Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 694

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 1
NORMAL PROCEDURES
INFLIGHT (CLIMB, CRUISE, AND DESCENT)
At the first indication of ice accretion:
1. Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
a. PRIMARY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
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
g. INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . BYPASS
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)
When climbing
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
Performance, Figure 5-9, Maximum Engine Torque for
Climb for approved settings.
S1-42 U.S.
(Continued)
(for ambient lighting conditions)
(rotate counterclockwise and PULL out)
CAUTION
NOTE
through icing
). Refer to POH/AFM, Section 5,
g
(Continued Next Page)
CESSNA
MODEL 208B 867 SHP
GARMIN G1000
(select HIGH if required)
conditions, it
FAA APPROVED
208BPHCUS-S1-00
is