The Blériot-SPAD S.540 was a trainer monoplane built by SPAD in the early 1930s. The specification lists a crew of two, a length of 7.08 m, a wingspan of 10.9 m, a height of 2.8 m, a wing area of 19 square metres, an empty weight of 630 kg, a gross weight of 862 kg and a maximum speed of 145 km/h from one 89 kW Salmson 9AC nine-cylinder air-cooled radial piston engine. The English Wikipedia article is a short stub that carries the specification table and a single descriptive sentence, and gives no account of the design, service or production of the aircraft.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.540 (Wikipedia)
Of Make
Source Blériot-SPAD S.540 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.540 (Wikipedia)LeadQuote, Lead
The Bleriot-SPAD S.540 was a trainer monoplane aircraft built by SPAD in the early 1930s.
Sources
1. Blériot-SPAD S.540 (Wikipedia)
Specifications
Empty weight: 630 kg (1,389 lb)
Specifications, maximum mass
Gross weight: 862 kg (1,900 lb)
Specifications, top speed
Maximum speed: 145 km/h (90 mph, 78 kn)
Specifications, powerplant
Salmson 9AC 9-cylinder air-cooled radial piston engine, 89 kW (120 hp)
Lead
The Bleriot-SPAD S.540 was a trainer monoplane aircraft built by SPAD in the early 1930s.
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