* * * FOR ALL
TASK 72-31-45-200-807
1 . General.
A.This procedure gives instructions to do an inspection of the stages 6-10 compressor rotor spool (spool):
•
(01-480 , 72-31-00) (SIN 050AR)
•
(01-481 , 72-31-00) (SIN 050AR) (SB 72-0051)
•
(02-480 , 72-31-00) (SIN 050AR) (SB 72-0157).
B.Give particular attention to the important areas that follow:
•
Disk bores and webs
•
Interstage seal teeth
•
Air slots
•
Boltholes
•
Dovetail slots
•
Locking lug slots
•
Flanges
•
Fillets
•
Inertia welds.
2 . Tools, Equipment, and Materials.
NOTE:
You can use equivalent alternatives for tools, equipment, and consumable materials.
A.Tools and Equipment.
NOTE:
For information and purchase of probe arm fixturing, part fixtures, part riser, EC 9ft cable extension, cleaning tools, replacement items etc., contact GEAE FST Group (ndttooling@ge.com). Provide following information for each inquiry:
•
Document calling out the inspection
•
Engine Line
•
Part Name
•
Part Number
•
Inspection System/Model
•
Inspection Areas/Zones (ex: bores, webs, etc.)
(1)Special Tools. None.
(2)Standard Tools and Equipment.
 
Description
Manufacturer
 
Eddy current probe US-2280 (for ID inertia weld inspection)
Deleted
 
Eddy current probe US-2286 (for ID inertia weld inspection)
Deleted
 
Eddy current probe US-2289 (for OD inertia weld inspection)
Deleted
 
Eddy current probe US-3338 (for web, web slope and bore inspection) - not provisioned
Deleted
 
Eddy current probe US-3800 (for bore faces inspection)
United Western Technologies “UniWest”. Email: info@uniwest.com
 
Eddy current probe US-3813 (for web and web slope inspection).
United Western Technologies “UniWest”. Email: info@uniwest.com
 
Eddy current probe US-3815 (for I.D. and O.D. inertia weld inspections)
United Western Technologies “UniWest”. Email: info@uniwest.com
(3)Locally Manufactured Tools. None.
B.Consumable Materials.
 
Code No.
Description
 
C04-166
Shot, Peening, Conditioned Cut Wire (Cut Wire Shot, CCW14)
 
C10-021
Tape, Plastic (plastic tape)
 
C10-205
Almen Test Strips (test strips)
C.Referenced Procedures.
 
ATA No.
Description
 
70-32-02
Fluorescent Penetrant Inspection
 
Deleted
 
70-32-86
Enhanced 2 Mhz Eddy Current Inspection of Life Limited Hardware Using Systems Under Computer, Numeric, or Robotic Control
 
70-33-03
Special Inspection for Surface Fretting or Galling
 
70-42-00
Blending and Removal of High Metal Procedures
 
70-42-01
Polishing Bolt Hole Surfaces
 
70-47-01
Shotpeening
 
72-31-45
Cleaning 001
 
72-31-45
Repair 002
 
72-31-45
Repair 005
D.Expendable Parts. None.
3 . Specific Inspection Procedure.
NOTE:
Any findings beyond manual limits that can be indicative of a possible crack of metallurgical defect must be reported to GE through a myGEAviation Technical Inquiry.
Subtask 72-31-45-160-001
A.Make sure you remove the seal teeth coating before you do the inspections. Refer to TASK 72-31-45-100-801 (72-31-45, CLEANING 001).
Subtask 72-31-45-230-002
B.Do a Class G fluorescent penetrant inspection of the spool. Refer to TASK 70-32-02-230-001 (FLUORESCENT PENETRANT INSPECTION).
(1)Give particular attention to the important areas that follow:
•
Disk bores and webs
•
Interstage seal teeth
•
Air slots
•
Boltholes
•
Dovetail slots
•
Locking lug slots
•
Flanges
•
Fillets
•
Inertia welds.
(2)Do an inspection of the stage 6-10 spool deep cavity inner surfaces of the spacer arms zone 1 to zone 4 with a remote viewing video system. Refer to TASK 70-32-02-230-001 (FLUORESCENT PENETRANT INSPECTION) (paragraph 1.A.(5)(i)) and Figure 803.
(3)Masking is not necessary.
(4)Indications are not permitted. This does not include indications of 0.015 inch (0.38 mm) or less, which are non-interpretable and permitted.
(a)Optionally indications on the forward or aft pressure faces which are more than 0.015 inch (0.38 mm) can be interpreted at 30X or higher magnification after doing the following steps:
1Clean the area with a solvent dampened cotton swab or absorbent material.
2Application of dry developer and/or non-aqueous wet developer (NAWD) are not necessary when doing inspections at magnifications of 30X or higher.
3Do an inspection in the necessary inspection window for bleed back method (for example 10 minutes).
4Do an inspection at 30X or higher magnification at the same circumferential location on the pressure faces as seen with standard magnification (3X, 5X or 10X).
Subtask 72-31-45-110-005
C.Do an eddy current inspection at all inertia weld areas.
(1)Clean the spool. Refer to TASK 72-31-45-100-801 (72-31-45, CLEANING 001).
Subtask 72-31-45-250-001
(2)Do an eddy current inspection of the inertia weld surfaces both inside diameter (ID) and outside diameter (OD). Refer to TASK 70-32-86-250-801 (ENHANCED 2 MHZ EDDY CURRENT INSPECTION OF LIFE LIMITED HARDWARE USING SYSTEMS UNDER COMPUTER, NUMERIC, OR ROBOTIC CONTROL).
NOTE:
Deleted.
NOTE:
Changes to the procedure or substitutions for the equipment can cause you to detect less cracks. When you want to do or use something different, the procedure and equipment must be evaluated by General Electric Company.
NOTE:
For calibration, use correction factor for Rene 88 material. Refer to TASK 70-32-86-250-801 (ENHANCED 2 MHZ EDDY CURRENT INSPECTION OF LIFE LIMITED HARDWARE USING SYSTEMS UNDER COMPUTER, NUMERIC, OR ROBOTIC CONTROL).
NOTE:
Use a probe holder as appropriate to provide adequate coverage for all zones specified on the Eddy Current Scan Plan. Refer to Figure 801.
(a)Inspect the inertia weld areas (zone 6-7, zone 7-8, zone 8-9, and zone 9-10) shown in the eddy current scan plan. Refer to Figure 801.
1Use probe US-3815 for both ID and OD inspection.
2Deleted.
(b)Record the calibration data and inspection results on the eddy current inspection data sheet. Refer to Figure 802.
(c)Eddy current inspection evaluation limits.
1The evaluation limit for the inertia welds is 1000 mV.
(d)Eddy current inspection reject limits.
1The reject limit for the inertia welds is 1000 mV or greater, after evaluation is complete.
(e)All stage 6-10 spool that are rejected by the limits in Subtask 72-31-45-250-001 (paragraph 3.C.(2)(d)) are not serviceable.
(f)All stage 6-10 spool that are not rejected by the limits in Subtask 72-31-45-250-001 (paragraph 3.C.(2)(d)) are serviceable.
(g)Make sure that all records that were made during the eddy current inspection are as complete as possible. Permanently keep these records for each spool that was inspected.
Subtask 72-31-45-160-002
D.Do an eddy current inspection of all spool webs, web slopes and bore faces.
(1)Clean the spool. Refer to TASK 72-31-45-100-801 (72-31-45, CLEANING 001).
Subtask 72-31-45-250-002
(2)Do an eddy current inspection of the spool webs, web slopes and bore faces both forward and aft surface. Refer to TASK 70-32-86-250-801 (ENHANCED 2 MHZ EDDY CURRENT INSPECTION OF LIFE LIMITED HARDWARE USING SYSTEMS UNDER COMPUTER, NUMERIC, OR ROBOTIC CONTROL).
NOTE:
Deleted.
NOTE:
Changes to the procedure or substitutions for the equipment can cause you to detect less cracks. When you want to do or use something different, the procedure and equipment must be evaluated by General Electric Company.
NOTE:
For calibration, use correction factor for Rene 88 material. Refer to TASK 70-32-86-250-801 (ENHANCED 2 MHZ EDDY CURRENT INSPECTION OF LIFE LIMITED HARDWARE USING SYSTEMS UNDER COMPUTER, NUMERIC, OR ROBOTIC CONTROL).
NOTE:
Use a probe holder as appropriate to provide adequate coverage for all zones specified on the eddy current scan plan. Refer to Figure 801.
(a)Do an inspection of all the zones on the webs, web slopes, and bores shown in the eddy current scan plan. Refer to Figure 801 for zone definitions.
1Use probe US-3813 for web and web slopes inspection.
2Use probe US-3800 for bore faces inspection.
(b)Record the calibration data and inspection results on the eddy current inspection data sheet. Refer to Figure 802.
(c)Eddy current inspection evaluation limits.
1The evaluation limit for the webs, web slopes, and bore faces is 500 mV.
Subtask 72-31-45-250-003
(d)Eddy current inspection reject limits.
1The reject limit for the spool webs, web slopes and bore faces is 500 mV or greater, after the evaluation is complete.
(e)All the stages 6-10 spool that are not rejected by the limits in Subtask 72-31-45-250-003 (paragraph 3.D.(2)(d)) are serviceable.
(f)All the web slopes and bore faces (zones 6-10BFF, 6-10FWS, 6-10BAF, and 6-10AWS) of stages 6-10 spool that are rejected by the limits in Subtask 72-31-45-250-003 (paragraph 3.D.(2)(d)) are not serviceable. Refer to Figure 801 for zone definitions.
(g) All the webs (zones 6-10FW and 6-10AW) of stages 6-10 spool that are rejected by the limits in Subtask 72-31-45-250-003 (paragraph 3.D.(2)(d)) , determine if the indication is a defect, or if it can be an repairable surface anomaly. Refer to Figure 801 and Figure 804 and evaluate as follows:
1If it is a defect on the spool web, the part is not serviceable. This condition cannot be repaired. Refer to Figure 804 and as follows:
aIt is not permitted to use polish/blend procedure for tooling marks, nicks, dents or any other type of indications that are not acceptable.
2If the indication on the spool web is an repairable surface anomaly (surface waviness or blended surface), polish/blend the indication. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES), Subtask 70-42-00-350-038 (paragraph C.(3)(e)) and as follows:
aMake and record at least one photograph of the rejected area if not already done.
CAUTION:
MAKE SURE TO REMOVE THE MINIMUM QUANTITY OF PARENT MATERIAL NECESSARY TO REMOVE THE DEFECT.
bPolish/blend to remove the defect, it is permitted to polish/blend 360 degrees if necessary.
cMaximum depth of 0.002 inch (0.05 mm) and minimum radius of 0.5 inch (12.7 mm) are required.
NOTE:
These are only maximum and minimum requirements, the recommendation is to polish a smoother surface to avoid probe uneven contact.
3Do an eddy current inspection of the polish/blended area again. Refer to Subtask 72-31-45-160-002 (paragraph 3.D.) and as follows:
aIf any rejection is found, do paragraph 3.D.(2)(f) again and as follows:
(1)Total cumulative polish/blend must be in the limits of paragraph 3.D.(2)(f)2(c).
4Peen the repaired area of the spool web. Refer to TASK 70-47-01-380-016 (SHOTPEENING) and as follows:
aApply C10-021  plastic tape to the areas you will not peen.
bCoverage must be a minimum of 125 percent.
cAn intensity verification is necessary with a simulative fixture.
dUse C04-166  CCW14 cut wire shot.
eIntensity must be 0.006-0.012N.
fOverspray is permitted.
gRemove all plastic tape.
(h)Make sure that all records that were made during the eddy current inspection are as complete as possible. Permanently keep these records for each spool that was inspected.
* * * FOR ALL
Figure 801   (Sheet 1 ) Eddy Current Scan Plan - HPCR Stage 6-10 Spool
* * * FOR ALL
Figure 801   (Sheet 2 ) Eddy Current Scan Plan - HPCR Stage 6-10 Spool
* * * FOR ALL
Figure 802   Eddy Current Inspection Data Sheet - HPCR Stage 6-10 Spool
* * * FOR ALL
Figure 803   HPCR 6-10 Spool Inspection - Deep Cavity Inner Surfaces of the Spacer Arms
* * * FOR ALL
Figure 804   (Sheet 1 ) HPC Rotor Stage 6-10 Spool Web Eddy Current Inspection Plan
* * * FOR ALL
Figure 804   (Sheet 2 ) HPC Rotor Stage 6-10 Spool Web Eddy Current Inspection Plan
* * * FOR ALL
Figure 805   Deleted
4 . Visual Inspection.
Refer to Figure 806.
Subtask 72-31-45-220-156
A.Visual inspection serviceable limits for wear, fretting, galling, and REPAIR 006 are not applicable to the stage 8 portion of the HPC rotor stage 6-10 spool P/N 2628M56G01   with part serial numbers listed in GEnx-1B SB 72-0484 Table 1. The stage 8 portion is defined as the area between the inertia welds defined as B and C on Figure 801.
Subtask 72-31-45-220-157
B.Visual inspection serviceable limits for nicks, dents, scratches, wear, fretting, galling, and REPAIR 006 are not applicable to the stage 8 portion of the HPC rotor stage 6-10 spool P/N 2628M56G01   with part serial numbers listed in GEnx-1B SB 72-0484 Table 2. The stage 8 portion is defined as the area between the inertia welds defined as B and C on Figure 801.
Subtask 72-31-45-220-045
C.Do an inspection of all surfaces (does not include the interstage seal teeth) for:
(1)Cracks:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
* * * FOR ALL
Figure 806   (Sheet 1 ) Spool - Inspection
* * * FOR ALL
Figure 806   (Sheet 2 ) Spool - Inspection
* * * FOR ALL
Figure 806   (Sheet 3 ) Spool - Inspection
* * * FOR ALL
Figure 806   (Sheet 4 ) Spool - Inspection
Subtask 72-31-45-220-046
(2)Pitting on all areas of the spool (does not include the stage 6 spacer arm, the stage 7 spacer arm, the stage 8 spacer arm, the stage 9 spacer arm, the stage 10 spacer arm, and/or the discourager seal) caused by corrosion (identified by black or green deposits):
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-047
(3)Red deposits or oxidation without pits:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-144
(4)Pitting on the stage 6 spacer arm caused by corrosion (identified by black or green deposits):
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-145
(5)Pitting on the stage 7 spacer arm caused by corrosion (identified by black or green deposits):
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-146
(6)Pitting on the stage 8 spacer arm caused by corrosion (identified by black or green deposits):
Maximum serviceable limit:
Not serviceable.
Repair method (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484):
Replace the spool.
Repair method:
Repair. Refer to TASK 72-31-45-300-807 (72-31-45, REPAIR 006).
Subtask 72-31-45-220-147
(7)Pitting on the stage 9 spacer arm caused by corrosion (identified by black or green deposits):
Maximum serviceable limit:
Not serviceable.
Repair method:
Repair. Refer to TASK 72-31-45-300-807 (72-31-45, REPAIR 006).
Subtask 72-31-45-220-148
(8)Pitting on the stage 10 spacer arm caused by corrosion (identified by black or green deposits):
Maximum serviceable limit:
Not serviceable.
Repair method:
Repair. Refer to TASK 72-31-45-300-807 (72-31-45, REPAIR 006).
Subtask 72-31-45-220-149
(9)Pitting on the discourager seal caused by corrosion (identified by black or green deposits):
Maximum serviceable limit:
Not serviceable.
Repair method:
Repair. Refer to TASK 72-31-45-300-807 (72-31-45, REPAIR 006).
Subtask 72-31-45-220-048
D.Do an inspection of the flange mating faces for:
(1)Pickup and high metal:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-049
(2)Nicks, dents, pits, and scratches:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-050
(3)Fretting, galling, and wear:
Maximum serviceable limit:
Any amount, within limits of TASK 70-33-03-220-006 (SPECIAL INSPECTION FOR SURFACE FRETTING OR GALLING) , after removal of high metal.
Repair method:
Replace the spool.
* * * FOR ALL
Figure 807   (Sheet 1 ) Spool Inspection Areas
* * * FOR ALL
Figure 807   (Sheet 2 ) Spool Inspection Areas
Subtask 72-31-45-220-052
E.Do an inspection of the forward rabbet for:
(1)Nicks, dents, and scratches on parent metal:
Maximum serviceable limit:
Any amount, any length, 0.003 inch (0.08 mm) in depth, after the removal of high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)). Total length for all nicks, dents, and scratches must not be more than 5 percent of the rabbet surface.
Repair method:
Repair. Refer to TASK 72-31-45-300-801 (72-31-45, REPAIR 001).
Subtask 72-31-45-220-053
(2)Fretting, galling, or wear on parent metal:
Maximum serviceable limit:
Any amount, within the limits of TASK 70-33-03-220-006 (SPECIAL INSPECTION FOR SURFACE FRETTING OR GALLING) .
Repair method:
Repair. Refer to TASK 72-31-45-300-801 (72-31-45, REPAIR 001).
Subtask 72-31-45-220-054
(3)Corrosion pits on parent metal:
Maximum serviceable limit:
Not serviceable.
Repair method:
Repair. Refer to TASK 72-31-45-300-801 (72-31-45, REPAIR 001).
Subtask 72-31-45-220-103
(4)Chipped or missing HVOF or APS coating:
Maximum serviceable limit:
Any amount, any length, 0.003 inch (0.08 mm). Total length for all chipped or missing coating must not be more than 5 percent of the rabbet surface.
Repair method:
Repair. Refer to TASK 72-31-45-300-801 (72-31-45, REPAIR 001).
NOTE:
Forward Rabbet Diameter can possibly have APS or HVOF Inco 218 thermal spray coating.
Subtask 72-31-45-220-104
F.Do an inspection of the aft rabbet for:
(1)Nicks, dents, and scratches:
Maximum serviceable limit:
Any amount, any length, 0.003 inch (0.08 mm) in depth, after the removal of high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)). Total length for all nicks, dents, and scratches must not be more than 5 percent of the rabbet surface.
Repair method:
Repair. Refer to TASK 72-31-45-300-803 (72-31-45, REPAIR 003).
Subtask 72-31-45-220-105
(2)Fretting, galling, or wear:
Maximum serviceable limit:
Any amount, within the limits of TASK 70-33-03-220-006 (SPECIAL INSPECTION FOR SURFACE FRETTING OR GALLING) .
Repair method:
Repair. Refer to TASK 72-31-45-300-803 (72-31-45, REPAIR 003).
Subtask 72-31-45-220-106
(3)Corrosion pits:
Maximum serviceable limit:
Not serviceable.
Repair method:
Repair. Refer to TASK 72-31-45-300-803 (72-31-45, REPAIR 003).
NOTE:
There is no HVOF or APS coating on the aft rabbet.
Subtask 72-31-45-220-055
G.Do an inspection of the interstage seal teeth for:
(1)Cracks:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-056
(2)Chipped or missing coating after you apply the coating again:
Maximum serviceable limit:
Any amount, 0.30 inch (7.6 mm) in length, if apart by a minimum of 0.50 inch (12.7 mm). Total length on each seal tooth must not be more than 2.00 inches (50.8 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-802 (72-31-45, REPAIR 002) .
Subtask 72-31-45-220-099
(3)Nicks, dents, and scratches on seal teeth diameter FU only:
Maximum serviceable limit:
Any amount, 0.003 inch (0.08 mm) in depth, after the removal of high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)).
Maximum repairable limit:
Any amount that can be removed by blending inward on the seal tip to any between 0.032 to 0.040 inch (0.81 to 1.02 mm) in depth, and 0.80 inch (20.32 mm) in length, or any up to 0.032 inch (0.81 mm) maximum in depth, and 1.00 inch (25.40 mm) in length, if the limits in the notes are kept.
Repair method:
•
Remove coating. Refer to Repair.
•
Manually blend. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES), Subtask 70-42-00-350-038 (paragraph C.(3)(e)). Keep a minimum blend radius of 2.00 inches (50.8 mm)
•
Swab etch the blended area. Refer to TASK 70-24-00-110-033 Class C (ETCHING PROCEDURES FOR FLUORESCENT-PENETRANT INSPECTION).
•
Spot-fluorescent-penetrant inspect the blended areas. Refer to TASK 70-32-03-230-002 Class G (SPOT-FLUORESCENT-PENETRANT INSPECTION).
•
Replace the coating. Refer to Repair.
NOTE:
Maximum cumulative length of blends on any of the tooth must not be more than 5.00 inches (127.0 mm).
NOTE:
Total cumulative length of all blends between any stage must not be more than 10.00 inches (254.0 mm).
NOTE:
Measurement must be made at the OD of the serration sections.
NOTE:
Minimum distance between blends must not be less than 1.00 inch (25.4 mm).
NOTE:
Blends on any stage of seals cannot be in line axially across more than 2 serrations in a row.
Subtask 72-31-45-220-057
(4)Nicks, dents, and scratches on seal teeth diameter DH, diameter DE, diameter KG, and diameter KN:
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484 Table 2):
Diameter DE only, not serviceable.
Maximum serviceable limit:
Any amount, 0.003 inch (0.08 mm) in depth, after the removal of high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)).
Maximum repairable limit:
Any amount that can be removed by blending inward on the seal tip to a maximum of 0.030 inch (0.77 mm) in depth and 0.800 inch (20.32 mm) in width, if the limits in the notes are kept.
Repair method:
•
Remove coating. Refer to Repair.
•
Manually blend. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES), Subtask 70-42-00-350-038 (paragraph C.(3)(e)). Keep a minimum blend radius of 2.00 inches (50.8 mm).
•
Swab etch the blended area. Refer to TASK 70-24-00-110-033 (ETCHING PROCEDURES FOR FLUORESCENT-PENETRANT INSPECTION), Class C.
•
Do a spot-fluorescent-penetrant inspection of the blended areas. Refer to TASK 70-32-03-230-002 (SPOT-FLUORESCENT-PENETRANT INSPECTION), Class G.
•
Replace the coating. Refer to Repair.
NOTE:
Maximum cumulative length of blends on any of the tooth must not be more than 6.700 inches (170.18 mm).
NOTE:
Total cumulative length of all blends between any stage must not be more than 13.400 inches (340.36 mm).
NOTE:
Measurement must be made at the OD of the serration sections.
NOTE:
Minimum distance between blends must not be less than 1.00 inch (25.4 mm).
NOTE:
Blends on any stage of the seals cannot be in line axially across more than 2 serrations in a row.
Subtask 72-31-45-220-058
(5)Seal tip wear into the parent metal:
Maximum serviceable limit:
Any amount, if OD dimensional limits are within Subtask 72-31-45-220-086 (paragraph 5.C.) . Discoloration of the parent metal is not permitted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-059
(6)Seal face wear into the parent metal:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-060
(7)Pits:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-110
H.Do an inspection of the dovetail forward and aft rail for:
(1)Nicks, dents, and scratches on the stage 6, 7, and 8 dovetail rails:
Maximum serviceable limit:
Not serviceable.
Maximum repairable limit:
One location for each stage, 0.020 inch (0.51 mm) in depth.
Repair method:
Blend. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) . Only one blend repair for each stage can be applied but it can be located on any circumferential location of the forward and aft rail OD. Final blend depth must not be more than 0.020 inch (0.51 mm). Keep a minimum blend radius of 1.00 inch (25.4 mm).
Subtask 72-31-45-220-111
(2)Nicks, dents, and scratches on the stage 9 and 10 dovetail rail:
Maximum serviceable limit:
Any amount, 0.003 inch (0.07 mm) in depth.
Maximum repairable limit:
One location for each stage, 0.020 inch (0.51 mm) in depth.
Repair method:
Blend. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)). Only one blend repair can be applied for each stage but it can be located on any circumferential location of the forward and aft rail OD. Final blend depth must not be more than 0.020 inch (0.51 mm). Keep a minimum blend radius of 1.00 inch (25.4 mm).
Subtask 72-31-45-220-061
I.Do an inspection of the dovetail pressure surfaces and fillets for:
(1)Fretting or galling:
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484):
Stage 8, not serviceable.
Maximum serviceable limit:
Any amount, 0.002 inch (0.05 mm) in depth, and within the limits of TASK 70-33-03-220-006 (SPECIAL INSPECTION FOR SURFACE FRETTING OR GALLING) .
Repair method:
Replace the spool.
Subtask 72-31-45-220-062
(2)Nicks, dents, and scratches in fillet:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-063
(3)Nicks, dents, and scratches on the pressure face:
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484 Table 2):
Stage 8, not serviceable.
Maximum serviceable limit:
Any amount, 0.003 inch (0.08 mm) in depth, after the removal of high metal on the pressure surfaces. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)).
Repair method:
Replace the spool.
Subtask 72-31-45-220-064
(4)Pits:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-065
J.Do an inspection of the dovetail slot bottoms for:
(1)Nicks and dents:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-066
(2)Circumferential and axial scratches:
Maximum serviceable limit:
Not serviceable.
Maximum repairable limit:
Any amount, 0.005 inch (0.13 mm) in depth after blending, if they are a minimum of 1.00 inch (25.4 mm) apart after blending. Blend radius must be 0.25 inch (6.4 mm). Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)).
Repair method:
Manually blend. Blend radius must be 0.25 inch (6.4 mm). Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)).
Subtask 72-31-45-220-067
(3)Fretting marks from blade lock set screw:
Maximum serviceable limit:
Not serviceable.
Maximum repairable limit:
Any amount, 0.079 inch (2.01 mm) in width, 0.003 inch (0.07 mm) in depth on stage 8. Any amount, 0.079 inch (2.01 mm) in width, 0.004 inch (0.10 mm) in depth on stage 10. Any amount, 0.079 inch (2.01 mm) in width, 0.0015 inch (0.038 mm) in depth on stages 6,7, and 9.
Repair method:
Polish to remove high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038 (paragraph C.(3)(e)).
Subtask 72-31-45-220-068
K.Do an inspection of the flange boltholes for:
(1)Nicks, dents, and scratches on the ID of bolthole diameters LT and LU:
Maximum serviceable limit:
Not serviceable.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-805 (72-31-45, REPAIR 004) .
Subtask 72-31-45-220-069
(2)Pits:
Maximum serviceable limit:
Not serviceable.
Repair method:
Repair. Refer to TASK 72-31-45-300-805 (72-31-45, REPAIR 004) .
Subtask 72-31-45-220-070
(3)Nicks, dents, and scratches on the 45 degree chamfer:
Maximum serviceable limit:
Not serviceable.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-805 (72-31-45, REPAIR 004) .
Subtask 72-31-45-220-071
(4)Pits on the 45 degree chamfer:
Maximum serviceable limit:
Not serviceable.
Repair method:
Repair. Refer to TASK 72-31-45-300-805 (72-31-45, REPAIR 004) .
Subtask 72-31-45-220-072
(5)Fretting, galling, or wear on boltholes:
Maximum serviceable limit:
Any amount within TASK 70-33-03-220-006 (SPECIAL INSPECTION FOR SURFACE FRETTING OR GALLING) .
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-805 (72-31-45, REPAIR 004) .
L.Do an inspection of stage 6-10 spool disk for:
Subtask 72-31-45-220-150
(1)For part numbers 2439M35G01, 2439M35G02, 2445M40G02, and 2610M90G01:
(a)Scratches on web, hub, web slope, bore surfaces (does not include bore edge corner radius), and stage 7 disk hook (does not include all corner radii, refer to Figure 815):
Maximum serviceable limit:
Any amount if within the limits provided in Subtask 72-21-45-220-153 (paragraph 10.A.) Table 1 and Figure 809. If necessary, remove high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038, (paragraph 4.C.(e)).
Repair method:
Replace the spool.
(b)Nicks and dents on web, hub, web slope, bore surfaces (does not include bore edge corner radius), and stage 7 disk hook (does not include all corner radii, refer to Figure 815):
Maximum serviceable limit:
Any amount if within the limits provided in Subtask 72-21-45-220-153 (paragraph 10.B.) Table 2 and Figure 810. If necessary, remove high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038, (paragraph 4.C.(e)).
Repair method:
Replace the spool.
Subtask 72-31-45-220-151
(2)For part numbers 2357M30G02:
(a)Scratches on web, hub, web slope, bore surfaces (does not include bore edge corner radius), and stage 7 disk hook (does not include all corner radii, refer to Figure 815):
Maximum serviceable limit:
Any amount if within the limits provided in Subtask 72-21-45-220-153 (paragraph 10.C.) Table 3 and Figure 811. If necessary, remove high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038, (paragraph 4.C.(e)).
Repair method:
Replace the spool.
(b)Nicks and dents on web, hub, web slope, bore surfaces (does not include bore edge corner radius), and stage 7 disk hook (does not include all corner radii, refer to Figure 815):
Maximum serviceable limit:
Any amount if within the limits provided in Subtask 72-21-45-220-153 (paragraph 10.D.) Table 4 and Figure 812. If necessary, remove the high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038, (paragraph 4.C.(e)).
Repair method:
Replace the spool.
Subtask 72-31-45-220-152
(3)For part numbers 2628M56G01   and 2628M56G02   :
(a)Scratches on web, hub, web slope, bore surfaces (bore edge radius included if specified elsewhere):
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484 Table 2):
Stage 8, not serviceable.
Maximum serviceable limit:
Any amount if within the limits provided in Subtask 72-21-45-220-153 (paragraph 10.E.) Table 5 and Figure 813. If necessary, remove the high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038, (paragraph 4.C.(e)).
Repair method:
Replace the spool.
(b)Nicks and dents on web, hub, web slope, bore surfaces (bore edge radius included if specified elsewhere):
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484 Table 2):
Stage 8, not serviceable.
Maximum serviceable limit:
Any amount if within the limits provided in Subtask 72-21-45-220-153 (paragraph 10.F.) Table 6 and Figure 814. If necessary, remove high metal. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) , Subtask 70-42-00-350-038, (paragraph 4.C.(e)).
Repair method:
Replace the spool.
Subtask 72-31-45-220-073
M.Do an inspection of the disk bores for:
(1)Nicks, dents, and scratches (does not include stage 7 disk hook area). Refer to Figure 815.
Maximum serviceable limit:
Not serviceable. Unless specified elsewhere.
Maximum repairable limit:
Any amount, 0.005 inch (0.12 mm) in depth, after blending, if they are a minimum of 1.00 inch (25.4 mm) apart. Blend radius must be 2.00 inches (50.8 mm) or more.
Repair method:
Manually blend. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) .
Subtask 72-31-45-220-074
(2)Damage in the edge radius. Refer to Figure 815.
Maximum serviceable limit:
Not serviceable. Unless specified elsewhere.
Maximum repairable limit:
Any amount, if the damage can be removed by a radius blend, not more than 0.005 inch (0.12 mm) in depth with a minimum blend radius of 6.00 inches (152.4 mm).
Repair method:
Manually blend. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) .
Subtask 72-31-45-220-112
N.Inspect the wire seal slots for:
(1)Wear on the wire seal slot surfaces at the stage 6 (forward slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.005 inch (0.12 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-804 (72-31-45, REPAIR 005) and/or TASK 72-31-45-300-806 (72-31-45, REPAIR 007) .
Subtask 72-31-45-220-113
(2)Wear on the wire seal slot surfaces at the stage 6 (forward slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.004 inch (0.10 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-114
(3)Wear on the wire seal slot surfaces at the stage 6 (aft slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.005 inch (0.12 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-115
(4)Wear on the wire seal slot surfaces at the stage 6 (aft slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the loading and locking slots
• Any amount, 0.006 inch (0.15 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-804 (72-31-45, REPAIR 005) and/or TASK 72-31-45-300-806 (72-31-45, REPAIR 007) .
Subtask 72-31-45-220-116
(5)Wear on the wire seal slot surfaces at the stage 7 (forward slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the loading and locking slots
• Any amount, 0.002 inch (0.05 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-804 (72-31-45, REPAIR 005) and/or TASK 72-31-45-300-806 (72-31-45, REPAIR 007) .
Subtask 72-31-45-220-117
(6)Wear on the wire seal slot surfaces at the stage 7 (forward slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.002 inch (0.05 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-118
(7)Wear on the wire seal slot surfaces at the stage 7 (aft slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.001 inch (0.02 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-119
(8)Wear on the wire seal slot surfaces at the stage 7 (aft slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.002 inch (0.05 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-804 (72-31-45, REPAIR 005) and/or TASK 72-31-45-300-806 (72-31-45, REPAIR 007) .
Subtask 72-31-45-220-120
(9)Wear on the wire seal slot surfaces at the stage 8 (forward slot and forward face):
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484):
Not serviceable.
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.001 inch (0.02 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-804 (72-31-45, REPAIR 005) and/or TASK 72-31-45-300-806 (72-31-45, REPAIR 007) .
Subtask 72-31-45-220-121
(10)Wear on the wire seal slot surfaces at the stage 8 (forward slot and aft face):
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484):
Not serviceable.
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.001 inch (0.02 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-122
(11)Wear on the wire seal slot surfaces at the stage 8 (aft slot and forward face):
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484):
Not serviceable.
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.002 inch (0.05 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-123
(12)Wear on the wire seal slot surfaces at the stage 8 (aft slot and aft face):
Maximum serviceable limit (for stage 6-10 spool part number 2628M56G01 with part serial numbers listed in GEnx-1B SB 72-0484):
Not serviceable.
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.002 inch (0.05 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-804 (72-31-45, REPAIR 005) and/or TASK 72-31-45-300-806 (72-31-45, REPAIR 007) .
Subtask 72-31-45-220-124
(13)Wear on the wire seal slot surfaces at the stage 9 (forward slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.003 inch (0.07 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-806 (72-31-45, REPAIR 007).
Subtask 72-31-45-220-125
(14)Wear on the wire seal slot surfaces at the stage 9 (forward slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, of 0.003 inch (0.07 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-126
(15)Wear on the wire seal slot surfaces at the stage 9 (aft slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.003 inch (0.07 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
NOTE: (HES) Revision: Any amount, 0.001 inch in depth, at the slot surfaces adjacent to loading and locking slots. Refer to CTP-NX-25-0003.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-127
(16)Wear on the wire seal slot surfaces at the stage 9 (aft slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.002 inch (0.05 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-806 (72-31-45, REPAIR 007).
Subtask 72-31-45-220-128
(17)Wear on the wire seal slot surfaces at the stage 10 (forward slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.003 inch (0.07 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-806 (72-31-45, REPAIR 007).
Subtask 72-31-45-220-129
(18)Wear on the wire seal slot surfaces at the stage 10 (forward slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.003 inch (0.07 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-130
(19)Wear on the wire seal slot surfaces at the stage 10 (aft slot and forward face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.003 inch (0.07 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
NOTE: (HES) Revision: Any amount, 0.001 inch in depth, at the slot surfaces adjacent to loading and locking slots. Refer to CTP-NX-25-0003.
Maximum repairable limit:
Deleted.
Repair method:
Replace the spool.
Subtask 72-31-45-220-131
(20)Wear on the wire seal slot surfaces at the stage 10 (aft slot and aft face):
Maximum serviceable limit:
• Any amount, 0.012 inch (0.30 mm) in depth, at the slot surfaces minimum 2.00 inches (50.8 mm) away from the edge of the loading and locking slots
• Any amount, 0.003 inch (0.07 mm) in depth, at the slot surfaces adjacent to loading and locking slots.
Maximum repairable limit:
Deleted.
Repair method:
Repair. Refer to TASK 72-31-45-300-806 (72-31-45, REPAIR 007).
Subtask 72-31-45-220-075
O.Do an inspection of other surfaces for:
(1)Nicks and scratches:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-076
(2)Dents:
Maximum serviceable limit:
Not serviceable.
Repair method:
Replace the spool.
Subtask 72-31-45-220-077
P.Do an inspection of all areas for:
(1)Discoloration:
Maximum serviceable limit:
Any amount.
Repair method:
Replace the spool.
5 . Application of Coatings
Subtask 72-31-45-350-006
A.Apply the coating to the spool. Refer to Repair.
6 . Dimensional Inspection.
Refer to Figure 807.
Subtask 72-31-45-220-078
A.Measure each diameter at 10 equally-spaced locations. Calculate the average diameter dimension. Compare the average diameter dimension to the dimension given in the dimensional inspection.
NOTE:
You must measure diameter W and EB each time there is an actual overspeed, or if you think an overspeed condition occurred. Refer to Subtask 72-31-45-220-092 (paragraph 7.B.). Contact GE for disposition of parts.
Subtask 72-31-45-220-079
B.Do an inspection of the diameters as follows:
(1)Diameter B:
Minimum serviceable limit:
15.204 inches (386.18 mm).
Maximum serviceable limit:
15.208 inches (386.28 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-803 (72-31-45, REPAIR 003).
Subtask 72-31-45-220-098
(2)Diameter H:
Minimum serviceable limit:
6.636 inches (168.55 mm).
Maximum serviceable limit:
6.640 inches (168.66 mm).
Repair method:
Replace the spool.
Subtask 72-31-45-220-084
(3)Diameter M:
Minimum serviceable limit:
21.088 inches (535.64 mm).
Maximum serviceable limit:
21.092 inches (535.74 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-801 (72-31-45, REPAIR 001).
Subtask 72-31-45-220-086
C.Do an inspection of the interstage seal teeth diameters before you apply the coating for:
(1)Diameter FU:
Minimum serviceable limit:
21.825 inches (554.35 mm).
Maximum serviceable limit:
21.849 inches (554.96 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-802 (72-31-45, REPAIR 002) .
Subtask 72-31-45-220-087
(2)Diameter DH:
Minimum serviceable limit:
22.344 inches (567.54 mm).
Maximum serviceable limit:
22.368 inches (568.15 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-802 (72-31-45, REPAIR 002) .
Subtask 72-31-45-220-088
(3)Diameter DE:
Minimum serviceable limit:
22.470 inches (570.74 mm).
Maximum serviceable limit:
22.494 inches (571.35 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-802 (72-31-45, REPAIR 002) .
Subtask 72-31-45-220-089
(4)Diameter KG:
Minimum serviceable limit:
22.530 inches (572.26 mm).
Maximum serviceable limit:
22.554 inches (572.87 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-802 (72-31-45, REPAIR 002) .
Subtask 72-31-45-220-090
(5)Diameter KN:
Minimum serviceable limit:
22.530 inches (572.26 mm).
Maximum serviceable limit:
22.554 inches (572.87 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-802 (72-31-45, REPAIR 002) .
7 . Special Dimensional Inspection.
Refer to Figure 807.
Subtask 72-31-45-220-091
A.Do an inspection of diameter W and diameter EB, if an N2 overspeed has occurred, or if you think an overspeed occurred. Contact GE for the initial length of diameter W and diameter EB.
Subtask 72-31-45-220-092
B.Diameter W and diameter EB:
Maximum serviceable limit:
Initial length, plus 0.008 inch (0.20 mm).
Repair method:
Contact GE for disposition of parts.
8 . Bolthole Inspection Procedure.
Refer to Figure 807.
Subtask 72-31-45-350-003
A.Deleted.
Subtask 72-31-45-350-004
A.A.Deleted.
Subtask 72-31-45-220-095
B.Measure the boltholes as follows:
(1)Diameter LT:
Minimum serviceable limit:
0.329 inch (8.36 mm).
Maximum serviceable limit:
0.337 inch (8.55 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-805 (72-31-45, REPAIR 004) .
(2)Diameter LU:
Minimum serviceable limit:
0.4560 inch (11.583 mm).
Maximum serviceable limit:
0.4640 inch (11.785 mm).
Repair method:
Repair. Refer to TASK 72-31-45-300-805 (72-31-45, REPAIR 004) .
9 . Post Inspection Procedure.
Subtask 72-31-45-380-004
A.Shotpeen the rim region and dovetail post surfaces of the HPC rotor 6-10 spool. Refer to TASK 70-47-01-380-016 (SHOTPEENING), Figure 808, and do as follows:
(1)Apply a mask to the coated areas (rabbets and seal wire grooves at which thermal spray repair. Refer to TASK 72-31-45-300-804 (72-31-45, REPAIR 005) has been completed).
(2)Use C04-166  CCW14 cut wire shot.
(3)Shotpeen to an intensity of 6-12N.
(4)A minimum coverage of 125 percent is necessary.
(5)Verification of intensity is necessary on the peened areas. Use C10-205  test strips.
(6)Overspray is permitted.
Subtask 72-31-45-350-015
B.Re-apply the coating on the interstage seal teeth. Refer to TASK 72-31-45-300-802 (72-31-45, REPAIR 002).
10 . Tables.
Subtask 72-31-45-220-153
NOTE:
(HES) New Limit added. Refer to CTP-NX-25–0003.
A.Table 1.
 
Stage 6-10 disk scratch serviceable limits for part numbers 2439M35G01, 2439M35G02, 2445M40G02, and 2610M90G01
 
A
B
C
D
E
 
Zone
Radius (inches) as distance from center line
Axial distance from Face Z (applicable for stage 7 hook areas, refer to Figure 809)
Max serviceable depth (inches)
Max allowable length (inches)
 
Stage 6
 
A
9.729 - 5.485
N/A
0.0005
N/A
 
B
5.485 - 4.154
0.001
 
C
4.154 - 3.623
0.0005
 
D
5.515 - 4.649
0.001
 
E
4.649 - 3.623
0.0005
 
Stage 7
 
A
N/A
up to 0.52
0.0025
N/A
 
B
up to 0.88
0.0015
 
C
3.7 - 5.8
N/A
0.001
 
D
5.3 - 6.3
0.0015
 
E
6.3 - 6.8
0.001
 
F
6.8 - 10.3
0.0005
 
G
8.3 - 10.3
0.0015
 
H
5.8 - 8.3
0.0005
 
Face Z
N/A
Forward face
0.0025
 
Stage 8 for part numbers 2439M35G01, 2439M35G02, and 2610M90G01
 
A
10.551 - 8.0
N/A
0.005
Refer to Table 7
 
B
8.0 - 6.27
0.004
 
C
6.27 - 5.7
0.003
 
D
5.7 - 4.02
0.005
 
E
Bore ID (does not include bore edge radius)
0.004
 
F
10.551 - 4.02
0.005
 
Stage 8 for part number 2445M40G02
 
A
10.55 - 10.23
N/A
0.005
N/A
 
B
10.23 - 10.05
0.003
 
C
10.05 - 8.3
0.002
 
D
8.3 - 5.63
0.001
 
E
5.63 - 4.83
0.004
 
F
4.83 - 4.55
0.003
 
G
4.55 - 3.98
0.002
 
H
Bore ID (does not include bore edge radius)
0.001
 
I
4.36 - 3.98
0.002
 
J
4.86 - 4.36
0.003
 
K
5.38 - 4.86
0.005
 
L
5.71 - 5.38
0.004
 
M
10.046 - 5.713
0.002
 
N
10.2 - 10.046
0.003
 
O
10.55 - 10.20
0.004
 
Stage 9
 
A
10.5 - 8.3
N/A
0.005
Refer to Table 7
 
B
8.3 - 5.97
0.004
 
C
5.97 - 4.21
0.005
 
D
4.21 (fwd) 4.21 (aft) includes bore ID (does not include bore edge radius)
0.004
 
E
5.97 - 4.21
0.005
 
F
8.3 - 5.97
0.004
 
G
10.5 -8.3
0.005
 
Stage 10
 
A
10.57 - 10.019
N/A
0.005
Refer to Table 7
 
B
10.019 - 9.87
0.004
 
C
9.87 -7.82
0.005
 
D
7.82 - 6.524
0.004
 
E
6.524 - 4.641
0.005
 
F
4.641 (fwd) - 4.641 (aft) includes bore ID (does not include bore edge radius)
0.004
 
G
6.544 - 4.641
0.005
 
H
7.473 - 6.544
0.004
 
I
10.57 - 7.473
0.005
NOTE:
For the border values in ranges given in column B (radius distance) use lower depth value from column D.
NOTE:
Use applicable radius (bore ID or end of bore edge radius) to calculate exact distance from engine center line to indication found. Refer to Figure 815 and Figure 816.
B.Table 2.
 
Stage 6-10 disk nicks/dents serviceable limits for part numbers 2439M35G01, 2439M35G02, 2445M40G02, and 2610M90G01
 
A
B
C
D
 
Zone
Radius (inches) as distance from center line
Axial distance from Face Z (applicable for stage 7 hook areas, refer to Figure 810)
Max serviceable depth (inches)
 
Stage 6
 
A
9.729 - 5.485
N/A
0.001
 
B
5.485 - 4.154
0.0015
 
C
4.154 - 3.623
0.001
 
D
4.154 - 3.623
0.001
 
E
5.485 - 4.154
0.0015
 
F
9.729 - 5.485
0.001
 
Stage 7
 
A
N/A
up to 0.64
0.003
 
B
up to 0.5
0.004
 
C
0.64 - 0.88
0.0025
 
D
0.88 - 3.755 (radius) (does not include corner radius)
0.002
 
E
6.8 - 10.3
N/A
0.001
 
F
6.3 - 6.8
0.002
 
G
5.3 - 6.3
0.0025
 
H
4.03 - 5.3
0.001
 
I
3.7 - 5.8
0.0025
 
J
5.8 - 7.3
0.001
 
K
7.3 - 8.3
0.0015
 
L
8.3 - 9.3
0.002
 
M
9.3 - 10.3
0.0025
 
Face Z
N/A
Forward face
0.005
 
Stage 8 for part numbers 2439M35G01, 2439M35G02, and 2610M90G01
 
A
10.551 - 7.1
N/A
0.005
 
B
7.1 - 5.74
0.004
 
C
5.74 - 4.8
0.003
 
D
4.8 - 4.02
0.005
 
E
Bore ID (does not include bore edge radius)
0.004
 
F
10.551 - 4.02
0.005
 
Stage 8 for part number 2445M40G02
 
A
10.55 - 10.18
N/A
0.005
 
B
10.18 - 8.3
0.003
 
C
8.3 - 6.36
0.002
 
D
6.36 - 5.63
0.001
 
E
5.63 - 4.85
0.005
 
F
4.85 - 4.54
0.004
 
G
4.54 - 3.98
0.003
 
H
Bore ID (does not include bore edge radius)
0.002
 
I
4.366 - 3.98
0.003
 
J
4.659 - 4.366
0.004
 
K
5.8 - 4.659
0.005
 
L
10.046 - 5.8
0.003
 
M
10.23 - 10.046
0.004
 
N
10.55 - 10.23
0.005
 
Stage 9
 
A
10.5 - 7.45
N/A
0.005
 
B
7.45 - 5.97
0.004
 
C
5.97 - 5.14
0.005
 
D
5.14 - 4.15
0.005
 
E
4.15 (fwd) - 4.15 (aft) includes bore ID (does not include bore edge radius)
0.004
 
F
5.14 - 4.15
0.005
 
G
5.97 - 5.14
0.005
 
H
7.45 - 5.97
0.004
 
I
10.5 - 7.45
0.005
 
Stage 10
 
A
10.57 - 7.335
N/A
0.005
 
B
7.335 - 6.524
0.004
 
C
6.524 - 4.588
0.005
 
D
4.588 (fwd hub) - 4.537 (aft hub), includes bore ID (does not include bore edge radius)
0.004
 
E
6.544 - 4.537
0.005
 
F
7.097 - 6.544
0.004
 
G
10.57 - 7.097
0.005
NOTE:
For the border values in ranges given in column B (radius distance) use lower depth value from column D.
NOTE:
Use applicable radius (bore ID or end of bore edge radius) to calculate exact distance from engine center line to indication found. Refer to Figure 815 and Figure 816.
C.Table 3.
 
Stage 6-10 disk scratch serviceable limits for part numbers 2357M30G02
 
A
B
C
D
 
Zone
Radius (inches) as distance from center line
Max serviceable depth (inches)
Max allowable length (inches)
 
Stage 6
 
A
9.16 - 5.51
0.0005
N/A
 
B
5.51 - 4.64
0.0015
 
C
4.64 - 4.34
0.001
 
D
4.34 (fwd) - 4.34 (aft) include bore ID (does not include bore edge radius)
0.0005
 
E
4.64 - 4.34
0.001
 
F
5.51 - 4.64
0.0015
 
G
8.65 - 5.51
0.0005
 
Stage 7
 
A
10.31 - 7.8
0.0015
N/A
 
B
7.8 - 6.78
0.001
 
C
5.81 - 4.88
0.003
 
D
6.29 - 5.24
0.0025
 
E
6.9 - 10.3
0.0005
 
Face Z
N/A
0.003
 
Stage 8
 
A
10.11 - 8.84
0.0015
N/A
 
B
8.84 - 6.87
0.001
 
C
6.87 - 5.60
0.0005
 
D
5.602 - 4.80
0.001
 
E
4.08 bore ID includes bore ID (does not include bore edge radius)
0.0005
 
F
4.26 - to bore ID
0.0005
 
G
4.75 - 4.26
0.0015
 
H
8.84 - 4.75
0.001
 
I
10.11 - 8.84
0.0015
 
J
10.55 - 10.11
0.003
 
Stage 9
 
A
10.516 - 8.145
0.005
Refer to Table 7
 
B
8.145 - 5.95
0.004
 
C
5.95 - 5.11
0.005
 
D
5.11 - 4.08
0.005
 
E
4.08 (forward) - 4.08 (aft) includes bore ID (does not include bore edge radius)
0.004
 
F
5.11 - 4.08
0.005
 
G
5.95 - 5.11
0.005
 
H
8.145 - 5.95
0.004
 
I
10.516 - 8.145
0.005
 
Stage 10
 
A
10.61 - 10.02
0.005
Refer to Table 7
 
B
10.02 - 9.57
0.004
 
C
9.57 - 8.28
0.005
 
D
8.28 - 6.66
0.004
 
E
6.66 - 5.66
0.005
NOTE:
New limit 0.004
 
F
5.66 - 4.48
0.005
 
G
4.48 (forward) to 4.48 (aft) include bore ID (does not include bore edge radius)
0.004
 
H
5.66 - 4.48
0.005
 
I
6.48 - 5.66
0.005
 
J
8.11 - 6.48
0.004
 
K
10.61 - 8.11
0.005
NOTE:
For the border values in ranges given in column B (radius distance) use lower depth value from column D.
NOTE:
Use applicable radius (bore ID or end of bore edge radius) to calculate exact distance from engine center line to indication found. Refer to Figure 815 and Figure 817.
D.Table 4.
 
Stage 6-10 disk nicks/dents serviceable limits for part numbers 2357M30G02
 
A
B
C
D
 
Zone
Radius (inches) as distance from center line
Axial distance from Face Z (applicable for stage 7 hook areas, refer to Figure 812)
Max serviceable depth (inches)
 
Stage 6
 
A
9.65 - 5.51
N/A
0.001
 
B
5.51 - 4.64
0.002
 
C
4.64 - 4.01
0.0015
 
D
4.01 (fwd) - 4.01 (aft) includes bore ID (does not include bore edge radius)
0.001
 
E
4.64 - 4.01
0.0015
 
F
5.51 - 4.64
0.002
 
G
9.65 - 5.51
0.001
 
Stage 7
 
A
10.296 - 8.81
N/A
0.0025
 
B
8.81 - 7.298
0.002
 
C
7.298 - 6.779
0.0015
 
D
6.779 - 5.817
0.001
 
E
5.817 - 4.886
0.003
 
F
10.3 - 9.784
0.0015
 
G
9.784 - 6.292
0.001
 
H
6.292 - 5.243
0.003
 
I
3.464 - 3.319
Aft face of S7 hook
0.0005
 
J
N/A
0.342 - 0.691
0.0005
 
K
N/A
0.234 - 0.48
0.0005
 
Face Z
3.525 - 3.319
Forward face
0.0005
 
Stage 8
 
A
10.55 - 10.23
N/A
0.004
 
B
10.23 - 8.29
0.002
 
C
8.29 - 4.75
0.0015
 
D
4.75 - 4.547
0.0015
 
E
4.547 - 3.975
0.001
 
F
3.975 (fwd) - 4.268 (aft) includes bore ID (does not include bore edge radius)
0.0015
 
G
4.75 - 4.268
0.002
 
H
5.1 - 4.75
0.002
 
I
8.29 - 5.1
0.0015
 
J
9.87 - 8.29
0.002
 
K
10.33 - 9.87
0.003
 
L
10.55 - 10.33
0.004
 
Stage 9
 
A
10.516 - 7.292
N/A
0.005
 
B
7.292 - 5.11
0.004
 
C
5.11 - 4.02
0.005
 
D
4.02 (fwd) - 4.02 (aft) includes bore ID (does not include bore edge radius)
0.004
 
E
5.67 - 4.02
0.005
 
F
7.292 - 5.67
0.004
 
G
10.516 - 7.292
0.005
 
Stage 10
 
A
10.61 - 7.47
N/A
0.005
 
B
7.47 - 6.48
0.004
 
C
6.48 - 4.44
0.005
 
D
Bore ID (does not include bore edge radius)
0.004
 
E
6.48 - 4.44
0.005
 
F
7.47 - 6.48
0.004
 
G
10.61 - 7.47
0.005
NOTE:
For the border values in ranges given in column B (radius distance) use lower depth value from column D.
NOTE:
Use applicable radius (bore ID or end of bore edge radius) to calculate exact distance from engine center line to indication found. Refer to Figure 815 and Figure 817.
E.Table 5.
 
Stages 6, 7, and 8 disk scratch serviceable limits for part numbers 2628M56G01 and 2628M56G02
 
A
B
C
D
E
 
Zone
Radius (inches) as distance from center line
Axial distance from Face Z (Applicable for stage 7 hook areas, refer to Figure 813)
Max serviceable depth (inches)
Max allowable length (inches)
 
Stage 6
 
A
5.48 - 6.42
N/A
0.0005
N/A
 
B
4.60 - 5.48
0.0015
 
C
4.15 - 4.60
0.001
 
D
3.66 - 4.15
0.0005
 
E
Bore ID (does not include bore edge radius)
0.0005
 
F
3.66 - 3.90
0.0005
 
G
3.90 - 4.46
0.001
 
H
4.46 - 5.60
0.0015
 
I
5.60 - 6.42
0.0005
 
Stage 7
 
A
6.28 - 7.034
N/A
0.0015
N/A
 
B
5.50 - 6.28
0.002
 
C
4.92 - 5.50
0.0015
 
D
4.363 - 4.92
0.001
 
E
4.035 - 4.363 (does not include bore edge radius)
0.0005
 
F
3.962 - 4.962 (does not include bore edge radius)
0.003
 
FR
N/A
Radius
0.001
 
G
4.962 - 5.368
N/A
0.0035
 
H
5.368 - 5.82
0.0033
 
I
5.82 - 6.393
0.002
NOTE:
New limit 0.001
 
J
6.393 - 7.021
0.001
 
K
N/A
Radius
0.003
 
L
Radius
0.001
 
M
0.225 to 0.750
0.002
 
N
up to 0.400
0.003
 
Face Z
Forward face
0.005
 
Stage 8
 
A4
10.2 - 10.56
N/A
0.002
N/A
 
A3
8.71 - 10.2
0.0015
 
A2
7.37 - 8.71
0.0013
 
A1
6.0 - 7.37
0.001
 
A
5.71 - 6.0
0.0005
 
B
5.3 - 5.71
0.0013
 
C
4.76 - 5.3
0.002
 
D
4.13 - 4.76
0.0015
 
E
3.98 - 4.13
0.0013
 
F
Bore ID (does not include bore edge radius)
0.0012
 
G
3.98 - 4.12
0.0013
 
H
4.12 - 4.66
0.0015
 
I
4.66 - 4.89
0.002
 
J
4.89 - 5.49
0.0023
 
K
5.49 - 5.7
0.002
 
L
5.7 - 60
0.0015
 
L1
6.0 - 10.17
0.0015
 
L2
10.17 - 10.4
0.002
 
L3
10.4 -10.56
0.0023
 
Stage 9
 
Webs (9FW, 9AW). Refer to Figure 801
N/A
0.002
Refer to Table 7
 
Stage 10
 
Webs (10FW, 10AW). Refer to Figure 801.
N/A
0.002
Refer to Table 7
NOTE:
For the border values in ranges given in column B (radius distance) use lower depth value from column D.
NOTE:
Use applicable radius (bore ID or end of bore edge radius) to calculate exact distance from engine center line to indication found. Refer to Figure 815 and Figure 816.
F.Table 6.
 
Stages 6, 7, and 8 disk nicks/dents serviceable limits for part numbers 2628M56G01 and 2628M56G02
 
A
B
C
D
 
Zone
Radius (inches) as distance from center line
Axial distance from Face Z (applicable for stage 7 hook areas, refer to Figure 814)
Max serviceable depth (inches)
 
Stage 6
 
A
6.42 - 10.25
N/A
0.001
 
B
5.85 - 6.42
0.0013
 
C
5.58 - 5.85
0.0015
 
D
5.12 - 5.58
0.002
 
E
4.60 - 5.12
0.003
 
F
4.15 - 4.60
0.002
 
G
3.66 - 4.15
0.0015
 
H
Bore ID (does not includes bore edge radius)
0.0013
 
I
3.66 - 4.15
0.0015
 
J
4.15 - 4.60
0.0023
 
K
4.60 - 5.36
0.003
 
L
5.36 - 5.60
0.0025
 
M
5.60 - 6.42
0.0015
 
N
6.42 - 10.25
0.001
 
Stage 7
 
A
7.034 - 10.25
N/A
0.001
 
B
6.68 - 7.034
0.002
 
C
6.20 - 6.68
0.0025
 
D
5.86 - 6.20
0.0035
 
E
5.63 - 5.86
0.0033
 
F
5.37 - 5.63
0.003
 
G
5.10 - 5.37
0.0025
 
H
4.90 - 5.10
0.002
 
I
4.46 - 4.90
0.0015
 
J
4.035 - 4.46 (does not include bore edge radius)
0.0013
 
K
3.962 - 4.7 (does not include bore edge radius)
0.0045
 
JR
N/A
Radius
0.0005
 
KR
Radius
0.0025
 
IR
Radius
0.001
 
L
4.7 - 5.5
N/A
0.005
 
M
5.5 - 5.8
0.0045
 
N
5.8 - 6.15
0.002
 
O
6.15 - 6.92
0.0013
 
P
6.92 - 7.021
0.0015
 
R
7.021 - 10.25
0.001
 
S
N/A
Radius
0.003
 
T
Radius
0.001
 
U
0.225 to 0.800
0.002
 
W
up to 0.400
0.003
 
Face Z
Forward face
0.004
 
Stage 8
 
A4
10.23 - 10.56
N/A
0.0025
 
A3
9.5 - 10.23
0.002
 
A2
6.75 - 9.5
0.0015
 
A1
6.0 - 6.75
0.0013
 
B
5.77 - 6.0
0.001
 
C
5.53 - 5.77
0.0013
 
D
5.26 - 5.53
0.0025
 
E
5.07 - 5.26
0.003
 
F
4.71 - 5.07
0.0025
 
G
4.34 - 4.71
0.002
 
H
3.98 - 4.34
0.0015
 
I
Bore ID (does not include bore edge radius)
0.0015
 
J
3.98 - 4.27
0.0015
 
K
4.27 - 4.56
0.002
 
L
4.56 - 4.76
0.0023
 
M
4.76 - 5.6
0.0025
 
N
5.6 - 6.0
0.002
 
O1
6.0 - 6.1
0.002
 
O2
6.1 - 9.2
0.0015
 
O3
9.2 - 10.2
0.002
 
O4
10.2 - 10.56
0.0025
 
Stage 9
 
Webs (9FW, 9AW). Refer to Figure 801
N/A
0.002
 
Stage 10
 
Webs (10FW, 10AW). Refer to Figure 801
N/A
0.002
NOTE:
For the border values in ranges given in column B (radius distance) use lower depth value from column D.
NOTE:
Use applicable radius (bore ID or end of bore edge radius) to calculate exact distance from engine center line to indication found. Refer to Figure 815 and Figure 816.
G.Table 7.
 
Max scratch depth (inches)
Max scratch length (inches)
 
0.001
1.000
 
0.002
0.250
 
0.003
0.170
 
0.004
0.130
 
0.005
0.100
NOTE:
Max serviceable depth value for scratches must be read from Tables 1, 3, and 5. This table provides max length of scratches for given depth value.
* * * FOR ALL
Figure 808   HPC 6-10 Spool - Post Inspection Shotpeening Zones
* * * FOR ALL
Figure 809   Definition Zones for Scratches for Part Numbers 2439M35G01, 2439M35G02, 2445M40G02, and 2610M90G01
* * * FOR ALL
Figure 810   Definition Zones for Nicks and Dents for Part Numbers 2439M35G01, 2439M35G02, 2445M40G02, and 2610M90G01
* * * FOR ALL
Figure 811   Definition Zones for Scratches for Part Numbers 2357M30G02
* * * FOR ALL
Figure 812   Definition Zones for Nicks and Dents for Part Numbers 2357M30G02
* * * FOR ALL
Figure 813   Definition Zones for Scratches for Disk Stages 6-8, Part Numbers 2628M56G01 and 2628M56G02
* * * FOR ALL
Figure 814   Definition Zones for Nicks and Dents for Disk Stages 6-8, Part Numbers 2628M56G01 and 2628M56G02
* * * FOR ALL
Figure 815   (Sheet 1 ) Bore Area Edge Radius Locations and Disk Sections
* * * FOR ALL
Figure 815   (Sheet 2 ) Bore Area Edge Radius Locations and Disk Sections
* * * FOR ALL
Figure 815   (Sheet 3 ) Bore Area Edge Radius Locations and Disk Locations
* * * FOR ALL
Figure 815   (Sheet 4 ) Bore Area Edge Radius Locations and Disk Locations
* * * FOR ALL
Figure 816   Distance from Engine Center Line to Bore ID for Part Numbers 2628M56G01, 2628M56G02, 2445M40G02, 2439M35G01, 2439M35G02, and 2610M90G01
* * * FOR ALL
Figure 817   Distance from Engine Center Line to Bore ID for Part Numbers 2357M30G02