Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 695

Table of Contents

Advertisement

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
NORMAL PROCEDURES
INFLIGHT (CLIMB, CRUISE, AND DESCENT)
5. Minimum Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95 KIAS
6. WING LIGHT Switch. . . . . . . . . . . . . . . . . . . . . AS REQUIRED
The autopilot may be used in icing conditions. However,
every 10-15 minutes the autopilot should be disengaged to
detect any out of trim conditions caused by ice buildup. If
significant out of trim conditions are detected, the autopilot
should remain off for the remainder of the icing encounter.
When disengaging the autopilot with ice buildup
on the airplane, the pilot should be alert for out
of trim forces. Pilot control wheel input should
be applied as required to prevent potential
undesired flight path deviations.
Monitor airspeed in icing conditions with the
autopilot engaged. The autopilot will maintain
altitude or vertical speed at the expense of
airspeed as drag increases due to ice accretion
on the airplane.
If
pre-stall
oscillations
attitude while increasing power to Max Rated.
Promptly extend WING FLAPS to TO/APR to help
stabilize the airplane. If necessary, do not
attempt to maintain altitude until positive
recovery from buffet is achieved. Increase
airspeed to 95 KIAS or greater before retracting
flaps. If the flaps are subsequently retracted,
maintain at least 10 KIAS above initial buffet
airspeed.
FAA APPROVED
208BPHCUS-S1-00
SECTION 9 - SUPPLEMENTS
(Continued)
NOTE
WARNING
buffet
or
uncommanded
are
encountered,
SUPPLEMENT 1
(Continued)
pitch
reduce
pitch
S1-43
U.S.

Advertisement

Table of Contents
loading

Table of Contents