TASK 72-00-32-050-014 LPC/Intermediate Case Module Components - Remove The T2.5 Thermocouple, Removal-012

DMC:V2500-A0-72-00-3250-05A-520A-B|Issue No:001.00|Issue Date:2014-05-01

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 72-00-32-050-014 LPC/Intermediate Case Module Components - Remove The T2.5 Thermocouple, Removal-012

General

This TASK gives the procedure to remove the T2.5 thermocouple.

Fig./item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig./item numbers are used. For the service bulletin alpha-variants refer to the IPC.

For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the item number.

Apply the approved CoMat 10-058 PENETRATING OIL before the removal of threaded parts. Let the parts soak before removal.

Seal all openings when the components are disconnected to prevent contamination from unwanted material.

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 10-058 PENETRATING OIL0AM53CoMat 10-058

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-32-050-002 Remove the T2.5 Thermocouple

    2. Refer to Figure.

    3. Remove the two nuts EEC Core Harness And Voltage Divider Harness Assembly (71-52-43, 01-015) and EEC Core Harness And Voltage Divider Harness Assembly (71-52-43, 01-017) that attach the T2.5 thermocouple leads to the terminal block. Remove the T2.5 thermocouple leads from the terminal block. Refer to the view at A.

    4. Remove the bolt Fan Frame Assembly And Related Parts (72-32-03, 01-510) that attaches the earth lead to the bracket Fan Frame Assembly And Related Parts (72-32-03, 01-495). Remove the earth lead from the bracket.

    5. Remove the bolt Fan Frame Assembly And Related Parts (72-32-03, 01-510) that attaches the bracket Fan Frame Assembly And Related Parts (72-32-03, 01-495) to the terminal block Fan Frame Assembly And Related Parts (72-32-03, 01-500). Remove the terminal block from the intermediate structure.

  1. Figure: Remove the T2.5 Thermocouple

    Remove the T2.5 Thermocouple

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:X222X
Supply Number:CoMat 10-058
Type:sp01
Supply Short Name:CoMat 10-058 PENETRATING OIL
Supply Name:CoMat 10-058 PENETRATING OIL
Suppliers:
ManufacturerRemarks
X222X