AEROPRAKT A32-214-POH, Руководство по эксплуатации для пилотов

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AEROPRAKT-32 Pilot Operating Handbook A32-214-POH
24
C.G. position for the maximum take-off weight:
Item Weight, lbs ×
CG arm,
inch
=
Moment,
lbs×inch
Empty airplane 771 × 65.68 = 50639
Crew (2×70.0 kg) 350 × 65.5 = 22925
Baggage 20 × 91.3 = 1826
Fuel (2×57 l) 180 × 77.2 = 13896
Total: 1321 89286
X
CG
= Total moment / Total weight = 67.59
Note : X
CG
must be between 60 inch and 70 inches. (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