• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 00:09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

 - push the line key adjacent to  - the CFDS MENU page comes into view.
 the CFDS indication.
 - push the line key adjacent to  - the SYSTEM REPORT/TEST page comes
 the SYSTEM REPORT/TEST  into view.
 indication.
 - push the line key adjacent to  - the SYSTEM REPORT/TEST NAV page comes
 the NAV indication.  into view.
 - push the line key adjacent to  - the ADR1 (ADR2) (ADR3) page comes
 the ADR1 (ADR2) (ADR3)  into view.
 indication (related to the
 removed TAT sensor).
 - push the line key adjacent to  - the CURRENT STATUS page comes into
 the CURRENT STATUS indication.  view.
 - push NEXT PAGE key until you  - CURRENT STATUS pages 5/8 and 7/8 come
 get ADR1 (ADR2) (ADR3)/CURRENT  into view:
 STATUS pages 5/8 and 7/8.  do a check of the TAT data (OPEN, XXX
 DEGC). 

R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-11-18Page 409 1 1 May 01/05 1 1 1CES 1 NOTE : As an alternative procedure, you can do this operational test


____
 without the CFDS
 (Ref. TASK 34-11-18-710-001).


R **ON A/C 051-099, 106-149, 204-299, 301-399, 401-499,
 Subtask 34-11-18-710-050-B
 D. Do the operational test of the TAT sensor with the CFDS.
 (1)
 Do the operational test of the Probe Ice Protection. (Ref. TASK 30-31-00-710-001)

 (2)
 Do the operational test of the INPUT STATUS: NOTE : The TAT sensor 1 is related to the ADIRU 1 and 3. The TAT


____
 sensor 2 is related to the ADIRU 2.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the center pedestal, on one  On the MCDU:
 MCDU:
 - push the MCDU MENU mode key.  - the MCDU MENU page comes into view.
 - push the line key adjacent to  - the CFDS MENU page comes into view.
 the CFDS indication.
 - push the line key adjacent to  - the SYSTEM REPORT/TEST page comes
 the SYSTEM REPORT/TEST  into view.
 indication.
 - push the line key adjacent to  - the SYSTEM REPORT/TEST NAV page comes
 the NAV indication.  into view.
 - push the line key adjacent to  - the ADR1 (ADR2) (ADR3) page comes
 the ADR1 (ADR2) (ADR3)  into view.
 indication (related to the
 removed TAT sensor).
 - push the line key adjacent to  - the INPUT STATUS page comes into
 the INPUT STATUS indication.  view.

 1EFF : ALL 1 34-11-18Page 410 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 34-11-18Page 411 1 1 May 01/05 1 1 1CES 1 SENSOR - TOTAL TEMPERATURE (11FP1,11FP2) - ADJUSTMENT/TEST


R R R R  -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------- push NEXT PAGE key until you - INPUT STATUS pages 3/8 and 7/8 come get ADR1 (ADR2) (ADR3)/INPUT into view: STATUS pages 3/8 and 7/8. do a check of the TAT data (OPEN, XXX . C). 
R R R  NOTE : As an alternative procedure, you can do this operational test____ without the CFDS (Ref. TASK 34-11-18-710-001).
 **ON A/C ALL
 5. Close-up________
 Subtask 34-11-18-860-055
 A. Put the aircraft back to its initial configuration.
 (1) On the MCDU , push the MCDU MENU mode key.
 (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 (3) Make sure that the work area is clean and clear of tool(s) and other items.
 (4) Remove the access platform(s).

 

__________________________________________________________
 TASK 34-11-18-710-001
 Test of the TAT Sensor (11FP1, 11FP2) without the CFDS
 1. Reason for the Job
__________________
 Do this test after the removal/installation of the TAT Sensor (11FP1,11FP2) when the CFDS is unserviceable.
 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 34-10-00-860-005 ADIRS Stop Procedure FOR FIN 11FP2 31-60-00-860-001 EIS Start Procedure 34-10-00-860-002 ADIRS Start Procedure
 
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 NAVIGATION 导航1(87)