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SECTION 3
CESSNA
ABNORMAL PROCEDURES
MODEL 208B G1000
XSIDE AHRS
This message is displayed on both PFDs and indicates that both PFDs
are displaying data from the opposite side Attitude Heading Reference
System. Normally the pilot's side displays ADC1 and the copilot's side
displays ADC 2. Refer to GARMIN G1000 Cockpit Reference Guide for
additional information.
MULTI-FUNCTION DISPLAY FAN FAILED
An overheat condition may arise in the associated display. In this case,
screen brightness will be reduced automatically by 50% to lower
internal temperature. Use reversionary capabilities, if necessary.
PRIMARY FLIGHT DISPLAY 1 FAN FAILED
An overheat condition may arise in the associated display. In this case,
screen brightness will be reduced automatically by 50% to lower
internal temperature. Use reversionary capabilities, if necessary.
PRIMARY FLIGHT DISPLAY 2 FAN FAILED
An overheat condition may arise in the associated display. In this case,
screen brightness will be reduced automatically by 50% to lower
internal temperature. Use reversionary capabilities, if necessary.
INADVERTENT OPENING OF AIRPLANE DOORS IN
FLIGHT
If any of the airplane doors should inadvertently open in flight, the
airplane should be slowed to 125 KIAS or less to reduce buffeting of the
doors. If the upper cargo door is open, slow to 100 KIAS or less and
lower flaps to full down so that wing downwash will move the door
towards its normally closed position. Closing the upper cargo door (or
upper half of the passenger door on the Standard 208B) can be
accomplished after airspeed has been reduced by pulling the door
forcefully closed and latching the door. If the door cannot be closed in
flight, a landing should be made as soon as practical in accordance
with the checklist procedures. On Cargo Versions, an open cargo door
cannot be closed in flight since the inside of the upper door has no
handle.
If any cargo pod doors inadvertently open in flight, the airplane should
be slowed to 125 KIAS or less and landed as soon as practical. During
the landing, avoid a nose-high flare to prevent dragging an open rear
cargo pod door on the runway.
FAA APPROVED
208BPHBUS-01
3-80
U.S.
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