• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-22 06:40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

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 27-96-00-710-055
 A. Do this test:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the circuit breaker panel 121VU: - open the C/B 20CE2.  On the upper ECAM display unit:- the F/CTL FCDC2 FAULT message isshown.
 2. On the center pedestal, on the ECAM control panel: - push the F/CTL key.  On the lower ECAM display unit, theF/CTL page comes into view.Make sure that: - there are no crosses on the EFCS servocontrols.

 

 -------------------------------------------------------------------------------
ACTION  RESULT
 -------------------------------------------------------------------------------On the upper ECAM display unit, make sure that:
 -no F/CTL FCDC1 FAULT message is shown.
 3. On the circuit breaker panel  On the upper ECAM display unit: 121VU: - the F/CTL FCDC2 FAULT message goes
 -close the C/B 20CE2.  out of view.
 4. On the circuit breaker panel  On the upper ECAM display unit: 49VU: - the F/CTL FCDC1 FAULT message is - open the C/B 20CE1. shown.
 -
make sure that no F/CTL FCDC2 FAULT
 message is shown.
 On the lower ECAM display unit, on the
 F/CTL page:


 -
make sure that there are no crosses
 on the EFCS servocontrols.

 

 5. On the circuit breaker panel  On the upper ECAM display unit: 49VU: - the F/CTL FCDC1 FAULT message goes
 -close the C/B 20CE1.  out of view.
 5. Close-up________
 Subtask 27-96-00-860-059
 A. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).


 1EFF : ALL 1 27-96-00Page 503 1 1 Feb 01/05R 1 1 1CES 1


 TASK 27-96-00-710-002
 Operational Test of the Computers Engagement/Disengagement
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 279000-01 Do the check of the pushbutton switches related to the ELACs and SECs for their correct operation.
 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 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
 3. Job Set-up
__________
 Subtask 27-96-00-860-060
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 On the overhead panel 23VU, make sure that:

 -the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).

 (3)
 On the overhead panel 24VU, make sure that:

 -the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).

 (4)
 On the center pedestal, on the panel 8VU, make sure that:

 -the SWITCHING/ATT HDG, SWITCHING/AIR DATA, SWITCHING/EIS DMC and SWITCHING/ECAM/ND XFR selector switches are in the NORM position.

 (5)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (6)
 On the center pedestal, on the ECAM control panel:

 


 -push the F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
 Subtask 27-96-00-865-054
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 4. Procedure
_________
 Subtask 27-96-00-710-054
 
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 FLIGHT CONTROLS 飞行操纵9(115)