DA 62 AFM
Emergency
Procedures
3.7.6 ENGINE FAILURES IN FLIGHT
(a) Engine Failure During Initial Climb
WARNING
As climb is a flight condition which is associated with high
power settings, airspeeds lower than v
MCA
= 76 KIAS (flaps
UP) or 70 KIAS (flaps T/O) should be avoided as a sudden
engine failure can lead to loss of control. In this case, it is
very important to reduce the asymmetry in thrust to regain
directional control.
1. Rudder. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . maintain directional control
2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . v
YSE
= 87 KIAS up to 1999 kg
(4407 lb)
89 KIAS above 1999 kg (4407 lb)
3. Operative engine . . . . . . . . . . . . . . . . . . . . . . increase power as required if directional
control has been established
Establish minimum/zero sideslip condition. (approx. half ball towards good engine;
3° to 5° bank).
4. Inoperative engine . . . . . . . . . . . . . . . . . . . . . Secure according to 3.7.3 - ENGINE
SECURING (FEATHERING)
PROCEDURE
Land as soon as possible according to 3.7.7 - LANDING WITH ONE ENGINE
INOPERATIVE. If a diversion is required before landing, continue according to Section
3.7.9 - FLIGHT WITH ONE ENGINE INOPERATIVE.
END OF CHECKLIST
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 3 - 37
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