CESSNA
MODEL 208B 867 SHP
GARMIN G1000
EMERGENCY PROCEDURES
AMBER
BELOW
FLASHING AND AURAL WARNING HORN SOUNDS
IF ENROUTE (FLAPS UP)
1. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . VERIFY DISCONNECT
2. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE
3. Icing Conditions . . . . . . . . . . . . . . . . . . . . EXIT IMMEDIATELY
4. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95 KIAS
5. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
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
When landing is assured the BELOW ICING MIN SPD
annunciator can be pushed to silence the horn.
FAA APPROVED
208BPHCUS-S1-00
SECTION 9 - SUPPLEMENTS
(Continued)
ICING
MIN
(minimum or greater during exit)
WARNING
NOTE
SUPPLEMENT 1
SPD
ANNUNCIATOR
(airspeed above 95 KIAS)
U.S.
S1-31