TASK 72-00-41-300-001 HPC Assembly - HPC Rear Outer Case - Replace Missing And/or Damaged Helicoil Or Thinwall Insert(s), Repair-001 (VRS6518)

DMC:V2500-A0-72-00-4102-00A-920A-B|Issue No:002.00|Issue Date:2016-11-01

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 72-00-41-300-001 HPC Assembly - HPC Rear Outer Case - Replace Missing And/or Damaged Helicoil Or Thinwall Insert(s), Repair-001 (VRS6518)

Effectivity

FIG/ITEM

PART NUMBER

ASSEMBLY

02-400

6A2949

A

02-400

6A3557

A

02-400

6A4154

B

02-400

6A5495

B

02-400

6A5682

B

02-400

6A8162

B

02-400

6B1427

B

Material of component

PART IDENT

MATERIAL

HP Compressor Rear Outer Case Assembly

Corrosion Resistant Steel

General

NOTE

This repair scheme is a Special Procedure and does not replace piece part, repair VRS6306 (Repair damaged helicoil or thin wall inserts).

NOTE

If this repair performed without the front case installed, ensure that suitable precautions are taken to avoid damage to the bare rotor blades and stator vanes.

This repair must only be done when the instruction to do so is given in 72-00-41-200-001 Inspection/Check (Special Procedure 01).

This TASK gives the procedure to repair missing and/or damaged helicoil or thinwall insert(s) in the HP compressor rear outer case assembly, by replacement.

The practices and processes referred to in the procedure by the TASK/SUBTASK number are in the SPM.

Price and Availability

Refer to international aero engines.

NOTE

Equipment and materials necessary to do this repair are in the SPM TASKS given below:
SPM TASK 70-23-05-230-501
SPM TASK 70-35-08-300-501
SPM TASK 70-35-26-300-501

NOTE

It is possible that some materials in the consumable materials chart cannot be used for some or all of the necessary applications. Before you use the materials, make sure the types, quantities and applications of the materials necessary are legally permitted in your location. All person must obey all applicable federal, state, local and provincial laws and regulations when it is necessary to work with these materials.

NOTE

To identify the consumable materials, refer to the PCI.

NOTE

Other necessary consumable materials are referred to in the SPM TASKs.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Approved workshop equipmentLOCALApproved workshop equipment
Chemical Cleaning EquipmentLOCALChemical Cleaning Equipment
Penetrant Crack Test EquipmentLOCALPenetrant Crack Test Equipment
Workshop Inspection EquipmentLOCALWorkshop Inspection Equipment
Vacuum cleaning equipmentLOCALVacuum cleaning equipment

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-459 AQUEOUS WIPE CLEANER71410CoMat 01-459
CoMat 02-001 ADHESIVE TAPE (MASKING)LOCALCoMat 02-001
CoMat 02-005 ADHESIVE TAPE (MASKING)LOCALCoMat 02-005
CoMat 02-121 TEMPORARY MARKER PENCIL/CRAYONIE304CoMat 02-121
CoMat 06-064 FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY)LOCALCoMat 06-064

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
INSERT - SCREW THREAD, .250 DIA X 1.5DU1653AGS373290

02-432

Assembly A

INSERT - SCREW THREADU1653AS5276180

02-432

Assembly B

Helicoil insert0AM53AGS373320

02-433

Assembly A

INSERT - SCREW THREADU1653AS5276220

02-433

Assembly B

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-41-220-047 Examine the Assembly

    1. NOTE

      Adjacent components which prevents the access during the repair or damaged components, must be removed. Use applicable disassembly tasks.

      Refer to Figure, Figure and Figure.

    2. Examine and identify the repair location.

      3. Mark all damaged insert hole(s).

      1. Make sure access to all the repair areas.

    2. SUBTASK 72-00-41-350-001 Mask the Assembly

    1. NOTE

      This SUBTASK is to prevent foreign objects falling into the engine.

      Refer to Figure, Figure and Figure.

    2. Mask all repair holes opening to the inner side of engine.

    4. Mask holes other than repair holes.

      5. Mask all open holes adjacent to the repair area.

    3. SUBTASK 72-00-41-350-002-A00 Remove the Damaged Helicoil Insert(s), Assembly A

    1. Remove the damaged helicoil insert(s).

      2. Refer to SPM TASK 70-35-08-300-501, SUBTASK 70-35-08-350-001.

    4. SUBTASK 72-00-41-350-002-B00 Remove the Damaged Thinwall Insert(s), Assembly B

    1. Remove the damaged thinwall insert(s).

      2. Refer to SPM TASK 70-35-26-300-501, SUBTASK 70-35-26-350-001.

    5. SUBTASK 72-00-41-110-002 Chemically Clean

    1. Locally clean the repair hole(s).

      2. Locally clean the repair hole(s) to remove the debris.

    3. Locally degrease the repair area.

      4. Refer to SPM TASK 70-11-03-300-503, SUBTASK 70-11-03-300-003.

    6. SUBTASK 72-00-41-220-049 Examine the Repair Area

    1. Refer to Figure, Figure and Figure.

    2. Examine the repair area.

      3. Visually examine the repair area.

      1. Make sure the damaged insert is removed completely.

      2. Make sure all debris is removed.

    7. SUBTASK 72-00-41-230-002 Do a Crack Test

    1. Do a local penetrant crack test.

    8. SUBTASK 72-00-41-110-004 Chemically Clean

    1. Locally clean the part to remove penetrant.

      2. Refer to SPM TASK 70-11-03-300-503, SUBTASK 70-11-03-300-003.

    9. SUBTASK 72-00-41-350-004-A00 Install the Helicoil Insert(s), Assembly A

    1. Refer to Figure, Figure and Figure.

    2. Install the helicoil insert(s).

      3. Refer to SPM TASK 70-35-08-300-501, SUBTASK 70-35-08-350-002.

      1. Use AGS3732 insert HPC Rear Outer Case And Related Parts (72-41-23, 02-432), 90 off and/or AGS3733 insert HPC Rear Outer Case And Related Parts (72-41-23, 02-433), 20 off as necessary.

    10. SUBTASK 72-00-41-350-004-B00 Install the Thinwall Insert(s), Assembly B

    1. CAUTION

      DO NOT PUT TOO MUCH FORCE FOR SWAGING OPERATION. IT CAN DAMAGE THE COMPRESSOR CASE.

      Refer to Figure, Figure and Figure.

    2. Install the thinwall insert(s).

      3. Refer to SPM TASK 70-35-26-300-501, SUBTASK 70-35-26-350-001.

      1. Use AS52761 INSERT - SCREW THREAD (02-432), 80 off and/or AS52762 INSERT - SCREW THREAD (02-433), 20 off, as necessary.

    11. SUBTASK 72-00-41-220-050-A00 Examine the Helicoil Insert(s), Assembly A

    1. Refer to Figure, Figure and Figure.

    2. Examine the helicoil insert(s).

      3. Refer to SPM TASK 70-35-08-300-501, SUBTASK 70-35-08-220-001.

    12. SUBTASK 72-00-41-220-050-B00 Examine the Thinwall Insert(s), Assembly B

    1. Refer to Figure, Figure and Figure.

    2. Examine the thinwall insert(s).

      3. Refer to SPM TASK 70-35-26-300-501, SUBTASK 70-35-26-350-001.

    13. SUBTASK 72-00-41-220-051 Remove the Masking

    1. Refer to Figure, Figure and Figure.

    2. Remove the masking.

    3. Remove all the masking done in Step.

    14. SUBTASK 72-00-41-350-006 Record the Repair

    1. Record the repair.

    2. Record VRS6518 in the Engine Log Book.

    15. Figure: Repair Details and Dimensions - Assembly A and Assembly B

    Repair Details and Dimensions - Assembly A and Assembly B

    Figure: Repair Details and Dimensions - Assembly A

    Repair Details and Dimensions - Assembly A

    Figure: Repair Details and Dimensions - Assembly A

    Repair Details and Dimensions - Assembly A

    Figure: Repair Details and Dimensions - Assembly B

    Repair Details and Dimensions - Assembly B

    Figure: Repair Details and Dimensions - Assembly B

    Repair Details and Dimensions - Assembly B

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the effectivity table to add PN 6B1427 and spare parts. (09VR891A)

Change Type:

Added spare reference in install the thinwall insert(s), assembly B. (09VR891A)

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:71410
Enterprise Name:HENKEL CORPORATION (WAS: TURCO PRODUCTS, INC)
BU Name:HENKEL CORPORATION (WAS: TURCO PRODUCTS, INC)
Street:32100 STEPHENSON HIGHWAY
City:MADISON HEIGHTS
State:MI
Zip Code:48071
Country:USA
Phone Number:1-248-583-9300
Fax Number:1-248-583-2976
Internet:www.aerospace.henkel.com
Manufacturer Code:IE304
Enterprise Name:DELETED
BU Name:DELETED,SEE CAGE CODE 0V6W9
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:U1653
Enterprise Name:Society Of British Aerospace Companies, LTD.
Part Number:AGS3732
Part Name:INSERT - SCREW THREAD, .250 DIA X 1.5D
Manufacturer Code:U1653
Link not Found
Part Number:AS52761
Part Name:INSERT - SCREW THREAD
Manufacturer Code:U1653
Part Number:AS52762
Part Name:INSERT - SCREW THREAD
Manufacturer Code:U1653
Manufacturer Code:71410
Supply Number:CoMat 01-459
Type:sp01
Supply Short Name:CoMat 01-459 AQUEOUS WIPE CLEANER
Supply Name:CoMat 01-459 AQUEOUS WIPE CLEANER
Specification Groups:
Doc NumberType
SPMC 148-1TURCO 6780
Suppliers:
ManufacturerRemarks
71410
Manufacturer Code:LOCAL
Supply Number:CoMat 02-001
Type:sp01
Supply Short Name:CoMat 02-001 ADHESIVE TAPE (MASKING)
Supply Name:CoMat 02-001 ADHESIVE TAPE (MASKING)
Specification Groups:
Doc NumberType
OMAT: 230 (RR REF)ZINC OXIDE AT142
JCR-197 (JAEC REF)ZINC OXIDE AT142
Suppliers:
ManufacturerRemarks
LOCAL
K6835
U0415
Manufacturer Code:LOCAL
Supply Number:CoMat 02-005
Type:sp01
Supply Short Name:CoMat 02-005 ADHESIVE TAPE (MASKING)
Supply Name:CoMat 02-005 ADHESIVE TAPE (MASKING)
Specification Groups:
Doc NumberType
OMAT: 2/94 (RR REF)AT 7 BLACK, WATERPROOF
Suppliers:
ManufacturerRemarks
LOCAL
U0415
K6835
Manufacturer Code:IE304
Supply Number:CoMat 02-121
Type:sp01
Supply Short Name:CoMat 02-121 TEMPORARY MARKER PENCIL/CRAYON
Supply Name:CoMat 02-121 TEMPORARY MARKER PENCIL/CRAYON
Specification Groups:
Doc NumberType
OMAT: 261BEROL VERITHIN (HARD TYPE)
Suppliers:
ManufacturerRemarks
IE304
K5720
K6835
LOCAL
Manufacturer Code:X222X
Supply Number:CoMat 06-064
Type:sp01
Supply Short Name:CoMat 06-064FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY)
Supply Name:CoMat 06-064 FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY)
Specification Groups:
Doc NumberType
It is not permitted to mix the selected CoMat 06‐064 letter suffix material with other CoMat 06‐064 letter suffix materials.Where CoMat 06‐064 is specified with no suffix, use one of the CoMat 06‐064 letter suffix materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Tool Number:Approved workshop equipment
Tool Name:Approved workshop equipment
Link not Found
Link not Found
Manufacturer Code:LOCAL
Tool Number:Vacuum cleaning equipment
Tool Name:Vacuum cleaning equipment
Link not Found