SECTION 3 CESSNA
EMERGENCY PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
ENGINE FAILURE (Continued)
If an airstart is to be attempted, follow the AIRSTART checklist
procedures. Successful airstarts with starter assist can be achieved at
all airspeeds normally flown and up to an altitude of 14,000 feet.
However, above 14,000 feet, or with the N
g speed below 10%, starting
temperatures tend to be higher and caution is required.
• The FUEL CONDITION lever can be moved
momentarily to CUTOFF and then back to LOW
IDLE if overtemperature tendencies are
encountered. This reduces the flow of fuel to the
combustion chamber.
• If a rise in N
g
and ITT are not indicated within 10
seconds, place FUEL CONDITION lever to CUTOFF
and abort start. Refer to ENGINE FAILURE DURING
FLIGHT and EMERGENCY LANDING WITHOUT
ENGINE POWER.
If the engine starter is inoperative, refer to EMERGENCY LANDING
WITHOUT ENGINE POWER.
208BPHCUS-00
3-40
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