• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-29 14:34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

_
 - replace the control alternator (Ref. AMM TASK 73-21-30-000-002) and (Ref. AMM TASK 73-21-30-400-002).
 B. Do a minimum idle check (Ref. AMM TASK 71-00-00-710-006).
 F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page 293
 E E Nov 01/04 ERE ECES

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E


 TASK 77-00-00-810-886
 Loss of the Data on ARINC Bus from the EIU to the FADEC on Engine 1
 1. Possible Causes_______________
 - EIU-1 (1KS1)

 - harness J3 between the EIU (1KS1) and the ECU (4000KS)

 - CONT-ZONE TEMPERATURE (8HK)

 - ECU (4000KS)


 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 21-63-34-000-001  Removal of the Zone Controller (8HK)
 AMM 21-63-34-400-001  Installation of the Zone Controller (8HK)
 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 (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 73-25-34-710-040  Operational Test of the Engine Interface Unit (1KS1,1KS2)
 AMM 73-29-00-710-040  Operational Test of the FADEC on the Ground (with Engine non Motoring)
 ASM 73-25/06
 3. Fault Confirmation__________________
 A. Test
 (1) Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 73-25-34-710-040).

 (2) Do the operational test of the FADEC 1A and 1B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).


 F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page 294
 E E Nov 01/04 ERE
ECES  4. Fault Isolation

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E


_______________
 A. If the fault symptom is identified by the upper ECAM warning ENG1 BLEED STATUS FAULT and the tests of the EIU and FADEC give no maintenance messages:
 - do a check for open or short to ground of the harness J3 between the EIU (1KS1) and the ECU (4000KS) pins AB/5A, 5C to pins J3/22, 23 (Ref. ASM 73-25/06).
 (1) If the wiring is not correct:

 - repair the above wiring.

 (2) If the wiring is correct:

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

 (3) If the fault continues:

 - replace the CONT-ZONE TEMPERATURE (8HK) (Ref. AMM TASK 21-63-34-000-001) and (Ref. AMM TASK 21-63-34-400-001).

 (4) 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).
 F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page 295
 E E Nov 01/04 ERE
ECES  TASK 77-00-00-810-887

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E


 Loss of the Data on ARINC Bus from the EIU to the FADEC on Engine 2
 1. Possible Causes_______________
 - EIU-2 (1KS2)

 - harness J3 between the EIU (1KS2) and the ECU (4000KS)

 - CONT-ZONE TEMPERATURE (8HK)

 - ECU (4000KS)


 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 21-63-34-000-001  Removal of the Zone Controller (8HK)
 AMM 21-63-34-400-001  Installation of the Zone Controller (8HK)
 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 (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)
 
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 发动机指示(104)