• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 08:16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

1. On the ELEC panel 35VU:  On the panel 35VU:
 - release the BAT1 and BAT2  - the OFF legends of the BAT1 and BAT2
 pushbutton switches.  pushbutton switches come on.
 2. On the panel 35VU:  On the panel 35VU:
 - push the BAT1 and BAT2  - the OFF legends of the BAT1 and BAT2
 pushbutton switches.  pushbutton switches go off.
 3. On the panel 122VU:  On the lower ECAM display unit:
 - open the circuit breaker  - the TR1(2) supplies the DC1(2)
 3PU1(2).  busbar.
 4. On the panel 125VU (124VU):  On the upper ECAM display unit:
 - open the circuit breaker  - the TR1(2) FAULT indication comes
 4PU1(2).  into view.

 

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
5. On the panels 122VU and 125VU (124VU):
 -close the circuit breakers 3PU1(2) and 4PU1(2).
 6. On the MCDU, on the ELEC page:
-push the line key adjacent to the TR1(2) indication.
 7. On the MCDU:
-push the line key adjacent to the RESET indication.
8. On the MCDU:
 -push the line key adjacent to the RETURN indication until the ELEC page comes into view.
 9. On the panel 35VU:
-release the AC ESS FEED
pushbutton switch.

10. On the panel 35VU:
-push the AC ESS FEED
pushbutton switch.

11. On the ECAM control panel: On the lower ECAM display unit:
 -
the TR1(2) no longer supplies the DC1(2) busbar,

 -
the DC2(1) busbar supplies the DC1(2) busbar, through the DC BAT busbar,


 -The AC ESS busbar supplies the DC ESS busbar through the ESS TR.
There is no change.
On the MCDU:
-
the TR1(2) page comes into view.

On the TR1(2) page:

-
the NO FAULT indication comes intoview.

 On the upper ECAM display unit:

 -
the TR1(2) FAULT indication goes out of view.

 On the lower ECAM display unit:

 -
the TR1(2) supplies the DC1(2) busbar.


On the panel 35VU:
-
the ALTN legend of the AC ESS FEEDpushbutton switch comes on.

On the panel 35VU:

-
the ALTN legend of the AC ESS FEEDpushbutton switch goes off.


On the lower ECAM display unit:
 1EFF : ALL 1 24-32-00Page 505 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-push the ELEC key to get the ELEC page.
12. On the panel 35VU:
-release the BAT1 and BAT2 pushbutton switches.
13. On the panel 35VU:
-push the BAT1 and BAT2 pushbutton switches.
14.
 On the panel 123VU:

- open the circuit breaker 2PU1(2).

15.
 On the panel 123VU:

-close the circuit breaker 2PU1(2).

16.
 On the MCDU, on the ELEC page:

-push the line key adjacent to the TR1(2) indication.

 17.
 On the MCDU:


-push the line key adjacent to the RESET indication
-
the ESS TR no longer supplies the DCESS busbar (the normal configuration comes into view).

On the panel 35VU:

-
the OFF legends of the BAT1 and BAT2pushbutton switches come on.

On the panel 35VU:

-
the OFF legends of the BAT1 and BAT2pushbutton switches go off.

On the upper ECAM display unit:

-
the TR1(2) FAULT indication comesinto view.

 On the lower ECAM display unit:

 -
the TR1(2) no longer supplies the DC1(2) busbar,

 -
the DC2(1) busbar supplies DC1(2) busbar through the DC BAT busbar,

 -
the voltage from TR1(2) = 0 V,

 -
the AC ESS busbar supplies the DC ESS busbar through the ESS TR.

On the lower ECAM display unit:

-
the voltage from TR1(2) isapproximately 28 V.

On the MCDU:

-
the TR1(2) page comes into view.

On the MCDU, on the TR1(2) page:

-
the NO FAULT indication comes intoview.

 On the upper ECAM display unit:

 -
the TR1(2) FAULT indication goes out of view.

 On the lower ECAM display unit:

 -
the TR1(2) supplies the DC1(2) busbar.


 1EFF : ALL 1 24-32-00Page 506 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
18.
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
 
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 ELECTRICAL POWER 电源2(33)