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