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 72-45-33-300-004 HPT Stage 2 Blade Retaining Plate - Plasma Spray Repair The Outside Diameter Mating Face, Repair-004 (VRS3515)
Preliminary Requirements
Pre-Conditions
| Action/Condition | Data Module/Technical Publication |
|---|---|
| Make sure that all the cleaning and inspection procedures are done before this repair. |
Support Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 03-080 METAL SPRAYING POWDER,Co BASE ALLOY | IE426 | CoMat 03-080 | ||
| DELETED | LOCAL | DELETED |
Spares
NONESafety Requirements
NONEProcedure
Grind the front face on Surface S to remove all the coating by SPM TASK 70-32-07-100-501. Use IAE 53-18.
SUBTASK 72-45-33-320-051-001 Remove the Coating from the Front Outer Mating Face
Remove a minimum amount of parent material.
Machine or grind the front face on Surface S to remove all the damage or wear by SPM TASK 70-32-07-100-501. Use IAE 53-18.
SUBTASK 72-45-33-320-051-002 Machine or Grind to Remove Wear or Damage from the Front Outer Mating Face
Do the procedure given in SPM TASK 70-11-03-300-503.
Clean the retaining plate.
SUBTASK 72-45-33-100-051 Clean the Stage 2 HPT Retaining Plate
Do the Fluorescent Penetrant Inspection (FPI) procedure by the applicable part number task given in TASK 72-45-33-200-000 (Inspection-000). Cracks are not permitted.
Do a fluorescent penetrant inspection of the front outer mating face.
SUBTASK 72-45-33-230-060 Fluorescent Penetrant Inspection of the Front Outer Mating Face
Grit blast outside of the repair area is not permitted.
Shotpeen is not required on the repair area.
Use masks or maskants.
Refer to SPM TASK 70-34-18-380-501.
Apply masks and grit blast the front outer mating face for plasma coat.
SUBTASK 72-45-33-120-051 Grit Blast the Front Outer Mating Face before Coating
Make sure the masking is still applied in all the areas not to be coated. Apply the plasma spray to a thickness which will permit you to final machine the part to the dimensions given in the figure. The minimum thickness of the coating after finish machining is 0.003 in. (0.08 mm). Do the procedure given in SPM TASK 70-34-03-340-501.
Plasma spray the front outer mating face.
Remove the masks or maskants after plasma spray. Refer to SPM TASK 70-34-18-380-501.
SUBTASK 72-45-33-340-051 Plasma Spray the Front Outer Mating Face
Finish grind the front outer mating face of the retaining plate by SPM TASK 70-32-07-100-501.
SUBTASK 72-45-33-320-052 Finish Grind the Front Outer Mating Face after Plasma Spray
Mark the part with "VRS3515" adjacent to the part number by SPM TASK 70-09-00-400-501, subtask 70-09-00-400-001, using the vibration peen, dot peen or electrolytic etch methods. Remove high spots caused by marking.
Refer to Figure for the electrical contact area.
No burning, pitting or selective attach on the electrical contact areas is permitted.
Permanently mark the part. Refer to Figure for the marking location. Ensure the part is marked as follows:
SUBTASK 72-45-33-350-051 Identify the Repair
Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

