TASK 72-41-34-200-020 HPC Unison Ring Control Rod Connectors - Examine (Stage 4 Through 6), Inspection-020

DMC:V2500-A0-72-41-3451-00A-300A-C|Issue No:002.00|Issue Date:2021-08-01

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 72-41-34-200-020 HPC Unison Ring Control Rod Connectors - Examine (Stage 4 Through 6), Inspection-020

Effectivity

FIG/ITEM PART NO.

04-360

6A2611

04-360

6A7434

05-360

6A3688

05-360

6A7435

06-360

6A2607

General

This TASK gives the procedure for the inspection of the stage 4, 5 and 6 control rod connectors.

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.

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 the SPM.

References

Refer to the SPM for data on these items.

Definition 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 70-20-01-200-501

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 72-41-34-230-069 Examine the Stage 4, 5 and 6 Control Rod Connectors (04-360, 05-360 and 06-360) for Cracks

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

      2. Do the test for cracks on the part that is given below.

        PART IDENT TASK/SUBTASK

        Stage 4, 5 and 6 control rod connectors

        SPM TASK 70-23-02-230-501

        1. Cracked

        1. Reject

    2. SUBTASK 72-41-34-220-141 Examine the Stage 4, 5 and 6 Control Rod Connectors (04-360, 05-360 and 06-360) Body at Location 1

    1. Refer to Figure.

      2. Nicked.

        1. Up to 0.005 in. (0.13 mm) in depth

        1. Accept

        2. More than in Step.

        1. Reject.

      3. Scored.

        1. Up to 0.005 in. (0.13 mm) in depth

        1. Accept

        2. More than in Step.

        1. Reject.

      4. Scratched.

        1. Up to 0.005 in. (0.13 mm) in depth

        1. Accept

        2. More than in Step.

        1. Reject.

    3. SUBTASK 72-41-34-220-142 Examine the Stage 4, 5 and 6 Control Rod Connectors (04-360, 05-360 and 06-360) Bolt Holes at Location 2

    1. Refer to Figure.

      2. Elongated

      1. Reject

      3. Burred

      1. Reject

    4. SUBTASK 72-41-34-220-143 Examine the Stage 4, 5 and 6 Control Rod Connectors (04-360, 05-360 and 06-360) Bushes at Location 3

    1. Refer to Figure.

      2. Loose

      1. Repair, VRS6238 TASK 72-41-34-300-020 (REPAIR-020)

      3. Bore.

        1. Scored.

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

          1. Accept

          2. More than in Step.

          1. Repair, VRS6238 TASK 72-41-34-300-020 (REPAIR-020)

        2. Scratched.

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

          1. Accept

          2. More than in Step.

          1. Repair, VRS6238 TASK 72-41-34-300-020 (REPAIR-020)

        3. Wear.

          1. If the bushbore diameter is between 0.318 to 0.320 in. (7.95 to 8.00 mm)

          1. Accept

          2. More than in Step.

          1. Repair, VRS6238 TASK 72-41-34-300-020 (REPAIR-020)

        4. Missing.

          1. If the bushes are missing

          1. Repair, VRS6238 TASK 72-41-34-300-020 (REPAIR-020)

      4. Inner and outer faces.

        1. Galled.

          1. Up to 0.005 in. (0.13 mm) in depth

          1. Accept

          2. More than in Step.

          1. Repair, VRS6238 TASK 72-41-34-300-020 (REPAIR-020)

        2. Scored.

          1. Up to 0.005 in. (0.13 mm) in depth

          1. Accept

          2. More than in Step.

          1. Repair, VRS6238 TASK 72-41-34-300-020 (REPAIR-020)

    5. Figure: Stage 4, 5 and 6 control rod connectors - inspection locations

    Stage 4, 5 and 6 control rod connectors - inspection locations

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the procedural steps. (20VG080A)

Change Type:

Added step references. (Editorial)