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SECTION 4 CESSNA<br />

NORMAL PROCEDURES MODEL 208B G1000<br />

SHORT FIELD LANDING (Continued)<br />

The landing performance in Section 5 is based on the above<br />

procedure. A reduction in ground roll of approximately 10% will result<br />

from the use of reverse thrust (POWER Lever full aft to provide<br />

increased power from the gas generator and a reverse thrust propeller<br />

blade angle).<br />

CAUTION<br />

To minimize propeller blade erosion or possible<br />

propeller blade damage, reverse thrust should be used<br />

only when necessary to shorten the ground roll.<br />

Bringing the propeller out of reverse before<br />

decelerating through approximately 25 knots will<br />

minimize propeller erosion.<br />

CROSSWIND LANDING<br />

For crosswind approaches, either the wing-low, crab or combination<br />

method can be used. A flap setting between 10° and 30° is<br />

recommended. Use a minimum flap setting for the field length. After<br />

touchdown, lower the nose wheel and maintain control. Maintain a<br />

straight course using the steerable nose wheel, ailerons, and<br />

occasional braking if necessary.<br />

BALKED LANDING<br />

In a balked landing (go-around) climb, the wing flap setting should be<br />

reduced to 20° after takeoff power is applied. After all obstacles are<br />

cleared and a safe altitude and airspeed are obtained, the WING<br />

FLAPS should be retracted.<br />

4-52<br />

U.S.<br />

FAA APPROVED<br />

208BPHBUS-00

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