(2) Make sure that there is no ECAM and CFDS fault message shown.
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TASK 76-12-00-810-828
Disagree between HPSOV position and Master Lever position on Engine 1
1. Possible Causes
_______________
- EIU (1KS1)
- CTL SW-ENG/MASTER 1 (3KC)
- HMU
- aircraft wiring
- ECU (4000KS)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 73-21-10-000-002 Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-002 Installation of the Hydromechanical Unit (HMU)
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 73-29-00-710-040 Operational Test of the FADEC on the Ground (with Engine Non motoring) ASM 76-12/01 R AWM 76-12-01
3. Fault Confirmation
__________________
A. Do the operational test of the FADEC on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
4. Fault Isolation
_______________
A. If the test gives the CFDS message ENG MSTR, HMU or MASTER LEVER, HMU:
- replace the EIU (1KS1) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
(1) If the fault continues: R - replace the CTL SW-ENG/MASTER 1 (3KC) on the 115VU (Ref. AWM 76-12-R 01).
(2) If the fault continues:
- replace the HMU (Ref. AMM TASK 73-21-10-000-002) and (Ref. AMM TASK 73-21-10-400-002).
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R (3) If the fault continues:
R - do a check of the aircraft wiring between the pin AA/4E and AA/5A
R of EIU (1KS1) and the pin 2A and 2B of ENG/MASTER control switch
R (3KC).
R (a) If there is no continuity:
R - repair the above wiring (Ref. ASM 76-12/01)
R (4) If the fault continues:
R - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref.
R AMM TASK 73-21-60-400-001).
R B. Do the test given in Para. 3.
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TASK 76-12-00-810-829
Disagree between HPSOV position and Master Lever position on Engine 2
1. Possible Causes
_______________
- EIU (1KS2)
- CTL SW-ENG/MASTER 1 (2KC)
- HMU
- aircraft wiring
- ECU (4000KS)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 73-21-10-000-002 Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-002 Installation of the Hydromechanical Unit (HMU)
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 73-29-00-710-040 Operational Test of the FADEC on the Ground (with Engine Non motoring) ASM 76-12/01 R AWM 76-12-01
3. Fault Confirmation
__________________
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 發動機控制(26)
