TASK 72-60-29-300-010 Deoiler Housing Assembly - Nickel Plate The Impeller Seat, Repair-010 (VRS5085)

DMC:V2500-A0-72-60-2904-04A-647A-C|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 72-60-29-300-010 Deoiler Housing Assembly - Nickel Plate The Impeller Seat, Repair-010 (VRS5085)

Effectivity

FIG/ITEM

PART NO.

01-390

4B0088

01-390

4B0315

01-390

4B0347

Material of component

PART IDENT

IAE

SYMBOL

MATERIAL

Deoiler assembly

Aluminum alloy

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
OvenLOCALOven
Magnifying Glass, 4xLOCALMagnifying Glass, 4x

Consumables, Materials and Expendables

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

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-60-29-320-111 Machine the Impeller Seat of the Deoiler Housing

    1. Refer to Figure.

      2. Machine diameter of impeller seat.

      1. Seat diameter must be between 3.3012 in. and 3.2972 in. (83.85 mm and 83.75 mm) after removal of damage.

      2. Remove all damage and wear.

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

    2. SUBTASK 72-60-29-220-192 Examine the Deoiler Housing

      1. Do fluorescent penetrant inspection for cracks.

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

      2. No cracks are permitted.

    3. SUBTASK 72-60-29-330-086 Nickel Plate the Impeller Seat of the Deoiler Housing

    1. Refer to Figure.

      2. Mask areas of deoiler housing not to be plated.

      3. Do the nickel plating.

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

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

      3. Plating out of the seat diameter is permitted but must be removed.

    4. Remove the mask.

      5. Clean and dry the support.

      1. Flush with cold water.

      2. Flush with hot water.

      3. Dry with air blast.

    4. SUBTASK 72-60-29-370-084 De-Embrittle the Deoiler Housing

      1. Put housing into the oven at 241 deg F to 260 deg F (116 deg C to 127 deg C) for 60 to 90 minutes.

      1. Do this procedure in less than 4 hours after plating.

    5. SUBTASK 72-60-29-220-193 Examine the Deoiler Housing

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

      1. Plating must have a constant colour.

      2. No circumferential cracks are permitted.

      3. No roughness and blisters are permitted.

    6. SUBTASK 72-60-29-320-112 Machine the Impeller Seat of the Deoiler Housing

    1. Refer to Figure.

      2. Machine diameter.

      1. Last dimension of seat diameter must be between 3.2953 in. and 3.2933 in. (83.70 mm and 83.65 mm).

      2. Clean edges of the groove and chamfer where necessary.

    7. SUBTASK 72-60-29-220-194 Examine the Nickel Plated Area

    1. Refer to Figure.

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

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

    8. SUBTASK 72-60-29-350-106 Record the Repair

      1. Make a mark VRS5085 adjacent to the part number.

      1. Refer to SPM TASK 70-09-00-400-501 and SUBTASK 70-09-00-400-001 .

    9. Figure: Nickel Plate the Diameter of the Impeller Seat

    Nickel Plate the Diameter of the Impeller Seat

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the effectivity table to add part number 4B0347. (11VF849A)

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
Link not Found
Manufacturer Code:LOCAL
Tool Number:Magnifying Glass, 4x
Tool Name:Magnifying Glass, 4x
Manufacturer Code:LOCAL
Tool Number:Oven
Tool Name:Oven
Manufacturer Code:LOCAL
Tool Number:Workshop inspection equipment
Tool Name:Workshop inspection equipment