AEROPRAKT-22LS Pilot Operating Handbook
A22LS-POH-04
22
X
CG
must be between 1.470 m [58 in] and 1.780 m [69.94 in] (19% and 37% MAC) as
shown in
Fig 2.
Item
Weight,
Kg/lbs.
×
CG arm,
m / inch
= Moment,
kg×m / lbs×inch
Empty weight
322.8/712 ×
1.488/59 =
480.2/41,676.1
Crew (2×85 kg)
180.0/397 ×
1.60/63 =
288.0/24,997.0
Baggage
15.0/33.1 ×
2.30/91 =
34.5/2,994.4
Full fuel (114 l)
82.1/181 ×
2.0/79 =
164.2/14,251.8
Total:
599.9/1,322.6
966.9/83,919.3
X
CG
= Total moment / Total weight =
1.612/63.5
m
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
1.
2.
3.
4.
5.
6.
