TASK 72-32-71-300-022 LPC Bleed Valve Support Ring - Repair The Worn Stud Pin Holes By Bush, Repair-022 (VRS1358)

DMC:V2500-A0-72-32-7121-00A-664A-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 72-32-71-300-022 LPC Bleed Valve Support Ring - Repair The Worn Stud Pin Holes By Bush, Repair-022 (VRS1358)

Effectivity

FIG/ITEM

PART NO.

01-600

5A0950

01-600

5A3703

Material of component

PART IDENT

SYMBOL

MATERIAL

Support ring

Aluminum alloy

General

Price and availability - none

The practices and processes referred to in the procedure by TASK/SUBTASK 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
Standard workshop equipmentLOCALStandard workshop equipment
Horizontal boring millLOCALHorizontal boring mill
Rotary tableLOCALRotary table
Penetrant Crack Test EquipmentLOCALPenetrant crack test equipment
Bore gageLOCALBore gage
Depth gage micrometerLOCALDepth gage micrometer
OvenLOCALOven
Vibrating marking pencilLOCALVibrating marking pencil
Dial set indicatorLOCALDial set indicator
Heat protection glovesLOCALHeat protection gloves
IAE 3J12747 Assembly fixture0AM53IAE 3J127471

Consumables, Materials and Expendables

NONE

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Bushing5A1797AR
Bushing5A1798AR

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-71-320-051 Machine the Worn Stud Pin Hole(s) on the Support Ring Assembly

    1. Refer to Figure, Figure, Figure and Figure.

      2. Set a rotary table on to the horizontal boring machine.

      3. Put the assembly fixture on to the boring machine.

      4. Set the assembly fixture by plane B, diameter D and surface E.

      2. Make sure the datum B and D are set to locate correctly.

    5. Install and clamp the support ring into the assembly fixture.

      6. Machine the worn stud pin hole.

      7. Remove sharp edge.

    8. Remove the support ring from the assembly fixture.

    2. SUBTASK 72-32-71-220-139 Examine the Machined Stud Pin Hole(s)

    1. Refer to Figure and Figure.

      2. Measure the dimensions of the stud pin hole(s) on the support ring.

      1. Use bore gage.

    3. SUBTASK 72-32-71-230-079 Examine the Machined Stud Pin Hole(s) of the Support Ring for Cracks

      1. Do a penetrant crack test on the machined hole(s).

      1. No cracks are permitted.

      2. Refer to the SPM TASK 70-23-02-230-501.

    4. SUBTASK 72-32-71-330-054 Apply the Chromate Conversion Coating to the Support Ring

      1. Apply the chromate conversion coating to the machined stud pin hole(s).

      1. Refer to the SPM TASK 70-38-02-300-503, SUBTASK 70-38-02-300-002.

    5. SUBTASK 72-32-71-350-076 Install Bush(es) (01-690 and/or 01-700) to the Support Ring

    1. Refer to Figure and Figure.

      2. Heat the support ring at 230 to 302 deg F (110 to 150 deg C) for one hour.

      1. Use an Oven.

      3. Install the bush(es) to the support ring.

        1. Use 5A1797 bushing, 01-690 and/or 5A1798 bushing 01-700.

    6. SUBTASK 72-32-71-220-140 Examine the Bush(es) for Location

    1. Refer to Figure and Figure.

      2. Visually examine the bush(es) for location.

      1. Make sure the bush(es) are pushed fully into positions.

    7. SUBTASK 72-32-71-350-077 Identify the Repair

    1. Make a mark VRS1358 adjacent to the part number.

    2. Refer to the SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      3. Apply the chromate conversion coating to the marked letter.

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

    8. Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

Requirements After Job Completion

Follow-On Conditions

NONE
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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
Link not Found
Link not Found
Manufacturer Code:LOCAL
Tool Number:Depth gage micrometer
Tool Name:Depth gage micrometer
Manufacturer Code:LOCAL
Tool Number:Dial set indicator
Tool Name:Dial set indicator
Manufacturer Code:LOCAL
Tool Number:Heat protection gloves
Tool Name:Heat protection gloves
Link not Found
Manufacturer Code:0AM53
Tool Number:IAE 3J12747
Tool Name:IAE 3J12747 Assembly fixture
Manufacturer Code:LOCAL
Tool Number:Oven
Tool Name:Oven
Manufacturer Code:LOCAL
Tool Number:Penetrant crack test equipment
Tool Name:Penetrant Crack Test Equipment
Manufacturer Code:LOCAL
Tool Number:Rotary table
Tool Name:Rotary table
Link not Found
Link not Found