- N1 = 0
- N2 = 0
- FF = 0
- EGT = ambient temperature
4. Fault Isolation
_______________
A. If the test is confirmed:
(1) Do a check and repair the wiring between the FADEC GND PWR pushbutton switch (7KS2) and the EIU 2 (1KS2), (Ref. ASM 73-25/08).
(2) If the fault continues:
- replace the P/BSW-ENG/FADEC GND PWR/ 2 (7KS2).
B. Do the functional test of the ECU (Ref. AMM TASK 73-21-60-720-040).
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A. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
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TASK 73-29-00-810-808
Loss of the Output 1 Bus of the ECU 2 Channel B
1. Possible Causes
_______________
- ECU (4000KS)
- aircraft wiring
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) R AMM 73-25-34-710-040 Operational Test of the Engine Interface Unit R (1KS1,1KS2)
ASM 73-25/10
3. Fault Confirmation
__________________
R A. Do the operational test of the Engine Interface Unit (Ref. AMM TASK 73-R 25-34-710-040).
4. Fault Isolation
_______________
R A. If the test gives the maintenance message EIU2 : NO FADEC 2B DATA:
R - replace the ECU (4000KS), (Ref. AMM TASK 73-21-60-000-001) and (Ref.
R AMM TASK 73-21-60-400-001).
R (1) If the fault continues:
R - do a check and repair the aircraft wiring of the output 1 bus on
R channel B from the ECU (4000KS) to the first terminal block (Ref.
R ASM 73-25/10).
R B. Do the test given in Para. 3.
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TASK 73-29-00-810-809
Loss of the Output 1 Bus of the ECU 2 Channel B
1. Possible Causes
_______________
- ECU (4000KS)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 22-96-00-710-001 Operational Test of the AFS
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) ASM 73-25/10
3. Fault Confirmation
__________________
R A. Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001).
4. Fault Isolation
_______________
R A. If the test gives the maintenance message AFS : FADEC 1:
R - replace the ECU (4000KS), (Ref. AMM TASK 73-21-60-000-001) and (Ref.
R AMM TASK 73-21-60-400-001).
R (1) If the fault continues:
R - do a check and repair the aircraft wiring of the output 1 bus on
R channel B from the ECU (4000KS) to the first terminal block (Ref.
R ASM 73-25/10).
R B. Do the test given in Para. 3.
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TASK 73-29-00-810-810
Loss of the Output 1 Bus of the ECU 2 Channel B
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 發動機燃油和控制 2(89)
