TASK 79-22-41-300-016 Oil Scavenge Pump - Related Parts - Nickel Plate The Piloting Diameter Of The Cover Assembly, Repair-016 (VRS5351)

DMC:V2500-A0-79-22-4100-02A-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 79-22-41-300-016 Oil Scavenge Pump - Related Parts - Nickel Plate The Piloting Diameter Of The Cover Assembly, Repair-016 (VRS5351)

Effectivity

FIG/ITEM

PART NO.

01-330

4B7002

01-330

4B7318

01-330

4B7347

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. 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
FPI Inspection StationLOCALFPI Inspection Station
BasketLOCALBasket
Process Plating TanksLOCALProcess Plating Tanks
OvenLOCALOven
Magnifying glassLOCALMagnifying glass
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 79-22-41-320-068 Machine the Piloting Diameter of the Cover Assembly

    1. Refer to Figure.

      2. Machine the piloting diameter

      1. Remove all damage and wear. The piloting diameter must be between 4.9901 and 4.9956 in. (126.750 and 126.89 mm) after the removal of the damage.

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

    2. SUBTASK 79-22-41-230-163 Examine the Cover 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 79-22-41-330-072 Nickel Plate the Piloting Diameter of the Cover Assembly

    1. Refer to Figure.

      2. Mask the areas of the cover 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. The plating out of the piloting diameter area is permitted, but must be removed.

    4. Remove the mask

      5. Clean and dry the cover assembly

      1. Flush with cold water.

      2. Flush with hot water.

      3. Dry with air blast.

    4. SUBTASK 79-22-41-370-057 De-embrittle the Cover 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 79-22-41-220-168 Examine the Cover Assembly

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

      1. Plating must have a constant color. No circumferential cracks are permitted.

      2. No roughness or blistering is permitted.

    6. SUBTASK 79-22-41-320-069 Machine the Piloting Diameter of the Cover Assembly

    1. Refer to Figure.

      2. Machine the piloting diameter

      1. Machine the piloting diameter, the dimension must be between 4.9980 to 4.9960 in. (126.950 to 126.900 mm).

      2. Chamfer, where necessary

    7. SUBTASK 79-22-41-220-169 Examine the Nickel Plated Area

    1. Refer to Figure.

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

      1. Use a 4X Magnifying glass. The natural network crack, emphasized 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

    8. SUBTASK 79-22-41-350-075 Record the Repair

    1. Refer to Figure.

      2. Vibro engrave VRS5351 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
Link not Found
Link not Found
Manufacturer Code:LOCAL
Tool Number:Oven
Tool Name:Oven
Link not Found
Link not Found
Manufacturer Code:LOCAL
Tool Number:Workshop inspection equipment
Tool Name:Workshop inspection equipment