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Dewoitine D.19

From Wikipedia, the free encyclopedia
D.19
Role Fighter
Manufacturer Dewoitine
First flight 1925
Number built 5

TheDewoitine D.19was afighter aircraftbuilt inFrancein 1925 in response to aFrench Air Forcesolicitation.

Design and development

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A development of theD.1,the D.19 shared the D.1'sparasol-wingconfiguration, but featured an all-new wing of increasedspan,and had double the engine power. Although rejected by the French Air Force, a demonstration for theSwiss governmentin August 1925 led to an order for three aircraft. An additional example was sold toBelgium,incorporating the same changes requested by the Swiss. These included a change in the wing (changing back to become more similar to the D.1), and the replacement of theLamblin radiatorswith a more conventional frontal radiator.

Operational history

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While the first Swiss D.19 was entirely constructed by Dewoitine in France, the remaining two aircraft were supplied to be assembled by the Swiss factoryEKW.The aircraft were used for many years by the SwissFliegertruppeas trainers for fighter pilots, remaining in service until 1940. All three participated in the international aviation meet atDübendorfin 1927, with one of the D.19s winning the closed-circuit race.

Operators

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Belgium
Switzerland
Czechoslovakia
  • Civil registration L-BYSA

Specifications (D.19 C.1)

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Data fromJane's all the World's Aircraft 1928,[1]Aviafrance:Dewoitine D.19[2]

General characteristics

  • Crew:1
  • Length:7.87 m (25 ft 10 in)
  • Wingspan:10.8 m (35 ft 5 in)
  • Height:3.4 m (11 ft 2 in)
  • Wing area:20 m2(220 sq ft)
  • Empty weight:964 kg (2,125 lb)
  • Gross weight:1,300 kg (2,866 lb)
  • Fuel capacity:156 kg (344 lb) (ca. 109 L (29 US gal; 24 imp gal))
  • Powerplant:1 ×Hispano-Suiza 12JbV-12 water-cooledpiston engine,300 kW (400 hp)
  • Propellers:2-bladed wooden fixed pitch propeller

Performance

  • Maximum speed:265 km/h (165 mph, 143 kn) at sea level
262 km/h (163 mph; 141 kn) at 2,000 m (6,600 ft)
259 km/h (161 mph; 140 kn) at 3,000 m (9,800 ft)
256 km/h (159 mph; 138 kn) at 4,000 m (13,000 ft)
250 km/h (160 mph; 130 kn) at 5,000 m (16,000 ft)
  • Range:400 km (250 mi, 220 nmi)
  • Service ceiling:8,500 m (27,900 ft)
  • Rate of climb:7.3 m/s (1,440 ft/min)
  • Wing loading:65 kg/m2(13 lb/sq ft)
  • Power/mass:0.288 kW/kg (0.175 hp/lb)

Armament

References

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  1. ^Grey, C.G., ed. (1928).Jane's all the World's Aircraft 1928.London: Sampson Low, Marston & company, ltd. pp. 18d–19d.
  2. ^Parmentier, Bruno."Dewoitine D-19".Aviafrance(in French). Paris.Retrieved21 February2018.
  3. ^Cortet 1997, p. 20
  • Cortet, Pierre (June 1997). "Les Premier Chasseurs Dewoitine: quatrième partie".Avions(in French). No. 51. pp. 16–20.

Further reading

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  • Taylor, Michael J. H. (1989).Jane's Encyclopedia of Aviation.London: Studio Editions. p. 323.