• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 18:01来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者


 1EFF : ALL 1 32-42-00Page 422 1 1 May 01/04R 1 1 1CES 1


 TASK 32-42-00-440-002
 Reactivation of the Normal Braking - After disconnection of the Green Hydraulic Supply
 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 32-42-02
 Normal Braking - Green Brake System

 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 -------------------------------------------------------------------------------
29-10-00-864-001 Depressurize the Green Hydraulic System 32-42-00-710-001 Operational Check of the Normal Braking System 32-42-00-870-001 Bleeding of the Normal Braking at the Brake Units 32-42-00-991-004 Fig. 403
 3. Job Set-up
__________ Subtask 32-42-00-941-057
 A. Safety Precautions
 (1) Put the warning notice(s) in position to tell persons not to operate the landing gear control lever and the brake pedals.
 1EFF : ALL 1 32-42-00Page 423 1 1 May 01/04R 1 1 1CES 1


 Subtask 32-42-00-860-076
 B. Aircraft Maintenance Configuration
 (1)
 Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).

 (2)
 Make sure that the parking brake control-switch is set to OFF before you do this procedure.


 4. Procedure
_________ (Ref. Fig. 403/TASK 32-42-00-991-004) Subtask 32-42-00-440-054
 A. Reactivation after Isolation of the Green hydraulic supply
 (1)
 Cut and remove the lockwire that attaches the knurled sleeve (2).

 (2)
 Remove the self-adhesive fabric tape from the sleeve (2).

 (3)
 Connect the sleeve (2) to the half-coupling (1).

 (4)
 Bleed the Green braking system at the related brake (Ref. TASK 32-42-00-870-001).


 Subtask 32-42-00-710-059
 B. Test
 (1)
 Do the operational test of the normal braking system (Ref. TASK 32-42-00-710-001).

 (2)
 During this test, make sure that there are no leaks on the hydraulic connector.


 5. Close-up
________ Subtask 32-42-00-860-077
 A. Put the aircraft back to its initial configuration.
 (1)
 Remove the warning notice(s).

 (2)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


 1EFF : ALL 1 32-42-00Page 424 1 1 May 01/04R 1 1 1CES 1


 (3) Remove the temporary placard which tells that the normal braking is

 not operational.

 1EFF : ALL 1 32-42-00Page 425 1 1 May 01/04 1 1 1CES 1


 TASK 32-42-00-040-005 Check of the non affected Tachometers after Loss of the Autobrake Function
 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 32-42-05
 Landing Gear
 Tachometer

 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 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page
 3. Job Set-up
__________ Subtask 32-42-00-860-084
 A. Aircraft Maintenance Configuration
 (1)
 On the panel 400VU, make sure that the L/G normal control lever is set to DOWN.

 (2)
 On the panel 402VU, make sure that the A/SKID & NOSE WHEEL switch is set to ON.

 (3)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 

 1EFF : ALL 1 32-42-00Page 426 1 1 May 01/04 1 1 1CES 1


 (4) On one MCDU, get the SYSTEM REPORT/TEST/L/G page (Ref. TASK 31-32-00-860-009).
 Subtask 32-42-00-941-065
 B. Safety Precautions
 (1) Put the warning notice(s) on the L/G normal control-lever to tell persons not to move it.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM LANDING GEAR 起落架6(122)