SECTION 6 CESSNA
WEIGHT AND BALANCE/ MODEL T182T NAV III
EQUIPMENT LIST GFC 700 AFCS
U.S.
WEIGHT AND BALANCE (Continued)
BAGGAGE TIEDOWN (Continued)
When baggage is contained in all three areas, the two forward eyebolts
on the cabin floor, the eyebolts just aft of the baggage door or the
eyebolts at the bottom of the forward portion of the shelf area and the
eyebolts near the upper forward surface of the shelf area should be
used.
The rear bench seat can be removed to access the floorboard area of
the rear cabin. Baggage may then be tied down using ten tiedown
eyebolts to standard attach points located in the interior area of the
airplane shown in Figure 6-6.
The maximum allowable floor loading of the rear cabin area is 200
pounds/square foot; however, when items with small or sharp support
areas are carried, the installation of a plywood floor is recommended to
protect the airplane structure.
The maximum rated load weight capacity for each of the ten tiedowns is
140 pounds. Rope, strap or cable used for tiedown should be rated at a
minimum of ten times the load weight capacity of the tiedown fittings
used. Weight and balance calculations for items in the area of the rear
seat and baggage area can be figured on the Loading Graph using the
lines labeled Rear Passengers or Cargo.
T182TPHBUS-00
6-10
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