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Dewoitine D.520

Dewoitine D.520 of GC III/6 flown by Pierre Le Gloan attacking Fiat CR.42s of the Regia Aeronautica over Southern France, 15th June 1940. On this day, Le Gloan became the second pilot in WWII to down five aircraft in a single sortie, four CR.42s and a BR.20 bomber.

Country of Origin:

France

Manufacturer:

Dewoitine

Designer:

Robert Castello and Jacques Henrat

Major Variants:

D.520

Role:

Single-Seat Fighter, Fighter Trainer

Operated by:

France, Bulgaria, Germany, Italy.

First Flight:

2 October, 1938 by Marcel Doret at Toulouse-Francazal.

In Service:

First production machines to Armée de l'Air in January 1940 (to operational units in April)

Number Built:

Three prototypes plus 437 before Armistice. Further 478 built in Vichy France. Various other prototypes and projects (see Variants).

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Overview

The Dewoitine D.520 was the best fighter available to the Armée de l'Air (French Air Force) at the beginning of the German invasion of France in May 1940. In April 1940, in a comparison with a captured Messerschmitt Bf 109E-3, the D.520 was found to be inferior in terms of speed, but markedly superior in maneuverability.  D.520 pilots managed 108 confirmed kills, and 39 probables; this against 26 lost in air combat.  However, it appeared in insufficient numbers to stem the tide of the Luftwaffe.  French pilots had just received their D.520's and had less than one month to train in them in the earliest of units (some units had less than 3 days in the new aircraft before entering combat!). It's likely that after fully working up the D.520 with proper training the aircraft would have performed even better.  As opposing fighters improved, the production D.520's remained much in the same configuration as they appeared in 1940, and became progressively outclassed by their rivals as the war continued. The full potential of this excellent aircraft was never realized.

In 1927, due to a lack of orders, Emile Dewoitine moved his business to Switzerland and designed the D.27, a monoplane fighter adopted by the Swiss from 1931. In that same year, Dewoitine returned to France and reorganized his private venture as Societe Aeronautique Francaise and delivered limited numbers of a D.27 variant, the D.37, to the Armée de l'Air.  In 1932, Dewoitine began the design of what was to be first modern low-wing monoplane fighter in French service,: the D.500 series, based on the C1 requirement issued two years previously. In 1936, Dewoitine left SAF, and established an autonomous design bureau in June 1936 under the leadership of Robert Castello The new bureau's first task was to design a new C1 requirement (single-seat fighter) aircraft. The initial design was rejected by the Service Technique Aéronautique (Aeronautical Technical Service) of the Armée de l'Air as the projected top speed of 500 km/h was too low, who insisted that the minimum top speed should be 520 km/h. Dewoitine made some alterations to the design (now called the D.520 for the speed requirement), including a new type of Hispano-Suiza engine. By this time, the Service had chosen the Morane-Saulnier MS.406 as their new fighter, and rejected the D.520.

Dewoitine was confident that their D.520 was the better machine, and decided to carry on with the production of two prototypes at their own expense. Dewoitine's design office was absorbed by the Societe Nationale de Construction Aeronatiques du Midi (SNCAM), and he was named deputy managing director. On 3 April 1938, a government contract was awarded to Dewoitine, and the first prototype flew on 2 October at Toulouse-Francazal. After some modifications, the required top speed was achieved. During 1938, the French realized the poor state of their Air Force to wage modern warfare, and orders were placed for new machines. Two hundred D.520's were ordered by the government on 17 April 1939, less than two months after the second prototype made its first flight.

By the start of WWII (in 1939), only the three prototypes had flown, and the first production aircraft finally flew on 31 October of that year. Dewoitine made it into the order book again in June and September 1939, and also in January, April, and May 1940 with orders totaling 2,200 D.520's - 120 of them for the Aéronavale (French Naval Air Service).

A handful of D.520's were operational with Groupe de Chasse I/3 by the time of the German attack on France (10 May 1940). GC II/3, GC II/7, and GC III/3 were in the process of conversion to the D.520 from the MS.406 on the date of the attack. GC I/3 was hurriedly sent into battle, and as more D.520's became available from the Toulouse factory, they were rushed to frontline units as fast as possible. During the Battle of France, D.520's had accounted for 108 confirmed kills and 39 probables (versus 26 aircraft lost in air combat). Italy declared war against France on 10 June, and began offensive operations in metropolitan France on the night of 12-13 June with a bombing raid on the important French naval base at Toulon. It was in the defense of these raids that on 15 June, Adjudant Pierre le Gloan, flying a D.520 of GCIII/6, shot down four Fiat CR.42 fighters and one BR.20 bomber in a single sortie, taking his score to 11. By the time of the Armistice, 437 D.520's had been built in Toulouse, 351 going to the Armée de l'Air and 52 to the Aéronavale. Of these, 106 had been lost in combat or, mostly, in accidents.

After the Armistice, 153 D.520's were located in Vichy France, 175 had escaped to North Africa, and three crossed the English Channel. At this time, the Germans allowed Vichy France to maintain a reduced air force. However, no D.520 was to remain in service in mainland France, and all surviving D.520's in France were dispersed and stored. On October 16th 1940, the Germans reacted angrily when they learned that three D.520's of GCI/3 had landed in Gibraltar to join the dissidents.  They asked immediately for the group to be disbanded but its commander simply altered the name of the unit from GCI/3 to GCIII/3.  In April 1941, the German Armistice Commission approved the production for the Vichy Air Force of 550 D.520's from the SNCASE organization (SNCA du Sud-Est) who had taken over SNCAM's assets, and 349 of these were completed by November 1942.

Vichy French D.520's later saw action against France's former allies in the 1941 Syrian Campaign (Le Gloan accounting for six RAF Hurricanes and a Gladiator in his D.520), and during Operation Torch, the Allied landings in French North Africa in November 1942. The rapid declaration of the French African colonies for the Free French and Allied cause in the wake of Operation Torch carried consequences for mainland France: the Germans quickly swept into the "free zone" of unoccupied Vichy France, capturing 1,876 aircraft.  Among these were a quantity of airworthy D.520's as well as 169 still on the production lines. SNCASE was ordered by its new masters to continue production, and a further 129 D.520's were completed. Of the D.520's seized by the Germans, some were transferred to JG-103 and JG-105 (Luftwaffe training units). Sixty D.520s went to the Italian Regia Aeronautica, and were used as front-line fighters in defense against Allied bombers by Gruppi 8, 13, 22, 24, 59, 60, 161, and 169. The Bulgarian Air Force received 120 D.520's, and used them operationally against the US 9th Air Force. It was previously believed that the Rumanian Air Force had received a small number of D.520's, but recent information suggests that these were aircraft in transit to Bulgaria. Rumanian Air Force records do not seem to record the receipt of any D.520’s.

In August of 1944, as the South of France was being liberated, fighter Groupe Doret was formed and equipped with D.520's abandoned by the Germans in Tarbes and Toulouse. Groupe Doret was named after Marcel Doret, its commander, and the same test pilot that first took the D.520 into the air in October 1938. These planes took part in the attacks on remaining German resistance pockets.   In November of 1944, Groupe Doret was integrated into GC II/8 Saintogne of the newly formed Atlantic Air Forces.  D.520's of this group were used as escorts for A-24 Dauntless strikes on German-held pockets on the Atlantic coast.  In February 1945, the surviving Saintogne Dewoitines were then added to GCB I/18 and used as ground support and reconnaissance aircraft.  At the conclusion of this second Battle of France, only ten D.520's were still in flying condition in metropolitan France.

After the war, the D.520 served with training units in the new Armee de l'Air. Several were converted to two-seat configuration (D.520DC). The last D.520 was finally withdrawn from service in September 1953, and today no flying examples of this fine fighter remain.

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Variants

Type

Number Built

Remarks

D.520.01

1

First prototype. Single-seat, single-engine, low-winged monoplane with all-metal stressed-skin construction, monocoque fuselage and monospar wing. Hispano-Suiza HS 12Y-21 driving two-bladed fixed pitch wooden propeller, short racing-style fin, twin underwing radiators, no armament, and fixed tail-skid. Change to Hispano-Suiza HS 12Y-29 with three-bladed propeller, and single central radiator achieved required 520 km/h top speed and solved overheating problem.

D.520.02

1

Second prototype. Powered by Hispano-Suiza HS 12Y-29 with three-bladed propeller. Central radiator, taller fin, new canopy, strengthened landing gear. Armament of one 20 mm cannon firing through spinner, and two underwing 7.5 mm (0.295 in) machine guns.

D.520.03

1

Third prototype. Similar to second prototype. Powered by Hispano-Suiza HS 12Y-31 with Szydlowski supercharger. Tail wheel fitted in place of the skid.

D.520

905
437 before Armistice; 478 after Armistice

Production D.520. Similar to third prototype. Powered by Hispano-Suiza HS 12Y-45 with Szydlowski supercharger. First production aircraft flew on 31 October, 1939. Four hundred thirty seven D.520's completed by time of the Armistice. Further 478 built by SNCASE in Vichy France. D.520's competed after May 1942 had Hispano-Suiza HS 12Y-49 (supercharger with higher altitude rating).

D.520z

1

Development of D.520. Redesigned and lengthened engine cowling with Hispano-Suiza HS 12Z of 882 kW (1,200 hp), new cooling system, modified landing gear, and armament of three 20 mm cannon. Projected top speed of 650 km/h. Project formulated in 1939. In 1942, Vichy France requested German approval for construction of three prototypes and 230 production aircraft.  Approval granted for construction of single prototype and 105 production aircraft.  In March 1943 (shortly after occupation of Vichy France) Germany halted construction of the prototype.  Some post-war testing done. Never flew.

D.521

1

Development of D.520. Due to probable shortages of HS 12Y 45 engine, plans were to use Rolls-Royce Merlin III in production D.520's from 251st aircraft onwards. A production D.520 was fitted with the Merlin III, and armament of two 20 mm cannons and two machine guns, but heavier engine resulted in centre-of-gravity (CG) problems. The aircraft was considered to be too unstable, and development was abandoned in favour of D.524.

D.522

0

Planned development of D.520. Due to probable shortages of HS 12Y 45 engine, plans were to use American Allison V-1710C-15 engines of 1,040 hp (764 kW) in production D.520's. Manufacture of engines was to be by Ford Motor Company. Aircraft designated as D.522. Project abandoned after Armistice (22 June 1940).

D.523

1

Development of D.520. New powerplant to be Hispano-Suiza HS 12Y-51 with Szydlowski-Planiol supercharger, giving 1,000 hp (735 kW) in production D.520's from 601st aircraft onwards. First flight on 9 May 1939. Top speed of 570 km/h. Not proceeded with.

D.524

1

Development of D.520. New powerplant to be Hispano-Suiza HS 12Y-89ter with 1,200 hp (882 kW) in production D.520's from 781st aircraft onwards. Projected speed was 616 km/h at 7,000 m. Prototype (ex-D.520 no. 41) never flew.

D.525

1

Development of D.523. New Hispano-Suiza supercharger instead of Szydlowski-Planiol supercharger in production D.520's from 751st aircraft onwards. Never flew.

D.530

0

Planned development of D.520. This was a planned derivative of the D.520 with a Rolls-Royce Merlin of 1,400 hp or Hispano-Suiza 12Y (1,800 hp) engine. Not built.

D.550

1

Racing development of D.520. Hispano-Suiza HS 12Ycrs engine and shortened wings.

D.551

18
(Total D.551/2)

Military development of D.550 racer. Hispano-Suiza HS 12Y 51 engine. Eighteen aircraft (D.551 and D.552) at various stages of completion at date of Armistice (22 June 1940). None completed.

D.552

18
(Total D.551/2)

Military development of D.550 racer. Hispano-Suiza HS 12Z engine. Eighteen aircraft (D.551 and D.552) at various stages of completion at date of Armistice (22 June 1940). None completed.

D.553

0

Planned development of D.550 racer with supercharged Hispano-Suiza HS 12Z engine.

D.554

0

Planned development of D.550 racer with supercharged Hispano-Suiza HS 12Z engine.

HD.780

1

Seaplane fighter development of D.520. Powered by Hispano-Suiza HS 12Y 51 of 1,100 hp, twin floats, and a new inverted-gull wing (W shape). Construction started November 1939 - development abandoned April 1940 in favour of D.790. Never flew.

D.790

0

Planned shipboard development of HD.780. Powered by Hispano-Suiza HS 12Y-29 of 920 hp, landing gear from D.520, armament of one 20 mm cannon firing through spinner, and two underwing 7.5 mm (0.295 in) machine guns. Not built due to Armistice.

SE.520z

1

Development of D.520. Redesigned and lengthened engine cowling with Hispano-Suiza HS 12Z. Constructed after the Liberation. Not proceeded with.

D.520DC

13
(converted from D.520)

Post-war conversion of D.520. Armée de l'Air requested a prototype conversion of D.520 (sn: 243) to a two-seater advanced trainer with dual controls. After successful trials, 20 conversions were ordered. Converted aircraft were designated D.520DC (double commande - dual control).  Only 13 actually converted.

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Specifications

Model

D.520

Dimensions

Span

33 ft 5 ½ in (10.2 m)

Length

28 ft 9 in (8.75 m

Height

8 ft 5 ¼ in (2.57 m

Wing area

171.91 sq ft (15.97 m2)

Powerplant

Type

Hispano-Suiza 12Y45

Cubic Capacity

2,197 in3 (36 l)

Cylinders

12-cylinder Vee

Horsepower

935 hp (697 kW)

Weights and Loads  (note - these figures vary for individual aircraft, and are often not directly comparable)

Weight (maximum takeoff)

6,144 lb (2,790 kg)

Weight (normal loaded)

Unknown

Weight (empty)

4,449 lb (2,036 kg)

Performance (note - these figures vary for individual aircraft, and are often not directly comparable)

Maximum speed at [height]

332 mph at 18,045 ft
(534 km/h at 5,500 m)

Stalling speed

Unknown

Climb to [height]

5.48 min to 13,125 ft (4,000m)

Service ceiling

34,450 ft (10,500 m

Range

950 ml (1,530 km)

Armament

Armament

1x Hispano-Suiza HS-404 20 mm cannon firing through spinner

4x MAC 34 M39 7.5 mm (0.295 in) machine guns in wings

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