3. Job Set-up
__________
 Subtask 32-47-00-941-051

 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 32-47-00-865-052
 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
 1EFF : ALL 1 32-47-00Page 405 1 1 Nov 01/03 1 1 1CES 1

 4. Procedure
_________ (Ref. Fig. 401/TASK 32-47-00-991-001) Subtask 32-47-00-440-050
 A. Reactivation of the Brake Temperature Sensor
 (1)
 Remove and discard the lockwire around the tape on the electrical connector (2).

 (2)
 Remove the self-adhesive tape from the electrical connector (2).

 (3)
 Remove the blanking caps from the two connectors.

 (4) Connect the connector (2) to the temperature sensor (1). Subtask 32-47-00-865-055
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GW, 4GG
 Subtask 32-47-00-810-050
 C. Do a trouble shooting of the brake temperature system (Ref. TSM 32PB101)
 5. Close-up
________ Subtask 32-47-00-942-050
 A. Remove the warning notice(s) and the temporary placards from the cockpit.
 1EFF : ALL 1 32-47-00Page 406 1 1 Feb 01/98 1 1 1CES 1

 BRAKE SYSTEM TEMPERATURE - ADJUSTMENT/TEST
__________________________________________ TASK 32-47-00-710-001 Operational Test of the Brake Temperature System WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice(s)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
 3. Job Set-up
__________ Subtask 32-47-00-860-051
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 On the panel 400 VU, make sure that the landing gear control-lever is in the DOWN position.

 1EFF : ALL 1 32-47-00Page 501 1 1 Feb 01/98 1 1 1CES 1

 (3) Do the EIS Start procedure (Ref. TASK 31-60-00-860-001).
 Subtask 32-47-00-865-050
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/BRK/TEMP/DET/UNIT 1GW M37 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33
 Subtask 32-47-00-941-052
 C. Safety Precautions
 (1) Put the warning notice(s) on the landing gear control-lever to tell persons not to operate it.
 4. Procedure
_________
 Subtask 32-47-00-710-050
 A. Test of the Brake Temperature System
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the ECAM control panel:
 -push the WHEEL key.  - on the lower ECAM DU, the WHEEL page comes into view. Make sure that the temperatures shown relate to the ambient temperature with a precision of plus or minus 25 deg.C (45 deg.F). NOTE: In case of negative temperatures, or temperatures near 0 deg.C (32 deg.F), the indication on the display unit ranges from 0 deg.C to 25 deg.C (32 deg.F to 77 deg.F) approximately.
 1EFF : ALL 1 32-47-00Page 502 1 1 Feb 01/98 1 1 1CES 1 Subtask 32-47-00-860-050
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架8(27)