Weight And Balance Responsibilities - Beechcraft C23 SUNDOWNER 180 Pilot Operating Handbook

BEECHCRAFT Sundowner 180 Section VI
C23 (M-1285
and
After) Wt
and
Bal/Equip List
WEIGHT AND BALANCE RESPONSIBILITIES
The Basic Empty Weight and Moment of
the
airplane at the
time of delivery are shown on
the
airplane Basic Empty
Weight and Balance form. Useful
load items which
may be
loaded
into the airplane are
shown
on the Useful Load
Weights and Moments tables. The minimum and maxi-
mum moments are shown on the Moment Limits vs
Weight
table
and can also be
plotted
on the Moment Limits
vs Weight graph as
visual
indication thatthe limit is within
the operational
envelope. These moments correspond to
the forward and aft center-of-gravity
flight limits for a
particular
weight. The airplane must be loaded in such a
manner to keep the center-of-gravity
within
these limits.
NOTE
THE FLOOR STRUCTURE LOAD LIMIT
IS
100
POUNDS
PER SQUARE FOOT.
ALL
BAGGAGE/CARGO
MUST BE
SECURED.
August,
1980
6-11