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SECTION 6
CESSNA
MODELT210M
WEIGHT
&
BALANCE/
EQUIPMENT LIST
WEIGHT AND BALANCE
The following information will enable you to operate your Cessna
within the prescribed weight and center of gravity limitations. To figure
weight and
balance,
use the Sample Loading Problem, Loading Graph, and
Center of Gravity Moment Envelope as
follows:
Take the basic empty weight and moment from appropriate weight and
balance records carried in your airplane, and enter them in the column
.-----..
titled YOUR AIRPLANE on the Sample Loading
Problem.
NOTE
In addition to the basic empty weight and moment noted on
these
records,
the C.G. arm (fuselage station) is also
shown, but need not be used on the Sample Loading
Problem. The moment which is shown must be divided by
1000 and this value used as the moment/ 1000 on the loading
problem.
Use the Loading Graph to determine the moment/ 1000 for each
additional item to be carried, then list these on the
loading
problem.
NOTE
Loading Graph information for the pilot, passengers and
baggage is based on seats positioned for average occu-
pants and baggage loaded in the center of the baggage
areas as shown on the Loading Arrangements
diagram.
For loadings
whi
ch may differ from these, the Sample
Loading Problem lists fuselage stations for these items to
indicate their forward and aft C.G. range limitation (seat
travel or baggage area limitation). Additional moment
calculations,
based on the actual weight and
C.G.
arm
(fuselage station) of the item being loaded, must be made if
the position of the load is different from that shown on the
Loading Graph.
Total the weights and moments/ 1000 and plot these values on the
Center of Gravity Moment Envelope to determine whether the point falls
within the envelope, and if the loading is acceptable.
BAGGAGE TIE-DOWN
A nylon baggage net having six tie-down straps is provided to secure
baggage in the area aft of the wheel well and on the backs of the fifth and
sixth seats when they are used for stowing
baggage.
6-6
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