| A-22
Aeroprakt A-22
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| Excellent design |
A-22 - ultralight aeroplane of "classic" light aeroplane layout. The design goal was to create an ultralight aeroplane with maximum level of comfort, pleasant appearance, pilot seats situated side-by-side (preferrable by many), steerable nose wheel (for easier ground handling), with good flight performance.
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| Comfortable cockpit |
Unlike the A-20 designed for flight performance in the first place, the A-22 was designed with the pilot comfort and pleasure in mind. So A-22 makes a good alternative to A-20 and customers are free to decide which they like best.
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| Excellent pilot view |
A-22 structure is almost completely all-metal (only engine cowling, wing fillets and wheel spats are made of composites) with fabric covering of wing and control surfaces. Extensive glazing of the cockpit provides excellent nearly all-round pilot view.
Detailed photos of A-22
Characteristics
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Max. level speed |
190 km/h |
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Stalling speed (flaps down) |
55 km/h |
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Max. range (90 fuel, still air) |
1100 km |
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Max. endurance (90 l fuel) |
12 h |
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Rate of climb (ISA, sea level) |
5 m/s |
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Engine: Rotax-912 |
80 h.p. |
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Takeoff/landing run (no wind) |
90 m |
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Wing span |
10,0 m |
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Length |
6.3 m |
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Height |
2,4 m |
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Wing area |
13,7 m2 |
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Max. TO weight |
450 kg |
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Empty weight |
260 kg |
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Loads |
+4 / -2 |
A-22 TOW
Engine: Rotax 912 ULS 100 P.S
Towing characteristics (glider - "Jantar std.3"):
Take-off distance - 210 m.
Average climb - 2,5 m/s
Towing characteristics (glider - L-13 "Blanik" with two pilots):
Take-off distance - 170 m.
Average climb - 1,8 m/s
AEROPRAKT Ltd.
Authorised distributor for the Baltic States - JSC "AEROTEKA"
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