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 72-32-17-300-002 No. 2 And 3 Bearing Compartment Oil Jets - Blend Repair, Repair-002 (VRS1220)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-400 | 5A1701 |
01-400 | 5A5385 |
01-500 | 5A1643 |
01-500 | 5A5348 |
01-600 | 5R0197 |
01-600 | 5R0581 |
01-700 | 5R0071 |
01-700 | 5R0574 |
01-700 | 5R0293 |
General
Price and availability - none
The practices and processes referred to in the procedure by the TASK number are in the SPM.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-019 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-019 | ||
| CoMat 05-020 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-020 | ||
| CoMat 05-021 WATERPROOF SILICON CARBIDE | 44197 | CoMat 05-021 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Use abrasive stone or CoMat 05-019 WATERPROOF SILICON CARBIDE, CoMat 05-020 WATERPROOF SILICON CARBIDE and CoMat 05-021 WATERPROOF SILICON CARBIDE and/or a fine file.
Surface finish of the repaired area must be the same as the adjacent surface.
Refer to the SPM TASK 70-35-03-300-501.
Scallop, make smooth and/or hand polish to remove the burrs.
SUBTASK 72-32-17-350-054 Remove the Damage of the Oil Jet Assembly
Refer to TASK 72-32-17-200-004 (INSPECTION-004, CONFIG-001).
Visually examine the repaired area.
SUBTASK 72-32-17-220-074 Examine the Oil Jet Assembly
Refer to TASK 72-32-17-200-004 (INSPECTION-004, CONFIG-001).
Refer to the SPM TASK 70-23-05-230-501.
Fluorescent penetrant examine the repaired area.
SUBTASK 72-32-17-230-053 Examine the Oil Jet Assembly
Figure: Oil Jet Assembly - Repair Limit
Oil Jet Assembly - Repair Limit

