AEROPRAKT A32, Pilot Operating Handbook

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AEROPRAKT-32 Pilot Operating Handbook A32-060-POH
23
C.G. position for the maximum take-off weight:
Item
Weight,
kg/lbs.
×
CG arm,
m/inch
=
Moment,
kg×m/lbs×inch
Empty airplane
724.2 × 62.4 = 45190
Crew (2× 79.5 kg) 350 × 65.5 = 22925
Baggage
45 × 91.3 = 4109
Fuel (2×57 l)
181.0 × 77.2 = 13973
Total: 1300.2 86197
X
CG
= Total moment / Total weight = 66.3
Note : X
CG
must be between 1.529 m and 1.780 m (19% and 37% MAC) as shown in
Fig. 2
.
6.2 Installed equipment list
This subsection contains a table with the list of the installed optional equipment affecting
weight and balance of the aircraft. It is responsibility of the aircraft owner/operator that any
such equipment installed in the aircraft after the date of its manufacture is listed in the
table below.
No. Equipment description and Part No. Weight, kg CG arm, m