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 72-42-61-300-010 Outer Combustion Chamber Liner - Repair The Plasma Coating On The Rear Outside Diameter, Repair-010 (VRS3100)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-501 | 2A0550-01 |
01-501 | 2A1383 |
01-501 | 2A1385 |
01-501 | 2A1399 |
01-501 | 2A1618 |
01-501 | 2A1620 |
01-501 | 2A1666 |
01-501 | 2A2013 |
01-501 | 2A2032 |
01-501 | 2A2723-01 |
01-501 | 2A2837-01 |
01-501 | 2A3345-01 |
01-501 | 2A3345-001 |
01-501 | 2A3345-002 |
01-501 | 2A3345-003 |
01-501 | 2A3345-004 |
01-501 | 2A3347-01 |
01-501 | 2A3347-001 |
01-501 | 2A3347-002 |
01-501 | 2A3347-003 |
01-501 | 2A3347-004 |
01-501 | 2A3347-005 |
01-501 | 2A3439-01 |
01-501 | 2A3439-001 |
01-501 | 2A3439-002 |
01-501 | 2A3439-003 |
01-501 | 2A3439-004 |
01-501 | 2A3439-005 |
01-501 | 2A3439-006 |
01-501 | 2A3439-007 |
01-501 | 2A3439-008 |
01-501 | 2A3440-01 |
01-501 | 2A3440-001 |
01-501 | 2A3440-002 |
01-501 | 2A3440-003 |
01-501 | 2A3440-004 |
01-501 | 2A3440-005 |
01-501 | 2A3440-006 |
01-501 | 2A3440-007 |
01-501 | 2A3441-01 |
01-501 | 2A3441-001 |
01-501 | 2A3441-002 |
01-501 | 2A3441-003 |
01-501 | 2A3441-004 |
01-501 | 2A3441-005 |
01-501 | 2A3441-006 |
01-501 | 2A3441-007 |
01-501 | 2A3441-008 |
01-501 | 2A3442-01 |
01-501 | 2A3442-001 |
01-501 | 2A3442-002 |
01-501 | 2A3442-003 |
01-501 | 2A3442-004 |
01-501 | 2A3442-005 |
01-501 | 2A3442-006 |
01-501 | 2A3442-007 |
01-501 | 2A3442-008 |
01-501 | 2A4284-01 |
01-501 | 2A4309-01 |
01-501 | 2A4312-01 |
01-501 | 2A4314-01 |
01-501 | 2A4314-001 |
01-520 | 2A2711-01 |
General
The practices and processes referred to in the procedure by the TASK number are in the SPM.
Preliminary Requirements
Pre-Conditions
| Action/Condition | Data Module/Technical Publication |
|---|---|
| Make sure that all the cleaning and inspection procedures are done before this repair. | |
| If you use a chemical removal procedure, all details must be removed by the given repairs: | TASK 72-42-61-300-004 |
| TASK 72-42-61-300-008 | |
| TASK 72-42-61-300-015 | |
| TASK 72-42-61-300-007 | |
| TASK 72-42-61-300-006 |
Support Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Deleted.
Remove the coating that is on the part by SPM TASK 70-32-07-100-501.
Make sure you remove all the details.
Apply a mask or maskants to all the areas that are not to be removed by SPM TASK 70-38-24-300-503.
Remove the coating that is on the part by chemical removal procedure. Refer to the SPM TASK 70-33-90-300-503.
Remove the coating that is on the part by high pressure water jet. Refer to the SPM TASK 70-15-01-160-501.
Remove the coating that is on the part by one or more of the procedures that follow:
SUBTASK 72-42-61-350-064 Remove the Coating from the Rear Outside Diameter of the Combustion Chamber Outer Liner
Clean the part by Aqueous Cleaning Method by SPM TASK 70-11-03-300-503.
SUBTASK 72-42-61-110-056 Clean the Combustion Chamber Outer Liner
Do a fluorescent penetrant inspection of the repair area by the SPM TASK 70-23-03-230-501.
Do a fluorescent penetrant inspection of the repair area by the SPM TASK 70-23-08-230-501.
Do a fluorescent penetrant inspection of the repair area by one of the methods that follow. Refer to Figure.
SUBTASK 72-42-61-230-058 Fluorescent Penetrant Inspect the Repair Area
Do a dimensional inspection of the repair area.
Do a visual inspection of the repair area to make sure that you removed all the coating.
Refer to Figure.
SUBTASK 72-42-61-220-163 Examine the Rear Outside Diameter Seal on the Combustion Chamber Outer Liner
Prepare the surface for coating. Refer to the SPM TASK 70-34-18-380-501.
SUBTASK 72-42-61-380-001 Prepare the Surface of the Rear Outside Diameter
Refer to Figure.
Deleted.
Coating out of the repair area is not permitted. Use masks or maskants.
Do not grind the coating.
Coating thickness 0.003 - 0.005 in. (0.076 - 0.128 mm).
Coat the rear outside diameter of the outer liner by IAE 53-5. Refer to the SPM TASK 70-34-03-340-501.
SUBTASK 72-42-61-350-065 Coat the Rear Outside Diameter of the Combustion Chamber Outer Liner
Refer to Figure.
Examine the rear outside diameter.
SUBTASK 72-42-61-220-126 Examine the Rear Outside Diameter of the Combustion Chamber Outer Liner after Repair
Mark VRS3100 adjacent to the part number, use vibration peen method. Refer to the SPM TASK 70-09-00-400-501.
SUBTASK 72-42-61-350-066 Identify the Repair
Figure: Rear outside diameter plasma coating repair
Rear outside diameter plasma coating repair

Requirements After Job Completion
Follow-On Conditions
| Action/Condition | Data Module/Technical Publication |
|---|---|
| If removed, all details must be installed by the given repairs: | TASK 72-42-61-300-004 |
| TASK 72-42-61-300-008 | |
| TASK 72-42-61-300-015 | |
| TASK 72-42-61-300-007 | |
| TASK 72-42-61-300-006 |
