Emergency
Procedures
DA 62 AFM
(b) Engine Failure During Flight
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 up to 95% load
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
Page 3 - 38 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E
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