TASK 72-50-22-300-044 LPT Stage 5 Vane - Touch-Up Coating After Blend Repair , Repair-044 (VRS4249)

DMC:V2500-A0-72-50-2205-02A-609A-C|Issue No:002.00|Issue Date:2013-11-01

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 72-50-22-300-044 LPT Stage 5 Vane - Touch-Up Coating After Blend Repair , Repair-044 (VRS4249)

Effectivity

FIG/ITEM

PART NO.

01-350

3A1825

01-350

3A2305

Material of component

IAE

DESCRIPTION

SYMBOL

MATERIAL

Stage 5 turbine vane

MTS1206E/MAR-M-247

General

Price and availability - none

The practices and processes referred to in the procedure by the TASK numbers are in the SPM.

Deleted.

NOTE

For more equipment and materials necessary to do this repair, refer to the SPM TASK 70-37-27-370-501 and SPM TASK 70-38-14-380-501.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-50-22-330-072 Prepare the Material and Surfaces

      1. Prepare the material and the surface.

      1. Refer to the SPM TASK 70-38-14-380-501.

    2. SUBTASK 72-50-22-380-061 Touch-Up Coating of the Stage 5 Turbine Vane

      NOTE

      Deleted.

      1. Apply coating in area A1.

      1. Refer to the SPM TASK 70-38-14-380-501 and to Figure.

    3. SUBTASK 72-50-22-370-055-001 Diffusion Heat Treatment of the Recoated Stage 5 Turbine Vane

      NOTE

      Before diffusion heat treatment remove the honeycomb, refer to VRS4168 TASK 72-50-22-300-047 (REPAIR-047) or VRS4331 TASK 72-50-22-300-063 (REPAIR-063).
      After diffusion heat treatment replace the honeycomb, refer to VRS4168 TASK 72-50-22-300-047 (REPAIR-047) or VRS4331 TASK 72-50-22-300-063 (REPAIR-063).
      Do the precipitation heat treatment after honeycomb replacement VRS4168 TASK 72-50-22-300-047 (REPAIR-047) or VRS4331 TASK 72-50-22-300-063 (REPAIR-063).

      1. Diffuse the recoated stage 5 turbine vane.

      1. Refer to the SPM TASK 70-38-14-380-501.

      2. Precipitation heat treat the stage 5 turbine vane.

      1. Refer to the SPM TASK 70-37-27-370-501, alloy IAE 1447.

        Optional precipitation heat treatment of 1575 deg F to 1625 deg F (857 deg C to 885 deg C) for 8 hours can be used.

    4. SUBTASK 72-50-22-370-055-002 Diffusion Heat Treatment of the Recoated Stage 5 Turbine Vane

      NOTE

      Precipitation heat treatment is not necessary after optional diffusion heat treatment.

      1. Diffuse the recoated stage 5 turbine vane.

      1. Refer to the SPM TASK 70-38-14-380-501 except diffusion heat treat at 1575 deg F to 1625 deg F (857 deg C to 885 deg C) for 2 hours.

    5. SUBTASK 72-50-22-220-220 Do the Post Repair Inspection

      1. Examine the recoated areas.

      1. Refer to the SPM TASK 70-38-14-380-501.

    6. Figure: Touch-up coating of the stage 5 turbine vane

    Touch-up coating of the stage 5 turbine vane

Requirements After Job Completion

Follow-On Conditions

NONE