Beechcraft Baron 58 - Page 41

BEECHCRAFT Baron 58
Serial TH 773 and After
Section I
General
e.G.
Arm
e.G. Limits
Usable Fuel
Unusable
Fuel
Standard
Empty
Weight
Basic
Empty
Weight
Payload
Useful
Load
Maximum
Ramp
Weight
Maximum
Take-off
Weight
The arm obtained by adding
the air-
plane's individual
moments and
dividing the sum by
the total weight.
The extreme center of gravity loca-
tions
within which the airplane must
be operated at a given weight.
Fuel available for flight planning.
Fuel remaining
after a runout test
has been completed in accordance
with governmental regulations.
Weight of a standard airplane
including unusable fuel,
full
operating fluids and full oil.
Standard
empty weight plus
optional equipment.
Weight of occupants, cargo and
baggage.
Difference
between ramp weight
and basic empty weight.
Maximum weight approved for ground
maneuvering. (It includes
weight of
start, taxi, and run up fuel).
Maximum weight approved for the
start of the take off run.
September, 1979
1-19