TASK 72-32-51-300-026 Front Seal Runner Ring - Replace The Self Locking Shank Nuts, Repair-026 (VRS1857)

DMC:V2500-A0-72-32-5102-01A-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 72-32-51-300-026 Front Seal Runner Ring - Replace The Self Locking Shank Nuts, Repair-026 (VRS1857)

Effectivity

FIG/ITEM

PART NO.

01-200

5R0068

Material of component

RR

DESCRIPTION

SYMBOL

MATERIAL

Ring, A/O Nut

12Cr-2Ni-2Mo-0.3V Steel

General

Price and Availability

Refer to IAE for any of the followings:

Tools

Engine parts

Repair of spares

This repair TASK gives the procedure for replacing the self locking shank nuts.

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Hand pressLOCALHand press
IAE 3J13235 Fixture, Peening0AM53IAE 3J132351

Consumables, Materials and Expendables

NONE

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Nut, self locking shankAS2787024

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-51-350-074 Remove the Damaged Self Locking Shank Nuts (01-210)

      1. Remove the damaged self locking shank nuts.

      2. Refer to the SPM TASK 70-35-11-300-501.

    1. SUBTASK 72-32-51-220-158 Examine the Nut Ring (01-200) Nut Location Holes

      1. Visually examine the nut location holes.

      2. Make sure that no dents or nicks exist.

    1. SUBTASK 72-32-51-350-075 Install the New Self Locking Shank Nuts (01-210)

      1. Install new self locking shank nuts.

      2. Refer to the SPM TASK 70-35-11-300-501.

      3. Use IAE 3J13235 Fixture, Peening 1 off and a hand press.

    2. Visually examine the silver coating inside of the shank for loose flakes of the silver coating and remove the flakes using cloth.

    1. SUBTASK 72-32-51-220-159 Examine the Nut Ring (01-200)

      1. Visually examine the repaired areas.

      2. Use 10X magnifying glass.

      3. Make sure that no nicks, burrs or scores exist.

  1. Figure: Replace the self locking nut

    Replace the self locking nut

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 3J13235
Tool Name:IAE 3J13235 Fixture, Peening