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CESSNA SECTION 3<br />

MODEL 208B G1000 EMERGENCY PROCEDURES<br />

ENGINE MALFUNCTIONS<br />

LOSS OF OIL PRESSURE (Red OIL PRESS LOW CAS<br />

MSG)<br />

1. Oil Pressure Indication . . . . . . . . . . . . . . . . . . . . . . . MONITOR<br />

CAUTION<br />

If oil pressure indications confirm warning CAS MSG,<br />

proceed in accordance with Engine Failures checklists<br />

or at the discretion of the pilot and consistent with<br />

safety, continue engine operation in preparation for an<br />

emergency landing as soon as possible.<br />

FUEL CONTROL UNIT MALFUNCTION IN THE<br />

PNEUMATIC OR GOVERNOR SECTIONS (Engine Power<br />

Rolls Back To Idle)<br />

1. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE<br />

2. EMERGENCY POWER Lever . . . . . . . . . . . . . . . . . . . . . . USE<br />

(maintain 65% Ng minimum during flight)<br />

CAUTION<br />

The EMERGENCY POWER lever overrides normal fuel<br />

control functions and results in the direct operation of<br />

the fuel metering valve. Utilize slow and smooth<br />

movement of the EMERGENCY POWER lever to avoid<br />

engine surges, and/or exceeding ITT, Ng , and torque<br />

limits.<br />

EMERGENCY POWER LEVER NOT STOWED (Red EMERG<br />

PWR LVR CAS MSG)<br />

1. EMERGENCY POWER Lever . . . . . . . . . . . VERIFY NORMAL<br />

FAA APPROVED<br />

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

3-27

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