TASK 72-45-22-300-005 HPT Stage 1 Duct Support Segment - Plasma Coat The Segment Front Face, Repair-005 (VRS3764)

DMC:V2500-A0-72-45-2200-01A-609A-C|Issue No:001.00|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 72-45-22-300-005 HPT Stage 1 Duct Support Segment - Plasma Coat The Segment Front Face, Repair-005 (VRS3764)

Effectivity

FIG/ITEM

PART NO.

01-010

2A4130

Material of component

DESCRIPTION

IAE

SYMBOL

MATERIAL

Stage 1 HPT duct support set

Nickel alloy

General

Price and availability - Refer to IAE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
IAE 3P16273 Grind fixture0AM53IAE 3P16273

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINEDK026CoMat 03-066

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-22-350-064 Remove the Damage or Wear and all the Coat from the Front Face of the Detail Segment

    1. Refer to Figure and Figure.

    2. Remove the damage or wear and all of the coat from the front face of the detail segment by one or more of the methods that follow.

      3. Remove all the coat.

      1. Refer to the SPM TASK 70-33-79-300-503.

      4. Remove all the coat.

      1. Refer to the SPM TASK 70-33-90-300-503.

      5. Grind to remove the damage or wear and all the coat. Remove the minimum amount of parent material necessary to do the repair.

    2. SUBTASK 72-45-22-350-065 Prepare the Part for Coat

    1. Refer to Figure and Figure.

      2. Clean the part.

      1. Refer to the SPM TASK 70-11-03-300-503.

    3. Do a dimensional inspection of the repair area. Make sure that all of the coating is removed.

      4. Do a fluorescent penetrant inspection of the part.

      5. Grit blast the front face of the detail segment.

      1. Refer to SPM TASK 70-34-18-380-501.

        Mask areas which are not to be coated.

        Grit blast out of repair area shown is not permitted.

    3. SUBTASK 72-45-22-340-055 Apply Plasma Coating on the Front Face of the Detail Segment

    1. Refer to Figure and Figure.

      2. Plasma coat the repair area.

      1. Coat to a sufficient thickness to permit finish grinding.

        Coat in the holes or out of repair area shown is not permitted. Use masks.

        Final coating thickness, after finsh grinding, must be 0.002 to 0.008 in. (0.05 to 0.20 mm).

    4. SUBTASK 72-45-22-100-001 Clean the Part

    1. Refer to Figure and Figure.

      2. Clean the part.

      1. Refer to the SPM TASK 70-11-03-300-503.

    5. SUBTASK 72-45-22-220-080 Examine the Repaired Area

    1. Refer to Figure and Figure.

    2. Do a dimensional inspection of the part.

      3. Examine the repaired coat.

      1. Refer to the SPM TASK 70-34-03-220-001.

    6. SUBTASK 72-45-22-350-066 Identify the Part

    1. Refer to Figure and Figure.

      2. Mark VRS3764 on the repaired part adjacent to the part number.

      1. Make a permanent mark by the procedures given in the SPM TASK 70-09-00-400-501.

        NOTE

        If VRS3764 is marked on the part, do not mark the part again.

        Use a vibratory pin method.

    7. Figure: Repair Details and Dimensions

    Sheet 1

    Legend
    Repair Details and Dimensions

    Sheet 1

    Close

    Figure: Repair Details and Dimensions

    Sheet 2

    Legend
    Repair Details and Dimensions

    Sheet 2

    Close

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:DK026
Enterprise Name:STARCK GMBH AND CO KG
BU Name:STARCK GMBH AND CO KG
Street:IM SCHLEEKE 78-91
City:38642 GOSLAR
Country:GERMANY
Phone Number:49-5321-7510
Fax Number:49-5321-7516 192
Internet:www.hcstarck.com
Manufacturer Code:DK026
Supply Number:CoMat 03-066
Type:sp01
Supply Short Name:CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINE
Supply Name:CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINE
Specification Groups:
Doc NumberType
AMS 7875 (PW REF)AMPERIT 585.435
Suppliers:
ManufacturerRemarks
DK026
Manufacturer Code:0AM53
Tool Number:IAE 3P16273
Tool Name:IAE 3P16273 Grind fixture