TASK 72-32-83-200-004-A00 LPC Stage 2 Stator - Examine, Inspection-004

DMC:V2500-A0-72-32-8320-00A-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 72-32-83-200-004-A00 LPC Stage 2 Stator - Examine, Inspection-004

Effectivity

FIG/ITEM

PART NO.

01-800

5A0071

01-800

5A7378

01-800

5A1418

General

This TASK gives the procedure for the inspection of the LP compressor stage 2 stator assembly. For the other LP compressor booster stage vanes parts, refer to TASK 72-32-83-200-000 (INSPECTION-000).

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. Refer to TASK 72-32-83-100-000 (CLEANING-000).

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 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 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 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

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 72-32-83-230-059 Examine the LP Compressor Stage 2 Stator Assembly (01-800) for Cracks

    1. Clean the parts. Refer to TASK 72-32-83-100-000 (CLEANING-000).

    2. Do the crack test on the parts that are given below.

      PART IDENT

      TASK/SUBTASK

      LP compressor stage 2 stator assembly

      3. Inner shroud ring.

        1. Cracked

        1. Reject

      4. Vanes.

        1. Cracked

        1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

    2. SUBTASK 72-32-83-220-077 Examine the LP Compressor Stage 2 Stator Assembly (01-800) Leading Edge

    1. Refer to Figure.

      2. Examine the leading edge at location 1.

        1. Dented.

          1. In zone A

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          2. In area other than Step

          1. Up to 0.040 in. (1.01 mm) in depth

          2. Repair, VRS1398 TASK 72-32-83-300-002 (REPAIR-002)

          3. More than in 0.040 in. (1.01 mm) in depth

          4. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        2. Nicked.

          1. In zone A

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          2. In area other than Step

          1. Up to 0.040 in. (1.01 mm) in depth

          2. Repair, VRS1398 TASK 72-32-83-300-002 (REPAIR-002)

          3. More than in 0.040 in. (1.01 mm) in depth

          4. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        3. Cracked

        1. Refer to Step

    3. SUBTASK 72-32-83-220-078 Examine the LP Compressor Stage 2 Stator Assembly (01-800) Trailing Edge

    1. Refer to Figure.

      2. Examine the trailing edge at location 2.

        1. Dented.

          1. In zone A

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          2. In area other than Step

          1. Up to 0.040 in. (1.01 mm) in depth

          2. Repair, VRS1398 TASK 72-32-83-300-002 (REPAIR-002)

          3. More than in 0.040 in. (1.01 mm) in depth

          4. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        2. Nicked.

          1. In zone A

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          2. In area other than Step

          1. Up to 0.040 in. (1.01 mm) in depth

          2. Repair, VRS1398 TASK 72-32-83-300-002 (REPAIR-002)

          3. More than in 0.040 in. (1.01 mm) in depth

          4. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        3. Cracked

        1. Refer to Step

    4. SUBTASK 72-32-83-220-079 Examine the LP Compressor 2 Stator Assembly (01-800) Convex and Concave Airfoil Surface

    1. Refer to Figure.

      2. Examine the convex and concave airfoil surface at location 3.

        1. Dented.

          1. In zone A

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          2. In area other than Step

          1. Up to 0.010 in. (0.25 mm) in depth

          2. Repair, VRS1398 TASK 72-32-83-300-002 (REPAIR-002)

          3. More than in 0.010 in. (0.25 mm) in depth

          4. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          5. To cause a distortion on opposite surface

          6. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        2. Nicked.

          1. In zone A

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          2. In area other than Step

          1. Up to 0.010 in. (0.25 mm) in depth

          2. Repair, VRS1398 TASK 72-32-83-300-002 (REPAIR-002)

          3. More than in 0.010 in. (0.25 mm) in depth

          4. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

          5. To cause a distortion on opposite surface

          6. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

    5. SUBTASK 72-32-83-220-080 Examine the LP Compressor Stage 2 Stator Assembly (01-800) Outer Platform

    1. Refer to Figure.

      2. Examine the outer platform at location 4.

        1. Galled.

          1. Up to 0.005 in. (0.12 mm) in depth

          1. Repair, VRS1399 TASK 72-32-83-300-006 (REPAIR-006)

          2. More than in 0.005 in. (0.12 mm) in depth

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        2. Worn in the bolt holes.

          1. Up to 0.010 in. (0.25 mm) in depth

          1. Repair, VRS1399 TASK 72-32-83-300-006 (REPAIR-006)

          2. More than in 0.010 in. (0.25 mm) in depth

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        3. Cracked

        1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

    6. SUBTASK 72-32-83-220-081 Examine the LP Compressor Stage 2 Stator Assembly (01-800) Inner Shroud Ring

    1. Refer to Figure.

      2. Examine the inner shroud ring at location 5.

        1. Corroded

        1. Repair, VRS1951 TASK 72-32-83-300-048 (REPAIR-048)

        2. Nicked

          1. Up to 0.010 in. (0.25 mm) in depth

          1. Accept

          2. More than in 0.010 in. (0.25 mm) in depth

          1. Repair, VRS1951 TASK 72-32-83-300-048 (REPAIR-048)

        3. Dented.

          1. Up to 0.010 in. (0.25 mm) in depth

          1. Accept

          2. More than in 0.010 in. (0.25 mm) in depth

          1. Repair, VRS1951 TASK 72-32-83-300-048 (REPAIR-048)

    7. SUBTASK 72-32-83-220-082 Examine the LP Compressor Stage 2 Stator Assembly (01-800) Molding Rubber

    1. Refer to Figure.

      2. Examine the molding rubber at location 6.

        1. Eroded

        1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        2. Peeled.

          1. Up to 30 percent of each section length at location 6

          1. Accept

          2. More than in Step

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

    8. SUBTASK 72-32-83-220-083 Examine the LP Compressor Stage 2 Stator Assembly (01-800) Abradable Seal

    1. Refer to Figure.

      2. Examine the abradable seal at location 7.

        1. Rubbed by the seal fins.

          1. Up to 0.040 in. (1.01 mm) in depth

          1. Accept

          2. More than in 0.040 in. (1.01 mm) in depth

          1. Repair, VRS1400 TASK 72-32-83-300-014 (REPAIR-014)

        2. Worn.

          1. If the inner diameter is between 27.957 and 27.964 in. (710.10 and 710.30 mm)

          1. Accept

          2. More than 27.964 in. (710.30 mm)

          1. Repair, VRS1400 TASK 72-32-83-300-014 (REPAIR-014)

    9. SUBTASK 72-32-83-220-084 Examine the LP compressor Stage 2 Stator Assembly (01-800) Platform Flowpath Surface

    1. Refer to Figure.

      2. Examine the flowpath at location 8.

        1. Scratched.

          1. Up to 0.008 in. (0.20 mm) in depth

          1. Repair, VRS1399 TASK 72-32-83-300-006 (REPAIR-006)

          2. More than 0.008 in. (0.20 mm) in depth

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        2. Nicked.

          1. Up to 0.008 in. (0.20 mm) in depth

          1. Repair, VRS1399 TASK 72-32-83-300-006 (REPAIR-006)

          2. More than 0.008 in. (0.20 mm) in depth

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

        3. Dented.

          1. Up to 0.008 in. (0.20 mm) in depth

          1. Repair, VRS1399 TASK 72-32-83-300-006 (REPAIR-006)

          2. More than 0.008 in. (0.20 mm) in depth

          1. Repair, VRS1401 TASK 72-32-83-300-015 (REPAIR-015)

    10. Figure: Locations on the LP compressor stage 2 stator assembly

    Locations on the LP compressor stage 2 stator assembly

Requirements After Job Completion

Follow-On Conditions

NONE