TASK 72-45-21-300-012 HPT Case - Install The Helicoil Inserts In The BSI Bosses, Repair-012 (VRS1985)

DMC:V2500-A0-72-45-2101-00A-659A-C|Issue No:001.00|Issue Date:2015-02-01

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 72-45-21-300-012 HPT Case - Install The Helicoil Inserts In The BSI Bosses, Repair-012 (VRS1985)

Effectivity

FIG/ITEM PART NO.

01-010

2A0250

01-010

2A0250SL87VA156

01-010

2A1591

01-010

2A1591SL87VA156

01-010

2A1600

01-010

2A1600SL114902

Material of component

PART IDENT

IAE

SYMBOL

MATERIAL

HP Turbine Case Assembly

Inconel 718

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 TASK 72-45-21-100-000.

NOTE

The tools for the removal and installation of the inserts can be purchased from EMHART TEKNOLOGIES INDUSTRIAL DIVISION, Supplier Code 01556.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
STI tap0AM534FPB

Emhart Teknologies products

Hand installation tool0AM537552-4

Emhart Teknologies products

Tang break-off tool0AM533695-4

Emhart Teknologies products

Thread plug gage0AM533694-4

Emhart Teknologies products

10X magnifying glassLOCAL10X magnifying glass

Consumables, Materials and Expendables

NONE

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Helicoil Insert0AM531191-4TN250AR

FIG/ITEM 01-090

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-21-320-052 Machine the Damaged Threads

    2. Refer to Figure.

    3. Machine the damaged threads.

      1. Tap the hole and remove the chips.

      2. Use STI tap.

    1. SUBTASK 72-45-21-220-082 Examine the Threads

    2. Refer to Figure and Figure.

      1. Examine the threads.

    1. SUBTASK 72-45-21-350-080 Install the New Helicoil Inserts

    2. Refer to Figure.

      1. Put the 1191-4TN250 into the tip of the insertion tool.

    3. Put the insert into the threaded hole.

    4. Turn the handle clockwise so the top of the insert is three-quarters to one and a half pitch below the face of the boss.

      1. Break the tang of the insert at the notch.

    1. SUBTASK 72-45-21-220-083 Do A Torque Check

      1. Torque check the installed helicoil insert.

      2. Refer to SPM TASK 70-35-08-300-501.

      3. Torque the bolt to between 65 and 85 lbfin (7.3 and 9.6 Nm).

      1. Examine the helicoil insert position.

      2. The insert must not protrude out of insert hole.

      3. The insert must not move.

    1. SUBTASK 72-45-21-350-081 Stake the New Helicoil Insert

    2. Refer to Figure.

    3. Do a staking at two locations.

    1. SUBTASK 72-45-21-220-084 Examine the Repaired Area

    2. Refer to Figure.

      1. Visually examine the repaired area.

      2. No damage is permitted.

      3. No cracks are permitted.

    1. SUBTASK 72-45-21-350-082 Vibro Engrave VRS1985

      1. Vibro engrave VRS1985 near to the part number.

        1. Refer to SPM TASK 70-09-00-400-501, (SUBTASK 70-09-00-400-001).

        2. Use vibro engraving equipment.

  1. Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Repair Details and Dimensions

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Added new Repair-012. (14VJ702)

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:LOCAL
Enterprise Name:LOCALLY SUPPLIED
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