- 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 EIU 2 (1KS2) to the relay (12KS2) pin AB/9C to pins AA/X, Z (Ref. ASM 73-25/09).
B. Do the test given in Para. 3.A.
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Failure of the Relay 15KS1 Control on the EIU 1
1. Possible Causes
_______________
- EIU-1 (1KS1)
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 73-25-34-710-044 Read the Class 3 Faults
3. Fault Confirmation
__________________
A. Test Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) to read the Class 3 Faults (Ref. AMM TASK 73-25-34-710-044).
4. Fault Isolation
_______________
A. If the test gives the maintenance message CHECK 15KS1 RELAY CIRCUIT OR EIU 1:
- replace the EIU-1 (1KS1) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
NOTE : As relay 15KS1 is not installed, no maintenance action in line is
____ necessary. When the message comes into view on the EIU Class 3 report, replace the EIU 1 at the "A" check that follows.
B. If the EIU 1 (1KS1) is replaced:
- do the test given in Para. 3.A.
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Failure of the Relay 15KS1 Control on the EIU 2
1. Possible Causes
_______________
- EIU-2 (1KS2)
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 73-25-34-710-044 Read the Class 3 Faults
3. Fault Confirmation
__________________
A. Test Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) to read the Class 3 Faults (Ref. AMM TASK 73-25-34-710-044).
4. Fault Isolation
_______________
A. If the test gives the maintenance message CHECK 15KS2 RELAY CIRCUIT 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).
NOTE : As relay 15KS2 is not installed, no maintenance action in line is
____ necessary. When the message comes into view on the EIU Class 3 report, replace the EIU 2 at the "A" check that follows.
B. If the EIU 2 (1KS2) is replaced:
- do the test given in Para. 3.A.
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TASK 73-25-00-810-853
Failure of the EIU on Engine 1
1. Possible Causes
_______________
- EIU-1 (1KS1)
- aircraft wirings
- C/B-ENGINE/1/FADEC A/AND EIU 1 (2KS1)
- C/B-ENGINE/ENG1/FADEC B/AND EIU 1 (4KS1)
- ECU (4000KS)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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) R AMM 73-25-34-710-043 Operational Test of the Engine Interface Unit ASM 73-25/05
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本文链接地址：A320 Trouble Shooting Manual 排故手册 发动机燃油和控制 2(39)
