Aeropro CZ - A240 - Pilot Operating Handbook and Flight Training Supplement
September 1, 2014
3-21
3. Weight and balance information
3.1 Installed equipment list:
VFR Day
airspeed indicator
X
altimeter / vertical speed indicator
X
slip indicator (in EFIS instrument)
X
EIS engine instrumentation
X
control light of EIS
X
fuel pressure indicator
X
magnetic compass
X
ELT
X
12v power socket
X
wingtip strobe/position lights
X
attitude indicator or EFIS
optional
radio / intercom
X
transponder-encoder
X
GPS or iPad mount
optional
3.2 Center of gravity (CG) range and determination
Aircraft handling and performances have been determined for this range of CG positions.
Front limit (in)
Rear limit (in)
Center of gravity limits
10.2
16.4
3.2.1 Weight and balance determination for flight
WARNING
To assure safe flying, the aircraft must not be operated in
violation of its approved weight and balance limitations.
Maximum take-off weight is the maximum weight approved for the start of the take-off roll.
The table given below represents the maximum amount of fuel for given crew weight and given weight in
the baggage compartment. The CG (center of gravity) position is within the approved range for all
combination in the table and any interpolation between displayed values.