TASK 72-32-00-200-007 Seal Ring - Examine, Inspection-007

DMC:V2500-A0-72-32-0007-00A-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 72-32-00-200-007 Seal Ring - Examine, Inspection-007

Effectivity

FIG/ITEM

PART NO.

02-495

5A0777

General

This TASK gives the procedure for the inspection of the seal ring. For the other parts of the LP compressor/intermediate case module, refer to TASK 72-32-00-200-000.

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 72-32-00-100-000.

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. Limits for cracks are given in the SUBTASK for each part.

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

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

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

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 72-32-00-240-051 Examine the Seal Ring (02-495) for Cracks

    1. NOTE

      For the method to clean the part, refer to the SPM TASK 70-11-14-300-503.

      Clean the part. Refer to TASK 72-32-00-100-000.

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

        PART IDENT

        TASK/OP

        Seal ring

        SPM TASK

        1. Cracked

        1. Reject

          PART IDENT

          PROCEDURE

          CURRENT/INSPECT

          TASK/OP

          Seal ring

          TB using continuous wet simultaneous inking with the CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDER

          500 amp

          Visually examine for longitudinal and radial defects. Do a check for doubtful indications using low power magnification.

          If necessary, examine under white light at 15X binocular

          SPM TASK

          6-turn solenoid continuous wet inking

          6000 A/T

          Do again the magnetisation and inspection along shaft length. Visually examine for circumferential defects. Do a check for doubtful indications using low power magnification. If necessary, examine under white light at 15X binocular

    2. SUBTASK 72-32-00-220-076 Examine the Seal Ring (02-495) Inside Diameter

    1. Refer to Figure.

      2. Examine the inside diameter at location 1.

        1. Worn.

          1. If the inside diameter is between 1.5847 and 1.5856 in. (40.250 and 40.275 mm)

          1. Accept

          2. More than 1.5856 in. (40.275 mm)

          1. Reject

    3. SUBTASK 72-32-00-220-077 Examine the Seal Ring (02-495) Outside Diameter

    1. Refer to Figure

      2. Examine the outside diameter at location 2.

        1. Worn.

          1. If the outside diameter is between 2.163 and 2.164 in. (54.94 and 54.97 mm)

          1. Accept

          2. Less than 2.163 in. (54.94 mm)

          1. Reject

    4. SUBTASK 72-32-00-220-078 Examine the Seal Ring (02-495) Faces

    1. Refer to Figure.

      2. Examine the front and rear faces at location 3.

        1. CAUTION

          CONTINUOUS GALLING WITNESS RADIALLY ACROSS ABUTMENT FACES ARE NOT PERMITTED.

          Galled.

          1. Any galls

          1. Repair, VRS1191 TASK 72-32-00-300-009

    5. Figure: Locations on the seal ring

    Locations on the seal ring

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