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 72-50-22-300-003 LPT Stage 7 Vane - Replace The Honeycomb Seal Segments On The Outer Buttress, Repair-003 (VRS4033)
Material of component
RR | ||
|---|---|---|
DESCRIPTION | SYMBOL | MATERIAL |
Stage 7 turbine vane | Inconel 713 | |
Honeycomb seal segment | Hastelloy X |
General
Price and availability - none
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
NOTE
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Illuminated comparator magnifier | LOCAL | Illuminated comparator magnifier | ||
| Fluid tank | LOCAL | Fluid tank | ||
| Grinding machine | LOCAL | Grinding machine | ||
| Spot welding machine | LOCAL | Spot welding machine | ||
| Vertical turning lathe | LOCAL | Vertical turning lathe | ||
| Vernier caliper | LOCAL | Vernier caliper | ||
| IAE 3M14200 Grinding/turning fixture | 0AM53 | IAE 3M14200 | 1 | |
| IAE 3M14220 Cross slide table | 0AM53 | IAE 3M14220 | 1 | |
| IAE 3M14221 Electrode guide | 0AM53 | IAE 3M14221 | 1 | |
| IAE 3M14222 Electrode holder | 0AM53 | IAE 3M14222 | 1 | |
| IAE 3M14223 Universal joint electrode | 0AM53 | IAE 3M14223 | 1 | |
| IAE 3M14224 Spot welding fixture | 0AM53 | IAE 3M14224 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-001 SOLVENT, DELETED | 0AM53 | CoMat 01-001 | ||
| CoMat 01-183 WETTING AGENT FOR ACIDCLEANER | 1XY28 | CoMat 01-183 | ||
| CoMat 02-142 WETTING AGENT | 08340 | CoMat 02-142 | ||
| CoMat 02-143 DELETED | 0AM53 | CoMat 02-143 | ||
| CoMat 02-144 BONDING AGENT | C7208 | CoMat 02-144 | ||
| CoMat 03-151 HIGH TEMP. BRAZING FILLERPOWDER | LOCAL | CoMat 03-151 | ||
| CoMat 03-227 WHITE STOP OFF | D3309 | CoMat 03-227 | ||
| CoMat 03-234 BRAZING FILLER TAPE | LOCAL | CoMat 03-234 | ||
| CoMat 10-061 STODDARD SOLVENT | LOCAL | CoMat 10-061 |
Spares
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Honeycomb seal segment | 3A1572 | 1 |
Safety Requirements
NONEProcedure
Use a vertical turning lathe and the IAE 3M14200 Grinding/turning fixture 1 off. Remove the damaged honeycomb seal segment fully.
Keep the material removal to the minimum to permit subsequent repairs.
The minimum acceptable dimension for repair is 0.307in. (7.80 mm).
To get this dimension it is permitted to let stay a braze thickness of 0.005in. (0.13 mm).
Refer to Figure.
Machine the worn honeycomb seals.
SUBTASK 72-50-22-325-061 Machine the Damaged Honeycomb Seal Segments
Refer to the SPM TASK 70-11-01-300-503.
Vapor degrease.
SUBTASK 72-50-22-110-082 Clean the Stage 7 Turbine Vane
Refer to the SPM TASK 70-12-08-300-503.
Wet abrasive blast the machined area.
SUBTASK 72-50-22-120-056 Wet Abrasive Blast the Stage 7 Turbine Vane
Use the IAE 3M14220 Cross slide table 1 off and a spot welding machine.
Install the cross slide table on to the spot welding machine.
Use the IAE 3M14222 Electrode holder 1 off.
Install the electrode holder on to the spot welding machine.
Use the IAE 3M14223 Universal joint electrode 1 off.
Make sure that the electrode insert with the mark "outer" (part of the universal joint electrode) is installed.
Install the universal joint electrode on to the electrode holder.
Use the IAE 3M14221 Electrode guide 1 off.
Install the electrode guide on to the cross slide table.
Use the IAE 3M14224 Spot welding fixture 1 off.
Install the spot welding fixture on to the electrode guide.
Align the honeycomb seal segment, refer to Figure.
Position the honeycomb seal segment on to the stage 7 turbine vane.
SUBTASK 72-50-22-310-056 Braze in the New Honeycomb Seal Segment
NOTE
If CoMat 03-151 HIGH TEMP. BRAZING FILLERPOWDER is used, perform steps G. to I. If CoMat 03-234 BRAZING FILLER TAPE is used, perform steps J. to L.Refer to the SPM TASK 70-11-01-300-503.
Vapor degrease.
SUBTASK 72-50-22-110-084 Clean the Stage 7 Turbine Vane
Use 200:1 mixture of water and CoMat 02-142 WETTING AGENT or.
1:1 mixture of CoMat 10-061 STODDARD SOLVENT and CoMat 02-143 DELETED or.
2500:1 mixture of water and CoMat 01-183 WETTING AGENT FOR ACIDCLEANER for acid cleaner or.
1:1 mixture of CoMat 01-001 SOLVENT, DELETED and the CoMat 10-061 STODDARD SOLVENT.
Prepare fluid tank.
Refer to the SPM TASK 70-31-07-310-501, except for the following:
No unbrazed cells around the edges of the honeycomb segment are permitted.
The minimum space between unbonded areas of more than 0.063 sqin (40.65 sqmm) should be 1.00in. (25.4 mm).
Use a vernier caliper and an illuminated comparator magnifier.
No braze filled cells are permitted.
The honeycomb wall thickness must not be increased by more than 0.001in. (0.03 mm) in the area above the braze fillet.
Acceptance limits.
SUBTASK 72-50-22-210-056 Examine the Brazed Honeycomb Seal
Grind to the dimensions.
Refer to Figure.
Use the IAE 3M14200 Grinding/turning fixture 1 off and a grinding machine.
Finish machine the honeycomb seal segment.
Refer to the SPM TASK 70-12-08-300-503 or use a wire brush.
De-burr the honeycomb seal segment.
SUBTASK 72-50-22-325-062 Do the Post Repair
Refer to the SPM TASK 70-11-01-300-503.
Vapor degrease.
SUBTASK 72-50-22-110-085 Clean the Honeycomb Seal Segment
Refer to Figure.
Dimensionally examine the stage 7 turbine vane.
SUBTASK 72-50-22-220-127 Do the Post Repair Inspection
Refer to the SPM TASK 70-09-00-400-501.
Electrolytically etch or vibro-peen VRS4033 adjacent to the part number.
SUBTASK 72-50-22-350-067 Make a Mark to Identify the Repair
Figure: Replace the honeycomb seal segment on the outer buttress of the stage 7 turbine vane
Replace the honeycomb seal segment on the outer buttress of the stage 7 turbine vane

Figure: Replace the honeycomb seal segment on the outer buttress of the stage 7 turbine vane
Replace the honeycomb seal segment on the outer buttress of the stage 7 turbine vane

Figure: Special procedures for brazing the honeycomb seal segment on the outer buttress of the stage 7 turbine vane
Special procedures for brazing the honeycomb seal segment on the outer buttress of the stage 7 turbine vane

