AEROPRAKT-22LS Pilot Operating Handbook
A22LS-POH-04
24
7
Weight and Balance and Equipment List
This section contains information about weight and balance requirements for the safe
operation of the airplane. It is responsibility of the pilot in command to ensure before every
flight that weight and balance of the airplane remains within the specified limits. Failure to
do so may cause deterioration in airplane's flight performance and stability characteristics
and, as consequence, lead to unsafe operation.
7.1 Weight and Balance Chart
This subsection contains weighing and CG location data of the aircraft in configuration
“as
manufactured
”. Any permanent modification of the aircraft configuration (such as
replacement, removal/installation of any parts or/and equipment) essentially affecting those
data shall be accounted for in this weight and balance chart by appropriate revisions of this
subsection data.
Weight readings at: front wheel 159 lbs.
left wheel
285 lbs.
right wheel 283 lbs.
Total empty weight: ............................... 727 lb.
Total maximum take-off weight .................. 1323 lb.
Fig. 2
Empty C.G. position from the datum (engine flange):
