Beechcraft Baron 58 - Loading Instructions; MOMENT LIMITS Vs WEIGHT

Section VI
Wt and BaljEquip list
LOADING INSTRUCTIONS
BEECHCRAFT Baron 58
Serial TH 773 and After
It is the responsibility of the airplane operator to ensure that
the airplane is properly loaded. At the time of delivery,
Beech
Aircraft Corporation provides the necessary weight
and balance data to compute individual loadings. All
subsequent changes in airplane weight and balance are the
responsibility of the airplane owner and/or operator.
The
empty weight and moment of the airplane at the time of
delivery are shown on the airplane Empty Weight and
Balance form. Useful load
items which may be loaded into
the airplane are shown on the Useful Load Weight and
Moment tables. The minimum and maximum moments are
indicated on the Moment Limits vs Weight table. These
moments correspond to the forward and aft center of gravity
flight limits for a particular weight. All moments are divided
by 100 to simplify computations.
MOMENT LIMITS vs WEIGHT
Moment limits are based on the following weight and
center of gravity limit data (landing gear down).
WEIGHT FORWARD
CONDITION CG LIMIT AFT CG LIMIT
5400 lb. (58
78.0
86.0
max. take-off
or landing)
4990 lb. (58A
76.6 86.0
max. take-off
or landing)
4200 lb. or less 74.0
86.0
6~10
October 1 976