The Blériot-SPAD S.62 was a French one-seat, single-engine biplane flight training aircraft designed in the 1920s, and it was presented at the Military Airplane School Contest of 1923. The S.62 was a biplane of wood and canvas construction. The specification lists a crew of one, a length of 6.77 m, a wingspan of 8.65 m, a height of 2.80 m and a wing area of 23.70 square metres. Its empty weight was 717 kg and its gross weight 1,025 kg, and a single Hispano-Suiza 8Ab V-8 water-cooled piston engine of 130 kW gave it a maximum speed of 180 km/h.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
Source Blériot-SPAD S.62 (Wikipedia)
Of Make
Source Blériot-SPAD S.62 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.62 (Wikipedia)LeadQuote, Lead
The Blériot-SPAD S.62 was a French one-seat, single-engine biplane flight training aircraft designed in the 1920s.
Originated In
Also in Geography Atlas: where this subject originated.
Source Blériot-SPAD S.62 (Wikipedia)LeadQuote, Lead
The Blériot-SPAD S.62 was a French one-seat, single-engine biplane flight training aircraft designed in the 1920s.
Sources
1. Blériot-SPAD S.62 (Wikipedia)
Specifications
Empty weight: 717 kg (1,581 lb)
Specifications, maximum mass
Gross weight: 1,025 kg (2,260 lb)
Specifications, top speed
Maximum speed: 180 km/h (110 mph, 97 kn)
Specifications, powerplant
Hispano-Suiza 8Ab V-8 water-cooled piston engine, 130 kW (180 hp)
Lead
The Blériot-SPAD S.62 was a French one-seat, single-engine biplane flight training aircraft designed in the 1920s.
View the SourceReader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.
Sign in to dispute this or suggest a correction.