• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-24 08:43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


 (4)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (5)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (6)
 Close the access door 196BB.

 (7)
 Remove the warning notice(s).

 


 CONTACTOR - YELLOW ELECTRIC PUMP SUPPLY (3805GX,3806GX) - REMOVAL/INSTALLATION
______________________________________________________________________________ TASK 29-24-55-000-001 Removal of the Contactor - Yellow Electric Pump Supply (3805GX, 3806GX) WARNING : MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT
_______ ELECTRICAL CIRCUITS. THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS CONNECTED.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking cap No specific warning notices No specific access platform 2.10 m (6 ft. 11 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-24-55-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 29-24-55-941-052
 A. Safety Precautions
 (1)
 In the cockpit, on the overhead panel 35VU, make sure that these pushbutton switches are released:

 -APU GEN
 -1 BAT 2
 -GEN 1, GEN 2
 -EXT PWR.

 (2)
 In the cockpit, put warning notices to tell persons not to operate the pushbutton switches on these overhead panels:

 -21VU (EMER ELEC PWR)
 -25VU (APU)
 -35VU (ELEC).

 (3)
 Make sure that the external power connector is not connected to the aircraft receptacle (20XG) (receptacle behind the access door 121AL).

 


 Subtask 29-24-55-010-052
 B. Get Access
 (1)
 Put the access platform in position at the access door 822.

 (2)
 Put a warning notice on the access door 121AL to tell persons not to connect the external power connector.

 (3)
 Open the access door 822.


 4. Procedure
_________
 (Ref. Fig. 401/TASK 29-24-55-991-001)
 Subtask 29-24-55-020-051

 A. Removal of the Contactor
 (1)
 Remove the cover (1) of the panel 107VU.

 (2)
 Disconnect the electrical connector (4).

 (3)
 Put a blanking cap on the connector (4) and the electrical receptacle (3).

 

R CAUTION : REMOVE THE CONTACTOR ONLY AND NOT THE BASE OR THE MODULE
_______ R WHERE THE WIRES ARE CONNECTED.
 (4)
 Loosen the 6 captive screws (6) which stay in position in their housing.

 (5)
 Remove the contactor (5).

 


 Contactors - Yellow Electric Pump Supply (3805GX, 3806GX)
 Figure 401/TASK 29-24-55-991-001

 

 TASK 29-24-55-400-001
 Installation of the Contactor - Yellow Electric Pump Supply (3805GX, 3806GX)
 WARNING : MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT
_______
 ELECTRICAL CIRCUITS.
 THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS
 CONNECTED.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint free cloth
 No specific warning notices
 No specific access platform 2.10 m (6 ft. 11 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 11-002  USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
 
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 HYDRAULIC POWER 液压6(107)