The Blériot-SPAD S.54 was a French biplane trainer aircraft of the early 1920s, developed by the Société pour l'aviation et ses dérivés (SPAD). The specification lists a crew of one, a length of 7.24 m, a wingspan of 8.96 m, a height of 2.57 m, a wing area of 23.52 square metres, an empty weight of 520 kg, a gross weight of 757 kg and a maximum speed of 120 km/h from one 97 kW Clerget 9B nine-cylinder air-cooled rotary piston engine. The English Wikipedia article is a short stub that carries the specification table and no account of the aircraft's design, service or production.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.54 (Wikipedia)
Of Make
Source Blériot-SPAD S.54 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.54 (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.54 (Wikipedia)LeadQuote, Lead
The SPAD S.54 was a French biplane trainer aircraft of the early 1920s
Sources
1. Blériot-SPAD S.54 (Wikipedia)
Specifications
Empty weight: 520 kg (1,146 lb)
Specifications, maximum mass
Gross weight: 757 kg (1,669 lb)
Specifications, top speed
Maximum speed: 120 km/h (75 mph, 65 kn)
Specifications, powerplant
Clerget 9B 9-cylinder air-cooled rotary piston engine, 97 kW (130 hp)
Lead
The SPAD S.54 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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