The Blériot-SPAD S.34 was a French twin-seat, single-engine biplane flight training aircraft designed in 1920. Its side-by-side seating arrangement was unique for its time. 150 aircraft were built, 125 of them for the French Air Force, which used them until 1936, and the Finnish Air Force bought two in 1921 but withdrew them by 1925 because of inadequate maintenance. A bis variant with a 130 hp Clerget 9B rotary engine was built in three examples for the Aéronavale. The specification lists a crew of one instructor and one pupil, a length of 6.50 m, an empty weight of 440 kg, a gross weight of 690 kg and a maximum speed of 136 km/h.
Facts
Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.34 (Wikipedia)
Of Make
Source Blériot-SPAD S.34 (Wikipedia)
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Manufactured By
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Source Blériot-SPAD S.34 (Wikipedia)LeadQuote, Lead
The Blériot-SPAD S.34 was a French twin-seat, single-engine biplane flight training aircraft designed in 1920.
Originated In
Also in Geography Atlas: where this subject originated.
Source Blériot-SPAD S.34 (Wikipedia)LeadQuote, Lead
The Blériot-SPAD S.34 was a French twin-seat, single-engine biplane flight training aircraft designed in 1920.
Sources
1. Blériot-SPAD S.34 (Wikipedia)
Lead
The Blériot-SPAD S.34 was a French twin-seat, single-engine biplane flight training aircraft designed in 1920.
Specifications
Empty weight: 440 kg (970 lb)
Specifications, maximum mass
Gross weight: 690 kg (1,521 lb)
Specifications, top speed
Maximum speed: 136 km/h (85 mph, 73 kn)
Specifications, powerplant
Le Rhône 9C 9-cylinder rotary engine, 60 kW (80 hp)
Lead, units built
150 aircraft were built, 125 for the French Air Force
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