME+ 0.00 4.45 126 <20 M 6 10%GROOV+ 0.00 LEVEL
Page 13 of 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG 490 999 UNIT NA SIG NA M6 LEG NA CH# LOCATION REEL TO REEL 11 11 DATE 01/30/89 EXTENT CURVE 3: SP1=81 ;SP2=42;SP3=20 2.75 40 81 M6 81% ASME+ 0.00 2.56 70 67 M6 60Y.ASME + 0.00
- 2. 12 104 42 M6 42Y. ASME+ 0.00 2.06 122 20 M6 20% ASME+ 0.00 4.45 126 <20 M6 107.GROOV+ 0.00 M6 CURVE 4: SP1=81 ;SP2=60;SP3=42 2.75 40 80 M6 817. ASME+ 0.00 2.56 70. 59 M6 607.ASME .+ 0.00 2.12 104 41 M6 42% ASME+ 0.00 2.06 122 34 M6 207. ASME+ 0.00 4.45 126 32 M6 107.GROOV+ 0.00 M6 CURVE 5: SP1=60;SP2=42;SP3=20 2.56 70 60 M6 607.ASME.+ 0.00
- 2. 12 104 42 M6 42% ASME+ 0.00 2.06 122 20 M6 20% ASME+ 0.00 4.45 126 <20 M6 107.GROOV+ 0.00 RUN 17: SAVES-100/3;81/1 ;60/1 ;42/1;20/1 ;10/1
"* 490 999 490 999 SUPPRESSIONS: TSP 11 ; 4M DNT/1 0.39 216 RES M 6 4M 1.89 40 100 M6 M6 DENT+ 0.00 CURVE 1: SP1=100;SP2=60;SP3=20 1007.ASME+ 0.00 2.38 41 97 M6 81Y. ASME+ 0.00 2.04 66 59 M6 607.ASME + 0.00 1 .50 105 30 M6 42Y. ASME+ 0.00 1.56 129 20 M6 20% ASME+ 0.00 3.45 136 <20 M6 10Y.GROOV+ 0.00 M6 CURVE 2: SP1=81;SP2=60~SP3=20 2.42 40 81 M 6 81% ASME+ 0.00 2.04 65 59 M 6 607.ASME + 0.00 1.50 103 33 M 6 427. ASME+ 0.00 1.55 127 <20 M 6 207. ASME+ 0.00 3.45 135 <20 M 6 107.GROOV+ 0.00 M6 CURVE 3: SP1=81;SP2=42;SP3~20 2.43 40 80 M 6 81Y. ASME+ 0.00 2.04 65 67 M 6 607.ASME + 0.00 1.52 102 41 M 6 42Y. ASME+ 0.00 1.56 128 <20 M 6 207. ASME+ 0.00 3.45 134 <20 M 6 10Y.GROOV+ 0.00 M6 CURVE 4: SP1=81;SP2=60;SP3=42 2.43 40 81 M 6 81Y. ASME+ 0.00 2.04 65 60'M 6 607.ASME + 0.00
- 1 .52 102 1.56 128 42 M6 33 M 6 42% ASME+ 0.00 20% ASME+ 0.00 LEVEL
Page 14 of 27 PLANT UNIT S/6 LEG REEL TO REEL DATE MIZ-18 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG I. CH# LOCATION EXTENT 490 999 3.45 134 32 M 6 10%GROOV+ 0.00 M6 CURVE 5: SP1=60;SP2=42;SP3=20 2.04 65 59 M 6 60%ASME + 0.00 1.52 102 41 M 6 42% ASME+ 0.00 1 .56 128 <20 M 6 20% ASME+ 0.00 3.45 134 <20 M 6 10%GROOV+ 0.00 RUN 18: SAVES-t00/6;81/1 ;60/1 ;42/1 ;20/1 ;10tl SUPPRESSIONS: TSP/1; 4M DNT/1 490 999 0.34 0 RES M 6 4M DENT+ 0.00 490 999 M 6 CURVE I: SP1=100;SP2=60;SP3=20
- 1. 92 40 99 M 6 100%ASME+ 0.00 2.45 41 97 M 6 81% ASME+ 0.00
- 1. 93 65 59 M 6 60%ASME + 0.00
- 1. 36 108 30 M 6 42% ASME+ 0.00 1.43 136 20 M 6 20% ASME+ 0.00
- i. 3.22 143 <20 2.45 40 80
- 1. 93 64 59 1.36 107 33 1.44 136 <20 M 6 10%GROOV+ 0.00 M 6 CURVE 2: SP1=81; SP2=60;SP3=20 M 6 81% ASME+ 0.00 M 6 60%ASME + 0.00 M 6 42% ASME+ 0.00 M 6 20% ASME+ 0.00 3.22 142 <20 M 6
- 10%GROOV+ 0.00 M 6 CURVE 3: SP1=81; SP2=42; SP3=20 2.45 40 81 M 6 81% ASME+ 0.00
- 1. 93 64 68 M 6 60%ASME + 0.00
- 1. 36 107 42 M 6 42% ASME+ 0.00 1 .44 136 20 M 6 20% ASME+ 0.00 3.22 1"42 <20 M 6 10%GROOV+ 0.00 M 6 CURVE 4: SP1=81; SP2=60;SP3=42 2.45 40 80 M 6 BlY. ASME+. 0.00
- 1. 93 64 60 M 6 60%ASME + 0.00 1.36 107 41 M*6 42% ASME+ 0.00 1.44 136 35 M 6 20% ASME+ 0.00 3.22 142 34 M 6 10%GROOV+ 0.00 M 6 CURVE 5: SP1=60; SP2=42; SP3=20
- 1. 93 64 60 M 6 60%ASME + 0.00 1.36 107 42 M 6 42% ASME+ 0.00 1.44 136 20 M 6 20% ASME+ 0.00 3.22 142 <20 M 6 10%GROOV+ 0.00 NOTE: HEREAFTER, ONLY CURVE 1 TO ESTABLISH PHASE SPREADS RUN 19: SAVES-100/6;81/1 ;60/3;42/1;20/1 ;10/1 1 490 999 0.39 0 RES M 6 4M DENT+ 0.00 LEVEL
Page 15 of 27
- P.LANT MIZ-18 QUAL ST IN- RUN VOLTS DEG UNIT NA SIG NA LEG NA CH# LOCATION REEL TO REEL 11 11 DATE 01 /30/89 EXTENT 1 490 999 M6 CURVE 1: SP1=100; SP2=60; SP3=20
- 1. 62 40 100 M 6 100%ASME+ 0.00 2.04 42 96 M 6 817. ASME+ 0.00 1 .65 70 59 M 6 607.ASME + 0.00 1 .28 112 30 M 6 427. ASME+ 0.00 1 .33 136 <20 M 6 207. ASME+ 0.00 2.97 141 <20 M 6 107.GRODV+ 0.00 RUN 20: SAVES- 100/6;81/1 ;60/6;42/1 ;20/1 ;10/1 SUPPRESSIONS: TSP/ 1; 4M DNT/1 490 999 0.40 158 RES M 6 4M DENT+ 0. 00 490 999 1. 49* 40 99 M 6 101i'J%ASME+ 0.00 1 .87 43 95 M 6 817. ASME+ 0. 00
- 1. 57 76 59 M 6 607.ASME + 0.00 1.31 116 30 M 6 427. ASME+ 0.00 1 .34 135 <20 M 6 207. ASME+ 0.00 2.95 141 <20 M 6 107.GROOV+ 0.00 RUN 21: SAVES- 100/6;81/l ;60/6;42/1;20/3;10/l SUPPRESSIONS- TSP/!; 4M DNT/1 RUN 21: SAVES-100/6;81/l ;60/6;42/l ;20/3;10/1 490 999 0.41 159 RES M 6 4M DENT+ 0.00 490 999 M6 CURVE 1: SP1=100;SP2=60;SP3=20 1 .48 40 100 M6 1007.ASME+ 0.00
- 1. 87 42 97 M6 81% ASME+ 0.00 1.58 75 60 M6 607.ASME + 0.li'l0 1 .31 115 30 M6 42% ASME+ 0.00 1.33 134 20 M *6 207. ASME+ li'J.li'l0 2.95 140 <20 M6 10/.GROOV+ 0.00 RUN 22: SAVES- 100/~;81/1 ;60/6;42/l ;20/6;10/l SUPPRESSIONS: TSP/1; 4M ONT/ l 490 999 0.54 16.1 RES M 6 4M DENT+ 0.00 490 999 M6 CURVE 1: SP1=100; SP2=60; SP3=20 1 .86 40 100 M6 100%ASME+ 0.00 2.35 43 95 M6 81% ASME+ 0.00
- 1. 98 75 60 M6 60/.ASME + 0.00
- 1. 62 114 31 M6 427. ASME+ 0.00
- 1. 70 136 <20 M6 207. ASME+ 0.00 LEVEL
Page 16 of 27 PLANT UNIT S/G LEG REEL TO REEL DATE MIZ-18 QUAL NA NA NA 11 11 01/30/89 ST IN- RUN VOLTS DEG % CH# LOCATION EXTENT 490 999 3.76 141 <20 M 6 10%GROOV+ 0.00* RUN 23: SAVES-100/4;81/1 ;60/1 ;42/1 ;20/4;10/1 SUPPRESSIONS- TSP/1; 4M ONT/ 1 490 999 0.40 5 RES M 6 4M DENT+ 0.00 490 999 M6 CURVE I: SP1 =100; SP2=60;SP3=20 2.09 40 100 M 6 100%ASME+ 0.00 2.69 41 97 M 6 811. ASME+ 0.00 2.21 66 59 M 6 601.ASME + 0.00
- 1. 63 107 30 M 6 42% ASME+ 0.00
- 1. 75 134 <20 M 6 20% ASME+ 0.00 3.86 140 <20 M 6 10%GROOV+ 0.00 RUN 24: SAVES-100/5;81/1 ;60/1 ;42/1 ;20/5;10/1 SUPPRESSIONS- TSP/1; 4M ONT I 1 1 490 999 0.44 2 RES M 6 4M DENT+ 0.00 2.20 38 99 M 6 100%ASME+ 0.00
- 2.82 39 97 2.30 63 59 1.65 106 30
- 1. 79 134 20 4.01 142 <20 M6 M6 M6 M6 M6 81% ASME+
60%ASME + 42% ASME+ 20% ASME+ 10%GROOV+ 0.00 0.00 0.00 0.00 0.00 RUN ZS: SAVES-100/5;81/1 ;60/2;42/1 ;20/5;10/1 SUPRESSIONS- TSP/1; 4M ONT I I 490 999 0.45 359 RES M 6 4M DENT+ 0.00 490 999 M6 CURVE 1: SP1=1001SP2~60;SP3=2~ 2.04 39 100 M6 100%ASME+ 0.00 2.62 41 96 M6 81% ASME+ 0.00
- 2. 16 67 60 M6 60%ASME + 0.00 1.64 108 31 M6 42% ASME+ 0.00
- 1. 75 135 20 M6 20% ASME+ 0.00 3.89 141 <20 M6 10%GROOV+ 0.00 RUN 26: SAVES- 100/3;81/1 ;60/I ;42/1 ;20/3;10/1 SUPPRESSIONS-TSP/1; 4M ONT/I 1 490 999 0.41 228 RES M 6 4M DENT+ 0.00 M6 CURVE I: SP1=100; SP2=60; SP3=20
- 1. 99 40 100 M 6 100%ASME+ 0.00 2.57 41 97 M 6 811. ASME+ 0.00
- 2. 19 65' 60 M 6 60%ASME + 0.00
- 1. 64 104 30 M 6 42% ASME+ 0.00
- 1. 69 130 20 M 6 20% ASME+ 0.00 LEVEL
Page 17 of 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG UNIT NA S/G NA LEG NA CH# LOCATION REEL TO REEL 11 11 DATE 01/30/89 EXTENT 490 999 3.76 136 <20 M 6 10%GROOV+ 0.00 RUN 27: SAVES-100/4;81/1 ;60/2;42/l ;20/4;10/l SUPPRESSIONS: TSP/1; 4M D/1 1 490 999 0.40 216 RES M 6 4M Df::NT+ 0.00 M6 CURVE 1: SP1=100; SP2=60; SP3=20 1 .90 40 100 M 6 100'7.ASME+ 0.00 2.44 41 97 M 6 81'7. ASME+ 0.00 2.03 66 61 *M 6 60'7.ASME + 0.00 1.47 106 31 M 6 42% ASME+ 0.00 1.48 132 <20 M 6 20% ASME+ 0.00 3.27 138 <20 M 6 10'7.GROOV+ 0.00 RUN 28: SAVES-100/3;81/1;60/~ ;42/1 ;20/3;10/1 SUPPRESSIONS: TSP/1; 4M DNT/1 1 490 999 0.25 169 RES M 6 4M DENT+ 0.00 M6 CURVE 1: SP1=100; SP2=60;SP3=20 2.03 40 100 M 6 100'7.ASME+ 0.00 2.61 41 97 M 6 81'7. ASME+ 0.00 2.21 67 60 M 6 60'7.ASME + 0.00 1.67 105 31 M 6 42% ASME+ 0.00
- 1. 74 131 <20 M 6 20'7. ASME+ 0.~0 3.83 136 <20 M 6 10'7.GROOV+ 0.00 RUN 29: SAVES- 100/4181/1;60/1 ;42/1 ;20/4;10/1 SUPPRESSIONS- TSP/1;4M DNT/1 1 490 999 0.40 231 RES M 6 4M DENT+ 0.00 M6 CURVE 1: SP1=100; SP2=60; SP3=20 2 .10 40 100 M 6 100'7.ASME+ 0.00 2.70 41 97 M 6 81% ASME+ 0.00 2.21 66 60 M 6 60'7.ASME + 0.00 1 .64 108 30 M*6 42'7. ASME+ 0.00
- 1. 75 135 20 M 6 20'7. ASME+ 0.00 3.87 141 <20 M 6 10'7.GROOV+ 0.00 RUN 30: SAVES- 100/4;81/1;60/2;42/1 ;20/4;10/1 SUPPRESSIONS- TSP/1; 4M DNT/1 1 490 999 0.23 174 RES M 6 4M DENT + 0.00 M 6 CURVE 1: SP1=100; SP2=60; SP3=20
- 1. 95 40 100 M 6 100%ASME+ 0.00 2 .5,1 41 98 M 6 81% ASME+ 0.00 2.09 69 60 M 6 60%ASME + 0.00 1 .63 108 31 M 6 42% ASME+ 0.00
- 1. 70 133 <20 M 6 20% ASME+ 0.00 3.74 139 <20 M 6 107.GROOV+ 0.00 LEVEL
Page 18 of 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG UNIT NA S/G NA LEG NA CH# LOCATION REEL TO REEL 11 11 DATE 01 /30/89" EXTENT RUN 31: SAVES- 100/5;81/1 ;60/2;42/1 ;20/5;10/1 SUPPRESSIONS- TSP/1; 4M DNT/1 1 490 999 0.43 4 RES 4M SEN T +0.00 M 6 CURVE 1: SP1=100; SP2=60;SP3=20 2.00 40 100 M 6 100%ASME+ 0.00 2.56 41 98 M 6 81% ASME+ 0.00 2.10 69 60 M 6 60%ASME + 0.00
- 1. 61 111 30 M 6 42% ASME+ 0.00
- 1. 70 136 20 M 6 20% ASME+ 0.00 3.76 142 <20 M 6 10%GROOV+ 0.00 RUN 32: SAVES- 100/6;81/1 ;60/2;42/1;20/6;10/1 SUPPRESSIONS- TSP/1; 4M DNT/1 1 490 999 0.28 175 RES M 6 4M DENT+ 0.00 M6 CURVE 1: SP1=100; SP2=60; SP3=20 2.09 40 99 M 6 100%ASME+ 0.00 2.66 42 96 M 6 81% ASME+ 0.00 2 .14 69 59 M 6 60%ASME + 0.00
- 1.62 112 30 M 6
- 1. 74 139 20 M 6 3.88 145 <20 M 6 42% ASME+ 0.00 20% ASME+ 0.00 i0%GROOV+ 0.00 CONTINUED ON DISC 25
- LEVEL
Page 19 of 27 PLANT UNIT S/6 LE6 REEL TO REEL DATE
- MIZ-18 QUAL DZS ST IN- RUN VOLTS DE6 NA NA NA
% CH# LOCATION UNT ANL 11 MIZ-18 QUALIFICATION B.CURTIS III 11 01/30/89 EXTENT DAT 3/08/89 REL #11 MIZ18 QUAL OSK 2S PRB 580 SLF NEW.MIX PARAMETRIC STUDY (CONTINUED)
RUN 33: SAVE?- 100/6;81/1;60/3;42/1;20/6;10/1 SUPPRESSIONS- TSP/1; 4M DNT/1 1 490 999 0.48 3 RES M 6 4M DENT+ 0.00 M6 CURVE 1: SP1=100;SP2=60;SP3=20
- 1. 97 40 100 M 6 1007.ASME+ 0.00 2.52 41 98 M 6 81% ASME+ 0.00 2.06 71 59 M 6 607.ASME + 0.00
- 1. 61 113 30 M 6 42% ASME+ 0.00
- 1. 71 137 <20 M 6 20% ASME+ 0.00
- 3. 77 143 <20 M 6 10%6ROOV+ 0.00 RUN 34: SAVES-100/7;81/1 ;60/3;40/1;20/7;10/1 SUPPRESSIONS- TSP/1; 4M D/1 1 490 999 0.51 2 RES M 6 4M DEMT + 0.00 M6 CURVE 1: SP1=100SP2=60;SP3=20 2.05 40 99 M 6 1007.ASME+ 0.00 2.61 42 96 M 6 81% ASME+ 0.00 2.09 71 59 M 6 607.ASME + 0.00 1.62 113 31 M 6 42% ASME+ 0.00
- 1. 73 140 20 M 6 20% ASME+ 0.00 3.85 145 <20 M 6 10%6ROOV+ 0.00 RUN 35: SAVES-100/8;81/1 ;60/3/;40/1 ;20/8;10/1 SUPPRESSIONS- TSP/1; 4M 0/1 1 490 999 0.56 4 RES M 6 4M DENT+ 0.00 M6 CURVE 1: SP1=100; SP2=60; SP3=20
- 2. 12 40 100 M 6 1007.ASME+ 0.00 2.70 42 96 M 6 81% ASME+ 0.00 2.15 71 60 M 6 60%ASME + 0.00 1.64 115 30 M 6 42% ASME+ 0.00
- 1. 78 141 20 M 6 20% ASME+ 0.00 3.97 146 <20 M 6 10%GROOV+ 0.00 RUN 36: SAVES-100/8;81/1 ;60/3;40/1;20/8;10/1 SUPPRESSIONS: TSP/1; 4M DNT/2 1 490 999 0.35 184 RES M 6 4M DENT+ 0.00 LEVEL
Page 20 of 27 PLANT UNIT S/G LEG REEL TO REEL DATE
- MIZ-18 QUAL 025 ST IN- RUN VOLTS DEG 490 999 NA 1 ."87 40 99 M 6 NA NA CH# LOCATION M6 11 11 01/30/89 EXTENT CURVE 1: SPl =100; SP2=60;SP3=20 100%ASME+ 0.00 2 .40 41 97 M 6 81% ASME+ 0.00
- 1. 91 68 59 M 6 60%ASME + 0.00 1.44 112 30 M 6 42% ASME+ 0.00 1.58 138 <20 M 6 20% ASME+ 0.00 3.54 144 <20 M 6 107.GROOV+ 0.00 RUN 37: MIX IS 400-600-100-10 SAVES: 100/3/81/1 ;60/1 ;40/1;20/3;10/1 SUPPRESS IONS: TSP/1; 4M DNT/1 1 490 999 0.45 287 RES M 7 4M DENT+ 0.00
- M7 CURVE 1: SP1=100;SP2=60;SP3=20 2.81 40 100 M 7 1007.ASME+ 0.00 3.66 40 100 M 7 81% ASME+ 0.00 2.96 68 60 M 7 60%ASME + 0.00 2.25 108 31 M 7 42% ASME+ 0.00 2.37 135 20 M 7 207. ASME+ 0.00 5.25 139 <20 M 7 10%GROOV+* 0.00 RUN 38: SAVES-100/6;81/1;60/3;42/1 ;20/6;10/1 SUPPRESSIONS: TSP/1; 4M D/1 1 490 999 0.66 167 RES M 7 4M DENT+ 0.00 M7 CURVE 1: SP1=100; SP2=60;SP3=20 2.80 39 *99 M 7 100%ASME+ 0.00 3.64 40 98 M 7 81% ASME+ 0.00 2.86 68 59 M 7 60%ASME + 0.00 2.20 110 31 M 7 427. ASME+ 0.00 2.40 138 <20 M 7 20% ASME+ 0.00 5.44 143 <20 M 7 10%GROOV+ 0.00 RUN 39: SAVES-100/6;80/1';60/3;42/1 ;20/6;10/1 SUPPRESSIONS- TSP/1; 4M DNT/2 1 490 999 0.37 288 RES M 7 4M DENT+ 0.00 M7 CURVE 1: SP1=100;SP2=60;SP3=20 2.47 40 100 M 7 100%ASME+ 0.00 3.25 40 100 M 7 81% ASME+ 0.00 2.56 67 60 M 7 607.ASME + 0.00
- 1. 93 108 31 M 7 42% ASME+ 0.00 2 .14 138 20 M 7 20% ASME+ 0.00 4.87 143 <20 M 7 10%GROOV+ 0.00 RUN 40: 400-600-100-10 8MIL DENT SAVES: 100/3;81/1 ;60/1 ;42/1;20/3;10/1 SUPPRESSIONS- TSP/1; SM DNT/1 LEVEL
Page 21 of 27 PLANT UNIT S/G LEG REEL TO REEL DATE
- MIZ-18 QUAL D2S ST IN- RUN VOLTS DEG 1 490 999 NA NA NA
% CH# LOCATION 2;25 212 RES M 7 SM DENT+ 0.00
.11 11 01/30/89 EXTENT M7 CURVE 1: SP1=100; SP2=60; SP3=20 2.88 40 100 M 7 100%ASME+ 0.00 3.32 45 91 M 7 81% ASME+ 0.00 2.82 69 60 M 7 607.ASME + 0.00 2.23 10B 30 M 7 427. ASME+ .0 .00 2.59 130 20 M 7 20% ASME+ 0.00 5.82 135 <20 M 7 10%GROOV+ 0.00 RUN 41: SAVEs.:...100;E; 81Il;60/ ~-; 42/ 1 ; 20/3; 10/ L SUPPRESSIONS- TSP/1; SM DNT/2 1 490 999 1.61 211 RES M 7 8M DENT+ 0.00 M7 CURVE 1 : SP1=100; SP2=60; SP3=20 2.39 39 100 M 7 100%ASME+ 0.00 2.88 42 93 M 7 81% ASME+ 0.00 2.4B 65 60 M 7 607.ASME + 0.00
- 1. 99 10;3 30 M 7 42% ASME+ 0.00 2.39 124 20 M 7 207. ASME+ 0.00 5.45 129 <20 M 7 107.GROOV+ 0.00
- 1 490 999 RUN 42: SAVES- 100/~;81/l;60/?;42/L;20/6;10/~
SUPPRESSIONS: TSP/ 1; SM DNT/2
- 1. 91 211 RES M 7 2.53 40 100 M 7 M7 BM DENT+ 0.00 CURVE 1: SP1=100;SP2=60;SP3=20 1007.ASME+ 0.00 2.93 43 93 M 7 81% ASME+ 0.00 2.39 67 59 M 7 607.ASME + 0.00 1 .BB 109 29 M 7 427. ASME+ 0.00 2.2B 132 <20 M 7 20% ASME+ 0.00 5.22 13B <20 M 7 107.GROOV+ 0.00 RUN 43: SAVES-100/§;Sl/1;60/3;42/1;20/6;10/1 SUPPRESSIONS- TSP/1; BM DNT/2 1 490 999 1.85 205 RES M 7 BM DENT+ 0.00 M7 CURVE 1: SP1=100; SP2=60'; SP3=20 2.40 40 100 M 7 100%ASME+ 0.00 2.75 43. 94 M 7 Bl% ASME+ 0.00 2.31 69 60 M 7 60%ASME + 0.00 1 .B6 111 29 M 7 42~' ASME+ 0.00 2.23 132 20 M 7 20% ASME+ 0.00 5.05 137 <20 M 7 107.GROOV+ 0.00 RUN 44: SAVES-100/6;81/1;60/3;42/1 ;20/6;10/1 SUPPRESSIONS- TSP/I; BM DNT/3 LEVEL
Page 22 of 27 PLANT UNIT S/G LEG REEL TO REEL DATE
- MIZ-18 QUAL D2S ST IN- RUN VOLTS DEG 1 490 999 NA NA NA CH# LOCATION 1.55 208 RES M 7 BM DENT+ 0.00 11 11 01/30/89 EXTENT M7 CURVE 1: SP1=100;SP2=60;SP3=20 2.09 40 100 M 7 100%ASME+ 0.21 2.48 44 92 M 7 81% ASME+ 0.00 2.13 67 60 M 7 60%ASME + 0.00
- 1. 72 107 29 M 7 42% ASME+ 0.00 2.07 128 20 M 7 20% ASME+ 0.00 4.70 133 <20 M 7 10%6ROOV+ 0.00 RUN 45: 400-600-100 11 MIL DENT SAVES-100/3;81/1 ;60/1;42/1 ;20/3;10/1 SUPPRESSIONS- TSP/1; 11 M DENT /1 490 999 1 .32 200 RES M 7 11 M DENT+ 0.00 490 999 M 7 CURVE 1: SP1=100;SP2=60;SP3=20 1.54 40 100 M 7 100%ASME+ 0.00
- 1. 85 43 94 M 7 817. ASME+ 0.00 1.56 70 60 M 7 607.ASME + 0.00 1.29 108 31 .M 7 427. ASME+ 0.00
- 1 490 999 1.54 130 20 3.32 131 <20 M 7 20% ASME+ 0.00 M 7 107.GROOV+ 0.00 RUN 46: SAVES-100/3;81/1 ;60/1;42/1;20/3;10/1 SUPPRESSIONS- TSP/1; 11M DNT/2 0.98 195 RES M*7 11 M DENT+ 0.00 1 490 999 M 7 CURVE 1: SP1=100;SP2=60; SP3=20 1.39 40 100 M 7 1007.ASME+ 0.00 .
- 1. 71 41 98 M 7 81% ASME+ 0.00 1.54 67 60 M 7 607.ASME + 0.00 1.33 104 30 M 7 427. ASME+ 0.00 1.61 124 20 M 7 20% ASME+ 0.00 3.52 124 20 M 7 107.GROOV+ 0.00 RUN 47: SAVES-100/6;81/1 ;80/3;42/1;20/6;10/1 SUPPRESSIONS- TSP/1; 11 M ONT /2 490 999 1.14 205 RES M 7 11 M DENT+ 0.00 490 ggg M 7 CURVE 1: SP1=100;SP2=80;SP3=20 1.41 39 100 M 7 100%ASME+ 0.00
- 1. 68 42 95 M 7 817. ASME+ 0.00 1 .40 72 60 M 7 60%ASME + 0.00 1.21 111 30 M 7 427. ASME+ 0.00 1 .46 130 20 M 7 20% ASME+ 0.00 LEVEL
Page 23 of 27
- PLANT UNIT S/G LEG REEL TO REEL DATE
- MIZ-18 QUAL 025 ST IN- RUN VOLTS DEG 490 999 NA NA NA CH# LOCATION 3:14 131 <20 M 7 10%GROOV+
11 0.00 11 01 /30/89 EXTENT RUN 48: MIX IS 400-600-100-10 11M ONT SAVES-100/6;81/1 ;60/3;42/1 ;20/6;10/1 SUPPRESSIONS- TSP/1; 11M DNT/2 490 999 1. 18 205 RES M 7 1 lM DENT+ 0.00 490 999 M7 CURVE 1: SP1=100;SP2=60;SP3=20 1 .48 40 100 M7 1007.ASME+ 0.00 1.81 43 94 M7 817. ASME+ 0.00 1.50 69 60 M7 607.ASME + 0.00 1.22 109 30 M7 427. ASME+ 0.00 1.55 132 20 M7 207. ASME+ 0.00 3.32 133 <20 M7 107.GROOV+ 0.00 RUN 49: 400-600-200-10 15 MIL DENT SAVES- 100/6;81/1;60/3/42/1 ;20/6;10/1 SUPPRESSIONS- TSP/1; 15M DNT/2 490 999 0.82 183 RES M B SUPPORT + 0.04
- 490 999 0.77 38 100 1.03 39 97 1.08 63 60 0.89 90 32 1.04 108 20 M8 M8 M8 M8 M8 M8 CURVE 1: SP1=100;SP2=60;5P3=20 1007.ASME+ 0.00 817. ASME+ 0.00 607.ASME + 0.00 42% ASME+ 0.00 207. ASME+ 0.00 2.14 109 <20 M8 107.GROOV+ 0.00 RUN 50: SAVES-100/9;81/1 ;60/6;42/1;20/9;10/1 SUPPRESSIONS- TSP/1; ISM DNT/2 490 999 0. 90 185 RES M 8 15M DENT+ 0.00 490 999 M 8 CURVE 1: SP1=100;SP2=60;5P3=20 0.79 40 100 M 8 1007.ASME+ 0.00 1.03 41 98 M 8 81% ASME+ 0.00 1.05 69 59 M 8 607.ASME + 0.00 0.85 98 33 M 8 42% ASME+ 0.00 0.98 117 <20 M 8 20% ASME+ 0.00 2.05 116 20 M 8 10%GROOV+ 0.00 RUN 51: SAVES-100/9;81/1 ;60/6;42/1;20/9;10/1 SUPPRESSIONS- TSP/1; 15M DNT/3 1 490 999 0.74 187 RES M 8 15M DENT+ 0.00
- LEVEL
Page 24 of 27 PLANT UNIT S/G LEG REEL TO REEL DATE
- MIZ-18 QUAL D2S ST IN- RUN VOLTS DEG 490 999 NA 0.72 40 100 NA* NA CH# LOCATION M8 M8 11 11 01/30/89 CURVE 1: SP1=100;SP2=60;SP3=20 100%ASME+ 0.00 EXTENT 0.99 42 96 M8 81% ASME+ 0.00 1 .04 66 60 M8 60%ASME + 0.00 0.86 91 34 M8 427. ASME+ 0.00 0.99 109 20 M8 207. ASME+ 0.00 2.06 110 <20 M8 107.GROOV+ 0.00 RUN 52: 400-600-100 ISM ONT SAVES- 100/9;81/1;60/6;42/1;20/9;10/I SUPPRESSIONS- TSP/I; ISM DNT/3 490 999 0.82 186 RES M 7 ISM DENT+ 0.00 490 999 M7 CURVE I: SP1=100;SP2=60;SP3=20
- 0. 72 40 100 M7 100%ASME+ 0.00 0.91 40 100 M7 817. ASME+ 0.00 0.98 67 60 M7 607.ASME + 0.00 0.90 92 30 M7 427. ASME+ 0.00 1.07 103 20 M7 20% ASME+ 0.00 2.32 104 <20 M7 107.GROOV+ 0.00
- 490 999 RUN 53: 400-600-100-10 15M ONT SAVES- 100/9;81/1;60/6;42/1120/9;10/1 SUPPRESSIONS- TSP/I; 15M DNT/3 0.78 18S RES.M 7 15M DENT+ 0.00 490 999 M7 CURVE 1: SPl=l00; SP2=60; SP3=20*
0.75 40 100 M7 1007.ASME+ 0.00 1.07 39 97 M7 81% ASME+ 0.00 1.14 61 59 M7 607.ASME + 0.00 0.93 88 32 M7 42{. ASME+ 0.00 1.08 107 <20 M7 20% ASME+ 0.00 2.28 110 <20 M7 107.GROOV+ 0.00
- LEVEL
Page 25 of 27 PLANT UNIT S/6 LE6 REEL TO REEL DATE
- MIZ-18 QUAL ST IN- RUN VOLTS DE6 MIZ18 QUAL NA NA NA
% CH# LOCATION 11 11 NEW.MIX/ANALYSIS CURVE PARAMETRIC STUDY DAT 3/ 1/89 01/30/89 INDEX 490 999 7.68 40 99 3 100%ASME+ 0.00 27-26 5.93 83 76 3 81% ASME+ 0.00 80-26
- 6. 12 109 59 3 60%ASME + 0.00 133-26 4.90 133 39 3 42% ASME+ 0.00 186-26 5.00 153 20 3 20% ASME+ 0.00 239-26 8.98 149 24 3 10%GROOV+ 0.00 286-20 7.15 28 70 3 SUPPORT + . 0. 00 339-32 76.29 181 ONT M 1 4M DENT+ 0.00 392-20
Page 26 of 27
- PLANT MIZ-18 QUAL ST IN- RUN VOLTS DEG UNIT NA S/G NA LEG NA
% CH# LOCATION REEL TO REEL 24 24 DATE 02/02/89 EXTENT UNT MIZ-18 QUALIFICATION DAT 3/17/89 ANL B. CURTIS II I REL 24 OSK 3S <3RD STUDY DISK>
DEF WASTAGE PRB 540 SLF NEW.MIX/DATA ANALYSIS CURVE PARAMETRIC STUDY EVALUATION OF 540 PROBE RUN 54: SAVES-100/3;81/1 ;60/1;42/1120/3;10/1 SUPPRESSIONS- TSP/I; 4M DNT/1 1 490 999 1 .15 226 RES M 2 4M DENT+ 0.00 M 2 CURVE 1: SP1=1001SP2=60;SP3=20 1 490 999 3.39 39 100 M2 1001.ASME+ 0.00 4.52 40 98 M2 SIX ASME+ 0.00 3.66 68 60 M2 60%ASME + 0.00 2.93 109 30 M2 42% ASME+ 0.00 3.30 131 20 M2 20% ASME+ 0.00 6.51 134 <20 M2 10%GROOV+ 0.00 RUN 55: SAVES-100/3;81/I ;60/1;42/1;20/3;10/I SUPPRESSIONS- TSP/I; 4M DNT/2 1 490 999 0.83 228 RES M 2 4M DENT+ 0.00 M 2 CURVE I: SP1=100;SP2=60;SP3=20 1* 490 999 2.82 38 100 M 2 100%ASME+ 0.00 3.82 40 96 M 2 81% ASME+ 0.00 3.10 67 59 M 2 60%ASME + 0.00 2.48 108 29 M 2 42% ASME+ 0.00 2.85 129 <20 M*2 20X ASME+ 0.00 5.63 132 <20 M 2 10%GROOV+ 0.00 RUN 56: 8 M ONT SAVES-100/6;81/1;60/3;42/1;20/6;10/1 SUPPRESSIONS- TSP/1;8M ONT/~ Z..,.. 490 999 2.36 218 RES M 2 BM DENT+ 0.00 490 999 M 2 CURVE 1: SP1=100;SP2=60;SP3=20 3.64 37 100 M 2 100%ASME+ 0.00 4.66 40 96 M 2 81% ASME+ 0.00
- 3.74 74 60 M 2 60%ASME + 0.00 3.40 118 28 M 2 42% ASME+ 0.00 LEVEL
Page 27 of 27
- PLANT UNIT S/G LEG REEL TO REEL DATE MIZ-18 QUAL NA NA NA 24 24 02/02/89 ST IN- RUN VOLTS DEG 7. CH# LOCATION EXTENT 490 999 3.91 133 20 M 2 20X ASME+ 0.00 7.77 13S <20 M 2 10XGROOV+ 0.00 RUN S7: II MIL DENT SAVES- 100/6181/1 ;60/3/;42/I ;30/6;10/1 SUPPRESSIONS-TSP/l;llM DNT-2 490 999 1.69 216 RES M 2 llM DENT+ 0.00 490 999 M2 CURVE 1: SP1=100;SP2=60;SP3=20 2.41 38 99 M2 100XASME+ 0.00 3.04 41 96 M2 SIX ASME+ 0.00 2.37 75 S9 M2 60XASME + 0.00 2.23 121 26 M2 42% ASME+ 0.00 2.6S 132 20 M2 20X ASME+ 0.00 S.23 13S <20 M2 10XGROOV+ 0.00 RUN SS: IS MIL DENT SAVES- 100/9181/1;60/6142/1;20/9110/1 SUPPRESSIONS- TSP/1; ISM DNT/3
- 490 999 490 999 1.S0 2S RES M 2 ISM DENT+ 0.00 M 2 CURVE 1 :SP1=100;SP2=60;SP3=20 2.07 36 100 M 2 100XASME+ 0.00 2.S7 40 96 M 2 81% ASHE+ 0.00 1.97 84 60 M 2 60%ASME + 0.00 2.0S 123 27 M 2 42% ASME+ 0.00 2.3S 132 20 M 2 20% ASME+ 0.00 4.66 130 21 M 2 10% ASME+ 0.00
- LEVEL
Page 1 - 8 8.0 STATISTICAL ANALYSIS Defect data was collected as described in section s.o, Technique Specifics, for all defects contained in the sample matrix (Section 2, attachment 2-A). Wastage, IGA and . circumferential slit (crack) defect standards simulating the actual de~radation present in the Palisades steam generators were examined. The total number of defects tested for each degradation type is as follows:
- NO. OF TYPE DEFECTS COMMENT Wastage 93 61 ASME pit type defects and 32 large volume wastage defects IGA 193 Two defects per standard were tested and metallurgically examined to determine actual defect depth Crack 30 Circumferential slit defects Each defect was examined five times with each individual probe. Five probes were used from each techni~e. Data analysis was performed on the data collected with the first four ~robes and first four examinations runs. The fifth probe and fifth run were only *analrzed if invalid data was collected during the four initial probes/runs.
Data analysis was performed by a team of four Level IIA analysts under the supervision of a Level III analyst. None of the analysts had prior knowledge of the depth of the defects being analyzed. Following data analysis, the eddy current results for each technique were merged with the corresponding defect depth data. Attachment 8-A contains printouts for each data base. Detection limits were established for each technique by reviewing the eddy current results for the most shallow defects which were consistently detected. For example, the 580 bobbin probe detected all 20% through wall defects which did not contain dents. The detection limit for this technique, for defects without dents is, therefore, "20%" with a 100% assurance of detection. Statistics were performed to determine the mean difference between the eddy current reading (ECTDEP) and the actual depth measurement (METDEP) for each defect:
Page 2 - 8 H
~ [ECTDEP_A. - METDEP;.]
Mean Difference = N Metallurgical examination of the IGA defects resulted in depth measurements based on: 1. Average IGA front (AI), 2. Maximum average IGA front (MAI), 3. Maximum penetration (MP),
- 4. Average stringer depth (AS) and 5. Maximum average stringer depth (MAS). Statistical analysis showed that the 580 bobbin, 4C4F and 8Xl probes all responded most accurately to the average IGA front measurement. This is consistent with the ~revious 4C4F IGA qualification conducted in 1984.
Statistical analysis of the IGA defects used the average IGA front measurement for METDEP in the mean difference calculation. Areas of degradation which were not detected and nonquantifiable indications (NQD's) were excluded from the mean difference and standard deviation calculations. A limited number of data points were treated as statistical outliers in accordance with generally accepted statistical practices.
- The results of the statistical*analysis follow. Table 1 contains a summary of the results
- Page 3-8
- TABLE 1 STATISTICAL ANALYSIS
SUMMARY
(Based on All Data Points Bounded by the Given Defect Depth and Dent Size) Defect Detection Defect Dent Standard Technique Type Limit (%) Depth (%) Size Mean Deviation 580 Bobbin Wastage 20 > 20 < 8 2.95 8.03 540 Bobbin Wastage 20 > 20 < 8 3.27 8.55 580 Bobbin IGA - 30 > 30 < 10 -4.18 8.39 Average Front
!GA - 30 > 30 < 10 -25.19 15.19 Maximum Penetration
- 8Xl Pancake IGA -
Average Front IGA - 30 30 30 30
< 10 10 -2.62
-23.64 18.78 22.25 Maximum Penetration 4C4F Pancake IGA - 30-38 > 30 < 10 -0.52 14.67 Average Front IGA - 30-38 > 30 < 10 -22.70 18.81 Maximum Penetration 8Xl Pancake Crack 35 > 52 < 10 0.51 12.54 4C4F Pancake Crack 50 > 52 < 10 5.73 12.53 MRPC Crack 35 > 52 < 10 -11.30 11.89 MI0889-1691AA-TC01
P_age 4 - ~
- 580 Bobbin Probe - Wastage Defects Detection limit:
20% through-wall for defects without dents with 100% assurance of detection. 20% through-wall for dents up to 8 mils radial with 84% assurance of detection. 30% through-wall for dents up to 8 mils radial with 100% assurance of detection. A 20%-100% through-wall defect residing in a 10 mil radial dent will be detected with 80% assurance. - Ability to detect defects residing in dents larger than 10 mils radial decreases rapidly with increasing dent size. Sizing Ability: Sizing results are based on defects greater than or equal to 20% through-wall with dents ranging from 0-10 mils radia*l
- Sample/
Dent Size No. Defects (mils) Evaluated Mean Standard Deviation All defects 685 2.95 8.03
>= 20%
Dent <= 8 Dent = 0 122 1.94 6.23 Dent = 2 192 3.05 6.21 Dent = 4 191 4.13 6.23 Dent = 8 180 2.29 11. 62 Dent = 10 199 -1.14 12.83
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., Page 11 - 8 540 Bobbin Probe - Wastage Defects Detection limit: 20% through-wall for defects without dents with 100% assurance of detection. 20% through-wall for dents up to 8 mils radial with 72% assurance of detection. 30% through-wall for dents up to 8 mils radial with 100% assurance of detection.
- A 20%-100% through-wall defect residing in a 10 mil radial dent will be detected with 83% assurance.
*. Ability to detect defects residing in dents larger than 10 mils radial decreases rapidly with increasing dent size.
Sizing Ability: Sizing results are based on defects greater than or equal to 20% through-wall with dents ranging from 0-10 mils radial
- Sample/
Dent Size No. Defects (mils) Evaluated Mean Standard Deviation All defects 671 3.27 8.55
>= 20%
Dent <= 8 Dent = 0 125 1.00 6.59 Dent = 2 193 3.25 8.12 Dent = 4 179 3.74 9.58 Dent = 8 174 4.44 8.87 Dent = 10 215 4.91 14.40
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---~-~*---~~~t~~~~:tH'i*14~#~}!i}fJ541$\1.!MW,iiflfW
)
* ~:.i40 WflSlflf,E *-* ECT ,.
- VS MCI l>EPTH HY l>EI\
Al..L J>E; DEN1=8
. :r.E'.
B l.b: 2;* HONl>AY, AUGUb r ~1 1., 1.*****I * \
- [
I 1... t PLOT OF ECTDEP*METDEP LEGEND: A t OBS, Et = 2 OBS, ETC. I 90 + .*
,rr---+---*** ,....
, *:C________L. D c A A A H Z E A [I I' )" It 80 + I A [t e** - . B c: A [C *
"l:_~
)",, I rI if A A A B A A A A A 1*. 1:: A )'*
*. -*-r----
I I I Et C A 9-*--1f******** A A A *
,,~,
60 +
... -------***- .I B
A c A i)"
- ..-~~~
- I F.
t* *I (I [t A c
" I B c (I Et (I
- 1*=
1.
,, :r.
so ---~ ~--**- ECTDEP I
* --'--*- - .... ~ .. I A
A E c A 8 A A B A
~
t* .... 40 + I A c: (I Et c A "c=*--. )*.* I A
.. A *")
... 30 + Et (I
- I I*
"['*-----, I I
- I
... .*--*~***-*-**+ I I
- r-.
IA I 'tJ
~CD
.... to + I I I
'.J\
- r*_ 0 +
I
**** **** ********- ****t***** ----******---*****-**! ................. ****-**-*I**-***
I* Jo ..... --+--------****+- -*-*------*--+-..-- ...... ****-**-*I**-****** ... ******** **-****** *-**. ***-:*** .............. ...... 0 *****-*** --*---* ......*... **--***
... ~'."iO
.... t:~*
l.iO 1,:*; 10 -1~:; UO 20 25 30 3!"i 4() 4 **' . h.J
~11*:1m:r* '
o=[,, NOTE: - . .. 1 096 HIDDEN i
; "11
-------~""~
I
.:h
- ,r=--
* ~----
!.HO WABTAGE -**
EtY l>l n::*1** ALL. DI:.. *~.*.;TS i>ENT=10
\"TH
'l.ZE vn MET DEPTH le',: ~.'2 MDNl>AY, AUGUST ~.'i,
*-*II 1-.
Pl.OT OF ECTDEP*HETDEP LEGEND: A 1 OBS, B 2 OBS, ETC. i.
** 90 +
I r---- r.
**'[...
.. **.*~--- eo 1
I
*-*+*-***
I
--* c A
A A A A f.t A I> El p A (I A. 8 (I A A
" I -*-.
.--rn- A ii I>
I*
~)
"~
(I A A A A c
***.. '.1 :: 70 I
+A D A C A
.. - . r* A-** ....... -A f:
A A A A A I>
.,, I A A A B (I A c
.:1**
,. I A A A [1 A
.. D A ... ----*
< 60 ! ~-- A A E G D A
(I I
- "~------- :-- c A CG B t~
**9** e (I A A C
." " I A c D B
*9* --**--
A
"~'* *. -+*v*-*----- A
... *;,;\ I B D A
*rr11:..._-----*- ECTDEP I
-r .... D J:<
D E A c
.. 40 +
I A A A
**F:**r*- --------. A 111**
f.t B I
-**----- -~ B (I
; *--- A
** 30 +
- I
.. ~--~- !.
..l~. ----- +
*1" .* .---.l---;zo--
I A
..."[ - lI 'U 10
+
I I I A
~
t-'
*{.
- 0 +
--+---*+-*--+---**t---**-*+*---*+*---****---*+-***-*-* **
. - - - - - . *20 22 24 26 28 30 3:'. 34 3(1
- 30 40
-~*-* ... -.. I ......... f *- .... **f****
42 44 46
......f ....... *f ...... *****I*-
4fl ~*;o ~*::!
--*---+---+----+*---+---+---+--*+---+---+---+---+---+----+--
~.i4 ~;1, !'m 60 1.:'. 64 1.1.. bO 10 *n *74 "76 71:1 Bo
~
( . t11' 1 l>FF'
,,:1 . . . . ----------- . *- 1*
1** t f. ~~~"."1l:'Ellg~ ~::- ___..._ __.__..;~i~'.:l~illlW.a~
Page 18 - 8 580 Bobbin Probe - IGA Defects Detection limit: 25% through-wall for defects without dents with 100% assurance of detection. 30% through-wall for dents up to 15 mils radial with 88% assurance of detection. . Ability to detect defects residing in dents larger than 15 mils radial decreases rapidly with increasing dent size. Sizing Ability: Sizing results are based on defects having an average IGA front greater than or equal to 30% through-wall with dents ranging from 0-10 mils radial (sizin~ of defects residing in dents greater than 10 mils is incon~istent). Sample/ . Dent Size No. Defects (mils) Evaluated Mean Standard Deviation
- All defects
>= 30%
Dent <= 10 1010 -4.18 8.39 Dent = 0 128 -4.86 7.82 Dent = 2 176 -7.56 7.15 Dent = 4 192 -4.38 7.81 Dent = 6 174 -0.92 8.08 Dent = 8 149 -6.36 6.68 Dent = 10 191 -1.68 9.99
' I [ ECTDEF' I l't.. Dl
'."1UO JGf\ *** I: CI OF ECll>H'MAJ.
DENTS <"" 1 LEGEND : A DF *V~i. *I
'~' i Ml* I 1!1:'.r"rl I
""" :*~o Ol.1B, B ~! Olt!:i, ETC.
ll>: /I I MfJN!lrW' 1'11.h:;w:: I :: J ' 1***1 D A
. . ... - -~?.-.. *-*** - .~ fl I
I
'[-*----*-,----
- 80 +
I 8
--** -- *- ---F p E
P LKI AAC c BPY H A B If D BA
* --*-**-*----*!*---*--- I l>B C A B AOB ("
I CA 1-1 c A fl [I FIA I A A B Et [C A AA
"[ 70 ---+*-- *----*I ii Et F A DCB D E F
- .. *-----r:... A CB Aft A
A ***- A A A E I AB A CA A 60 + A G A BD F ABA .. ****-** .... A
.., 1---*- A A. F BD 8 G 8 B A 8 A A A A AAE C A E A B
" 50
-** --: +
A B B C A Et AA B f' (I Et A ACA A C B i>Ail A BAC AC DA AD AD E B D 1-1 D E: A EFC FEE BGB flt A H c A C A G G E (I it A I D
- i----* :- tll>C AFA A F
B A M tAe BACBACAA F F D C C IA ij[l(I c E: E: A A
*~L_.. ----~ I CDA A B BEDGBCBBA 8 E I 8
'40 +-. AB A A AAAF Aft (I B Gi! [c
" I D E A AEIBACDA EID C El I A A l>A A BllADAAA c A A
' ' [_ _ _ T_ A C A rncti\ B r:: c A AA AB A FCABD B
- . *--- :1o_ _____ f A A D
c OB E C[I C B DA D D B A le A
! G EA A A A I A A c A B A A fJ =[-~~-*--!
AF"A D A AA A
" -*- ------ -* ... II 8 B A A A A [I I c A A "[---iu-- -
u I
- J.
I A c '-cl
~ I
---------*- I ~ro 0 + ,_.
*.o
*-- -*** ,._._ ******- ...*---*+-***** ........ *-*******-..**---**--*-****+- *---**--*---*+-*- *-*--**-*****-**! -******** ********** . ....... -* -** ****-**
~[_.
-~-+~---~--*-------+-------+-------+-----**-+------- ---*****
c:*r** 60 (",'.'.} *70 1'5 80 85 '?() 9'..'i 20 25 30 35 40 4:; 50 ... 1 *. 1
")()
(1T ,~,:L
* ~';no r.r.ri *** r:c1 m . n Ml: 1 n1:.r-H1 DFNTS uv ni:::.
<"' H. *
- zr 11 >~ :m i b * 'l I. HUNl>tiY, (ll.11 .* l.l!'i I ::I, 1******1 ...
r 90 + PL.OT llF ECTDEP*AI l>ENT=*O LEGEND : A = t Ol:l!:l, 0 2 OBS, Ere. I
------ -1 I
. - BO --- --**+I I
I A fl
- C::~. ~-f-- .
[t (I 1 .* A B F I,. E F I E I
"[ I
__ }. I c A (I
" I D
"[-~-+*
,. I c A
,. Et:TDEP I D A B
.. --- 1-*-~ 9 A c I D I c 40 + (I [f
**r-* * *-*
--.I -** F-""
A c D
,. I (I c
--** - *----,---* F.: Ee 30 + A A I D
- r-. ---: G
*-. -w-*-**-t:. A I [I I A
- r-*- . =-- --*-r 'U
*----*-*** -- ., Pl 01:l CD *r--*
0
-T-*
. ----*---;ro-*- 32.
I I
+
-+----+-*---*+-----t*-*-*-*-+--**--*+--*****-**-t -**-** ***+-** *****-*t*****- *** * -+ * **-*** ****t*-
34 36 38 40 4::> 44 46 4R ::iO
***-**** I*** *****-*I *******
0.2 54 I*******-** I*-* * **-**-t****-*- -***!*********-*-+*--**--*I*****-******+ ******-*-+-***********I-***********+**** ****** *I*****
'.'!<'. !'Of.I 60 t..2 64 1.tl., I.I] 70 7'2 74 71.t
*n1
- io I'll
,_,:*r
! I
* ~'*DO *11.<' **** n~ ~f; DUH S <,~ H>° I O" i:cv or::: :zr (II Ml_ r m:r 111 PLOT OF ECTDEP*AI LEGEND : A =' 1 OllS , [c "' 2 OE1S, ETC
- ECTDEP I
- r-------:
110 ***
... --rou-- -*+* -----***
I I
- r-~-!-* ---- E
.. I Ft
,, **-*-*----*-r-** *-**- - .
I Et I 80 + H
**1 r**-- c I. ~ .----ro--1---
f' A F A D r.
. AA A *. 50 +
[IC DA A A c A If A [l A-H
-A DA A HA F CEI D H AC A HC *.. AA fl [I A Et [I ~~f-.L---30---~+-- --*--**-* -- *-- -* - A D A
- L _____ ._ -i-
" I A 20 + D ~~-**--
II c
- -*--iu--**--L I 8
f'
"[---*r* I
= 0 ~-+-------+-------+-------+-------~---
"' - ._.. -------- 20 25 30 3~.. . '1(J
*****f**-* **- *-*** -*. *O **
~5 r;o
(.,() 70 7~; (ll) fl!'.i 9() (?!'.'* fi I -~[___*-~.~-~
* '.AJO .I (;(, :... EC"I . m:-r . : ; ML r IJl'.F" I H EtY J>Et DENTB <=* l.O.
'ZE
.I °>= ~:SO
\
I i (,: 111. ML!NDl'\Y, Al.Jf,l.J!:; I :.,1 , 1".****~:. I r*------- f'LCIT OF ECTDF.F'MAI LEGEND: I>ENT='I A "" 1 ems, [l "" 2 OBS, ETC.
*c___ -----* }- -
90 +
- __________ L_ F' 80 ...
I ,,c=:=-1*- .. 70
-------**r*---*****--.
+
I I H B A
" I I A A **~---r
.. 60 + G B I A A F A AA B c A F [I A El> F A A FA A
- .[-- -:T:EP--:
-*- -* *-*---------*1 A
A A A (l[l II B AEt I l:l (If.I 40 + A A D A A t llA c
- [.. I c A A BA A 30 +
I I K II A Et t c D EB A c I> D
,,~--1 A
" I fl A A o<V
- -- -I
+
I A I
"[ ,--
~
1-tj
- _. ____ 10_____ &:
(])
,------.**** 0
*--*-----*- *34
+ - ...
--+----+----+----*+---*-+*-*-*-******-+*-*-**--*-+*-*-****-*I*-*---**-*+-***-****+***
36 38 40 42 44 41,, 40 ~'iO ~*;::*
*****I *-***** *+*******-****I*********** I
~34 ~-_:;1. ~*;n /,(\ ~2
*I*-********* *l**-****-**-+*****-******-*t-- * ****--* I*-**** .. -*+*---**-*i*-*****"****I*-**- *---*I ****-*********-t ******-******!********
64 6~ 60 7<> 7~ 74 76 78 *no R~ N N 00 (l I ,..[
--- . ---~--* - . **- .
f'
- ~
rJ-
* ~.-.no lGr'.<\ *-* FCI J)f'.V!:i MLT l>EPHI DFNTS BY DE
<"' .1. '*
DENT,,,6
*zl:
ol )'" ::110 1 .-, : 4 l t1f INDrW. Allf;IJ!:.T ~.'I ,
.1."'.l.
r*un UF ECTl>EF'ttAI LEGEND : A "c :I. Oli!'l , D = 2 OBS , ETC
- r*. *10 +
'[ ___ .. _ _ TI ___ ...
r ' I
, ..... ___ ~ _____ I K K
.,, *:1u *t- Et A A r* " I Et c [I
" I A I*
f "[
-~---;--
---. I
-H
[l B I D A A A "':.."[:. 60
-1
+
I [i A (\'> .. I D A c
. I Et
-,r-- ...
[I A E c -* D D
~
[i "i=:".'.- A c {~ EcTDEP 1..... .,,.c B A D E f'., D A C D
.. 'L"-'-"- -*- I [i
'l A A
~ I I
- A E
., 40 + A
------g-*
**~"
E'. 1>
*,: . I
~ ! ,'. . -T A A
. 30 + c [I
- E c
-*E A
.."[
--. ..-. '!:!O'
*+
A A A A A I
.. r-----~
I
- i . 10 - . ~ "'d Ill
()t) I CD I N
~ --!
w
.~ --+ ---------+- 35 --- --- -*--- ----;;-
40 ,
..... ... ****** ****** I. .... , ......... _....,. ,
.... ................ ... .. ..... *-* .. f *~****
" . 30 '.'i() r.*r. ;.1') ,{, ~..; "/(! ',.'.'i 1:10 w:. ****) CX>
{,I
,. [
- j
* ~*,fl() 11:;A .... FCI DENTS <== H*
I~!:'.!;'. IW DE:. DENT=8 l.f.: HI::. I m::PIH tI >"* ;m 1f,:11 MONI>AY. AUGU!:: I' :?l
- 1***1 *
- r-PL.OT OF Er:TDEf'ttAI LEGEND: A 1 Of.IS, Et 2 OBS, ETC.
** 90 +
I
** *r-*- ---.- I E L F' p
' ... - *----*-- I
~ 00 + D A
... I A
,, I [I A " [ * - - - - - i - -*-*- --A**
B A
- _. ___ ?~-------~
... I I
A A ...**c*----1 60 I
+
I I E A F r. A A ... I A A E
,. I *CA Et ":r [ '*--so-*---+- [t c
... ) I A AC A
,,. ECTDEP I E Ee * -*-..------r--- . A Et [t
... I [I A
- 40 + (I fl fl A A c A
- *' ,' [
- II
...."--------r 30 + I A [t [t A A A
- 1
. - -A* A I
I A
* .. ""20 -- - + A
- r**-- I I
'::t ....Y~- --
+
I A 1-rj pl I oq
' .. I I
CD
"(--------* -- I "".i:-
r 0 +
~* --+-----*-*---+-**--------* . -*-+****-- *--- . ****-*******-****** .................. *****-******** ***** I. **** *-*I ........ ......... *--~** t**-**** .......... ****-*** ..... *** :>:>
" .... -------------- 35 110 '15 ~o e-r.-
**'*** 1.,0 /,!**, /() *r; no fJ~j r,10 <<;*~**
*c I I*
r ***-------*-*---
"'I
* :**;no 1(,(1 **
- l:CI BY DE J>E:NTB ("" t<.
DI **~ /.L 11
- Ml. I 1.11 I' 111
)"' ~~()
I;, *1 I 1*;1 Jtll ,,:,y, ()(.!i.Uf, I :*i , , ..*. ,
- r---- *---*- DENi.,,10 F'L.Ol OF ECTl>EP*AI LEGEND : A "" 1. OBS, B "' :2 OBS, ETC.
+
*c*----.---
'70 I
- I F I I
10 t:JV + f' I A II A "l~
"**.*-*___ 70
-.-- I I
+
A A DB tA c [I A H i>Efl l
- 60 I
+
A CEI CA ABA AB
-**- -- ---*---A A
A
,, ;, I B B El " . -* __ ._______ r--*-*** A c B l ~
- so I A I
+ r-I C A
(I A
- -**u 11 A A
B c D
-A*
A (I A
., . ECTDEP I 8 11 A c E !; " ****---------rPI*** A A A A
- I C A El A (I
., 40 +A A A (I
- . - - - - - "£-**A
- J Ll *~ ' ::
I
-.11-AA Mi c El A
A l . 30
+
I I I Dl:l All c A
- I 11 F
* .-*--:zu-*--**-+**
t lO I **- ----- - A A [I
'1j'
~Cll
-'.;_, +
'I ,N
- r.
U1 0 +
-------:ro-*
--+---------+---------+
35 40
. --------+-**-------+----
45 c.o
*--- 5:'0
******- ~***
(,()
.. ***I** *****-**** *** **- *****---t ***-*-*--*-****-**--***I**-******-**-*****-**-*-**.. +**--**-*---~-*****--*
b5 70 75 1'10 0 ~* I*****--... ** *-*-***********I****-**
, .. (-!*>>
':¥J
,_,:L.;...._.*- - - --=-
Page 26 - 8 8Xl Pancake Probe - IGA Defects Detection limit: 15% through-wall for defects without dents with 96% assurance of detection. 30% through-wall for dents up to 15 mils radial with 88% assurance of detection. 40% through-wall for dents up to 30 mils radial with 88% assurance of detection. Sizing Ability: Sizing results are based on defects having an average IGA front greater than or equal/ to 30% through-wall with dents ran~ing from 0-10 mils radial. Note that sizin~ of defects residing in dents g~eater than or equal to 2 mils is inconsistent. Sample/
- Dent Size (mils)
All defects
>= 30%
Dent <= 10 No.* Defects Evaluated 881 Mean
-2.62 Standard Deviation 18.78 Dent = 0 90 -5.59 9.53 Dent = 2 156 -11.33 15.14 Dent = 4 167 -1. 31 19.28 Dent = 6 163 -2.30 19.36 Dent = 8 145 1. 08 23.48 Dent = 10 160 2.48 16.97
- r- ---~~~~~p
- r*un m:
UX1. IG(\ .... FCI 1)1:.b Ml:'! IJLJ'."111 ECTl>EF*AI DENTS <" j_
- LEGEND: A ~
I ) ,,. :rn 1 DBS, B 2 O[IG, ETC. 1 b: '\II i*111Nl1r1Y, Al.11.l.lh 1 ~:1, 0 1 ,. . .
\
* . -****no-**-+-
'[---* ---.----
- t.00 I
+ . .. -----*--- -***I .
A
" I
" 90 + A A AH t DA
~c:-~r-Al D C B B D *DH FD l>Al A A A A A c BD E*FC tJ DB i:: D D A c Dl>D ECA n I F A A B AE c E [I [I A Ell BEi
*1 .----- --- . C GB AC
~ I A A fl AAA C AA (I B E I) (I fj le C l'.il'I A i) IJ A Ail t a t: Et [I B A A A A CC All A BA A AA fl A I A llD A A c C B A BB B BA A A (I B ll re A D l> AAB A Ee A t:A E: AA A A re
*.. A C A AA C A 'BC c BD A D B BB 60 + D A A [I [I AA El B B ED A A flA c [I (1 A
- f; . *: _.___ A c
A A A B AB A A AA AAB AA A B A A B B B [I CC [i A A A A A A A
. ill'f' A E
A A
._;*--~-*- + le A lt l':I Ale t:A C AC A [I A A t.
- A A Ef[C [I A A C: A c
.*r,,___- , A A D DA A r::
A AA BD A C A BC CAC'! D A D A fl A
- ra*---- . ---*--
~o ~ A DA A A A AC BAD c
FAB D c (I A
. r ,,,. A AA CD D DI~
B AA C l':I CM C (:I i) (I A
** B A T -----
(I [* A HA A E 30 + A B B A BC A A [I EC A F A
/ft - r:.
~~-~-
A AEi A Ee A A
--rn -- AB A (I C A A HA B c fl A [I A A A lf Et A A
, AA A A
A C c AAF* AA l':I A A A AC [I A A A A
" I r. ABA [I fl l)(c A A A
- r-~---! A Ii A
A A A (I A A AA [I A A A
*t __ -~ I A AA
>i::J Ill
=c--- . . * -* *- - ;)(*)-* . *- - ; .-* - .*- .- - . . _._ . *- - - _._*- . _. . .
"-*-* - *-*-*- . I A m:c A ,,,. (Jtj CD I A A A A 0 + N
--.I
"";~~-----;~------ ---~~- ------;;----------~~ ~~;------ --~;;;- ~;;- ;~ ~;,--*-* -----~~~ -~;,--- ;;~~ --;i';~ . . . .
00 AI
*[
'~':'* ~--* ---*- ---- ----. ~
- DFNTS <= l.
Ft: I BY I>I I\'. Vb ML I Ill. AI >* 30 l>l::l' 111 I ..... -l4 MIJt~l*flY' At.11 .* w:; r : '.I.' ... DENT=<> PL.01 llF ECTDEF'*AI LEGEND: A
- l OBS, B
- 2 UBS, ETC~
90 + I
- 1- *- -------:-- (I F!
---0~- .. --:,. ..
I l* A
,, I A [. " r-*** A I)
I.
- [ __ _I!>__ -- f A A A A
ll
" D l-~--
------~
6 r B Et B n I
,. I A A A ,. [ 30 - ..I c ,, _....__ ~tT~. A A
- A A Et 40 + D A A
- t *-----,.
I c I A A c c A I c B Ee
- 30 + A a A
- A B c
~[_-OU -
A B B Et A A
+ A I A . G-,
u d - * ~~- I I
~ *r---. .
I I
~ 0
~+----+----+---*-*+
30 32 34 36
-*--*-+----~.
38 40
-- -*- *--** --+*- ****-**-* ***-*- *--****** *-*- .******
4:1 44 4f:I
.. *** ***- * ***** I****- .-*-*I ... ***-*** I** -*-****! *---**** ***t***--*-***
'.';"' ~.-.n 60 1,2 114 t..lo
***+*- ****-- t**-- ..... +-*-*-* *****-*--**-*-**~*-*** *-*-**I**
110 *10 72 74 71.o 71-1
. -- fl I.
I I* C--
- l:JXj. .IGA *** ECT !)r-.VS MFI DENTS <"'
HY J)E h.. ZE. 1°1: >"~ :~o DFPHI 1. 6 : 'I 'I Mf.INI>IW . AUGl.l!'.* I :-.* I. , Ir. 4 DENT=2
- r PLOT OF ECTDEF'1tAI LEGEND: A m l OBS, B
- 2 OBS, ETC.
100 + I i
- [" I I
A
*-9()" + A I)
---*-* --- --. I I c A
[I F A l
" I
" I c: [I
** BO + I)
. - . I B I A A I A I A
..=r-*
70 I A
- I
.. Et A
A c
- [ *-- ::~~-:
.. *-**----- I AA A
B e B B B c A
- 1-* ----r----
" I c B l50 + AA A
[I c 40
+
AD A AC A A A B B B A (I c
- r--------T *-* I
.A A
A A (i A B C D B
-* 30 + A I> A A I A f A
s--- I I I I> I> A Ir A (.1 li:J
..1 20 + A B Ill oq I r* (])
I I> A I A I:< N
\0 I A .=1*
10 +
--+----+----+----t----+----+----+----t-~--+----1--
44 46 48 50 5' 54 SA SA 60 li7 "4
**I***
66 ~*U 7(i
'/) 74 fl .....*. ,_ ........................ - *...
7(, 10 oo I-*-*** ****-*I***---*--+******-**** l**-**-****-**I * ******-***!****. *-** I** 02 U4 e1i on 90 9~ OJ . .. ft I
- _~[*
- O.><I. JG(\ .... FCT r>'
l.*Y UE l>FNTB <'"' 1<1 . AI V!:i MF I nr.r*1 H
*zE
>~ :~o i 1,: 4 f\Y, Al.tf;Ub I' ~.:.I ,
~*..
r DENl'~4 PLOT OF ECTl>EP*AI LEGEND: A
- l OBS, B
- 2 OBS, ETC.
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B
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30 35 40 4':i ~.)0 ~;r:, ")(> .~,~) '/() 'l'."i f:IO m:; 90 fll l_l=r
- l:J'(i. r.r;.-, .. u:T 1)1_.Vb ML!' J:-LF' Ill DENTS EIY DE
<= ~
'ZF I >= 30
\ ,-, -~ l Mi:lNl*rW, r'\t*1;U!'- I ~**1 ,
- t ,, '
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- PL.OT OF ECTI>C:T'*AI DENT""""'
LEGEND: A
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90 + I
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A c A A A A Et. A
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=~
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+
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- I -- f.io*-* +
I [. A A I) A () AE E Ee "l. -.. - - I F A I A A E B
-*i A [I BA A A " I A A A A c . [I
- 70 + A (I AA c
., . *--* ----*-***-**1* [I BA A I A A E AA c B *-r- -----, I A A (I BA
- . --~-* . r
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A A A A A BA BB A I A [I (t A A A [I
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+
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Page 34 - 8
- --* 4C4F Pancake Probe - IGA Defects Detection limit:
25% through-wall for defects without dents with 94% assurance of detection. 30% through-wall for dents up to 6 mils radial with 79% assurance of detection. 38% through-wall for dents up to 10 mils radial with 84% assurance of detection. 40% through-wall for dents up to 15 mils radial with 81% assurance. Ability to detect defects residing in dents larger than 15 mils radial decreases rapidly with increasing dent size. Sizing Ability: Sizing results are based on defects having an average IGA front greater than or equal to 30% through-wall with dents ranging from 0-10 mils radial (sizing of defects residing in dents greater than 10 mils is inconsistent). Sample/ Dent Size No. Defects (mils) Evaluated Mean Standard Deviation All defects 957 -0.52 14.67
>= 30%
Dent <= 10 Dent = 0 126 -2.52 9.83 Dent = 2 171 -5.16 10.48 Dent = 4 181 -1.99 15.17 Dent = 6 163 2.03 15.12 Dent = 8 146 -0.11 18.73 Dent = 10 170 4.44 14.55
I I
- 4C4 u;(\ -* [.(;'1 l>ENTB <,,.
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------- T I
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nr. l~ Vb HI.. I i>El" ..111 ZE tl >~ 30 I/,, '1 ,' ~\1 INl!(l.l', At.11;1.JF. I .:.* j , t** I* r--- PLOT OF ECTDEP*AI LEGEND: A DENf*"'6
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=1 OF<S, Ft ~ 2 DEIS, ETC.
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fl r ECTDEP PLOT OF ECTDEPMAI DE:NT,,H> LEGEND: A
- i OBS, D
- 2 OBS, ETC.
110 +
*-----*-r
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Page 42 - 8 Merger of 580 Wastage and 580 IGA Bobbin Data The 580 wastage and 580 IGA data were merged to de~ermine the overall accuracy of the 580 bobbin probe on combined wastage and IGA ~efects. No. Defects Standard wastage IGA Evaluated Mean Deviation Defects Defects 1695 -1.30 8.96
>= 20% >=30%
with dents with dents
<= 8 mils <= 10 mils Dent = O Dent = o 250 -1.54 7.85 Dent = 2 Dent =2 368 -2.02 8.52 Dent = 4 Dent = 4 383 -0.14 8.24 Dent =6 Dent =6 174 -0.92 8.08 Dent = 8 Dent = 8 329 -1.62 l_O. 60
_ _i_'.. N/A Dent = 10 191 -1.68 9.99
* !'.ol.10 I Gf., flNI> WI)!:;,
ILn - WAf:>l"Al~I: DL~rs DENT~1
<* lO Co*
DATA HFl:;:GEI> I AI )m 30 B I HEIDEf' >-=* :W i6:51 MONDAY, AUGUST 21,
- 1 I I
*I f"'LOI OF ECTI>EPttHETI>Ef' LEGEND: A .,., 1 OBS, Et =2 OBS, ETC. - -* *-*---J: *:1 r:c*1 DEF' 110 ...
_J: I
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100 ... c I c 90 ... E 8 EIO *I* D AD A A B A F PH ID CHWLIHL BGCOALi>c PIH J c
.- - _J:
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---E:-
- I I
.J C I "[L' . . -6.....-0---.--+*---- --* c i "":,,;. :* I c "'<** I c C! ....
- A
- 50 +
A A (f D F A
- r- I D
.A A
c: A A (I
- l£:L ---~- . . - f"
() Ee I ll A l c c
- 40 + [C B I F c t,._-l A D (f c E B A A I D I D G
='~---r-
. L______ -*-I - .
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- I
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1.*~ 7~; nt f:l" 9:*:i '?9 1 o::; ... HI.° IDET" l_lot!
"'t'
* '.'*0() l(~(l AIJI\ wMr' 11.;A DENTE> <* * . 1)(1 I A MEJ**f,[.J*
I Al >'" *m WASTAGE - I>F.: N rs <'"' ... / METDF :P \ '"' ::?() EtY l>ENr S.LZF l>ENT*,,,2 1 /, '.'* j t-IUNh1'1", (11.Ji.;l.W."f .1 , .,
- I*
- I F'l...llT OF ECTl>EF~MMETDET l..LGENO: A 1. m:ir:, J* :?. Ol:*S, F'TC.
r- 110
----- f*
- - *--1xx-10 V\J
.l
+
I
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[
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c c
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- I UC A A
" 50 + (I DA C A (I u
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[--
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... I B B Cf.I D H
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- I c AA f.I f.I I A H A [I A [I [t
- A. A B A D
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~
, I A I
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**"' f..()
(.,~*:; 70 75 f~ A~ 90 c_;* ~:_:; X> Ml* 11'1 r I - I*
.., [ .
I . -* - -------*
* ::A:lO lGr) 'AND Wllff!.Dfrf'A tU:J\l,[D IGA.- DENTS <.
LJA!:iTAf,E *** DE NT!; <"'. BY DENI' SIZE I AJ >m 30 HETI)FP i'"' 2() 1**
- 1 .. -**- *--*-- ------ PLOT DF FCTDFF'ttHETllEF' LEGEND: A t OE*S, Et :~ DEtS I ETC.
[ -----, ECTDEP I
- ----~-1 I [t z
A
~~
('" F
- [ ___ : *--- -
I A A c E: A F N [t A
., ----~*-*- -~ - A c A BA A i.:
c B I A A CN Ei CH
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-------r "Ic A A c A I)
,,,---r.l30
- 1._ -
+
I (I A A A A (I K B l* c D A A A B J) A
*T_________ :- I I A A
- --- 10 -~ A 1 " I I
- [*--~- ---~-+--------~ ---*-**-
* --- -- - 20 25
-I*- ....
30 _,,_***--~--*- 3~
*--* *-+ .. *-* **--" -+ .. ---* ....... I . ,,,,,,
r-1:-
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70 7::-;
" ....... I -.. ,, ....... " -*I ..._,,..............
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+ .... ' ..........,,
40 , J.
- 111 I T;EI *
;_1:[ ~:--*---~OBS HIDDEN
* :*:.no 1t.o'1 NII> i..1n!il**>co1r1 ru.1.,,_.1:.1*
Hd'I WAH I rir;r. .. m: N n; <: J)f: NT!:; <,.. HY DUH DIZE
*1 1 _,,.,, .10 Ml :*1 Jlr: p ) ,,, :*.~()
- 11. ~-., 1-i11tJ1*,\'r', (\(il,IJ'.:-1 :1.
,,_.,*(*
F'l...O I or ECTl>EP>1HE I DEP L.FGENll : t\ t DBS,. E* ::.~ OBS, ElC. ECTDEF' I
- [** -i* I< I<
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"c (1
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+
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A
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- ii
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- I I
r=-* -~~;----~--;;--------~~----- ---~;,-- I
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/.() 70 1:10 B~."1 )
* ~'.UO lGA 1.1~(1 WAfflAC:.E *** DENTS AtJI* Wt1Bf.**>r1IA l>LNTf:l <,.
BY DEN I" SIZE
'/ Al ., "
METDf:T'
~u: :r: i,[:f*
,~()
>,, ::.*o j/, "*'* 111.JMl*llY, (11.11,UF-I ::; , 1.\. . .
.:r- PLOT OF ECTIJEF'*HETllF.P DENT::B LEGEND: A 1 fl[IS, B 2 Cl[IS, El C.
ECTDEF' I
'[*- -----r- --
- I E A E I I~ L Pf'
*-*- -----80
--* __+!_ . A I) l:CA A A I A A G
,, I E ..... - B ft A A
--- A A A D c
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A B A A DA Et tt A [I I A A AA A I B B
- [--~- A B c A
F
- . ____60------{- :---- c: F G A F E D A
" I B A A A A B E A
- c r: -
II IIA 1
*rr-A A
F c A A D lt c E A E D D B AC
£1 C A (i
E £1 ii 8 A A Et Ac A A B Et 40 + F B B --
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* ;l
~
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u
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+
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40 45 50
~~;
t** i,()
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("1,J 70 m 80 85 90 9~
.i::-
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IGri *** I>ENHi <. l~Mi !AGE ** l>FNTS <,, FIY l>J:NT HIZE
/ AI )-,, :m METDFP >"" :.*o I ... ~- '., 11* INI .,-,y. {)I.II_,( I I :. ) '
** I**
PLO r (IF" ETTl>E.f*HFTOFP l...EGFNO: A
- [----------:-
ECTDEP I F I " ---n~ ... c I A I.I A " I DE< [I
- [
" . 70
----~
T--
+
1 A A CA bt:i<< t Et A CEt Afl A " CA -A-
+ A AEtA A I fl 9 (I
- -A e F.1
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-*- E. -,~
AA A c B .* 30 + A'B Dfl A A
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**-**** .. I-**
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*1~*; no
. tll* JT>l:T
Page 50 - 8 8Xl Pancake Probe - Crack (Circumferential Slit) Defects Detection limit: 35% through-wall for dents up to 10 mils radial with 99% assurance of detection. No data exists for dents > 10 mils. Sizing Ability: Sizing results are based on circumferential slit data greater than or equal to 35% through-wall with dents ranging from o-10 mils radial. Sample/ Dent size No. Defects (mils) Evaluated Mean Standard Deviation All defects 380 2.67 14.71
>= 35%
., Dent <= 10 Dent = 0 Dent = 2 142 45 5.03 2.49 16.42 10.69 Dent = 3 15 4.07 6.31 Dent = 4 57 5.79 11. 79 Dent = 6 46 0.93 6.95 Dent = 8 46 2.04 11.29 Dent = 10 29 -11.72 23.27 For comparison with the 4C4F crack results: Sizing results are based on circumferential slit data greater than or equal to 52% through-wall with dents ranging from o-10 mils radial.
*Sample/
Dent Size No. Defects (mils) Evaluated Mean Standard Deviation All defects 308 0.51 12.54
>=52%, Dent<=lO
~
- F'l.l.ll 1:1> .I l:l*:t1L1: ... Fl .. I 'I I v:.> 11r:*1 l)Ef' I H llf::N l"l < ,. 1 (l ti 11... b / HEH>U* >"' 3~.';
llF FCJl)l.'.F,.*ME.ll>Lf'* 1..rr;EN[): A,.,. 1*llUS, B 2 OBS, ETC~ 16:53 MONDAY, AUGUST 21,
**.9 iB
~*
,-j ECTI>Ef' 110 *I*
- _ j:
100 + z __J: R
** N G
<jl() *I* fl A c
._].:
D A A A F c A D A D A [I A __ ao + [I A Et A (I [C c A II A [I c
+ (I A
A A A A A c A c B A E [I I) F E c 8 A G c: E II A B
-*-***].II II I A A A E B [I
--9 c
I I A (I c A c A [I A A c c B c A* c
*+ A A A D c A Et F
-*A ... **-**-* .....
II J" I A A A A b A I c 9 9 A A A I A A c A II
+ (I A .I F.t A A I
I A A A c G c: A
*-_~]:
I A A A A
+ A A A Et A I A 9
.I c A A.A A .,
I A A A
+ A Et I
I I B A A A A
-*-]:"
+ A- c ll I A A c I "
I 9 A
+
I I A A Ji VI
\U I
--+--*-----+---*--*---l*----**--*-+--*-**---**--l*---*-*--****+-*---*---+-----*-.. -+-*--*----+-***--*---*i--------+-..:-...;.:.. ___ +----**---+-*------+-------*+-------+--
30 35 40 4~:'.i 50 55 60 65 HETDEP 70 75 BO 85 90 95 100 105 J~ 20 OBS HIDDEN ."
]:
------ ----- . - f'LOl IJF ECTl>EPvHETDEF' ux i cr~ACI<
DENTS ( ""
... ECT .
j 0 LEGEND: A V!'l HCT
*nu* >.,., :';;;*
a l UBS, fl m: r* n1 2 ClflS, ETC. u, : '..'i.'J HIJND;W , .~UGI.I!:> I :'.1 I. , 1. i(. [ ECTDEP I 110 + I
'[-*
- 100 I
+;-* z R ,.. -------*!--**-* I N I G **r--
[I
,, 90 +
1----- D A A c I) F c A
- L_~
~ av
__+:__ . **- _:El D A B A Ee (I A c A I B c
- I C D c c A r*~ r*~------ -A- F *9 E-
- j -'.: -----~-t ~ -
A B E G B 8 70 E (I B c I A 1:: Ee c A B
- I C El A A c c 11' 60 + D C A B A-F
.A
- ( , o 1-~- .; . ""i) -
A- - A
.... A
- I C A
- I G c
~It I A *- A .:.'j *W, 40 +A I B " ---T* A
- I A
* + J:t
- 30
- -
- r *---*--*
L.. -'°--*+ c .... I I A I C
- I
"[-----.-~ A
- ____10*-**-: ~ . I
'U Pl (JQ CJ) 0 + ~
------.,.._*;;;+;;...:_;_.;...;_*__ _.:._ ___ +;;_.:. __ ... ______ ... _. ____ .. +--..---f*-**-*-----f*-..---* ,._,,_ ... _..,. ----*- ..........._,.........................................................- ........-- ***+-****-- ***-..**********+****-" - *+*.. -*.. -*******-- ..--....----* ......... ****-*-* .......... "'
- L.
. :52 :54 56 58 60 l.2 64 66 68 70 72 * *74 76 H" '1 DET' 70 BO 82 84 f:l6 BO 90 92 94. 96 'i'B l.00 lO .*~ NOTE:
- -~L ____*_;.
.. 20 OBS H IDDEN
- B>'. t 1:1 *:ACV l"CI f , ) . V S r1i:1
[IY l>E ME I l>FI* .
. 'l:E
~3~'i l!EF* n1 t () ~*,,, ~ MllNl>.'IY, f11.11,IJL I :*t, ,..*. )
r 100 ... F'l.DT OF n::n>EF'MMElI>EF' DENT=O LEGEND: A t OBS, Et 2 OEtS, ETC. M r--- T I A G F l.*
- .. 90**-*** ... A A
- r-* ---- A A B (I A A
.. 90 + B A c A
- L ______ 70_
i
+
I I I I 8 A A A A A A A A A B A c B B A A E A c A A A c
.. I I
A B c A D "t*
"h*
----~--- .I I
A A A A A (I A [I A A A A
- _;'---~CT!>Ef>__ { B B A A [I
- I A A
* :50 + B A A A
*-1 --*-- A A
**~-,
* ~ _,, I I A "I_ ___ -*---- -*--- T A
- 40 + A [I rr* -----r--
I A c A A B
*- . - -"30 +I A
- i:-**- --2~ *+
A A
"'CJ A
I ~ ro I
'Jl I w I
=1*** -
.. 10 +
--+-----*--+----*---+-----*-*--~--*-*-*----M~-*-***-*-**o*~Oo** **--**** -** ,_.............. ~-- .... .... ,.. -*****-**t**-***********-* ****** ...... ,................. _...... .... **-*** '))
30 35 40 4~3 50 !)5 I,,() <.~:; 7() 'l~:*; no O!"i 9() *n:i I 00 1 {)~~i _,:[ _______ _ Ml"IJ)r:I*
** l'lld. CW\('I( .... rc*1 l l . Vh 1w on*
- zr METJ>H* ~:\~i ML I lllJ** I 11 11.::.1 i1f.lNll(.iY, f.\1.11,U!::.J ;.:;, ,,,. . . '
l- F'LDT OF EClDEPt1METUEP LEl~ENll: A 1 DBS, n :'.! UBS, ETC. 100 + E I F
*--*--* r* Jl I Et I A 90-*** ---+
" I " [-- *----*-.-- I
- - *--~---- +,'
I
- r--*--* - I A c
- t _ *--~O I
A (I T " I A ~'--~ *~ A D mm " I
- r:
50 + A I (I _ ..... I A A I*
- 40 +
I A
- T----*-*
A ~[-30 I I
+
A A (I
- r-:-----r-
.. -* .... -- *- .. I I
A I I
~~-~-+~------+--------*
* - .. -- *----- 30 35
.. +-----""---*i*--*-*-----*+ .............
40 45 50
* * * ~-*
r.*r.:-
*h.}
(,() ... ~-;
'('()
...... I* ................. - i .......................... ..
no
...................... - .........., .... _ ................. +- ...,_,.. _........ i ..- ...
<;>() <jl~,; 1. 00 1 ()~)
. M['l IJF:I'
'.I
- 0>-1 l.l*:ACI<
PLOT OF ECTDEf'*MEl DEF' r:rr 11.vi; l1Y OE MFTDL DENT=3 LEGEND: A 7.E 3~'j Ml': r l>EP-1 H 1 OBS, B
- 2 OBS, ETC.
l * '. d 111.lNJ;(,_Y, Al 11.Ub"I ;" 1 , 1' . ' . *'- ECTDEf' I I
- r
- i I
I j" I I
.._I .. -----r-. I 'l *97* +
I A 86 + 85 +
--* 1!14 *---*- + A 83 + A ,,=r 82 + A * *m** +
80 + l' - --* : 79
~~
76
+
+ A
-*** ***-7s--*- -*+. A
... *74 .
73
+
+
A B
"?:i*--+ .. c
- [ 71 70
+
+
~.,--------.,_
A A 68 + 67 +
- r- **-:~ ----: A I
I
..I I
*- **-**- --* I I 1-tj I
I ~CJ) I I \.J1
- - *- .... I U1 I
"=1 **-*** *** ... ")()
71.
*c-r1F 11>r r*
. I
- 1':.CI IW DE*
HETI>H" r** v~:; DENT*=4 lL
~~~;
ML.T btJ*TH r:'L.OT OF ECTDEF'lfHETOF;F' LEGEND: A 1 OF.IS, E* 2 OBS, ETC. 100 + .J I
***--*-* ---**--r-** A r <,Jo-* .. +
I I I A B [I lt
- [___ - BO -- -1 I A
[t A A A
*- 1- c I [I c
;r---70__!__ _ I A B
A
,,[ I
... I I A [t
. I A 1i..
c (I
=~~*------ A
- 6:..... -~~-i A
- I [t
* .!50 + A
- 'f' - --*-----~
40 + I A A A
- I
....*,,~'
* =~*
"'**-**-~----:v-A A
. 'I
- [___i a
20
-,+ A I
=r-**------,
I
" 10 +
,. --+---------+-**-**-*- ---***-**-*!*****-*-*****-*********--*- ***--*** .. ***************-* ****+*** ....... *I****-* . I I** ****** ...... ** ***-* .... !********-***-** ***-**** ...., ..................... *********-* -**- ***-*** ........ ******** 00
~ ~ ~ ~ ~ 1.~i ';'{) n<* n:**; <10 *?:', 1 '><>
. Ill l(.'l:'I*
- nx 1. Cl'~ACI<. . n:rp***v!:i f.1Y l>EI HE'I DEP
; :r.E 3~1 HFT DH'l'H l ,t, : ~...! 111.lNDAY , AUG US f :" 1. , 1 '. * .II r
110 + PLOT IJF ECTDEPttMETDEP DENT=6 LEGEND: A 1 IJ[tS, [I 2 OBS, ETC. r I
- -i .
I I
**100 + '-
I
,, I (I .I
- ~ 90 1 *-
I
+
A
*-*-, A A I
I
~[* -* -~~-----f A B
..... -- *-*- . I I
I E
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- --*--~-~-:-A
" I A
[t A .[:.*'
~*
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.~.
60 + 1
. : ~.~ . I
-----.-.:~
50 + D I B
----r-A __ _
"F I A
=t~. I A
,- 30
+
+
I I I
=[* -
I 20 +
. --+----+----+-..**--+--*--i**-..-- * *t---.. -*-*t-*-*-.. --+ **--*-....*i*-*-*-........ -.... *-*t ...... _.... *i - ....... *I"-"""* ... I ... ...., ....... *---1*-.. *- ... _.., ... - ..... _.., ....... _,,_ ..........-.. -*+-*-.. -*- .....--..-....*+-*-.. -*-*I*-"*"" ...........*-*-*+*-.. - . . 52 54 56 50 60 l.12 64 61.. ,1,(1 70 72 74 '76 70 . no A~* B4 06 1:10 9<> 'i'2 94 96 9EI 1 (>()
ME:: 1 nu*
'.[___ ------* -
f.IX 1 Cl~(ll .I< [Cl I>' IW DEN
- ME:l DEF' ,_ .
DENT=B VS HE.I DEF'IH
**i PLOT OF ECTDEP*METOEF' LEGEND: A 1 OBS, B 2 009, ETC.
- 1.10 +
r* E li A c A
,, B A ., : 80 + "L'
- " . -~- --*- *--... .. -.: A -
A
- . I I
-,..,....-...,.,r---:i:- A A B A ,."
- B
- A
- 60
,.-~;;m-ris*-.- - r - - -
+A
- i ~
- 'L ____.., '(I
- 50 + A
- I A
- r# I A 3~--qo *--_J_ I B E
* --,I *-
- L. 30 I
+
---- I I
V1
* ---, I 00 20 +
--+----+----+----+----+----+----+----i ----+----+----+ --* -+----+-----f *-I - ........ *I ............. " * ........... ., ....... _. ...._., ........ _ .._..,.... - ........ t-*---...... ___ ,,_. _. .... *-*-.......... -........... +--*-*
*52 54 56 50 60 1..2 ,,., 66 l,(:J 7t) *7;* *74 u, 70 no El2 EM nl, nn 1;10 *n 94 9t.. ?D 1 oo
~r---
'l:
- B)< l Cl~ACI< ... Fl. l r**
HY l>EI MEll>Ef'
* ~I VS l'iLT l">El*' I l*I lf.:
.5~."i
- 1. b. ~:*,:~ l'i* lNI *(\Y, f~t11:;1.1::. f ;: 1 , I*..... .
r 90 + I f'LDT OF ECTl)Ef'ttt1ETDEF' DENT*,,10 LEGEND: A i. (J[lf). (I ;!. OBS , ETC
- A
'l*-- ---T *.... --*00 *-**--- +*
I I A A A I I A
-------* -*1 "[
A
. I A 70 + A " --**---**- "j **c----,
I I A A 9
., 60 + D ".. - .... *******-* ... -*. . *1I
- I I
N
~----.*
- kt____ ~!l>EP -*l.
I
. ..-.-----.-- --40 +
+ {
I A 30 +
- 1* ---*r I
(I
- 20 + H I f'
- r---1:-- l I
A A A >tj A Pl
. I ()q
(]) A U1
*.o
~r-----~-- *-:-+----+*---*-+-----+----**----*-*+-*******--****-*- **-**-**
... . . . . - ..... 40 41 42 43 44 4~ 41.o 47 4A
*-***+*****
4'7'
*******I ***** ** ***I*** *** ** I****
50 !:"ii. ~~,::.,
******I * ** * ***-f***
~:i.!. ~*i4
****** i *****
~~.~-:;
*******!********- * *!********-****I******** --f
~.:ib ~:;*7 ~;,n ~:;(r
* **-*-***of*******-*** i*-*** *****+************
bO 6:1. 6::.' I**** **********I*-**** l.:~ b4 00 Mr::*rnFF ~~t... *--**---------** *- . . .
Page 60 - 8 4C4F Pancake Probe - Crack (Circumferential Slit) Defects Detection limit: 50% through-wall for dents up to 8 mils radial with 100% assurance of detection. 50% through-wall for dents up to 10 mils radial with 88%
-assurance of detection.
No data exists for dents > 10 mils. Sizing Ability: sizing results are based on circumferential slit data greater than or equal to 52% through-wall with dents ranging from 0-10 mils radial. Sample/ Dent Size No. Defects (mils) Evaluated Mean Standard Deviation All defects 297 5.73 12.53
>= 52%
Dent <= 10
- Dent = 0 Dent = 2 Dent = 3 94 32 16 2.01 0.97 11.19 9.60 5.98 8.31 Dent = 4 46 14.17 14.45 Dent = 6 46 3.78 12.17 Dent = 8 46 6.24 13.29 Dent = 10 17 11.12 18.18
- 4L*l I l*:1iO:
l>[N'l U.I:
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- 1
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-+--------------------------------------- * - - - - - - - - - - - - - - - - - - - - - - - - - - * - - - --4
<'>3
. Mt::. IDU"
._1:[* --------
Page 69 - 8
/
MRPC - crack (Circumferential Slit) Defects Detection limit: 35% through-wall for dents up to 10 mils radial with 98% assurance of detection. No data exists for dents > 10 mils. Sizing Ability: Sizing results are based on circumferential slit data greater than or equal to 35% through-wall with dents ranging from o-10 mils radial. Sample/ Dent Size No. Defects (mils) Evaluateq Mean Standard Deviation All defects 425 -8.82 15.87
>= 35%
Dent <= 10 Dent = 0 135 -9.05 16.21 ...\~
*Dent = 2 Dent = 3 Dent = 4 45 16 60
-9.04
-17.56
-11.40 14.17
- 11. 78 11.88 Dent = 6 62 -6.05 19.23 Dent = 8 46 -12.22 8.20 Dent = 9 15 3.07 21.32
*Dent = 10 46 -5.74 18.41 For comparison with the 4C4F crack results:
Sizing results are based on circumferential-slit data greater than or equal to 52% through-wall with dents ranging from o-10 mils radial. Sample/ Dent Size ~o. Defects (mils) Evaluated Mean Standard Deviation All defects 315 -11.30 11.89
>=52%, Dent<=lO
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v Page 80-8
- Conclusions based on the qualification project are as follows:
- 1. The 580 bobbin probe characterizes wastage type degradation more accurately and consistently than the 540 bobbin probe. Both techniques have a tendency to overcall the depth of the defect by approximately 3%. The qualification results for the 580 and 540 bobbin probes in conjunction with the Miz-18 tester are superior to that of the Miz-12 tester in both dented and non-dented regions.
- 2. The 580 bobbin probe has. a tendency to undercall the average IGA front by approximately 4%, however, it provides much more consistent characteriza-tion than either the 4C4F or 8Xl pancake probes. Taking both the mean and standard deviation into account the 580 bobbin probe provides the best overall characterization of IGA. None of the three probes accurately size the IGA maximum penetration depth.
- 3. The 8Xl pancake probe and the MR.PC have crack detection capabilities which are superior to the 4C4F pancake probe. Both the 8Xl and MR.PC are able to consistently detect cracks at 35% through wall versus 50% for the 4C4F.
- 4. Neither the 8Xl pancake probe, the MR.PC or the 4C4F pancake probe are capable of consistently sizing the depth of cracks
- Page 1 of 136 ATTACHMENT 8-A I -
WAS DA TA. 58(": ID DEF PRO ECTl ECT2 ECT3 ECT4 ECT5 DENT CIRC AXIAL DEPTH %DEPTH
~----------------------------~-----------------------------------------------------------------
168 A 1 74 72 73 B2 -- 0.110 0.110 0.029 J.'
~V 168 A 2 74 74 74 74 *t -- 0.110 0.110 0.029 60 168 A 3 75 76 76 74 -- 0.110 0.110 0.029 60 168 A 4 75 74 73 75 *t -- 0.110 0.110 0.029 60 168 168 B
B
,,1. 64 74 66 79 65 79 64 81 t
t 2 2 0.110 0.110 0.110 0.110 0.029 0.029 60 60 168 B 3 72 74 79 77 l 2 0.110 0.110 0.029 60 168 B 4 52 NGD 62 65 a 2 0.110 0.110 0.029 60 168 c 1 70 66 67 66 a 4 0.110 0.110 0.030 . 63 168 c 2 69 72 70 72 4 0.110 0.110 0.030 63 168 c 3 77 71 77 73 *a 4 0.110 0.110 0.030 63 168 c 4 45 NGD 44 41
- 4 0.110 0.110 0.030 63 168 D 1 82 71 72 69 6 0.110 0.110 0.030 63 168 D 2 50 42 38 49 6 0.110 0.110 0.030 63 168 168 D
D 3 4 66 NGD 67 NGD 66 44 67 50
- 6 6
0.110 0.110 0.110 0.110 0.030 0.030 63 63 168 E 1 82 73 80 72 *; 8 0.110 0.110 0.030 63 168 E 2 36 45 28 30 8 0.110 0.110 0.030 63 168 E 3 41 37 28 23 a* 8 0.110 0.110 0.030 63 168 E 4 48 NGD 45 42 a 8 0.110 0.110 0.030 63 168 F 1 43 50 53 49 a 10 0.110 0.110 0.028 58 168 F 2 45 - 42 40 / 42
- 10 0.110 0.110 0.028 58
*a o.lio 168 F 3 -- 37 43 31 35 10 0.110 0.028 58 168 F 4 40 NGD 44 ND 10 0.110 0.110 0.028 58 I
169 A 1 60 60 62 60 a -- 0.109 0.109 0.028 58
\\
169 A 2 64 64 62 63
-- 0.109 0.109 0.028 58 169 A 3 62 64 64 64 0.109 0.109 0.028 58 169 A 4 64 64 64 64 *a -- 0.109 0.109 0.028 58 169 B 1 60 64 67. 59 a 2 0.109 0.109 0.029 60 169 B 2 71 74 75 77 a 2 0.109 0.109 0.029 60 169 169 B
B 3 4 66 69 67 68 66 68 64 68
*a 2 2
0.109 0.109 0.109 0.109 0.029 0.029 60 60 169 c 1
,,. 51 56 51 58
- 4 0.109 0.109 0.028 58 169 c 68 68 69 71 4 0.109 0.109 0.028 58 169 c 3 63 63 61 64
- 4 0.109 0.109 0.028 58 c
- 169 169 D 4
1 60 64 60 64 61 62 62 64 *a 6 4 0.109 0.109 0.109 0.109 0.028 0.029 58 60 169 D 2 72 74 72 73 a 6 0.109 0.109 0.029 60 169 D 3 69 70 65 64 6 0.109 0.109 169 169 D E 4 1 62 59 62 63 63 62 62 60 l 6 7 0.109 0.109 0.109 0.109 0.029 0.029 0.028 60 60 58 169 E 'I
- l. 59 57 58 57 l 7 0.109 0.109 0.028 58 169 E 3 67 68 70 66 t 7 0.109 0.109 0.028 58 169 E 4 60 61 58 60 *- 7 0.109 0.109 0.028 58 169 169 F
F 1 2 63 60 64 64 67 60 65 66
- 10 10 0.109 0.109 0.109 0.109 0.028 0.028 58 58 169 F 3 79 70 75 73
- t 10 0.109 0.109 0.028 58 169 F 4 66 66 66 66 l 10 0.109 0.109 0.028 58 170 A 1 57 58 60 60
* -- 0.109 0.109 0.029 59 170 A l. 59 60 58 59 l -- 0.109 0.109 0.029 59 170 A 3 62 62 62 61 l -- 0.109 0.109 0.029 59
-- 170 170 A
B 4 1 62 67 62 68 62 66 62 68
- l 0.109 0.109 0.109 0.109 0.029 0.029 59 59
Page 2 of 136 * ., WASDATA.580 ID DEF PRO 170 B 2 ECT1 68 ECT2 69 ECT3 68 ECT4 ECT5 DENT 68 2 CIRC 0.109 AXIAL 0.109 DEPTH i:DEPTH 0.029 59 170 B 3 65 63 63 63
- 2 0.109 0.109 0.029 59 170 170 B
c ., 4 1 66 64 63 64 64 63 63 68 '** 2 4 0.109 0.109 0.109 0.109 0.029 0.029 59 59 170 c 63 63 63 63 4 0.109 0.109 0.029 59 170 c 3 L 57 57 57 57 4 0.109 0.109 0.029 59 170 c 4 62 63 63 66 4 0.109 0.109 0.029 59 170 170 D D 1 2 63 57 64 55 62 67 69 57
6 6
0.109 0.109 0.109 0.109 0.029 1).029 59 59 170 D 3 62 66 64 62 '
- 6 0.109 0.109 0.029 59 170 D 4 64 67 67 61 6 0.109 0.109 0.029 59 170 170 E
E 1 2 B2 63 76 65 B2 6B 81 6B
8 B
0.109 0.109 0.109 0.109 0.029 0.029 59 59 170 E 3 76 76 75 76 ' 8 0.109 0.109 0.029 59 170 170 E F 4 1 73 6.3
.B2 60 49 63 B2 57
8 10 0.109 0.109 0.109 0.109 0.029 0.029 59 59 170 170 F
F 2 3 54 57 56 62 54 57 54 55
*' 10 10 0.109 0.109 o.109 0.109 0.029 0.029 59 170 F 4 NQD NQD 65 65 ' 10 0.109 0.109 0.029 59 59 178 17B A
A *2 1 97 97 97 96 97 97 98 . '* 0.050 0.050 0.050 0.050 0.049 0.049 100 100 178 A 3 99 99 99 98 0.050 0.050*-* 0.049 100 178 A 4 97 96 9B 96 0.050 0.050 0.049 100
- 178 17B 17B 178 178 178 178 B
B B 3 B c c c 1 2 4 1 2 3
*74 Bl 75
'5261 75 74 BO 74 53 51 60 74 73 81 75 51 52 60 74 73 80 75 50 52 60 0.075 0.075 0.075 0.075 0.110 0.110 0.075 0.075 0.075 0.075 0.110 0.110 0.037 0.037 0.037 0.037 0.027 0.027 BO BO BO 80 59 59 0.110 0.110 0.027 59 178 c 4 51 59 53 . 53 ' 0.110 o*.110 0.027 178 178 D
D 1 2 41 l 42 41 42 41 43 41
0.190 0.190 0.190 0.190 0.018 0.018 59 39 39 178 178 D
D 3 4 42 46 49 41 48 41 51 43
'* 0.190 0.190 0.190 0.190 0.018 0.018 39 39 178 E 1 22 21 21
- 178 178 E
E 2 3
'2520 22 25 21 25 18
- 0.190 0.190 0.190 0.190 0.009 0.009 20 20 26 0.190 0.190 0.009 178 E 4 21 20 22 17 '
- 0.190 0.190 0.009 20 20 302 A 1 67 71 77 73 2 0.196 302 A 2 74 74 72 76 '* 2 0.196
.688
.688 0.038 0.038 78 78 302 A 71 71 72 72 2 0.196 .688 0.038 78 302 302 A
B 4 1 73 63 74 59 74 63 74 57 '* 2 2 0.196 0.196
.688
.750 0.038 0.030 78 61 302 B 2 62 65 63 63
- i 2 0.196 .750 0.030 61 302 B 3 62 63 63 SB 2 0.196 .750 0.030 61 302 B 4 61 62 60 bl 2 0.196 .750 0.030 61 302 c 1 33 27 30 ND 2 0.196 1.500 0.017
' 35
... 302 302 302 302 302 c c c D D 2 3 4 2 NQD NQD 43 ND 10 NQD 44 ND NQD 1 NQD 45 40 ND 30 42 44 34 ND 27 i i 2 2 2 2 "i. 0.196 0.196 0.196 0.196 0.196 1.500 1.5(10 1.500
.688
.688 0.017 0.017 O.Oli 0.010 i).010 35 35 3~
20 20
Page 3 of 136
/*
WASDATA.5BO ID DEF PRO ECTl ECT2 ECT3 ECT4 ECT5 DENT CIRC AXIAL DEPTH i.DEPTH 302 D 3 51 43 36 42 2 0.196 .6B8 0.010 20 302 D 4 ND ND 16 17 ** 2 0.196 .6B8 0.010 20 303 A 1 73 75 70 71
- 2 0.5BB .B13 0.036 73 303 A 2 73 71 74 75
- 2 0.5BB .B13 0.036 73 303 303 A
A T 4 74 BO 72 71 74 7B 75 77
** 2 2
0.5B8 0.5BB
.B13
.B13 0.036 0.036 73 73 303 B 1 56 57 57 56
- 2 0.588 .688 0.028 57 303 B 2 59 59 59 59
- 2 0.588 .688 0.028 57 303 B 3 56 57 55 57
- 2 0.588 .688 0.028 57 303 B
*c 4 5B 57 57 55
- 2 0.588 .688 0.028 57 303 1 33 35 33 34 2 0.58B .688 O.OlB 37 303 c 2 50 4B 48 49 2 0.5B8 .688 O.OlB 37 303 c 3 39 40 41 41
- 2 0.5B8 .688 O.OlB 37 303 c 4 41 41 39 41
- 2 0.588 .688 0.018 37 303 D 1 19 25 23 34
- 2 0.58B .813
.an 0.015 31 303 D 2 34 35 33 34
- 2 0.588 0.015 31 303 303 D
D 3 4 37 34 37 34 37 34 35 30
*i 2 2
0.588 0.588
.813
.813 0.015 .
0.015 31 31 306 306 A A 1 2 78 BO 82 71 Bl 77 B2 so *l 4 4 0.196 0.19b
.68B
.6B8 0.040 0.040 82 82 306 A 3 78 75 77 78
- 4 0.196 .6BB 0.040 82 306 A 4 81 79 82 81
- 4 0.196 .688 0.040 82 306 B 1 62 60 66 63 4 0.196 .750 0.029 59 -
306 B 2 63 64 62 64 4 0.196 .750 0.029 59
/
i . 306 B 3 63 61 62 62
- 4 0.196 .750 0.029 59 306 B c
4 65 58 61 62
- 4 0.196 .750 0.029 59 306 c
1 40 33 41 46
- 4 0.196 1.063 O.OlB 37 306 c
2 46 4B 53 44
- 4 0.196 1.063 O.OlB 37 306 3 46 48 48 47
- 4 0.196 1.063 O.OlB 37 306 306 c
D 4 1 42 16 42 24 44 NOD 42 ND *t 4 4 0.196 0.19b 1.063
.563 O.OlB 0.011 37 22 306 D 2 32 30 37 30 t 4 0.196 .563 0.011 22 306 D 3 42 4B 46 48 4 0.196 .563 0.011 22 306 D 4 ND ND 31
- 34
- 4 0.196 .563 0.011 22 307 A 1 72 73 72 i2
- 4 0.5B8 .813 0.035 71 307 ft 2 72 72 75 72
- 4 0.5B8 .813 0.035 71 '
307 A 3 68 70 6B 6B
- 4 0.588 .B13 0.035 71 307 307 A
B 4 1 76 59 76 62 75 60 76 5B
- 4 4
0.5B8 0.588
.B13
.750 0.035 71 307 307 B B 2 3
63 57 62 57 60 57 60 56
'** 4 4
0.58B 0.588
.750
.750 0.028 0.028 0.028 57 57 57 307 B c
4 60 59 56 55
- 4 0.588 .750 0.028 57 307 307 c 1
2 39 49 41 51 39 50 48 50
- 4 4
0.588 0.588
.750
.750 0.019 0.019 39 39 307 r... 'T
'*' 43 41 44 43 *t 4 0.588 .750 0.019 39 307 307
\,
D 1 4 49 30 49 32 44 30 43 44
- 4 4
0.588 0.588
.750
.813 0.019 0.015 39 31 307 D
' 45 44 47 48
- 4 0.588 .813 0.015 31
.\ 307 D 3 41 38 39 39
- 4 0.588 .813 0.015 31 307 il 4 40 39 39 38 4 0.588 .813 0.015 31 310 A 81 82 77 77
- 8 0.196 .Bl3 0.039 BO 310 310 A
A 2 3 74 77 66 77 73 77 69 74
** 8 B
0.196 0.196
*B13
.813 0.039 .
0.039 80 80
Page 4 of 136 WASDATA.580 ID DEF PRO ECTl ECT2 ECT3 ECT4 ECT5 DENT CIRC AXIAL DEPTH 7.DEPTH 310 A 4 78 70 75 77
*t 8 0.196 .813 0.039 80 310 B 1 57 57 64 57 8 0.196 .750 0.029 59 310 B 2 55 55 55 55 t 8 0.196 .750 0.029 59 310 B 3 56 60 60 61 t B 0.196 .750 0.029 59 310 B 4 52 53 54 56 t 8 0.196 .750 0.029 59 310 c 1 48 48 50 51 i B 0.196 .750 0.019 39 310 c 2 46 49 42 45 t 8 0.196 .750 0.019 39 310 c 3 53 52 52 51 t B 0.196 .750 0.019 39 310 c 4 45 45 45 47 t 8 0.196 .750 0.019 39 310 D 1 48 53 56 ' 53 t 8 0.196 .688 0.010 20 310 D 2 ND ND NGD NGD
- 8 0.196 .688 0.010 20 310 D 3 ND 67 57 63
- 8 0.196 .688 0.010 20 310 D 4 44 37 42 44
- B 0.196 .688 0.010 20 311 A 1 79 74 BO 73
- B 0.588 .750 0.038 78 311 A ".I. 69 70 67 66
- B 0.588 .750 0.038 78 311 A 311 A 3
4 74 76 75 68 72 70 74 70
*t 8
8 0.588 0.588
.750
.750 0.038 0.038 78 78 311 B 311 B 2 1 63 55 60 54 58 56 63 55
*l 8 B
0.588 0.588
.750
.750 0.030 0.030 61 61 311 B 3 60 60 58 58
- 8 0.588 .750 0.030 61 311 B 311 c 4 55 57 57 57
- B 0.588 .750 0.030 61 311 c 1 49 48 50 53
- 8 0.588 .750 0.021 43 2 .45 42 48 42
*t B 0.568 .750 0.021 43 311 c 3 47 46 48 49 8 0.588 .750 0.021 43 311 c 4 50 49 46 46 8 0.588 .750 0.021 43 311 D 1 44 44* 42 43 8 0.588 .813 0.016 33 311 D 2 39 40 39 40 8 0.588 .813 0.016 33 311 D 3 44 44 45 44 t B 0.588 .813 0.016 33 311 D 4 41 41 39 40 t B 0.588 .813 0.016 33 314 A 314 A 2 1 73 62 64 64 66 53 74 60
- 10 10 0.196 0.190
.688
.688 0.038 0.038 77 7i 314 A 314 . A 3
4 60 73 65 71 62 71 63 72
*t 10 10 0.196 0.196
.688
.688 0.038 0.038 77 77 314 8 1 63 60 63 64
- 10 0.196 .750 0.031 63 314 B 2 55 56 62 57
- 10 0.196 .750 0.031 63 314 B 314 B 3
4 49 64 53 57 49 59 52 55
*t 10 10 0.196 0.196
.750
.750 0.031 0.031 63 63 314 c 314 c 2 1 46 43 47 49 47 51 47 53
- 10 10 0.196 0.196
.813
.813 0.020 0.020 41 41 314 c
- 314 c 3 40 46 40 50
- 10 0.196 .813 0.020 41 4 NGD 37 44 44
- 10 0.196 .813 0.020 41 314 D 1 35 33 38 47
- 10 0.196 .813 0.012 20 314 D .I. N9D ND ND 61
- 10 0.196 .813 0.012 20 314 D 3 27 60 61 68
- 10 0.196 .813 0.012 20 314 D 315 A 4
1 NQD 82 N9D 76 26 78 39 BO *l 10 10 0.196 0.588
.B13 1.000 0.012 0.039 20 80 315 H'* "i. 78 BO 67 81 l 10 0.588 1.000 0.039 BO 315 A 315 A 3
4 70 82 69 76 72 82 71 81
*l 10 10 0.598 0.588 1.000 1.000 0.039 0.039 80 80 315 B 315 B 1
.,i.
51 51 50 53 52 49 52 52
*t 10 10 0.5B8 0.588
.813
.B13 0.029 0.029 59 59 315 B 315 B. 4 3 47 53 46 50 46 54 46 56
*i 10 10 0.588 0.588
.813
.813 0.029 0.029 59 59
Page 5 of 136 llASDATA.580 ID DEF PRO ECTl ECT2 ECT3 ECT4 ECT5 DENT CIRC AXIAL DEPTH 4DEPTH
----------------------------------------~------------------------------------------------------
315 L c 1
*2 42 41 40 40
- 10 0.588 .875 0.020 41 315 c
36 35 35 41
- 10 0.588 .875 0.020 41
~15 c
3 46 43 43 46
- 10 0.588 .875 0.020 41 315 4 49 45 46 43
- 10 0.588 .875 0.020 41 315 315 D
D 1 2 39 35 30 31 29 43 37 43
*i 10 10 0.588 0.588
.688
.688 0.016
.0.016 33 33 315 D 3 52 36 40 41
- 10 0.588 .688 0.016 33 315 D 4 44 40 43 41
- 10 0.588 .688 0.016 33 317 317 A.
A 1 82 82 82 B2
- 2 0.078 0.078 0.038 76 2 81 81 81 81 2 0.078 0.078 0.038 76 317 A 3 82 82 82 82 2 0.078 0.078 0.038 76 317 4 82 82 317 A 82 82
- 2 0.078 0.07B 0.038 76 B 1 BO 82 B2 82
- 4 0.078 0.078 0.040 BO 317 B 2 81 81 81 Bl
- 4 0.078 0.078 0.040 80 317 317 B 3 4
B2 B2 82 82
- 4 0.078 0.078 0.040 80
**l B 82 82 82 82 4 0.078 0.078 0.040 BO 317 c 1 82 82 82 82 B 0.078 0.078 0.040 80 317 c 2 81 81 81 Bl 8 0.078 0.078 0.040 80 c
317 c 3 82 82 82 82
- B 0.078 0.07B 0.040 80 317
- m D 1 4 79 82 82 82
- 8 0.078 0.078 0.040 BO 73 73 74 74
- 10 0,07B .0 *.07B . 0.032 . 64 317 D 2 66 67 64 67
- 10 0.07B 0.078 0.032 64 1.\.
317 317 319 319 319 319 D D A A A A 3 4 1 2 3 4 81 67 NGD 26 ND ND 81 70 NGD 27 ND 50 75 NGD 19 10 ND ND 81 ND ND 29 ND 76 10 10 4 4 4 4 0.078 0.078 0.190 0.190 0.190 0.190 0.07B 0.078 0.190 0.190 0.190 0.190 . 0.032 0.032' 0.012 0.012 0.012 0.012 64 64 25 25 25 25 319 319 B B 1 2 ND 3 ND 54 ND 47 ND 30
- 5 0.190 0.190 0.190 0.014 29
- 5 0.190 0.014 29 319 319 B 3 4
ND ND ND ND ND
- 5 0.190 0.190 0.014 29 319 B
c 1 ND ND ND ND ND ND ND
- 5 0.190 0.190 0.014 29 319 c 'l
'" 56 ND NGD NGD
*l 9 9
0.190 0.190 0.190 0.190 0.013 0.013 27 27 319 c 3 ND ND ND ND l 9 0.190 0.190 0.013 27 c 319 4 ND ND ND ND
- 9 0.190 0.190 0.013 27 319 D 1 ND ND ND ND
- 11 0.190 0.190 0.012 25 319 319 D
D 2 3 49 ND NGO ND NGO ND
'NGO ND
*J 11 11 0.190 0.190 0.190 0.190 0.012 0.012 25 25 319 320 D 4 ND ND ND ND
- 11 0.190 0.190 0.012 25 320 A 1 2
B2 B2 82 B2
- 2 0.080 0.080 0.040 83 320 A
3 82 Bl 81 81
- 2 0.080 0.080 0.040 83 320 A
A 4 B2 82 82 61 82 82 82 82 *l 2 2 0'.080 0.080 0.080 o*.000 0.040 0.040 83 83 320 320 B 1 79 82 81 80
- 5 0.080 0.080 0.040 83 B 82
~
.i. 81 81 81 5 0.080 0.080 0.040 83 320 B 3 80 78 78 80 5 0.080 0.080 0.040 83 320 320 B
c 4 82 82 82 82
** 5 O.OBO 0.080 0.040 B3 c
1 81 81 79 82
- 8 0.080 0.080 0.038 79 320 ~
*.i. 70 81 81 81 8 0.080 0.080 0.038 79 320 c 3 NGD 66 NGO 8
.. 320 c 77
- 0.080 0.080 0.038 79 320 4 82 ND 82 81
- 8 0.080 0.080 0.038 79 D 1 59 64 67 63
- 10 0.080 0.080 0.036 75
Page 6 of 136 *
* /
,,. -- ~
WASDATA.580 ID DEF PRO 320 320 320 D n* D 2 3 4 ECT1 43 30 82 ECT2 48 19 b3 ECT3 47
<20 55 ECT4 ECT5 DENT 47 ND bO t
t t 10 10 10 CIRC 0.080 0.080 0.080 AXIAL 0.080 0.080 DEPTH 7.DEPTH 0.080 0.03b 0.03b 0.03b 75 75 75 3b9 3b9 A A 1 2 ND ND ND ND ND 49 ND NGD
** 10 0.078 0.078 0.040 BO t 10 0.078 0.078 0.040 BO 3b9 A 3 ND ND ND ND t 10 0.078 0.078 0.040 BO 3b9 A 4 ND ND ND ND t 10 0.078 0.078 0.040 80 3b9 B 1 ND ND ND ND t 10 0.109 0.109 0.030 bO 3b9 B 2 29 29 3 NGD t 10 0.109 0.109 0.030 60 3b9 B 3 ND ND ND ND t 10 0.109 0.109 0.030 bO 3b9 4 ND ND ND ND 10 3b9 B
c 1 ND ND ND ND
*t 10 0.109 0.187 0.109 0.187 0.030 0.020 60 40 3b9 c 2 b5 12 NGD 68 l 10 0.187 0.187 0.020 40 3b9 c 3 ND ND ND ND t 10 0.187 0.187 0.020 40 3b9 c 4 ND ND ND ND t 10 0.187 0.187 0.020 40 369 D 1 ND ND ND ND l 10 0.187 0.187 0.015 30 369 D 2 59 NQD 61 NGD 10 0.187 0.187 0.015 30 369 D 3 ND ND ND ND *l 10 0.187 0.187 0.015 30 3b9 D 4 ND ND ND ND i 10 0.187 0.187 0.015 30 369 E 2 43 72 ND NGO l 10 0.000 0.000 0.000 0 369 E 3 ND ND ND ND l 10 0.000 0.000 0.000 0 369 E 4 ND ND ND ND t 10 0.000 0.000 0.000 0 370 A 1 ND ND ND ND t 15 0.078 0.078 0.040 80 370 A 2 ND NGD NGD NGO t 15 0.078 0.078 0.040 80
. 370 A 3 ND ND ND ND 15 0.078 0.078 0.040 80
\'
370 A 4 NGD NGD ND ND *t 15 0.078 0.078 0.040 BO 370 B 1 ND ND ND ND t 15 0.109 0.109 0.030 60 370 B 2 NGO NGO NGO NGO 15 0.109 0.109 0.030 60 370 B 3 ND ND ND ND
- 15 0.109 0.109 0.030 60 370 B 4 NGO NGD NGO ND l* 15 0.109 0.109 0.030 60 370 c 1 ND ND ND ND t 15 0.187 0.187 0.020 40 370 c ,. 2 NGD NGD NGD NGD 15 0.187 0.187 0.020 40 370 c ,. ND ND ND ND *g 15 0.187 0.187 0.020 40 370 c 4 NGD NGD ND ND t 15 0.187 0.187 0.020 40 370 D 1 ND ND ND ND t 15 0.187 0.187 0.015 30 370 D 2 NGD NGD NGO NGD 15 0.187 0.187 0.015 30 370 D 3 ND ND ND ND t* 15 0.187 0.187 0.015 30 370 370 D
E 2 4 NGO NGD NGD NGD
- ND NGD ND NGO
~
15 15 0.187 0.000 0.187 0.000 0.015 0.000 30 0 370 E 3 ND ND ND HD 15 0.000 o.ooo o.ooo 0 370 E 4 NGD NGD ND ND
- 15 0.000 0.000 0.000 0 371 A 1 ND ND ND llD
- 20 0.078 0.078 0.040 80 371 A 2 ND ND ND ND *t 20 0.078 0.078 0.040 80 371 A "/
" ND ND ND ND t 20 0.078 0.078 0.040 80 371 A 4 ND ND ND ND i 20 0.079 0.078 0.040 80 371 B 1 ND ND ~rn ND 20 0.109 0.109 0.030 60 371 B "i. NGO NGD NGO t~~D
- 20 0.109 0.109 0.030 60 371 B 3 ND ND ND ND *t 20 0.109 0.109 0.030 60 371 B 4 ND ND NQD ND t 20 0.109 0.109 0.030 60 371 \, 1 ND ND ND ND l 20 0.187 0.187 0.020 40 371 371 c
c 2 3 NGD ND NGD ND NGD ND NGD ND
- 20 20 0.187 0.187 0.187 0.187 0.020 0.020 40 40 371 c 4 ND ND NGO ND l* 20 0.187 0.187 0.020 40
Page 7 of 136 ./. WASDATA.580 ID DEF PRO ECT1 ECT2 ECT3 ECT4 ECT5 DENT CIRC AXIAL DEPTH %DEPTH 371 D 1 ND ND ND ND a 20 0.187 0.187 0.015 30 371 D ,, NGD NGD NGD NGD a 20 0.187 0.187 0.015 30 371 " 3 D ND "ND ND ND t 20 0.187 0.187 0.015 30 . 371 D. 4 ND ND NOD ND a 20 0.187 0.187 0.015 30 371 E 2 NOD NOD NOD NOD a 20 0.000 0.000 o.ooo 0 3i1 E 3 ND ND ND ND t 20 0.000 o.ooo 0.000 0 371 E 4 ND ND NOD ND a 20 o.ooo 0.000 o.ooo 0 372 A 1 ND. ND ND ND 25 0.078 0.078 0.040 BO 372 A 2 ND ND ND ND
- 25 0.07B 0.07B 0.040 BO 372 A 3 ND ND ND ND *a 25 0.078 0.078 0.040 BO 372 A 4 ND ND NOD NOD 25 0.078 0.078 0.040 80 372 B 1 ND ND ND ND
- 25 0.109. 0.109 0.030 60 372 B 2 NGO NOD NOD NOD
- 25 0.109 0.109 0.030 60 372 372 B
B 3 4 ND ND ND ND ND NGD ND NOD t 25 25 0.109 0.109 0.109
'. 0.109 0.030 0.030 60 60 372 c 1 ND ND ND ND a 25 0.187 0.187 0.020 40 372 c 2 NOD NOD NGO NGD g 25 0.187 0.187 0.020 40 372 c 3 ND ND ND ND a 25 0.187 0.187 0.020 AO 372 c 4 ND ND NGO NOD t 25 0.187 0.1B7 0.020 40 372 D 1 ND ND ND ND a 25 0.187 0.187 0.015 30 372 D- 2 NGD NOD NOD NOD a 25. 0.187 0.187 0.015 30 372 D 3 ND ND ND ND t 25 0.187 0.187 0.015 30 372 D. 4 ND ND NOD NOD a 25 0.187 0.187 0.015 30 372 E 2 NGO NOD NGO NGD a 25 o.ooo 0.000 0.000 0 372 E 3. ND ND ND ND a 25 0.000 0.000 o.ooo 0 372 E 4 ND ND NGO NGO a 25 0.000 o.ooo o.ooo 0
- ~
Page 8 of 136 ISADATA.580 ID DEF PRO ECTl ECT2 ECT3 ECT4 ECT5 AI MAI llP AS MAS DENT AXIAL CIRC DEPTH 382 D 13 14 16 20 30.8 31.5 77.6 45.3 47.3 2 0.20 0.588 30 382 D 2 30 20 20 ,~
* .:i 30.B 31.S 77.6 45.3 47.3 2 0.20 0.588 30 382 D 3 20 B 8 18 30.8 77.6 45.3 47.3 2 0.20 0.588 30 382 D 4 18 8 14 12 30.8 31.S 77.6 45.3 47.3 2 0.20 O.SBB 30 382 E NGD 43 43 35 26.2 33.3 58.6 50.2 50.2 2 0.20 0.588 30 382 E 2 52 53 53 51 26.2
.;;..;,.;; 58.6 50.2 50.2 2 0.20 0.588 30 382 E ., tmD 48 45
*-' 29 26.2 33.3 58.6 50.2 50.2 2 0.20 0.58B 30 382 E 4 45 48 56 54 26.2 33.3 58.6 50.2 50.2 2 0.20 o.5BB 30 383 D 1 17 12 ND ND 11. 5 12.1 26.1 2 0.20 0.588 20 383 D 2 ND ND ND ND 11. 5 12.1 26.1 2 0.20 0.5B8 20 383 D 3 ~m ND ND NGD 11. ~* 12.1 26.l 2 0.20 0.588 20 383 D 4 ND ND ND ND 11.5 12.1 26.1 2 0.20 O.SBB 20 383 E 1 ND ND ND ND 11.8 14.2 24.2 2 0.20 0.5B8 20 383 E 2 ND ND ND ND 11.8 14.2 24.2 2 0.20 0.5B8 20 383 E 3 ND ND ND ND 11.8 14.2 24.2 2 0.20 0.5B8 20 383 E ND ND ND ND 11.B 14.2 24.2 2 0.20 0.5B8 20 384 D 46 43 43 44 51.B 53.0 78.2 2 0.20 0.5B8 40 384 D 44 43 48 42 51.8 53.1) 78.2 2 0.20 O.SBB 40 384 D '._. 45 45 46 49 53.0 78.2 384 D 4 41 39 39 39 't 51.£ 51.8 $3.0 78.2 2
2 0.20 0.20 0.5B8 0.5B8 40 40 384 E 37 39 41 39 t 46.3 53.3 71.5 2 0.20 0.5B8 40 384 E 2 57 54 53 52 t 46.3 53.3 71.5 2 0.20 0.588 40 3B4. E -*' 35 33 53 46 t 46.3 53.3 71.5 2 0.20 0.588 40 3B4 E 4 42 43 48 49 t 46.3 53.3 71.5 2 0.20 0.5BB 40 385 D 41 41 42 41 t 52.1 52.3 73;7 2 0.20 0.58B 50
- . . 385 3B5 D
D 2 3 40 44 39 43 41 44 39 4B
*l 52.l 52.1 52.3.
52.3 73.7 73.7 2 2 0.20 0.20 0.58B 0.5B8 50 50 385 D 4 41 40 42 43 52.1 52.3 73.7 2 0.20 0.5BB 50 385 E 1 43 45 45 44 *t 45.8 50.4 60.5 2 0.20 0.58B 50 385 E 2 52 52 51 51 t 45.8 S0.4 60.5 2 0.20 o.5B8 50 385 E 3 37 41 42 54 t 45.8 50.4 60.5 2 0.20 0.588 50 385 E 4 43 45 49 50 l 45.8 50.4 60.5 2 0.20 0.5BB 50 386 D 40 40 38 39 t 52.8 53.3 75.4 2 0.20 0.588 60 386 D 2 32
.,,,, 32 33 t 52.e 53.3 75.4 2 0.20 0.5BB 60 386 D 40 38 39 44 t 52.8 53.3 75.4 2 0.20 0.588 60
- 386 D 4 35 34 39 40 t 52.8 53.3 75.4 2 0.20 0.5B8 60 386 t. 1 42 43 41 42 t 50.4 55.6 67.6 2 0.20 0.5B8 60 386 E 2 59 51 49 52 t 50.4 55.6 67.6 2 0.20 0.5BB 60 386 E .,.;, 34 34 37 3B t 50.4 55.6 67.6 2 0.20 0.5B8 60 386 E 4 42 46 49 47 50.4 55.6 67.6 2 0.20 60 3B7 D 49 49 49 51
*t 57.9 58.9 90.6 2 0.20 0.5BB 0.5BB BO 387 D 2 44 47 46 46 t 57.9 58.9 90.6 2 0.20 0.5B8 BO 387 D 3 49 50 50 54 t 57.9 58.9 90.6 2 0.20 0.58B BO 387 387 D
t. 4 46 57 46 57 46 58 49 49
*t 57.9 54.9 58.9 60.0 90.6 78.2 2
2 0.20 0.20 0.588 0.588 80 BO 387 E 'l 61 61 59 59 t 54.9 60.0 7B.2 2 . 0.20 0.588 BO 387 E 3 ~.7 56 55 59 t 54.9 60.0 78.2 2 0.20 0.588 BO 387 E 4 47 54 51 60 t 54.9 60.0 78.2 2 0.20 0.588 BO 388 D 79 80 76 BO t 91.2 91.4 99.6 2 0.20 0.588 100 388 D 2 79 82 ! 82 BO t 91.2 91.4 99.6 2 0.20 0.588 100 388 D 3 79 77 79 77 t 91.2 91.4 99.6 2 0.20 0.5B8 100 388 n 4 75 75 79 78 t 91.2 91.4 99.6 2 0.20 0.588 100 388 E 1 87 82 82 B2 t 92.2 98.4 100.0 2 0.20 0.588 100
Page 9 of 136 ISADATA.580
- ID 3BB 388 388 389 3B9 DEF PRO E
E E D D 4 2 1 L ECT1 BB 91 82 39 31 ECT2 90 91 82 37 31 ECT3 B2 91 82 37 31 ECT4 82 91 82 37 35 ECT5 l l l s* AI 92.2 92.2 92.2 43.3 43.3 MAI 98.4 98.4 98.4 43.9 43.9 MP 100.0 100.C 100.0 79.2 79.2 AS 59.0 59.0 11AS 59.2 59.2 DENT 2 2 4 4 2 AXIAL 0.20 0.20 0.20 0.20 0.20 CIRC 0.588 0.588 0.5B8 0.5BB 0.5BB DEPTH 100 100 100 30 30 389 D ~
*J 2B 22 27 30 t 43.3 43.9 79.2 59.0 59.2 4 0.20 0.5BB 30 3B9 D 4 2B 2B 30 30 t 43.3 43.9 79.2 59.0 59.2 4 0.20 0.5BB 30 3B9 E 1 97 97 97 100 t 32.4 41.2 62.6 4 0.20 0.5BB 30 3B9' E 2 INC INC INC me t 32.4 41.2 62.6 4 0.20 0.588 30 389 E 3 1156 r!SS 1'!56 1156 t 32.4 41.2 62.6 4 0.20 0.588 30 389 E 4 INC INC INC INC l 32.4 41.2 62.b 4 0.20 0.588 30 391) D 1 ND ND 15 ND t 21.5 22.3 63.0 39.4 40.9 4 0.20 0.5BB 20 390 D ~
.:. ND 10 3 3 t 21.5 22.3 63.0 39.4 40.9 4* 0.20 0.588 20 391) D "!
.J .3 ND ND NDD t 21.5 22.3 63.0 39.4 40.9 4 0.20 0.588 20 390 D 4 8 ND ND NDD i 21.5 22.3 63.0 39.4 40.9 4 0.20 0.588 20 390 E 1 ND ND ND ND l 1B *.1 22.1 51.3 36.9 37.7 4 0.20 0.588 20 390 E 2 ND ND ND ND l lB.1 22.1 51.3 36.9 37.7 4 0.20 0.5BB 20 390 E "!
.:_. ND ND ND ND : lB.1 ??
...... .1.' 51.3 36.9 37.7 4 0.20 0.5B8 20 390 E 4 *ND ND ND ND l 1B.1 22.1 51.3 36.9 37.7 4 0.20 0.588 20 391 D 1 L 34 37 36 40 s 43.9 44.9 85.4 60.5 61.9 4 0.20 0.5B8 40 391 D ')
42 40 40 42 s 43.9 44.9 B5.4 60.5 61.9 4 0.20 0.588 40 391 39 36 38 43 43.9 44.9 B5.4 60.5 61.9 4 0.20 0.5B8 40 (l. D .J l 391 33 34 34 34 43.9 44.9 B5.4 60. ~. 61.9 4 0.20 0.588 40 391 D E 4 1 32 41 3B 42 s' 41. 9 47.6 69.8 57.7 57.7 4 0.20 0.58B 40 391 E "i. 55 54 57 54 41.9 47.6 69.B 57.7 57.7 4 0.20 0.58B 40 391 E 3 30 29 35 18 'l 41.9 47.6 69.8 57.7 57.7 4 0.20 0.588 40 391 E 4 39 45 49 47 s 41.9 41.b 69.B 57.7 57.7 4 0.20 0.58B 40 392 D 1 32 31 32 32 t 45.6 45.8 77.6 4 0.20 0.588 50 392 D 2 . 39 38 38 37 l 45.6 45.B 77.6 4 0.20 0.5B8 so 392 D 3 35 33 29 33. g 45.6 45.8 77.6 4 0.20 0.588 50 392 D 4 30 30 34 30 l 45.6 45.8 77.6 4 0.20 0.588 50 392 392 E E 1
"i.
25 . 41 35 44 34 46 32 50 *l 44.3 44.3 51.3 51.3 69.7 69.7 61.1 61.1 61.1 61.1 4 4 0.20 0.20 0.58& 0.588 50 50 392 E 3 24 23 34 22
- 44.3 51.3 69.7 61.1 61.1 4 0.20 0.5BB 50 392 c:. 4 37 43 48 41
- 44.3 51.3 69.7 61.1 61.1 4 0.20 0.5B8 50 393 0 1 49 49 50 50 l 53.9 56.0 81.5 64.7 64.7 4 0.20 0.588 60 393 D ~
L 46 46 49 48 l 53.9 56.0 81.5 64.7 64.7 4 0.20 0.5BB 60 393 D *7., 51 51 51 55 l 53.9 56.0 81.5 64.7 64.7 4 0.20 0.588 60 393 D 4 4B 51 52 50 l 53.9 56.0 81.5 64~7 64.7 4 0.20 0.5B8 60 393 E 1 51 52 51 59 54.2 60.4 73.6 4 0.20 0.588 60
., *l 393 E i. 55 60 61 53 54.2 60.4 73.6 4 0.20 .0.588 60 393 E .,,. 47 47 49 58 l 54.2 60.4 73.6 4 0.20 0.5BB 60 393 E *
'T 52 53 53 57 .l 54.2 60.4 73.6 4 0.20 0.58B 60 394 394 D 1 51 51 54 47 51 50 54 48
*l 58.2 58.2 59.8 59.B 91.3 91.3 4
4 0.20 0.58B 0.5B8 BO BO 394 D D
,.2
*J 53 53 53 56 l 58.2 59.B 91.3 4 0.20 0.20 0.5BB BO 394 D 4 51 51 51 53 l 5B.2 59.8 91.3 4 0.20 0.588 BO 394 E 1 60 60 59 60 l 48.0 57.0 73.5 4 0.20 0.588 so 394 E 2 b4 59 59 56 l 48.0 57.0 73.5 4 0.20 0.588 80 394 E ..,~ 58 58 58 59 l 48.0 57.0 73.5 4 0.20 0.5B8 BO 794 s E 4 57 58 53 58 48.C 57.0 73.5 4 0.20 0.588 80 395 D 1 76 75 76 75 B2.0 83.6 100.0 4 0.20 0.588 100 395 n u 2 76 74 75 76
*l 82.0 83.6 100.0 4 0.20 0.588 100
Page 10 of 136 ISADATA.580
- ID DEF PRO 395 395 395 395 395 D
D E E E 3 1 2 3
't ECT1 75 75 82 82 81 ECT2 75 72 82 82 81 ECT3 74 7~.
82 82 81 ECT4 75 75 82 82 82 ECTS s l l
*l AI 82.0 82.0 79.8 79.8 79.8 MAI 83.6 83.b 88.4 88.4 88.4 MP 100.0 100.0 96.1 96.1 96.1 AS MAS DENT 4
4 4 4 4 AXIAL 0.20 0.20 0.20 0.20 0.20 CIRC 0.588 . 0.588 0.588 0.588 0.588 DEPTH 100 100 100 100 100 395 E 4 82 82 82 82 s 79.8 88.4 96.1 4 0.20 0.588 100 396 D 1 37 38 37 37 l 42.3 44.5 80.5 58.2 58.2 6 0.20 0.588 30 396 D 2 48 38 42 42 l 42.3 44.5 80.5 58.2 58.2 6 0.20 0.588 30 396 D 3 43 42 42 48 s 42.3 44.5 80.5 58.2 58.2 6 0.20 0.588 30 396 D 4 43 39 41 47 s 42.3 44.5 80.5 58.2 58.2 6 0.20 0.588 30 396 E l 46 46 47 49 l 31.3 40.5 72.9 55.4 55.5 6 0.20 0.588 30 396 *E 2 61 56 59 56 l 31.3 40.5 72.9 55.4 55.5 6 0.20 0.588 30 396 E 396 E 3 4 38 49 51 45 41 43 51 38
*t 31.3 31.3 40.5 40.5 72.9 72.9 55.4 55.4 55.5 55.5 6
6 0.20 0.20 0.588 0.588 30 30 397 D 1 42 46 46 43 l 29.6 30.6 62.9 49.8 50.7 6 0.20 0.588 20 397 D 397 D 3 38 41 32 40 37 42 32 47
*l 29.6 29.6 30.6 30.6 62.9 62.9 49.B 49.8 50.7 50.7 6
6 0.20 0.20 0.588 0.588 20 20
~.,.,
-~7 J D 4 44 44 46 45 i 29.6 30.6 62.9 49.B 50.7 6 0.20 0.588 20 397 t'... 1 49 NilD 50 49 t 24.9 29.B 61. 9 45.6 50.1 6 0.20 0.588 20 397 E 73 68 68 69 l 24.9 29.B 61.9 45.6 50.l 6 0.20 0.588 20 397 E .'-
.) 70 47 55 63 l 24.9 29.8 61. 9 45.6 50.1 6 0.20 0.588 20
(. 397 E 4 66 66 60 46 l 24.9 29.8 61.9 45.6 50.1 6 0.20 0.588 20 398 D 1 17 20 19 23 12.5 12.8 23.2 6 0.20 0.588 40 396 D 2 32 16 21 14 l* 12.5 12.8 23.2 6 0.20 0.588 40 398 D .
.) 22 20 19 22 l 12.5 12.8 23.2 6 0.20 0.588 40 398 D 4 40 24 24 23 l 12.5 12.8 23.2 6 0.20 0.588 40 398 E 1 NilD ND ND 40 l 13.4 14.6 36.2 26.0 26.0 6 0.20 0.588 40 398 E 2 82 77 82 82 l 13.4 14.6 36.2 26.0 26.0 6 0.20 0.588 40 398 .. E 398 E 3
4 81 ND NilD NilD 81 ND NilD 50
- 13.4 13.4 14.6 14.6 36.2 36.2 26.0 26.0 26.0 26.0 6
6 0.20 0.20 0.588 0.588 40 40 399 D 1 48 48 47 49 l* 54.2 54.8 84.4 6 0.20 0.588 50 399 D 2 49 46 48 46 54.2 54.8 84.4 6 0.20 0.588 ~o 399 D 3 51 50 50 54 t 54.2 54.8 S4.4 6 0.20 0.588 50 399 D 4 . 48 51 53 53 i 54.2 54.8 84.4 6 0.20 0.588 50 399 E ** 37 37 37 37 l . 49 .6 56.3 72.4 6 0.20 0.588 50 399 E 2 49 48 54 54 49.6 56.3 72.4 6 0.10 0.586 50 399 E 3 30 23 30 55 l* 49.6 56.3 72.4 6 0.20 0.588 50 399 E 4 46 51 43 50 49.6 56.3 72.4 6 0.20 0.588 50 400 D 1 45 46 47 49
- 50.4 51.4 83.7 6 0.20 0.588 60 400 D 400 D 2
'T 50 49 46 48 48 48 51 53
** 50.4 50.4 51.4 83.7 6 0.20 0.588 60
" 51.4 83.7 6 0.20 0.588 60 400 D 4 51 51 51 51
** 50.4 51.4 83.7 6 0.20 0.588 60 400 E 400 E 2 1 28 43 27 46 28 51 24 52
- 39.8 39.8 47.0 47.0 71.8 71.8 54.9 54.9 54.9 54.9 6
6 0.20 0.20 0.588 0.588 bO 60 400 E 3 25 33 19 . 47
- 39.B 47.0 400 !:... 4 45 48 45 46 ': 39.8 47.0 71.8 71.8 54.9 54.9 54.9 54.9 6
6 0.20 0.20 0.588 0.588 60 60 401 D 1 82 78 82 78 t BL 9 84.2 100.0 6 0.20 o.~00 80 401 D 2 80 82 82 82 l 81.9 84.2 100.0 6 0.20 0.588 80 401 D 'T 82 81 81 ' 81 g 81. 9 84.2 100;0 6 0.20 0.588 BO 401 D 4 75 76 81 81 81.9 401 E 1 so 77 73 79 l 70.2 84.2 77.3 100.0 92.8 6 6 0:20 0.20 0.588 0.588 80 80 401 E 2 73 73 73 73 l 70.2 77.3 92.8 6 0.20 0.588 80 401 t' ~
'T
,. 77 74 71 64 l 70.2 77.3 92.8 6 0.20 0.588 80
Page 11 of 136 IGADATA.580
- ID DEF PRO 402 402 402 402 E
D D D D 4 1 2 3 4 ECTl 73 72 70 72 68 ECT2 72 69 69 70 . 68 ECT3 73 70 68 70 69 ECT4 65 70 69 68 66 ECT5 t i i i AI 70.2 73.0 73.0 73.0 73.0 MA! 77.3 74.0 74.0 74.0 74.0
!'IP 92.8 99.6 99.6 99.6 99.6 AS MAS DENT 6
6 6 6 AXIAL 0.20 0.20 0.20 0.20 CIRC 0.588 0.588 0.588 0.588 DEPTH 401 80 100 100 100 402 E 1 82 82 82 82 'l 76.2 81.5 94.6 6 6 0.20 0.20 0.588 0.588 100 100 402 E 2 82 77 82 82 l 76.2 81.5 94.6 6 0.20 0.588 100 402 402 E E 4 81 78 81 79 81 76 82 77
*l 76.2 76.2 81.5 81.5 94.6 94.6 6
6 0.20 0.20 0.588 0.588 100 100 403 D 1 ~lD ND ND ND l 13.5 14.4 48.0 26.7 28.6 8 0.20 0.588 30 403 D 2 ND ND ND ND l 13.5 14.4 48.0 26.7 28.6 8 0.20 0.588 30 403 D 3 ND HD ND ND i 13.5 14.4 4B.O 26.7 2B.6 B 0.20 0.5BB 30 403 D 4 ND ND ND ND 13.5 14.4 4B.O 26.7 28.6 B 0.20 0.5B8 30
*403 403 E
E 1 2. 37 40 40 25 41 36 41 32 i l
- 11. 7
- 11. 7 14.0 14.0 33.1 33.1
- 21. 7
- 21. 7 24.3 24.3 8
B 0.20 0.20 0.58B 0.5BB 30 30 403 E 3 42 20 35 51 l 11. 7 14.0 33.1 21.7 24.3 8 0.20 0.5B8 30
.i03 E 4 41 44 42 45 l 11. i 14.0 33.1 21. 7 24.3 8 0.20 0.588 30 404 D 1 37 24 26 34 l 16.1 16.4 59.2 33.4 34.3 8 0.20 0.588 20 404 D 2 38 37 44 31 i 16.1 16.4 59.2 33.4 34.3 8 0.20 0.588 20 404 D 3 50 50 38 55 l 16.1 16.4 59.2 33.4 34.3 B 0.20 0.588 20 404 4 40 36 .36 38 16.1 16.4 59.2 33.4 34.3 D 8 0.20 0.58B 20 404 E 1 ND ND ND ND 15.9 19.7 52.3 37.2 37.3 B 0.20 0.5BB 20
(_. 404 404 404 405 405 E E E D D 3 1 2 2 4 NGD ND ND 46 47 NGD ND ND 45 43 NGO ND ND 46 47 NGD ND ND 45 49
*l 15.9 15.9 15.9 49.5 49.5
*19. 7 19.7 19.7 50.B 50.8 52.3 52.3 52.3 B4.1 B4.1 37.2 37.2 37.2 37.3 37.3 37.3 8
B B 8 8 0.20 0.20 0.20 0.20 0.20 0.58B 0.5BB 0".5BB 0.5BB 0.5BB 20 20 20 40 40 405 D 3 51 51 49 4B 49.5 50.8 B4.1 B 0.20 0.58B 40 405 405 D E 4 1 46 ND 43 ND 51 ND 53 ND. *l 49.5 36.6 50.8 46.8 84.1 65.3 8 8 0.20 0.20 0.5BB 0.5BB 40 40 405 E 2 35 ~?
.:i~ 47 43 l 36.6 46.8 65.3 8 0.20 0.588 40 405 405 E
~
3 4
<20 26 ND 14 21 19 NGD NGD
*l 36.6 36.6 46.8 46.8 65.3 65.3 8
8 0.20 0.20 0.5BB 0.5BB 40 40 406 D 1 55 50 51 55 l 59.8 61. 7 90.B 8 0.20 0.588 50 406 D 2 49 49 53 47 l 59.9 61.7 90.B B 0.20 0.588 50 406 D 3 55 56 53 53 l 59.B 61. 7 90.B 8 0.20 0.5BB 50 406 D 4 52 54 54 55 l 59.B 61. 7 90.8 B 0.20 O.SBB 50 406 E 1 26 27 40 35 l 49.0 57.3 74.B B 0.20 0.5BB 50 406 E 2 38 3B 40 4B l 49.0 57.3 74.B B 0.20 0.58B 50 406 E 3 34 17 27 41 l 49.0 57.3 74.B 8 0.20 0.5B8 50 406 407 E D 4 1 36 60 . 33 55 41 59 35 60
*l 49.0 63.0 57.3 64.6 74.B BB.B 8
B 0.20 0.20 0.5BB 0.5BB 50 60 407 D J. 5B 57 62 5B l 63.0 64.6 8B.B B 0.20 0.5BB 60 407 D 3 67 59 SB 60 l 63.0 64.6 BB.8 B 0.20 0.5BB 60 40i D 4 57 58 59 57 l 63.0 64.6 8B.B B 0.20 0.5BB 60 407 E 1 39 35 33 2B l 50.6 59.0 72.6 B 0.20 0.5B8 61) 407 E 2 43 40 53 51 l 50.6 59.0 72.6 8 0.20 0.588 60 407 E 't 6 19 29 37 l 50.6 59.0 . 72.6 B 0.20 0.5B8 60 407 E 4 45 46 43 41 l 50.6 59.0 72.6 8 . 0.20 0.58B 60 408 0 1 82 82 B2 82 l 91.6 92.2 100.0 B 0.20 0.588 80
- __. 408 408 408 D
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Page 12 of l36 ISADATA. 580
- ID DEF PRO 408 408 408 E
E E 3 4 ECTl 82 73 79 79 ECT2 72 71 76 ECT3 82 77 Bl 79 ECT4 80 B2 66 75 ECT5 l l l l AI 76.1 76.1 76.1 76.1 MAI 83.9 83.9 83.9 83.9 MP 92.6 92.6 92.6 92.6 AS MAS DENT 8 B B 8 AXIAL 0.20 0.20 0.20 0.20 CIRC 0.588 0.5BB 0.588 0.588 DEPTH
--------------------------------------------------------------------------------------------------~---------------------------------
408 82 BO 80 BO 80 409 409 D D 2 82 82 82 82 82 82 82 82
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92.7 92.9 92.9 100.0 100.0 8 B 0.20 0.20 0.588 0.588 100 100 409 D 3 81 81 81 B2 92.7 92.9 100.0 409 409 D E
'I 82 82 82 82 82 82 82 82
' l l 92.7 81.0 92.9 88.9 100.0 100.0 8
8 8 0.20 0.20 0.20 0.588 0.588 0.588 100 100 100 409 409 E C' I-2 "l'
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'L 82 57 82 76 82 BO *l 81.0 81.0 88.9 88.9 .
100.0 100.0 8 B 0.20 0.20 0.588 0.588 100 100 409 E 4 82 82 82 82 l 81.0 88.9 100.0 8 0.20 0.588 100 410 D 50 47 31 47 l 30.2 31.3 69.7 51.0 51.B 10 0.20 0.5BB 30 410 D 2 54 41 48 42 l 30.2 31.3 69.7 51.0 51.8 10 0.20 0.588 30 410 410 D D 3 4 45 36 41
*J.J 40 50 43 46
- 30.2 30.2 31.3 31.3 69.7 69.7 51.0 51.0 51.8 51.B 10 10 0.20 0.20 0.588 0.588 30 30 410 410 E
E 2 ND ND ND ND ND ND ND ND *** 24.8 24.8 31.2 31.2 60.1 60.1 47.0 47.0 48.4 48.4 10 10 0.20 0.20 0.588 0.588 30 30 410 E 3 ND ND trn NGD 24.8 60.1 47.0 4B.4 31.2 10 0.20 0.588 30 410 E 4 ND ND ND ND 24.8 31.2 60.1 47.0 48.4 10 0.20 0.588 30 411 D 68 66 63 63
- 14.2 15.1 56.5 33.2
,..,. ., 35.7 10 0.20 0.588 20 411 D 2 69 60 61 61
*l 14.2 15.1 56. 5 35.7 10 0.20 0.588 20 v.JaL 411 D 3 NQD* tlGD NllD 64 14.2 15.1 56.5 33.2 35.7 10 0.20 0.588 20 411 D 4 55 63 76 71 14.2 15.1 56.5 33.2 35.7 10 0.20 0.588 20 411 E ND ND ND ND s* 12.2 15.6 34.9 25.9 25.9 10 0.20 0.588 20
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411 411 E E 2 3 ND ND ND HD ND ND ND NQD *s 12.2 12.2 15.6 15.6 34.9 34.9 25.9 25.9 25.9 25.9 10 10 0.20 0.20 o.5ee 0.588 20 20 411 E 4 ND ND ND NllD 12.2 15.6 34.9 25.9 25.9 10 0.20 0.588 20 412 D
., 47 42 42 47
- 39.9 41.6 83.3. 57.3 58.7 10 0.20 0.588 40 412 D L 56 53 53* 52 ** . 39.9 41.6 83.3 57.3 58.7 10 0.20 0.588 40 412 412
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D 1 2 ND 18 ND ND ND ND ND 18
** 12.4 12.4 13.4 13.4 19.9 19.9 0.20 0.20 0.588 0.5BB 30 30 .
464 D 3 3 16 16 NGD *t 12.4 13.4 19.9 --- 0.20 0.58B 30 464 D 4 12 9 12 3
*t 12.4 13.4 19.9 --- 0.20 0;588 30 464 E 1 ND ND ND ND 15.6 15.8 23.2 --- 0.20 0.5B8 30 464 E 2 20 14 27 38
- 15.6 15.B 23.2 --- 0.20 0.588 30 464 E 3 21 11 11 21
*t 15.6 15.B 23.2 --- 0.20 0.588 30 464 E 4 14 15 14 32 15.6 15.B 23.2 --- 0.20 ' 0.588 30 465 A 1 ND ND ND ND 12.6 13.2 18.5 6 0.20 0.5BB 40 465 A 2 ND ND ND ND
*l 12.6 13.2 18.5 6 0.5B8 40
,..,, 0.20 \
465 A. ND ND ND ND t 12.6 13.2 18.5 6 0.20 0.508 40 465 A 4 ND ND ND ND 12.6 13.2 18.5 6 0.20 0.508 40 465 B 1 54 61 49 56 t
- 10.3 11.0 18,8 10 0.20 0.508 40 465 B 2 47 SB 38 43 l 10.3 11.0 10.8 10 0.20 0.588 40 465 B 3 43 38 29 43 t 10.3 11.0 18.8 10 0.20 0.5B8 40 465 B 4 tlGD NGD NGD NGD t 10.3 11.0 18.8 10 0.20 0.588 40 465 c 1 ND 8 6 9 11.5 13.0 19.5 16 0.20 0.5B8 40 465 c ,. 2 ND ND ND ND l* 11.5 13.0 19.5 16 0.20 0.588 40 465 c .,, ND ND ND ND 11.5 13.0 19.5 16 0.20 0.588 40 ,: .
465 c 4 ND ND HD ND l* 11. 5 13.0 19.5 16 0.20 0.58B 40 465 D 1 5 6 3 6
*t 11. 7 12.5 19.0 21 0.20 0.588 40 465 D 2 17 31 24 24 11. 7 12.5 19.0 21 0.20 0.588 40 465 D 3 5 9 NGD 7 t 11.7 12.5 19.0 21 0.20 0.588 40 465 D 4 B 11 5 3 t 11. 7 12.5 19.0 21 0.20 0.588 40 465 465 E
E 1 2 22 65 21 39 18 50 22 36
*t 12.5 12.5 13.5 13.5 23.3 23.3 4
4 0.20 0.20 0.588 0.580 40 40
- ~
Page 18 of 136 ISADATA.580 ID DEF PRO ECT1 ECT2 ECT3 ECT4 ECT5 AI 11AI 11P AS 11AS DENT AXIAL CIRC DEPTH 465 E 3 3 14 9 11 t 12.5 13.5 23.3 4 0.20 0.588 40 465 E 4 38 39 38 24 12.5 13.5 23.3 4 0.20 0.588 40 466 D 1 29 15 14 25 t* 16.7 16.9 20.1 --- 0.20 0.588 20 466 D 2 22 25 34 55 ** 16.7 16.9 20.1 --- 0.20 0.588 20 466 D 3 3 18 NOD 21 t 16.7 16.9 20.1 --- 0.20 0.588 20 466 D 4 55 71 14 70
*t 16.7 16.9 20.1 --- 0.20 0.588 20 466 E 1 ND ND ND ND 17.3 17.6 21.0 --- 0.20 0.588 20 466 E 2 ND ND ND ND l 17.3 17.6 21.0 --- 0.20 0.588 20 466 E 3 ND ND NOD NOD t 17.3 17.6 21.0 --- 0.20 0.588 20 466 E 4 ND ND ND ND l 17 .3 17.6 21.0 --- 0.20 0.588 20 467 A 1 27 30 26 27 t 36.2 36.6 46.2 6 0.20 0.588 50 467 A 2 20 30 30 31 l 36.2 36.6 46.2 6 0.20 0.588 50 467 467 A
A 3 4 26 25 25 24 26 27 27 27 l 36.2 36.2 36.6 36.6 46.2 46.2 6 6 0.20 0.20 0.588 0.588 50 50 467 467 B B 1 2 37 30 37 33 37 30 37 34
*l 38.6 38.6 39.7 39.7 60.4 60.4 10 10 0.20 0.20 0.588 0.588 50 50 467 B 3 32 27 27 32 38.6 39.7 60.4 10 0.20 0.588 50 467 B 4 34 35 38 39 38.6 39.7 60.4 10 0.20 0.588 50 467 c 1 27 29 29 29 *t 38.1 . 38.6 57.8 4 0.20 0.588 50 467 "\, 2 30 30 30 30 38.l 38.6 57.8 4 0.20 0.588 50 467 c 3 36 36 35 30 t* 38.1 38.6 57.8 4 0.20 0.588 50 467 c 4 29 29 27 29 *. 38.1 38.6 57.8 4 0.20 0.588 50
'..\. 467 467 467 467 467 467 D D D D E E 2 1 2 3 4 1 22 30 28 29 32 36 22 30 35 31 34 36 22 30 28 22 28 35 23 30 33 27 29 36 l l l l l
- 40.6 40.6 40.6 40.6 43.0 43.0 41.1 41.1 41.1 41.1 43.4 43.4 54.9 54.9 54.9 54.9 58.4 58.4 21 21 21 21 15 15 0.20 0.20 0.20 0.20 0.20 0.20 0.588
. 0.588 0.588 0.588 0.588 0.588 50 50 50 50 50 50 467 467 E E 3 4
30
. 35 30 31 32 34 27 35 ** 43.0 43.0 43.4 43.4 58.4 58.4 15 15 0.20 0.20 0.588 0.588 50 50 468 D 1 33 33 32 32 t 43.6 43.B 50.6 --- 0.20 0.588 60 468 D 2 40 42 42 40 l 43.6 .43.8 50.6 --- 0.20 0.588 60 468 D 3 48 47 45 48 t 43.6 43.B 50.6 --- 0.20 0.588 60 468 D 4 41 42 43 42 43.6 43.8 50.6 --- 0.20 0.588 60 468 E 1 32 33 34 33 l* 45.2 45.3 50.4 --- 0.20 0.588 60 468 E 2 36 36 35 37
- 45.2 45.3 50.4 --- 0.20 0.588 60 468 E 3 42 42 43 42
- 45.2 45.3 50.4 --- 0.20 0.5BB 60 468 E 4 37 32 36 37
- 45.2 45.3 50.4 --- 0.20 0.588 60 469 469 D
D 1 2 17 5 20 18 22 6 17 20 ** . 17.2 17.2 lB.1 18.1 24.2 24.2 0.20 0.20 0.588 0.5BB BO BO 469 D 3 ND 11 5 3
- 17.2 18.1 24.2 --- 0.20 0.5BB BO
. 469 D 4 12 11 9 9
- 17.2 18.1 24.2 --- 0.20 0.588 BO 469 469 E
E 1 2 ND ND ND ND ND ND ND ND ** 19.3 19.3 19.9 19.9 27.2 27.2 0.20 0.20 0.588 0.588 80 80 469 E 3 ND ND ND ND
*l 19.3 19.9 27.2 --- 0.20 0.588 BO 469 I'"
~ 4 ND ND ND ND 19.3 19.9 27.2 --- 0.20 0.588 80 470 D 1 32 31 32 30 l 43.4 44.0 57 .o --- 0.20 0.588 100 470 D 2 37 37 37 38 43.4 44.0 57.0 --- 0.20 0.588 100 470 D 3 41 41 41 43 43.4 44.0 57.0 --- . 0.20 0.588 100 470 0 4 36 41 38 38 43.4 44.0 57.0 0.20 0.588 100 470 E 1 43 43 45 44
- 54.9 55.8 66.3 0.20 *o.588 100 470 470 E
E 2 3 51 55 49 55. 51 53 49 55
- 54.9 54.9 55.8 55.8 66.3 66.3 ---
0.20 0.20 0.588 0.588 100 100
Page 19 o.f 136
- ISADATA.580 ID DEF PRO 470 471 471 471 E *4 D
D D 1 "l. 3 ECTl 49 12 15 16 ECT2 50 15
.15 ND ECT3 48 18 15 14 ECT4 45 18 11 18 ECT5
'l AI 54.9 11.5
- 11. 5 11.5 llAI 55.B 11.9 11.9 11.9 l'IP 66.3 18.8 18.8 18.8 AS l'IAS DENT AXIAL 0.20 0.20 0.20 0.20 CIRC 0.588 0.588 0.588 0.588 DEPTH
--------------------------------------------------~---------------------------------------------------------------------------------
100 30 30 30 471 D 4 9 9 11 12 11.5 11.9 18.8 0.20 0.588 30 471 471 E E 1 l. 24 29 NOD 26 ND 24 29 42 12.7 12.7 14.4 14.4 20.1 20.1 0.20 0.20 0.588 0.588 30 30 471 471 E E 3 4 28 45 42 25 32 30 46 30
- 12.7 12.7 14.4 14.4 20.1 20.1 0.20 0.20 0.588 0.588 30 30 472 472 D
D
.,1 ND ND ND ND ND ND ND ND
'l 1.1 1.1 2.2 2.2 7.6 7.6 0.20 0.20 0.588 0.588 20 20 472 472 D
D 3 l. 4 ND ND ND NOD ND NOD ND NGD l 1.1 1.1 2.2 2.2 7.6 7.6 0.20 0.20 0.588 0.588 20 20 472 472 E 1 2 ND NOD ND NOD ND NOD ND tmD
0.9 0.9 1.6
*1.6 7.6 7.6 0.20 0.20 0.588 0.588 20 20 472 472 E
E E 3 4 ND ND ND NOD ND NOD NOD NOD l 0.9 0.9 1.6 1.6 7.6 7.6 0.20 0.20 0.588 0.598 20 20 473 20 15 18 17 34.0 36.7 41.8 0.20 0.588 40 473 D D 2 25 25 26 25 ' 34.0 36.7 41.8 0.20 0.588 40 473 473 D D 3 4 28 26 28 25 28 26 30 27
'l 34.0 34.0 36.7 36.7 41.8 41.8 0.20 0.20 0.588 0.588 40 40 473 E 1 39 42 42 40 l 30.7 33.4 38.5 0.20 0.588 40 473 E 2 42 44 42 43 30.7 33.4 38.5 0.20 0.588 40 473 473 E
E 3 4 45 44 45 43 46 44 43 45 l 30.7 30.7 33.4 33.4 38.5 38.5 0.20-0.20 0.588 0,588 40 40 ' 474 D 1 ND ND ND ND 17.8 18.6 26.9 0.20 0.588 50 474 D 2 11 5 6 ND
- l 17.B 18.6 26.9 0.20 0.588 50 474 D 3 ND ND NOD NOD 17.8 18.6 26.9 0.20 0.588 50 474 D 4 ND ND ND ND '* 17.8 18.6 26.9 0.20 0.588 50 474 E r 30 25 27 29 23.2 24.0 39.9 . 0.20 0.588 50 474 E 2 34 31. 34 24
- 23.2 24.0 39.9 0.20 0.588 50 474 474 E.
E 4
.,. 20 31 11 22 18 29 23 32
'l l
23.2 23.2 24.0 24.0 39.9 39.9 0.20 0.20 0.588 0.588 50 50 475 D 1 NGD 31 25 34 11.5 11. 7 17.5 0.20 O.SBB 60 475 D 2 58 45 48 36 11.5 il. 7 17.5 0.20 0.588 60 475 D 16 36 ND NOD 11.5 11.7 17.5 0.20 0,588 60 475 D 4 NOD 59 76 61 11.5 11.7 17.5 0.20 0.588 60 . 475 E 1 ND ND ND ND 13.7 13.B 18.7 0.20 0.588 60 475 E 2 NOD NGD NOD NOD
- 13.7 13.8 18.7 0.20 0.588 60 475 475 E
E 3 4 ND NOD ND NGD ND 96 NGO 96 i 13.7 13.7 13.8 13.8 18.7 18.7 0.20 0.20 0.588 0.588 60 60 476 D J.' 20 18 18 15 18.6 19.1 25.5 0.20 0.588 BO 476 D 2 15 15 17 14
- l 18.6 19.1 25.5 0.20 0.588 BO 476 D ,.... 7 9 9 16 l 18.6 19.1 25.5 0.20 0.588 BO 476 D 4 19 17 19 22 18.6 19.1 25.5 0.20 0.5B8 BO 476 476 E
E 1 2 21 22 18 24 18 24 18 24 l l 24.6 . 24.6 26.2 26.2 38.6 38.6 0.20 0.20 0.588 0.5BB BO BO 476 E 3 27 25 20 20 l 24.6 26.2 38.6 0.20 0.5B8 80 476 E 4 21 19 21 21 l 24.6 26.2 38.6 . 0.20 0.5BB BO 477 D 1 65 66 66 65 l 77.8 78.1 84.1 0.20 0.5BB 100 477 D 68 70 69 68 i 77.8 78.1 84.1 0.20 0.588 100 l.
*.* 477 D 74 74 72 75 l 77.B 78.1 84.1 0.20 0.5BB 100 477 D 4 68 67 66 68 l 77 .8 78.1 84.1 0.20 0.588 100
Page 20 of 136
!6ADAiA.5BO
- ID DEF PRO 477 477 477 477 480 E
E E E D
'l 3
4 1 ECTl 67 70 76 69 26 ECT2 70 76 70 25 ECT3 67 70 74 68 26 ECT4 74 68 25 ECT5
*l Al 79.2 79.2 79.2 79.2 MAI 80.6 80.6 80.6 80.6 MP 87.5 87.5 87.5 87.5 AS MAS CENT AXIAL 0.20 0.20 0.20 0.20 0.20 CIRC 0.588 DEPTH 68
*70 *68 100 0.588 . 100 0.588 0.588 100 100
,, 1. 763 40 480 D 36 36 36 37 0.20 1.763 40 480 D
~
3 41 42 29 42 0.20 1.763 40 480 D 4 ')C 25 26 35
- 0.20 1. 763 40 480 E Lu 37 34 35 36
- 0.20 2.355 40 480 E 2 40 39 38 39
- l 0.20 2.355 40 480 E 1' 47 47 46 4b 0.20 2.355 40
*.J 480 E 't 481 D 1 36 33 37 33 36 33 37 32 *l 0.20 0.20 2.355
. 0.460 40 40 481 D 2 40 39 39 39 l 0.20 0.460 40 481 D 3 45 46 45 45 i 0.20 0.460 40 481 D 4 34 ""1'
*)v *34 37 0.20 0.460 40 481 E 47 45 46 46
- 0.20 0.588 40 481 E 2 50 49 48 48
- l 0.20 0.588 40 481 E 3 481 E 4 54 48 54 47 54 47 54 49 s
0.20 0.20 0.588 0.588 40 40 482 D 1 tiD ND ND ND l 0.20 0.070 40 482 D i.,, ND ND ND ND l 0.20 0.070 40 482 *o 482 D 4 3 ND NGO tlD ND ND NGD ND NGD ** 0.20 0.20 0.070 0.070 40 40 482 E 1 ND ND ND ND 0.20 0.130 40 s* /1
- 482 E 2 89 87 89 NGD 0.20 0.130 40 482 E 3 ND ND
- ND ND 0.20 0.130 40 482 E 4 NGD ND 97 92 l 0.20 0.130 40 483 D 1 20 15 20 20 0.20 0.588 40 483 D 2 15 15 18 17
- l 0.20 o. 588 40 483 ..,
1' 20 18 18 20 l 0.20 0.588 40 483 '
't 17 19 19 19 l 0.20 0.588 40 483 483 E 2 ND
. ~
J.i 17 18 18 6 15 8 g 0.30 0.30 0.588 0.588 40 40 483 E "1' *.J 16 11 9 11 0.30 o. 588 40 483 E 4 NGD NGD NGD NGD
- 0.30 0.588 40 382 D 15 15 19 7
- 30.8 31.5 77.6 45.3 47.3 382 D .,
2 0.20 0.588 30 L 18 16 17 10* l* 30.8 31.5 77.6 45.3 47.3 2 0.20 0.588 30 382 D 3 24 22 24 21 l 30.B 31.5 77.6 45.3 47.3 2 0.20 0.588 30 382 D 4 29 22 17 27 30.8 31.5 77.6 45.3 47.3 2 0.20 0.588 30 382 E 1 21 34 25 29
- 26.2 33.3 382 382 E
2 3 31 27 27 31 28 24 29 29 l 26.2 26.2 33.3 33.3 58.6 58.6 58.6 50.2 50.2 50.2 50.2 50.2 50.2 2 2 2 0.20 0.20 0.20 0.588 0.588 0.588 30 30 30 382 383 E D 4 21 ND ND 9 NGD NGD 10 ND *l 26.2
- 11. 5 33.3 12.1 58.6 26:1 50.2 50.2 2 2
0.20 0.20 0.588 0.588 30 20 383 383 D D 2 1' ND NJD ND HD ND NGD ND NGD
- 11.5
- 11. 5 12.1 12.1 26.1 26.1 2 0.20 0.588 20 383 D 4 ND ND ND . ND '
l 11.5 12.1 26.1 2 2 0.20 0.20 . 0.588 0.588 20 20 383 E MD ND NGD ND 14.2 24.2 383 E 2 64 *ND ND ND 'l 11.3 11.8 14.2 24.2 2 2 0.20 0.20 0.588 0.588 20 20 383 E 3 ND ND HD ND
- 11.8 14.2 24.2 2 0.20 0.588 20 383 384 E
D 4 NGD 38 ND 3b HGD 38 ND 40
- 11.8 51.8 14.2 53.0 24.2 78.2 2 0.20 0.588 20
' 2 0.20 0.588 40
Page 21 of 136
- IRDATA. 580 ID DEF PRO ECT1 ECT2 ECT3 ECT4 ECT5 DENT CIRC
- AXIAL DEPTH '.~DEPTH 205 A 1 ND ND ND ND t -- 0.375 .008 0.049 100 205 A 2 ND.* ~D ND ND t -- 0.375 .008 0.049 100 205 A 3 ND ND ND ND t -- 0.375 .008 0.049 100 205 A 4 ND ND ND ND t -- 0.375 .008 0.049 100 205 B 1
.,i.
61 58 59 60 t -- 0.375 .007 0.028 60 205 B 89 . 89 87 82 t -- 0.375 .007 0.028 60 205 B 3 91 90 90 90 l -- 0.375 .007 0.028 60 205 B 4 89 89 90 89 l -- 0.375 .007 0.028 60 205 c 1 62 62 62 60 l -- 0.375 .007 0.038 80 205 c c 2 71 63 63 65 * -- 0.375 .007 0.038 80 205 205 c 3 4 68 61 68 59 72 62 72 59
*l -- 0.375 0.375
.007
.007 0.038 0.038 80 80 205 D 1 89 89 87 89 t -- 0.375 .006 0.019 40 205 D 2 65 62 62 65 i -- 0.375 .006 0.019 40 205 D 3 66 64 65 63
*l -- 0.375 .006 0.019 40 205 D 4 62 62 62 64 -- 0.375 .006 0.019 40 205 E 1 ND ND ND ND -- 0.375 .006 0.022 45 205 E 2 113 ND ND 51 t* -- 0.375 .006 0.022 45 205 E 3 54 113 58 54 t -- 0.375 .006 0.022 45 205 E 4 68 52 62 51
* ---- 0.375 .006 0.022 45 205 F 1 ND ND ND . ND 0.375 .006 0.010 20 205 F 2 ND ND ND ND 0.375 .0011 0.010 20 205 F 3 ND ND ND ND 0.375 .006 0.010 20 205 F 4 ND ND ND ND t -- 0.375 .006 0.010 20 209 209 A
A 1 2 39 39 43 23 42 33 35 *l -- 0.375 .006 0.018 38 31 0.375 .006 0.018 38 209 A 3 35 32 25 31 t -- 0.375 .006 0.018 38 209 A 4 22 24 28 28 t -- 0.375 .006 0.018 38 209 B 1 ND ND 21 38
- 10 0.375 .006 0.020 42 209 209 B
B 2 3 ND NGD ND NGO ND NGO ND 81
*s 10 10 0.375 0.375
.006
.006 0.020 0.020 42 42 209 209 B
c 4 1 NGO 50 81 53 77 47 77 40 .t
- 10 9
0.375 0.375
.006
.006 0.020 O.Oli 42 35 209 c 2 ND ND 69 ND t q 0.375 .006 0.017 35 209 c 3 39 52 50 44 .a 9 0.375 .006 0.017 35 209 c 4 ND ND ND ND
*t 9 0.375 .006 0.017 35 209 D 1 72 ND ND 76 6 0.375 .006 0.018 38 209 209 D
D 2 3 ND. NGO ND NUD ND NQD 48 NGD ** 6 b 0.375 0.375 .
.006
.006 0.018 0.018 38 38 209 D 4 ND 60 70 62 Ii 0.375 .006 0.018 38 209 E 1 82 82 ND 81
- 4 0.375 209 E 2 ND ND ND 51 '* 4 0.375
.006
.006 0.020 0.020 42 42 209 209 E
E 3 4 NGO 71 NGD 65 NGO 65 NQD 72
- 4 4
0.375 0.375
.006
.006 0.020 0.020 42 42 209 F 1 ND ND ND ND
- 2 0.375 .006 0.017 35 209 209 F
F 3 2 ND NGO ND NQD ND NGO ND NGD ** 2 2 0.375 0.375
.006
.006 0.017 35 209 210 F
A 1 4 ND 53 ND 53 ND 53 ND 53
2 0.375 0.375
.006
.006 0.017 0.017 0.025 35 35 52 210 A 61 63 57 60 -- 0.375 .OOli 0.025 52 210 A 3" 47 50 55 50 * -- 0.375 210 210 A
B 1 4 55 ND 58 ND 56 28 ND 61 l 10 (l.375 0.375
.006
.006
.006 0.025 0.025 0.025 52 52 52
Page 22 of 136
- CIRDATA.580 ID DEF PRO 210 210 210 210 B
B B c
'I 3
4 1 ECTl ND ND NGD ND ECT2 ND ND NGD ND ECT3 ND ND NGD 14 ECT4 ECT5 DENT ND ND NGD ND t t 10 10 10 8 CIRC 0.375 0.375 0.375 0.375 AXIAL
.006
.006
.006
.006 DEPTH 7.DEPTH 0.025 0.025 0.025 0.025 52 52 52 52 210 c 2 ND ND 82 ND t 8 0.375 .006 0.025 52 210 c 3 NGD NGD NGD NGD t 8 0.375 .006 0.025 52 210 c 4 ND NGD NllD NGD t 8 0.375 .006 0.025 52 210 D 1 ND ND 77 ND
- 6 0.375 .006 0.025 52 210 D 2 ND ND 82 ND
- 6 0.375 .006 . 0.025 52 210 210 D
D 3 4 67 ND 61 ND 70 ND 64 15 *t 6 6 0.375 0.375
.006
.006 0.025 0.025 52 52 2.10 E 1 ND ND ND ND t 4 0.375 ,006 0.026 54 210 210 E
E 2 3 i3 81 ND 79 ND 81 ND 78
*** 4 4
0.375 0.375
.006
.006 0.026 0.026 54 54 210 E 4 NGD ND Bl 79 t 4 0.375 .006 0.026 54 210 F 1 45 53 53 50 t 2 0.375 .006 0.027 56 210 F 2 54 47 53 49 t 2 0.375 .006 0.027 56 210 F 3 64 74 78 70 2 0.375 .006 0.027 56 210 F 4 51 SB 46 55
- 2 0.375 .006 0.027 56 211 A 1 71 72 71 72 ** -- 0.375 .006 0.030 63 211 A 2 73 15 70 74 t -- 0.375 .006 0.030 63 211 A 3 72 74 74 72 t -- 0.375 .006 0.030 63 211 A 4 73 73 72 72 t -- 0.375 .006 0.030 63 211 B 1 ND 20 22 28 a 10 0.375 .006 0.030 63
- 211 211 211 211 211 B
B B c c 2 3 4 1 2 ND NGD NGD ND ND ND NGD NOD 14 ND ND NGD NGD
- ND 7
ND NOD NGD 34 ND
*t t
*t 10 10 10 B
B 0.375 0.375 0.375 0.375
.006
.006
.006
*006 0.030 0.030 0.030 63 63 63 0.030 . 63.
O.U5 .006 0.030 63 211 c .,,
't Bl Bl 81 Bl
- B 0.375 .006 0.030 63 211 211 c
D 4 1 NGD ND NGD ND NGD NGD ND . ND ** B 6 0.375 0.375
.006
.006 0.030 0.032 63 67 211 D ...'I ND 82 82 82 t 6 0.375 .006 0.032 67 211 D .J NGD NllD NGD NGO t 6" 0.375 .006 0.032 67 211 D 4 ND ND NQD Bl t. 6 0.375 .006 0.032 67 211 E 1 ND ND ND ND
- 4 0.375 .006 0.031 65 211 211 E
E 2 3 82 72 82 66 82 69 82 68
- 4 4
0.375 0.375
.006
.006 0.031 0.031 65 65 211 211 E
F 4 1 70 ND NQD ND ND BO 78 ND ** *t 4 3 0.375 0.375
.006
.006 0.031 0.034 65 .
71 211 F 2 ND ND ND 81 3 0.375 .006 0.034 71 211 F 3 *81 Bl 81 78 3 0.375 .006 0.034 71 211 F 4*'<'""- ND ND ND ND 3 0.375 .006 0.034 71 212 A. ( 94 93 93 94 t -- 0.375 .006 0.049 100 212 ~ . 2 94 92 94 94 t -- 0.375 .006 0.049 100 212 A 3 94 94 94 94 t . -- 0.375 .006 0.049 100 212 A 4 94. 94 94 94
*t -- 0.375 .006 0.049 100 212 B 1 65 21 76 66 11 0.375 .006 0.049 100 212 B 2 45 55 ND B2 t 11 0.375 .006 0.049 100 212 B 3 67 60 59 70 t 11 0.375 .OOb 0.049 100 212 212 B
c 1 4 NGD 82
. NQD 82 NGO 82 73 82
*t 11 8
0.375 0.375
.006
.006 0.049 0.049 100 100 212 c 2 24 ND 82 82 t 8 0.375 .006 0.049 100
Page 23 of. 136 . CIRDATA.580 ID DEF PRO ECTl ECT2 ECT3 ECT4 ECT5 DENT CIRC AXIAL DEPTH ZDEPTH 212 c 3 81 Bl Bl Bl t B 0.375 .006 0.049 100 212 c 4 NllD ND ND ND B 0.375 .006 0.049 100 212 D 1 B2 B2 B2 82
- 6 0.375 .006 0.049 100 212 D 2 82 82 82 82
- 6 0.375 .006 0.049 100 212 D 3 81 Bl 81 81 *t 6 0.375 .006 0.049 100 212 D 4 82 82 82 82 t 6 0.375 .006 0.049 100 212 E 1 82 82 82 82 4 0.375 .006 0.049 100 212 E 2 82 82 B2 82 ** 4 0.375 .006 0.049 100 212 212 E
E 3 4 81 82 81 ND 81 82 81 NllD
- 4 4
0.375 0.375
.* 006
.006 0.049 0.049 100 100 212 F 1 82' 82 82 B2 t* 2 0.375 .006 0.049 100 212 F 2 B2 82 82 82 t 2 0.375 .006 0.049 100 212 F 3 81 81 81 81 t 2 0.375 .006 0.049 100 212 F 4 82 ND 82 NOD
- 2 0.375 .OOb 0.049 100
Page 24 of 136 WASDATA.540 ID D.EF PRO ECTl ECT2 ECT3 ECT4 ECT5 DENT CIRC AXIAL DEPTH '.tDEPTH 168 A 84 85 75 BS l 0.110 (l.110 0.029 60 168 A 2 74 74 73 74 0.110 0.110 0.029 60 168 168 A A 3 4 75 74 77 72 77 74 77 76
*l* 0.110 0.110 0.110 0.110 0.029 0.029 60 60 168 B 1 58 56 56 58 2 0.110 0.110 0.029 60 168 B 2 82 82 74 74
- l 2 0.110 0.111) 0.029 60 168 B 3 65 82 70 70 2 0.110 0.110 0.029 60 168 168 B
c 4 1 82 62 82 59 82 57 82 61
*l 2 4
0.110 0.110 0.110 0.110 0.029 0.030 60 63 168 c 2 82 82 74 82
- 4 0.110 0.110 0.030 63 168 c 3 53 56 46 77 4 0.110 0.110 0.030 63 168 c 4 73 77 72 77 l
- 4 0.110 0.110 0.030 63 168 D 1 63 80 69 63 6 0.110 0.110 0.030 63 168 D 2 79 82 81 79 6 0.110 0.110 0.030 63 168 D 3 ND NGD ND ND 6 0.110 0.110 0.030 63 168 D 4 NQD 82 NGD NGD 6 0.110 0.110 0.030 63 168 E 66 52 63 72 8 0.110 0.110 0.030 63 168 E 2 52 80 69 71 8 0.110 0.110 (i.030 ~*~*
168 E 3 82 NGD ND ND 8 0.110 0.110 0.030 63 168 E 4 NGD NGD NGO NQD *a 8 0.110 0.110 0.030 63 168 F 1 36 36 37 44 l 10 0.110 0.110 0.028 58 (. 168 F 2 40 48 57 42 l 10 0.110 0.110 0.028 58 168 F 3 54 68 ND ND
- 10 0.110 0.110 0.028 58 168 F 4 ND ND ND ND
- 10 0.110 0.110 0.028 58 169 A 1 61 61 61 61
- 0.109 0.109 0.028 58 169 A 2 65 65 65 64
- 0.109 0.109 0.028 58 169 169 A
A 3 4 63 64 64 63 64 63 64 64
- 0.109 0.109 0.109 0.109 0.028 0.028 58 58 169 B 1 64 67 66 64 2 0.109 0.109 0.029 60 169 B i. 60 59 57 60
- 2 0.109 0.109 0.029 ' 60 169 169 B
B 3 4 73 66 76 67 75 64 76 65
- 2 0.109 0.109 0.029 60 169 c c
1 55 55 55 53 '* 2 4 0.109 0.109 0.109 0.109 0.029 0.028 60 58 169 2 50 41 39 45 4 0.109 0.109 0.028 58 169 c 3 68 63 61 65 4 0.109 0.109 0.028 58 169 c 4 55 58 51 57 g 4 0.109 0.109 0.028 58 169 D 1 54 53 54 54
- 6 0.109 0.109 0.029 60 169 169 D
D 2 3 54 61 47 66 40 65 46 57
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- ID 423 424 424 424 424 DEF PRO E
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/, 69 62 63 25.9 29.4 62.7 41.2 48.2 15 0.20 o. 588 50 428 D 43 44 46 44 58.5 60.1 78.b 15 0.20 0.588 60 428 D 2 46 44 46 40 58.5 60.1 78.b 15 0.20 0.588 bO 428 D .,..;, 49 49 53 53 58.5 60.1 78.6 15 0.20 0.588 60 428 D 4 56 56 55 56 58.5 60.1 78.6 15 0.20 0.588 60 428 E 41 20 32 30 52.7 58.2 80.0 15 0.20 0.588 60 428 E 2 37 42 41 40 52.7 5B.2 80.0 15 0.20 0.588 60 428 E 3 38 45 61 55 52.7 58.2 80.0 15 0.20 0.588 60 428 E 4 70 68 64 65 52.7 58.2 80.0 15 0.20 0. 588 60.
429 D 82 82 82 82 90.3 91.5 100.0 15 0.20 0.588 80 429 D .I. 79 80 79 78 90.3 91. 5 100.0 15 0.20 0.588 80 429 D .;, 82 82 82 82 90.3 91.5 100.0 15 0.20 0.588 80 429 D 82 82 B2 82 90.3 91.5 100.0 15 0.20 0.588 BO 429 E 82 82 82 82 82.2 88.6 96.9 15 0.20 0.588 80 429 E 'l
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*j 35.7 42.3 84.4 60.5 73.1 25 0.20 0.588 30 438 E 2 29 21 24 31 35.7 42.3 84.4 60.5 73.1 25 0.20 0.588 30 438 E 3 24 <20 NGD 43 35.7 42.3 84.4 60.5 73.1 25 0.20 0.588 30 438 t:. 4 bb bl 55 49 35.7 42.3 84.4 60.5 73.1 25 0.20 0.588 30 439 D 1 ND NGD 82 NGD 22.5 23.1 61.7 49.B 53.5 25 0.20 0.588 20 439 D 2 ND ND ND ND 22.5 23.1 61. 7 49.8 53.5 25 0.20 0.588 20 439 D 3 ND ND NGD NllD l 22.5 23.1 6L7 49.8 53.5 25 0.20 0.588 20
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Page 40 of 136
!SADIHA.540
- ID 443 444 444
.444 444 DEF PRO E
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- 82 ND NQD ND NGO ND NQD ND NGD ND 8.1 8.1 48.2 48.2 48.2 48.2 10.2 10.2 49.3 49.3 49.3 49.3 21.3 21.3 69.2 69.2 69.2 69.2 17.2 17.2 17.2 17.2 30 30 30 30 30 0.20 0.20 0.20 0.20 0.20 0.588 0.588 0.588 0.588 0.588 20 20 40 40 40 30 0.20 0.588 40 447 E NGO NGD NQD NGD 40.4 44.4 78.2 56.0 62.5 30 0.20 0.588 40 447 E 2 tmD ND ND ND 40.4 44.4 78.2 56.0 62.5 30 0.20 0.588 40 447 E N9D NGD NGD N9D 40.4 44.4 78.2 56.0 62.5 30 0.20 0.588 40 447 E 4 ND ND ND tlD 40.4 44.4 78.2 56.0 62.5 30 0.20 0.588 40
?48 D 1 NQD NGD 82 NGD 34.0 34.9 71.5 49.0 49.7 30. 0.20 0.588 50 448 D ND . ND ND tlD 34.0 34.9 7L5 49.0 49.7 30 0.20 0.588 50 448 D 3 NOD NGD NGD NGO 34.0 34.9 71.5 49,0 49.7 30 0.20 0.588 50 448 D 4 ND ND ND ND 34.0 34.9 71. 5 49.0 49.7 30 0.20 0.588 so 448 E 1 NOD NQD NQD NGD 34.1 38.0 63.1 47.3 49.7 30 0.20 0.588 50 448 E 2 ND ND ND ND 34.1 38.0 63.1 47.3 49.7 30 0.20 0.588 50 448 E .,"i NGD NOD NGD . NGD 34.1 38.0 63.1 47.3 49.7 30 0.20 0.588 50 448 c: 4 ~rn ND ND tm 34.1 38.0 63.1 47.3 49.7 30 0.20 0.588 50 449 D 82 82 82 82 56.9 58.7 73.3 30 0.20 0.588 60 449 D 2 ND ND . ND ND 56.9 58.7 73.3 30 0.20 0.588 60 449 n 3 NQD 82 NQD 82 56.9 58.7 73.3 30 0.20 0.588 60 4;9 D .. NQD ND ND
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Page 41 of 136 ISA DATA. 540
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