TASK 75-00-49-300-009 Engine Air Off-Take Air Ducts - Replace The Insert, Repair-009 (VRS6234)

DMC:V2500-A0-75-00-4901-00A-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 75-00-49-300-009 Engine Air Off-Take Air Ducts - Replace The Insert, Repair-009 (VRS6234)

Effectivity

FIG/ITEM

PART NO.

01-250

6A2290

Material of component

DESCRIPTION

SYMBOL

MATERIAL

HP compressor stage 7 bleed valve and cabin air duct assembly

TDN

Titanium alloy

General

Price and availability

Refer to International Aero Engines AG.

This TASK replaces damaged wire thread inserts in the HP compressor stage 7 bleed valve and cabin air duct assembly.

NOTE

Consumable materials necessary to do this Repair are given in SPM TASK 70-35-08-300-501

NOTE

Special tools necessary to do this Repair are given in SPM TASK 70-35-08-300-501

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NONE

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Screw lock helicoil insertLOCALAGS 3732

FIG/ITEM 01-262

Safety Requirements

NONE

Procedure

    1. SUBTASK 75-00-49-350-055 Remove the Damaged Helicoil Insert

    1. Refer to Figure.

      2. Remove the damaged helicoil insert

      1. Refer to SPM TASK 70-35-08-300-501.

    2. SUBTASK 75-00-49-350-056 Install the helicoil Insert

    1. Refer to Figure.

      2. Install the helicoil insert

      1. Refer to SPM TASK 70-35-08-300-501.

    3. SUBTASK 75-00-49-230-059-001 Do a Crack Test

      1. Do a crack test on the repaired area

      1. Refer to SPM TASK 70-23-01-230-501.

    4. SUBTASK 75-00-49-230-059-002 Do a Crack Test

      1. Do a crack test of the repaired area

      1. Refer to SPM TASK 70-23-03-230-501.

    5. SUBTASK 75-00-49-220-067 Do an Inspection of the Helicoil Insert

      1. Do an inspection of the helicoil insert

      1. Refer to SPM TASK 70-35-08-300-501.

    6. Figure: Helicoil Insert Location

    Helicoil Insert Location

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
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