TASK 72-32-71-300-018 LPC Bleed Valve Support Ring - Replace The, Repair-018 (VRS1747)

DMC:V2500-A0-72-32-7121-01A-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 72-32-71-300-018 LPC Bleed Valve Support Ring - Replace The, Repair-018 (VRS1747)

Effectivity

FIG/ITEM

PART NO.

02-600

5A0463

02-600

5A1497

02-600

5A1639

Material of component

PART IDENT

SYMBOL

MATERIAL

Support ring assembly

-

Aluminum alloy

General

Price and availability - none

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-099 LINT-FREE CLOTHLOCALCoMat 02-099
CoMat 03-026 LIQUID NITROGENLOCALCoMat 03-026

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Pin5A049610

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-71-350-072 Remove the Damaged Pins

    1. Refer to Figure.

      2. Remove the damaged pin.

      1. Press out the damaged locating pins.

      2. Use hand tools.

    2. SUBTASK 72-32-71-220-134 Examine the Pin Holes of the Support Ring Assembly

    1. Refer to Figure.

      2. Visually examine the pin holes.

      1. Cracks, nicks, scratches and burrs are not permitted.

      2. Use 10X magnifying glass.

    3. Dimensionally examine the pin holes.

    3. SUBTASK 72-32-71-380-058 Apply the Surface Protection to the Support Ring Assembly

      1. Apply chromate conversion coating to the repaired surfaces, if necessary.

      1. Refer to the SPM TASK 70-38-02-300-503.

    4. SUBTASK 72-32-71-350-073 Install the New Pins to the Support Ring Assembly

    1. Refer to Figure.

      2. Clean the new pins and the pin holes.

      1. Use clean dry air blast or CoMat 02-099 LINT-FREE CLOTH.

      3. Freeze the new pins.

      4. Install the new pin.

      1. Press the pins into the pin holes.

      2. Use hand tools.

    5. SUBTASK 72-32-71-220-135 Examine the Pins of the Support Ring Assembly

    1. Refer to Figure.

      2. Visually and dimensionally examine the installed pins.

      1. Make sure the pin is installed in the support ring with no movement.

    6. Figure: Replace the Pins of the Support Ring Assembly

    Replace the Pins of the Support Ring Assembly

Requirements After Job Completion

Follow-On Conditions

NONE
Link not Found
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Manufacturer Code:X222X
Supply Number:CoMat 02-099
Type:sp01
Supply Short Name:CoMat 02-099 LINT-FREE CLOTH
Supply Name:CoMat 02-099 LINT-FREE CLOTH
Specification Groups:
Doc NumberType
WHERE COMAT 02-099 IS SPECIFIED WITH NO SUFFIX, USE COMAT 02-099A OR COMAT 02-099B.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:CoMat 03-026
Type:sp01
Supply Short Name:CoMat 03-026 LIQUID NITROGEN
Supply Name:CoMat 03-026 LIQUID NITROGEN
Specification Groups:
Doc NumberType
OMAT:220BB-N-411 T2GBC1
JCR-135BB-N-411 T2GBC1
Suppliers:
ManufacturerRemarks
LOCAL
U2046
U2096