Export Control
EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.Copyright
© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).Applicability
All
Common Information
TASK 72-41-23-300-002 HPC Rear Outer Case - Replace The Lining, Repair-002 (VRS6179)
Effectivity
FIG/ITEM | PART NO. | ASSEMBLY |
|---|---|---|
02-400 | 6A2949 | A |
02-400 | 6A3557 | A |
02-400 | 6A4154 | A |
02-400 | 6A5495 | A |
02-400 | 6A5682 | C |
02-400 | 6A8162 | C |
Material of component
PART IDENT | MATERIAL |
HP compressor rear outer case assembly | Corrosion resistant steel |
General
This Repair must only be done when the instruction to do so is given in 72-41-23 Inspection/Check.
This TASK gives the procedure to repair the HP compressor rear outer case assembly by the replacement of the lining.
TASKs identified by SPM TASK are in the Standard Practices and Processes Manual (SPM).
Price and availability
Refer to International Aero Engines
Related repairs
HP Compressor Rear Outer Case Assembly - Replace Surface Protection, refer to VRS6178, TASK 72-41-23-300-003 (REPAIR-003).
NOTE
NOTE
It is possible that some materials in the Consumable Materials chart cannot be used for some or all of the necessary applications. Before you use the materials, make sure the types, quantities and applications of the materials necessary are legally permitted in your location. All persons must obey all applicable federal, state, local and provincial laws and regulations when it is necessary to work with these materials.
To identify the consumable materials, refer to the Overhaul Processes and Consumables Index (PCI).
Other necessary consumable materials are referred to in the SPM TASKs.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Abrasive blast equipment | LOCAL | Abrasive blast equipment | ||
| Chemical cleaning equipment | LOCAL | Chemical cleaning equipment | ||
| Gloves | LOCAL | Gloves | Cotton or polythene | |
| Dial indicator | LOCAL | Dial indicator | ||
| Grinding machine | LOCAL | Grinding machine | ||
| Lathe | LOCAL | Lathe | ||
| Metal spray equipment | LOCAL | Metal spray equipment | ||
| Penetrant Crack Test Equipment | LOCAL | Penetrant crack test equipment | ||
| Standard workshop equipment | LOCAL | Standard workshop equipment | ||
| Brush | LOCAL | Brush | Vacuum assisted | |
| Vibrating marking pencil | LOCAL | Vibrating marking pencil | ||
| Workshop inspection equipment | LOCAL | Workshop inspection equipment | ||
| IAE 3R18658 Turn/Grind fixture | 0AM53 | IAE 3R18658 | 1 | |
| IAE 3R18659 Mask | 0AM53 | IAE 3R18659 | 1 | |
| IAE 3R18660 Mask | 0AM53 | IAE 3R18660 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-001 ADHESIVE TAPE (MASKING) | LOCAL | CoMat 02-001 | ||
| CoMat 02-006 ADHESIVE TAPE ALUMINIUM FOIL | K0993 | CoMat 02-006 | ||
| CoMat 03-096 PLASMA SPRAY POWDER | LOCAL | CoMat 03-096 | ||
| CoMat 03-239 METAL SPRAYING POWDER, CHROMIUM CARBIDE/NICHROME 75/25, FINE | LOCAL | CoMat 03-239 | ||
| CoMat 03-240 METAL SPRAYING POWDER, CHROMIUM CARBIDE/NICHROME 75/25, FINE | LOCAL | CoMat 03-240 | ||
| CoMat 05-001 ABRASIVE MEDIUM, ALUMINIUM OXIDE, 20/30 GRADE | LOCAL | CoMat 05-001 | ||
| CoMat 06-064 FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY) | LOCAL | CoMat 06-064 |
Spares
NONESafety Requirements
NONEProcedure
NOTE
This SUBTASK is an alternative to Step.Chemically degrade the lining at area identified AD.
Abrasive blast the area identified AD.
SUBTASK 72-41-23-330-001 Remove the Lining

CAUTION
SURFACES FOR REPAIR MUST BE FULLY CLEANED AND NOT TOUCHED BY HAND. CLEAN COTTON OR POLYTHENE GLOVES MUST BE WORN.NOTE
This SUBTASK is an alternative to Step.Install the turn/grind fixture on to the machine and set to run true.
SUBTASK 72-41-23-325-051 Remove the Lining
Use CoMat 02-001 ADHESIVE TAPE (MASKING)and/or IAE 3R18659 Mask 1 off and IAE 3R18660 Mask 1 off.
Seal the areas not to be repaired.
Refer to the SPM TASK 70-12-02-120-501.
Use CoMat 05-001 ABRASIVE MEDIUM, ALUMINIUM OXIDE, 20/30 GRADE with abrasive blast equipment.
Abrasive blast the rear outer case on area AD.
SUBTASK 72-41-23-120-051 Abrasive Blast the Rear Outer Case Assembly

CAUTION
SURFACES FOR REPAIR MUST BE FULLY CLEANED AND NOT TOUCHED BY HAND. CLEAN COTTON OR POLYTHENE GLOVES MUST BE WORN.If the diameter is less than or equal to 23.2580 in. (590.762 mm), continue the repair from Step.
If the diameter is more than 23.2580 in. (590.762 mm) but less than 23.2860 in. (591.464 mm), continue the repair.
Measure the diameter AC to calculate the repair area.
SUBTASK 72-41-23-220-205-A00 Examine the Rear Outer Case Assembly, Assembly A
If the diameter is less than or equal to 23.2580 in. (590.762 mm), continue the repair from Step.
If the diameter is more than 23.2580 in. (590.762 mm) but less than 23.2860 in. (591.464 mm), continue the repair.
Measure the diameter AC to calculate the repair area.
If the diameter is less than or equal to 23.1808 in. (588.792 mm), continue the repair from Step.
If the diameter is more than 23.1808 in. (588.792 mm) but less than 23.2078 in. (589.478 mm), continue the repair.
Measure the diameter AF to calculate the repair area.
SUBTASK 72-41-23-220-205-B00 Examine the Rear Outer Case Assembly, Assembly C
Use CoMat 02-006 ADHESIVE TAPE ALUMINIUM FOIL and IAE 3R18659 Mask 1 off and IAE 3R18660 Mask 1 off.
Seal the areas not to be sprayed.
Refer to the SPM TASK 70-34-03-340-501.
Apply a bond coat of sufficient thickness to get the correct dimensions after the top coat is applied.
Apply the plasma spray to area AD.
SUBTASK 72-41-23-340-055 Apply the Plasma Spray (Bond Coat) to the HP Compressor Rear Outer Case Assembly
Use CoMat 02-006 ADHESIVE TAPE ALUMINIUM FOIL and IAE 3R18659 Mask 1 off and IAE 3R18660 Mask 1 off.
Seal the areas not to be sprayed.
Refer to the SPM TASK 70-34-01-340-501, SUBTASK 70-34-01-340-026.
Use CoMat 03-239 METAL SPRAYING POWDER, CHROMIUM CARBIDE/NICHROME 75/25, FINE or CoMat 03-240 METAL SPRAYING POWDER, CHROMIUM CARBIDE/NICHROME 75/25, FINE with metal spray equipment.
Apply a layer of sufficient thickness to get the correct dimensions after the assembly is machined.
Apply the lining to area AD.
SUBTASK 72-41-23-340-051 Apply the Lining to the HP Compressor Rear Outer Case Assembly
Use IAE 3R18658 Turn/Grind fixture 1 off with a grinding machine and a dial test indicator.
Install the turn/grind fixture on a grinding machine and set to turn correctly.
SUBTASK 72-41-23-324-051 Machine the Lining
Refer to Figure.
SUBTASK 72-41-23-350-062 Identify the Repair
Repair VRS6178, TASK 72-41-23-300-003 (REPAIR-003).
Apply the surface protection again.
SUBTASK 72-41-23-380-058 Re-apply the Surface Protection
Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions - Assembly C
Repair Details and Dimensions - Assembly C

Figure: Repair Details and Dimensions - Assembly C
Repair Details and Dimensions - Assembly C

