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CESSNA SECTION 4<br />

MODEL 208B G1000 NORMAL PROCEDURES<br />

ENGINE CLEARING PROCEDURES (DRY<br />

MOTORING RUN)<br />

The following procedure is used to clear an engine at any time when it<br />

is deemed necessary to remove internally trapped fuel and vapor, or if<br />

there is evidence of a fire within the engine. Air passing through the<br />

engine serves to purge fuel, vapor, or fire from the combustion section,<br />

gas generator turbine, power turbine, and exhaust system.<br />

1. FUEL CONDITION Lever . . . . . . . . . . . . . . . . . . . . . . . CUTOFF<br />

2. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM<br />

3. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON<br />

(to supply current for the starter motor)<br />

4. AVIONICS No 1 Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON<br />

5. FUEL SHUTOFF Knob . . . . . . . . . . . . . . . . . . OPEN (push in)<br />

6. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF<br />

WARNING<br />

If fire is suspected, leave the FUEL BOOST switch<br />

OFF, otherwise turn it ON to provide lubrication for<br />

the engine-driven fuel pump elements.<br />

7. STARTER Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MOTOR<br />

CAUTION<br />

• Do not exceed the starting cycle limitations; refer to<br />

Section 2.<br />

• Should a fire persist, as indicated by sustained ITT,<br />

close the FUEL SHUTOFF Knob and continue<br />

motoring the engine.<br />

8. STARTER Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF<br />

9. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF<br />

10. AVIONICS No 1 Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF<br />

11. FUEL SHUTOFF Knob . . . . . . . . . . . . . . . . . CLOSED (pull out)<br />

12. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF<br />

Allow the required cooling period for the starter before any further<br />

starting operation is attempted.<br />

FAA APPROVED<br />

208BPHBUS-00 U.S.<br />

4-39

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