Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 120

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Emergency
Procedures
DA 42 NG AFM
Page 3 - 36 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E
3.7.6 ENGINE FAILURES IN FLIGHT
(a) Engine Failure During Initial Climb
WARNING
As the climb is a flight condition which is associated with high
power settings, airspeeds lower than v
MCA
= 71 KIAS (flaps
UP) or 68 KIAS (flaps APP) 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
= 85 KIAS/
above v
MCA
= 71 KIAS (flaps UP)
or v
MCA
= 68 KIAS (flaps APP) as
required
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
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