TASK 72-44-50-300-017 HPT Stage 1 Cooling (TOBI) Duct - Weld The Air Pressure Passage Cracks, Repair-017 (VRS3808)

DMC:V2500-A0-72-44-5001-04A-627A-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 72-44-50-300-017 HPT Stage 1 Cooling (TOBI) Duct - Weld The Air Pressure Passage Cracks, Repair-017 (VRS3808)

Effectivity

FIG/ITEM

PART NO.

01-010

2A0008-01

01-010

2A1997-01

01-010

2A1997-001

01-010

2A1997-002

01-010

2A1997-003

01-010

2A2141-01

01-010

2A3180-01

01-010

2A3329-01

01-010

2A3487-01

01-010

2A3487-001

01-010

2A3491-01

01-010

2A3914-01

01-010

2A3914-001

01-010

2A4086

Material of component

DESCRIPTION

SYMBOL

MATERIAL

Stage 1 HPT cooling duct assembly

-

Nickel alloy

General

Price and availability - Refer to IAE

The practices and processes referred to in this 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

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 03-284 WELDING FILLER WIRE, NiBASELOCALCoMat 03-284

Spares

NONE

Safety Requirements

CAUTION

YOU CANNOT USE THIS PROCEDURE TO REPAIR STAGE 1 HPT COOLING DUCT ASSEMBLIES THAT ARE PART OF AN ENGINE CONFIGURATION THAT USES STAGE 1 HPT COOLING AIR PRESSURE TUBE. THIS REPAIR PLUG WELDS THE AIR PRESSURE PASSAGE OPENING, PREVENTING THE AIR PRESSURE TUBE FROM FUNCTIONING. REFER TO SB V2500-ENG-0166 FOR REMOVAL OF THE AIR PRESSURE TUBE.

Procedure

    1. SUBTASK 72-44-50-350-083 Remove the Honeycomb Ring

      1. Remove the honeycomb ring from the Stage 1 HPT Duct Assembly.

      2. Repair, VRS3179 TASK 72-44-50-300-003 (REPAIR-003).

    1. SUBTASK 72-44-50-350-084 Rout Cracks

    2. Refer to Figure and Figure.

    3. Rout to fully remove the cracks in the Air Pressure Passage Boss, below the flange lip.

    1. SUBTASK 72-44-50-230-070 Examine the Repair Area

      1. NOTE

        Crack can be removed before weld. It can be done by a certified welder. It is not necessary to get certification from a fluorescent penetrant inspector.

        Do a fluorescent penetrant inspection of the repair area.

      2. Refer to the SPM TASK 70-23-05-230-501. Use high sensitivity procedure.

    1. SUBTASK 72-44-50-110-063 Clean the Repair Area

    2. Clean the area to be welded with a stainless steel wire brush.

      1. Solvent wipe the area to be welded.

      2. Refer to the SPM TASK 70-11-26-300-503.

    1. SUBTASK 72-44-50-310-057 Weld Repair

    2. NOTE

      Locally manufacture suitable tooling to minimize weld distortion.
      When you repair cracks, the air passage must be plug welded.

      Refer to Figure.

      1. Weld build up the routed area. Use the Manual Gas Tungsten Arc Weld (GTAW-MA) procedure.

      1. Plug weld opening of the air pressure passage. Use the Manual Gas Tungsten Arc Weld (GTAW-MA) procedure.

    1. SUBTASK 72-44-50-370-059 Heat Treat the Repaired Area

      1. NOTE

        Heat treatment can be done with the honeycomb installation by Repair, VRS3179 TASK 72-44-50-300-003 (REPAIR-003).

        Solution heat treat and precipitation harden the stage 1 HPT cooling duct.

      2. Refer to the SPM TASK 70-37-32-370-501.

      3. Solution heat treat the duct at 1725 to 1775 deg F (941 to 968 deg C) for one hour in a protective atmosphere.

      4. Cool at 40 deg F (4 deg C) for one minute or faster to 1300 to 1350 deg F (704 to 732 deg C).

      5. Precipitation heat treat the duct at 1300 to 1350 deg F (704 to 732 deg C) for eight hours.

      6. Furnace cool at a rate of 100 deg F (38 deg C) maximum for one hour to 1125 to 1175 deg F (607 to 635 deg C).

      7. Hold at 1125 to 1175 deg F (607 to 635 deg C) for eight hours.

      8. Air cool to room temperature.

    1. SUBTASK 72-44-50-230-071 Examine the Part

      1. Do a fluorescent penetrant inspection of the duct.

      2. Refer to the SPM TASK 70-23-03-230-501.

    1. SUBTASK 72-44-50-350-085 Blend the Repaired Area

    2. Refer to Figure.

      1. NOTE

        It is not necessary to blend the inner diameter of the air pressure passage since the rear opening of the passage will be plug welded.

        Blend the repaired area. A mismatch of +0.010 in. (+0.25 mm) is permitted.

      2. Refer to the SPM TASK 70-35-03-300-501.

    1. SUBTASK 72-44-50-110-064 Clean the Repaired Area

      1. Clean the duct.

      2. Refer to the SPM TASK 70-11-26-300-503.

    1. SUBTASK 72-44-50-220-125 Examine the Part

    2. Refer to Figure.

    3. Examine the duct for hardness. Surface M must be Rockwell 34 HRC minimum or equivalent.

      1. Do a dimensional inspection of the part.

      2. Refer to TASK 72-44-50-200-000 (INSPECTION-000).

    1. SUBTASK 72-44-50-350-086 Identify the Repair

    2. Refer to Figure.

      1. Make a mark "VRS3808" adjacent to the part number.

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

    1. SUBTASK 72-44-50-350-087 Install the Honeycomb Ring

      1. Install the honeycomb ring to the Stage 1 HPT Duct Assembly.

      2. Repair, VRS3179 TASK 72-44-50-300-003 (REPAIR-003).

  1. 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

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 03-284
Type:sp01
Supply Short Name:CoMat 03-284 WELDING FILLER WIRE, Ni BASE
Supply Name:CoMat 03-284 WELDING FILLER WIRE, NiBASE
Specification Groups:
Doc NumberType
INCONEL 718 AMS 5832 AWS 5.14 MSRR9500/220
INCONEL 718 AMS 5832 AWS 5.14CLASS ER NI FE Cr-2 OMAT:3/206
INCONEL 718 AMS 5832 AWS 5.14CLASS ER NI FE Cr-2
Suppliers:
ManufacturerRemarks
LOCAL
28553
IE137
08489
IE508
0ZDB5
2R602
55596
58401
80357
K6835