Cessna 206H - Cruise; Descent; Enroute Climb; Maximum Performance Climb

SOLOY TURBINE PAC SECTION 4
POHS CESSNA T206H/206H NORMAL PROCEDURES
4-12
F.A.A. Approved November 17, 2015
ENROUTE CLIMB
NORMAL CLIMB
1. Airspeed – 100 – 120 KIAS
2. Ice Protection – AS REQUIRED
3. Power Control – 78 PSI Torque or 738C TOT and 1810
propeller RPM
4. Fuel Selector Valve - BOTH
MAXIMUM PERFORMANCE CLIMB (V
y
)
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 810C TOT and 1810 N
P
for 5 Minutes Maximum, then 78 PSI Torque or 738C TOT and
1810 propeller RPM.
4. Fuel Selector Valve – FULL OPEN
WARNING
WITH 1/8 FUEL TANK QUANTITY OR LESS, OR IF
THE INSTALLED FUEL LOW LIGHTS ARE ON,
CLIMBS AT SPEEDS BELOW V
y
ARE PROHIBITED.
CRUISE
1. Ice Protection – AS REQUIRED
2. Propeller Speed – SET 1630 – 1810 RPM (Propeller Control)
3. Power Control – SET (Observe TOT and/or Torque Limits)
4. Elevator and Rudder Trim – ADJUST
DESCENT
1. Ice Protection – AS REQUIRED
2. Power Control – SET FLIGHT IDLE
3. Seat Belts and Shoulder Harness – SECURE
4. Altimeter – SET
5. NAV/GPS Switch – SET
6. Fuel Valve – BOTH
7. Wing Flaps – AS DESIRED (0º-10º below 140 KIAS; 10º-40º
below 100 KIAS).
UNCONTROLLED
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