BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
Page 13 of 52
SECTION 2
WEIGHT AND BALANCE.
2.1 General
In order to achieve the performance, safety and optimal flying characteristics, which are designed,
into the aircraft, it must be flown with the weight and centre of gravity (C.G.) position within the
approved operating range (envelope). The pilot must ensure that the aircraft is loaded within the
loading envelope before takeoff. A weight and balance calculation can be helpful in determining
how much fuel or baggage can be boarded so as to keep within the allowable limits. Check
calculations prior to adding fuel to ensure against over loading.
2.2 Airplane weighing procedure
At the time of delivery, CLASS Inc. provides each airplane with the basic empty weight and centre
of gravity location. This data is supplied on Form WB-1
WARNING!
Misloading carries serious safety consequences for any aircraft. If the C.G. is too far forward, it
may be difficult to rotate for takeoff or landing. If the C.G. is too far aft, the aircraft may rotate
prematurely on takeoff or tend to pitch up during climb. Longitudinal stability will be reduced.
This can lead to inadvertent stalls and even spins; and spin recovery becomes more difficult as
the center of gravity moves aft of the approved limit.
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