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 75-32-52-300-004 HPC Stage 7 Bleed Outlet Duct Silencer - Blend Repair Surface Damage, Repair-004 (VRS6241)
Effectivity
FIG/ITEM | PART NO. | |
01-250 | 6A2092 | Assembly A |
01-350 | 6A2092 | Assembly A |
01-250 | 6A6535 | Assembly B |
01-350 | 6A6536 | Assembly B |
01-250 | 6A4404 | Assembly B |
01-350 | 6A4404 | Assembly B |
01-250 | 6A6537 | Assembly B |
01-350 | 6A6538 | Assembly B |
01-250 | 6A8338 | Assembly B |
01-350 | 6A8338 | Assembly B |
Material of the component
PART IDENT | SYMBOL | MATERIAL |
HPC air silencer - stage 7 - Assy A | TEY | Titanium alloy |
HPC air silencer - Stage 10 - Assy A | TEY | Titanium alloy |
HPC air silencer - Stage 7 - Assy B | QAR | Nickel alloy C263 |
HPC air silencer - Stage 10 - Assy B | QAR | Nickel alloy C263 |
General
The practices and processes referred to in the procedure by the TASK number are in the SPM.
This Repair must only be done when the instruction to do so is given in 75-32-52 Inspection/Check.
Price and availability.
Refer to International Aero Engines.
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Workshop Inspection Equipment | LOCAL | Workshop Inspection Equipment | ||
| Penetrant Crack Test Equipment | LOCAL | Penetrant Crack Test Equipment |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-020 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-020 | ||
| CoMat 05-021 WATERPROOF SILICON CARBIDE | 44197 | CoMat 05-021 | ||
| CoMat 05-106 ABRASIVE STONE | K6835 | CoMat 05-106 | ||
| CoMat 05-110 EMERY POLISHING PAPER | 0AM53 | CoMat 05-110 | ||
| CoMat 05-111 EMERY POLISHING PAPER | 06565 | CoMat 05-111 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Refer to SPM TASK 70-35-03-300-501.
The maximum depth to remove the damage must not be more than 0.005 in (0.13 mm).
Remove all sharp corners.
The diameter of the repaired area is to be 50 times the depth.
Remove the damage.
Refer to SPM TASK 70-35-03-300-501.
Use CoMat 05-020 WATERPROOF SILICON CARBIDE abrasive paper and/or CoMat 05-021 WATERPROOF SILICON CARBIDE.
Polish the repaired area to remove the scratches.
Polish the area of repair.
SUBTASK 75-32-52-350-051-A00 Remove the Damage, Assembly A

CAUTION
TITANIUM COMPONENT - YOU MUST USE SILICON CARBIDE TYPE ABRASIVE WHEELS, STONES AND PAPERS TO DRESS, BLEND AND POLISH THIS COMPONENT.
CAUTION
TITANIUM COMPONENT - AVOID BUILD UP OF HEAT BY APPLYING ONLY GENTLE PRESSURE AND KEEPING THE TOOL SPEED AS LOW AS POSSIBLE
CAUTION
TITANIUM COMPONENT - YOU MUST MAKE SURE THAT WHEN YOU REMOVE MATERIAL, BLEND AND POLISH, NO SPARKS ARE PRODUCED.
CAUTION
TITANIUM COMPONENT - IF THE MATERIAL SHOWS A CHANGE IN COLOR, TO DARKER THAN A LIGHT STRAW COLOR, THE COMPONENT IS TO BE REJECTED.Refer to Figure.
Refer to SPM TASK 70-35-03-300-501.
The maximum depth to remove the damage must not be more than 0.005 in (0,13 mm)
Remove all sharp corners.
The diameter of the repaired area is to be 50 times the depth.
Remove the damage.
Refer to SPM TASK 70-35-03-300-501.
Polish the repaired area to remove the scratches.
Polish the area of repair.
SUBTASK 72-32-52-350-051-B00 Remove the Damage, Assembly B
Refer to Figure.
The maximum depth of the repair must not be more than 0.005 in. (0.13 mm).
Do a visual and dimensional inspection.
SUBTASK 75-32-52-220-060 Examine the Repair
Refer to the SPM TASK 70-23-01-230-501.
Cracks are not permitted.
Do a penetrant crack test.
SUBTASK 75-32-52-230-054-001 Do a Crack Test
Refer to the SPM TASK 70-23-03-230-501.
Cracks are not permitted.
Do a penetrant crack test.
SUBTASK 75-32-52-230-054-002 Do a Crack Test
Figure: An Example of an Area to be Repaired
An Example of an Area to be Repaired

