TASK 71-51-41-200-402 EEC Fan Harness - Related Parts - Examine The Fan EEC Harness Bracket Remaining Parts, Inspection-002

DMC:V2500-A0-71-51-4100-02A-310A-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 71-51-41-200-402 EEC Fan Harness - Related Parts - Examine The Fan EEC Harness Bracket Remaining Parts, Inspection-002

Effectivity

FIG/ITEM

PART NO.

05-821

4W0002

05-824

4W0164

05-841

4W0002

05-844

4W0164

05-851

4W0002

05-854

4W0164

05-871

4W0002

05-874

4W0164

05-881

4W0002

05-884

4W0164

05-891

4W0002

05-894

4W0165

05-911

4W0002

05-914

4W0165

05-921

4W0002

05-924

4W0164

05-944

4W0102

05-991

4W0002

05-994

4W0164

06-567

4W0164

06-569

4W0002

General

This TASK gives the procedure for the inspection of the fan EEC harness bracket remaining parts. For the other fan EEC harness parts refer to Inspection-000 TASK 71-51-41-200-400 and TASK 71-51-41-200-300 in the Component Maintenance Manual (CMM-EHC-V2500-1IA).

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

All the parts must be cleaned before they are examined. Refer to the Cleaning-000 TASK 71-51-41-100-400.

All the 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 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, 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 71-51-41-220-066 Examine the Bolts

      1. Threads

        1. Crossed

        1. Reject

        2. Stripped

        1. Reject

        3. Missing

        1. Reject

        4. Worn

        1. Refer to SPM TASK 70-42-01-400-501.

      2. Surfaces

        1. Nicked

          1. Nicked to a depth of 0.002 in. (0.05 mm).

          1. Accept

          2. More than in Step.

          1. Reject

      3. Head

        1. Burred

          1. Burred but with no decrease in function.

          1. Accept

          2. More than in Step.

          1. Reject

    2. SUBTASK 71-51-41-220-067 Examine the Self-Locking Nuts

      1. Threads

        1. Crossed

        1. Reject

        2. Stripped

        1. Reject

        3. Missing

        1. Reject

        4. Worn

        1. Refer to SPM TASK 70-42-01-400-501.

      2. Surfaces

        1. Burred/nicked.

          1. Burred/nicked but with no decrease in function.

          1. Accept

          2. In excess of Step.

          1. Reject

Requirements After Job Completion

Follow-On Conditions

NONE