TASK 71-21-11-300-013 Front Mount Tube - Repair The Damaged Outer Diameter By Nickel Plate, Repair-013 (VRS1075)

DMC:V2500-A0-71-21-1102-00A-647A-C|Issue No:001.00|Issue Date:2014-05-01

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 71-21-11-300-013 Front Mount Tube - Repair The Damaged Outer Diameter By Nickel Plate, Repair-013 (VRS1075)

Effectivity

FIG/ITEM

PART NO.

01-150

5A1698

01-150

5A6025

Material of component

PART IDENT

SYMBOL

MATERIAL

Engine front mount tube assembly

Nickel base alloy

General

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Universal GrinderLOCALUniversal Grinder
Nickel Plate EquipmentLOCALNickel Plate Equipment
Penetrant Crack Test EquipmentLOCALPenetrant Crack Test Equipment
OvenLOCALOven
IAE 3J12857 Grinding fixture0AM53IAE 3J128571

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 71-21-11-110-063 Remove the Dry Film Lubricant

      1. Remove the dry film lubricant.

      1. Refer to TASK 71-21-11-100-000 (CLEANING-000).

    2. SUBTASK 71-21-11-330-001 Grind the Damaged Outer Diameter

    1. Refer to Figure.

      2. NOTE

        If surface has been previously repaired using nickel plate, remove old plating completely.

        Install the fixture on the grinding machine.

      3. Grind the damaged outer diameter to the dimensions given in the figure.

      1. Hold outer diameter to a maximum value, but any previous plating and damage must be completely removed.

      2. Keep material removal to a minimum.

    3. SUBTASK 71-21-11-370-001 Stress Relieve the Engine Front Mount Tube Assembly

      1. Heat treat the part for one hour at 374 to 410 deg F (190 to 210 deg C).

      1. Use an Oven 1 off.

    4. SUBTASK 71-21-11-230-061 Examine the Engine Front Mount Tube Assembly for Cracks

      1. Fluorescent penetrant examine the repaired area.

      1. Refer to the SPM TASK 70-23-05-230-501.

    5. SUBTASK 71-21-11-220-009 Examine the Engine Front Mount Tube, Outer Diameter

    1. Refer to Figure.

    2. Measure the outer diameter of engine front mount tube.

    6. SUBTASK 71-21-11-330-002 Nickel Plate Engine Front Mount Tube, Outer Diameter

    1. Refer to Figure.

      2. Nickel plate the outer diameter of the engine front mount tube to the dimensions given in the figure.

      1. Refer to SPM TASK 70-33-06-330-503.

    7. SUBTASK 71-21-11-370-002 Heat Treat the Engine Front Mount Tube

      1. Heat treat part for one hour at 374 to 410 deg F (190 to 210 deg C).

      1. Use an Oven 1 off.

    8. SUBTASK 71-21-11-220-010 Examine the Engine Front Mount Tube, Outer Diameter after Plating

    1. Refer to Figure.

      2. Visually examine the nickel plate.

      1. Refer to the SPM TASK 70-33-06-300-503.

    3. Measure the dimension of the outer diameter.

    9. SUBTASK 71-21-11-320-001 Grind the Engine Front Mount Tube, Outer Diameter after Plating

    1. Refer to Figure.

      2. Install the fixture on the grinding machine.

    3. Grind the plated outer diameter to the dimensions given in the fixture.

    10. SUBTASK 71-21-11-220-011 Examine the Engine Front Mount Tube

    1. Refer to Figure.

      2. Visually examine and measure the dimensions of the outer diameter.

      1. Refer to TASK 71-21-11-200-000 (INSPECTION/CHECK-000).

    11. SUBTASK 71-21-11-350-006 Identify the Repair

      1. Mark VRS1075 adjacent to the part number.

      1. Refer to the SPM TASK 70-09-00-400-501.

      2. Use electrolytic marking equipment.

    12. SUBTASK 71-21-11-380-004 Apply the Dry Film Lubricant to the Engine Front Mount Tube Assembly

      1. Apply the dry film lubricant to the repaired area.

      1. Refer to VRS1101, TASK 71-21-11-300-004 (REPAIR-004).

    13. Figure: Repair details and dimensions (Before plating)

    Repair details and dimensions (Before plating)

    Figure: Repair details and dimensions (Plating)

    Repair details and dimensions (Plating)

    Figure: Repair details and dimensions (After plating)

    Repair details and dimensions (After plating)

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:0AM53
Tool Number:IAE 3J12857
Tool Name:IAE 3J12857 Grinding fixture
Manufacturer Code:LOCAL
Tool Number:Nickel Plate Equipment
Tool Name:Nickel Plate Equipment
Manufacturer Code:LOCAL
Tool Number:Oven
Tool Name:Oven
Link not Found
Manufacturer Code:LOCAL
Tool Number:Universal Grinder
Tool Name:Universal Grinder