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ENGINE FAILURE DURING TAKEOFF
(AT OR ABOVE V )—TAKEOFF CONTINUED
1
1. Power ................................................................................ MAXIMUM ALLOWABLE
2. Airspeed ........................................................ MAINTAIN (take-off speed or above)
3. Landing Gear (when positive climb established) ............................................... UP
4. Propeller (inoperative engine) ............................................... VERIFY FEATHERED
5. Airspeed (after obstacle clearance altitude is reached) ................................ V YSE
MENU RETURN King Air B200 & B200C Pro Line 21
Revision 1.1 FOR TRAINING PURPOSES ONLY E-5A