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CESSNA SECTION 3<br />

MODEL 208B G1000 ABNORMAL PROCEDURES<br />

ABNORMAL LANDING<br />

LANDING WITH FLAT MAIN TIRE<br />

1. Airplane. . . . . . . . . . . . . . . FLY (as desired to lighten fuel load)<br />

2. FUEL SELECTORS . . . . . . . . . . . . POSITION ONE SIDE OFF<br />

(to lighten load on side of flat tire maximum<br />

fuel unbalance of 200 pounds)<br />

3. Approach . . . . . . . . . . . . . . . . . . . . . . NORMAL (FLAPS FULL)<br />

4. Touchdown . . . . . . . . . . . . . . . . . . . . . . INFLATED TIRE FIRST<br />

Hold airplane off flat tire as long as<br />

possible with aileron control.<br />

5. Directional Control . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN<br />

(using brake on wheel with inflated tire as required)<br />

LANDING WITH FLAT NOSE TIRE<br />

1. Passengers and Baggage . . . . . . . . . . MOVE AFT (if practical)<br />

Remain within approved C.G. envelope.<br />

2. Approach . . . . . . . . . . . . . . . . . . . . . . NORMAL (FLAPS FULL)<br />

3. Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOSE HIGH<br />

Hold nose wheel off as long as possible during roll.<br />

4. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM NECESSARY<br />

AVIONICS/AUTOPILOT<br />

AILERON MISTRIM (�AIL OR AIL� INDICATION PFD)<br />

1. Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY<br />

2. AP/TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS<br />

(high aileron control forces possible)<br />

NOTE<br />

The YAW DAMPER does not need to be disconnected for<br />

this procedure. Therefore it is permissible to use the LEFT<br />

half of either Manual Electric Pitch Trim Switch or 1 press of<br />

the AP button on the Autopilot Mode Control panel to<br />

disconnect the autopilot.<br />

3. AILERON TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRIM<br />

4. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE (as desired)<br />

FAA APPROVED<br />

208BPHBUS-01 U.S.<br />

3-51

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