Latécoère 28: Француздық ұзақ қашықтыққа арналған ұшақтар тарихы

The Latécoère 28 was a long distance monoplane aircraft designed and produced by the French aircraft manufacturer Latécoère. First flown in 1927, it had a fixed tailwheel undercarriage and an enclosed cockpit for its crew of two. When configured for airline use, the Latécoère 28 could accommodate up to eight seated passengers. It was produced in both land and floatplane configurations, being marketed towards the civilian market both as a mail plane and passenger airliner. During its operating life, the Latécoère 28 became the main stay of Air France's predecessor, Aéropostale, which heavily used the aircraft during the 1930s in its efforts to establish intercontinental air mail services and support French colonialism and French cultural influence during the Interwar period. Its pilots included famous poets and French men of letters, such as Antoine de Saint Exupéry and Jean Mermoz, along with numerous veteran pilots from the First World War.

The Latécoère 28 was a development of the Latécoère 26. A total of about fifty aircraft of several versions were produced between 1927 and 1932. The seaplane version, the Latécoère 28 3, was the first to make a postal delivery crossing of the South Atlantic when Jean Mermoz flew from Dakar to Natal in 21 hours and a half aboard the Comte de La Vaulx (prototype n° 919) on 12 May 1930. Unfortunately, the plane was lost at sea during the return flight (with no loss of life, nor of mail). Early examples had been furnished with Renault 12Jbr engines; however, all use of this powerplant was quickly substituted for by Hispano Suiza 12, which waw capable of providing up to 500 hp (370 kW). The floatplane version was equipped with the Hispano Suiza 12Lbr, which could generate to up 650 hp (480 kW).

The Latécoère 28 was a long range high wing single engined monoplane. The fuselage, which was highly streamlined and largely supported by light metal tubing, was internally divided into three sections, each with its own distinct structure and function. The forwardmost section of the aircraft was the bow, the double tubular framework of which constitutes the engine bed in the form of a girder cradle. Two struts are used to deliver power to the propeller, while various accessories of the engine, including the radiator, fire extinguishers, control lines, fuel piping, and oil tank. Maintenance access to the engine was achieved via a removable aluminium hood. Directly behind the engine was two spaces, the pilot's room and the first baggage hold, the former being above the latter. The majority of the central section was divided from the pilot's room via two substantial bulkheads, between which were located the fuel tanks; these bulkheads were also the attachment points for both the wings and landing gear. Aft of the bulkhead was the passenger cabin, to the rear of which was the lavatory and a second baggage hold. Both the doors and windows had reinforced metal frames; a total of ten openable windows, along with washable fabric walls, a carpeted floor, ten baggage nets, and three ceiling
lights for night flying were present in the passenger cabin. The rear section comprised a relatively simple arrangement of four girders that supported the tail unit; these were braced with piano wires and enclosed in a light wood cowling. Reinforced box ribs gave the wing rigidity of the wing at key attachment points, such as with the fuselage and towards the ends of the ailerons; the wing was primarily attached to the fuselage via four bolts, two for each spar. Each of the ailerons, which had an all metal framework, were fitted with a light metal horn. The vertical empennage of the tail was outfitted with a triangular fin and a balanced semi circular rudder. The fin was supported at either end by a cross piece attached to the upper longerons of the fuselage and was braced via four wires running to the triangular horizontal stabilizer. The structure of the tail largely comprised light metal tubular members and stamped ribs, the majority of which was joined using rivets. The exterior was mainly covered by fabric. Both the rudder and the elevator were balanced. The aircraft's flight controls comprised a rudder bar, a wheel for the ailerons and a control stick for the elevator.

The first aircraft were used by Aéropostale on the African mail routes connecting Casablanca and Dakar. The aircraft also inaugurated a Paris Madrid service. The Latécoère 28 became famous in South America because of the regular mail service it performed between France and Argentina, amongst other destinations. This aircraft's introduction made it possible to send a letter from Paris to Santiago de Chile in what seemed then like an astonishingly short four days. Previously, the mail steamships had taken weeks or months. The Latécoère 28 was also operated in a military capacity. Venezuela purchased three aircraft for use as bombers while the French government supplied several to the Second Spanish Republic during the Spanish Civil War.

Laté 28.0
Initial production with a Renault 12Jbr engine, 17 built (some later converted to 28.1). Laté 28.1
Further production with a Hispano Suiza 12Hbxr engine, 29 built. Laté 28.2
Mail carrier, one built (n°948). Laté 28.3
Mail carrier floatplane, five built. Three entered service with Air France under the erroneous designation Latécoère 28.1/H
Laté 28.3/H
A wheeled landing gear version of the 28.3, one built. Laté 28.3 I
A passenger version of the 28.3, powered by a Gnome et Rhône 14Kb Mistral Major radial engine, one built. Laté 28.4 I
A development of the 28.3 with a Hispano Suiza 12Nbr engine, one built
Laté 28.5
Structurally strengthened version with a Hispano Suiza 12Nbr engine. Laté 28.6
For Venezuela powered by a Hispano Suiza 12Nbr engine, three built. Laté 28.8
One 28.0 modified with an enlarged wingspan
Laté 28.9
Three seat landplane bomber for Venezuela, three built.