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 72-41-21-300-057 HPC Heatshields - Blend Repair On The Stage 8 Heatshield, Repair-057 (VRS6290)
Material of component
PART IDENT | SYMBOL | MATERIAL |
|---|---|---|
HP compressor stage 8 heat shield assembly | EBQ | Corrosion resistant steel |
General
This Repair must only be done when the instruction to do so is given in 72-41-21 Inspection/Check.
This Repair has been raised to repair the surface damage on the HP compressor stage 8 heat shield assembly.
The practices and processes referred to in the procedure by the TASK number are in the SPM.
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 05-106 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.
The maximum depth of the repaired areas is to be 0.005 in. (0.133 mm).
Refer to the SPM TASK 70-35-03-300-501.
Remove small areas of damage as necessary.
Refer to the SPM TASK 70-35-03-300-501.
Make the damaged areas smooth.
Make sure all the scratches are removed and the surface finish is the same as the adjacent material.
Refer to the SPM TASK 70-35-03-300-501.
Polish the area.
SUBTASK 72-41-21-350-105 Remove the Damaged Areas
Refer to Figure.
SUBTASK 72-41-21-220-264 Examine the Repair
Refer to the SPM TASK 70-23-01-230-501.
Do the penetrant crack test.
SUBTASK 72-41-21-230-111-001 Examine the Stage 8 Heat Shield for Cracks
Refer to the SPM TASK 70-23-03-230-501.
Do the penetrant crack test.
SUBTASK 72-41-21-230-111-002 Examine the Stage 8 Heat Shield for Cracks
Figure: An example of an area to be repaired
An example of an area to be repaired

