TASK 72-32-55-200-001-A00 Front Bearing Compartment Seal Support - Examine, Inspection-001

DMC:V2500-A0-72-32-5500-00A-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 72-32-55-200-001-A00 Front Bearing Compartment Seal Support - Examine, Inspection-001

Effectivity

FIG/ITEM PART NO.

01-100

5W2050

General

This TASK gives the procedure for the inspection of the seal support. For the other No. 1 bearing front seal support parts, refer to TASK 72-32-55-200-000 (INSPECTION-000).

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. Refer to TASK 72-32-55-100-000 (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 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 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

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

NOTE

To identify consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Magnetic particle inspection equipmentLOCALMagnetic particle inspection equipment

(Refer to SPM TASK 70-24-00-240-501).

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDERLOCALCoMat 06-011

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-55-240-051 Examine the Seal Support Assembly (01-100) for Cracks

    1. Clean the part. Refer to TASK 72-32-55-100-000 (CLEANING-000).

      2. NOTE

        During the magnetic inspection, it is recommended that you use CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDER.

        Do the crack test on the part that is given below. Use the applicable magnetic inspection procedure.

        PART IDENT PROCEDURE CURRENT/INSPECT TASK/SUBTASK

        Seal support

        assembly

        TB using wet

        continuous or

        simultaneous

        inking with

        1000 AM.

        Seal support

        assembly outside

        diameter visually

        inspect for

        longitudinal and

        radial defects.

        Check doubtful

        indications using

        low power

        magnification.

        If necessary,

        inspect under

        white light at

        X10 binocular

        Solenoid coil

        wet continuous

        or simultaneous

        inking

        6000 A/T.

        Do again the

        magnetization

        and inspection

        along seal

        support assembly

        length visually

        inspect for

        circumferential

        defects.

        Check doubtful

        indications

        using low power

        magnification.

        If necessary,

        inspect under

        white light at

        X10 binocular

        1. Cracked

        1. Reject unless referred to differently in the procedure

    2. SUBTASK 72-32-55-220-052 Examine the Seal Support Assembly (01-100) Surface

    1. Refer to Figure.

      2. Examine the surface at location 1.

        1. Nicked.

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

          1. Accept

          2. More than in Step

          1. Repair, VRS1301 TASK 72-32-55-300-001 (REPAIR-001)

        2. Dented.

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

          1. Accept

          2. More than in Step

          1. Repair, VRS1301 TASK 72-32-55-300-001 (REPAIR-001)

        3. Scratched.

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

          1. Accept

          2. More than in Step

          1. Repair, VRS1301 TASK 72-32-55-300-001 (REPAIR-001)

        4. Galled.

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

          1. Accept

          2. More than in Step

          1. Repair, VRS1301 TASK 72-32-55-300-001 (REPAIR-001)

    3. SUBTASK 72-32-55-220-053 Examine the Seal Support Assembly (01-100) Insert

    1. Refer to Figure.

      2. Examine the insert at location 2.

        1. Thread damage

        1. Repair, VRS1302 TASK 72-32-55-300-002 (REPAIR-002)

    4. SUBTASK 72-32-55-220-054 Examine the Seal Support Assembly (01-100) Painted Surface

    1. Refer to Figure.

      2. Examine the painted surface at location 3.

        1. Damaged

        1. Repair, VRS1303 TASK 72-32-55-300-003 (REPAIR-003)

    5. SUBTASK 72-32-55-220-055 Examine the Seal Support Assembly (01-100) Flange Diameter

    1. Refer to Figure.

      2. Examine the flange diameter at location 4.

        1. Flange diameter.

          1. If minimum diameter is between 16.69382 to 16.69539 in. (424.023 to 424.063 mm)

          1. Accept

          2. If minimum diameter is between 16.67382 to 16.69382 in. (423.515 to 424.023 mm)

          1. Repair, VRS1304 TASK 72-32-55-300-004 (REPAIR-004)

          3. Less than in Step

          1. Reject

    6. SUBTASK 72-32-55-220-063 Examine the Seal Support Assembly (01-100) Jack Screw Holes

    1. Refer to Figure.

      2. Examine the jack screw holes at location 5.

        1. Thread damage

        1. Repair, VRS1515 TASK 72-32-55-300-009 (REPAIR-009)

    7. Figure: Inspection of the Seal Support Assembly

    Inspection of the Seal Support Assembly

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X222X
Supply Number:CoMat 06-011
Type:sp01
Supply Short Name:CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDER
Supply Name:CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDER
Specification Groups:
Doc NumberType
Where CoMat 06-011 is specified with no suffix, use one of the CoMat 06-011 letter suffix alternative materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Tool Number:Magnetic particle inspection equipment
Tool Name:Magnetic particle inspection equipment