TASK 71-52-43-200-402 EEC Core Harness And Voltage Divider Harness Assembly - Related Parts - Examine The EEC Harness Core Bracket, Inspection-002

DMC:V2500-A0-71-52-4300-01A-300A-C|Issue No:001.00|Issue Date:2014-05-01

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 71-52-43-200-402 EEC Core Harness And Voltage Divider Harness Assembly - Related Parts - Examine The EEC Harness Core Bracket, Inspection-002

Effectivity

FIG/ITEM

PART NO.

05-940

5W2166

General

NOTE

The consumable materials are given in the related SPM TASK.

This TASK gives the procedure for the inspection of the EEC harness-core bracket. For the other EEC harness-core parts, refer to Inspection/Check-000TASK 71-52-43-200-400 and Inspection-000 TASK 71-52-43-200-300 in the Component Maintenance Manual - Electrical Harnesses and Cables (CMM-EHC-V2500-1IA).

Fig./item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig./item numbers are used. For the service bulletin alpha variants refer to the IPC.

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

All the parts must be cleaned before any part is examined. Refer to the Cleaning-000 TASK 71-52-43-100-400.

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 the relevant SUBTASK. Do the test before the part is visually examined.

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 must 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 the repairs have been completed satisfactorily.

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

References

Refer to the SPM for data on these items:

Definitions of Damage - Specified Types of Damage, SPM TASK 70-02-02-350-501.

Inspection Policy and 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 71-52-43-230-051 Examine the Bracket for Cracks

    1. Clean the part. Refer to Cleaning-000 TASK 71-52-43-100-400.

      2. Do the test for cracks on the parts that are given below. Use the applicable penetrant procedure.

        1. Bracket (05-940). Refer to SPM TASK 70-23-00-230-501.

          1. Cracked

          1. Reject

    2. SUBTASK 71-52-43-220-065 Examine the Bracket

      1. Examine all the surfaces.

        1. Nicked, galled or scratched.

          1. To a depth of 0.002 in. (0.05 mm).

          1. Accept

          2. More than in Step.

          1. Reject

      2. Dented

        1. To a depth of 0.150 in. (3.8 mm).

        1. Accept

        2. More than in Step.

        1. Reject

    3. SUBTASK 71-52-43-220-066 Examine the Bracket Bolt Holes

      1. Worn

        1. If the width of the slotted bolt holes is less than 0.279 in. (7.08 mm) and the distance between the worn holes and the edge of the bracket is more than 0.066 in. (1.68 mm).

        1. Accept

        2. Other than in Step.

        1. Reject

Requirements After Job Completion

Follow-On Conditions

NONE