TASK 72-60-43-300-009 Angle Gearbox Driven Bevel Gearshaft - Chromium Plate The Roller Bearing Shoulder, Repair-009 (VRS5628)

DMC:V2500-A0-72-60-4301-03A-647A-C|Issue No:001.00|Issue Date:2014-05-01

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 72-60-43-300-009 Angle Gearbox Driven Bevel Gearshaft - Chromium Plate The Roller Bearing Shoulder, Repair-009 (VRS5628)

Effectivity

FIG/ITEM

PART NO.

01-420

4P2206

Material of component

PART IDENT

SYMBOL

MATERIAL

Bevel Gearshaft

10NiCrMo40

General

Price and availability - none

The practices and processes referred to in the procedure by the TASK numbers are in the SPP

NOTE

  1. To identify the consumable materials refer to the PCI

  2. Other consumable materials are given in the SPM

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Workshop inspection equipmentLOCALWorkshop inspection equipment
Grinding MachineLOCALGrinding Machine
FurnaceLOCALFurnace
Magnifying glass, 5xLOCALMagnifying glass, 5x
Vibrating marking pencilLOCALVibrating marking pencil

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 05-030 CAST STEEL SHOT DELETED0AM53CoMat 05-030

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-60-43-320-065 Machine the Roller Bearing Shoulder

    1. Refer to Figure.

      2. Machine the roller bearing shoulder.

      1. The preplating dimension must be 1.3691 in. minimum (34.775 mm minimum) in relation to surface D.

      2. Remove all damage and wear.

      3. Keep the removal of material to the minimum necessary to remove the damage.

      4. Surface rough must be 63 microin. (1.6 micron) before plating.

    2. SUBTASK 72-60-43-240-061 Examine the Bevel Gearshaft

      1. Do the magnetic particle inspection for cracks.

      1. Refer to the SPM TASK 70-24-01-240-501.

      2. No cracks are permitted.

    3. SUBTASK 72-60-43-380-057 Shot-Peen the Roller Bearing Shoulder

      1. Shot-peen the roller bearing mating face to an intensity of 0.006A to 0.008A in.

      1. Refer to the SPM TASK 70-38-04-300-503.

    4. SUBTASK 72-60-43-330-058 Chromium Plate the Roller Bearing Shoulder

      1. Do the chromium plate.

      1. Refer to the SPM TASK 70-33-02-330-501.

      2. Plate to a sufficient thickness to permit the machining to the last dimensions.

      3. The plate out of the roller bearing mating face is permitted but must be removed.

    5. SUBTASK 72-60-43-370-061 De-embrittle the Gearshaft

      1. Put the gearshaft into the oven at 260 to 289 deg F (127 to 143 deg C) for 5 hours.

      1. Do this process as soon as possible in less than 4 hours after the plating.

    6. SUBTASK 72-60-43-220-087 Examine the Plating

      1. Do the visual inspection of the plating for finish, cracks and adhesion.

      1. Plating must have a constant color.

      2. No bubbles or sign of burned metal are permitted.

    7. SUBTASK 72-60-43-320-066 Machine the Roller Bearing Shoulder

    1. Refer to Figure.

      2. Machine the roller bearing shoulder.

      1. The last dimension must be between 1.3858 to 1.3701 in. (35.800 to 34.800 mm) in relation to surface D.

    8. SUBTASK 72-60-43-220-088 Examine the Chromium Plated Area

      1. Do the visual inspection of the plated area for cracks and adhesion.

      2. The natural network of crack, made more apparent by grinding, is permitted.

      2. Measure the thickness of the plating.

      1. Do not accept thickness less than 0.001 in. (0.025 mm) after the last machining.

    9. SUBTASK 72-60-43-350-060 Record the Repair

      1. Vibro engrave VRS5628 adjacent to the part number.

      2. Remove the metal lifted by marking.

      3. Refer to the SPM TASK 70-09-00-400-501.

    10. Figure: Repair details and dimensions

    Repair details and dimensions

Requirements After Job Completion

Follow-On Conditions

NONE
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:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:0AM53
Supply Number:CoMat 05-030
Type:sp01
Supply Short Name:CoMat 05-030 CAST STEEL SHOT DELETED
Supply Name:CoMat 05-030 CAST STEEL SHOT DELETED
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
0AM53
Manufacturer Code:LOCAL
Tool Number:Furnace
Tool Name:Furnace
Manufacturer Code:LOCAL
Tool Number:Grinding Machine
Tool Name:Grinding Machine
Link not Found
Link not Found
Manufacturer Code:LOCAL
Tool Number:Workshop inspection equipment
Tool Name:Workshop inspection equipment