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 72-42-61-300-019 Outer Combustion Chamber Liner - Two-Coat Repair The Plasma Coat On The Front Inside Diameter, Repair-019 (VRS3742)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-501 | 2A0550-001 |
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 | 2A0546-01 |
01-520 | 2A1384-01 |
01-520 | 2A2711-01 |
01-520 | 2A2840-01 |
General
Price and availability - Refer to IAE
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-024 MASKING TAPE (CREPE PAPERBACKING) | 0AM53 | CoMat 02-024 | ||
| CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINE | DK026 | CoMat 03-066 | ||
| CoMat 03-096 PLASMA SPRAY POWDER | LOCAL | CoMat 03-096 | ||
| CoMat 06-018 FLUORESCENT PENETRANT (POST-EMULSIFIED HIGH SENSITIVITY) | 37676 | CoMat 06-018 | ||
| CoMat 06-065 FLUORESCENT PENETRANT (WATER WASHABLE HIGH SENSITIVITY) | K6858 | CoMat 06-065 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Repair, VRS3090 TASK 72-42-61-300-002 (REPAIR-002).
SUBTASK 72-42-61-350-097 Remove the Coating from the Front Inside Diameter of the Combustion Chamber Outer Liner
Refer to the SPM TASK 70-11-03-300-503 or SPM TASK 70-11-26-300-503.
SUBTASK 72-42-61-110-056 Clean the Combustion Chamber Outer Liner
Refer to the SPM TASK 70-23-05-230-501. Use CoMat 06-018 FLUORESCENT PENETRANT (POST-EMULSIFIED HIGH SENSITIVITY) or CoMat 06-065 FLUORESCENT PENETRANT (WATER WASHABLE HIGH SENSITIVITY). No cracks are permitted.
SUBTASK 72-42-61-230-055 Examine the Combustion Chamber Outer Liner
Refer to Figure.
SUBTASK 72-42-61-220-068 Examine the Front Inside Diameter of the Combustion Chamber Outer Liner
Refer to Figure.
Apply CoMat 03-096 PLASMA SPRAY POWDER coating 0.009 to 0.011 in. (0.23 to 0.28 mm) thick.
Refer to the SPM TASK 70-34-03-340-501.
SUBTASK 72-42-61-340-053 Apply a Base Coat to the Front Inside Diameter of the Combustion Chamber Outer Liner
Apply CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINE. Refer to Figure and Figure for coat thickness.
Refer to the SPM TASK 70-34-03-340-501. Do not grind the coating.
SUBTASK 72-42-61-340-052 Coat the Front Inside Diameter of the Combustion Chamber Outer Liner
Refer to Repair, VRS3092 TASK 72-42-61-300-004 (REPAIR-004), Repair, VRS3095 TASK 72-42-61-300-007 (REPAIR-007), Repair, VRS3096 TASK 72-42-61-300-008 (REPAIR-008) or Repair, VRS3450 TASK 72-42-61-300-015 (REPAIR-015).
SUBTASK 72-42-61-350-098 Install the Detail Parts to the Combustion Chamber Outer Liner
Refer to the TASK 72-42-61-200-000 (INSPECTION/CHECK-000).
SUBTASK 72-42-61-220-069 Examine the Front Inside Diameter of the Combustion Chamber Outer Liner after Repair
Make a permanent mark by the SPM TASK 70-09-00-400-501.
SUBTASK 72-42-61-350-101 Identify the Repair
Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions (PN 2A2711-01 and 2A2840-01)
Repair Details and Dimensions (PN 2A2711-01 and 2A2840-01)

Figure: Repair Details and Dimensions (PN 2A1384-01 and 2A0546-01)
Repair Details and Dimensions (PN 2A1384-01 and 2A0546-01)

