Fightersfighter biplane
S.510
The Blériot SPAD S.510 was a French single-seat, single-engined biplane fighter aircraft. First flying in 1933, 60 were built for the Armée de l'Air (French Air Force), entering service in 1936. The type remained in service as a fighter-trainer at the start of the Second World War. It was the last French biplane fighter to enter production.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Société Pour L'Aviation et ses Dérivés
- Category
- Fighters
- First flight
- 1933-01-06
Specifications
- Cruise speed
- 175 kt
- Max speed
- 200 kt
- Range
- 472 nm
- Service ceiling
- 33,100 ft
- Rate of climb
- 15 ft/min
- Max takeoff weight
- 4,034 lb
- Empty weight
- 2,756 lb
- Powerplant
- Hispano-Suiza 12Xbrs
- Engines
- 1
- Seats
- 1
- Length
- 24.5 ft
- Wingspan
- 29 ft
- Height
- 12.2 ft
- Number built
- 61
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.