TASK 75-32-54-200-401 HPC Stage 10 Bleed Valve - Related Parts - Examine The Bracket, Inspection-001

DMC:V2500-A0-75-32-5400-00A-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 75-32-54-200-401 HPC Stage 10 Bleed Valve - Related Parts - Examine The Bracket, Inspection-001

Effectivity

FIG/ITEM

PART NO.

01-398

5W8307

General

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

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

The policy that is necessary for inspection is given in the SPM TASK 70-20-01-200-501.

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.

Do not discard any part until you are sure there are no repairs available. Refer to the instructions in 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 SPM for data on these items:

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

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 75-32-54-230-053 Examine the Bracket (01-398) for Cracks

    1. Clean the Part. Refer to Cleaning-001 TASK 75-32-54-100-401.

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

        1. Bracket. Refer to SPM TASK 70-23-01-230-501.

          1. Cracked

          1. Reject

    2. SUBTASK 75-32-54-220-060 Examine the Bracket (01-398) Bolt Holes

    1. Refer to Figure.

      2. Worn

        1. The worn hole is less than 1.2 times of nominal diameter and the distance between the worn hole and the edge of bracket is more than 0.066 in. (1.68 mm).

        1. Accept

        2. Other than in Step.

        1. Reject

    3. Figure: Bracket

    Bracket

Requirements After Job Completion

Follow-On Conditions

NONE