• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 12:12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

 Write the P/N reference.

 4.
 Push the line key adjacent to the  - The MCDU MENU page comes into view. RETURN indication until the MCDU MENU page comes into view.

 (2)
 Make sure that the P/N shown on the CFDIU LRU IDENTIFICATION page is the same as the computer P/N (given on the front face).

 NOTE: If the P/N is not the same, you must remove the computer and return it to the shop.

 (3)
 If the P/N reference of the CFDIU starts:

 (a)
 With B401XXXX, do the procedure in Para B.

 (b)
 With C128XXXX, go to Para 5.

 

 


R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page 505 1401-499, 1Aug 01/05 1 1 1CES 1 Subtask 31-32-00-710-052


 B. Do this test:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the panel 121VU: - open the circuit breaker 2TW.

2.
 On the MCDU 3:


-push the line key adjacent to the CFDS indication.
3. On the MCDU 3:
-push the line key adjacent to the SYSTEM REPORT/TEST indication.
 4. On the MCDU 3:
-set a system menu. To do this, push the line key adjacent to the system indication.
 5. On the MCDU 3:
-push the line key adjacent to the RETURN indication.
6. On the panel 121VU:
 -close the circuit breaker 2TW.
 7. On the MCDU 3:
-push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view.
On the MCDU 3:
-
after 5s approximately, on the MCDU MENU page, the CFDS indication goes out of view.

 -
after 30s approximately, on the MCDU MENU page, the CFDS indication comes into view again.


On the MCDU 3:
-
the CFDS BACK-UP MODE page comes intoview.

On the MCDU 3:

-
the SYSTEM REPORT/TEST page comesinto view.

On the MCDU 3:

-
the menu page of the set system comesinto view.

On the MCDU 3:

-
the SYSTEM REPORT/TEST page comesinto view.

On the MCDU 3:

-
the MCDU MENU page comes into view.


R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page 506 1401-499, 1Aug 01/05 1 1 1CES 1


R  **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 5. Close-up________ 
R  **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 Post SB  31-1163 For A/C 155-156,208-209,
 Subtask 31-32-00-860-119
 A. Put the aircraft back to its initial configuration.
 (1) De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).
 (2) Put the system back to the serviceable condition.
 (3) Put the aircraft back to the serviceable condition. 

R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page 507 1401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL


 TASK 31-32-00-740-002 BITE Test of the Centralized Fault Display Interface Unit (CFDIU) WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 NOTE : IGNORE ALL THE ECAM WARNINGS AS LONG AS THE COMPUTER IS IN THE MENU
____ MODE.
 1. Reason for the Job__________________ Self Explanatory
 2. Job Set-up Information______________________
 A. 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
 3. Job Set-up
__________ Subtask 31-32-00-861-055
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)
 1EFF : ALL 1 31-32-00Page 508 1 1 Feb 01/05R 1 1 1CES 1


 Subtask 31-32-00-865-058
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/MCDU/1 11CA1 B01 121VU CFDS/CFDIU/SPLY 2TW J18 121VU AUTO FLT/MCDU/2 11CA2 N20 
R  **ON A/C ALL 
R  Post SB  31-1163 For A/C 155-156,208-209, 
R  121VU CFDS/CFDIU/BACK/UP  8TW  J17 
R  **ON A/C ALL
 4. Procedure_________
 Subtask 31-32-00-740-050
 
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 指示/记录系统 2(46)