• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 09:19来源:蓝天飞行翻译 作者:航空
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) Use the Aircraft Schematic Manual (ASM) to find the computers related to the output buses from the FCU (FCU 1A & 1B/2A & 2B) and the FMGC 1 & 2 (FMGC OWN A & CB2) (Ref. ASM 22-86/03) and (Ref. ASM 22-86/02).
 (a) Do a check for maintenance message related to the above computers on the Post Flight Report.
 1 If there is a message:
_ R - do the trouble shooting procedure related to the maintenance R message. R
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞22-11-00∞∞∞∞∞∞∞∞∞∞Page 253
 Feb 01/05 CES (2) If the fault continues:


 2_ If there is no message:
 - do the trouble shooting procedure (Ref. TASK 31-32-00-810-
934).

 (a) do a check and repair:
 - for flags on Capt PFD, the wiring of the Arinc Buses from the FCU (FCU 1A & 1B), (Ref. ASM 22-86/03) and wiring of the Arinc Buses from the FMGC 1 (FMGC OWN A & FMGC OWN CB2), (Ref. ASM 22-86/02) to the others LRUs.

 - for flags on F/O PFD, the wiring of the Arinc Busses from the FCU (FCU 2A & 2B), (Ref. ASM 22-86/03) and wiring of the Arinc Busses from the FMGC 2 (FMGC OWN A & FMGC OWN CB2), (Ref. ASM 22-86/02) to the others LRUs.


 B. Do the test given in Para. 3.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞22-11-00∞∞∞∞∞∞∞∞∞∞Page 254
 Aug 01/04R
 CES


 AUTO LAND Warning Light Malfunction
 1. Possible Causes_______________
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM AMM  22-96-00-710-001 22-97-00-710-001  Operational Test of the AFSOperational Test of the LAND CAT III Capability
 3. Fault Confirmation__________________
 A. Not applicable.
 4. Fault Isolation_______________
 A. If the AUTO LAND operational warning light is mentioned in the log book report: - do the system test of the AFS (Ref. AMM TASK 22-96-00-710-001) and the LAND 3 CAPABILITY test (Ref. AMM TASK 22-97-00-710-001).
R R  (1) If these tests are incorrect: - if there is a message, do the trouble shooting procedure related to the maintenance message.
 (2) If these tests are correct: - do a check if any RA and/or ILS troubles in the PFR or mentioned in the Log Book. 
R R R (a) If yes, do the trouble shooting procedure related to the maintenance message. 
(b) If no, no maintenance action is required. But if the fault persist, suspect the AUTOLAND function and notably, troubleshoot consequently the RA and/or ILS systems (antenna, coax, ...) with related bite test and/or operational/functional test if necessary.

 

 AUTOTHRUST ENGAGEMENT - FAULT ISOLATION PROCEDURES
__________________________________________________
 TASK 22-31-00-810-801
 1. Possible Causes
 Loss of the ATH 1 ENGD Feedback _______________
 - FMGC-1 (1CA1)

 - wiring of the ATH OWN ENGD MON OWN and ATH OWN ENGD COM OWN discretes (on the FMGC 1 (1CA1))

 - wiring of ATH OWN ENGD MON OPP and ATH OWN ENGD COM OPP discretes (on the FMGC 1 (1CA1))


 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R 22-31-00-810-812 AMM 22-83-34-000-001 AMM 22-83-34-400-001 AMM 22-96-00-710-001 ASM 22-31/01  Unwanted A/THR 1 and 2 Inoperative WarningRemoval of the FMGC (1CA1,1CA2)Installation of the FMGC (1CA1,1CA2)Operational Test of the AFS
 3. Fault Confirmation__________________
 A. Test

 (1) On the FCU, push the A/THR pushbutton switch.

 (2) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) and read the result for the FMGC 1.


 4. Fault Isolation
_______________
 A. If the test gives the maintenance message AFS: FMGC1/ATHR ENGD FDBK:
 - replace the FMGC-1 (1CA1) (Ref. AMM TASK 22-83-34-000-001) and (Ref. AMM TASK 22-83-34-400-001).
 (1) If the fault continues:
 - do a check of the wiring of the ATH OWN ENGD MON OWN and ATH OWN ENGD COM OWN discretes (on the FMGC 1 (1CA1)) (from pin AE/12E to pin AE/1F and from pin AB/12D to pin AB/1F) (Ref. ASM 22-31/01).


 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320 Trouble Shooting Manual 排故手册 AUTO FLIGHT 自动飞行1(76)