CESSNA SECTION 7
MODEL T182T NAV III AIRPLANE AND SYSTEM DESCRIPTION
GFC 700 AFCS
U.S.
LANDING GEAR SYSTEM
The landing gear is of the tricycle type, with a steerable nosewheel and
two main wheels. Wheel fairings are standard equipment for both the
main wheels and nosewheel. Shock absorption is provided by the
tubular spring steel main landing gear struts and the air/oil nose gear
shock strut. Each main gear wheel is equipped with a hydraulically-
actuated disc type brake on the inboard side of each wheel.
BAGGAGE COMPARTMENT
The baggage compartment consists of the area from the back of the
rear passenger seats to the aft cabin bulkhead. Access to the baggage
compartment is gained through a lockable baggage door on the left
side of the airplane, or from within the airplane cabin. A baggage net
with tiedown straps is provided for securing baggage and is attached by
tying the straps to tiedown rings provided in the airplane. For baggage
area and door dimensions, refer to Section 6.
T182TPHBUS-01
7-23
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