Bernard SIMB AB 14
The Bernard SIMB AB 14 was a 1920s French single-seat sesquiplane fighter aircraft designed and built by the Société Industrielle des Métaux et du Bois (SIMB).[1][2] With a reluctance of the French authorities to purchase monoplanes the Bernard 14 was designed as a sesquiplane with Y-form struts bracing the wings on each side.[1] It was powered by a Hispano-Suiza 12Hb inline piston engine and had a fixed tailskid landing gear.[1] While on a test flight on 22 February 1926 the aircraft suffered a catastrophic structural failure of the upper wing and the only Bernard 14 was destroyed.[1]
Specifications
Data from [1]
General characteristics
- Crew: 1
- Length: 7.40 m (24 ft 3 in)
- Wingspan: 12.50 m (41 ft 0 in)
- Height: 3.10 m (10 ft 2 in)
- Wing area: 27 m2 (290 sq ft)
- Empty weight: 1,240 kg (2,734 lb)
- Max takeoff weight: 1,800 kg (3,968 lb)
- Powerplant: 1 × Hispano-Suiza 12Hb inline piston engine, 370 kW (500 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 230 km/h (143 mph; 124 kn)
Armament
- Guns: Two fixed 7.7mm (0.303in) synchronised machine-guns
References
- Notes
- Bibliography
- Liron, J.L. (1990). Les avions Bernard. Paris: Éditions Larivère.
External links
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