SECTION 3 CESSNA
ABNORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
FUEL
AMBER FUEL BOOST ON ANNUNCIATOR COMES ON
1. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . CHECK ON
IF CONDITIONS DO NOT WARRANT ITS USE
2. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
AMBER FUEL PRESS LOW ANNUNCIATOR COMES ON
IF AMBER FUEL PRESS LOW AND AMBER FUEL BOOST ON
ANNUNCIATORS REMAIN ON
4. Engine Indicating System . . . . . . . . . . . . . . . . . . . . . MONITOR
Watch for signs of fuel starvation.
5. Land as soon as possible.
IF AMBER FUEL PRESS LOW ANNUNCIATOR GOES OFF
4. FUEL QTY Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
(maximum fuel imbalance 200 pounds)
Carefully monitor fuel quantity and cabin odor for
evidence of a fuel leak.
5. Land as soon as practical and determine cause for motive flow
failure before next flight.
AMBER L, R, OR L-R FUEL LOW ANNUNCIATOR COMES
ON
1. FUEL TANK SELECTORS . . . . . . . . . . . . . . . . . . . . BOTH ON
2. FUEL QTY Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(maximum fuel imbalance 200 pounds)
1. FUEL TANK SELECTORS . . . . . . . . . . . . . . . . . BOTH ON
2. FUEL BOOST Switch
. . . . . . . . . . . . . . . . . . . . . . . . . . ON
3. IGNITION Switch
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
208BPHCUS-003-92