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Latécoère Late 8

late8

 

In 1922 the Late 8 prototype was flown. A six-passenger biplane with a single 300 hp / 224kW Renault 12Fe engine, the Late 8 transport was based on the Breguet 14, with a rear cockpit and of steel-tube fuselage construction.

It is believed that the Late 8 was used on Lignes Aeriennes Latecoere's France-Spain-Moroccan services.


Engine: 223kW Renault
Max take-off weight: 2270 kg / 5005 lb
Empty weight: 1500 kg / 3307 lb
Wingspan: 12.60 m / 41 ft 4 in
Length: 8.60 m / 28 ft 3 in
Height: 3.40 m / 11 ft 2 in
Wing area: 46.25 sq.m / 497.83 sq ft
Max. speed: 160 km/h / 99 mph
Cruise speed: 122 km/h / 76 mph
Ceiling: 3500 m / 11500 ft
Range: 500 km / 311 miles
Passengers: 6

 


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