TASK 72-32-87-200-002 Fan Case Rear Liner Panel - Examine, Inspection-002

DMC:V2500-A0-72-32-8702-00A-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 72-32-87-200-002 Fan Case Rear Liner Panel - Examine, Inspection-002

Effectivity

FIG/ITEM

PART NO.

02-100

5A0258

02-100

5A0809

02-100

5A0842

02-100

5A1379

02-100

5A1622

02-100

5A1680

02-100

5A1737

02-100

5A1743

02-100

5A2149

02-100

5A1119

02-150

5A0258

02-150

5A0809

02-150

5A0842

02-150

5A1379

02-150

5A1622

02-150

5A1680

02-150

5A1737

02-150

5A1743

02-150

5A2149

02-150

5A1120

02-200

5A0259

02-200

5A0814

02-200

5A0843

02-200

5A1380

02-200

5A1623

02-200

5A1681

02-200

5A1738

02-200

5A1744

02-200

5A2150

02-200

5A1122

02-250

5A0817

02-250

5A0844

02-250

5A1381

02-250

5A1625

02-250

5A2151

02-290

5A0815

02-290

5A1625

02-290

5A1626

02-300

5A0260

02-300

5A0818

02-300

5A0845

02-300

5A1382

02-300

5A1624

02-300

5A1682

02-300

5A1739

02-300

5A1745

02-300

5A2152

02-300

5A1125

02-350

5A0258

02-350

5A0809

02-350

5A0842

02-350

5A1379

02-350

5A1622

02-350

5A1680

02-350

5A1737

02-350

5A1743

02-350

5A2149

02-350

5A1121

02-400

5A0259

02-400

5A0814

02-400

5A0843

02-400

5A1380

02-400

5A1623

02-400

5A1681

02-400

5A1738

02-400

5A1744

02-400

5A2150

02-400

5A1123

02-450

5A0259

02-450

5A0814

02-450

5A0843

02-450

5A1380

02-450

5A1623

02-450

5A1681

02-450

5A1738

02-450

5A1744

02-450

5A2150

02-450

5A1124

02-500

5A0260

02-500

5A0818

02-500

5A0845

02-500

5A1380

02-500

5A1382

02-500

5A1624

02-500

5A1682

02-500

5A1739

02-500

5A1745

02-500

5A2152

02-500

5A1126

02-550

5A0260

02-550

5A0818

02-550

5A0845

02-550

5A1382

02-550

5A1624

02-550

5A1682

02-550

5A1739

02-550

5A1745

02-550

5A2152

02-550

5A1143

General

This TASK gives the procedure for the inspection of the fan case liner panel assembly.

The policy that is necessary for inspection is given in the SPM TASK 70-20-00-200-501.

All the parts must be cleaned before any part is examined. Refer to the TASK 72-32-87-100-000 (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.

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 70-20-00-200-501

Some data on these items is contained in this TASK. For more data on these items refer to the SPM.

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 72-32-87-220-055 Examine the Fan Case Liner Panel Assembly Bushes

    1. Refer to Figure and Figure

      2. Examine the bushes at location 1.

        1. Galled.

          1. Up to 0.015 in. (0.38 mm) in depth

          1. Accept

          2. More than in Step

          1. Reject

    2. SUBTASK 72-32-87-220-056 Examine the Fan Case Liner Panel Assembly Panel

    1. Refer to: Figure and Figure

      2. Examine the panel at location 2.

        1. Nicked, dented and scratched.

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

          1. Accept

          2. Up to 0.020 in. (0.50 mm) in depth

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          3. More than in Step

          1. Reject

        2. Cracked (Not go through the panel).

          1. Up to 0.050 in. (1.27 mm) in length, if the number of cracks which go to or come from the bush is 2 or lower

          1. Accept

          2. Up to 0.275 in. (7.0 mm) in length, if the number of cracks is less than 6 and total accumulative length of cracks within 0.275 in. (7.0 mm), if the crack does not reach the bush

          1. Accept

          3. More than in Step and up to 0.984 in. (25.0 mm) in length, if the crack does not reach the bush

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          4. More than in Step

          1. Reject

        3. Cracked (Go through the panel).

          1. Damaged area is within 0.775 sq in. (500 sq mm)

          1. Drill a hole to remove the damage and Repair, VRS1803 TASK 72-32-87-300-005 (REPAIR-005)

          2. More than in Step

          1. Reject

    3. SUBTASK 72-32-87-220-057 Examine the Fan Case Liner Panel Assembly Edge Corner

    1. Refer to Figure and Figure.

      2. Examine the edge corner at location 3.

        1. Damage up to 0.020 in. (0.50 mm) in depth and 0.50 in. (12.7 mm) in length

        1. Accept

    4. SUBTASK 72-32-87-220-080 Examine the Fan Case Liner Panel Assembly Side Face

    1. Refer to Figure and Figure.

      2. Examine the side face at location 7.

        1. Nicked, dented and scratched.

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

          1. Accept

          2. Up to 0.020 in. (0.50 mm) in depth

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          3. More than in Step

          1. Reject

        2. Cracked.

          1. Up to 0.275 in. (7.0 mm) in length, if the number of cracks is less than 6 and total accumulative length of cracks within 0.275 in. (7.0 mm)

          1. Accept

          2. More than in Step and up to 0.984 in. (25.0 mm) in length

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          3. More than in Step

          1. Reject

    5. SUBTASK 72-32-87-220-058 Examine the Fan Case Liner Panel Assembly Hole Edge

    1. Refer to Figure and Figure.

      2. Examine the hole edges at location 4.

        1. Damage up to 0.020 in. (0.50 mm) in depth and 0.50 in. (12.7 mm) in length

        1. Accept

    6. SUBTASK 72-32-87-220-072 Examine the Fan Case Liner Panel Assembly Panel

    1. Refer to Figure and Figure.

      2. Examine the ribs at location 6.

        1. Nicked, dented and scratched.

        1. In Zone A (The area up to one third of height from the rib top surface).

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

          1. Accept

          3. More than in Step

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

        4. In area other than Step.

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

          1. Accept

          6. Up to 0.020 in. (0.50 mm) in depth

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          7. More than in Step

          1. Reject

        2. Cracked.

          1. Up to 0.050 in. (1.27 mm) in length

          1. Accept

          2. Up to 0.984 in. (25.0 mm) in length

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          3. More than in Step

          1. Reject

    7. SUBTASK 72-32-87-220-065 Examine the Fan Case Liner Panel Assembly, Inner Surface

    1. Refer to Figure and Figure.

      2. Examine the inner surface at location 5.

        1. Erosion.

          1. Up to 0.0050 in. (0.13 mm) in depth

          1. Accept

          2. More than in Step

          1. Repair, VRS1803 TASK 72-32-87-300-005 (REPAIR-005)

        2. Cracked.

        1. Circumferential crack.

          2. Up to 6.000 in. (152.4 mm) in length, if crack goes through the panel

          1. Repair, VRS1809 TASK 72-32-87-300-003 (REPAIR-003)

          3. Up to 6.000 in. (152.4 mm) in length, if the crack does not go through the panel

          1. Repair, VRS1803 TASK 72-32-87-300-005 (REPAIR-005)

          4. More than in Step and Step

          1. Reject

        5. Longitudinal crack.

          6. Up to 3.00 in. (76.2 mm) in length, if crack goes through the panel

          1. Repair, VRS1809 TASK 72-32-87-300-003 (REPAIR-003)

          7. Up to 3.00 in. (76.2 mm) in length, if crack does not go through the panel

          1. Repair, VRS1803 TASK 72-32-87-300-005 (REPAIR-005)

          8. More than in Step and Step

          1. Reject

          9. If crack goes to or comes from the bush

          1. Reject

        3. Damaged hole (Material that is not there) with erosion within the limit in (1) (a).

        1. Up to 2.00 in. (50.8 mm) diameter.

          2. Up to two holes

          1. Repair, VRS1809 TASK 72-32-87-300-003 (REPAIR-003)

          3. More than in Step

          1. Reject

          4. More than 2.00 in. (50.8 mm) diameter

          1. Reject

          5. If damaged hole reaches the bush, edge corner or rib

          1. Reject

        4. Damaged hole (Material that is not there) with erosion more than the limit in (1) (a).

        1. Total hole area is within 0.775 sq in (500 sq mm).

          2. If the damaged hole or erosion does not reach the rib

          1. Repair, VRS1803 TASK 72-32-87-300-005 (REPAIR-005)

          3. More than in Step

          1. Reject

          4. More than in Step

          1. Reject

    8. SUBTASK 72-32-87-220-081 Examine the Fan Case Liner Panel Assembly Groove

    1. Refer to Figure and Figure.

      2. Examine the groove at location 8.

        1. Nicked, dented and scratched.

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

          1. Accept

          2. Up to 0.020 in. (0.50 mm) in depth

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          3. More than in Step

          1. Reject

        2. Cracked.

          1. Up to 0.984 in. (25.0 mm) in length

          1. Repair, VRS1936 TASK 72-32-87-300-006 (REPAIR-006)

          2. More than in Step

          1. Reject

    9. Figure: Locations on the fan case liner panel assembly

    Sheet 1

    Legend
    Locations on the fan case liner panel assembly

    Sheet 1

    Close

    Figure: Locations on the fan case liner panel assembly

    Sheet 2

    Legend
    Locations on the fan case liner panel assembly

    Sheet 2

    Close

Requirements After Job Completion

Follow-On Conditions

NONE