Fokker D.XVI

D.XVI
Role	Fighter
National origin	Netherlands
Manufacturer	Fokker
First flight	July 1929
Retired	1939
Primary user	Royal Netherlands Army
Produced	1930-1934
Number built	22
Variants	Fokker D.XVII

The Fokker D.XVI (sometimes written as Fokker D.16) was a sesquiplane fighter aircraft developed in the Netherlands in the late 1920s.

Development

The Fokker D.XVI was a conventional, single-bay sesquiplane with staggered wings braced with V-struts. It featured an open cockpit and fixed undercarriage with a tailskid. The wings were made up of wood spars and ribs with a plywood covering, while the fuselage was of steel tube construction with a fabric covering. Power was provided by an Armstrong Siddeley Jaguar radial engine fitted with a Townend ring.

Operational history

The Royal Netherlands Army ordered 14 aircraft, which differed from the prototype in having divided main undercarriage units in place of the prototype's cross-axle. Hungary purchased four aircraft with Gnome et Rhône-built Bristol Jupiter engines in place of the Armstrong Siddeley Jaguar engines used on the Dutch machines. Evaluation aircraft were also provided to China, Italy, Roumania and the Royal Netherlands East Indies Army. The Royal Netherlands East Indies Army machine was powered by a Curtiss V-1570, which crashed in March 1931 at Schiphol. The D.XVI also won a competition organised by the government of Roumania to select a new fighter, but despite this, no orders were placed. One Dutch Army aircraft was given to Roumania. In lieu of the radial-engined D.XVI, Fokker manufactured the similar Fokker D.XVII powered with an inline engine. One example was fitted with a three-bladed propeller and a full-chord NACA cowling.

Operators

Republic of China

Republic of China Air Force (RoCAF) - evaluation only

Hungary

Royal Hungarian Air Force - two aircraft

Italy

Regia Aeronautica - evaluation only

Netherlands

Royal Netherlands Air Force
Royal Netherlands East Indies Army - evaluation only

Romania

Royal Romanian Air Force - evaluation only

Specifications

Data from [1]

General characteristics

Crew: One pilot
Length: 7.34 m (24 ft 1 in)
Upper wingspan: 9.40 m (30 ft 10 in)
Lower wingspan: 7.12 m (23 ft 4 in)
Height: 2.70 m (8 ft 10 in)
Wing area: 18.5 m² (199 sq ft)
Empty weight: 1,005 kg (2,216 lb)
Gross weight: 1,475 kg (3,252 lb)
Powerplant: 1 × Armstrong Siddeley Jaguar 14-cylinder two-row air cooled radial engine, 340 kW (460 hp)
Propellers: 2-bladed

Performance

Maximum speed: 320 km/h (200 mph, 170 kn)
Range: 640 km (400 mi, 350 nmi)
Endurance: 3.5 hours

Armament

Guns: 2 × fixed, forward-firing 7.9 mm (.31 in) Vickers M20 machine guns, later replaced with FN Browning machine guns, in forward fuselage

References

Citations

Bibliography

Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 405.
World Aircraft Information Files. London: Bright Star Publishing. pp. File 894 Sheet 35.
"British Aero Engine's Success". Flight: 1168. 24 October 1930. Retrieved 2008-03-26.