TASK 72-32-51-300-007 LP Rotor Center Shaft - Replace The Jacking Pad Pins, Repair-007 (VRS1278)

DMC:V2500-A0-72-32-5101-02A-920A-C|Issue No:001.00|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 72-32-51-300-007 LP Rotor Center Shaft - Replace The Jacking Pad Pins, Repair-007 (VRS1278)

Effectivity

FIG/ITEM

PART NO.

01-100

5R7016

General

This Repair TASK gives the procedure for replacing jacking pad pins.

Material of component

RR

DESCRIPTION

SYMBOL

MATERIAL

Shaft

Titanium alloy

Jacking pad pin

AMS5643

Corrosion resistance steel

Price and availability

Refer to IAE for any of the following:

Tools

Engine parts

Repair of spares

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

NOTE

Special tools are identified in the procedure by the tool primary number.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Hand pressLOCALHand press
IAE 3J13233 Installing fixture0AM53IAE 3J132331
IAE 3J13234 Removing fixture0AM53IAE 3J132341

Consumables, Materials and Expendables

NONE

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Jacking pad pin5R0375

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-51-350-058 Remove the Damaged Jacking Pad Pins (01-120)

    2. Refer to Figure.

      1. Remove the pins.

      2. Use IAE 3J13234 Removing fixture 1 off and hand press.

    1. SUBTASK 72-32-51-220-066 Examine the Shaft (01-100) Pin Location Holes

      1. Visually examine the pin location holes.

      2. Make sure that no dents and/or scratches exist.

    1. SUBTASK 72-32-51-350-059 Install the New Jacking Pad Pins (01-120)

    2. Refer to Figure.

      1. Install the new pins.

      2. Use IAE 3J13233 Installing fixture 1 off and hand press.

    1. SUBTASK 72-32-51-220-067 Examine the Repaired Areas

      1. Visually examine the repaired areas.

        1. Refer to TASK 72-32-51-200-000 (INSPECTION-000).

        2. Use 10X magnifying glass.

  1. Figure: Jacking pad pin

    Jacking pad pin

Requirements After Job Completion

Follow-On Conditions

NONE
Link not Found
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
Link not Found
Manufacturer Code:LOCAL
Tool Number:Hand press
Tool Name:Hand press
Manufacturer Code:0AM53
Tool Number:IAE 3J13233
Tool Name:IAE 3J13233 Installing fixture
Manufacturer Code:0AM53
Tool Number:IAE 3J13234
Tool Name:IAE 3J13234 Removing fixture