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 72-41-21-300-023 HPC Cross Key Location Ring - Repair Surface Damage By Material Removal, Repair-023 (VRS6103)
Effectivity
FIG/ITEM | PART NO. | |
04-750 | 6A2856 | Assembly A |
04-750 | 6A4179 | Assembly A |
04-750 | 6A5737 | Assembly B |
04-750 | 6A5738 | Assembly B |
Material of component
DESCRIPTION | SYMBOL | MATERIAL |
|---|---|---|
HP compressor cross key | QRK or | Nickel, cobalt steel |
location ring | QTX |
General
This Repair must only be done when the instruction to do so is given in 72-41-21 Inspection/Check.
The practices and processes referred to in the procedure by the TASK/SUBTASK number are in the SPM.
Price and availability
Refer to International Aero Engines.
Related repairs
None.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Penetrant Crack Test Equipment | LOCAL | Penetrant crack test equipment | ||
| Workshop inspection equipment | LOCAL | Workshop inspection 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 | LOCAL | CoMat 05-110 | ||
| CoMat 05-111 EMERY POLISHING PAPER | 06565 | CoMat 05-111 |
Spares
NONESafety Requirements
NONEProcedure
Refer to TASK 72-41-21-100-000.
Chemically clean.
SUBTASK 72-41-21-110-132 Clean the Cross Key Location Ring
Refer to TASK 72-41-21-200-000.
Do a penetrant crack test.
SUBTASK 72-41-21-230-108 Do a Crack Test
Refer to Figure.
Refer to the SPM TASK 70-35-03-300-501.
The diameter of the repaired areas is to be 50 times the depth. The maximum depth of the repaired areas is to be 0.005 in. (0.13 mm).
Remove the damaged material as necessary. Do not remove more than is necessary.
Refer to the SPM TASK 70-35-03-300-501.
Make sure all damage marks are completely removed and the area(s) made smooth into the adjacent material.
Make the repaired area(s) smooth.
Refer to the SPM TASK 70-35-03-300-501.
Polish the repaired area(s) to remove the scratches and to give a smooth surface finish.
Polish the repaired area(s).
SUBTASK 72-41-21-350-098 Remove the Damaged Area(s)
Refer to Figure.
SUBTASK 72-41-21-220-261 Examine the Repaired Area(s)
Use penetrant crack test equipment.
Cracks are not permitted.
Refer to the SPM TASK 70-23-05-230-501.
Do the penetrant crack test of the damaged area(s).
SUBTASK 72-41-21-230-109 Do a Crack Test
Figure: Repair Details and Dimensions
Repair Details and Dimensions

