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 72-32-76-300-015 LPC Stage 2.5 Stator - Replace The Abradable Rubber Of The Outer Shroud Ring, Repair-015 (VRS1873)
Material of component
PART IDENT | SYMBOL | MATERIAL |
|---|---|---|
Ring, shroud outer | Aluminum alloy | |
Ring, shroud outer | Silicone rubber |
General
Price and availability - Refer to IAE
This repair scheme gives the procedure for replacing of abradable rubber.
The practices and processes referred to in the procedure by the TASK number are in the SPM.
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Hand Tools | LOCAL | Tools, Hand | ||
| Knife | LOCAL | Knife | Sharp | |
| Oven | LOCAL | Oven | ||
| Precision weighing scales | LOCAL | Precision weighing scales | ||
| Hardness tester (Durometer) | LOCAL | Hardness tester (Durometer) | ||
| IAE 3J12775 Bond test fixture | 0AM53 | IAE 3J12775 | 1 | |
| IAE 3J12785 Inspection stand | 0AM53 | IAE 3J12785 | 1 | |
| IAE 3J13214 Molding support | 0AM53 | IAE 3J13214 | 1 | |
| IAE 3J13155 Filler injector | 0AM53 | IAE 3J13155 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-076 METHYL ETHYL KETONE | LOCAL | CoMat 01-076 | ||
| CoMat 02-001 ADHESIVE TAPE (MASKING) | LOCAL | CoMat 02-001 | ||
| CoMat 02-005 ADHESIVE TAPE (MASKING) | LOCAL | CoMat 02-005 | ||
| CoMat 02-099 LINT-FREE CLOTH | X222X | CoMat 02-099 | ||
| CoMat 02-218 MOLD RELEASE AGENTS | 18598 | CoMat 02-218 | ||
| CoMat 08-032 PRIMER | B1571 | CoMat 08-032 | ||
| CoMat 08-037 DELETED | X111X | CoMat 08-037 | ||
| CoMat 08-038 SILICONE RUBBER COMPOUND | FAK74 | CoMat 08-038 | ||
| CoMat 02-217 MOLD RELEASE AGENTS | 18598 | CoMat 02-217 |
Spares
NONESafety Requirements
NONEProcedure
Apply adhesive tape for masking to the areas which do not require remaining rubber.
Refer to SPM TASK 70-12-07-120-501.
Use dry plastic blast to remove the remaining rubber.
Remove adhesive tape for masking.
Remove the remaining rubber from the outer shroud, if the remaining rubber is not fully removed in Step.
SUBTASK 72-32-76-350-066 Remove the Defective Rubber
Apply a very thin coat of CoMat 08-032 PRIMER with CoMat 02-099 LINT-FREE CLOTH.

CAUTION
THICK PRIMER WILL CAUSE BOND FAILURE OF SILICONE RUBBER.NOTE
Parts shall have CoMat 08-037 DELETED or CoMat 08-038 SILICONE RUBBER COMPOUND applied within 24 hours of completion of the primer application.Apply primer to the bond surface.
Refer to the SPM TASK 70-36-06-360-501.
Cure the CoMat 08-032 PRIMER.
SUBTASK 72-32-76-380-058 Apply Primer
Refer to the SPM TASK 70-36-06-360-501.
Use CoMat 08-037 DELETED or CoMat 08-038 SILICONE RUBBER COMPOUND The working life of the mixed silicone rubber is a maximum 6 hours at room temperature.
Measure out materials by weight as follows: 10 parts rubber 1 part curing agent.
SUBTASK 72-32-76-360-067 Mixing Instruction
Refer to Figure.
Use tools IAE 3J13214 Molding support 1 off and IAE 3J13155 Filler injector 1 off.
Set the tools to the repair part.
SUBTASK 72-32-76-360-068 Fill with Mixed Silicone Rubber
Refer to the SPM TASK 70-36-06-360-501.
Cure at 290 deg F to 310 deg F (143 deg C to 155 deg C) for one hour with the molding fixture.
Refer to the SPM TASK 70-36-06-360-501.
Cure the removed component at 390 deg F to 410 deg F (199 deg C to 210 deg C) for one hour out of the molding fixture.
SUBTASK 72-32-76-360-069 Cure the Silicone Rubber Compound
Refer to Figure.
SUBTASK 72-32-76-350-067 Remove Overfilled Silicone Rubber
Refer to Figure.
No bubbles are permitted.
No foreign inclusions are permitted.
No peelings are permitted.
Refer to Figure.
Refer to the SPM TASK 70-36-06-360-501.
If necessary, do this TASK again.
Visually examine the repaired area.
SUBTASK 72-32-76-220-127 Visually Examine the Repair Area
Refer to Figure.
Refer to Figure.
Use IAE 3J12775 Bond test fixture 1 off and IAE 3J12785 Inspection stand 1 off. No signs of bulging or air leakage are permitted.
NOTE
The bond test shall be done after curing (bake) the rubber to the conditions that follow:Inspection gas: Air or nitrogen gas.Gas pressure: 400 psi (28.1 Kg/sqcm).Inspection position: Refer to Figure.Vary the pattern as necessary to inspect not fully repaired areas.Probe angle: Approximately 45 degrees.Holes created by the bond test to be permitted.Do a bond test on the repaired area.
SUBTASK 72-32-76-220-130 Do a Bond Test on the Repaired Area
Figure: Silicone Rubber Application Area
Silicone Rubber Application Area

Figure: Replacement Of The Abradable Rubber
Replacement Of The Abradable Rubber

Figure: Bond Test Of The Abradable Rubber
Bond Test Of The Abradable Rubber

