DA 62 AFM
Abnormal Operating
Procedures
1. Safe altitude . . . . . . . . . . . . . . . . . . . . . . . check
2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . up to 1999 kg (4407 lb):
min. 87 KIAS
above 1999 kg (4407 lb):
min. 89 KIAS
3. FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . check UP
3. LANDING GEAR . . . . . . . . . . . . . . . . . . . . check UP
4. ECU A caution . . . . . . . . . . . . . . . . . . . . . . check OFF
5. VOTER switch . . . . . . . . . . . . . . . . . . . . . . ECU B
6. Wait . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 seconds
7. VOTER switch . . . . . . . . . . . . . . . . . . . . . . AUTO
If the ECU B caution persists: - land at the next suitable airfield.
NOTE
An ECU FAIL CAUTION is caused by various types of
malfunctions. These include internal ECU problems, sensor
failures or insufficient performance of air-, fuel-, or electrical
supply system (e.g. air filter icing).
NOTE
If additional engine problems are observed refer to 3.7.2 -
ENGINE TROUBLESHOOTING.
END OF CHECKLIST
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 4B - 17