TASK 79-22-41-300-031 Oil Scavenge Pump - Related Parts - Nickel Plate The Cover Seat In The Oil Casing Assembly, Repair-031 (VRS5368)

DMC:V2500-A0-79-22-4100-05A-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 79-22-41-300-031 Oil Scavenge Pump - Related Parts - Nickel Plate The Cover Seat In The Oil Casing Assembly, Repair-031 (VRS5368)

Effectivity

FIG/ITEM

PART NO.

01-690

4B7107

Material of component

DESCRIPTION

SYMBOL

MATERIAL

Casing Assembly

A357-T61 (AMS 4219)

General

Price and availability - none

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

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Workshop Inspection EquipmentLOCALWorkshop Inspection Equipment
Grinding MachineLOCALGrinding Machine
FPI inspection stationLOCALFPI inspection station
BasketLOCALBasket
Process Plating TanksLOCALProcess Plating Tanks
OvenLOCALOven
Magnifying glassLOCALMagnifying glass

4x

Vibrating marking pencilLOCALVibrating marking pencil

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-067 STRIPPABLE COATING71410CoMat 02-067

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 79-22-41-320-059 Machine the Cover Seat in the Casing Assembly

    1. Refer to Figure.

      2. Machine the cover seat

      1. Remove all damage and wear. The cover seat must be between 3.5456 to 3.5464 in. (90.060 to 90.080 mm) after the removal of the damage.

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

    2. SUBTASK 79-22-41-230-061 Examine the Casing Assembly

      1. Do the fluorescent penetrant inspection for cracks

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

      2. No cracks are permitted.

    3. SUBTASK 79-22-41-330-069 Nickel Plate the Cover Seat in the Casing Assembly

    1. Refer to Figure.

      2. Apply masking to the areas of the casing assembly not to be plated

      3. Do the nickel plating

      1. Refer to SPM TASK 70-33-08-300-503.

      2. Plate to a sufficient thickness to permit machining to the last dimensions indicated in the reference figure.

      3. Plating external to the piloting diameter area is permitted, but must be removed.

    4. Remove the mask.

      5. Clean and dry the drive gear

      1. Flush with cold water.

      2. Flush with hot water.

      3. Dry with an air blast.

    4. SUBTASK 79-22-41-370-055 De-embrittle the Casing Assembly

      1. Put the casing assembly into an Oven at 241 to 260 deg F (116 to 127 deg C) for 60 to 90 minutes

      1. Do this procedure as soon as possible, in less than 4 hours, after plating.

    5. SUBTASK 79-22-41-220-164 Examine the Casing Assembly

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

      1. Plating must have a constant color.

      2. No circumferential cracks are permitted.

      3. No roughness or blistering is permitted.

    6. SUBTASK 79-22-41-320-060 Machine the Cover Seat in the Casing Assembly

    1. Refer to Figure.

      2. Machine the cover seat

      1. The dimensions must be between 3.5433 to 3.5453 in. (90.000 to 90.050 mm).

      2. Chamfer, where necessary.

    7. SUBTASK 79-22-41-220-165 Examine the Nickel Plated Area

    1. Refer to Figure.

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

      1. Use a Magnifying glass. The natural network crack, shown by grinding is permitted.

      3. Measure the thickness of the plating

      1. Do not accept a thickness of less than 0.0006 in. (0.015 mm), after the last machining is not permitted.

    8. SUBTASK 79-22-41-350-073 Record the Repair

    1. Refer to Figure.

      2. Vibro-engrave VRS5368 adjacent to the part number

      2. Remove the metal lifted by marking.

    9. Figure: Repair Details And Dimensions

    Repair Details And Dimensions

Requirements After Job Completion

Follow-On Conditions

NONE
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:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:71410
Supply Number:CoMat 02-067
Type:sp01
Supply Short Name:CoMat 02-067 STRIPPABLE COATING
Supply Name:CoMat 02-067 STRIPPABLE COATING
Specification Groups:
Doc NumberType
TURCO 5580-G PMC 1835
Suppliers:
ManufacturerRemarks
71410
Manufacturer Code:LOCAL
Tool Number:Basket
Tool Name:Basket
Link not Found
Manufacturer Code:LOCAL
Tool Number:Grinding Machine
Tool Name:Grinding Machine
Link not Found
Manufacturer Code:LOCAL
Tool Number:Oven
Tool Name:Oven
Link not Found
Link not Found
Link not Found