TASK 72-00-40-200-003 HP System Module - Attaching Parts And Fittings - Examine, Inspection-003

DMC:V2500-A0-72-00-4002-00A-310A-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 72-00-40-200-003 HP System Module - Attaching Parts And Fittings - Examine, Inspection-003

Effectivity

FIG/ITEM

PART NO.

01-030

4W0003

01-050

BLT5654

01-080

5A1233

01-082

5A1232

General

This TASK gives the procedure for the inspection of the HP system module attaching parts and fittings. Refer to TASK 72-00-40-200-000 for more inspection procedures.

Fig/item numbers in parentheses in the procedure agree with those used in the EIPC. Only the primary Fig/item numbers are used. For the Service Bulletin alpha variants refer to the EIPC.

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

All the parts must be cleaned before any part is examined.

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.

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 can be shown to be necessary at a subsequent date.

All the 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.

References

Refer to the SPM for data on these items.

Definition of Damage TASK 70-02-02-350-501

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

Some data on these items is contained in this TASK. For more data on these items refer to the SPM.

Methods 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 72-00-40-220-132 Examine the Bolts (01-050)

      1. Stripped threads

      1. Reject

      2. Crossed threads

      1. Reject

      3. Pick-up on the threads

      1. Reject

      4. Burred on the head

      1. Reject

      5. Threads that are not there

      1. Reject

      6. Examine the bolt length.

        1. Bent

        1. Reject

      7. Examine the plain shank diameter.

        1. Worn.

        1. If the diameter is between 0.309 in. and 0.312 in. (7.85 and 7.92 mm)

        2. Accept

        3. Less than 0.309 in. (7.85 mm)

        4. Reject

        2. Galled

        1. Reject

    2. SUBTASK 72-00-40-220-133 Examine the Plate (01-080)

      1. Scored

      1. Reject

      2. Bent

      1. Reject

      3. Elongated hole

      1. Reject

      4. Bolt hole.

        1. Hole diameter less than 0.369 in. (9.36 mm)

        1. Accept

        2. More than in Step

        1. Reject

      5. Pin slot width.

        1. Less than 0.169 in. (4.30 mm)

        1. Accept

        2. More than in Step

        1. Reject

    3. SUBTASK 72-00-40-220-134 Examine the Pins (01-082)

      1. Burred

      1. Reject

      2. Scored

      1. Reject

      3. Pin diameter.

        1. More than 0.237 in.(6.01 mm)

        1. Accept

        2. Less than in Step

        1. Reject

      4. Plate location diameter.

        1. More than 0.143 in. (3.64 mm)

        1. Accept

        2. Less than in Step

        1. Reject

    4. SUBTASK 72-00-40-220-135 Examine the Nuts (01-030)

      1. Stripped threads

      1. Reject

      2. Crossed threads

      1. Reject

      3. Pick-up on the threads

      1. Reject

      4. Burred on the head

      1. Reject

      5. Threads that are not there

      1. Reject

      6. Self-locking torque.

        1. Within limits given in TASK 70-41-02-410-501

        1. Accept

        2. Other than in Step

        1. Reject

Requirements After Job Completion

Follow-On Conditions

NONE