AEROPRAKT 22LS, Руководство по эксплуатации для пилотов

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AEROPRAKT-22LS Pilot Operating Handbook A22LS-POH-04
C.G. position for the maximum take-off weight:
Item
Weight,
lbs.
×
CG arm,
inch
=
Moment,
lbs×inch
Empty airplane 766 × 61.6 = 47186
Crew (2×80.0 kg) 352 × 63.0 = 22176
Baggage 22 × 90.6 = 1993
Fuel (2×57 l) 181 × 78.7 = 14245
Total: 1321 85600
X
CG
= Total moment / Total weight = 64.8
Note : X
CG
must be between 59.06 in. and 68.94 in. (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, k
g
CG arm, m
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