The D 19 appeared in the summer of 1925 with a 400hp Hispano-Suiza 12Jb 12-cylinder water-cooled Vee-type engine. By comparison with the D 1, the D 19 had longer span, narrower chord ailerons and a wing spanning 12.50m with an area of 24.00sq.m. Demonstrated in Switzerland in August 1925, three examples of a modified version of the D 19 were ordered by the Swiss government. Specified armament was two fuselage-mounted 7.7mm guns, the paired Lamblin radiators mounted on the undercarriage legs replaced by a Chausson frontal radiator and a wing similar to that of the D 1 was adopted.
A second D 19 prototype was completed with these modifications, this being sold in 1928 to Belgium, and the first Swiss aircraft was ferried to the EKW (Eidg. Konstruktions-Werkstatte) in March 1926. The two other Swiss aircraft were transported to Switzerland in February 1927 for assembly by the EKW state aircraft factory at Thun, subsequently entering service with the Fliegertruppe.

The D 19 received a new wing of 25.00 sq.m similar to that of the D 9 and D 12 before CEPA testing, in which performance proved mediocre owing to mismatching of the propeller.

The three D 19s participated in the 1927 Zurich-Diibendorf international aviation meeting, one being winner of the closed-circuit race for fighters with a speed of 250km/h. Used primarily for combat training by the Fliegertruppe, one D 19 was lost in 1930, and the remaining two continued in service until 1940.

D 19
Max take-off weight: 1390 kg / 3064 lb
Empty weight: 980 kg / 2161 lb
Wingspan: 10.80 m / 35 ft 5 in
Length: 7.87 m / 25 ft 10 in
Height: 3.50 m / 11 ft 6 in
Wing area: 20.00 sq.m / 215.28 sq ft
Max. speed: 268 km/h / 167 mph
Range: 400 km / 249 miles

Evolved in parallel with the D 9 as a contender in the 1923 C1 programme, the larger, sin¬gle seat parasol D 12 fighter was powered by a 450hp Lorraine- Dietrich 12EW 12-cylinder W-type water-cooled engine and armed with two 7.7mm Vickers guns.
With a basically similar fuselage to that of the D 1, the D 12 first flown in June 1924.
In September 1924, the D 12 was fitted with a higher compression 450 hp Lor¬raine 12 Eb and a pair of 7.5mm Darne model 19 guns on the wing centre section.
The paired Lamblin radiators on the undercarriage legs was replaced by a frontal radiator and a wing similar to that finally adopted on the D 9 was fitted. On 5 February 1926, the D 12 was written off in an accident at Cazaux. A second prototype had meanwhile entered flight test, having flown at the end of 1925, this having a W-type Hispano-Suiza 12Gb engine, but further development was discontinued.
It was eventually to take third place in the 1923 C1 programme after the Nieuport-Delage 42 and the Gourdou- Leseurre 32.

Max take-off weight: 1636 kg / 3607 lb
Empty weight: 1070 kg / 2359 lb
Wingspan: 12.80 m / 41 ft 12 in
Length: 7.60 m / 24 ft 11 in
Height: 3.00 m / 9 ft 10 in
Wing area: 25.00 sq.m / 269.10 sq ft
Max. speed: 239 km/h / 149 mph

In the autumn of 1922, Dewoitine submitted to the CEDANA (Commission d’Examen des Appareils Nouveaux pour l’Aeronautique) a high-altitude version of the D 1 (which had then still to fly) designated D 8. One category of fighter in the 1921 C1 programme called for a speed of 240km/h at 7000m and a practical ceiling of at least 8500m. After discarding the proposal to equip the D 8 with a Rateau turbo-compressor, Dewoitine adopted the higher compression Hispano-Suiza 8Fe engine of 360hp. A larger wing of wood rather than metal construction was introduced and the prototype was rolled out in the late summer of 1923.
At Francazal, the D 8 attained an altitude of 2000m in 4.25 min, 3000m in 6.83 min, 4000m in 10.5 min and 5000m in 15.1 min. For publicity purposes this performance was attributed to the D 1 fighter. The C1 requirement for a high-altitude fighter having been abandoned, and, in June 1924, the D 8 was modified for an attempt on the world air speed record, fitted with a lightened version of the D 1 wing. On 23 December 1924, the D 8 established 100-, 200- and 500-km closed-circuit records while being flown by Marcel Doret, and, on 12 December, set a 1000km closed-circuit record of 221,775km/h.

Max take-off weight: 1100 kg / 2425 lb
Empty weight: 780 kg / 1720 lb
Wingspan: 12.80 m / 41 ft 12 in
Length: 7.50 m / 24 ft 7 in
Height: 2.75 m / 9 ft 0 in
Wing area: 25.00 sq.m / 269.10 sq ft
Max. speed: 245 km/h / 152 mph

Designed by Emile Dewoitine to compete in the French C1 single ¬seat fighter competition of 1921, the prototype D 1 flew for the first time on November 18 1922.
A high-wing monoplane with fabric-covered metal wings and an oval-section metal fuselage covered by duralumin sheet. Armament was two 7.7mm synchronised Vickers guns and power was provided by a 300hp Hispano-Suiza 8Fb (HS 42) eight-cylinder water-cooled engine.
The principal criticism being the poor forward visibility. A 120mm pylon was therefore inserted between wing and fuselage, the fighter, now referred to as the D.1bis, becoming a parasol monoplane. This modification was completed in August 1923, by which time the first three (of 10) pre-series aircraft had been supplied for official evaluation in the initial configuration. Two of these were lost in accidents and the third was modified to D.1bis parasol form.
After prolonged evaluation of all the 1921 contenders, the Dewoitine D 1 and Spad 80 each received a contract in 1924 for 80 aircraft, the two types being intended to replace Spad XIIIs and XXs in Aviation Militaire squadrons. A further 29 D 1 s were ordered subsequently f or the Aeronavale.
Dewoitine’s chief test pilot, Marcel Doret, set speed records (with and without payload) of 233.10 km/h (144.84 mph) on December 23, 1924, and the D 1 could climb to 5000 m (16404 ft) in 15.1 minutes.

The next five pre-series. aircraft (the fourth, fifth and sixth having been ordered by Czechoslovakia, Japan and Italy respectively, and the seventh and eighth by Switzerland) were all completed to D 1bis standard, but continuing criticism of forward view led to replacement of the shallow pylon between wing and fuselage by a cabane of inverted-vee struts on the prototype which thus became the D 1ter. The two pre-series aircraft for Switzerland were modified to this standard prior to delivery, the two lost during official trials) were completed as D 1ter fighters, the cabane struts being standardised for production D 1s. A contract had been placed in November 1923 on behalf of the Aeronautique Navale for 44 D 1s, with the government providing guarantees for 150 aircraft.
The production contract was placed with the SECM (Societe d’Emboutissage et de Constructions Mecaniques) which flew its first series D 1 on 18 January 1925. The production aircraft required several successive structural reinforcements, and did not gain acceptance by the Aviation Militaire until 1929. The D 1 was of mixed construction, with an open cockpit and two 7.5 mm (0.295 in) machine guns in the engine upper decking. The final version, the D 1 ter, had a more conventional strut type centre section cabane.

Most Aviation Militaire D ls were soon transferred to the Aeronavale units, including 3C2, 4C1, 7C1 and 7C3; by mid 1931 these units had re equipped with the Nieuport-¬Delage 62. The Aeronautique Navale took delivery of its D 1s from early 1925, and in the previous year an order for 20 had been placed on behalf of the Forces Aeriennes Terrestres, although these were never to equip a service unit.
Dewoitine D ls were exported to Japan (one), Switzerland (two) and Yugo¬slavia (79), and a further 126 were built (with modifications) by Ansaldo at Turin for the Regia Aeronautica, with the designation AC 2.

Engine: 300hp Hispano-Suiza 8Fb (HS 42)
Max take-off weight: 1240 kg / 2734 lb
Empty weight: 820 kg / 1808 lb
Wingspan: 11.50 m / 37 ft 8.75 in
Length: 7.50 m / 24 ft 7 in
Height: 2.75 m / 9 ft 0 in
Wing area: 20.00 sq.m / 215.28 sq ft
Max. speed: 247 km/h / 153 mph
Range: 400 km / 249 miles
Armament: two 7.7 mm (0.30 in) Vickers machine gun