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The Bernard SIMB AB 14 was a 1920s French single-seat sesquiplane fighter aircraft designed and built by the Société Industrielle des Métaux et du Bois (SIMB). With a reluctance of the French authorities to purchase monoplanes the Bernard 14 was designed as a sesquiplane with Y-form struts bracing the wings on each side. It was powered by a Hispano-Suiza 12Hb inline piston engine and had a fixed tailskid landing gear. While on a test flight on 22 February 1926 the aircraft suffered a catastrophic structural failure of the upper wing and the only Bernard 14 was destroyed.
The Nieuport-Delage NiD 120 series was a series of French single-seat parasol monoplane fighter aircraft of the 1930s. It was built in a number of versions, fitted with various types of engines, with six aircraft designated NiD 123 being sold to Peru.
The Bernard SIMB V.1 was a French single seat racing monoplane designed to compete for the 1924 Beaumont Cup. It crashed on its first flight and was not rebuilt.
The Bernard SIMB V.2 was a single-seat, single-engine French monoplane, built in the mid-1920s. It was originally designed for racing but was adapted for a successful attempt on the world absolute speed record.
The Bernard SIMB AB 12 was a French single engine, single-seat monoplane fighter aircraft built in the 1920s. Though advanced for its time, it failed to gain a production order and only one was built.
The Bernard 80 GR was one of three types built by different French constructors in response to a government call for an aircraft capable of setting new long-distance records. A single engine monoplane with a crew of two, the 80 GR set an absolute record for flight over a closed circuit in April 1931, covering 8,960 km (5,569 mi). Modifications led to a new designation as the Bernard 81 GR but no more records were set despite several attempts.
The Bernard H 110 was a single engine, single seat monoplane floatplane fighter designed for a French Navy competition. It flew in 1935 but had only made four test flights when the Bernard company was declared bankrupt, preventing further development.
The Bernard 260 C1 was a French all-metal, single-engine, low-wing monoplane with an open cockpit and fixed undercarriage, designed to a government single-seat fighter specification issued in 1930. After extensive comparative tests the Dewoitine D.500 was ordered in preference, though the performances of the two aircraft were similar.
The Bernard 160 was a three engine, multi-role monoplane designed in the early 1930s to meet a French government call for aircraft suited to policing and medical duties in its African colonies. Two prototypes were built and tested, but no further orders were placed.
The Nieuport-Delage NiD 37 was a single-engine, single-seat monoplane fighter aircraft and racer designed and built in France in the early 1920s. It had a small foreplane to bring the centre of pressure forward. Heavy, slower than expected and with turbo-supercharger problems, development ended without any entering service.
The Nieuport-Delage NiD 48 was a French single-engine parasol wing light fighter aircraft, designed and built in the 1920s. Its performance was not markedly better than that of the much heavier Nieuport-Delage NiD 62 then going into production, so only two were flown.
The Loire-Nieuport 161 was a single-seat, single-engine, all-metal, low-wing monoplane fighter designed and built in France in 1935 to compete for a government contract. Accidents delayed its development and only three prototypes were completed.
The Wibault Wib 210 C.1 was a single engine, single seat low wing monoplane fighter aircraft, designed and built in France in the late 1920s. Flight tests revealed vibration problems and development was quickly abandoned.
The Letov Š-7 was a single-seat, single-engine biplane fighter aircraft designed and built in Czechoslovakia in the early 1920s. It was designed for a single-seat fighter competition but did not reach production.
The Letov Š-13 was a single-seat, single-engine fighter aircraft designed and built in Czechoslovakia in the early 1920s. A biplane, it had aerodynamically thick wings which were originally cantilever structures, though interplane struts were later added. Only one was produced.
The Letov Š-14 was a single-seat, single-engine aircraft, designed and built in Czechoslovakia in the early 1920s. Originally intended as a biplane fighter, it was later modified into a monoplane and entered as a contestant in a speed competition.
The Letov Š-22 was a single-seat, single-engine aircraft designed and built in Czechoslovakia in the mid-1920s. A parasol-wing Dewoitine-style fighter, it was not successful, and only one was built.
The Hanriot HD.5 was a French two-seat fighter aircraft prototype, built towards the end of World War I. A single-engine biplane with an unusually narrow gap between the upper and lower wings, it did not enter production.
The de Marçay 4 was a single seat monoplane fighter built in France in 1923 for a government competition. It did not receive a production contract.
The unsuccessful French Farman F.200 of 1923 shared its type name with the 1929 Farman F.200, the progenitor of a series of parasol wing tourers. It was a two-seat touring aircraft, with a low, thick, cantilever wing. Only one was built and only briefly tested.