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The Westland IV and Westland Wessex were British high wing, three-engined light transport aircraft built by Westland Aircraft. In 1928, Westland began work on a small three-engined airliner, suitable for low volume, "feeder-liner" type operation, as a follow-on to its single-engined Westland Limousine transport. The new type was known as the Limousine IV early in development, which soon became the name Westland IV. The Westland IV was a high-winged monoplane with a mainly wooden structure. The fuselage was of square section and built around spruce longerons and ash frames, with internal wire bracing and fabric covering. The wings had wooden box spars and spruce wing ribs in a Warren girder arrangement, and were braced to the fuselage by streamlined struts. The aircraft had a fixed tailwheel undercarriage. The Westland IV first flew on 21 February 1929 at which time it was powered by the 95 hp (71 kW) Cirrus engine. This prototype was registered as G-EBXK and was certified for a crew of two and four passengers. The second machine had Hermes engines and a metal rear fuselage. The third machine, G-ABAJ, was modified to take the 105 hp (78 kW) Armstrong Siddeley Genet Major engines as well as some other changes and became the prototype Westland Wessex. The two Westland IVs were subsequently converted to Wessexes giving 10 aircraft in total.

The Short L.17 Scylla was a British four-engined 39-seat biplane airliner designed and built by Short Brothers at the request of Imperial Airways to supplement the Handley Page H.P.42 fleet already in service after Handley Page quoted an excessive price for two additional H.P.42s. They were ordered in 1933. Imperial Airways used the Scylla for scheduled flights from London to Paris and other European cities. Two aircraft were built, Scylla (G-ACJJ) and Syrinx (G-ACJK). Both served with the airline, until its merger into BOAC in 1939, when both were taken out of service the following year, Scylla after being wrecked and Syrinx being scrapped. The Scylla was a land-based development of the Short Kent (S.17) flying boat which used the Kent's flying surfaces on a new fuselage. It was an all-metal biplane with a wingspan of 113 ft (34 m) powered originally by four Bristol Jupiter XFBM radial engines mounted on vertical struts between the upper and lower planes. The square-section fuselage was mounted below the lower wing while the tail had a single fin and rudder with a horizontal stabilizer mounted mid way up. The Scylla was originally fitted with a Flettner-type trim tab mounted on arms extended out from the rudder's trailing edge to reduce control forces. An experimental servo tab mounted on the trailing edge of the rudder was also tested, on G-ACJJ Scylla which led to a patent application submitted jointly by Shorts and Dudley Lloyd Parkes on 7 August 1936. The main undercarriage had one fixed wheel on each side, mounted on three diagonally-braced struts, one to the upper and two to the lower edge of the fuselage; there was a single tailwheel. Ailerons were fitted to both upper and lower wings. The engine nacelles were designed to receive Bristol Jupiter, Pegasus or Perseus engines without modification, This later enabled the two inboard Jupiters of G-ACJK Syrinx to be easily replaced with Perseus IIL sleeve valve engines, to test their performance in airline conditions. Syrinx was fitted with four Pegasus XC engines when it was rebuilt after it had been severely damaged when blown over by crosswinds while taxiing at Brussels airport.

The Bell YFM-1 Airacuda was an American heavy fighter aircraft, developed by the Bell Aircraft Corporation during the mid-1930s. It was the first military aircraft produced by Bell. Originally designated the Bell Model 1, the Airacuda first flew on 1 September 1937. The Airacuda was marked by bold design advances and considerable flaws that eventually grounded the aircraft. The Airacuda was Bell Aircraft's answer for a "bomber destroyer" aircraft. Although it did see limited production, and one fully operational squadron was eventually formed, only one prototype and 12 production models were ultimately built, in three slightly different versions. In an effort to break into the aviation business, Bell Aircraft created a unique fighter concept touted to be "a mobile anti-aircraft platform" as well as a "convoy fighter." Created to intercept enemy bombers at distances beyond the range of single-seat fighter interceptors, the YFM-1 (Y, service test; F, fighter; M, multiplace) was an innovative design incorporating many features never before seen in a military aircraft, as well as several never seen again. Using a streamlined, "futuristic" design, the Bell Airacuda appeared to be "unlike any other fighters up to that time." According to Major Alexander De Seversky's 1942 book, Victory Through Air Power, the Bell Airacuda "represents a great engineering achievement. But its designation as ′convoy fighter′ is erroneous, since that requires different disposition of armament. With its maximum firepower directed forward, it really offers a preview of an effective long-range interceptor fighter." A forward-firing 37 mm (1.46 in) M4 cannon with an accompanying gunner was mounted in a forward compartment of each of the two engine nacelles. Although capable of aiming the cannons, the gunners' primary purpose was simply to load them with the 110 rounds of ammunition stored in each nacelle. The crew of five included the pilot and gunners; a copilot/navigator who doubled as a fire-control officer, using a Sperry Instruments "Thermionic" fire control system (originally developed for anti-aircraft cannon) combined with a gyro-stabilised and an optical sight to aim the weapons; and a radio operator/gunner armed with a pair of machine guns stationed at mid-fuselage waist blisters for defense against attack from the rear. An unusual feature of the Airacuda was the main door for entry. The door was opened and pulled down and hinges folded in on three steps for the crew to climb into the aircraft. For more information on design flaws, accidents and variants, click here.

The Caproni Ca.60 Transaereo, often referred to as the Noviplano (nine-wing) or Capronissimo, was the prototype of a large nine-wing flying boat intended to become a 100-passenger transatlantic airliner. It featured eight engines and three sets of triple wings. Only one example of this aircraft, designed by Italian aviation pioneer Gianni Caproni, was built by the Caproni company. It was tested on Lake Maggiore in 1921: its brief maiden flight took place on February 12 or March 2. Its second flight was March 4; shortly after takeoff, the aircraft crashed on the water surface and broke up upon impact. The Ca.60 was further damaged when the wreck was towed to shore and, in spite of Caproni's intention to rebuild the aircraft, the project was soon abandoned because of its excessive cost. The few surviving parts are on display at the Gianni Caproni Museum of Aeronautics and at the Volandia aviation museum in Italy. As early as 1913 Caproni, then aged 27, had said during an interview for the Italian sports newspaper La Gazzetta dello Sport that "aircraft with a capacity of one hundred and more passengers" would soon become a reality. It was after the war, however, that (besides converting some of his large wartime bombers into airliners) Caproni began designing a huge and ambitious passenger flying boat; he first took out a patent on a design of this kind on February 6, 1919. The idea of a large multi-engined flying boat designed for carrying passengers on long-range flights was considered, at the time, rather eccentric. Caproni thought, however, that such an aircraft could allow the travel to remote areas more quickly than ground or water transport, and that investing in innovative aerial means would be a less expensive strategy than improving traditional thoroughfares. He affirmed that his large flying boat could be used on any route, within a nation or internationally, and he considered operating it in countries with large territories and poor transport infrastructures, such as China. Caproni believed that, to attain these objectives, rearranging wartime aircraft would not be sufficient. On the contrary, he thought that a new generation of airliners (featuring extended range and increased payload capacity, the latter in turn allowing a reduction in cost per passenger) had to supersede the converted leftovers from the war. In spite of criticism from some important figures in Italian aviation, especially aerial warfare theorist Giulio Douhet, Caproni started designing a very innovative aircraft and soon, in 1919, he took out a patent on it. For more details of development, design, testing, etc., click here.

The Stearman-Hammond Y-1 was a 1930s American utility monoplane built by the Stearman-Hammond Aircraft Corporation and evaluated by the United States Navy and the British Royal Air Force. In the early 1930s Dean Hammond designed the Hammond Model Y, a low-wing monoplane twin-boom pusher monoplane. Hammond cooperated with the aircraft designer Lloyd Stearman to develop the type for production. They formed the Stearman-Hammond Aircraft Corporation in 1936 to build the aircraft as the Stearman-Hammond Y-1. The first aircraft was powered by a 125 hp (93 kW) Menasco C-4 piston engine driving a pusher propeller. The performance was not impressive so it was re-engined with a 150 hp (112 kW) Menasco C-4S and re-named the Y-1S. Although designed to be easy to fly the high price meant only 20 aircraft were produced. The aircraft had no rudder as such, the tailplane fins being adjustable but fixed in flight. Turning was by differential aileron and elevator alone. In 1934 the Bureau of Air Commerce held a competition for a safe and practical $700 aircraft. In 1936 the winner of the competition was the Stearman-Hammond Y-1, incorporating many of the safety features of the Ercoupe W-1. Two other winners were the Waterman Aeroplane and a roadable autogyro from the Autogiro Company of America, the AC-35. Twenty-five examples were ordered by the bureau at a price of $3,190 each. The first delivery was considered unacceptable in finish, prompting the production of the re-engineered Y-S model. Two Y-1S, serial numbers 0908 and 0909,were used for radio controlled development trials by the United States Navy as the JH-1. A successful unmanned radio-controlled flight was made with a JH-1 drone on 23 December 1937 at the Coast Guard Air Station, Cape May, N.J. Take-off and landing was controlled via a land based radio set; for flight maneuvers, control was shifted to an airborne TG-2. KLM purchased a Y-1 (PH-APY) for use in training their pilots in tricycle undercarriage. The Royal Air Force also evaluated a former KLM Y-1S in the 1940s. Approximately 2o built. Variants Hammond Model Y Prototype for the 1934 Bureau of Air Commerce safe airplane competition. Stearman-Hammond Y-1 Prototype aircraft with a 125hp (93kW) Menasco C-4 engine. Stearman-Hammond Y-1S (Specifications below) Production aircraft with a 150hp (112kW) Menasco C-4S engine. JH-1 United States Navy designation for two Y-1S used for tests.

From all-aero.com The Impulse 100 took three years of development and 1600 hours of flight testing (the prototype completing 1200 hours). Tested safe load factors were +-5,6G with a safety margin of 1,725. Kit quality control is achieved by vacuum bagging every individual composite piece. The cockpit has adjustable seats and unobstructed view through the canopy. Power is by a Jabiru 3300 engine consuming automotive fuel. The Carbon Fibre, German Kit Plane comes with dual controls & brakes, landing light, wingtip strobes, and electric flaps.

The Colomban MC-30 Luciole (English: Firefly) is an ultra-lightweight plans-built single-seat low-wing tail-dragger monoplane, designed by the French aeronautical engineer Michel Colomban, creator of the tiny single-seat Colomban Cri-cri twin-engined aircraft and the MC-100 Ban-Bi two-seat aircraft. The aircraft is supplied as plans for amateur construction. The Luciole is extremely light, weighing 97 kg (214 lb) empty. It has mixed construction of wood, plywood, metal, foam and glass reinforced plastic. The cantilever wings have foam ribs with a 1 mm plywood skin, sheathed in a thin layer of resin-bonded glass tissue. The Luciole is fitted with a V-Twin Briggs & Stratton four-stroke petrol engine directly driving a 2-bladed Arplast EcoProp 1.16 m (3.8 ft) diameter ground-adjustable propeller. The aircraft is very economical, consuming only 4.5 litres/hour at 150 km/h (93 mph). Although about seven Lucioles have been built in France, only one has been completed in the UK (and half a dozen are under construction), at least one is flying in Germany. The UK aircraft was built under the auspices of the LAA, and to date has logged some 100 hours, flying under a test permit. The Luciole is awaiting full approval from the LAA. LAA approval was required as the Luciole's wing loading of 43.5 kg/m2 was too high to benefit from original UK SSDR microlight sub-category. SSDRs (Single Seat De-Regulated) aircraft had to weigh less than 115 kg (254 lb) without fuel and pilot, and the wing loading could not be more than 10 kg/m2 However, the UK CAA changed the rules in May 2014, and the new SSDR rules state that the aircraft must be single seat, and must have an MTOW of 300 kg, i.e. it must weigh no more than 300 kg at takeoff, including pilot and fuel. Also, the stall speed must be 35 knots or less. There are no other design restrictions. In a flight test report, Francis Donaldson, the LAA's Chief Engineer, declared that although some design compromises were "clearly not ideal", overall he felt "very impressed with Michel Colomban's new creation", saying the aircraft "performed as claimed, was practical and fun". Donaldson's major criticism was that the elevator's GRP spring (to provide self-centering and to impart "feel") was in the cockpit and not in the tail, so that if the elevator control linkage failed, the aircraft could suffer catastrophic lack of pitch-control as "the Luciole would most likely be totally unflyable". However, Colomban has disclosed plans to "modify the system to relocate the tailplane's self-centering trim spring in the rear fuselage, attaching directly to the tailplane .... so a failure of the (linkage) would no longer be disastrous". Variants Colomban MC-30 Luciole Standard model powered by a Briggs & Stratton four-stroke engine. Luxembourg Special Aerotechnics MC30E Firefly Electric aircraft development of the basic design, first flown on 1 August 2011. Powered by 26 hp (19 kW) electric motor running from a 4.7-kWh Kokam battery. The aircraft weighs 113 kg (249 lb) empty and has a 55 minute endurance on a charge. The aircraft has achieved a top speed of 220 km/h (137 mph).

The Brügger MB-1, MB-2 and MB-3 Colibri is a family of small sports aircraft designed in Switzerland in the 1960s and 1970s for amateur construction. The Colibri family are single-seat, low-wing cantilever monoplanes with fixed tailwheel undercarriage powered by a four-cylinder horizontally opposed Volkswagen air-cooled engine automotive conversion. The MB-1 Colibri first flew in 1965 and served as a development aircraft for the definitive MB-2 Colibri 2 that flew in 1970. These aircraft had all-wooden framework with fabric-covered wings and plywood-covered fuselages. The pilot's seat was enclosed by an expansive bubble canopy. In 1976-77, Brügger built and flew an all-metal version as the MB-3. Many examples are actively flying in 2012. The MB-2 is noted for its handling qualities. Specifications of the MB-2 below.