Breda A.4
| A.4 | |
|---|---|
| Role | Training biplane |
| Manufacturer | Breda |
| First flight | 1926 |
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The Breda A.4 was a biplane trainer produced in Italy in the mid-1920s. It was of conventional configuration with a two-bay unstaggered wing cellule and seating for the pilot and instructor in tandem open cockpits. Apart from civil use, the A.4 was also adopted by the Regia Aeronautica as a trainer. At least some examples were produced in floatplane configuration as the A.4 idro.
Variants
- Breda A.4 : Two-seat primary training biplane.
- Breda A.4 HS : Similar to the Breda A.4, but powered by a 134 kW (180 hp) Hispano-Suiza piston engine.
- Breda A.4 idro : Floatplane version.
Operators
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Specifications
General characteristics
- Crew: 2, pilot and instructor
- Length: 8.20 m (26 ft 11 in)
- Wingspan: 10.86 m (35 ft 7 in)
- Height: 3.10 m (10 ft 2 in)
- Wing area: 40.0 m2 (430 ft2)
- Empty weight: 800 kg (1,764 lb)
- Gross weight: 1,060 kg (2,337 lb)
- Powerplant: 1 × Colombo D.110 six-cylinder water-cooled in-line piston engine, 97 kW (130 hp)
Performance
- Maximum speed: 140 km/h (87 mph)
- Range: 450 km (280 miles)
- Service ceiling: 3,500 m (11,480 ft)
See also
- Related lists
References
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Wikimedia Commons has media related to Breda aircraft. |
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 195.
- Уголок неба
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