TASK 72-41-34-200-001-B00 HPC Vane Ring Control Rods - Examine, Inspection-001

DMC:V2500-A0-72-41-3417-00C-300A-C|Issue No:002.00|Issue Date:2019-05-01

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 72-41-34-200-001-B00 HPC Vane Ring Control Rods - Examine, Inspection-001

Effectivity

FIG./ITEM

PART NO.

01-200

6A8647

01-250

6A8691

01-300

6A8690

01-350

6A8689

General

This TASK gives the procedure for the inspection of the stator vane actuating ring control rods.

Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.

The policy that is necessary for inspection is given in 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.

The procedure for the parts which must have a crack test is given in Step. Do the crack test before a 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 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 SPM.

References

Refer to SPM for data on these items:

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

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

Some data on these items is contained in this TASK. For more data on these items refer to 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 72-41-34-240-052 Do a Crack Test on the Stator Vane Actuating Ring Control Rods

    2. Clean the parts. Refer to TASK 72-41-34-100-000 (CLEANING-000).

      1. Do a crack test on the parts that follow:

        PART IDENT

        PROCEDURE

        CURRENT/INSPECT

        TASK/SUBTASK

        Control rods

        C.F. End to

        200 amps

        end

        SUBTASK 70-24-01-240-010

        Coil

        3500 Amp/Turns

        SUBTASK 70-24-01-240-014

        1. Cracked.

        2. Reject.

    1. SUBTASK 72-41-34-220-560 Examine the Stator Vane Actuating Ring Control Rods Threads at Location 12

    2. Refer to Figure.

      1. Crossed.

      2. Reject.

      1. Threads that are not there.

      2. Reject.

      1. Stripped.

      2. Reject.

      1. Worn.

      2. Reject.

    1. SUBTASK 72-41-34-220-561 Examine the Stator Vane Actuating Ring Control Rods Holes at Location 13

    2. Refer to Figure.

      1. Grooved.

      2. Reject.

      1. Chafed.

      2. Reject.

      1. Worn.

      2. Reject.

  1. Figure: Stator Vane Actuating Ring Control Rods - Inspection Locations

    Stator Vane Actuating Ring Control Rods - Inspection Locations

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the procedure to delete inspection instructions. (18VG158)