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SECTION 3 CESSNA<br />

EMERGENCY PROCEDURES MODEL 208B G1000<br />

EXPANDED EMERGENCY<br />

ENGINE FAILURE<br />

If an engine failure occurs during the takeoff roll, the most important<br />

thing to do is stop the airplane on the remaining runway. Those extra<br />

items on the checklist will provide added safety after a failure of this<br />

type.<br />

Prompt lowering of the nose to maintain airspeed and establish a glide<br />

attitude is the first response to an engine failure after takeoff.<br />

Feathering the propeller substantially reduces drag, thereby providing<br />

increased glide distance. In most cases, the landing should be planned<br />

straight ahead with only small changes in direction to avoid<br />

obstructions. Altitude and airspeed are seldom sufficient to execute a<br />

180° gliding turn necessary to return to the runway. The checklist<br />

procedures assume that adequate time exists to secure the fuel and<br />

electrical systems prior to touchdown.<br />

After an engine failure in flight, the best glide speed, as shown in Figure<br />

3-1, should be established as quickly as possible. Propeller feathering<br />

is dependent on existing circumstances and is at the discretion of the<br />

pilot. Maximum RPM selection will provide increased gas generator<br />

windmilling speed for emergency restarts in the event of a starter<br />

failure. On the other hand, to obtain the maximum glide, the propeller<br />

must be feathered.<br />

3-30<br />

U.S.<br />

(Continued Next Page)<br />

FAA APPROVED<br />

208BPHBUS-01

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