Cessna 206H - Engine Failure During Flight; Engine Failure Immediately after Takeoff; Engine Restart Procedure During Flight

SOLOY TURBINE PAC SECTION 3
POHS CESSNA T206H/206H EMERGENCY PROCEDURES
3-4
F.A.A. Approved May 23, 2003
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
1. Airspeed – 80 KIAS
2. Propeller Control – FEATHER (OUT)
3. Fuel Cutoff Control – CUTOFF (OUT)
4. Fuel Selector Valve – OFF (PRESS DOWN SAFETY SPRING
TO ALLOW MOVEMENT TO OFF)
5. Wing Flaps – AS REQUIRED (40 recommended)
6. Battery – OFF
ENGINE FAILURE DURING FLIGHT
1. Airspeed – BEST GLIDE SPEED
2. Fuel Cutoff Control – CUTOFF (OUT)
3. Monitor TOT
4. Propeller Control – FEATHER (OUT)
5. Power Control – FLIGHT IDLE
6. Generator – OFF
7. Electrical Load – REDUCE
8. If airstart is warranted, refer to ENGINE RESTART
PROCEDURE CHECKLIST.
9. If airstart is not warranted, refer to EMERGENCY LANDING
WITHOUT ENGINE POWER CHECKLIST.
ENGINE RESTART PROCEDURE DURING FLIGHT
1. Fuel Cutoff Control – CUTOFF (OUT)
2. Propeller Control – FEATHER (OUT)
3. Engine Inlet Anti-Ice – OFF
4. ACTIVATE engine alternate air system if in icing conditions.
5. Airspeed 75 – 120 KIAS below 15,000 FT. MSL.
110 – 120 KIAS 15,000 to 20,000 FT. MSL.
6. Fuel Selector – ON (BOTH if fuel low warning system installed).
7. Power Control – FLIGHT IDLE
8. Start Motor Switch – MOTOR
9. TOT 150 or lower and N
1
15% below 15,000 FT. MSL.
N
1
maximum obtainable above 15,000 FT. MSL.
10. Start Motor Switch – START and hold
11. Fuel Cutoff Control – RUN (IN)
12. TOT and N
1
– MONITOR (810 to 927C FOR 10 SECONDS
MAXIMUM)
13. De-energize the starter at 58% N
1
14. Propeller Control – IN
UNCONTROLLED
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