TASK 72-40-00-200-016 Air Deflector Plate - Examine, Inspection-016

DMC:V2500-A0-72-40-0037-00A-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 72-40-00-200-016 Air Deflector Plate - Examine, Inspection-016

Effectivity

FIG/ITEM

PART NO.

01-075

6A3992

01-075

6A5911

01-075

6A7458

01-075

6A7459

General

This TASK gives the procedure for the inspection of the air deflector plate. For the other parts of the HP system module, refer to TASK 72-40-00-200-000.

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 parts must be cleaned before any part is examined. Refer to TASK 72-40-00-100-000.

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 Step. Do the test before the parts are visually examined. Limits for cracks are given in the SUBTASK for each part.

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 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 the data on these items.

Definitions of damage, 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

NONE

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-40-00-230-062 Examine the Plate (01-075) for Cracks

      1. Clean the parts.

      2. Do the test for cracks on the parts that are given below.

        PART IDENT

        TASK/OP

        Plate

        1. Cracked

        1. Reject

    2. SUBTASK 72-40-00-220-150 Examine the Plate Surface (01-075) for Damage

      1. Scored.

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

        1. Accept

        2. More than in Step

        1. Repair, VRS1469 TASK 72-40-00-300-003

      2. Dented.

        1. Up to 0.010 in. (0.25 mm) in depth and 0.50 in. (12.7 mm) in diameter

        1. Accept

        2. More than in Step

        1. Repair, VRS1469 TASK 72-40-00-300-003

      3. Nicked.

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

        1. Accept

        2. More than in Step

        1. Repair, VRS1469 TASK 72-40-00-300-003

      4. Galled.

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

        1. Accept

        2. More than in Step

        1. Repair, VRS1469 TASK 72-40-00-300-003

      5. Distorted or bent

      1. Reject

    3. SUBTASK 72-40-00-220-151 Examine the Plate (01-075) Bolt Holes

      1. Examine the three mounting flange bolt holes, nominal diameter 0.354 in. (8.98mm) for wear.

        1. Within replacement limits of 0.371 in. (9.41mm)

        1. Accept

        2. More than replacement limits

        1. Reject

      2. Examine the two cooling air deflector bracket bolt holes, nominal diameter 0.226 in. (5.75mm) for wear.

        1. Within replacement limits of 0.242 in. (6.15mm)

        1. Accept

        2. More than replacement limits

        1. Reject

Requirements After Job Completion

Follow-On Conditions

NONE