CESSNA SECTION 7
MODEL
182T NAV Ill
AlRPLAhlE AND SYSTEMS DESCRIPTION
INTEGRATED SEAT BELTISHOULDER HARNESS
(Continued)
Removal is accomplished by lifting the release mechanism on the
buckle or by pressing the release button on the buckle and pulling
out and up on the harness. Spring tension on the inertia reel will
automatically stow the harness.
A manually adjustable seat beltlshoulder harness assembly is
available for all seats.
To use the manually adjustable seat beltlshoulder harness, fasten
and adjust the seat beltlshoulder harness first. Lengthen the seat
belt as required by pulling on the release strap on the belt. Snap
the connecting link firmly into the buckle, then adjust to length. A
properly adjusted harness will permit the occupant to lean forward
enough to sit erect, but prevent excessive forward movement and
contact with objects during sudden deceleration. Also, the pilot
must have the freedom to reach all controls easily.
Disconnecting the manually adjustable seat beltlshoulder harness is
accomplished by pushing the button on the buckle to release the
connecting link.
ENTRANCE DOORS AND CABIN WINDOWS
Entry to, and exit from, the airplane is accomplished through either
of two entry doors, one on each side of the cabin, at the front seat
positions (refer to Section
6
for cabin and cabin door dimensions).
The doors incorporate a recessed exterior door handle, a
conventional interior door handle, a key operated door lock (left
door only), a door stop mechanism, and
openable windows in both
the left and right doors.
NOTE
The door latch design on this model requires that the
outside door handle on the pilot and front passenger doors
be extended out whenever the doors are open. When
closing the door, do not attempt to push the door handle in
until the door is fully shut.
(Continued Next Page)
U.S.
7-25
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