Blériot-SPAD S.34
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| S.34 | |
|---|---|
| Type | Trainer aircraft |
| Manufacturer | Blériot |
| Designed by | André Herbémont |
| Maiden flight | 16 July 1920 |
| Introduced | 1920 |
| Retired | 1936 |
| Primary users | French Air Force Finnish Air Force |
| Number built | 150 |
The Blériot-SPAD S.34 was a French twin-seat, single-engine biplane aircraft designed in 1920. The side-by-side seating arrangement was unique for its time. 150 aircraft were built, 125 for the French Air Force, who used them until 1936.
The Finnish Air Force purchased two S.34s in 1921. Due to inadequate maintenance they did not last long and were withdrawn from service by 1925.
[edit] Variants
- S.34
- S.34-bis - variant with Clerget rotary engine for Aéronavale
[edit] Operators
- France
-
- Aéronautique Militaire (119 aircraft)
-
- Aéronavale (6 S.34-bis aircraft)
-
- Blériot flying school (16 aircraft)
- Argentina (6 aircraft)
- Finland
-
- Finnish Air Force (2 aircraft)
- Bolivia (1 aircraft)
[edit] Specifications (S.34)
Data from Suomen Ilmavoimat I 1918-27
General characteristics
- Crew: 2
- Length: 6.5 m (21 ft 4 in)
- Wingspan: 8.2 m (26 ft 11 in)
- Height: 2.3 m (7 ft 7 in)
- Wing area: m² (ft²)
- Empty weight: kg (lb)
- Useful load: kg (kg)
- Max takeoff weight: 700 kg (1540 lb)
- Powerplant: 1× Le Rhone C, 60 kW (80 hp)
Performance
- Never exceed speed: km/h (knots, mph)
- Maximum speed: 130 km/h (70 knots, 81 mph)
- Cruise speed: km/h (knots, mph)
- Stall speed: km/h (knots, mph)
- Range: km (nm, mi)
- Service ceiling 4,000 m (13100 ft)
- Rate of climb: m/min ()
- Wing loading: kg/m² (lb/ft²)
- Power/mass: W/kg (hp/lb)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- Keskinen, Kalevi; Partonen, Kyösti and Stenman, Kari: Suomen Ilmavoimat I 1918-27, 2005. ISBN 952-99432-2-9.
- Keskinen, Kalevi; Stenman, Kari and Niska, Klaus: Suomen ilmavoimien lentokoneet 1918-1939, Tietoteos, 1976.
[edit] See also
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