The Blériot-SPAD S.42 was a French biplane trainer aircraft of the early 1920s, developed by the Société pour l'aviation et ses dérivés (SPAD) from the prolific SPAD S.XIII fighter. Its operators were the French Aeronautical Service and the Imperial Iranian Air Force, which was reported in a British report of 1 July 1925 to have two operational aircraft, and only a few photographs of the type remain. The specification lists a crew of one, a length of 6.77 m, a wingspan of 8.65 m, a height of 2.65 m, an empty weight of 685 kg, a gross weight of 1,056 kg and a maximum speed of 175 km/h from one 130 kW Hispano-Suiza 8Ab water-cooled V-8 piston engine, with a range of 450 km.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Derived From
Source Blériot-SPAD S.42 (Wikipedia)
Exemplifies
Source Blériot-SPAD S.42 (Wikipedia)
Of Make
Source Blériot-SPAD S.42 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.42 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
developed by Société Pour L'Aviation et ses Dérivés (SPAD)
Originated In
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Source Blériot-SPAD S.42 (Wikipedia)LeadQuote, Lead
The SPAD S.42 was a French biplane trainer aircraft of the early 1920s
Sources
1. Blériot-SPAD S.42 (Wikipedia)
Specifications
Empty weight: 685 kg (1,510 lb)
Specifications, maximum mass
Gross weight: 1,056 kg (2,328 lb)
Specifications, top speed
Maximum speed: 175 km/h (109 mph, 94 kn)
Specifications, powerplant
Hispano-Suiza 8Ab V-8 water-cooled piston engine, 130 kW (180 hp)
Lead
The SPAD S.42 was a French biplane trainer aircraft of the early 1920s
Lead, manufacturer
developed by Société Pour L'Aviation et ses Dérivés (SPAD)
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