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
Summary of Contents for Cessna Grand Caravan Ex 208B
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