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时间:2011-03-29 14:33来源:蓝天飞行翻译 作者:航空
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 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
 C. Test
 (1) Start the engine 2 by the engine automatic start procedure (Ref. AMM TASK 71-00-00-710-003).

 (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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