------------------------------------------------------------------------------ Version of 4 July 1997 ------------------------------------------------------------------------------ --0--------------------------------------------------------------------------- --A--------------------------------------------------------------------------- A.2M, Vreeburg Twin-engined biplane bomber. Underpowered. One built, reportedly flown only once. Type: A.2M Country: The Netherlands Function: bomber Year: 1918 Crew: Engines: 2 * 110hp Le Rhone Speed: 140km/h Ceiling: Range: Armament: AH-64 Apache, Hughes The Netherlands selected the A{H-64} attack helicopter. The model bought is the AH-64D, but without Longbow radar. Until delivery of the AH-64D models begins, a number of AH-64As are leased from the US Army. --B--------------------------------------------------------------------------- B.1, Fokker Biplane flying boat. One delivered to the Dutch Navy. B.2, Fokker Shipboard biplane flying boat. One delivered to the Dutch Navy. Type: B.2 Country: The Netherlands Function: reconaissance Year: 1923 Crew: Engines: 1 * 360hp R.R. Eagle VIII Speed: 175km/h Ceiling: Range: Armament: --C--------------------------------------------------------------------------- C.I, Fokker Biplane reconaissance aircraft, very obviously a development of the {Fokker D.VII} fighter. The C.I was too late to enter service with the German air force. After the end of WWI, Anthony Fokker managed to transfer a number of aircraft and spare parts to the Netherlands. 250 were built, including 42 for the Soviet air force and 62 for the Dutch air force. Type: C.I Country: Netherlands Function: reconaissance Year: 1918 Crew: 2 Engines: 1 * 138kW BMW IIIa Wing Span: 10.50m Length: 7.23m Height: 2.87m Wing Area: 26.25m2 Empty Weight: 855kg Max.Weight: 1255kg Speed: 175km/h Ceiling: 4000m Range: 620km Armament: 2*mg7.7mm 4*b12.5kg C.II, Holland Two-seat biplane. Netherlands, one built. C.3, Fokker Biplane trainer, a reengined Fokker {C.I}. C.IV, Fokker Reconaissance biplane, an enlarged and more powerful development of the {C.I}. 159 were built, for the Dutch armed forces, Spain, the USSR, Argentina and the USA. Type: C.IV Function: reconaissance Country: The Netherlands. Year: 1923 Crew: 2 Engines: 1 * 336kW Napier Lion Wing Span: 12.90m Length: 9.20m Height: 3.40m Wing Area: 39.20m2 Empty Weight: 1450kg Max.Weight: 2270kg Speed: 214km/h Ceiling: 5500m Range: 1200km Armament: 3-4*mg7.7mm C.V, Fokker Two-seat reconaissance biplane. All C.Vs were of mixed construction. Five different sets of wings were available with surfaces between 37.5m2 and 46.10m2, and it was offered with engines between 350hp an 730hp. The C.V was succesfully exported. The C.V was still in Dutch front line service in May 1940. The Germans used some as night attack aircraft on the Eastern front in 1944, and Swiss C.V-Es served as target tugs until 1954! Type: C.V-D Country: The Netherlands Function: reconaissance Year: 1926 Crew: 2 Engines: 1 * 336kW Hispano-Suiza Wing Span: 12.50m Length: 9.55m Height: 3.50m Wing Area: 28.80m2 Empty Weight: 1420kg Max.Weight: 1915kg Speed: 200km/h Ceiling: 7000m Range: 770km Armament: 2*mg7.9mm 200kg C.VI, Fokker Reconaissance biplane. C.VIII, Fokker Parasol-wing, single-engined reconaissance aircraft. Nine C.VIIIW floatplanes sold to the MLD, one with wheeled landing gear to the LVA. Type: C.VIIIW Country: The Netherlands Function: reconaissance Year: Crew: 3 Engines: 1 * Speed: Ceiling: Range: Armament: C.IX, Fokker Heavier development of the {C.V}. Five sold to the Dutch LVA, one to Switzerland. C.X, Fokker Two-seat biplane reconaissance aircraft. The C.X was a sleek, good-looking aircraft; it replaced the older {C.V}. But it was immediately obsolete, being introduced in 1936. It was license-built in Finland, with a Bristol Pegasus radial engine. Type: C.X Country: The Netherlands Function: reconaissance Year: 1937 Crew: 2 Engines: 1 * 480kW R.R. Kestrel Wing Span: 12m Length: 9.2m Height: 3.3m Wing Area: Empty Weight: 1400kg Max.Weight: 2250kg Speed: 320km/h Ceiling: 8300m Range: 830km Armament: 2*mg7.9mm 400kg C.XI, Fokkker Catapult-launched floatplane; 14 built. Type: C.XI-W Function: reconaissance Year: 1938 Crew: 2 Engines: 1 * 570kW Bristol Pegasus III Wing Span: 13.0m Length: 10.4m Height: 4.5m Wing Area: Empty Weight: 1720kg Max.Weight: 2550kg Speed: 280km/h Ceiling: 6400m Range: 730km Armament: 2*mg7.9mm C.XIV-W, Fokker Biplane trainer and reconaissance aircraft, equipped with floats. The Dutch Navy bought 24. Type: C.XIV-W Function: trainer / reconaissance Year: 1937 Crew: 2 Engines: 1 * 336kW Wright Whirlwind R-975-E3 Wing Span: 12.05m Length: 9.55m Height: 4.25m Wing Area: 31.70m2 Empty Weight: 1315kg Max.Weight: 1945kg Speed: 230km/h Ceiling: 4800m Range: 950km Armament: 2*mg7.9mm --D--------------------------------------------------------------------------- D.IX, Fokker This was the final development of the {Fokker D.VII}, famous German fighter of the end of WWI. The prototype was delivered to the USAAS, which assigned it the designation {PW-6}. It offered only a marginally better performance than the D.VII. One built. Type: D.IX Country: The Netherlands Function: fighter Year: 1921 Crew: 1 Engines: 1 * 220kW Hispano Suiza 8Fb Wing Span: 8.99m Length: 7.09m Height: 2.74m Wing Area: 22.11m2 Empty Weight: 874kg Max.Weight: 1253kg Max. Speed: 223km/h Ceiling: Max. Range: 471km Armament: 2*mg D.X, Fokker Parasol-wing fighter, development of which began in Germany during WWI. The 185hp BMW engine was replaced by a 300hp Hispano-Suiza after transfer of the prototype to the Netherlands. Ten were sold to Spain and one to Finland. Twelve built. Type: D.X Country: The Netherlands Function: fighter Year: 1919 Crew: 1 Engines: 1 * 300hp Hispano-Suiza 8Fb Wing Span: 13.75m Length: 8.00m Height: 3.00m Wing Area: Empty Weight: 860kg Max.Weight: 1246kg Speed: 225km/h Ceiling: Range: Armament: 2*mg7.92mm D.XI, Fokker Sesquiplane fighter, of the familiar Fokker mixed construction. Most of the production (125) went to Russia, that used it as first-line fighter until 1929. Also sold to Argentina, Rumania (50), Spain, and Switzerland (2). 177 built. Three were evaluated by the USAAC as {PW-7}. Type: D.XI Country: The Netherlands Function: fighter Year: 1923 Crew: 1 Engines: 1 * 300hp Hispano-Suiza 8Fb Wing Span: 11.67m Length: 7.50m Height: 3.20m Wing Area: 21.80m2 Empty Weight: 865kg Max.Weight: 1250kg Speed: 225km/h Ceiling: 7000m Range: 440km Armament: 2*mg7.7mm D.XII, Fokker Biplane fighter, designed by Fokker for the American USAAS. It was a sesquiplane of mixed construction. Flight characteristics were unsatisfactory, even after redesign of the upper wing. Three built. Type: D.XII Country: The Netherlands Function: fighter Year: 1924 Crew: 1 Engines: 1 * 440hp Curtiss V-1150 Wing Span: 11.00m Length: 6.74m Height: 2.77m Wing Area: 21.83m2 Empty Weight: 998kg Max.Weight: 1400kg Speed: 250km/h Ceiling: Range: 1100km Armament: D.XIII, Fokker Sesquiplane fighter, a development of the {D.XI}. The official customer for this type was Argentina, but they really were intended for the reborn, still illegal German Luftwaffe on bases in Russia. A total of 52 were delivered. When Germany abandoned Lipetsk in 1933, the remaining 30 were handed over to the USSR. Type: D.XIII Country: The Netherlands Function: fighter Year: 1924 Crew: 1 Engines: 1 * 570hp Napier Lion XI Wing Span: 11m Length: 7.90m Height: 2.90m Wing Area: Empty Weight: 1220kg Max.Weight: 1650kg Speed: 270km/h Ceiling: 8000m Range: 600km Armament: 2*mg7.7mm D.XIV, Fokker The D.XIV was a low-wing monoplane fighter with fixed landing gear. The concept was reminiscent of the {Fokker V.25} of 1918, built in Germany. The D.XIV had an unusual, wide-chord wing with a sweptback leading edge. The pilot set behind the trailing edge. German military pilots praised the D.XIV, but development was abandoned after the prototype crashed. One built. Type: D.XIV Country: The Netherlands Function: fighter Year: 1925 Crew: 1 Engines: 1 * 590hp Hispano-Suiza 12Hb Wing Span: 10.76m Length: 7.90m Height: 3.25m Wing Area: Empty Weight: 950kg Max.Weight: 1350kg Speed: 274km/h Ceiling: Range: Armament: 2*mg7.92mm D.XVI, Fokker Biplane fighter, designed for the Dutch airforce to finally replace the {Fokker D.VII} of WWI vintage. The D.16 looked good and flew well, but its endurance was limited by its oil consumption, to a hour and a half -- the radial engine had been modified to make them more reliable, but at some cost! 21 were built, export models included. Type: D.XVI Country: The Netherlands Function: fighter Year: 1929 Crew: 1 Engines: 1 * 460hp A.S. Jaguar Wing Span: 9.40m Length: 7.20m Height: 2.70m Wing Area: 18.50m2 Empty Weight: 990kg Max.Weight: 1400kg Speed: 330km/h Ceiling: Range: 640km Armament: 2*mg7.92mm D.XVII, Fokker Biplane fighter, a development of the {D.XVI} with a liquid-cooled engine --- initially the Curtiss V-1570, later the Rolls-Royce Kestrel, and Fokker experimented also with Lorraine-Dietrich and Hispano-Suiza engines. The sleek, pretty D.XVII remained in service until 1940. Despite being relegated to training role, a few did fly combat missions. Twelve built. Type: D.XVII Country: The Netherlands Function: fighter Year: 1932 Crew: 1 Engines: 1 * 444kW R.R. Kestrel IIS Wing Span: 9.60m Length: 7.20m Height: 3.00m Wing Area: 20m2 Empty Weight: 1100kg Max.Weight: 1480kg Speed: 356km/h Ceiling: 8750m Range: 850km Armament: 2*mg7.9mm D.XXI, Fokker The D.XXI was a monoplane fighter with fixed landing gear, in itself nothing new for Fokker. The D.XXI had an enclosed cockpit and cantilever main wheel struts. Despite inherent obsolesence, the type had considerable success in Finland, but the 39 Dutch D.XXIs had little luck in May 1940. Finland license-built over 140, Denmark 10. Plans to build it in Spain were halted by the falangist victory in the civil war. Type: D.XXI Country: The Netherlands Function: fighter Year: 1936 Crew: 1 Engines: 1 * 620kW Bristol Mercury VIII Wing Span: 11.00m Length: 8.20m Height: 2.95m Wing Area: 16.20m2 Empty Weight: 1450kg Max.Weight: 2050kg Speed: 460km/h Ceiling: 11000m Range: 950km Armament: 4*mg7.9mm D.XXIII, Fokker Twin-engined, single-seat fighter. The D.XXIII had air-cooled in-line engines in a tandem arrangment, one in the nose and one in the end of the central nacelle. Slender booms carried the tailplane. The prototype was destroyed in 1940. Type: D.XXIII Country: The Netherlands Function: fighter Year: 1939 Crew: 1 Engines: 2 * 540hp Walter Sagitta I-SR Wing Span: 11.50m Length: 10.20m Height: 3.80m Wing Area: 18.50m2 Empty Weight: 2180kg Max.Weight: 2950kg Speed: 524km/h Ceiling: 9000m Range: 840km Armament: (2*mg7.9mm 2*mg13mm) DC.1, Fokker Reconaissance-fighter development of the Fokker {C.IV}. --E--------------------------------------------------------------------------- --F--------------------------------------------------------------------------- F.VI, Fokker The Fokker F.VI parasol-wing monoplane fighter was tested by the USAAS as the {PW-5}. It ordered 10 more. Structure was similar to that of the celebrated Fokker transports: a steel tube fuselage, and a thick cantilever wooden wing with horn-balanced ailerons. Twelve were built. Type: PW-5 Function: fighter Year: 1921 Crew: 1 Engine: 1 * 300hp Wright-Hispano H-2 Wing Span: 12.02m Length: 7.94m Height: 2.74m Wing Area: 22.95m2 Empty Weight: 878kg Max.Weight: 1218kg Max.Speed: 232km/h Ceiling: Max. Range: 2.0hrs Armament: 2*mg7.62mm b F-VII/3m, Fokker The F.VII/3m, a high-wing transport aicraft of mixed construction (wooden wing, steel tube fuselage) with three radial engines, was probably the most famous aircraft ever built by Fokker.The F.VII was used by many airliners and for many long-range flights, but it also had military users. The LVA had some with bomb racks under the fuselage. F-XX, Fokker The Fokker F-XX was a three-engined high-wing transport. It was similar in concept to earlier Fokker airliners such as the F.VII, but had a better streamlined fuselage and retractable landing gear. It was used by the Spanish Republican government during the civil war. F.27, Fokker The Fokker F.27 Friendship was Fokker's largest post-war succes; 768 were built, mostly commercial aircraft. Over 100 are in military service. The military transport version is called 'Troopship', a maritime patrol version is known as 'F.27 Maritime' or fully-armed 'F.27 Maritime Enforcer'. The F.27 is a clean high-wing aircraft with two turboprops. Type: F.27 Mk.200 Country: The Netherlands Function: transport Year: Crew: 2 Engines: 2 * 1730kW Rolls Royce Dart Mk 536-7R Wing Span: 29.00m Length: 23.56m Height: 8.5m Wing Area: 70m2 Empty Weight: 12148kg Max.Weight: 20410kg Speed: 480km/h Ceiling: 9145m Range: 4392km Load: 5970kg, 46 seats F.28 Fellowship, Fokker Small twin-engined jet transport; some are in military service, mainly as VIP transports. Type: F.28 Mk.3000 Country: The Netherlands Function: transport Year: Crew: 2-3 Engines: 2 * 44kN R.R. Spey RB.183-2 Mk.555-15P Wing Span: 25.07m Length: 27.4m Height: 8.47m Wing Area: 79m2 Empty Weight: 16780kg Max.Weight: 33110kg Speed: 843km/h Ceiling: 10675m Range: 2745km Load: 8985kg, 65 seats F.60, Fokker Transport version of the Fokker F.50, ordered by the Dutch Air Force. The F.50 is a modernized development of the {F.27}. FK.31, NVI The FK.31 was a parasol monoplane, designed as fighter and reconaissance aircraft. Despite the deep, fat fuselage the FK.31 had a good performance. The FK.31 mock-up -- claimed by Koolhoven to be a real aircraft! -- made a good impression on the Paris Salon of 1922, but the aircraft first flew in June 1923. Four were built for the Dutch kolonial forces and eight for Finland, that license-built four more. Its service life was very brief because of major contructional and technical faults, and excessively poor flying characteristics. Type: FK.31 Country: the Netherlands Function: fighter / reconaissance Wing Span: 13.70m Length: 7.80m Height: 3.40m Wing Area: 27.20m2 Empty Weight: Max.Weight: Year: 1924 Crew: 2 Engines: 1 * 450hp Bristol Jupiter Speed: 255km/h Ceiling: Range: 6.0hrs Armament: 2-3*mg FK.32, NVI Biplane trainer. The FK.32 was designed around the 130hp Clerget engine, of which large stocks were available. One built. Type: FK.32 Country: The Netherlands Function: trainer Year: 1925 Crew: 2 Engines: 1 * 130hp Clerget Speed: 150km/h Ceiling: Range: FK.34, NVI Three-seat floatplane development of the {FK.31}. The FK.34 had a weak construction. One built. Type: FK.34 Country: The Netherlands Function: observation Year: 1925 Crew: 3 Engines: 1 * 520hp Hispano-Suiza 50-12G Speed: 204km/h Ceiling: Range: Armament: FK.35, NVI The two-seat FK.35 was intended to be built in low-wing monoplane as well as biplane versions, and to be equipped with a powered gun turret. It never flew. Type: FK.35 (monoplane) Country: The Netherlands Function: Year: (1926) Crew: 2 Engines: 1 * 600hp Bristol Jupiter Speed: 260km/h Ceiling: Range: Armament: FK.51, Koolhoven Biplane trainer, later also built as light reconaissance aircraft. The FK.51 was a conventional, robust aircraft; the FK.51s that were still in service in May 1940 were wisely not used in combat. At least 28 were sold to the Spanish republican government, and later used by the air force of Franco. 142 built. Type: FK.51 Country: The Netherlands Function: trainer Year: 1936 Crew: 2 Engines: 1 * 350hp Armsotrong Siddeley Cheetah IX Wing Span: 9.00m Length: 7.85m Height: 2.85m Wing Area: 27m2 Empty Weight: 980kg Max.Weight: 1450kg Speed: 253km/h Ceiling: 6500m Range: 825kg Armament: FK.52, Koolhoven Two seat reconaissance-fighter biplane. Although it had such refinements as an enclosed cockpit and single-strut landing gear, in 1938 it was clearly an obsolete design. Koolhoven began building a few FK.52s anyway, and managed to sell some to Finland. Type: FK.52 Country: The Netherlands Function: reconaissance / fighter Year: 1938 Crew: 2 Engines: 1 * 830hp Bristol Mercury VIII Wing Span: 9.80m Length: 8.30m Height: 3.30m Wing Area: 28.40m2 Empty Weight: 1650kg Max.Weight: 2500kg Speed: 382km/h Ceiling: Range: 1130km Armament: 3*mg7.5mm 100kg FK.55, Koolhoven The FK.55 was a remarkable design for a modern monoplane fighter. The engine was buried in the fuselage, behind the pilot, and drove two-bladed contra-rotating propellers by an extension shaft; a cannon fired through the propeller spinner. Understandably, the streamlined FK.55 attracted much attention at the Paris salon in 1936 -- it was not known to the public that this was a mock-up! The real aircraft was less attractive. The FK.55 was a shoulder wing aircraft and this implied design problems with the retractable landing gear, that in the end was never fitted. Also, the engine and drive were underdeveloped and much bulkier than expected. It was flown only once. One built. Type: FK.55 Country: The Netherlands Function: fighter Year: 1938 Crew: 1 Engines: 1 * 860hp Lorraine Petrel Wing Span: 9.60m Length: 9.25m Height: 2.60m Wing Area: 16.00m2 Empty Weight: 1600kg Max.Weight: 2280kg Speed: 520km/h Ceiling: Range: 850km Armament: (1*g20mm 4*mg7.7mm) FK.56, Koolhoven The FK.56 was a monoplane trainer, but also used as reconaissance aircraft. The prototypes had a low-set gull wing, but series aircraft were mid-wing. FK.56s were ordered by the Dutch and Belgian airforces, but the German invasion of May 1940 prevented the delivery of most. Type: FK.56 Country: The Netherlands Function: trainer / reconaissance Year: Crew: 2 Engines: 1 * 450hp Wright Whirlwind Speed: 300km/h Ceiling: Range: Armament: 2*mg F.K.58, Koolhoven This was a monoplane fighter, designed and hastily built for France in the beginning of WWII. The F.K.58 was built of wood and steel tubes and of conventional appearance. The supply of engines and instruments from France was deficient; for delivery to France instruments were fitted, that were removed afterwards and brought back to the Netherlands! Aircraft ordered for the Dutch airforce were never built. Only 13 F.K.58s became operational. Type: F.K.58 Function: fighter Year: 1939 Crew: 1 Engines: 1 * 1036hp Gnome-Rhone 14N-39 Wing Span: 10.97m Length: 8.68m Height: 2.99m Wing Area: 17.30m2 Empty Weight: 1930kg Max.Weight: 2750kg Speed: 475km/h Ceiling: 10000m Range: 750km Armament: 4*mg7.5mm --G--------------------------------------------------------------------------- G.I, Fokker Designed as 'air cruiser', this was a twin-boom, twin-engined fighter aircraft. With its heavy armament and clean lines, the G.I was the best aircraft the Dutch air force had in May 1940. Two versions were built: The G.I originally produced in series for Spain, and a larger three-seat version for the Dutch airforce. In the end both types were used exclusively by the Dutch LVA. The small number of operational G.Is did well in the very brief fighting of May 1940. Surviving G.Is were later used by the Luftwaffe. 62 built. Type: G.I Function: fighter Year: 1938 Crew: Engines: 2 * 825hp P&W R-1535-SB4-G Wing Span: 16.50m Length: 10.38m Height: 3.35m Wing Area: 35.70m2 Empty Weight: 3150kg Max.Weight: 4800kg Speed: 443km/h Ceiling: Range: 1400km Armament: (4*mg7.9mm) Type: G.IA Function: fighter Year: 1938 Crew: 2-3 Engines: 2 * 830hp Bristol Mercury VIII Wing Span: 17.15m Length: 11.50m Height: 3.40m Wing Area: 38.30m Empty Weight: 3360kg Max.Weight: 4800kg Speed: 475km/h Ceiling: 9300m Range: 1520km Armament: 9*mg7.9mm 400kg --H--------------------------------------------------------------------------- --I--------------------------------------------------------------------------- --J--------------------------------------------------------------------------- --K--------------------------------------------------------------------------- Kingbird, Fokker Proposed AEW and AWACS version of the Fokker 50 turboprop airliner. The Kingbird is currently proposed with a Ericsson phased-array radar in a long boom, fitted on top of the fuselage. Proposal only; no orders yet. Dutch, 1994. --L--------------------------------------------------------------------------- --M--------------------------------------------------------------------------- --N--------------------------------------------------------------------------- --O--------------------------------------------------------------------------- --P--------------------------------------------------------------------------- --Q--------------------------------------------------------------------------- --R--------------------------------------------------------------------------- --S--------------------------------------------------------------------------- S.I, Fokker Trainer. S.II, Fokker Biplane trainer. Some were converted to ambulances; transparencies were added to create a closed cockpit and a litter was placed under a detachable aft fuselage panel. The S.II had side-by-side seating. S.III, Fokker Biplane trainer. 21 built. S.IV, Fokker Biplane trainer. S.IX, Fokker Biplane trainer, Dutch standard trainer from 1938 to 1940. Twenty built. Type: S.IX Function: trainer Year: 1937 Crew: 2 Engines: 1 * 123kW Armstrong Siddeley Genet Major Wing Span: 9.55m Length: 7.65m Height: 2.90m Wing Area: 23.00m2 Empty Weight: 695kg Max.Weight: 975kg Speed: 185km/h Ceiling: 4300m Range: 710km S.11 Instructor, Fokker Low-wing monoplane trainer. The Netherlands bought 40, that replaced the {Tiger Moth} in Dutch service. Israel bought 41. Macchi license-built 150 for the Italian air force, and 100 more were built in Brazil. Type: S.11 Country: The Netherlands Function: trainer Year: 1950 Crew: 2 Engines: 1 * 190hp Lycoming O-435 Wing Span: 11.00m Length: 8.15m Height: 2.40m Wing Area: 18.50m2 Empty Weight: 810kg Max.Weight: 1100kg Speed: 215km/h Ceiling: 4000m Range: 695km S.12, Fokker Fokker's Brazilian subsidiary built 50 of these, a development of the {S.11} with nosewheel landing gear. S-14 Machtrainer, Fokker The ugly S-14 jet trainer was built in limited numbers for the KLu. It was a straight-winged aircraft with a nose intake, this and side-by-side seating making a fuselage of large cross-section necessary. About 20 built. Type: S-14 Country: The Netherlands Function: trainer Year: 1951 Crew: 2 Engines: 1 * 1574kg R.R. Derwent VIII Wing Span: 12.00m Length: 13.30m Height: 4.70m Wing Area: 31.80m2 Empty Weight: 3765kg Max.Weight: 5350kg Speed: 730km/h Ceiling: 11125m Range: 900km --T--------------------------------------------------------------------------- T.2, Fokker Monoplane on floats, a torpedo bomber. Three were delivered to the U.S. Navy. Type: T.2 Country: The Netherlands Function: torpedo bomber Year: Crew: 3 Engines: 1 * 400hp Liberty Speed: 152km/h Ceiling: Range: 650km Armament: T.3, Fokker Larger development of the {T.2}. Five built for Portugal. It could use floats (T.3W) or wheeled landing gear. Type: T.3W Country: The Netherlands Function: torpedo bomber Year: Crew: Engines: 1 * 360hp R.R. Eagle Speed: Ceiling: Range: Armament: T.IV, Fokker Floatplane torpedo-bomber and reconaissance aircraft. The T.IV was a remarkably ugly, angular monoplane. 33 built. Type: T.IVA Function: torpedo-bomber / reconaissance Year: Crew: 4 Engines: 2 * 559kW Wright Cyclone SR-1820-F2 Wing Span: 26.20m Length: 17.60m Height: 6.00m Wing Area: 97.80m2 Empty Weight: 4665kg Max.Weight: 7200kg Speed: 260km/h Ceiling: 5900m Range: 1560km Armament: 3*mg7.9mm 800kg T.V, Fokker Medium bomber. Sixteen were built, of which nine participated in the fights of May 1940. Type: T.V Function: bomber Year: 1937 Crew: Engines: 2 * 690kW Bristol Pegasus XXVI Wing Span: 21.00m Length: 16.00m Height: 5.00m Wing Area: 66.20m2 Empty Weight: 4640kg Max.Weight: 7235kg Speed: 415km/h Ceiling: 7700m Range: 1630km Armament: 7*mg7.9mm 1000kg T.VIII W, Fokker Twin-engined floatplane, designed as torpedo bomber for the Dutch Navy. After May 1940, some T-VIII W were flown to England and used, with Dutch crews, for sea reconaissance; others were in German service. 36 built. Type: T-VIII W Function: torpedo bomber Year: 1940 Crew: 3-4 Engines: 2 * Wright R-975-E3 Wing Span: 18m Length: 13m Height: 5m Wing Area: 44m2 Empty Weight: 3100kg Max.Weight: 5000kg Speed: 285km/h Ceiling: 6800m Range: 2750m Armament: 2*mg7.9mm 605kg Troopship, Fokker F.27 See {F.27}. --U--------------------------------------------------------------------------- --V--------------------------------------------------------------------------- V.I, Spyker Biplane. One built. Type: V.I Country: The Netherlands Function: fighter ? Year: 1917 Crew: 1 Engines: 1 * 80hp Speed: Ceiling: Range: Armament: V.3, Spyker-Trompenburg Single-seat fighter biplane, developed in 1918 for the LVA. A conventional wooden, unstaggered biplane. It was cancelled as a consequence of the end of WWI. One huilt. Type: V.3 Country: Netherlands Function: fighter Year: 1919 Crew: 1 Engines: 1 * 130hp Clerget Wing Span: 8.19m Length: 6.30m Height: 2.60m Wing Area: Empty Weight: Max.Weight: Speed: 180km/h Ceiling: Range: Armament: 2*mg7.92mm --W--------------------------------------------------------------------------- --X--------------------------------------------------------------------------- --Y--------------------------------------------------------------------------- --Z--------------------------------------------------------------------------- ------------------------------------------------------------------------------