• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-29 14:33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

 (2) If the fault continues:


 - do a check and repair the wiring from the EIU 1 (1KS1) to the ENG panel (115VU) pins AA/4E, 5A to pins A/J, H (Ref. ASM 76-12/01).
 B. Do the test given in Para. 3.A.
 F 『

 ∞∞76-12-00∞∞∞∞∞∞∞∞∞∞Page 201
EEFF :  ALL  E 
E  E  May 01/98
 E  E
 ECES  E


 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 76-12-00-810-806
 Failure of the ENG 2/MASTER Control Switch
 1. Possible Causes
_______________
 - EIU-2 (1KS2)

 - CTL SW-ENG MASTER 2 (2KC)

 - wiring from the EIU2 (1KS2) to the ENG panel (115VU)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 71-00-00-710-002 Wet Motoring Check AMM 73-25-34-000-040 Removal of the Engine Interface Unit (EIU) (1KS1,1KS2) AMM 73-25-34-400-040 Installation of the Engine Interface Unit (EIU)
 (1KS1,1KS2)
 AMM 73-25-34-710-043 Operational Test of the Engine Interface Unit
 ASM 76-12/01

 3. Fault Confirmation
__________________
 A. Test Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 73-25-34-710-043).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message 115VU (MASTER LEVER 2) SW: R - replace the CTL SW-ENG MASTER 2 (2KC) and perform a wet motoring check R (Ref. AMM TASK 71-00-00-710-002).
 (1) If the fault continues:

 - replace the EIU-2 (1KS2), (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).

 (2) If the fault continues:


 - do a check and repair the wiring from the EIU2 (1KS2) to the ENG panel (115VU) pins AA/5A, 4E to pins A/G, L, (Ref. ASM 76-12/01).
 B. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞76-12-00∞∞∞∞∞∞∞∞∞∞Page 202
 E E May 01/98 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 76-12-00-810-807
 Failure of the ENG 1/MODE Selector Switch
 1. Possible Causes
_______________
 - SEL SW-ENG/MODE/CRANK/AUTO IGN/IGN (6KS)

 - EIU-1 (1KS1)

 - wiring from the EIU 1 (1KS1) to the ENG panel (115VU)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 73-25-34-000-040 Removal of the Engine Interface Unit (EIU)
 (1KS1,1KS2)
 AMM 73-25-34-400-040 Installation of the Engine Interface Unit (EIU)

 (1KS1,1KS2)
 AMM 73-25-34-710-043 Operational Test of the Engine Interface Unit
 ASM 73-25/08

 3. Fault Confirmation
__________________
 A. Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 73-25-34-710-043).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message 115VU CRANK/MODE AUTO/IGN SEL SW:
 - replace the SEL SW-ENG/MODE/CRANK/AUTO IGN/IGN (6KS).
 (1) If the fault continues:

 - replace the EIU-1 (1KS1), (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).

 (2) If the fault continues:


 - do a check and repair the wiring from the EIU 1 (1KS1) to the ENG panel (115VU) pins AA/1C, 1A, 1B to pins 22, 23, 24 (Ref. ASM 73-25/08).
 B. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞76-12-00∞∞∞∞∞∞∞∞∞∞Page 203
 E E Feb 01/98 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 76-12-00-810-808
 Failure of the ENG 2/MODE Selector Switch
 1. Possible Causes
_______________
 - SEL SW-ENG/MODE/CRANK/AUTO IGN/IGN (6KS)

 - EIU-2 (1KS2)

 - wiring from the EIU 2 (1KS1) to the switch (6KS)


 2. Job Set-up Information
______________________
 
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 发动机控制(19)