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 72-50-32-300-072 LPT Stage 6 Blade - Weld Build Up Repair The Knife Edge Seals, Repair-072 (VRS4560)
General
Price and availability - none
The practices and processes referred to in this procedure by the TASK number are in the SPM.
NOTE
NOTE
NOTE
NOTE
If repair of pre-twist is also required, then do VRS4303 TASK 72-50-32-300-054 (REPAIR-054) first, before start of this repair.
Do not repair turbine blades that have cracks extending into the outer shroud.
Before repair, write down the turbine blade part number and serial number.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| External grinding machine | LOCAL | External grinding machine | ||
| Tridimensional measuring unit | LOCAL | Tridimensional measuring unit | ||
| DELETED | 0AM53 | DELETED | ||
| IAE 3M14414 Welding fixture | 0AM53 | IAE 3M14414 | 1 | |
| IAE 3M14524 Grinding mounting block | 0AM53 | IAE 3M14524 | ||
| IAE 3M14471 Grinding fixture | 0AM53 | IAE 3M14471 | ||
| IAE 2M14184 Inspection mounting block | 0AM53 | IAE 2M14184 | ||
| IAE 3M14466 Welding mounting block | 0AM53 | IAE 3M14466 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 03-245 WELDING FILLER WIRE | LOCAL | CoMat 03-245 | ||
| CoMat 03-287 WELDING FILLER WIRE | LOCAL | CoMat 03-287 | ||
| CoMat 05-029 CAST STEEL SHOT, S110 | LOCAL | CoMat 05-029 | ||
| CoMat 05-030 CAST STEEL SHOT DELETED | 0AM53 | CoMat 05-030 | ||
| CoMat 05-031 CAST STEEL SHOT DELETED | 0AM53 | CoMat 05-031 | ||
| CoMat 05-138 SHOT, CAST STEEL, S110 | 11851 | CoMat 05-138 | ||
| CoMat 05-177 CUT WIRE SHOT,CW-14 | LOCAL | CoMat 05-177 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Use IAE 3M14524 Grinding mounting block 1 off, IAE 3M14471 Grinding fixture 1 off, and External grinding machine.
Keep material removal to a minimum.
Grind the knife edge seals.
SUBTASK 72-50-32-324-063 Machine the Knife Edge Seals
Refer to Figure.
SUBTASK 72-50-32-220-445 Examine the Machined Areas
Use IAE 3M14466 Welding mounting block 1 off and IAE 3M14414 Welding fixture 1 off.
Make sure that there is sufficient material to do last machining.
Refer to the SPM TASK 70-31-13-310-501.
Decrease temperature of the turbine blades to reduce heat affected zone to a minimum.
Gas tungsten arc weld build-up seal fins.
SUBTASK 72-50-32-310-087 Weld Build-Up Repair the Knife Edge Seals
Refer to the SPM TASK 70-37-10-370-501, Stress-Relief Cycle 5.
Stress-relieve the turbine blade.
SUBTASK 72-50-32-370-101 Heat Treatment after Weld Repair
NOTE
Do the stress-relief after all weld operations.Refer to the SPM TASK 70-23-04-230-501.
Cracks in knife edge welds can be repaired providing they do not extend into the outer shroud.
Do the test for cracks.
SUBTASK 72-50-32-230-194 Examine the Welded Areas for Cracks
Refer to Figure and Fig 72-32-50-990-309-002.
Use IAE 3M14524 Grinding mounting block 1 off, IAE 3M14471 Grinding fixture 1 off, and External grinding machine.
Grind the welded areas.
SUBTASK 72-50-32-324-064 Machine the Welded Areas
Refer to the SPM TASK 70-23-05-230-501.
Use high sensitivity level.
Cracks in knife edge welds can be repaired.
For limits refer to VRS4186 TASK 72-50-32-300-008 (REPAIR-008).
Do the test for cracks.
SUBTASK 72-50-32-230-195 Examine the Machined Areas for Cracks
Refer to the SPM TASK 70-38-13-380-501. Use CoMat 05-029 CAST STEEL SHOT, S110 or CoMat 05-030 CAST STEEL SHOT DELETED or CoMat 05-031 CAST STEEL SHOT DELETED or CoMat 05-138 SHOT, CAST STEEL, S110 or CoMat 05-177 CUT WIRE SHOT,CW-14 to an intensity of 6A.
Shotpeen blade root flanks plus corner radii to end faces.
Shotpeening is permitted in area A2.
Shotpeen area A1.
SUBTASK 72-50-32-380-093 Shotpeen the Surface A1 of the Stage 6 Turbine Blade
If you cannot read any of these, make new marks.
Use the roll stamp method.
Refer to the SPM TASK 70-09-00-400-501.
Examine the markings of part number and serial number.
SUBTASK 72-50-32-220-446 Examine the Stage 6 Turbine Blade Markings
Refer to the SPM TASK 70-09-00-400-501.
Vibropeen VRS4560 adjacent to the part number.
SUBTASK 72-50-32-380-094 Make a Mark to Identify the Repair
Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

