Reactivation of the Brake Temperature Monitoring-Unit

TASK 32-47-00-440-002-A
Reactivation of the Brake Temperature Monitoring-Unit

ZONE: 210
FIN: 2GW
FIN: 3GW

1. Reason for the Job
MMEL 32-47-01
BRAKE TEMPERATURE MONITORING UNIT (FAA ONLY)
2. Job Set-up Information
A. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD

B. Referenced Information

REFERENCE	DESIGNATION
TASK 24-42-00-861-001-A	Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A	De-energize the Ground Service Network Supplied from the External Power
TASK 32-47-00-710-001-A	Operational Test of the Brake Temperature System

3. Job Set-up
Subtask 32-47-00-861-051-A

A. Aircraft Maintenance Configuration
(1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).

Subtask 32-47-00-865-060-A

B. Table of the circuit breakers used in this procedure:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
121VU	HYDRAULIC/BRK/TEMP/DET/UNIT	1GW	M37

4. Procedure
Subtask 32-47-00-440-051-A

A. Reactivation of the Brake Temperature Monitoring-Unit
(1) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

Subtask 32-47-00-710-051-A

B. Operational Test
(1) Do an operational test of the brake temperature system (Ref. AMM TASK 32-47-00-710-001).

5. Close-up
Subtask 32-47-00-410-051-A

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.

Subtask 32-47-00-860-055-A

B. Put the aircraft back to its initial configuration.
(1) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).

[Rev.10 from 2021] 2026.04.01 00:50:18 UTC