Aeropro CZ - A220 taildragger - Pilot Operating Handbook and Flight Training Supplement
March 21, 2020
1. Airplane and systems description
The Aeropro A220 is an S-LSA aircraft designed as a high-wing monoplane. A two-spar wing is equipped
with external airfoil flaperons. Fuselage is an open truss structure welded of chromoly steel tubes. Tail
unit is formed of a lattice-work tube frame. The A220 is equipped with taildragger landing gear and
incorporates a steerable tail wheel.
Wing area including flaperons............................................... 122.53 sq. ft
Chord length (including flaperon)…………………………….. 4.265 ft
Wing loading …………………………………………………. . 10.1 lbs/sq. ft
Power loading....................................................................... 12.35 lbs/HP
Aspect-ratio........................................................................... 6.74:1
Propeller clearance (in-flight position)................................... 11.5 inches
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