TASK 72-32-86-200-001-D00 Intermediate Structure Rear Fairing - Examine, Inspection-001

DMC:V2500-A0-72-32-8600-00D-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 72-32-86-200-001-D00 Intermediate Structure Rear Fairing - Examine, Inspection-001

Effectivity

FIG/ITEM

PART NO.

01-100

5A0833

General

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. Refer to TASK 72-32-86-100-000.

All the parts must be visualy 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 Step. 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 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 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 numbers are in the SPM.

References

Refer to the SPM for data on these items.

Definition of Damages, SPM TASK 70-02-02-350-501

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

Some data on these items are 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

NameManufacturerPart Number / IdentificationQuantityRemark
Fluorescent Penetrant Inspection EquipmentLOCALFluorescent penetrant inspection equipment

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-86-230-054 Examine the Rear Fairing Assembly (01-100) for Cracks

    1. Clean the parts. Refer to TASK 72-32-86-100-000.

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

        PART IDENT

        TASK/SUBTASK

        Rear fairing assembly

        1. Cracked

        1. Reject

    2. SUBTASK 72-32-86-220-070 Examine the Rear Fairing Assembly (01-100) Surface

    1. Refer to Figure.

      2. Examine the fairing surface at location 1.

        1. Dented.

          1. Up to 0.004 in. (0.10 mm) in depth

          1. Accept

          2. Between 0.004 and 0.008 in. (0.10 and 0.20 mm) in depth

          1. Repair, VRS1415 TASK 72-32-86-300-001 (REPAIR-001)

        2. Nicked.

          1. Up to 0.004 in. (0.10 mm) in depth

          1. Accept

          2. Between 0.004 and 0.008 in. (0.10 and 0.20 mm) in depth

          1. Repair, VRS1415 TASK 72-32-86-300-001 (REPAIR-001)

          3. More than 0.008 in. (0.20 mm) in depth

          1. Reject

    3. SUBTASK 72-32-86-220-071 Examine the Rear Fairing Assembly (01-100) Seal

    1. Refer to Figure.

      2. Examine the seal at location 2.

        1. Damaged.

          1. Torn

          1. Repair, VRS1416 TASK 72-32-86-300-002 (REPAIR-002)

          2. Unbonded

          1. Repair, VRS1416 TASK 72-32-86-300-002 (REPAIR-002)

          3. Missing

          1. Repair, VRS1416 TASK 72-32-86-300-002 (REPAIR-002)

    4. SUBTASK 72-32-86-220-072 Examine the Rear Fairing Assembly (01-100) Bolt Hole

    1. Refer to Figure.

      2. Examine the bolt hole at location 3.

        1. Nicked

        1. Repair, VRS1415 TASK 72-32-86-300-001 (REPAIR-002)

        2. Scratched

        1. Repair, VRS1415 TASK 72-32-86-300-001 (REPAIR-002)

        3. Burred

        1. Repair, VRS1415 TASK 72-32-86-300-001 (REPAIR-002)

    5. SUBTASK 72-32-86-220-073 Examine the Rear Fairing Assembly (01-100) Seating Face

    1. Refer to Figure.

      2. Examine the seating face at location 4.

        1. Galled

        1. Repair, VRS1415 TASK 72-32-86-300-001 (REPAIR-002)

    6. SUBTASK 72-32-86-220-074 Examine the Rear Fairing Assembly (01-100) Front End

    1. Refer to Figure.

      2. Examine the front end at location 5.

        1. Galled

        1. Repair, VRS1415 TASK 72-32-86-300-001 (REPAIR-002)

    7. SUBTASK 72-32-86-220-075 Examine the Rear Fairing Assembly (01-100) Nut

    1. Refer to Figure.

      2. Examine the nut at location 6.

        1. Loose

        1. Repair, VRS1410, TASK 72-32-86-300-004 (REPAIR-004)

    8. SUBTASK 72-32-86-220-076 Examine the Rear Fairing Assembly (01-100) Surface

    1. Refer to Figure.

      2. Examine all the surfaces which do not include the identified locations.

        1. Nicked or dented

        1. Repair, VRS1415, TASK 72-32-86-300-001 (REPAIR-001)

    9. Figure: Locations on the rear fairing assembly

    Locations on the rear fairing assembly

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Fluorescent penetrant inspection equipment
Tool Name:Fluorescent Penetrant Inspection Equipment