CESSNA SECTION 6
MODEL 208B 867 SHP WEIGHT AND BALANCE/
GARMIN G1000 EQUIPMENT LIST
U.S.
WEIGHT AND BALANCE (Continued)
Information on the Weight and Moment Tables for crew,
passenger, and cargo is based on the pilot and front
passenger sliding seats positioned for average occupants
(e.g., Fuselage Station 135.5), the aft passenger fixed seats
(if installed) in the recommended position, and the baggage
or cargo uniformly loaded around the center (e.g., Fuselage
Station 172.1 in Zone 1) of the zone fore and aft boundaries
(e.g., Fuselage Stations 155.4 and 188.7 in Zone 1) shown
on Figure 6-11, Cabin Internal Loading Arrangements. For
loadings which may differ from these, the Loading
Arrangements figure and Sample Loading Problem lists
Fuselage Stations for these items to indicate their forward
and aft C.G. range limitations. 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
Weight and Moment Tables. For example, if seats are in
any position other than stated on Figure 6-11, Cabin
Internal Loading Arrangements, the moment must be
calculated by multiplying the occupant weight times the arm
in inches. A point nine inches forward of the intersection of
the seat bottom and seat back (with cushions compressed)
can be assumed to be the occupant C.G. For a reference in
determining the arm, the forward face of the raised aft
cargo floor is Fuselage Station 332.0.
Total the weights and moments/1000 and plot these values on the
Figure 6-18, Center of Gravity Moment Envelope to determine whether
the point falls within the envelope, and if the loading is acceptable.
It is the responsibility of the pilot to make sure that
the airplane is correctly loaded. Operation outside
of prescribed weight and balance limitations could
result in an accident and serious or fatal injury.
(Continued Next Page)
208BPHCUS-00 6-11
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