Wibault 368
# Wibault 368

The Wibault 368 was a single-engined aircraft built to contend for a French government prize for a long-range aircraft using a diesel engine in the late 1930s.

## Specifications (variant specified)

Data from L'avion de record Wibault 368: une filiation peu courante...

General characteristics

* Crew: 2
* Length: 11.876 m (39 ft 0 in)
* Wingspan: 17.102 m (56 ft 1 in)
* Height: 4.25 m (13 ft 11 in)
* Wing area: 37 $m^2$ (400 sq ft)
* Empty weight: 2,102 kg (4,634 lb)
* Max takeoff weight: 5,090 kg (11,222 lb)
* Fuel capacity: 2,960 litres (650 imp gal; 780 US gal)
* Powerplant: 1 × Clerget 14 F2 14-cylinder radial diesel engine, 370 kW (500 hp)
* Propellers: 2-bladed

Performance

* Maximum speed: 270 km/h (170 mph, 150 kn)
* Range: 10,000 km (6,200 mi, 5,400 nmi)
* Service ceiling: 5,000 m (16,000 ft)
