SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
ENGINE IGNITION PROCEDURES
For most operations, the IGNITION switch is left in the NORM position.
With the switch in this position, ignition is on only when the STARTER
switch is in the START position.
The use of ignition for extended periods of time will reduce
ignition system component life.
The IGNITION switch should be turned ON to provide continuous
ignition under the following conditions:
1. Operation on wet or contaminated runways.
2. Flight in heavy precipitation.
3. Flight in moderate or greater turbulence.
4. During inadvertent icing encounters prior to the INERTIAL
SEPARATOR being selected to BYPASS.
5. When near fuel exhaustion as indicated by Red RSVR FUEL
LOW annunciator.
Refer to Section 7, Airplane and System Description, Engine Ignition
System, for further details regarding the ignition system.
208BPHCUS-004-52
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