TASK 72-41-34-200-005-C00 HPC Inlet Variable Stator Vane Unison Rings - Examine, Inspection-005 - SBE 72-0418

DMC:V2500-A0-72-41-3422-00C-300A-C|Issue No:004.00|Issue Date:2019-08-01

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 72-41-34-200-005-C00 HPC Inlet Variable Stator Vane Unison Rings - Examine, Inspection-005 - SBE 72-0418

Effectivity

FIG/ITEM

PART NO.

02-440

6A7899

02-440

6A8075

02-540

6A7901

02-540

6A8077

General

This TASK gives the procedure for the inspection of the VIGV upper and lower unison rings.

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

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 those 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,

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 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 72-41-34-230-127 Examine the VIGV Upper and Lower Unison Rings 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

        VIGV upper and lower unison rings

        1. Cracked.

        1. Reject.

    2. SUBTASK 72-41-34-220-382 Examine the VIGV Upper and Lower Unison Rings Bodies at Location 1 and 2

    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. Repair, VRS6158 TASK 72-41-34-300-046 (REPAIR-046).

      3. Scored.

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

        1. Accept.

        2. More than in Step.

        1. Repair, VRS6158 TASK 72-41-34-300-046 (REPAIR-046).

      4. Scratched.

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

        1. Accept.

        2. More than in Step.

        1. Repair, VRS6158 TASK 72-41-34-300-046 (REPAIR-046).

    3. SUBTASK 72-41-34-220-450 Examine the VIGV Upper and Lower Unison Rings Stop Rivets at Location 3

    1. Refer to Figure.

      2. Stop rivets.

        1. Loose.

        1. Reject.

        2. Missing.

        1. Reject.

        3. Welds cracked.

        1. Repair, VRS6544 TASK 72-41-34-300-064 (REPAIR-064).

    4. SUBTASK 72-41-34-220-383 Examine the VIGV Upper and Lower Unison Rings Spacers at Location 4

    1. Refer to Figure.

      2. Loose.

      1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

        2. Inner bore.

          1. Scratched.

          1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

          2. Scored.

          1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

        3. Wear on the bore.

          1. Less than 0.202 in. (5.125 mm) in diameter.

          1. Accept.

          2. More than in Step.

          1. Reject.

    5. SUBTASK 72-41-34-220-384 Examine the VIGV Upper and Lower Unison Rings Dowels at Location 5

    1. Refer to Figure.

      2. Missing.

      1. Reject.

      3. Worn diameter.

        1. More than 0.4340 in. (11.016 mm).

        1. Accept.

        2. Less than Step.

        1. Reject.

      4. Screw thread inserts.

        1. Broken.

        1. Repair, VRS6156 TASK 72-41-34-300-014 (REPAIR-014).

        2. Crossed threads.

        1. Repair, VRS6156 TASK 72-41-34-300-014 (REPAIR-014).

        3. Threads that are not there.

        1. Repair, VRS6156 TASK 72-41-34-300-014 (REPAIR-014).

    6. SUBTASK 72-41-34-220-449 Examine the VIGV Upper and Lower Unison Rings Dowel at location 9

    1. Refer to Figure.

      2. Missing.

      1. Reject.

        2. Worn diameter.

          1. More than 0.4340 in. (11.016 mm).

          1. Accept.

          2. Less than in Step.

          1. Reject.

        3. Screw threads.

          1. Broken.

          1. Reject.

          2. Crossed threads.

          1. Reject.

          3. Threads that are not there.

          1. Reject.

    7. SUBTASK 72-41-34-220-385 Examine the VIGV Upper and Lower Unison Rings Bushes at Location 6

    1. Refer to Figure.

      2. Inner bore.

        1. Scored.

        1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

        2. Scratched.

        1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

        3. Wear.

          1. Less than 0.241 in. (6.112 mm) in diameter.

          1. Accept.

          2. More than Step.

          1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

      3. Bushes that are not there.

      1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

      4. Excessive bush movement (side to side).

      1. Repair, VRS6265 TASK 72-41-34-300-047 (REPAIR-047).

    8. SUBTASK 72-41-34-220-052 Examine the VIGV Lower Unison Ring Spindle at Location 7

    1. Refer to Figure.

      2. Loose.

      1. Reject.

        2. Threads.

          1. Crossed.

          1. Reject.

          2. Stripped.

          1. Reject.

          3. Picked-up.

          1. Reject.

        3. Wear (non threaded shank).

          1. If the diameter is between 0.373 in. to 0.374 in. (9.49 mm to 9.51 mm).

          1. Accept.

          2. Less than in Step.

          1. Reject.

    9. SUBTASK 72-41-34-220-386 Examine the VIGV Upper and Lower Unison Rings Spacer Holes at Location 8

    1. Refer to Figure.

      2. Burred edges.

      1. Reject.

      3. Elongated.

      1. Reject.

    10. Figure: VIGV Upper and Lower Unison Rings - Inspection Locations

    VIGV Upper and Lower Unison Rings - Inspection Locations

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the procedure to add repair reference. (19VG015)