CESSNA SECTION 3
MODEL 208B 867 SHP EMERGENCY PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
ENGINE FAILURES (Continued)
ENGINE FLAMEOUT DURING FLIGHT
AFTER SATISFACTORY RELIGHT AS EVIDENCED BY NORMAL
ITT AND N
g
INDICATIONS
3. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
4. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
(if cause of flameout has been corrected)
2.
2. Refer to AIRSTART procedure on following page for engine
restart information.
IF GAS GENERATOR SPEED (N
g
) IS ABOVE 50%
1. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
2. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
IF GAS GENERATOR SPEED (N
g
) IS BELOW 50%
1. FUEL CONDITION Lever. . . . . . . . . . . . . . . . . . . . . . CUTOFF
208BPHCUS-00 3-11
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