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 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
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 A. If the test gives the CFDS message ENG MSTR, HMU or MASTER LEVER, HMU:
 - replace the EIU (1KS2) (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 (2KC) 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 (1KS2) and the pin 2A and 2B of the ENG/MASTER control 
R  switch (2KC). 
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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