TASK 72-41-34-300-018 HPC Vane Actuating Crankshaft - Replace The Inserts In The Adaptable Crankshaft, Repair-018 (VRS6258)

DMC:V2500-A0-72-41-3411-00A-920A-C|Issue No:002.00|Issue Date:2016-08-01

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 72-41-34-300-018 HPC Vane Actuating Crankshaft - Replace The Inserts In The Adaptable Crankshaft, Repair-018 (VRS6258)

Effectivity

FIG/ITEM

PART NO

01-600

6A3805

01-600

6A4316

01-600

6A5889

01-600

6A7804

01-600

6A7975

Material of component

PART IDENTIFICATION

RR SYMBOL

MATERIAL

HP Compressor Vane Actuating Crankshaft

EAK

Jethete

General

This Repair must only be done when the instruction is given in TASK 72-41-34 Inspection/Check.

This Repair has been issued for the HP compressor adaptable crankshaft assembly insert replacement.

This repair scheme is to replace the inserts when they are broken, worn, cross threaded or missing. The inserts to be replaced are No. 10 0.190 inch diameter, 32 threads per inch, screw lock type.

Where reference is made to a SUBTASK within a TASK in the form.TASK, SUBTASK" the operator must read and apply the complete TASK. The SUBTASK is listed only when the TASK gives options for the processing of the component. The specified SUBTASK instructs what option must be used during application of the TASK for the successful completion of the repair scheme VRS6258.

TASKS identified by SPM TASK are in the Standard Practices Manual (SPM).

Price and availability

Refer to IAE

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 persons 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 Overhaul Materials Manual (OMat).

NOTE

Other necessary consumable materials are referred to in the OP TASKS in this TASK.

NOTE

Equivalent materials or equipment can be used.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Standard workshop equipmentLOCALStandard workshop equipment
10X Binocular inspection equipmentLOCAL10X Binocular inspection equipment

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 06-063 FLUORESCENT PENETRANT (POST-EMULSIFIED MEDIUM SENSITIVITY)LOCALCoMat 06-063

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Helicoil insertLOCALAGS3733

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-41-34-350-058 Remove the Damaged Helicoil Insert

      1. Remove the damaged helicoil insert.

      1. The SPM TASK 70-35-08-300-501 SUBTASK 70-35-08-350-001.

    2. SUBTASK 72-41-34-084-001 Fluorescent Penetrant Inspect

      1. Do a crack test of the threads on the holes the helicoil inserts were removed from.

      1. Refer to SPM TASK 70-23-01-230-501.

          1. If cracking is detected.

          1. Reject.

          2. If no cracking is detected.

          1. Continue with the repair.

    3. SUBTASK 72-41-34-350-059 Install the Helicoil Insert

      1. Install the helicoil insert.

      1. The SPM TASK 70-35-08-300-501 SUBTASK 70-35-08-350-002.

    4. SUBTASK 72-41-34-230-084-001 Do a Crack Test

      1. Do a crack test on the repaired area.

      1. Refer to the SPM TASK 70-23-01-230-501.

        Cracks are not permitted.

    5. SUBTASK 72-41-34-230-084-002 Do a Crack Test

    1. Deleted.

    6. SUBTASK 72-41-34-220-002 Do a Visual Inspection

      1. Do a visual inspection for cracking or other defect indications of the helicoil insert and the surrounding area of the HP Compressor Vane Actuating Crankshaft.

          1. If any defects are detected.

          1. Reject.

          2. If no defects are detected.

          1. Continue with the repair.

    7. SUBTASK 72-41-34-220-188 Do an Inspection of the Helicoil Inserts

      1. Do an inspection of the helicoil inserts.

      1. The SPM TASK 70-35-08-300-501 SUBTASK 70-35-08-220-001.

        2. If the wirethread is not in a satisfactory condition.

        1. Repeat the repair from Step.

        3. If the wirethread insert is in a satisfactory condition.

        1. Continue with the repair.

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the effectivity table. (89VR863A)

Change Type:

Added procedural steps 2, 6 and deleted step 5. (89VR863A)

Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Manufacturer Code:X222X
Supply Number:CoMat 06-063
Type:sp01
Supply Short Name:CoMat 06-063 FLUORESCENT PENETRANT (POST-EMULSIFIED MEDIUM SENSITIVITY)
Supply Name:CoMat 06-063 FLUORESCENT PENETRANT (POST-EMULSIFIED MEDIUM SENSITIVITY)
Specification Groups:
Doc NumberType
It is not permitted to mix the selected CoMat 06‐063 letter suffix material with other CoMat 06‐063 letter suffix materials. Where CoMat 06‐063 is specified with no suffix, use one of the CoMat 06‐063 letter suffix materials.
Suppliers:
ManufacturerRemarks
X222X
Link not Found
Link not Found