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 72-41-31-300-032 HPC Blank - Blend Repair, Repair-032 (VRS3845)
General
This repair must only be done when the instruction to do so is given in 72-41-31 Inspection/Check-012.
The practices and processes referred to in the procedure by the TASK number are in SPM.
Price And Availability - None
NOTE
NOTE
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 05-074 ALUMINIUM OXIDE ABRASIVE PAPER | 06565 | CoMat 05-074 | ||
| CoMat 05-111 EMERY POLISHING PAPER | 06565 | CoMat 05-111 |
Spares
NONESafety Requirements
NONEProcedure
Refer to SPM TASK 70-23-01-230-501.
Cracks are not permitted.
Do a penetrant crack test.
SUBTASK 72-41-31-230-069-003 Do a Crack Test
Refer to SPM TASK 70-23-03-230-501.
Cracks are not permitted.
Do a penetrant crack test.
SUBTASK 72-41-31-230-069-004 Do a Crack Test
Refer to Figure.
Make sure the damage marks are completely removed and the area is made smooth in to the adjacent material.
The maximum depth to remove the damage must not be more than 0.005 in. (0.13 mm). The diameter of the repaired area is to be 50 times the depth.
Refer to SPM TASK 70-35-03-300-501.
Remove the damage.
Polish the repaired area to remove the scratches and to give a surface finish the same as the adjacent material.
Refer to TASK 70-35-03-300-501.
Polish the area of repair.
SUBTASK 72-41-31-350-125 Remove the Damage
Refer to Figure.
Make sure the surface finish is the same as the adjacent material.
The maximum depth of the repair must not be more than 0.005 in. (0.13 mm).
The diameter of the repair must not be more than 0.250 in. (6.25 mm).
Do a visual and dimensional inspection.
SUBTASK 72-41-31-220-290 Examine the Repair
Refer to SPM TASK 70-23-01-230-501.
Cracks are not permitted.
Do a penetrant crack test.
SUBTASK 72-41-31-230-070-003 Do a Crack Test
Refer to SPM TASK 70-23-03-230-501.
Cracks are not permitted.
Do a penetrant crack test.
SUBTASK 72-41-31-230-070-004 Do a Crack Test
Figure: An Example of an Area to be Repaired
An Example of an Area to be Repaired

