The D 27 was evolved to meet the requirements of the STAe 1926 C1 leger programme for lightweight fighters.
Incorporating a split-axle (with independently articulated wheels) rather than cross-axle undercarriage, the D 27 was powered by the SLM Saurer built 500hp Hispano-Suiza 12Mb (HS 57) 12-cylinder Vee engine and had an armament of two synchronised 7.7mm guns. The fuel was carried in a tank which formed the underside of the centre fuselage. In emergency this tank could be jettisoned.

The liquidation of the Construction Aeronautique E Dewoitine in January 1927 resulted in the transfer of development of the D 27 to the EKW in Switzerland, where a prototype flew on 3 June 1928.

By the end of 1929, three had been ordered by Romania, one by Argentina and three by Yugoslavia (of which two were to be assembled by Zmaj at Zemun), and the prototype was undergoing evaluation by the Swiss Fliegertruppe in competition with Alfred Comte’s AC-1.

The five prototypes and two of a strengthened model, the D 53, were flown experimentally for a time on board the aircraft carrier Bearn.
In the autumn of 1928, the EKW initiated a pre-series of 12 D 27 fighters, these adopting a redesigned tail and a revised wing of 0.45sq.m less area, modifications first tested in the Laboratoire Eiffel wind tunnel. Meanwhile, in March 1928, Emile Dewoitine had reestablished himself in France, forming the Societe Aeronautique Francaise-Avions Dewoitine.

The second and third pre-series D 27s were delivered to France in April 1929, the former being re-engined with the 400hp HS 12Jb as the D 272 F-AJTE for Marcel Dorset for aerobatic demonstrations. After 267 flight hours it was accidently destroyed in 1936.

The latter undergoing STAe evaluation at Villacoublay from 28 May equipped with two 7.7mm Darne guns. On 29 November 1929, a contract was issued by France’s DGT (Direction Generale Technique) of the Ministere de l’Air for the second and third pre-series aircraft plus three (later increased to four) additional fighters to be assembled by Liore-et-Olivier.

The D 27 was offered to the Forces Aeriennes Terrestres as the D 271 with the 500hp HS 12Hb engine and as the D 273 with a Gnome-Rhone Jupiter VII with a compressor enabling 425hp to be delivered at 4000m, but neither model was adopted.

At the end of 1929, however, the decision was taken in principle to re-equip the fighter element of the Swiss Fliegertruppe with the D 27, a pre-series of five being ordered from the EKW as D 27 IIIs, with deliveries commencing in 1931. A pre-production batch of 15 followed, additional contracts being placed for 45 D 27 IIIs to bring deliveries to the Fliegertruppe to 66 (including the prototype). Sixty six were delivered from 1930 to the Swiss Fliegertruppe, which also received 11 examples of the D 26, a version fitted with a 250 hp Wright Cyclone radial engine. Fifty six of the Swiss D 27s were still in first line fighter squadron service when war broke out in 1939. During the following year, they were withdrawn to training units, from which they did not disappear completely for another decade.

On November 30, 1930, Dewoitine chief test pilot Doret broke the world 1000 km (621 mile) closed circuit speed record flying a Dewoitine D 27 at an average of 286.227 km/h (177.854 mph).

Swiss D 27 III
Take-off weight: 1415 kg / 3120 lb
Empty weight: 1038 kg / 2288 lb
Wingspan: 10.30 m / 33 ft 10 in
Length: 6.56 m / 21 ft 6 in
Height: 2.78 m / 9 ft 1 in
Wing area: 17.55 sq.m / 188.91 sq ft
Max. speed: 298 km/h / 185 mph
Range: 425 km / 264 miles
Armament: 2 x 7.5 mm (0.295 in) machine guns
Service ceiling: 8300 m / 27231 ft
Climb to service ceiling: 11 minutes

The Dewoitine D 27 was designed in Switzerland and built there by the EKW state aircraft factory at Thun. It first flew in 1929, with an SLM Saurer built Hispano Suiza 12 Mc engine of 600 hp, and a total of 85 were built at Thun between 1929 33. Sixty six of these were delivered from 1930 to the Swiss Fliegertruppe, which also received 11 examples of the D 26, a version fitted with a 250 hp Wright Cyclone radial engine.

Dewoitine D.26 Article

Most of the D 26s were used as advanced trainers, but after World War II a number survived doing duty as tugs for sailplanes.

The D 25 tandem two-seat day and night fighter was developed in response to the 1925 C2 (two-seat fighter) programme. Based on the single-seat D 21, but with local reinforcement of the aft fuselage to permit installation of an open turret for a gunner. The D 25 was powered by a 450hp Lorraine-Dietrich 12Eb water-cooled W-type engine, the D 25 entered flight test in 1926, but the C2 programme for which it was intended was abandoned and the type was offered for export.
Four were ordered by Argentina in 1928, and these, fitted with an armament of two 7.9mm synchronised Madsen guns and two similar weapons on a ring mount in the rear cockpit, were built under subcontract by the Hanriot company (which also built the last 10 D 21 single-seaters for Turkey).

Engine: 450hp Lorraine-Dietrich 12Eb
Take-off weight: 1750 kg / 3858 lb
Empty weight: 1182 kg / 2606 lb
Wingspan: 12.80 m / 41 ft 12 in
Length: 7.64 m / 25 ft 1 in
Height: 3.00 m / 9 ft 10 in
Wing area: 24.80 sq.m / 266.94 sq ft
Max. speed: 222 km/h / 138 mph

At the end of 1925, the second prototype D 12 single-seat fighter was re-engined with a 500hp Hispano- Suiza 12Gb (HS 50) 12-cylinder W-type water-cooled engine and redesignated D 21. The D 21 had the four 7.5 mm (0.295 in) Darne machine¬guns.
Intended for export, the D 21 was first demonstrated in January 1926 at Bruxelles-Evere, the first export order from Turkey, for two D 21s for evaluation. Czechoslovakia ordered three and Argentina 18, plus the prototype. Of these, the three Czech aircraft and seven of the Argentine aircraft were assembled by the EKW in Switzerland.

A manufacturing licence was obtained by Czechoslovakia, Skoda building 26 D 21s during 1928-29 (as Skoda D 1s) with Skoda L engines (derived from the HS 12G) of 562hp. Out dated by the late 20s, they were discharged by the Czechoslovak Army and used by the Police Air Patrol.

Argentina also procured a manufacturing licence and the Fabrica Militar de Aviones (FMA) built 58 examples during 1930-31, but with Madsen machine guns and the licence-built Lorraine-Dietrich 12Eb W-type engine. They became effectively D 12s, although the designation D 21 was retained.

One French built D 21 was sold to Switzerland, where in late 1926 Emile Dewoitine had taken up residence, his French company having been bankrupted by the lack of domestic orders for any type since the D 1, and where, in 1928, there appeared the final development of the D 1 formula, the D 27.

In the autumn of 1927, Turkey placed a follow-on order for 10 D 21s, these being delivered during 1928-29.

Max take-off weight: 1580 kg / 3483 lb
Empty weight: 1090 kg / 2403 lb
Wingspan: 12.80 m / 42 ft 0 in
Length: 7.93 m / 26 ft 0 in
Height: 3.00 m / 9 ft 10 in
Wing area: 24.80 sq.m / 266.94 sq ft
Max. speed: 267 km/h / 166 mph

Skoda D-1
Engine: Skoda L, 500 hp
Span 12.24 m
Length 7.64 m
Top speed 270 kph
Rate of climb: 10m/s
Service ceiling: 9000 m
Endurance: 1hr 30min
Armament: two synchronized machine guns

First flown in 1924, the Dewoitine D 9 was essentially a scaled¬ down development of the earlier D 1 single ¬seat parasol monoplane fighter, from which it differed mainly in being powered by a 420 hp Gnome Rhone 9 Ac radial engine, a licence-¬built version of the 9 cylinder Bristol Jupiter.
Developed for participation in the 1923 C1 programme, two prototypes were completed. The Aviation Militaire purchased one for evaluation, but despite the extra available power the performance was not significantly improved, the D 9 took only 9 seconds less than the D 1 to reach 5000 m (16404 ft), and no French production contracts resulted.
Early in the flight test programme, the standard D 1 wing was replaced with a new wing of 2.5 sq.m greater area. A six-month delay in the commencement of evaluation of the contenders in the C1 programme provided Dewoitine with the opportunity to increase wing area by yet a further 2.5sq.m.
Armament consisted of two fuselage-mounted 7.7mm Vickers guns and two Darne model 19 guns of 7.5mm calibre mounted on the wing centre section outside the area of the propeller disc.
The D 9, placed sixth among the contenders, was destroyed on 15 October 1925.
Apart from the prototypes, only 13 were manufactured by Dewoitine, two for Belgium in 1925, Switzerland acquired the sec¬ond prototype and assembled three others in 1928 from French built components, and Yugoslavia (eight). The components of three were delivered in 1927 to the EKW (Eidg. Konstruktions-Werkstatte) in Switzerland for assembly, with delivery to the Fliegertruppe in 1928.
The largest production was undertaken by Ansaldo in Italy, which built 147 for the Regia Aeronautica with the designation AC 3.

Max take-off weight: 1333 kg / 2939 lb
Empty weight: 945 kg / 2083 lb
Wingspan: 12.80 m / 41 ft 12 in
Length: 7.30 m / 23 ft 11 in
Height: 2.93 m / 9 ft 7 in
Wing area: 25.00 sq.m / 269.10 sq ft
Max. speed: 244 km/h / 152 mph
Range: 400 km / 249 miles