TASK 72-41-11-230-001 HPC Stage 3 - 8 Drum Disk - Do A Fluorescent Penetrant Inspection (FPI) Of The 7-8 Inner Cavity (Focused Inspection Location 10), Inspection-001

DMC:V2500-A0-72-41-1101-00A-351A-C|Issue No:003.00|Issue Date:2018-11-01

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 72-41-11-230-001 HPC Stage 3 - 8 Drum Disk - Do A Fluorescent Penetrant Inspection (FPI) Of The 7-8 Inner Cavity (Focused Inspection Location 10), Inspection-001

Effectivity

FIG/ITEM

PART NO.

01-200

6A3508

01-200

6A3648

01-200

6A3934

01-200

6A3936

01-200

6A4189

01-200

6A4900

01-200

6A5467

01-200

6A5592

01-200

6A5594

01-200

6A5659

01-200

6A6473

01-200

6A7379

01-200

6A7380

01-200

6A7382

01-200

6A7383

01-200

6A7384

01-200

6A7385

01-200

6A7401

01-200

6A7705

01-200

6A8236

01-200

6A8316

01-200

6A8318

01-200

6A8350

01-200

6B1379

01-200

6B1380

01-200

6B1381

01-200

6B1382

01-200

6B1383

01-200

6B1384

01-200

6B1385

01-200

6B1386

01-200

6B1387

01-200

6B1391

01-200

6B1392

01-200

6B1393

01-200

6B1401

01-200

6B1402

01-200

6B1403

01-200

6B1404

01-200

6B1405

01-200

6B1406

General

This focus inspection must only be done when specified by 72-41-11 Inspection (Inspection).

This procedure gives the instruction only to find the cracks in HP compressor stage 7/8 disk inner cavity at the inspection location 10. Refer to Figure. Refer to TASK 72-41-11-200-001-A00 (Inspection-001) for all other areas of the HP compressor stage 3 to 8 drum.

Ultra high sensitivity penetrant must be used for this focused FPI procedure.

The workshop procedure for this focus FPI TASK must be specified by a qualified level three trained Non-Destructive Test (NDT) specialist based on the requirements and procedures given in this TASK and the AMS 2647 - FPI for Aircraft and Engine Components Maintenance.

NOTE

To identify the consumable materials, refer to the PCI.

NOTE

Penetrants and removers must be from the same manufacturer. Developers do not have to come from the same manufacturer as the penetrant and remover. If possible, it is recommended to use the manufacturer's full system.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Penetrant process lineLOCAL
UV LightLOCAL

Hand held or fixture mounted

White lightLOCAL

Hand held or fixture mounted

Inspection mirrorLOCAL
Suction deviceLOCAL
IAE 2R19883 Rotary table inspection device0AM53IAE 2R198831
IAE 2R19884 Adapter0AM53IAE 2R198841

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-025 NITRIC ACID HNO3, TECHNICAL GRADELOCALCoMat 01-025
DELETEDLOCALDELETED
CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY)X222XCoMat 06-022
CoMat 06-030 NON AQUEOUS DEVELOPERLOCALCoMat 06-030
CoMat 06-032 DRY DEVELOPER37676CoMat 06-032
CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILICX222XCoMat 06-045

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-41-11-180-006 Control of Equipment and Materials

    2. Refer to the SPM TASK 70-23-00-230-501.

    1. SUBTASK 72-41-11-230-127 Do a Focus FPI of the HP Compressor Stage 8 Disk Inner Cavity Front Face

    2. Refer to Figure.

    3. Clean the HP compressor stage 3 to 8 drum before you start the inspection. Refer to TASK 72-41-11-110-001 (Special Procedure). Use CoMat 01-025 NITRIC ACID HNO3, TECHNICAL GRADE.

      1. Visually examine the stage 7/8 disk inner cavity at inspection location 10, for surface contamination that can mask the cracks.

      2. Use a hand held or fixture mounted white light source and inspection mirror. If contamination is found, refer to TASK 72-41-11-200-001 (Inspection-001).

      1. Penetrant application and processing.

        1. NOTE

          Penetrant processing must be done in accordance with the SPM TASK 70-23-00-230-501 and SPM TASK 70-23-04-230-501. Use CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY), CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILIC and CoMat 06-030 NON AQUEOUS DEVELOPER to find the crack). This TASK gives additional instructions necessary because of part's geometry.
          Penetrant must be first applied to the stage 7/8 disk inner cavity before you apply it to the external surfaces of the drum.
          The part must be dry and cool 120 deg F (49 deg C maximum) before you apply the penetrant to prevent damage to the penetrant liquid.
        2. Make sure that the stage 7/8 inner cavity surfaces are fully covered with the penetrant, with the use of a mirror and UV light source, specially on the area outboard from the bolt holes. The penetrant contact time must not be less than 20 minutes and not more than 60 minutes.

        1. Initial Cleaning.

        2. Do the cleaning initially until all the pooled penetrant and the unwanted surface on the inner cavity is removed. If necessary, use a standard spray gun nozzle to clean the inner surfaces.

        1. Emulsification.

        2. The maximum total CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILIC contact time is 90 seconds.

        3. If the part is held horizontally during the process, put half of the HP compressor stage 3 to 8 drum initially into the emulsifier and let the cavities to fill with emulsifier. Rotate the drum a number of turns before you put the drum fully into the emulsifier.

        4. If the part is held vertically during the process, tap the part lightly on each side when you put the part fully into the emulsifier to make sure that the surface is covered and the air pockets are removed from the inner cavity.

        1. Stop bath.

        2. To prevent contamination of the stop bath, remove the unwanted emulsifier from the internal cavity with a suction tube before you put the part fully into the stop bath. You must complete this procedure in the permitted emulsification time.

        3. Put the part fully into water stop bath to stop the emulsification process.

        1. Final cleaning with water.

        2. Make sure that the HP compressor 7/8 inner cavity surfaces are fully cleaned. If necessary, move and rotate the drum to clean. Use a standard spray gun to clean the inner surfaces.

        1. Remove the pooled water.

        2. Remove the pooled water in the inner cavities of the part with the use of suction device and air blast with maximum of 25 psi (0.17 kPa). If necessary, move and rotate the part to remove the water.

        1. Oven dry. Refer to SPM TASK 70-23-04-230-501.

        2. Dry the part in an air re-circulating oven.

        3. If necessary, apply more air blast with the maximum of 25 psi (0.17 kPa) to remove the remaining pooled water in the inner cavity. If necessary, move and rotate the drum to remove water from the inner cavity. Make sure that the part is made dry in the permitted drying time.

        4. Before you apply the developer, make sure that the HP compressor 7/8 inner cavity surfaces are fully dry with the use of a mirror.

        1. Apply developer.

        2. Apply CoMat 06-032 DRY DEVELOPER to the HP compressor 7/8 inner cavity surfaces. Use a standard spray gun nozzle to apply the developer to the inner surfaces.

        3. Make sure that inner cavities are fully covered with the developer, with the use of a white light source and an inspection mirror.

        4. Let the developer dry for a minimum of 10 minutes before you continue with the inspection.

      1. Examine the HP compressor 7/8 inner cavity at inspection location 10 for cracks.

      2. NOTE

        A second operator will be necessary to help in examining the component.

        Refer to Figure.

      3. Engage the part onto the inspection devices IAE 2R19883 Rotary table inspection device and IAE 2R19884 Adapter or IAE approved alternative, such that the stage 7/8 inner bores get easy access to the illumination equipment. Make sure that the part can be rotated easily related to the viewing and illumination equipment.

      4. Inspection area location 10 must be directly illuminated with UV light held in the fixture IAE 2R19883 Rotary table inspection device or IAE approved alternative, as reflecting UV off the inspection mirror decreases its intensity. The UV light guide must also be used in its operational range to make sure sufficient UV intensity.

      5. Visually examine the HP compressor stage 7/8 inner cavity at inspection location 10 for cracks with the use of a mirror and UV light source.

        1. If a crack indication is found, apply penetrant wipe off procedure. Refer to the SPM TASK 70-23-04-230-501, SUBTASK 70-23-04-230-004

        2. If there is a repeat crack indication, reject the drum.

          NOTE

          Make sure that a rejected drum is disposed in line with the individual overhaul shop procedure.
          1. If there is no repeat crack indication, examine the part for crack indications again after 10 minutes of application of the CoMat 06-030 NON AQUEOUS DEVELOPER.

          2. If crack indications are found, reject the drum.

            NOTE

            Make sure that a rejected drum is disposed in line with the individual overhaul shop procedure.
        1. If there is no crack indication, apply CoMat 06-030 NON AQUEOUS DEVELOPER with aerosol to the HP compressor stage 7/8 inner cavity inspection location 10 and examine immediately.

        2. If there is a repeat crack indication, reject the drum.

          NOTE

          Make sure that a rejected drum is disposed in line with the individual overhaul shop procedure.
          1. If there is no crack indication, examine the part for cracks again after 10 minutes of application of the CoMat 06-030 NON AQUEOUS DEVELOPER.

          2. If crack indications are found, reject the drum.

            NOTE

            Make sure that a rejected drum is disposed in line with the individual overhaul shop procedure.
        1. Final cleaning.

        2. Clean location 10 in accordance with SPM TASK 70-11-26-300-503.

  1. Figure: HP Compressor Stage 7/8 Inner Cavity Profile - Focus Inspection Location

    HP Compressor Stage 7/8 Inner Cavity Profile - Focus Inspection Location

    Figure: HP Compressor Stage 3 to 8 Drum Installation on Inspection Tooling

    HP Compressor Stage 3 to 8 Drum Installation on Inspection Tooling

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Remove CoMat 01-031 reference and add SPM link (REA18VC068)

Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:37676
Enterprise Name:ITW MAGNAFLUX
BU Name:MAGNAFLUX CORPORATION
Street:155 HARLEM AVE
City:GLENVIEW
State:IL
Zip Code:60025
Country:USA
Phone Number:1-847-657-5300
Fax Number:1-847-867-5388
Internet:www.magnaflux.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X222X
Enterprise Name:N/A – REFER TO APPLICABLE COMAT SUFFIX
Manufacturer Code:5FCA4
Supply Number:CoMat 01-025
Type:sp01
Supply Short Name:CoMat 01-025 NITRIC ACID HNO3, TECHNICAL GRADE
Supply Name:CoMat 01-025 NITRIC ACID HNO3, TECHNICAL GRADE
Specification Groups:
Doc NumberType
orTECHNICAL GRADE SP.GR. 1.42 NITRIC ACID
orTECHNICAL GRADE 42 BAUME NITRIC ACID
TECHNICAL GRADE 67.5 WT% NITRIC ACID
Suppliers:
ManufacturerRemarks
5FCA4
K6835
LOCAL
U0PR4
U0SV8
U6726
V272V
Manufacturer Code:X222X
Supply Number:CoMat 06-022
Type:sp01
Supply Short Name:CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY)
Supply Name:CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY)
Specification Groups:
Doc NumberType
ARDROX 985-P14 OMAT: 652 (CHEMETALL OAKITE 985-P14)It is not permitted to mix the selected CoMat 06‐022 letter suffix material with other CoMat 06‐022 letter suffix materials. Where CoMat 06‐022 is specified with no suffix, use one of the CoMat 06‐ 022 letter suffix materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:01PQ6
Supply Number:CoMat 06-030
Type:sp01
Supply Short Name:CoMat 06-030 NON AQUEOUS DEVELOPER
Supply Name:CoMat 06-030 NON AQUEOUS DEVELOPER
Specification Groups:
Doc NumberType
ARDROX 9D1B
Suppliers:
ManufacturerRemarks
01PQ6
D1940
K6858
Manufacturer Code:37676
Supply Number:CoMat 06-032
Type:sp01
Supply Short Name:CoMat 06-032 DRY DEVELOPER
Supply Name:CoMat 06-032 DRY DEVELOPER
Specification Groups:
Doc NumberType
ZYGLO ZP-4B
Suppliers:
ManufacturerRemarks
37676
Manufacturer Code:X222X
Supply Number:CoMat 06-045
Type:sp01
Supply Short Name:CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILIC
Supply Name:CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILIC
Specification Groups:
Doc NumberType
USE THE COMAT 06‐045 LETTER SUFFIX MATERIAL THAT IS APPLICABLE TO THE APPLIED PENETRANT. REFER TO THE APPLICABLE SPM FPI TASK.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:DELETED
Type:sp01
Supply Short Name:DELETED
Supply Name:DELETED
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:0AM53
Tool Number:IAE 2R19883
Tool Name:IAE 2R19883 Rotary table inspection device
Manufacturer Code:0AM53
Tool Number:IAE 2R19884
Tool Name:IAE 2R19884 Adapter
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