Caudron C.67
Caudron · France · first flew 1922 · light aircraft
The Caudron C.67 was a simple single-seat biplane with a low-powered engine, built and flown in France in 1922.
Recognition (WEFT)
| W — Wings | Mid-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 5.8 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Small single-seat biplane
- Low-powered three-cylinder Anzani engine in the nose
- Sport aircraft with a span of only 7.3 m
A very small biplane with a wingspan of 7.3 m and a three-cylinder engine at the nose.
Specifications
- The Caudron C.67 has a length of 5.8 m (19 ft).
- It has a wingspan of 7.3 m (24 ft).
- Its maximum speed is 95 km/h (59 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was designed by Paul Deville and first flew in April or May 1922. It was powered by a 25 hp Anzani three-cylinder engine.
Variants
There were no variants: only one was built.
Where you'll see it
Only one example was built, as a sport aircraft, and it did not go into production.
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