TASK 72-45-22-840-001 HPT Stage 1 Duct Support Segment - Provide A Turbine Case And Vane Assembly That Will Allow Individual Segment Replacement, Rework-001 - SBE 72-0092

DMC:V2500-A0-72-45-2200-00A-933A-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 72-45-22-840-001 HPT Stage 1 Duct Support Segment - Provide A Turbine Case And Vane Assembly That Will Allow Individual Segment Replacement, Rework-001 - SBE 72-0092

Effectivity

FIG/ITEM

PART NO.

01-010

2A0177

General

The practices and procedures referred to in the procedure by the TASK number are in the SPM.

Refer to the indicated Service Bulletin for specific application requirements.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
IAE 3P16273 Grind fixture0AM53IAE 3P162731

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-22-220-064 Examine the Stage 1 Duct Support Assembly

      1. Examine each segment for Dimension L.

      1. Refer to Figure and Figure requirements.

      2. If the duct segment is in the limit, mark the new part number adjacent to the part number that was there before.

      1. NUMBER BEFORE: 2A0178.

        NEW NUMBER: 2A1313.

        Refer to Figure requirements.

        Do the procedure given in the SPM TASK 70-09-00-400-501 and use the vibration peen method.

    3. If the duct segment is not in the limit, do the rework.

    2. SUBTASK 72-45-22-320-054 Machine the Duct Segment

      1. Set-up and machine Surface B to get Dimension K.

      1. Refer to Figure requirements.

        Remove the minimum amount of material and keep the maximum material thickness.

    3. SUBTASK 72-45-22-340-053 Coat the Duct Segment

      1. Coat the duct segment to get a 0.002 to 0.008in. (0.051 to 0.203 mm) thickness after the finish machining.

      1. Refer to Figure requirements.

        Do the procedure given in the SPM TASK 70-34-03-340-501.

        No coating is permitted in the holes.

    4. SUBTASK 72-45-22-320-055 Finish Machine the Duct Segment

      1. Set-up and finish machine the duct segment coating.

      1. Refer to Figure requirements.

    5. SUBTASK 72-45-22-350-059 Identify the Duct Segment

      1. Mark the new part number adjacent to the part number that was there before.

      1. NUMBER BEFORE: 2A0178.

        NEW NUMBER: 2A1313.

        Refer to Figure requirements.

        Do the procedure given in the SPM TASK 70-09-00-400-501 and use the vibration peen method.

    6. SUBTASK 72-45-22-440-051 Assemble the Turbine Case and Vane Assembly

      1. Install the 2A1313 stage 1 HPC duct support assemblies (19 off) in the turbine case and vane assembly.

      1. Do the procedure given in TASK 72-45-20-440-001.

    7. SUBTASK 72-45-22-350-060 Identify the New Turbine Case and Vane Assembly

      1. Mark the new part number adjacent to the part number that was there before.

      1. NUMBER BEFORE: 2A1357.

        NEW NUMBER: 2A1764.

        Refer to Figure requirements.

        Do the procedure given in the SPM TASK 70-09-00-400-501 and use the vibration peen method.

    8. Figure: Location of the stage 1 HPT duct support assembly

    Location of the stage 1 HPT duct support assembly

    Figure: Modification of the stage 1 duct support assembly

    Modification of the stage 1 duct support assembly

    Figure: Modification of the stage 1 duct support assembly

    Modification of the stage 1 duct support assembly

Requirements After Job Completion

Follow-On Conditions

NONE
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:0AM53
Tool Number:IAE 3P16273
Tool Name:IAE 3P16273 Grind fixture