TASK 71-52-43-200-401 EEC Core Harness And Voltage Divider Harness Assembly - Related Parts - Examine The EEC Harness-Core Raceways, Inspection-001

DMC:V2500-A0-71-52-4300-00A-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 71-52-43-200-401 EEC Core Harness And Voltage Divider Harness Assembly - Related Parts - Examine The EEC Harness-Core Raceways, Inspection-001

Effectivity

FIG./ITEM

PART NO.

05-100

5W2176

05-100

5W2556

General

This TASK gives the procedure for the inspection of the EEC harness-core raceway. For the other EEC harness-core parts, refer to Inspection-000 TASK 71-52-43-200-400 and Inspection-000 TASK 71-52-43-200-300.

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

A ** following repair referenced in this inspection indicates that the repair is not yet published in the current revision of the manual and the part must be rejected. Contact IAE for additional information concerning FAA approved repair date.

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 number are in the SPM.

NOTE

The consumable materials are given in the related SPM TASK.

References

Refer to the SPM for data on these items.

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 71-52-43-230-054 Examine the Raceway for Cracks

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

      2. Do the crack test on the parts that are given below. Use the applicable penetrant inspection procedure.

      1. Raceway (05-100). Refer to SPM TASK 70-23-00-230-501.

        2. Cracked

        1. Reject

    2. SUBTASK 71-52-43-220-070 Examine the Surfaces of the Raceway

    1. Refer to Figure.

      2. Distorted

        1. With no decrease in function.

        1. Accept

        2. Limits more than Step

        1. Reject

      3. Nicked, scratched or scored.

        1. Up to 0.002 in. (0.05 mm) in depth.

        1. Accept

        2. Limits more than Step

        1. Repair, VRS7001 (REPAIR-001) TASK 70-35-24-300-501.

    3. SUBTASK 71-52-43-220-071 Examine the Raceway Clips

    1. Refer to Figure.

      2. Cracked or damaged.

      1. Repair, VRS7001 (REPAIR-001) TASK 70-35-24-300-501.

      3. Bent or distorted.

      1. Repair, VRS7001 (REPAIR-001) TASK 70-35-24-300-501.

    4. SUBTASK 71-52-43-220-058 Examine the Raceway Bolt Holes at Location 1 Detail A

    1. Refer to Figure.

      2. Worn

        1. The distance between edge and worn hole is not less than 0.05 in. (1.27 mm).

        1. Accept

        2. Less than 0.05 in. (1.27 mm)

        1. Repair, VRS7001 (REPAIR-001) TASK 70-35-24-300-501.

      3. Burred

      1. Repair, VRS7001 (REPAIR-001) TASK 70-35-24-300-501.

    5. Figure: Inspection of the Raceway

    Inspection of the Raceway

Requirements After Job Completion

Follow-On Conditions

NONE