/ ANBO I
The ANBO I was a single-seat aircraft developed in Lithuania, proposed as a trainer for the Army.
It was a low wing, braced monoplane of conventional tailwheel configuration.
The fuselage structure was of fabric-covered welded steel tube,
The wing had a wooden, two spar structure and was fabric covered but the fuselage, also fabric covered, had a welded steel tube structure.
The first flight took place in 1925.
Ten years later the aircraft was sold to Lithuanian Aviation Museum in Kaunas where it is exhibited today.
5.75 m (18 ft 10 in)
10 m (32 ft 10 in)
1.95 m (6 ft 5 in)
11.40 m2 (122.7 sq ft)
190 kg (419 lb) equipped
300 kg (661 lb)
35 kg (77 lb) fuel and oil
1 × Anzani 3 cylinder radial, 30 kW (40 hp)
2-bladed Dorand, 1.90 m (6 ft 3 in) diameter
142 km/h (88 mph, 77 kn) at ground level
4,200 m (13,800 ft)
Time to altitude
7 min to 1,000 m (3,300 ft)
30 m (98 ft)
40 m (130 ft)
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