• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 13:46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

 - PITCH AXIS OK (DSO 09) signal ELAC 1 MON part (Ref. ASM 27-92/33)


 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : ALL ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B260
 Aug 01/05 CES


 (2) If the fault continues:

 (a) Do a check of the wiring of the PITCH AXIS OK (DSO 09) signal from the ELAC 1 COM part to the MON part (DSI 12) (Ref. ASM 27-92/33).

 - if there is continuity, see para. (b)

 - if there is no continuity, repair the above wiring.

 

 (b) Do a check and repair the wiring of the PITCH AXIS OK (DSO 09) signal from the ELAC 1 MON part to the COM part (DSI 12) (Ref. ASM 27-92/33).


 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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B261
 Aug 01/05R
 CES  Loss of the YAW DAMPER Signal from the FAC 1/2 to the ELAC1


 1. Possible Causes
_______________
 - ELAC-1 (2CE1)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
 AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
 AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
 ASM 27-92/37

 3. Fault Confirmation
__________________
 A. Test Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ELAC1 OR WIRING FROM FAC 1/2:
 - replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring . from the ELAC1 (2CE1) pin AA/11E to the first terminal block . from the ELAC1 (2CE1) pin AA/8E to the first terminal block . from the ELAC1 (2CE1) pin AE/8H to the first terminal block . from the ELAC1 (2CE1) pin AE/7K to the first terminal block (Ref. ASM 27-92/37).
 B. Test
 Do the test given in Para. 3.A.

 「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B262
 Aug 01/05R
 CES  Loss of the YAW DAMPER signal from the FAC 1/2 to the ELAC2


 1. Possible Causes
_______________
 - ELAC-2 (2CE2)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
 AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
 AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
 ASM 27-92/37

 3. Fault Confirmation
__________________
 A. Test Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ELAC2 OR WIRING FROM FAC 1/2:
 - replace the ELAC-2 (2CE2) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring . from the ELAC2 (2CE2) pin AA/11E to the first terminal block . from the ELAC2 (2CE2) pin AA/8E to the first terminal block . from the ELAC2 (2CE2) pin AE/8H to the first terminal block . from the ELAC2 (2CE2) pin AE/7K to the first terminal block (Ref. ASM 27-92/37).
 B. Test
 Do the test given in Para. 3.A.

 「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B263
 Aug 01/05R
 CES  TASK 27-93-00-810-934


 Failure of the ELAC1 at the AP Engagement
 1. Possible Causes
_______________
 - FMGC-1 (1CA1)

 - ELAC-1 (2CE1)

 - FMGC-2 (1CA2)

 - SSTU-ROLL CTL, F/O (4CE2)
 
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 飞行操纵 3(78)