* * * FOR ALL
TASK 72-31-45-300-802
1 . Seal Teeth Strip and Recoat
A.This procedure gives instructions to repair high pressure compressor rotor stage 6-10 spool (spool) seal teeth by removing the existing coating and recoating. Refer to Figure 901.
B.The following maximum repairable limits apply to this repair:
NOTE:
The information below gives maximum repairable limits for the applicable Inspection sections. The paragraphs are numbered the same as the manual Inspection sections.
(4)Visual Inspection.
(e)Do an inspection of the interstage seal teeth for:
2Chipped or missing coating after you apply the coating again:
Maximum repairable limit:
Any amount
(6)Dimensional Inspection.
(c)Do an inspection of the interstage seal teeth diameters before you apply the coating for:
1Diameter FU:
Maximum repairable limit:
21.821 inches (554.25 mm)
2Diameter DH:
Maximum repairable limit:
22.340 inches (567.44 mm)
3Diameter DE:
Maximum repairable limit:
22.466 inches (570.64 mm)
4Diameter KG:
Maximum repairable limit:
22.526 inches (572.16 mm)
5Diameter KN:
Maximum repairable limit:
22.526 inches (572.16 mm)
C.The subsequent table gives a list of the part numbers that are applicable to this repair. All part numbers are applicable to all paragraphs unless specified differently.
 
Part Number(s)
 
2357M30G02  
2439M35G01  
2439M35G02  
2445M40G02  
 
2610M90G01  
2628M56G01  
2628M56G02  
--
D.Proprietary/Complex Process Statement.
(1)None.
2 . Tools, Equipment, and Materials.
NOTE:
Repair sources can use equivalent alternatives for tools, equipment, and consumable materials, however, the repair source must demonstrate and document equivalency.
A.Tools and Equipment.
(1)Special Tools. None.
(2)Standard Tools and Equipment. None.
(3)Locally Manufactured Tools.
 
Description
Figure
 
Machining Fixture (fixture)
904
B.Consumable Materials.
 
Code No.
Description
 
C04-113
Abrasive, Grit, Aluminum Oxide 220 Mesh (aluminum oxide)
 
C04-166
Shot, Peening, Conditioned Cut Wire (CCW14 shot)
 
C10-012
Tape, Masking, High Temperature (tape)
 
C10-021
Tape (plastic tape)
C.Referenced Procedures.
 
ATA No.
Description
 
70-00-03
Machining Data
 
70-21-00
Chemical Cleaning
 
70-21-01
Cleaning Method 1 - Solvent Degreasing
 
70-21-03
Cleaning Method 3 - Steam Cleaning
 
70-21-04
Cleaning Method 4 - Dry Abrasive Blast Cleaning
 
70-21-09
Deleted
 
70-23-00
Stripping Procedures
 
70-23-07
Stripping of Thermal Spray Aluminum Oxide, Non-Ferrous, and Bond Coatings
 
70-23-12
Stripping Thermal Sprayed Coatings
 
70-23-23
Removal of Coatings by High Pressure Water Stripping
 
70-24-00
Etching Procedures for Fluorescent-Penetrant Inspection
 
70-24-01
Swab Etching Procedure
 
70-32-00
Indirect Inspection Methods
 
70-32-03
Spot-Fluorescent-Penetrant Inspection
 
70-42-00
Blending and Removal of High Metal Procedures
 
70-47-01
Shotpeening
 
70-49-00
Thermal Spraying
 
70-49-02
Thermal Spraying Aluminum Oxide - Alumina (Powder)
 
70-49-10
Thermal Spraying Nickel-Aluminum (Powder)
 
72-31-45
Inspection 001
D.Expendable Parts. None.
E.SPD Information. None.
F.Special Solutions. None.
G.Test Specimens. Refer to TASK 70-49-02-340-003 (THERMAL SPRAYING ALUMINUM OXIDE - ALUMINA (POWDER)) and TASK 70-49-10-340-011 (THERMAL SPRAYING NICKEL-ALUMINUM (POWDER)) .
3 . Dimensional Information.
Subtask 72-31-45-220-107
A.Refer to Figure 901 for specified dimensions and locations.
NOTE:
The dimensional data identified within this procedure was designed using inches as the base unit of measurement for dimensional values. The conversion to millimeters is rounded to one less decimal digit than inches. For minimum dimensions, converted values are rounded up. For maximum dimensions, converted values are rounded down. To avoid conversion errors, do not reconvert from millimeters to inches.
 
Minimum
Maximum
Minimum
Maximum
 
In-Process
In-Process
Finish
Finish
Reference
 
Description
Dimension
Dimension
Dimension
Dimension
Dimension
 
Dia FU
21.821 in.
21.843 in.
21.853 in.
21.863 in.
--
 
(554.25 mm)
(554.81 mm)
(555.07 mm)
(555.32 mm)
 
Dia DH
22.340 in.
22.362 in.
22.372 in.
22.382 in.
--
 
(567.44 mm)
(567.99 mm)
(568.25 mm)
(568.50 mm)
 
Dia DE
22.466 in.
22.488 in.
22.498 in.
22.508 in.
--
 
(570.64 mm)
(571.19 mm)
(571.45 mm)
(571.70 mm)
 
Dia KG
22.526 in.
22.548 in.
22.558 in.
22.568 in.
--
 
(572.16 mm)
(572.71 mm)
(572.98 mm)
(573.22 mm)
 
Dia KN
22.526 in.
22.548 in.
22.558 in.
22.568 in.
--
 
(572.16 mm)
(572.71 mm)
(572.98 mm)
(573.22 mm)
4 . Setup Information.
Subtask 72-31-45-930-001
A.If necessary, make the machining fixture. Refer to Figure 905.
Subtask 72-31-45-350-009
B.Deleted.
Subtask 72-31-45-350-010
C.Set-up the spool for machining as follows:
(1)Install the spool on the fixture aft end down. Refer to Figure 904 and as follows:
(a)Surface L must be flat to 0.002 inch (0.05 mm) or less.
(b)Diameter M must have a runout of 0.002 inch (0.05 mm) or less.
5 . Procedure.
Subtask 72-31-45-100-004
A.Alternative Procedure Available. Remove the coating from the seal teeth as follows:
(1)Set-up the seal in the fixture. Refer to Subtask 72-31-45-930-001 (paragraph 4.A.), Setup Information.
(2)Remove the thermal coating from the seal teeth. Refer to TASK 70-23-00-100-001 (STRIPPING PROCEDURES) and TASK 70-23-23-330-008 (REMOVAL OF COATINGS BY HIGH PRESSURE WATER STRIPPING).
Subtask 72-31-45-100-005
A.A.Alternative Procedure. Remove the coatings from the seal teeth as follows:
(1)Remove the top coating and bond coating from the seal teeth. Refer to TASK 70-23-00-100-001 (STRIPPING PROCEDURES), TASK 70-21-04-120-001 (CLEANING METHOD NO. 4 - DRY ABRASIVE BLAST CLEANING), TASK 70-23-12-110-027 (STRIPPING THERMAL SPRAYED COATINGS), and as follows:
(a)If necessary, grit-blast thermal spray coating to remove top coat. Refer to TASK 70-21-04-120-A01 (DRY ABRASIVE BLAST CLEANING METHOD 4A) and as follows:
1Apply C10-012  tape to areas that you will not grit blast.
2Use 220 mesh C04-113  aluminum oxide at 75-90 psia (517-621 kPa).
(b)If necessary, apply C10-012  tape again.
(c)Remove the bond coating. Refer to TASK 70-23-00-100-001 (STRIPPING PROCEDURES), TASK 70-23-12-110-027 (STRIPPING THERMAL SPRAYED COATINGS) or TASK 70-23-07-110-023 (STRIPPING OF THERMAL SPRAY ALUMINUM OXIDE, NON-FERROUS, AND BOND COATINGS).
(d)Remove the plastic tape.
(e)If necessary, remove the remaining coating residue with plastic media blast. Refer to TASK 70-21-04-120-E01 (DRY ABRASIVE BLAST CLEANING METHOD 4E).
(f)If you used plastic media blast, clean to remove the plastic media residue. Refer to TASK 70-21-03-160-001 (CLEANING METHOD NO. 3 - STEAM CLEANING).
Subtask 72-31-45-220-108
B.Do a dimensional inspection of the repair diameters. Refer to Subtask 72-31-45-220-107 (paragraph 3.A.), Dimensional Information, Figure 902, and as follows:
(1)Measure each diameter at 10 equally-spaced locations. Calculate the average diameter dimension.
(2)If the repair diameter is within in-process dimensions and there is no damage on the surface refer to Subtask 72-31-45-200-002 (paragraph 5.G.).
(3)If the repair diameter is within in-process dimensions but there are damages or remaining coating on the diameter surface or if the diameter is more than the maximum in-process dimension, machine the diameter. Refer to Subtask 72-31-45-320-003 (paragraph 5.C.).
(4)If the repair diameter is less than the minimum in-process dimension, the spool is not repairable with this repair procedure.
Subtask 72-31-45-320-003
C.If necessary, machine the seal teeth. Refer to TASK 70-00-03-800-004 (MACHINING DATA), Subtask 72-31-45-220-107 (paragraph 3.A.), Dimensional Information, Figure 902, and as follows:
(1)Set-up the seal for machining. Refer to Subtask 72-31-45-350-010 (paragraph 4.C.), Setup Information.
(2)Machine the seal teeth to the in-process dimensions.
Subtask 72-31-45-350-011
D.If you machined the seal teeth, blend the burrs and rolled edges from the seal teeth. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES) and as follows:
(1)Break all edges to 0.0050 inch (0.12 mm) maximum.
Subtask 72-31-45-100-006
E.Clean the spool. Refer to TASK 70-21-00-110-051 (CHEMICAL CLEANING) and TASK 70-21-03-160-001 (CLEANING METHOD 3 - STEAM CLEANING).
Subtask 72-31-45-110-007
F.Etch the repair area. Refer to TASK 70-24-00-110-033 (ETCHING PROCEDURES FOR FLUORESCENT-PENETRANT INSPECTION), TASK 70-24-01-110-034 (SWAB ETCHING PROCEDURE), and as follows:
(1)Use Class C or Class G etchant.
Subtask 72-31-45-200-002
G.Do an inspection of the repair diameters. Refer to TASK 70-32-00-200-002 (INDIRECT INSPECTION METHODS), TASK 70-32-03-230-002 (SPOT-FLUORESCENT-PENETRANT INSPECTION), and as follows:
(1)Use Class G penetrant.
(2)Indications more than 0.015 inch (0.38 mm) are not permitted.
(3)Linear indications are not permitted.
NOTE:
Linear indications are indications that are at least four times longer than they are wide.
Subtask 72-31-45-380-002
H.Peen the seal teeth diameters. Refer to TASK 70-47-01-380-016 (SHOTPEENING) and as follows:
(1)Set-up the seal in the fixture. Refer to Subtask 72-31-45-930-001 (paragraph 4.A.), Setup Information.
(2)Apply C10-021  plastic tape to diameter M and diameter B. Refer to Figure 902.
(3)Coverage must be a minimum of 125 percent.
(4)Intensity verification necessary with a simulative fixture.
(5)Use C04-166  CCW14 shot.
(6)Intensity must be 0.006-0.012N.
(7)Overspray is permitted.
(8)Direct impingement required.
(9)Remove all plastic tape.
Subtask 72-31-45-340-003
I.Thermal-spray the spool and the test specimens. Refer to TASK 70-49-00-340-001 (THERMAL SPRAYING), TASK 70-49-10-340-011 (THERMAL SPRAYING NICKEL-ALUMINUM (POWDER)), Figure 902, and as follows:
(1)Deleted.
(2)Apply a mask to the part. Refer to Figure 904 and as follows:
(a)Use C10-012  tape.
(3)Grit blast area JD, area JE and the test specimens. Refer to Figure 904, and as follows:
(a)The final surface finish must agree with nickel-base material.
Subtask 72-31-45-110-008
(4)Clean area JD, area JE and the test specimens. Refer to TASK 70-21-01-110-001 (CLEANING METHOD 1 - SOLVENT DEGREASING) and Figure 904.
Subtask 72-31-45-340-004
(5)Apply bond coat to areas JD and JE on each seal tooth, and to the test specimens. Refer to TASK 70-49-00-340-001 (THERMAL SPRAYING), TASK 70-49-10-340-011 (THERMAL SPRAYING NICKEL-ALUMINUM (POWDER)), Figure 902, and as follows:
NOTE:
Spray coat must be applied within 2 hours after grit blasting.
(a)Apply a mask to the part. Refer to Figure 904 and as follows:
1Use C10-012  tape.
(b)Overspray is permitted only in area JF.
(c)The bond coating thickness in area JD must be 0.002-0.005 inch (0.06- 0.12 mm).
(d)The bond coating thickness in area JE must be 0.002-0.008 inch (0.06- 0.20 mm).
(e)Do the all the quality assurance tests specified in TASK 70-49-10-340-011 (THERMAL SPRAYING NICKEL-ALUMINUM (POWDER)).
(6)Apply top coat to areas JD and JE on each seal tooth, and to the test specimens. Refer to TASK 70-49-00-340-001 (THERMAL SPRAYING), TASK 70-49-02-340-003 (THERMAL SPRAYING ALUMINUM OXIDE - ALUMINA (POWDER)), Figure 902, and as follows:
(a)If necessary, apply a mask to the part again. Refer to Figure 904 and as follows:
1Use C10-012  tape.
(b)Overspray is permitted only in area JF.
(c)The final machined top coating thickness in area JD must be 0.003- 0.013 inch (0.08-0.33 mm).
(d)The final top coating thickness in area JE must be 0.003-0.013 inch (0.08-0.33 mm).
(e)Do all the quality assurance tests specified in TASK 70-49-02-340-003 (THERMAL SPRAYING ALUMINUM OXIDE - ALUMINA (POWDER)).
1The porosity for the top coat may be less than or equal to V-4.
Subtask 72-31-45-320-004
J.Machine the spool. Refer to TASK 70-00-03-800-004 (MACHINING DATA), Subtask 72-31-45-220-107 (paragraph 3.A.), Dimensional Information, Figure 902, and as follows:
(1)Set-up the seal in the machining fixture. Refer to Subtask 72-31-45-930-001 (paragraph 4.A.), Setup Information and Subtask 72-31-45-350-010 (paragraph 4.C.), Setup Information.
(2)Machine the repair diameters to the finish dimensions.
Subtask 72-31-45-100-007
K.Clean the spool. Refer to TASK 70-21-00-110-051 (CHEMICAL CLEANING) and TASK 70-21-03-160-001 (CLEANING METHOD 3 - STEAM CLEANING).
Subtask 72-31-45-220-109
L.Do a visual inspection of the machined coating on the seal teeth. Refer to TASK 72-31-45-200-807 (72-31-45, INSPECTION 001).
* * * FOR ALL
Figure 901   Compressor Rotor Spool Stages 6-10
* * * FOR ALL
Figure 902   (Sheet 1 ) Compressor Rotor Spool Stages 6-10 - Dimensional Information
* * * FOR ALL
Figure 902   (Sheet 2 ) Compressor Rotor Spool Stages 6-10 - Dimensional Information
* * * FOR ALL
Figure 902   (Sheet 3 ) Compressor Rotor Spool Stages 6-10 - Dimensional Information
* * * FOR ALL
Figure 903   Compressor Rotor Spool Stages 6-10 - Masking
* * * FOR ALL
Figure 904   (Sheet 1 ) Machining Fixture - Setup Information
* * * FOR ALL
Figure 904   (Sheet 2 ) Machining Fixture - Setup Information
* * * FOR ALL
Figure 905   (Sheet 1 ) Machining Fixture
* * * FOR ALL
Figure 905   (Sheet 2 ) Machining Fixture
* * * FOR ALL
Figure 905   (Sheet 3 ) Machining Fixture
* * * FOR ALL
Figure 905   (Sheet 4 ) Machining Fixture
* * * FOR ALL
Figure 905   (Sheet 5 ) Machining Fixture
* * * FOR ALL
Figure 905   (Sheet 6 ) Machining Fixture
* * * FOR ALL
Figure 905   (Sheet 7 ) Machining Fixture