BRAKE SYSTEM TEMPERATURE - DEACTIVATION/REACTIVATION____________________________________________________
TASK 32-47-00-040-001
Brake Temperature Sensor Deactivation
1. Reason for the Job__________________
R R R R Refer to the MMEL TASK: 32-60-03-H) Position and Warning Indications on ECAM WHEEL page Brake temperature
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific No specific No specific No specific circuit breaker(s) safety clip(s)self-adhesive tape, 20 mm (0.8 in.) 30 mm (1.2 in.) widetemporary placardwarning notice
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire-corrosion resistant steel dia. 0.8 mm (0.032 in.)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-47-00-991-001 Fig. 401
3. Job Set-up
__________ Subtask 32-47-00-941-050
A. Put a warning notice in position in the cockpit to tell persons not to operate the landing gear control lever and the brake pedals.
Subtask 32-47-00-865-051
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/BRK/TEMP/DET/UNIT 1GW M37 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36
4. Procedure
_________
(Ref. Fig. 401/TASK 32-47-00-991-001) Subtask 32-47-00-040-050
A. Deactivation of the Brake Temperature Sensor
(1)
Disconnect the connector (2) from the temperature sensor (1).
(2)
Put blanking caps on the two connectors.
(3)
Clean the electrical connector (2) of the brake temperature sensor and apply two or three turns of self-adhesive tape, 20 mm (0.8 in.) 30 mm (1.2 in.) wide around the electrical connector (3).
(4)
Tightly wind 3 or 4 turns of lockwire-corrosion resistant steel dia.
0.8 mm (0.032 in.) around the tape on the electrical connector (2). Twist the lockwire and put it through the nearest locking hole.
NOTE : Make sure that the lockwire cannot rub when the landing gear
____
operates.
(5) Put the temporary placard in the cockpit to warn the crew that the brake temperature system is inoperative on the wheel 1 (2, 3, 4).
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Brake Temperature Sensor Deactivation/Reactivation
Figure 401/TASK 32-47-00-991-001
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5. Close-up
________ Subtask 32-47-00-942-051
A. Remove the safety device.
(1) Remove the warning notice.
(2) Make an entry in the log book. Subtask 32-47-00-865-054
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GW, 4GG
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TASK 32-47-00-440-001
Brake Temperature Sensor Reactivation
1. Reason for the Job
__________________
R Refer to the MMEL TASK: 32-60-03-H) R Position and Warning R Indications on ECAM WHEEL page R Brake temperature
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific warning notice
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
TSM 32PB101 (for corrective action)
32-47-00-991-001 Fig. 401
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本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架8(26)
