red750

The Sud-Ouest Corse was a French mail and passenger transport aircraft, built by SNCASO. The Corse began as the S.O.90 Cassiopée, a nine-passenger aircraft. The S.O.93 Corse and S.O.94 Corse II prototypes were developed as the S.O.95 Corse III. The aircraft was a cantilever mid-wing monoplane, powered by two Renault 12S engines with a retractable conventional landing gear. Seating up to 13 passengers, the seats could be quickly removed in order to carry more cargo. Intended to serve Air France, it failed their aircraft requirements. 60 aircraft were built for Aeronavale, and a small number for other overseas airlines. Variants SNCASO SO.90 Cassiopée Wartime prototype for 8 passengers and powered by 325 hp Bearn 6D-07 engines. First flew 16 August 1943 with 3 built. S.O.93 Corse Prototype powered by Renault 12S engines, 1 built. S.O.94 Corse II Production 10 passenger version, 15 built. S.O.94R Radar training conversion of S.O.94. S.O.95M Corse III Production 13 passenger version with tail-wheel undercarriage, all 45 built for military use.

The Avocet AV24 is the first aircraft in Avocet's clean-sheet design program created for better dynamic stability, increased control, and lower drag. Design iterations were coordinated with engineers from aerospace industry leaders, including NASA, Lockheed Martin Skunk Works and McDonnell Douglas Boeing.

The Bradley BA 100 Aerobat is an American aerobatic homebuilt aircraft that was designed and produced by Bradley Aerospace of Chico, California. When it was available the aircraft was supplied as a kit for amateur construction. The BA 100 Aerobat features a cantilever low-wing, a single-seat enclosed cockpit under a bubble canopy, fixed tricycle landing gear, or optional conventional landing gear, and a single engine in tractor configuration. The all-metal aircraft is made from sheet aluminum. Its 18.40 ft (5.6 m) span wing lacks flaps and has a wing area of 63.00 sq ft (5.853 m2). The cabin width is 22 in (56 cm). The acceptable power range is 70 to 100 hp (52 to 75 kW) and the standard powerplant is the 70 hp (52 kW) Volkswagen air-cooled engine. For aerobatics the BA 100 is stressed to +/-9g. The BA 100 Aerobat has a typical empty weight of 348 lb (158 kg) and a gross weight of 620 lb (280 kg), giving a useful load of 272 lb (123 kg). With full fuel of 10 U.S. gallons (38 L; 8.3 imp gal) the payload for pilot and baggage is 212 lb (96 kg). Factory kit options included conventional landing gear and a STOL kit. The manufacturer estimated the construction time from the supplied kit as 150 hours. Production has concluded. By 1998 the company reported that 33 kits had been sold and 28 aircraft were flying. In December 2013 three examples were registered in the United States with the Federal Aviation Administration. airport-data.com lists seven registered unit in the US.

The Alvarez Polliwagen is a 1970s homebuilt aircraft. The aircraft has a combination of many high performance features not typically found in a Volkswagen air-cooled engine-powered homebuilt. he Polliwagen is a low wing, side-by-side configuration, T tailed, tricycle landing gear equipped aircraft with tip tanks. The aircraft was developed and tested with a one quarter scale radio controlled model. Ailerons and flaps are full span. The fuselage is built from composites with foam cores. The aircraft's engine is configured with a turbocharger and constant speed propeller. Entrance is through a swing up canopy.

The Handley Page H.P.54 Harrow was a heavy bomber designed and produced by the British aircraft manufacturer Handley Page. It was operated by the Royal Air Force (RAF) and used during the Second World War, although not as a bomber. The Harrow was developed during the 1930s as a derivative of the Handley Page H.P.51, an unsuccessful monoplane bomber-transport hybrid. It was a twin-engine, high-wing monoplane with a fixed undercarriage. In 1935, the Air Ministry wrote Specification B.29/35 around the Harrow proposal, seeking a 'stop-gap' heavy bomber to facilitate the expansion of the RAF's bomber squadrons. Handley Page updated the design with new features and along with structural changes to enable more rapid construction. Despite incorporating several modern features, including hydraulically-powered turrets, steam-based cabin heating, and variable-pitch propellers, the performance of the Harrow did not match that of contemporary bombers such as the Armstrong Whitworth Whitley. On 14 August 1936, the Air Ministry ordered one hundred Harrows for the RAF. While the Fleet Air Arm also placed a separate order for one hundred Harrows, Handley Page did not have the capacity to produce these aircraft. On 13 January 1937, the first Harrow was delivered to No. 214 Squadron; by the end of that same year, all one hundred of the RAF-bound units had been delivered. By the end of 1939, the Harrow had been rapidly displaced as a frontline bomber, it was flown as a transport aircraft instead, which included its use as an air ambulance. It participated in several major actions, including an unorthodox defensive role for The Blitz in the winter of 1940–1941 and Operation Market Garden in September 1944. Limited numbers served through to the conclusion of the conflict, the RAF withdrew the Harrow in May 1945. As a transport, the Harrow was routinely used to convey equipment and personnel between domestic military bases across Britain, as well as to continental airfields prior to the Fall of France.It also occasionally undertook risky flights between England and Gibraltar; two aircraft were recorded as having been lost on this route. Harrows also operated in support of Allied forces in their advance into north-west Europe, evacuating wounded from the Arnhem operation during September 1944. Seven Harrows were destroyed by a low level attack by Luftwaffe fighters of JG 26 and JG 54 on Evere airfield as part of Unternehmen Bodenplatte, the German attack on Allied airfields in north-west Europe, on 1 January 1945, leaving only five Harrows intact. These were retired on 25 May 1945. The Harrow also served in a novel operational role at the height of The Blitz against Britain in the winter of 1940–1941. Six Harrows equipped 420 Flight (later 93 Squadron) which used lone Harrows to tow Long Aerial Mines (LAM) into the path of German bombers. The LAM had an explosive charge on the end of a long cable and the unorthodox tactic was credited with the destruction of between four and six German bombers. The experiment was judged of poor value and the planned deployment of Douglas Havocs in the LAM role was cancelled. Seven Harrows were also used by 782 Naval Air Squadron of the Fleet Air Arm as transports from June 1941 to July 1943, being used to carry engines and spare parts as well as passengers. For more details on development and operational experience, click here. 100 Harrows were built.

The Boeing YB-9 was the first all-metal monoplane bomber aircraft designed for the United States Army Air Corps. The YB-9 was a much enlarged twin-engine development of Boeing's single-engine Model 200 Monomail commercial transport. In May 1930, Boeing had flown its Model 200 Monomail single-engined mailplane. The Monomail was of radical design for the time, being a semi-monocoque, stressed skin cantilever monoplane with a retractable undercarriage. Air Corps bomber squadrons of the day were largely equipped with slow strut-braced biplanes built from steel-tube frames covered in doped fabric, such as the Keystone B-6, and Boeing decided to design and build a twin-engined bomber using the same techniques used in the Monomail to re-equip the Air Corps. Boeing built two prototypes of a new bomber as a private venture, which differed in the engines used, with the Model 214 powered by two liquid-cooled Curtiss V-1570-29 Conqueror engines while the Model 215 had two Pratt & Whitney R-1860 Hornet B radial engines. Both aircraft were low winged cantilever monoplanes with a slim, oval cross-section fuselage accommodating a crew of five. The pilot and co-pilot sat in separate open cockpits, with the co-pilot, who doubled as the bombardier sitting forward of the pilot. Two gunners, each armed with a single machine gun sat in nose and dorsal positions, while a radio operator sat inside the fuselage. Like the Monomail, a retractable tailwheel undercarriage was used. The first of the two prototypes to fly was the radial powered Model 215 which, carrying civil markings and the aircraft registration X-10633, made its first flight on 13 April 1931. It was leased to the Air Corps for testing under the designation XB-901, demonstrating a speed of 163 mph (262 km/h). Testing was successful, and both the XB-901 and the as-yet incomplete Model 214 were purchased as the YB-9 and Y1B-9 respectively on 13 August 1931, with an order for a further five for service testing following. The Y1B-9 (Y1 indicating funding outside normal fiscal year procurement), powered by two liquid-cooled Curtiss V-1570-29 'Conqueror' engines, first flew on 5 November 1931. The increased power from these engines, combined with improved streamlining of the engine nacelles, increased its top speed to 173 mph (278 km/h). The YB-9, meanwhile, had been re-engined with more powerful Hornet Bs, demonstrating slightly better performance than the Y1B-9, which was therefore also re-engined with Hornet Bs. The five Y1B-9A service test aircraft (Boeing Model 246) had the Pratt & Whitney R-1860-11 Hornet B engines which powered the re-engined YB-9 and Y1B-9 and a redesigned vertical stabilizer modeled on the 247D transport. While enclosed canopies were considered and designed, the B-9 was never fitted with them. Although it equaled the speed of existing American fighter aircraft, no further aircraft were built, as the Glenn L. Martin Company had flown a prototype of a more advanced bomber, the XB-907, which was ordered into production as the Martin B-10. The first of the five Y1B-9As entered service with the 20th and 49th Bombardment Squadrons, 2nd Bomb Group on 14 September 1932, with all examples built being in service by the end of March 1933. The new bomber proved impossible to intercept during air exercises in May 1932, strengthening calls for improved air defense warning systems. Two B-9s were destroyed during crashes in 1933, one of the accidents being fatal, while the remaining aircraft were gradually phased out over the next two years, with the last being withdrawn on 26 April 1935.

The Mikoyan-Gurevich MiG-25 (Russian: Микоян и Гуревич МиГ-25; NATO reporting name: Foxbat) is a supersonic interceptor and reconnaissance aircraft that is among the fastest military aircraft to enter service. Designed by the Soviet Union's Mikoyan-Gurevich bureau, it is an aircraft built primarily using stainless steel. It was to be the last plane designed by Mikhail Gurevich, before his retirement. The first prototype flew in 1964 and the aircraft entered service in 1970. Although its thrust was sufficient to reach Mach 3.2+, its speed was limited to prevent engines from overheating at higher air speeds and possibly seriously damaging them, and therefore the operational top speed was limited to Mach 2.83. The MiG-25 features a powerful radar and four air-to-air missiles, and it still has the world record for reached altitude of 38 km (125,000 ft). The appearance of the MiG-25 sparked concern in the West and prompted increases in performance requirements for the McDonnell Douglas F-15 Eagle, then already under development in the late 1960s. The capabilities of the MiG-25 were better understood by the West in 1976 when Soviet pilot Viktor Belenko defected in a MiG-25 to the United States via Japan. Production of the MiG-25 series ended in 1984 after completion of 1,186 aircraft. A symbol of the Cold War, the MiG-25 flew with Soviet allies and former Soviet republics, remaining in limited service in several export customers. It is one of the highest-flying military aircraft,[6] one of the fastest serially produced interceptor aircraft, and the second-fastest serially produced aircraft after the SR-71 reconnaissance aircraft, which was built in very small numbers compared to the MiG-25.[8] As of 2018, the MiG-25 remains the fastest manned serially produced aircraft in operational use and the fastest plane that was offered for supersonic flights and edge-of-space flights to civilian customers. Because of the thermal stresses incurred in flight above Mach 2, the Mikoyan-Gurevich OKB had difficulties choosing what materials to use for the aircraft. They had to use E-2 heat-resistant Plexiglas for the canopy and high-strength stainless steel for the wings and fuselage. Using titanium rather than steel would have been ideal, but it was expensive and difficult to work with. The problem of cracks in welded titanium structures with thin walls could not be solved, so the heavier nickel steel was used instead. It cost far less than titanium and allowed for welding, along with heat-resistant seals. The MiG-25 was constructed from 80% nickel-steel alloy, 11% aluminium, and 9% titanium. The steel components were formed by a combination of spot welding, automatic machine welding, and hand arc welding methods. The MiG-25 was theoretically capable of a maximum speed exceeding Mach 3 and a ceiling of 27 km (89,000 ft). Its high speed was problematic: Although sufficient thrust was available to reach Mach 3.2, a limit of Mach 2.83 had to be imposed as the engines tended to overspeed and overheat at higher airspeeds, possibly damaging them beyond repair. For extensive details on background, development, operational history and 25 variants, click here.

The Boeing Model 40 is a United States mail plane of the 1920s. It was a single-engined biplane that was widely used for airmail services in the United States in the 1920s and 1930s, especially by airlines that later became part of United Airlines. It became the first aircraft built by the Boeing company to carry passengers. In 1925, the US Post Office issued a requirement for a mailplane to replace the ex-military DH-4s then in use. The new aircraft was required to use the same water-cooled Liberty V12 engine as used by the DH-4, of which large stocks of war-built engines were available. The resultant aircraft, the Boeing Model 40, was a conventional tractor biplane, with the required Liberty engine housed in a streamlined cowling with an underslung radiator. The aircraft's fuselage had a steel tube structure, with an aluminum and laminated wood covering. Up to 1,000 lb (450 kg) of mail was carried in two compartments in the forward fuselage, while the single pilot sat in an open cockpit in the rear fuselage. The wings and tail were of wooden construction, and the Model 40 had a fixed conventional landing gear. The Model 40 made its first flight on July 7, 1925. Although the prototype was purchased by the US Post Office, the production order went to the Douglas M-2. The Contract Air Mail Act of 1925 set out the gradual privatization of the Post Office's Air Mail routes. In late 1926, bids were requested for the main transcontinental trunk mail route, which was to be split into eastern and western sections, with Boeing bidding for the western section. Boeing revived the design for the tender, with the Model 40A replacing the Liberty engine with a 425 hp (317 kW) air-cooled Pratt & Whitney Wasp radial engine, which was 200 lb (91 kg) lighter than the Liberty, even ignoring the weight of the Liberty's radiator and cooling water. The fuselage was redesigned to make more extensive use of welded steel tubing, and an enclosed cabin was fitted between the mail compartments, allowing two passengers to be carried as well as 1,200 lb (540 kg) of mail. Boeing's bid of $3 per lb was much less than any of the competing bids, and Boeing was awarded the San Francisco to Chicago contract in January 1927, building 24 Model 40As for the route (with a further aircraft being used as a testbed by Pratt & Whitney). The next model to reach production was the Model 40C, with an enlarged cabin allowing four passengers to be carried. Meanwhile, Boeing Air Transport's Model 40As were modified by replacing their Wasp engines with 525 hp (391 kW) Pratt & Whitney Hornet radial engines to become the Model 40B-2. The Model 40B-4 was a new-build aircraft combining the four-passenger cabin of the Model 40C with the Hornet engine of the B-2. Production continued until February 1932. Boeing's airline, Boeing Air Transport, commenced operations on the San Francisco–Chicago route on July 1, 1927. Variants Model 40 Original 1925 design with Liberty engine. Model 40A Revised 1927 design for BATC. the aircraft was powered by a Pratt & Whitney Wasp radial engine, plus seating for two passengers in an enclosed cabin; 25 built. Received Dept of Air Commerce Approved Type Certificate #2. Model 40B Model 40As re-engined with a 525 hp (391 kW) Pratt & Whitney Hornet radial piston engine. 19 Model 40A were converted. Redesignated Model 40B-2. Model 40B-4 Revised Model 40B with seating for four passengers and other improvements. Equipped with openable windows, plus seating for four passengers; 38 built. Model 40B-4A (Specifications below) One Model 40B used as engine testbed by Pratt & Whitney. Model 40H-4 Four Model 40B-4s built by Boeing Canada. Two aircraft were exported to New Zealand. Model 40C Similar to Model 40B-4 but with Pratt & Whitney Wasp engine of Model 40A. (ten built, all later converted to Model 40B-4 standard). Model 40X Unique special-order machine similar to Model 40C with only two-passenger cabin and extra open cockpit forward of pilot's cockpit. Model 40Y Unique special-order machine similar to Model 40X, but with Pratt & Whitney Hornet engine.

The Chaika L-4 (чайка, English: Seagull) is a twin engine amphibious aircraft, designed and built in Russia in the 2000s. It has sold in small numbers and remains in production. Several companies and groups have developed a series of designs which began at an offshoot of the Trod Kuznetsov aircraft engine plant in Samara. Beginning with the L-3, they differ in size and engine type but all are twin engine amphibians with a characteristic V tail. The L-4 is a direct development of the L-6M, promoted by AeroVolga. Its design began in August 2004. All L-4 variants have the same layout and all are largely built of composite materials. They are high-wing monoplanes with twin engines mounted close to the fuselage, on top of the wing. The wings have straight taper on both edges and almost square tips. The L-4 has a pair of flaps on each wing. Its hull has two steps and there are small winglets at waterlevel just aft of the trailing edge. The cabin extends from below the leading edge rearwards to the winglets. Fixed floats under the wings stabilize the L-4 on water; it is operable with waves to 400 mm (15 in) high. The most unusual feature of the L-4 is the empennage arrangement: it has twin fins, mounted on the fuselage and extended forward with long, curved dorsal fillets, separated at the base by the full fuselage width and leaning slightly outwards. The fins carry conventional rudders and the single tailplane is mounted upon the fin tips, extending well beyond them. Tailplane and single piece elevator together are trapezoidal; there is a trim tab at the centre of the elevator. The reason for the design is that the spine serves as a walkway to access the plane from behind, when moored at shore. The L-4 has a conventional undercarriage for land use, all three wheels and the water rudder being retractable. The first flight of the L-4 was in June 2005. The most recent variant, the more powerful L-44 flew in 2009. By mid-2008 sales, probably including L-6s from AeroVolga, had reached 14. Variants L-4 Original design, no longer produced. L-42 Improved, with Rotax 912 ULS flat four 73.3 kW (98.6 hp) engines. L-42M Further improvements: weight savings, winglets, crew ergonomics. Marketed by Aviatech1.com. L-44 More powerful Rotax 914 engines, as detailed below. First flown 2009. L-65 Improved with Rotax 915 iS engines. Improved with Rotax 915 iS engines.

The Bloch MB.150 (later MB.151 to MB.157) was a French fighter aircraft developed and produced by Société des Avions Marcel Bloch. It featured an all-metal construction, complete with a retractable undercarriage, low cantilever wing and a fully enclosed cockpit. The MB.150 was originally developed to conform with the requirements of the 1934 French Air Ministry competition seeking a new fighter design. Despite the competition being won by the competing Morane-Saulnier M.S.406, it was decided to proceed with development. Initially proving unable to attain flight, the modified prototype conducted its maiden flight in October 1937. Service trials of the MB.150 determined the aircraft to hold sufficient promise to warrant further work, leading to the adoption of an expanded and strengthened wing and a more refined Gnome-Rhone 14N-7 engine. During spring 1938, following the completion of further proving trials, an order for a pre-production batch of 25 aircraft was placed. Redesigns of the MB.150 design led to the improved MB.151 and MB.152 which entered squadron service with the Armée de l'Air. By the outbreak of the Second World War, around 120 aircraft had been delivered to the Armée de l'Air but most were not sufficiently equipped to be considered operational. An improved MB.155 had greater range. Ordered into production in 1940, only ten aircraft had been completed by the Fall of France. The MB.157, a further improved model with a heavier and more powerful engine, was completed during the Vichy era. Though it demonstrated promising performance, it did not enter production. On 13 July 1934, the Service Technique Aéronautique (Aeronautical Technical Service) of the French Air Force issued the "C1 design" requirement for a new and completely modern single-seat interceptor fighter. Envisioned to make use of a monoplane layout and a retractable undercarriage, the prospective fighter aircraft was to serve as a replacement for the French Air Force's existing inventory of Dewoitine D.371, Dewoitine D.500, and Loire 46 aircraft. Amongst the various aviation companies who took interest in the specification, to which the potential for a large production order was attached, was French aircraft manufacturer Société des Avions Marcel Bloch. The design team, headed by Maurice Roussel, was assembled at Bloch's Courbevoie facility in Paris. They designed an all-metal stressed skin monoplane, powered by a single 930 hp Gnome-Rhône 14Kfs radial engine and armed with a pair of wing-mounted Hispano-Suiza-built HS.404 cannon. During September 1935, construction of the type's first prototype, designated as the Bloch 150-01, commenced. Although the C.1 competition was ultimately won by a rival design, the Morane-Saulnier M.S.406, it was decided to independently continue with the design's development. During 1936, these efforts culminated in the first attempted flight of the MB.150.01 prototype; unfortunately, the aircraft proved unable to leave the ground during the attempt. In the ensuing disappointment work on the design was temporarily halted, but development was resumed during early 1937. Following the implementation of various modifications, consisting of a strengthened wing of greater area, revised undercarriage arrangement and the installation of a 701 kW (940 hp) Gnome-Rhone 14N-0 radial engine with a three-blade constant speed propeller, on 29 September 1937, the MB.150 finally conducted its maiden flight. Approximately 663 were built. For more details on development, operational history and 8 variants, continue reading here.

The Bloch MB.120 was a French three-engine colonial transport aircraft built by Société des Avions Marcel Bloch during the 1930s. The MB.120 design was selected by the French government for transport use in French overseas territories. It was an all-metal high-wing cantilever monoplane. The prototype was re-worked from the MB.71. Standard accommodation was for a crew of three and up to 10 passengers. The civil aircraft normally carried only four passengers, the rest of the aircraft was filled with mail. Ten production aircraft were produced, six for civil use and four for the French Air Force. The aircraft entered operation in 1934 for Air Afrique, which was a new airline set up by the French government on 11 May 1934 to provide service between the French African territories. Both the civil and military aircraft served only in French Africa. Variants MB.120.01 : First prototype. MB.120 : Three-engined colonial transport aircraft. Ten built.

Explore the amazing features and capabilities of the world’s biggest helicopters like the famous Soviet Mil Mi-26 or the gigantic US CH-53 Helicopter originally built for the US Marine Corps .

The Blackburn B-24 Skua was a carrier-based low-wing, two-seater, single-radial engine aircraft by the British aviation company Blackburn Aircraft. It was the first Royal Navy carrier-borne all-metal cantilever monoplane aircraft, as well as the first dive bomber in Fleet Air Arm (FAA) service. The aircraft took its name from the sea bird which 'divebombs' any potential predators that come too close to its nest. The Skua was designed during the mid-1930s to Specification O.27/34, and was a radical design for the era, combining the functions of a dive bomber and fighter. Its enclosed cockpit and monoplane configuration were obvious shifts from preceding FAA aircraft such as the Hawker Nimrod and Hawker Osprey biplanes. On 9 February 1937, the first prototype performed its maiden flight; it was ordered straight off the drawing board to accelerate its development. In November 1938, the Skua was introduced to FAA service; 33 aircraft were operational by the outbreak of the Second World War. During the early half of the conflict, the Skua was heavily involved in the Norwegian campaign and sank the German cruiser Königsberg, the first major warship sunk in war by air attack and by dive-bombers. It was present during the Battles of Narvik, the Dunkirk evacuation and also the early stages of the Mediterranean theatre. While a capable dive bomber, its poor top speed and rate of climb meant it was severely limited as a fighter aircraft. Despite this, Fleet Air Arm pilots achieved moderate success with the Skua, scoring numerous aerial victories during the Norwegian and Mediterranean campaigns, with at least one pilot making ace status with five victories. In 1941, the Skua was relegated from frontline operations, but continued to be operated in secondary roles, typically training and target tug duties, as late as March 1945. The Blackburn Skua was configured as a low-wing cantilever monoplane of all-metal construction Its fuselage drew on the design of the Blackburn Shark, an earlier biplane, making extensive use of flush-riveted Alclad. It was internally divided into two water-tight compartments beneath the pilot's and gunner's cockpits to provide sufficient buoyancy in the event of a forcing landing at sea For the same reason, the crew compartments were also watertight up to the edges of the cockpit. The fuselage was stressed to withstand catapult-assisted takeoffs and arrested landings aboard aircraft carriers; a hydraulic damping device was incorporated in the hook. The mainplane, both the structure and covering of which was also composed of Alclad, was built as three separate units. The twin-spar heavy centre section was bolted beneath the fuselage to form the bottom of the watertight compartment. The outer wing panels, which tapered in both plan and thickness, ended in detachable upswept tips and were sealed between the main spars to form additional watertight compartments. Recesses in the lower surface of the wing accommodated modified Zap flaps that were used to shorten takeoff runs, steepen glides, and limit the aircraft's speed during steep dives. Balanced ailerons were fitted, which used inset hinges with mass balance assistance. The number built was 192. For many more details, click here.

The Bilsam Sky Cruiser is a Polish microlight aircraft designed and produced by Bilsam Aviation of Poznań, introduced in the early 2000s. The aircraft is supplied as a complete ready-to-fly-aircraft, as a kit and in the form of plans for amateur construction. The manufacturer's website is non-functional and has been so since about 2008, so it is not clear if the company is still in business. The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 450 kg (992 lb). The aircraft has a maximum gross weight of 450 kg (992 lb). With a Rotax 912 ULS engine it is an accepted US light sport aircraft and also a Transport Canada accepted Advanced Ultra-Light Aeroplane. Originally shown as a pusher configuration design in 2003, by 2004 the aircraft had been redesigned. In its production configuration the Sky Cruiser features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cabin with doors for access, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration. The aircraft is made from composite material. Its 9.0 m (29.5 ft) span wing mounts flaps and has a wing area of 10.35 m2 (111.4 sq ft). The standard engine used is the 100 hp (75 kW) Suzuki automotive conversion powerplant. The aircraft has a typical empty weight of 250 kg (550 lb) and a gross weight of 450 kg (990 lb), giving a useful load of 200 kg (440 lb). With full fuel of 60 litres (13 imp gal; 16 US gal) the payload for pilot, passenger and baggage is 157 kg (346 lb). The Sky Cruiser was redesigned by BOT Aircraft as the BOT SC07 Speed Cruiser.