TASK 72-45-14-840-001 HPT Stage 1 Blade - Rework The Blades, Rework-001 - SBE 72-0046

DMC:V2500-A0-72-45-1401-00A-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 72-45-14-840-001 HPT Stage 1 Blade - Rework The Blades, Rework-001 - SBE 72-0046

Effectivity

FIG/ITEM

PART NO.

01-010

2A1721

General

You must do the rework on the stage 1 HPT cooling duct assembly given in TASK 72-44-50-840-001, SBE 72-0046 - REWORK 001 at the same time you do the rework given in this procedure.

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

Refer to the indicated Service Bulletin for specific application requirements.

Repair facilities

The source Demonstration requirements of this rework means that any facility not authorized to accomplish this rework either utilize the Authorized Rework Vendors listed below or contact IAE Technical Services to determine if a qualification program can be initiated at their facility.

IAE-INTERNATIONAL AERO ENGINES AG
400 Main Street
East Hartford CT 06108
ATTN:  Director Technical Services

Authorized rework vendors for this bulletin are listed below:

CHROMALLOY RESEARCH AND TECHNOLOGY
CHROMALLOY AMERICAN CORPORATION
Blaisdell Road
Orangeburg, New York 10962 USA

The designation by IAE of an authorized rework vendor indicates that the vendor has demonstrated the necessary capability to enable it to carry out the rework. However, IAE makes no warranties or representations concerning the qualifications or quality standards of the vendors to carry out the rework, and accepts no responsibility whatsoever for any work that may be carried out by a vendor, other than when IAE is listed as the vendor. Authorized rework vendors do not act as agents or representatives of IAE.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-14-350-053 Rework the Stage 1 HPT Blades

      1. Send the blades to the approved rework vendor to do the modification and identification.

      1. Refer to Figure.

    2. SUBTASK 72-45-14-350-054 Identify the Reworked Stage 1 HPT Blades with the New Part Number

      1. Make sure the new part number is marked adjacent to the part number that was there before when the rework is completed.

      1. NUMBER BEFORE - 2A1721.

        NEW NUMBER - 2A2421.

    3. SUBTASK 72-45-14-350-055 Identify the 2A2321 Stage 1 Turbine Rotor Assembly

      1. Mark the new stage 1 turbine rotor assembly number adjacent to the number that was there before. Use the vibration peen method.

        1. NUMBER BEFORE - 2A2321.

          NEW NUMBER - 2A2521.

        1. Refer to procedure given in TASK 70-09-00-400-501.

    4. SUBTASK 72-45-14-350-056 Identify the 2A1621 Stage 1 Turbine Rotor Assembly

      1. Mark the new stage 1 turbine rotor assembly number adjacent to the number that was there before. Use the vibration peen method.

        1. NUMBER BEFORE - 2A1621.

          NEW NUMBER - 2A2721.

        1. Refer to procedure given in TASK 70-09-00-400-501.

    5. SUBTASK 72-45-14-350-057 Identify the 2A1021 Stage 1 Turbine Rotor Assembly

      1. Mark the new stage 1 turbine rotor assembly number adjacent to the number that was there before. Use the vibration peen method.

        1. NUMBER BEFORE - 2A1021.

          NEW NUMBER - 2A6321.

        1. Refer to procedure given in TASK 70-09-00-400-501.

    6. SUBTASK 72-45-14-350-058 Identify the 2A1921 Stage 1 Turbine Rotor Assembly

      1. Mark the new stage 1 turbine rotor assembly number adjacent to the number that was there before. Use the vibration peen method.

        1. NUMBER BEFORE - 2A1921.

          NEW NUMBER - 2A6421.

        1. Refer to procedure given in TASK 70-09-00-400-501.

    7. SUBTASK 72-45-14-350-059 Identify the 2A0400 Rotor and Stator Assembly

      1. NOTE

        Before you identify the rotor and stator assembly, you must rework the stage 1 HPT cooling duct assembly by the procedures given in TASK 72-44-50-840-001, SBE 72-0046 - Rework 001.

        Mark the new rotor and stator assembly number adjacent to the number that was there before. Use the vibration peen method.

        1. NUMBER BEFORE - 2A0400.

          NEW NUMBER - 2A1700.

        1. Refer to procedure given in TASK 70-09-00-400-501.

    8. SUBTASK 72-45-14-350-060 Identify the 2A1300 Rotor and Stator Assembly that Incorporates Service Bulletin V2500-ENG-72-0011

      1. NOTE

        Before you identify the rotor and stator assembly, you must rework the stage 1 HPT cooling duct assembly by the procedures given in TASK 72-44-50-840-001 SBE 72-0046 - Rework 001.

        Mark the new rotor and stator assembly number adjacent to the number that was there before. Use the vibration peen method.

        1. NUMBER BEFORE - 2A1300.

          NEW NUMBER - 2A5200.

        1. Refer to procedure given in TASK 70-09-00-400-501.

    9. SUBTASK 72-45-14-350-061 Identify the 2A1300 Rotor and Stator Assembly when Service Bulletin V2500-ENG-72-0011 is not Incorporated

      1. NOTE

        Before you identify the rotor and stator assembly, you must rework the stage 1 HPT cooling duct assembly by the procedures given in TASK 72-44-50-840-001, SBE 72-0046 - Rework 001.

        Mark the new rotor and stator assembly number adjacent to the number that was there before. Use the vibration peen method.

        1. NUMBER BEFORE - 2A1300.

          NEW NUMBER - 2A5100.

        1. Refer to procedure given in TASK 70-09-00-400-501.

    10. Figure: Rework of the stage 1 HPT blades

    Rework of the stage 1 HPT blades

Requirements After Job Completion

Follow-On Conditions

NONE