NOTICE

SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B G1000
TAKEOFF
POWER SETTING
Refer to the Maximum Engine Torque for Takeoff chart in Section 5 to
determine the torque corresponding to the surface altitude and OAT
conditions. This torque should be obtainable without exceeding 805°C
ITT or 101.6% N g .
Takeoff roll is most smoothly initiated by gradually advancing the
POWER Lever until propeller RPM nears 1900. Smoothly release the
brakes and continue advancing the POWER Lever until the takeoff
torque is reached.
NOTE
As airspeed increases during takeoff, an increase in torque
at a fixed POWER Lever position is normal and need not be
reduced provided the torque limit (1865 foot-pounds) is not
exceeded.
WING FLAP SETTINGS
A flap setting of 20° is recommended for all takeoffs unless a strong
crosswind exists at which time 10° flaps may be preferred. Use of 20°
flaps provides for a lower liftoff speed, as well as a reduction in ground
roll and total distance over an obstacle compared to takeoff with flaps
up.
Flap settings greater than 20° are not approved for takeoff.
SHORT FIELD TAKEOFF
If an obstruction dictates the use of a steep climb angle after liftoff,
accelerate to and climb at an obstacle clearance speed of 83 KIAS with
20° flaps. Takeoff performance data is shown in Section 5 based on this
speed and configuration.
4-44
NOTE
The 83 KIAS obstacle clearance speed is a recommended
safe speed under all conditions, including turbulence and
complete engine failure. The actual VX speed with flaps 20°
is 70 KIAS at maximum takeoff weight as noted in the Climb
Gradient - Takeoff Flap Setting - Flaps 20 chart in Section 5.
U.S.
(Continued Next Page)
FAA APPROVED
208BPHBUS-00