Blériot-SPAD S.31

SPAD S.31
Role	Racer aircraft
National origin	France
Manufacturer	SPAD
First flight	1920
Number built	1

Last updated February 05, 2019

The Bleriot-SPAD S.30 was a French racer aircraft built in the early 1920s.

Design

The S.31 was a biplane with a monocoque fuselage of wood and canvas construction, as well as floats. It was built to participate in the 1920 Schneider Cup.

Specifications

Data from^[1]

General characteristics

Crew: 1
Length: 8.20 m (26 ft 11 in)
Wingspan: 10.43 m (34 ft 3 in)
Height: 3.42 m (11 ft 3 in)
Wing area: 31.45 m² (338.5 sq ft)
Empty weight: 1,075 kg (2,370 lb)
Gross weight: 1,510 kg (3,329 lb)
Powerplant: 1 × Hispano-Suiza inline engine, 250 kW (340 hp)
Propellers: 2-bladed fixed pitchpropeller

Performance

Maximum speed: 210 km/h (130 mph; 113 kn)

References

↑ "SPAD S-31 - Hydravion de course - Un siècle d'aviation française". Aviafrance.com. 1997-05-05. Retrieved 2019-02-04.

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[1] "SPAD S-31 - Hydravion de course - Un siècle d'aviation française". Aviafrance.com. 1997-05-05. Retrieved 2019-02-04.

v t e SPAD and Blériot-SPAD aircraft
SPAD aircraft	S.A-1, 2, 3 & 4 S.C S.D S.E S.F S.G S.H S.V S.VII S.XI S.XII S.XIII S.XIV S.XV S.XVI S.XVII S.XX
Blériot-SPAD aircraft	S.20 S.26 S.27 S.29 S.30 S.33 S.34 S.41 S.42 S.45 S.46 S.48 S.50 S.51 S.54 S.56 S.58 S.61 S.66 S.70 S.81 S.86 S.91 S.116 S.126 S.510 S.710

Blériot-SPAD S.31

Contents

Design

Specifications

See also

References