Guillemin JG.10
Blériot Aéronautique · France · first flew 1931 · light aircraft
The Guillemin JG.10, also called the Blériot-Guillemin JG.10, was a French two-seat touring aircraft. It was designed to be as simple and safe to fly and maintain as a car.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Low-wing monoplane with a wingspan of 13 m on a fuselage only 7.1 m long |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Low-wing monoplane with a wingspan of 13 m on a fuselage only 7.1 m long
- Single Renault 4Pb inline engine in the nose, driving a tractor propeller
- Two-seat touring layout with provision for parachutes
A small low-wing single-engined two-seater with a long 13 m wing, a slim 7.1 m fuselage and an inline engine in the nose.
Specifications
- The Guillemin JG.10 has a length of 7.1 m (23 ft).
- It has a wingspan of 13 m (43 ft).
- Its maximum speed is 160 km/h (99 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
J. Guillemin designed the aircraft for Blériot Aéronautique, and it first flew on 1 June 1931. Only one was built.
Variants
There were no variants: only one JG.10 was built.
Where you'll see it
The single aircraft was powered by a 95 hp Renault 4Pb air-cooled four-cylinder inline engine. It had a top speed of 160 km/h and a range of about 500 km.
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