TASK 75-24-48-300-009 HPT ACC Air Manifold - Re-shape the Manifold - Repair-009 (VRS1531)

DMC:V2500-A0-75-24-4801-00A-271A-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 75-24-48-300-009 HPT ACC Air Manifold - Re-shape the Manifold - Repair-009 (VRS1531)

Effectivity

FIG/ITEM

PART NO.

02-500

2A0202

02-500

2A1540

02-500

2A3665

Material of component

DESCRIPTION

RR SYMBOL

MATERIAL

Turbine cooling manifold assembly

Fe-18Cr-10Ni

Turbine cooling manifold assembly (part)

47.5Ni-22Cr-1.5Co-9.0Mo-0.6W 18.5Fe

General

Price and availability - none.

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

For the method to clean the parts, refer to Cleaning-000 TASK 75-24-48-100-100.

NOTE

Local application, Fluorescent Penetrant Inspection Equipment (Refer to SPM TASK 70-23-05-230-501).

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Fluorescent Penetrant Inspection EquipmentLOCALFluorescent Penetrant Inspection Equipment

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 75-24-48-350-082 Re-Shape the Turbine Cooling Manifold Assembly

      1. Lightly hit all around the concave side of any dent or deformed surface to smooth out.

      1. Use of small hammer permissible.

    2. SUBTASK 75-24-48-220-071 Examine the Turbine Cooling Manifold Assembly (02-500)

    1. Refer to Figure.

      2. Dimensionally check the tube at location 1 for distortion.

      1. Refer to Figure.

      2. Residual creases within 0.19 in. (0.50 mm) contour tolerance in constrained are permitted.

      3. Dimensionally check the joint at location 2.

      1. Refer to Figure.

      2. Outer diameter should be within 3.079 in. (78.206 mm).

      4. Dimensionally check the welded bracket at location 3.

      1. Dimension should be within the limit specified in Figure.

      5. Dimensionally check the pin and support at location 4.

      1. Refer to Figure.

      6. Do the test for cracks.

      1. Refer to SPM TASK 70-23-05-230-501.

      2. No cracks are permitted.

    3. Figure: Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

    Re-shape the Turbine Cooling Manifold Assembly

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
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