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 72-41-23-300-003 HPC Rear Outer Case - Replace The Surface Protection, Repair-003 (VRS6178)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
02-400 | 6A2949 |
02-400 | 6A3557 |
02-400 | 6A4154 |
02-400 | 6A5495 |
02-400 | 6A5682 |
02-400 | 6A8162 |
02-400 | 6B1427 |
General
This repair must only be done when the instruction to do so is given in the inspection procedures (identified by the applicable part number) located in TASK 72-41-23-200-001-A00, TASK 72-41-23-200-001-B00 and TASK 72-41-23-200-001-C00, Inspection-001.
This Repair replaces the surface protection on the HPC Rear Outer Case.
TASKS identified by SPM TASK are in the Standard Practices Manual (SPM).
More equipment and materials necessary to do this repair are in each SPM TASK identified in this repair.
Price and Availability
Refer to International Aero Engines.
Related Repairs
HPC Rear Outer Case - Replace the Damaged Shank Nuts, refer to Repair, VRS6279 TASK 72-41-23-300-011 (REPAIR-011).
Preliminary Requirements
Pre-Conditions
| Action/Condition | Data Module/Technical Publication |
|---|---|
| Make sure that all the cleaning and inspection procedures, including any required FPI and other needed repairs, are done before this repair. | |
| Make sure the Shank Nuts are removed. | TASK 72-41-23-300-011 |
Support Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 06-073 INK, METAL MARKING | LOCAL | CoMat 06-073 | ||
| CoMat 07-035 CORROSION RESISTANT COATING | LOCAL | CoMat 07-035 | ||
| CoMat 07-104 ALUMINIUM HIGH HEAT RESISTANT PAINT | LOCAL | CoMat 07-104 | ||
| CoMat 07-125 LACQUER | 0W199 | CoMat 07-125 | ||
| CoMat 07-175 COATING COMPOUND - ALUMINUM, INORGANIC BINDER | 53012 | CoMat 07-175 |
Spares
NONESafety Requirements
NONEProcedure
If the surface protection coating is not already removed or not completely removed, remove the coat completely by TASK 72-41-00-100-000 (Cleaning-000).
SUBTASK 72-41-21-330-071 Remove the Coat
Use vibration peen by SPM TASK 70-09-00-400-501.
SUBTASK 72-41-21-350-280 Mark the Part
For PN 6A2949, PN 6A3557, PN 6A4154 and PN 6A5495, refer to Figure.
For PN 6A5682, PN 6A8162 and PN 6B1427, refer to Figure.
Use CoMat 07-035 CORROSION RESISTANT COATING (Type A or B Coating) by SPM TASK 70-38-21-380-501.
For PN 6A2949, PN 6A3557, PN 6A4154 and PN 6A5495, refer to Figure.
For PN 6A5682, PN 6A8162 and PN 6B1427, refer to Figure.
Use CoMat 07-104 ALUMINIUM HIGH HEAT RESISTANT PAINT (Type A or B Coating) by SPM TASK 70-38-21-380-501.
For PN 6A2949, PN 6A3557, PN 6A4154 and PN 6A5495, refer to Figure.
For PN 6A5682, PN 6A8162 and PN 6B1427, refer to Figure.
Use CoMat 07-175 COATING COMPOUND - ALUMINUM, INORGANIC BINDER (Type A or B Coating) by SPM TASK 70-38-42-380-501.
Prepare the surface and apply the surface protection coating and examine the coated surface on the part by one of the following procedures. Refer to Figure and Figure. Unless otherwise stated in the figures, apply coat all over the part.
SUBTASK 72-41-21-380-155 Apply Surface Protection
Use temporary marking by SPM TASK 70-09-01-400-501.
CoMat 06-073 INK, METAL MARKING must be completely dry prior to application of CoMat 07-125 LACQUER.
Apply two thin coats of CoMat 07-125 LACQUER to avoid dissolving ink pigment. Allow each layer to dry prior to the next coat.
Heavier application of CoMat 07-125 LACQUER is permitted after the light application of the coating completely dries.
Mark the part with the part number and VRS6178 adjacent to the assembly part number. See Figure Index [2] and Figure, Index [2].
SUBTASK 72-41-21-350-281 Mark the Part
Figure: Repair Details and Dimensions
(1) Area To Be Masked. Dry Abrasive Blast And Coat Not Allowed In These Areas And Holes.

Repair Details and Dimensions

Repair Details and Dimensions

Repair Details and Dimensions

Repair Details and Dimensions

Repair Details and Dimensions

Figure: Repair Details and Dimensions
(1) Area To Be Masked. Dry Abrasive Blast And Coat Not Allowed In These Areas And Holes.

Repair Details and Dimensions

Repair Details and Dimensions

Repair Details and Dimensions

Repair Details and Dimensions

Requirements After Job Completion
Follow-On Conditions
| Action/Condition | Data Module/Technical Publication |
|---|---|
| Replace the Shank Nuts. | TASK 72-41-23-300-011 |
