TASK 72-32-03-200-003-C00 Fan Frame - Examine, Inspection-003

DMC:V2500-A0-72-32-0301-00C-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 72-32-03-200-003-C00 Fan Frame - Examine, Inspection-003

Effectivity

FIG/ITEM

PART NO.

03-100

5A1763

03-100

5A1764

03-100

5A1765

03-100

5A1766

03-100

5A1767

03-100

5A1768

03-100

5A1769

03-100

5A1770

03-100

5A1771

03-100

5A1772

03-100

5A1773

03-100

5A1774

03-100

5A1775

03-100

5A1776

03-100

5A1777

03-100

5A1778

03-100

5A1779

03-100

5A1780

03-100

5A1781

03-100

5A1782

03-100

5A1783

03-100

5A1784

03-100

5A1785

03-100

5A1786

03-100

5A1787

03-100

5A1788

03-100

5A1789

03-100

5A1790

03-100

5A1791

03-100

5A1792

General

This TASK gives the procedure for the inspection of the fan frame assembly. For other intermediate structure parts, refer to TASK 72-32-03-200-000 (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 72-32-03-100-000 (CLEANING-000)

All 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 SUBTASK 72-32-03-230-051 . Do the crack test before the part is visually examined.

A ** following a repair referenced in this inspection indicates that the repair is not yet published in the current revision of the manual and the part must be rejected. Contact IAE for additional information concerning FAA approved repair date.

Do not discard any part until you are sure there are no repairs available. Refer to the instructions in the repair before a discarded part is used again or oversize parts are installed.

Parts which must 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 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:

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 are 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

NameManufacturerPart Number / IdentificationQuantityRemark
Fluorescent Penetrant Inspection EquipmentLOCALFluorescent penetrant inspection equipment

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-03-230-082 Examine the Fan Frame Assembly (03-100) for Cracks

    1. Clean the part. Refer to TASK 72-32-03-100-000 (CLEANING-000).

      2. Do the crack test on the part that is given below: Use applicable penetrant inspection procedure.

        PART IDENT

        TASK/SUBTASK

        Fan frame assembly

        1. Outer struts.

          1. Cracked

          1. Repair, VRS1181 TASK 72-32-03-300-005 (REPAIR-005)**

        2. Other area.

          1. Cracked

          1. Reject

    2. SUBTASK 72-32-03-220-167 Examine the Fan Frame Assembly (03-100) Outer Struts

    1. Refer to Figure and Figure.

      2. Examine the outer struts at location 1.

        1. Dented.

          1. Area A, two smooth contoured dents per strut 0.030 in. (0.76 mm) in depth if there is no connecting distortion in Area B

          1. Accept

          2. Area B, two smooth contoured dents per strut 0.020 in. (0.50 mm) in depth

          1. Accept

          3. More than in Step or Step

          1. Repair, VRS1181 TASK 72-32-03-300-005 (REPAIR-005)**

        2. Nicked and scratched.

          1. Area A, any nicks or scratches

          1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

          2. Area B, any nicks or scratches

          1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

        3. NOTE

          Clean obstacles from the inside of the strut which have blocked tubes.

          Blocked.

          1. Air tubes

          1. Clean with high pressure air blast

        4. Cracked

        1. Repair, VRS1181 TASK 72-32-03-300-005 (REPAIR-005)**

      3. Examine the strut faces at location 2.

        1. Galled

        1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

        2. Scored

        1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

        3. Loose wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

        4. Damaged wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

        5. Locking torque of the wire thread inserts.

          1. Other than torque limits as given in the SPM TASK 70-42-01-400-501

          1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

    3. SUBTASK 72-32-03-220-168 Examine the Fan Frame Assembly (03-100) Inner Struts

    1. Refer to Figure.

      2. Examine the inner struts at location 3.

        1. Dented.

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

          1. Accept

          2. More than in Step

          1. Reject

        2. Nicked

        1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

        3. Blocked.

          1. Air tubes

          1. Clean with high pressure air blast

    4. SUBTASK 72-32-03-220-169 Examine the Fan Frame Assembly (03-100) Front Flanges

    1. Refer to Figure and Figure.

      2. Examine the front flange at location 4.

        1. Galled.

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

          1. Accept

          2. More than in Step

          1. Repair, VRS1180 TASK 72-32-03-300-004 (72-32-03-300, REPAIR 004)

          3. More than 30 percent of each flange surface

          1. Reject

        2. Nicked.

          1. Up to 0.006 in. (0.15 mm) in depth

          1. Accept

          2. More than in Step

          1. Repair, VRS1180 TASK 72-32-03-300-004 (72-32-03-300, REPAIR 004)

        3. Loose wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (72-32-03-300, REPAIR 006)

        4. Damaged wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (72-32-03-300, REPAIR 006)

        5. Locking torque of the wire thread inserts.

          1. Other than the torque limit as given in the SPM TASK 70-42-01-400-501

          1. Repair, VRS1182 TASK 72-32-03-300-006 (72-32-03-300, REPAIR 006)

        6. Damage self locking nut threads

        1. Repair, VRS1184 TASK 72-32-03-300-007 (72-32-03-300, REPAIR 007)

        7. Locking torque of the self locking nuts.

          1. Other than the torque limit as given in the SPM TASK 70-42-01-400-501

          1. Repair, VRS1184 TASK 72-32-03-300-007 (72-32-03-300, REPAIR 007)

        8. Loose rivets

        1. Repair, VRS1184 TASK 72-32-03-300-007 (72-32-03-300, REPAIR 007)

        9. Missing rivets

        1. Repair, VRS1184 TASK 72-32-03-300-007 (72-32-03-300, REPAIR 007)

        10. Loose pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (72-32-03-300, REPAIR 009)

        11. Damaged pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (72-32-03-300, REPAIR 009)

      3. Examine the snap diameter at location 0304.

        1. Worn.

          1. If the diameter is between 21.4961 and 21.5003 in. (546.000 and 546.110 mm)

          1. Accept

          2. More than 21.5003 in. (546.110 mm)

          1. Reject

        3. Write down the dimension of the diameter.

    5. SUBTASK 72-32-03-220-170 Examine the Fan Frame Assembly (03-100) Sealing Rubber

    1. Refer to Figure.

      2. Examine the sealing rubber at location 6.

        1. Torn

        1. Repair, VRS1185 TASK 72-32-03-300-008 (REPAIR-008)

        2. Unbonded

        1. Repair, VRS1185 TASK 72-32-03-300-008 (REPAIR-008)

    6. SUBTASK 72-32-03-220-171 Examine the Fan Frame Assembly (03-100) Rear Flange

    1. Refer to Figure and Figure.

      2. Examine the rear flange at location 7.

        1. Nicked.

          1. Up to 0.006 in (0.15 mm) in depth

          1. Accept

          2. More than in Step

          1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

        2. Loose wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

        3. Damaged wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

        4. Locking torque of the wire thread inserts.

          1. Other than the torque limit as given in the SPM TASK 70-42-01-400-501

          1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

        5. Loose pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (REPAIR-009)

        6. Damaged pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (REPAIR-009)

      3. Examine the snap diameter at location 0308.

        1. Worn.

          1. If the diameter is between 11.3381 and 11.3400 in. (287.986 and 288.036 mm)

          1. Accept

          2. More than 11.3400 in. (288.036 mm)

          1. Reject

        3. Write down the dimension of the diameter.

    7. SUBTASK 72-32-03-220-172 Examine the Fan Frame Assembly (03-100) V Groove

    1. Refer to Figure.

      2. Examine the V groove at location 9.

        1. Galled

        1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

    8. SUBTASK 72-32-03-220-173 Examine the Fan Frame Assembly (03-100) Thrust Mount Pads

    1. Refer to Figure.

      2. Examine the thrust mount pads at location 10.

        1. Loose pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (REPAIR-009)

        2. Damaged pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (REPAIR-009)

        3. Loose studs

        1. Repair, VRS1192 TASK 72-32-03-300-010 (REPAIR-010)

        4. Damaged studs

        1. Repair, VRS1192 TASK 72-32-03-300-010 (REPAIR-010)

      3. Examine the bore diameter in the thrust mount pads at locations 5005 and 5006.

        1. Worn.

          1. If the diameter is between 1.7323 and 1.7338 in. (44.000 and 44.039 mm)

          1. Accept

          2. More than 1.7338 in (44.039 mm)

          1. Reject

        3. Write down the dimension of the diameter.

      4. Examine the bore diameter in the thrust mount tube mount pad at location 5003.

        1. Worn.

          1. If the diameter is between 3.9371 and 3.9378 in. (100.000 and 100.022 mm)

          1. Accept

          2. More than 3.9378 in. (100.022 mm)

          1. Reject

        3. Write down the dimension of the diameter.

    9. SUBTASK 72-32-03-220-174 Examine the Fan Frame Assembly (03-100) PTO Sealing Plate Pad

    1. Refer to Figure.

      2. Examine the PTO sealing plate pad at location 13.

        1. Loose pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (REPAIR-009)

        2. Damaged pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (REPAIR-009)

        3. Loose wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

        4. Damaged wire thread inserts

        1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

        5. Locking torque of the wire thread inserts.

          1. Other than the torque limit as given in the SPM TASK 70-42-01-400-501

          1. Repair, VRS1182 TASK 72-32-03-300-006 (REPAIR-006)

    10. SUBTASK 72-32-03-220-175 Examine the Fan Frame Assembly (03-100) Flow Path Surface

    1. Refer to Figure.

      2. Examine the flow path surfaces at locations 14 and 15.

        1. Dented.

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

          1. Accept

          2. More than in Step

          1. Reject

        2. Nicked

        1. Repair, VRS1180 TASK 72-32-03-300-004 (REPAIR-004)

    11. SUBTASK 72-32-03-220-176 Examine the Fan Frame Assembly (03-100) Thermocouple (03-890)

    1. Refer to Figure.

      2. Visual examine the thermocouple at location 16.

        1. Clearance between the thermocouple and the fan frame assembly.

          1. No clearance

          1. Accept

          2. If clearance is identified

          1. Repair, VRS1727 TASK 72-32-03-300-013 (REPAIR-013)

      3. Do a loop resistance check between the almel stud and the chromel stud. Use a megger to measure the loop resistance of the thermocouple.

        1. If the loop resitance is between 0.4 and 1.8 ohms at room temperature

        1. Accept

        2. Other than in Step

        1. Repair, VRS1727 TASK 72-32-03-300-013 (REPAIR-013)

    12. SUBTASK 72-32-03-220-177 Examine the Fan Frame Assembly (03-100) Rear Wall Window

    1. Refer to Figure.

      2. Examine the rear wall window at location 17.

        1. Cracked.

          1. Up to 0.20 in. (5.08 mm) in length

          1. Repair, VRS1732 TASK 72-32-03-300-016 (REPAIR-016)

          2. Between 0.20 and 0.60 in. (5.08 and 15.24 mm) in length

          1. Repair, VRS1783 TASK 72-32-03-300-020 (REPAIR-020)**

          3. More than in Step

          1. Reject

    13. SUBTASK 72-32-03-220-178 Examine the Fan Frame Assembly (03-100) Bushing Bore

    1. Refer to Figure.

      2. Examine the bushing bore diameter at location 0408.

        1. Worn.

          1. If the diameter is between 1.7323 and 1.7332 in. (44.000 and 44.025 mm)

          1. Accept

          2. More than 1.7332 in. (44.025 mm)

          1. Reject

        3. Write down the dimension of the diameter.

    14. SUBTASK 72-32-03-220-179 Examine the Fan Frame Assembly (03-100) Booster Stage Bleed Valve Actuator (BSBVA) Mount Flange

    1. Refer to Figure.

      2. Examaine the BSBVA mount flange at location 18.

        1. Loose or damaged rivet nuts

        1. Repair, VRS1222 TASK 72-32-03-300-033 (REPAIR-033)

        2. Loose or damaged pins

        1. Repair, VRS1190 TASK 72-32-03-300-009 (REPAIR-009)

    15. SUBTASK 72-32-03-220-180 Examine the Fan Frame Assembly (03-100) Strut Fairing mount Flange

    1. Refer to Figure.

      2. Examine the strut fairing mount flange at location 19.

        1. Loose or damaged rivet nuts

        1. Repair, VRS1222 TASK 72-32-03-300-033 (REPAIR-033)

    16. Figure: Locations on the fabrication fan frame assembly

    Locations on the fabrication fan frame assembly

    Figure: Locations on the fabrication fan frame assembly

    Locations on the fabrication fan frame assembly

    Figure: Locations on the fabrication fan frame assembly

    Locations on the fabrication fan frame assembly

    Figure: Locations on the fabrication fan frame assembly

    Locations on the fabrication fan frame assembly

    Figure: Locations on the fabrication fan frame assembly

    Locations on the fabrication fan frame assembly

    Figure: Locations on the fabrication fan frame assembly

    Locations on the fabrication fan frame assembly

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Fluorescent penetrant inspection equipment
Tool Name:Fluorescent Penetrant Inspection Equipment