TASK 73-13-41-200-401 Fuel Nozzle And Support Assembly - Related Parts - Examine The Brackets, Inspection-001

DMC:V2500-A0-73-13-4100-01A-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 73-13-41-200-401 Fuel Nozzle And Support Assembly - Related Parts - Examine The Brackets, Inspection-001

Effectivity

FIG./ITEM

PART NO.

01-120

2A1466

01-120

6A6559

01-120

6A7452

01-180

2A1436

01-180

6A6558

01-340

2A1479

01-340

6A6557

01-400

2A1488

01-400

6A6556

01-400

6A7453

General

This TASK gives the procedure for the inspection of the brackets. For the other fuel nozzle parts, refer to Inspection-000 TASK 73-13-41-200-400.

Fig/item numbers in parentheses in the procedure agree with those used in the IPC.

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 Cleaning-000 TASK 73-13-41-100-200.

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.

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 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 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.

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

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 73-13-41-220-063 Examine the Brackets (01-120, 01-180, 01-340 and 01-400) Surfaces

    1. Refer to Figure.

      2. Examine all the surfaces.

        1. Cracked

        1. Reject

        2. Nicked

          1. Any nicks

          1. Repair, VRS1642 (Repair-001) TASK 73-13-41-300-001.

        3. Dented

          1. Any dents

          1. Repair, VRS1642 (Repair-001) TASK 73-13-41-300-001.

        4. Scratched

          1. Any scratches

          1. Repair, VRS1642 (Repair-001) TASK 73-13-41-300-001.

    2. SUBTASK 73-13-41-220-064 Examine the Brackets (01-120, 01-180, 01-340 and 01-400) Bolt Holes

    1. Refer to Figure.

      2. Examine the bolt holes at location 1.

        1. Worn

          1. Less than 0.36 in. (9.144 mm) in diameter of the worn holes.

          1. Accept

          2. More than in Step.

          1. Reject

    3. Figure: Inspection of the Bracket

    Inspection of the Bracket

Requirements After Job Completion

Follow-On Conditions

NONE