SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
TAKEOFF
NORMAL TAKEOFF
1.
Wing Flaps – 0 to 20
2.
Power Control – FLIGHT IDLE and stabilize at 1810 N
then TAKEOFF POWER (101.4 PSI torque or 810C TOT limits).
3.
Elevator Control – LIFT NOSE at 50 KIAS
4.
Climb Speed – 90 – 100 KIAS
5.
Wing Flaps – RETRACT after obstacles are cleared.
SHORT FIELD TAKEOFF
1.
Wing Flaps – 20
2.
Brakes – APPLY
3.
Power Control – FLIGHT IDLE STABILIZED AT 1810 N
then TAKEOFF POWER,
4.
Brakes – RELEASE
5.
Elevator Control – SLIGHTLY TAIL-LOW ATTITUDE
6.
Climb Speed – 60 KIAS until all obstacles are cleared.
7.
Wing Flaps – RETRACT after obstacles are cleared and 80 – 90
KIAS is reached.
Do not reduce power until wing flaps have
been retracted.
WITH 1/8 FUEL TANK QUANTITY OR LESS,
OR IF THE INSTALLED FUEL LOW LIGHTS
ARE ON, TAKEOFF IS PROHIBITED.
ENROUTE CLIMB
NORMAL CLIMB
1.
Airspeed – 100 – 120 KIAS
2.
Ice Protection – AS REQUIRED
3.
Power Control – 78 PSI Torque or 738C TOT and 1810 N
RPM
MAXIMUM PERFORMANCE CLIMB (V
1.
Airspeed – 97 KIAS at sea level to 74 KIAS at 20,000 feet with 5
minute power and 87 KIAS to 71 KIAS with max. continuous
power.
2.
Ice Protection – AS REQUIRED
3.
Power Control – 101.4 PSI Torque or 810C TOT and 1810 N
RPM for 5 Minutes Maximum, then 78 PSI Torque or 738C TOT
and 1810 N
F.A.A. Approved
NOTE
WARNING
RPM
p
4-9
SECTION 4
NORMAL PROCEDURES
)
y
October 4, 2005
RPM,
P
RPM,
P
p
P