DA 62 AFM
Emergency
Procedures
NOTE
If the problem does not clear itself, switch back to AUTO and
land on the nearest suitable airfield.
(b) Propeller Overspeed
NOTE
This procedure applies for continued propeller overspeed
due to a malfunction in the propeller constant speed unit or
a engine control unit malfunction.
1. POWER setting . . . . . . . . . . . . . . . . . . . . . . . reduce as required
If the problem does not clear:
2. Garmin G1000 . . . . . . . . . . . . . . . . . . . . . . . . check L/R ECU A/B FAIL caution
If L/R ECU A FAIL indicated:
3. VOTER switch . . . . . . . . . . . . . . . . . . . . . . . . ECU B
If L/R ECU B FAIL indicated:
3. VOTER switch . . . . . . . . . . . . . . . . . . . . . . . . ECU A
CAUTION
If the problem does not clear itself, switch back to AUTO and
land on the nearest suitable airfield. Prepare for engine
malfunction according to 3.7.6 - ENGINE FAILURES IN
FLIGHT.
CONTINUED
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 3 - 67