TASK 72-00-50-050-001 LPT Module Components - Remove The Exhaust Gas Temperature (EGT) Thermocouple, Removal-010

DMC:V2500-A0-72-00-5050-00A-520A-B|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 72-00-50-050-001 LPT Module Components - Remove The Exhaust Gas Temperature (EGT) Thermocouple, Removal-010

General

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.

Apply the approved pentrating oil before the removal of the threaded parts. Let the parts soak before removal. For the approved oils and procedures, refer to TASK 70-64-00-640-501.

Discard all rubber seal rings, cotter pins and seal washers removed in this procedure.

Remove and discard the lockwire before parts are disconnected or removed.

Transportation covers/blanks must be installed immediately after the removal of the components.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
CapsLOCALCaps

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-50-050-057 Remove the EGT Thermocouples

    1. NOTE

      The EGT thermocouples are installed through the vanes numbered 3, 6, 8 and 11, of the turbine exhaust case.

      Refer to Figure.

      2. Remove the harness ends from the thermocouple.

      1. Release the four nuts that attach the harness to the thermocouple connection.

      2. Remove the four nuts and washers.

      3. Remove the harness ends from the thermocouple.

      4. Install the nuts and the washers on the terminals.

    3. Cut and discard the wire. Release and remove the two bolts that attach the thermocouple to the boss on the exhaust case. Remove the thermocouple from the exhaust case.

    4. Do Step and Step again for the other three EGT thermocouples.

    5. Install the cups to all exposed apertures.

    2. Figure: Remove the Exhaust Gas Temperature (EGT) Thermocouple

    Remove the Exhaust Gas Temperature (EGT) Thermocouple

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Caps
Tool Name:Caps