The Blériot-SPAD S.33 was a small French airliner developed soon after the First World War. The aircraft was a biplane of conventional configuration whose design owed much to the Blériot company's contemporary fighter designs such as the S.20. Four passengers could be accommodated in an enclosed cabin within the monocoque fuselage, and a fifth passenger could ride in the open cockpit beside the pilot. A great success, it dominated its field throughout the 1920s, first on the CMA Paris to London route and later on continental routes served by Franco-Roumaine. One example was converted by CIDNA into a blind-flying trainer with a set of controls inside the blacked-out passenger cabin. A 190 kW Salmson CM.9 radial engine powered the 41 aircraft built.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.33 (Wikipedia)
Of Make
Source Blériot-SPAD S.33 (Wikipedia)
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Manufactured By
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Source Blériot-SPAD S.33 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
whose design owed much to the Blériot company
Originated In
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Source Blériot-SPAD S.33 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.33 was a small French airliner developed soon after World War I.
Sources
1. Wikipedia: Bleriot
Aircraft, Blériot-SPAD aircraftQuote, Aircraft, Blériot-SPAD aircraft
a five-seat development, the S.33 was produced, first flying at the end of 1920
View the Source 2. Blériot-SPAD S.33 (Wikipedia)
Specifications
Empty weight: 1,050 kg (2,315 lb)
Specifications, maximum mass
Gross weight: 1,797 kg (3,962 lb)
Specifications, top speed
Maximum speed: 180 km/h (110 mph, 97 kn)
Specifications, powerplant
Salmson CM.9 9-cylinder air-cooled radial piston engine, 190 kW (260 hp)
Variants
41 aircraft built.
Lead
The Bleriot-SPAD S.33 was a small French airliner developed soon after World War I.
Lead, manufacturer
whose design owed much to the Blériot company
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