This new aircraft was a parasol wing monoplane of conventional configuration with an enclosed cabin for four passengers and an open cockpit for the pilot.

[1] The Latécoère 14's parasol wing was rectangular in plan and built around a pair of metal girder spars and with wooden ribs.

The cabin started aft of the cockpit, had three windows on each side and accommodated four passengers who entered by an oval port-side door.

[1] The Latécoère 14 had conventional, fixed landing gear with mainwheels on a streamlined single axle, fitted with rubber cord shock absorbers.

[1] There were also variants powered by 280 kW (380 hp) Gnome-Rhône 9A engines, a nine-cylinder radial, housed under an ovoid cowling with its cylinder heads projecting for cooling.

[1] Lignes Aériennes Latécoère, operating as Compagnie générale d'entreprises aéronautiques (CGEA) flew at least fifteen[4] of these aircraft and used several of them on its routes between France and Morocco.