ALPHA Electro
www.pipistrel-aircraft.com
REV. 0
POH-167-00-40-150
Center of gravity range
•
The aircraft's safe in-flight center of gravity position ranges between 20% and 35% of
mean aerodynamic chord.
•
The in-flight center of gravity point ranges between 8 ⁄'' (220 mm) and 14'' (355
mm) aft of the datum. The datum is the wing's leading edge at the fuselage root.
G-load factors
Max. positive wing load: + 4 G
Max. negative wing load: – 2 G
1-6
General
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