• 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

R

 E E Feb 01/00 E E ECES
E TASK 73-25-00-810-874


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


 Loss of Data on the Second and Primary ECS Buses to the EIU 2
 1. Possible Causes
_______________
 - CONT-ZONE TEMPERATURE (8HK)

 - EIU-2 (1KS2)

 - wiring


 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 73-25-34-000-040 Removal of the Engine Interface Unit (EIU)

 (1KS1,1KS2) AMM 73-25-34-400-040 Installation of the Engine Interface Unit (EIU) (1KS1,1KS2) AWM 73-25-20
 3. Fault Confirmation
__________________
 A. Test
 (1) Not applicable.
 4. Fault Isolation
_______________
 A. If the fault is also present on engine 2:
 - replace the CONT-ZONE TEMPERATURE (8HK) (Ref. AMM TASK 21-63-34-000-001) and (Ref. AMM TASK 21-63-34-400-001).
 (1) If the fault is present on engine 2 only:
 - do a check of the wiring between the EIU2 (1KS2) pins AA/2J, AA/2K and terminal block 1853VT and between the EIU2 (1KS2) pins AA/3J, AA/3K and terminal block 1862VT (Ref. AWM 73-25-20).
 (a) If the wiring is not correct:

 - Repair as required.

 (b) If the wiring is correct:


 - replace the EIU-2 (1KS2) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 244
 E E Feb 01/05 ERE
ECES  F 『 E C F M E E E E 56 E E E

 

 B. No additional maintenance action is required if the fault is not confirmed.
 (1) Repeat the fault isolation procedure if the fault continues.
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 245
 E E Feb 01/05 ERE
ECES  TASK 73-25-00-810-879


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


 Loss of FCU Data on the EIU 1
 1. Possible Causes
_______________
 - EIU-1 (1KS1)

 - wiring from the EIU-1 (1KS1) pins AA/1J, 1K to the first terminal block


 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 73-25/06
 3. Fault Confirmation
__________________
 A. Test Do the operational test of the engine interface unit through the CFDS (Ref. AMM TASK 73-25-34-710-043).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message EIU 1 : NO FCU DATA:
 - replace the EIU-1 (1KS1) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
 (1) If the fault continues:
 - do a check and repair the wiring from the EIU-1 (1KS1) pins AA/1J, 1K to the first terminal block (Ref. ASM 73-25/06).
 B. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 246
 E E Feb 01/05 ERE
ECES  TASK 73-25-00-810-880


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


 Loss of FCU Data on the EIU 2
 1. Possible Causes
_______________
 - EIU-2 (1KS2)

 - wiring from the EIU-2 (1KS2) pins AA/1J, 1K to the first terminal block


 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)
 
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(50)