SECTION 9 - SUPPLEMENTS
CESSNA
SUPPLEMENT 1
MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
NORMAL PROCEDURES
(Continued)
APPROACH
If icing conditions exist, are anticipated, or at the first indication of ice
accretion:
1.
Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
a.
PRIMARY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . .
NORM
(select HIGH if required)
b.
MAX FLOW Switch . . . . . . . . . . . . . . . . . . . .
WINDSHIELD
(press momentarily)
c.
P/S HEAT/LOW A/S AWARE Switch . . . . . . . . . . . . . . .
ON
d.
STALL HEAT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
e.
BELOW ICING MIN SPD Switch Light . .
PRESS TO TEST
f.
LED PANELS/ANNUN Rheostat. . . . . . . . . . . . . .
ADJUST
(for ambient lighting conditions)
g.
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.
2.
CABIN HEAT and DEFROST Controls . . . . . . . . . . . . . . . . .
ON
3.
WING LIGHT Switch . . . . . . . . . . . . . . . . . . . . .
AS REQUIRED
208BPHCUS-S1-00
S1-44
Summary of Contents for Cessna Grand Caravan Ex 208B
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