SECTION 9 - SUPPLEMENTS
CESSNA
SUPPLEMENT 1
MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
NORMAL PROCEDURES
(Continued)
INFLIGHT (CLIMB, CRUISE, AND DESCENT)
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 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.
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.
PROP RPM Lever . . . . . . . . . . . . . . . . . . . . . . . . . . .
1900 RPM
4.
POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INCREASE
(as required to maintain safe airspeed or to climb out of icing
conditions, if possible)
NOTE
When climbing through icing conditions, it is
recommended that the Maximum Climb Power rating be
used (1900 RPM and 2397 ft-lb., not to exceed 825°C ITT
or 103.7% N
g
). Refer to POH/AFM, Section 5,
Performance, Figure 5-9, Maximum Engine Torque for
Climb for approved settings.
(Continued Next Page)
208BPHCUS-S1-00
S1-42
Summary of Contents for Cessna Grand Caravan Ex 208B
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