NOTE: The original aircraft weight and balance from the factory is
determined with the equipment installed as ordered by the customer. Refer
to the “Installed Equipment List” (AM905.0) for the current conguration
of the aircraft. For each ight, the aircraft weight and balance must be
calculated using the number of seats and seat locations, as installed for
that particular ight. Refer to the “Passenger and Crew Seat Weight and
Balance” section for determining the passenger seat center of gravity (arm)
in calculating the aircraft weight and balance.
8. Takeoff Weight and Moment – To determine the takeoff condition weight
and moment/1000: subtract the weight and moment/1000 for the fuel used
for start, taxi and run-up, from the ramp condition values.
• The total weight at takeoff must not exceed the maximum takeoff weight
of 6,750 pounds, unless aircraft is certied for increased gross weight
up to 7,255 pounds.
• The total moment/1000 must not exceed the C.G. limits established in
the Moment Limits chart.
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