Disagree between Data Received from the LGCIU 2
 1. Possible Causes
_______________
 - EIU-2 (1KS2)

 - LGCIU-2 (5GA2)

 - wiring from the pins AA/5D, 5E of the EIU-2 (1KS2) to the pins AB/3G, 3K of the LGCIU 2 (5GA2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2)
 AMM 32-31-71-400-001 Installation of the LGCIU (5GA1, 5GA2)
 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) ASM 73-25/16
 3. Fault Confirmation
__________________
 A. Not applicable.
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message CHECK LGCIU 2 L/G COMP SIGNALS (DISAGREE):
 - 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 LGCIU-2 (5GA2) (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).

 (2) If the fault continues:

 - do a check and repair the wiring from the pins AA/5D, 5E of the EIU-2 (1KS2) to the pins AB/3G, 3K of the LGCIU 2 (5GA2) (Ref. ASM 73-25/16).
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 240
 E E Feb 01/05 ERE
ECES  F 『 E C F M E E E E 56 E E E

 B. Test
 (1) During the subsequent engine start make sure that:

 - no ECAM warning or/and amber crosses do not come into view on the ECAM

 - the engine idle must not be high

 (2) After a subsequent flight make sure that the maintenance message is no more present.

 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 241
 E E Feb 01/05 ERE
ECES  TASK 73-25-00-810-873

 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 1
 1. Possible Causes
_______________
 - CONT-ZONE TEMPERATURE (8HK)

 - EIU-1 (1KS1)

 - 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 73-25-19
 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 1 only:
 - do a check of the wiring between the EIU1 (1KS1) pins AA/2J, AA/2K and terminal block 1853VT and between the EIU1 (1KS1) pins AA/3J, AA/3K and terminal block 1853VT (Ref. AWM 73-25-19).
 (a) If the wiring is not correct:

 - Repair as required.

 (b) 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).
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 242
 E E Feb 01/05 ERE
ECES  F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page 243

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

R  B. No additional maintenance action is required if the fault is not 
R  confirmed. 
R  (1) Repeat the fault isolation procedure if the fault continues. 
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 發(fā)動機燃油和控制 2(49)