• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-29 09:37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

 (1KS1,1KS2)
 AMM 73-25-34-710-043 Operational Test of the Engine Interface Unit
 ASM 73-25/06
 ASM 73-25/10

 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 CHECK ECU 2 A1 and B1 BUS or EIU 2:
 - replace the EIU-2 (1KS2) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
 (1) If the fault continues:

 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).

 (2) If the fault continues:


 - do a check and repair the wiring from the ECU 2 (4000KS) to the EIU 2 (1KS2) pins J3/24, 11 to pins AA/15A, 15C, and pins J4/24, 11 to pins AA/14K, 15J (Ref. ASM 73-25/06) and (Ref. ASM 73-25/10).
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 201
 E E Feb 01/99 E E ECES
E F 『 E C F M E E E E 56 E E E

 

 

 B. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 202
 E E Feb 01/98 E E ECES
E


 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 73-25-00-810-827
 Loss of Channel A Data from the ECU on Engine 1
 1. Possible Causes
_______________
 - EIU-1 (1KS1)

 - ECU (4000KS)

 - wiring from the ECU 1 (4000KS) to the EIU 1 (1KS1)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
R AMM 73-21-60-000-001 Removal of the Electronic Control Unit (ECU)(4000KS) AMM 73-21-60-400-001 Installation of the Electronic Control Unit R (ECU)(4000KS) 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 73-25/10

 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 EIU1 : NO FADEC 1A DATA:
 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
 (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 ECU 1 (4000KS) to the EIU 1 (1KS1) pins J3/24, 11 to pins AA/15A, 15C (Ref. ASM 73-25/10).
 B. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 203
 E E Feb 01/99 E E ECES
E


 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 73-25-00-810-843
 Failure of the ECU Power Supply on Engine 1
 1. Possible Causes
_______________
 - EIU-1 (1KS1)

 - ECU (4000KS)

 - wiring from the ECU 1 (4000KS) to the EIU 1 (1KS1)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 73-21-60-000-001 Removal of the Electronic Control Unit (ECU)(4000KS) AMM 73-21-60-400-001 Installation of the Electronic Control Unit R (ECU)(4000KS) 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 73-25/06
 ASM 73-25/10

 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
 
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 发动机燃油和控制 2(35)