TASK 75-24-49-200-101-B00 LPT ACC Connector Air Tube - Examine, Inspection-001

DMC:V2500-A0-75-24-4901-00C-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 75-24-49-200-101-B00 LPT ACC Connector Air Tube - Examine, Inspection-001

Effectivity

FIG/ITEM

PART NO.

01-010

3A2316

01-010

3A2335

General

This TASK gives the procedure for the inspection of the connector tube of the ACC.

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 SPM TASK 70-20-00-200-501.

All parts must be cleaned before any part is examined. Refer to Cleaning-000 TASK 75-24-49-100-100.

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 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 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.

Definitions of Damage, SPM TASK 70-02-02-350-501.

Record and Control of the Lives of Parts, SPM TASK 70-05-00-220-501.

Inspection of Parts, SPM TASK 70-20-00-200-501.

Some data on these items is 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 75-24-49-230-160 Examine the Connector Tube for Cracks

    1. Clean the parts. Refer to Cleaning-000 TASK 75-24-49-100-100.

      2. Do the test for cracks on the part that is given below. Use the applicable penetrant procedure.

        1. Connector Tube. Refer to SPM TASK 70-23-02-230-501.

          1. Cracked

          1. Repair, VRS4358 (Repair-027) TASK 75-24-49-300-027.

    2. SUBTASK 75-24-49-220-219 Examine the Connector Tube for Surface Damage

    1. Refer to Figure.

      2. Examine the surface in all areas.

        1. Nicked

          1. Not more than 0.005 in. (0.13 mm) maximum depth, no raised material.

          1. Accept

          2. Not more than 0.005 in. (0.13 mm) maximum depth, with raised material.

          1. Repair, VRS4359 (Repair-028) TASK 75-24-49-300-028.

          3. More than in Step.

          1. Repair, VRS4358 (Repair-027) TASK 75-24-49-300-027.

        2. Dented

          1. Not more than 0.015 in. (0.38 mm) maximum depth without deterioration to assembly or function.

          1. Accept

          2. More than in Step with deterioration to assembly or function.

          1. Reject

    3. SUBTASK 75-24-49-220-220 Examine the Connector Tube for Wear

    1. Refer to Figure.

      2. Examine the surface in area A1.

        1. Fretted

          1. Not more than 0.003 in. (0.08 mm) maximum depth on 25 percent of surface, no raised material.

          1. Accept

          2. Not more than 0.003 in. (0.08 mm) maximum depth on 25 percent of surface, with raised material.

          1. Repair, VRS4359 (Repair-028) TASK 75-24-49-300-028.

          3. More than in Step.

          1. Repair, VRS4478 (Repair-047) TASK 75-24-49-300-047.

      3. Examine the surface in area A2.

        1. Fretted

          1. Not more than 0.003 in. (0.08 mm) maximum depth on 25 percent of surface, no raised material.

          1. Accept

          2. Not more than 0.003 in. (0.08 mm) maximum depth on 25 percent of surface, with raised material.

          1. Repair, VRS4359 (Repair-028) TASK 75-24-49-300-028.

          3. More than in Step.

          1. Reject

      4. Examine the surface in area A3.

        1. Fretted

          1. Not more than 0.005 in. (0.13 mm) maximum depth, no raised material.

          1. Accept

          2. Not more than 0.005 in. (0.13 mm) maximum depth, with raised material.

          1. Repair, VRS4359 (Repair-028) TASK 75-24-49-300-028.

          3. More than in Step.

          1. Reject

    4. SUBTASK 75-24-49-220-221 Examine the Rivets, Clip Nuts and Angle Brackets

      1. Loose or damaged rivets.

      1. Repair, VRS4357 (Repair-032) TASK 75-24-49-300-032.

      2. Loose or damaged nuts.

      1. Repair, VRS4357 (Repair-032) TASK 75-24-49-300-032.

      3. Loose or damaged brackets.

      1. Repair, VRS4357 (Repair-032) TASK 75-24-49-300-032.

    5. Figure: Examine the Connector Tube

    Examine the Connector Tube

Requirements After Job Completion

Follow-On Conditions

NONE