TASK 72-50-53-300-063 Turbine Exhaust Case (TEC) - Nickel Plate The Oil Jet Mating Diameter, Repair-063 (VRS3246)

DMC:V2500-A0-72-50-5301-09A-647A-C|Issue No:002.00|Issue Date:2013-11-01

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 72-50-53-300-063 Turbine Exhaust Case (TEC) - Nickel Plate The Oil Jet Mating Diameter, Repair-063 (VRS3246)

Effectivity

FIG/ITEM

PART NO.

21-300

2A1209-01

21-300

2A2620-01

21-300

2A3111-01

21-300

2A3183-01

21-300

2A3455-01

21-300

2A3183-101

21-300

2A4258-01

21-300

2A4263-01

Material of component

PART IDENT

SYMBOL

MATERIAL

Turbine Exhaust Case

-

AMS 5354 stainless steel

General

Price and availability - refer to IAE

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
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 72-50-53-320-107 Machine the Oil Jet Mating Diameter

    1. Refer to: Figure

      2. Machine the oil jet mating diameter before nickel plate.

      1. Keep material removal to a miniumum so the plating will be 0.002 to 0.012 in. (0.05 to 0.30 mm) thick after finish machining.

        If the diameter was plated before, you can strip the plating.

        Refer to the SPM TASK 70-33-05-300-503.

    2. SUBTASK 72-50-53-230-094 Examine the Turbine Exhaust Case

      1. Fluorescent penetrant inspect the surface to be plated.

      1. Refer to the SPM TASK 70-23-02-230-501.

        No cracks are permitted.

    3. SUBTASK 72-50-53-330-070 Nickel Plate the Oil Jet Mating Diameter

    1. Refer to: Figure

      2. Apply a mask to the areas not to be plated.

      3. Nickel plate the diameter.

      1. Refer to the SPM TASK 70-33-06-300-501.

        Apply the plating to a sufficient thickness to permit finish machining.

        NOTE

        Plating outside the designated area is permitted but must be removed.

    4. Remove the mask.

    4. SUBTASK 72-50-53-110-111 Clean the Turbine Exhaust Case

      1. Clean and dry the case.

      1. Flush the case with cold water, then flush with hot water.

        Dry with air blast.

    5. SUBTASK 72-50-53-370-077 Bake the Turbine Exhaust Case after Nickel Plate

      1. Bake after nickel plate.

      1. Bake at 360 to 390 deg F (182 to 199 deg C) for three hours.

        Do this process as soon as possible in less than one hour after plating.

    6. SUBTASK 72-50-53-320-108 Machine the Oil Jet Mating Diameter after Nickel Plate

    1. Refer to: Figure

      2. Finish machine the diamter after nickel plate.

      1. Machine the diameter to 0.538 to 0.542 in. (13.66 to 13.77 mm).

    7. SUBTASK 72-50-53-220-205 Examine the Repair

      1. Visually examine the plated area for cracks and plating that is not attached to the base metal.

      1. Use a 4X or greater magnifying glass.

    8. Figure: Repair Details and Dimensions

    Repair Details and Dimensions

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Editorial correction due to conversion

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
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