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 72-50-24-300-029 LPT Stage 3 Inner Air Seal Ring - Plasma Spray The Vane Mating Face, Repair-029 (VRS4135)
General
Price and availability - none
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 |
|---|---|---|---|---|
| Turning lathe | LOCAL | Turning lathe | ||
| Grinding machine | LOCAL | Grinding machine |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-047 TAPE, HEAT REFLECTIVE | 52152 | CoMat 02-047 | ||
| CoMat 02-050 HIGH TEMPERATURE GLASS CLOTH TAPE | 76381 | CoMat 02-050 | ||
| CoMat 03-096 PLASMA SPRAY POWDER | LOCAL | CoMat 03-096 | ||
| CoMat 05-046 ALUMINUM OXIDE GRIT | 62596 | CoMat 05-046 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
SUBTASK 72-50-24-325-078 Machine the Vane Mating Face
Refer to Figure.
Examine dimensionally.
SUBTASK 72-50-24-220-144 Examine Machined Surface
Refer to the SPM TASK 70-11-34-300-503.
Aqueous degrease.
SUBTASK 72-50-24-110-109 Clean the Air Seal Ring
Refer to Figure.
Surface texture must be 120 to 200 microinch RMS (3.0 to 5.0 micrometer Ra).
Refer to the SPM TASK 70-34-03-340-501.
Grit blast the area A1.
SUBTASK 72-50-24-340-081 Prepare the Surfaces for the Plasma Spray Procedure
Refer to Figure.
Make sure that there is sufficient material to do last machining.
Refer to the SPM TASK 70-34-03-340-501.
In area A1 minimum coating thickness is 0.0039 in. (0.100 mm) after machining and maximum coating thickness is 0.0295 in. (0.750 mm) before machining.
Plasma spray the area A1.
Refer to the SPM TASK 70-34-03-340-501 for Acceptance Standards.
Examine the coating.
SUBTASK 72-50-24-340-082 Plasma Spray the Prepared Surfaces
Refer to Figure.
SUBTASK 72-50-24-325-079 Machine the Coated Areas
Refer to the SPM TASK 70-11-34-300-503.
Aqueous degrease.
SUBTASK 72-50-24-110-111 Clean the Air Seal Ring
Refer to Figure.
Examine the machined areas dimensionally.
Refer to the SPM TASK 70-34-03-340-501.
Examine the coating visually.
SUBTASK 72-50-24-220-149 Do the Post Repair Inspection
Refer to the SPM TASK 70-09-00-400-501.
Vibropeen VRS4135 and applicable beehive symbol adjacent to the part number.
SUBTASK 72-50-24-350-074 Make a Mark to Identify the Repair
Figure: Plasma Spray the Stage 3 Air Seal Ring
Plasma Spray the Stage 3 Air Seal Ring

Figure: Plasma Spray the Stage 3 Air Seal Ring
Plasma Spray the Stage 3 Air Seal Ring

