The Latécoère 24 was a French

France

The French Republic , The French Republic , The French Republic , (commonly known as France , is a unitary semi-presidential republic in Western Europe with several overseas territories and islands located on other continents and in the Indian, Pacific, and Atlantic oceans. Metropolitan France...

 three-engined parasol wing

Parasol wing

A parasol wing monoplane is an aircraft design in which the wing is not mounted directly to the fuselage, but rather, the fuselage is supported beneath it by a set of struts, called cabane struts...

ed flying boat

Flying boat

A flying boat is a fixed-winged seaplane with a hull, allowing it to land on water. It differs from a float plane as it uses a purpose-designed fuselage which can float, granting the aircraft buoyancy. Flying boats may be stabilized by under-wing floats or by wing-like projections from the fuselage...

, built in 1927 to test the longer stretches of the South Atlantic crossing. Trials showed that it was overweight and consequently performed below specification.

Design and development

In 1926, Latécoère were considering ways of crossing the South Alantic in steps. One obvious route from France's colonial possessions in West Africa and the Brazilian mainland involved a 1,400 mi ( 2,250 km) flight due south, from the Cape Verde Islands to Fernando de Noronha

Fernando de Noronha

Fernando de Noronha is an archipelago of 21 islands and islets in the Atlantic Ocean, offshore from the Brazilian coast. The main island has an area of and had a population of 3,012 in the year 2010...

, as its greatest step. The aircraft they designed to do this was a three-engined parasol winged flying boat, the Latécoère 24. It was designed to carry mail, not passengers.

With its parasol wing high above the hull, the three engines which were mounted in the upper surface were well clear of spray. Two of the three 500 hp (373 kW) Farman 12 Wd W-12 water-cooled inline engines were mounted as close to the centre line as propeller clearance would allow, in tractor configuration; the third was mounted on the centre line as a pusher. This arrangement minimised the asymmetric forces resulting from the loss of any one engine. Each drove a four-bladed propeller. The wing itself was rectangular in plan, square tipped and with a low aspect ratio of about 5.8. It was a steel structure, fabric covered. The ailerons filled most of the trailing edge and carried compensators. The major structural connections between wing and hull were via the sponsons; one pair of wide streamlined struts leaned outwards from the sponson tips to mid-span on each side, and another pair went almost vertically upwards from the same point. Struts direct from wing to fuselage strengthened the centre section, supported the engines and transferred their loads.

Seen side on, the Latécoère 24's fuselage was slender and elegant, yet from below it was broad beamed to match the stubby wings. At the widest point its beam was 3.5 m and its height 1.70 m (11 ft 6 in x 5 ft 7 in). It was built of spruce and ash. The trapesoidal sponsons were largely wooden, with metal longerons. There was a mooring position in the nose with a post room aft, followed by positions for navigator and radio operator. The pilot sat in an open cockpit to starboard. Behind him were fuel tanks within firewalls, followed by mail compartments. The planing bottom had two steps, the first at the trailing edge of the sponsons and the second well aft. The tail unit had a wide chord rounded fin that carried a nearly semi-circular rudder and a tailplane at mid height to keep it clear of the water. The tailplane incidence was adjustable on the ground; the elevators had leading edge compensators like those fitted to the ailerons.

The Latécoère 24 flew for the first time from Saint-Laurent-de-la-Salanque

Saint-Laurent-de-la-Salanque

Saint-Laurent-de-la-Salanque is a commune in the Pyrénées-Orientales department in southern France.-References:*...

 at the end of 1927, crewed by pilot Prévot and engineer Hoff. Official trials followed and the results were not encouraging. Much of the criticism was aimed at the fuselage, chiefly its hydrodynamics and its weight. Overall, the aircraft was some 10% heavier than had been calculated in the contract, and as a result speed, range and altitude were below the expected values. There were also concerns about the reliability of the Farman engines. Consequently, Latécoère began to design a similar aircraft with a new and lighter hull and more reliable Renault engines, but this, the Latécoère 27, never got off the drawing board. Meanwhile the Latécoère 24 was seriously damaged at its moorings when a squall lifted it onto a jetty on the Salanque. No more were built.

Specifications

Cited sources