Blériot-SPAD S.36
SPAD · France · first flew 1923 · reconnaissance aircraft
The Blériot-SPAD S.36 was a French reconnaissance aircraft built in the early 1920s.
Recognition (WEFT)
| W — Wings | Mid-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 9.02 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Biplane with a single Hispano-Suiza 8F engine
- Two-seat reconnaissance layout
- Span of 11.46 m
A single-engined two-seat tractor biplane 9.02 m long with a wing area of 39 square metres.
Specifications
- The Blériot-SPAD S.36 has a length of 9.02 m (30 ft).
- It has a wingspan of 11.46 m (38 ft).
- Its maximum speed is 200 km/h (124 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It first flew on 17 January 1923.
Variants
Only one example of the type was built.
Where you'll see it
It was powered by a 300 hp Hispano-Suiza 8F V-8 engine and had a maximum speed of 200 km/h.
Related aircraft
- Blériot-SPAD S.40
- Blériot-SPAD S.54
- Blériot-SPAD S.25
- Blériot-SPAD S.32
- Aero A.26
- Armstrong Whitworth Wolf
- Astra-Șeșefschi
- CAMS 33
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