SECTION 6
CESSNA
WEIGHT
&
BALANCEIEQUIPMENT LIST
MODEL
2088 (675 SHP)
WEIGHT
AND BALANCE
(Continued)
NOTE
Information on the Crew And Passenger and Cargo Weight
And Moment Tables is based on the pilot and front
passenger sliding seats positioned for average occupants
(e.g., 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., station
172.0 in zone 1) of the zone fore and aft boundaries
(e.g.,
stations 155.4 and 188.7 in zone I) shown on the Loading
Arrangements diagrams. For loadings which may differ
from these, the Loading Arrangements diagrams and
Sample Loading Problem lists fuselage stations for these
items to indicate their
foward 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 the Loading
Arrangements diagram, the moment must be calculated by
multiplying the occupant weight times the arm in inches. A
point
9
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
momentdl000 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.
WARNING
IT IS THE RESPONSIBILITY OF THE PILOT TO ENSURE
(Continued Next Page)
Revision 23
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