NOTICE

CESSNA SECTION 7
MODEL 208B G1000 AIRPLANE AND SYSTEMS DESCRIPTION
PILOT'S AND COPILOT'S SEATS (Continued)
The seat is not locked if the pin is retracted or only partially extends.
Raise or lower the seat by rotating a large crank under the front right
corner of the seat. Seat back angle is adjusted by rotating a small crank
under the front left corner of the seat. The seat bottom angle will
change as the seat back angle changes, providing proper support.
Seats are equipped with armrests which can be moved to the side and
raised to a position beside the seat back for stowage.
AFT PASSENGERS’ SEATS (COMMUTER) (Passenger
Version)
The third, sixth and eleventh seats of one Commuter configuration and
all aft seats of the second Commuter configuration are individual fixedposition
seats with fixed seat backs. Seats for the fourth and fifth,
seventh and eighth, and ninth and tenth positions of the first Commuter
configuration are two-place, fixed-position bench type seats with fixed
seat backs. All seats are fastened with quick-release fasteners in the
fixed position to the seat tracks. The seats are lightweight and quickremovable
to facilitate cargo hauling.
AFT PASSENGERS’ SEATS (UTILITY) (Passenger Version)
Individual collapsible seats are available for the aft eight passenger
positions. The seats, when not in use, are folded into a compact space
for stowage in the aft baggage area. When desired, the seats can be
unfolded and installed in the passenger area. The seats are readily
fastened with quick-release fasteners to the seat tracks in any one of
the eight seat positions.
HEADRESTS
Headrests are available for all pilot and passenger seat configurations,
except the Utility aft passenger seats. To adjust a pilot’s seat or copilot
seat headrest, apply enough pressure to it to raise or lower it to the
desired level. The aft passenger seat headrests are not adjustable.
208BPHBUS-00
U.S.
7-27