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    • Source: 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.


      Operators


      Lithuania
      Lithuanian Air Force


      Specifications



      Data from Les Ailes, November 1925General characteristics
      Crew: One
      Length: 5.75 m (18 ft 10 in)
      Wingspan: 10 m (32 ft 10 in)
      Height: 1.95 m (6 ft 5 in)
      Wing area: 11.40 m2 (122.7 sq ft)
      Empty weight: 190 kg (419 lb) equipped
      Gross weight: 300 kg (661 lb)
      Fuel capacity: 35 kg (77 lb) fuel and oil
      Powerplant: 1 × Anzani 3-cylinder radial, 30 kW (40 hp)
      Propellers: 2-bladed Dorand, 1.90 m (6 ft 3 in) diameter
      Performance

      Maximum speed: 142 km/h (88 mph, 77 kn) at ground level
      Endurance: 4 hr
      Service ceiling: 4,200 m (13,800 ft)
      Time to altitude: 7 min to 1,000 m (3,300 ft)
      Take-off distance: 30 m (98 ft)
      Landing distance: 40 m (130 ft)


      References




      Further reading


      Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.

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