Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 682

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 1
EMERGENCY PROCEDURES
INADVERTENT ENCOUNTER WITH FREEZING RAIN,
FREEZING DRIZZLE,
CRITICAL ICING SITUATION
APPROACH
1. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE
2. Recommended Airspeed. . . . . . . . . . . . . . . . . . . . . . . 120 KIAS
3. WING FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TO/APR
4. Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
a. PRIMARY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH
b. MAX FLOW Switch . . . . . . AIRFRAME then WINDSHIELD
c. P/S HEAT/LOW A/S AWARE Switch . . . . . . . . . . . . . . . ON
d. STALL HEAT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
e. LED PANELS/ANNUN Rheostat. . . . . . . . . . . . . . ADJUST
f. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
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.
5. ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY
(declare an emergency and request straight-in approach)
6. Minimum Airspeed. . . . . . . . . . . . . . . . . . . . . . . . . . . . 110 KIAS
S1-30 U.S.
OR OTHER
(Continued)
(as required to maintain airspeed and glidepath)
Do not exceed 850° ITT or 103.7% Ng.
(for ambient lighting conditions)
(rotate counterclockwise and PULL out)
CAUTION
MODEL 208B 867 SHP
GARMIN G1000
(Continued)
PERFORMANCE
(press momentarily)
FAA APPROVED
208BPHCUS-S1-00
CESSNA