SECTION 9 - SUPPLEMENTS
CESSNA
SUPPLEMENT 1
MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
EMERGENCY PROCEDURES
(Continued)
INADVERTENT ICING ENCOUNTER AT ALTITUDES
ABOVE 20,000 FEET
1.
IGNITION Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
2.
Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
a.
PRIMARY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . .
NORM
(select HIGH if required)
b.
MAX FLOW Switch . . . . . . . . . . . . . . . . . . . .
WINDSHIELD
(press momentarily and repeat if necessary to keep
windshield free of ice)
c.
P/S HEAT/LOW A/S AWARE Switch . . . . . . . . . . . . . . .
ON
d.
STALL HEAT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
e.
INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . .
BYPASS
(rotate counterclockwise and PULL out)
CAUTION
If the INERTIAL SEPARATOR is set to BYPASS at any
point due to suspected or actual icing conditions, do not
return it to NORMAL until the inertial separator door has
been visually inspected and verified free of ice and ice
protection fluid.
3.
CABIN HEAT and DEFROST Controls . . . . . . . . . . . . . . . . .
ON
4.
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . .
160 KIAS MAXIMUM
5.
Altitude . . . . . . . . . . . . . . . . . . . . .
DESCEND TO 20,000 FEET
(or below as soon as practical)
NOTE
•
Operate in accordance with the Normal Procedures
contained in this supplement at altitudes of 20,000 feet
or below.
•
Do not climb above 20,000 feet with any residual ice on
the airplane, regardless of atmospheric conditions.
•
Turn IGNITION switch OFF after exiting icing conditions.
208BPHCUS-S1-00
S1-24
Summary of Contents for Cessna Grand Caravan Ex 208B
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