AEROPRAKT A22LS, Pilot Operating Handbook

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AEROPRAKT-22LS Pilot Operating Handbook A22LS-POH-04
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C.G. position for the maximum take-off weight:
Item
Weight,
lbs.
×
CG arm,
inch
=
Moment,
lbs×inch
Empty airplane
727 × 60.6 = 44056.2
Crew (2×170 lbs.)
340 × 63.0 = 21420
Baggage
66 × 90.6 = 5979.6
Fuel (2×57 l)
180 × 78.7 = 14166
Total: 1313 85621.8
X
CG
= Total moment / Total weight = 65.21
Note : X
CG
must be between 59 inch and 69 inch (19% and 37% MAC) as shown in Fig. 2 .
7.2 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