page_title: ANBO I
section_title: Specifications
hierarchical_section_title: ANBO I / Specifications
caption_attribution_description: English: Anbo I 3-view drawing from L'Air January 15, 1926
context_page_description: 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.
context_section_description: Data from Les Ailes, November 1925
  General 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)
caption: Anbo I 3-view drawing from L'Air January 15, 1926
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