TASK 72-45-11-200-002 HPT Stage 1 Hub - Examine The Stage 1 Turbine Hub, Inspection-002

DMC:V2500-A0-72-45-1100-02A-300A-C|Issue No:003.00|Issue Date:2015-05-01

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 72-45-11-200-002 HPT Stage 1 Hub - Examine The Stage 1 Turbine Hub, Inspection-002

Effectivity

All Stage 1 Turbine Hubs.

General

This TASK gives the procedure for the inspection of the Stage 1 Turbine Hub for cracks in the critical areas.

Fig/Item numbers in parentheses in the procedure agree with those used in the IPC.

The policy that is necessary for inspection is given in the SPM TASK 70-20-00-200-501.

All parts must be cleaned before any part is examined. Refer to the SPMTASK 72-45-11-100-000 (CLEANING-000).

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

References

Refer to the SPM for data on these items.

Definition of Damage, SPM TASK 70-02-02-350-501

Record and Control of Lives of Parts, SPM TASK 70-05-00-220-501.

Marking of Parts, SPM TASK 70-09-00-400-501.

Inspection of Parts, SPM TASK 70-20-00-200-501.

Some data on these items is contained in this TASK. For more data on these items refer to the SPM.

Method of Testing for Crack Indications.

Chemical Processes.

Surface Protection.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-11-230-060 Examine the Stage 1 Turbine Hub (01-011) for Cracks

    1. Refer to Figure.

    2. Clean the Part. Refer to TASK 72-45-11-100-000(CLEANING-000).

      3. Do the test for cracks on the part that is given below. Use the applicable penetrant procedure.

        NOTE

        Make sure you check the important areas for cracks, when you inspect the hub. These areas are shown in Figure.

        PART IDENT/SUBTASK

        Stage 1 turbine hub

        (Dip or Spray)

        1. Cracked

        1. Reject

    2. Figure: Stage 1 Turbine Hub Important FPI Inspection Locations

    Stage 1 Turbine Hub Important FPI Inspection Locations

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised format. (editorial change)