SOLOY TURBINE PAC SECTION 4
POHS CESSNA T206H/206H NORMAL PROCEDURES
4-26
F.A.A. Approved May 23, 2003
BALKED LANDING
In a balked landing (go-around) climb, apply power as required
and maintain torque and TOT within allowable limits. The flap
setting should be reduced to 20. After all obstacles are cleared
and a safe altitude and airspeed are obtained, the wing flaps
should be retracted.
SECURING AIRPLANE
After the airplane is taxied to a stop, set the parking brake. Turn off the
avionics master switch and all other radio and electrical switches.
After two minutes of engine operation (taxi time may be included) at N
1
speeds of 59% to 65%, move the Fuel Cutoff Control to the CUTOFF
position. The propeller can also be feathered above 700 N
p
RPM at
shutdown to minimize the spool down time of the propeller.
WARNING
IDLE DWELL TIME PRIOR TO SHUTDOWN IS
IMPORTANT TO PREVENT HARMFUL
ACCUMULATION OF CARBON IN THE ENGINE,
WHICH CAN RESULT IN COMPLETE ENGINE
STOPPAGE.
CAUTION
AN AFTERFIRE (RECOGNIZED BY A RAPID
INCREASE IN TOT) CAN OCCUR DURING
SHUTDOWN IF FUEL CUTOFF IS NOT
COMPLETE. IF A SHUTDOWN FIRE OCCURS,
IMMEDIATELY ENGAGE THE STARTER AND
MOTOR THE ENGINE WITHOUT IGNITION TO
EXTINGUISH THE FIRE. THE TEMPERATURE
LIMITATIONS AND MAINTENANCE ACTION
MUST BE OBSERVED.
Engines subjected to salt water or other chemically laden atmosphere
(including pesticides) shall undergo water rinsing after shutdown following
the last flight of the day. Procedures for the rinse, cleaning and
preservation of the compressor are explained in the Rolls Royce 250-C20
Series, Operation and Maintenance Manual.
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