Blériot-SPAD S.510

Airplanes

Length

7.46 m

Flat Wing Span

8.84 m

Height

3.72 m

Flat Wing Area

22 m²

Max Speed

370 km/h

Max Ceiling

10100 m

Number of Engines

First Flight

1933-01-06

Entry Into service

1936-01-01

Number Built

Maximum Take-Off Weight

1.83 t (paragliders: kg)

Maximum Range

875 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Blériot-SPAD S.510	1.83	875

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
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Albatros L 82	Siemens-Halske Sh 14	7.41	9	Compare

All data (20 fields)

Name: Blériot-SPAD S.510
Manufacturer: Blériot Aéronautique
Description: The Blériot SPAD S.510 was a French single-seat, single-engined biplane fighter aircraft.
First Flight: 1933-01-06
Entry Into service: 1936-01-01
Designer: André Herbemont
Type: Fighter
Length (m): 7.46
Height (m): 3.72
Cockpit Crew: 1
Max Speed (km/h): 370
Max Ceiling (m): 10100
Armament: 4 × 7.5 mm MAC 1934 machine guns
Number Built: 61
Powerplant Description: 1 × Hispano-Suiza 12Xbrs V-12 liquid-cooled piston engine, 515 kW (690 hp) each
Primary Users: French Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Bl%C3%A9riot-SPAD_S.510
Flat Wing Span (m): 8.84
Flat Wing Area (m²): 22
Number of Engines: 1