TASK 72-00-50-200-004 LPT Module - Brackets - Examine, Inspection-004

DMC:V2500-A0-72-00-5004-00A-300A-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 72-00-50-200-004 LPT Module - Brackets - Examine, Inspection-004

Effectivity

FIG/ITEM

PART NO.

01-330

5T8123

01-330

5T8100

01-330

6A6594

General

This TASK gives the procedure for the inspection of the brackets.

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 70-20-01-200-501.

All parts must be cleaned before any part is examined. Refer to TASK 72-00-50-100-000.

All parts must be visually examined for damage, corrosion and wear. Any defects that are not identified in the procedure must be referred to IAE.

The procedure for those parts which must have a crack test is given in Step. Do the test before the parts is visually examined. Limits for cracks are given in the SUBTASK for each part.

Do not discard any part until you are sure there are no repairs available. Refer to the instructions in the Repair before a discarded part is used again or oversize parts are installed.

Parts which should be discarded can be held although no repair is available. The repair of a discarded part could be shown to be necessary at a later date.

All parts must be examined to make sure that all repairs have been completed satisfactorily.

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

References

Refer to the SPM for the data on these items.

Definitions of damages, TASK 70-02-02-350-501

Inspection of parts, TASK 70-20-01-200-501

Some data on these items are 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 72-00-50-230-051 Examine the Brackets (01-330) for Cracks

    1. NOTE

      1. For the method to clean the parts, refer to the SPM TASK 70-11-01-300-503.

      Clean the parts.

      2. Do the test for cracks on the parts that are given below.

        PART IDENT

        TASK/OP

        Bracket

        Refer to the SPM TASK

        1. Cracked

        1. Reject

    2. SUBTASK 72-00-50-220-145 Examine the Brackets (01-330) Outer Surfaces

    1. Refer to Figure.

      2. Nicked

      1. Repair, VRS1114 TASK 72-00-50-300-006

      3. Dented

      1. Repair, VRS1114 TASK 72-00-50-300-006

      4. Scratched

      1. Repair, VRS1114 TASK 72-00-50-300-006

    3. SUBTASK 72-00-50-220-146 Examine the Brackets (01-330) Bolt Holes

    1. Refer to Figure.

      2. Worn.

        1. Less than replacement limits

        1. Accept

        2. More than replacement limits

        1. Reject

    4. Figure: Bolt holes

    Bolt holes

Requirements After Job Completion

Follow-On Conditions

NONE