Textron Cessna Grand Caravan Ex 208B - Page 683

CESSNA SECTION 9 - SUPPLEMENTS
MODEL 208B 867 SHP SUPPLEMENT 1
GARMIN G1000
U.S.
FAA APPROVED
EMERGENCY PROCEDURES (Continued)
AMBER BELOW ICING MIN SPD ANNUNCIATOR
FLASHING AND AURAL WARNING HORN SOUNDS
IF ENROUTE (FLAPS UP)
1. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . VERIFY DISCONNECT
2. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE
(airspeed above 95 KIAS)
3. Icing Conditions . . . . . . . . . . . . . . . . . . . . EXIT IMMEDIATELY
4. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95 KIAS
(minimum or greater during exit)
5. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
WARNING
WING Flaps must be extended to TO/APR anytime
airspeed is below 95 KIAS.
IF ON APPROACH (WING FLAPS - TO/APR)
1. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . VERIFY DISCONNECT
2. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE
3. Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTINUE
4. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
(observe minimum airspeed for icing with WING FLAPS TO/
APR)
5. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
NOTE
When landing is assured the BELOW ICING MIN SPD
annunciator can be pushed to silence the horn.
S1-31208BPHCUS-S1-00