TASK 72-45-11-300-015 HPT Stage 1 Hub - Machine Repair The Hub Axial Length, Repair-015 (VRS3508)

DMC:V2500-A0-72-45-1100-04A-659A-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 72-45-11-300-015 HPT Stage 1 Hub - Machine Repair The Hub Axial Length, Repair-015 (VRS3508)

Effectivity

FIG/ITEM PART NO.

01-010

2A2021

Material of component

PART IDENT

SYMBOL

MATERIAL

Stage 1 turbine hub

-

Nickel alloy

General

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

Price and availability - not applicable

Repair Facilities

The Source Demonstration requirements of this repair means that any facility not authorized to accomplish this repair either utilize the Authorized Repair Vendors listed below or contact IAE Repair Development Group to determine if a qualification program can be initiated at their facility.

IAE - INTERNATIONAL AERO ENGINES AG
400 Main Street
East Hartford
CT 06108 USA
Attn:  Manager Repair Development

Authorized Repair Vendors for Repair VRS3508 are listed below:

Pratt and Whitney Aftermarket Services (PWAS)
East Hartford Engine and Component Center
Rotating Parts
400 Main Street, Well 14
East Hartford, CT 06108-0969
USA
Tel: (860) 565-4579
Fax: (860) 565-0349

Turbine Component Repair
Caval Tool Division
655 New Britain Ave
Newington, CT 06131 USA

MTU-Maintenance GmbH
Airport Hannover
Munchner Strasse 31
30855 Langenhagen, Germany

Ishikawajima - Harima Heavy Industries Co., Ltd.
Mizuho - Machi
Nishitama - Gun
Tokyo 190 -12
JAPAN
Attn:  Program Manager, V2500

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Machining equipmentLOCALMachining equipment
Standard inspection equipmentLOCALStandard inspection equipment

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

CAUTION

USE THIS REPAIR FOR THE DAMAGED PARTS WHICH HAVE LESS THAN THEIR LIFE CYCLE LIMIT. THIS REPAIR WILL NOT EXTEND THE LIFE CYCLE. DO NOT REPAIR THE TURBINE HUB THAT HAS A CRACK OR AN INDICATION THAT IS NOT CLEARLY THE RESULT OF LOCAL DAMAGE SUCH AS DENTS, NICKS, SCRATCHES AND CORROSION PITS. IF CRACKS OR OTHER UNUSUAL CONDITIONS ARE FOUND BY THE PENETRANT TEST OR VISUAL INSPECTION, REJECT THE PART.

Procedure

    1. SUBTASK 72-45-11-320-055 Machine the Hub Axial Length

      1. Set-up and machine the hub end surface to 2.557in. (64.948 mm) minimum length to remove the damage.

      2. Refer to Figure.

      1. Machine the chamfer to 0.030 to 0.050in. (0.76 to 1.27 mm) by 40 to 50 degrees.

      2. Refer to Figure.

      1. Machine the chamfer to 0.015 to 0.035in. (0.38 to 0.89 mm) by 40 to 50 degrees.

      2. Refer to Figure.

    1. SUBTASK 72-45-11-220-088 Examine the Repair Area

      1. Examine the repaired surface.

      2. Refer to Figure.

    1. SUBTASK 72-45-11-350-057 Identify the Repair

      1. Mark VRS3508 adjacent to the part number.

      2. Make a permanent mark by the procedures given in the SPM TASK 70-09-00-400-501.

        Use the vibration peen method.

  1. Figure: Stage 1 turbine hub machine repair areas

    Stage 1 turbine hub machine repair areas

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Machining equipment
Tool Name:Machining equipment
Manufacturer Code:LOCAL
Tool Number:Standard inspection equipment
Tool Name:Standard inspection equipment