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red750

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  1. The FMP Qualt 201 is a Czech ultralight and light-sport aircraft, designed and produced by FMP s.r.o. of Prague. The aircraft is supplied as a complete ready-to-fly-aircraft. The Qualt 201 was derived from the earlier FMP Qualt 200, which it replaced in production. The 201 was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed open cockpit under a bubble canopy, fixed conventional landing gear, a T-tail and a single engine in tractor configuration. The aircraft is made from composites. Its 9.2 m (30.2 ft) span wing has an area of 10.5 sq m (113 sq ft) and mounts split-style flaps. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke, the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS and the 85 hp (63 kW) Jabiru 2200 four-stroke powerplants.
  2. The Fly Synthesis Wallaby is an Italian two-seat, microlight monoplane manufactured by Fly Synthesis. The Wallaby is a high-wing monoplane with a high tail boom and with a 37 kW (50 hp) Rotax 503 piston engine fitted in front of the wing. Below the wing is an enclosed cabin with two seats and a fixed tricycle landing gear. The aircraft is available built or as a kit.[1] A Rotax 582 powered variant, the Wallaby R582 is also available. The design uses the wing from the Storch CL mated to a new high tailboom fuselage design, with the design goal of producing an economical aircraft.[3] The aircraft is sold as the Lafayette Wallaby in the United States. Reviewer Marino Boric described the design in a 2015 review as "very pleasant to fly". Variants Wallaby R503 Rotax 503 powered Wallaby R582 Rotax 582 powered
  3. The Flaeming Air FA 04 Peregrine is a German ultralight and light-sport aircraft, designed and produced by Flaeming Air of Zellendorf, Brandenburg. The aircraft is supplied as a complete ready-to-fly-aircraft. The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules, with different models for each category. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear, or optionally conventional landing gear and a single engine in tractor configuration. The aircraft is made from composites, with its fuselage, wing spars, flaps and rudder made from carbon fibre. Its 10.05 m (33.0 ft) span wing has an area of 9.27 sq m (99.8 sq ft). The standard engines available are the 100 hp (75 kW) Rotax 912ULS, 120 hp (89 kW) Jabiru 3300 and the 100 hp (75 kW) Continental O-200 four-stroke powerplants. The FA 04 can be used for aero-towing gliders up to 750 kg (1,653 lb) gross weight. Variants FA 01 Smaragd (Emerald) Initial model for the European FAI microlight class, with a gross weight of 472.5 kg (1,042 lb). FA 02 Kit aircraft with a gross weight of 650 kg (1,433 lb). FA 04 Peregrine Light-sport model for the US market, with a gross weight of 600 kg (1,323 lb). FA 04 SL Super-light model with an empty weight of 270 kg (595 lb), including a ballistic parachute.
  4. The Fly Synthesis Storch (English: Stork) is an Italian ultralight aircraft, designed and today produced by Gryphen Aircraft Industries (ex- Fly Synthesis), introduced in 1990. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction. The Storch was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration. The aircraft is of mixed construction, with the fuselage made from composites and the tail boom an aluminum tube. The HS model has a 8.70 m (28.5 ft) span wing with an area of 11.8 sq m (127 sq ft) and flaperons. Standard engines available are the 80 hp (60 kW) Rotax 912UL and the 85 hp (63 kW) Jabiru 2200 four-stroke powerplants. All controls are operated by teleflex cables, except the ailerons, which are operated by push-pull tubes. In 2024 a new version of the Storch was released, with a full composite fuselage, enhancing the aircraft performance significantly. Specifications listed below. Variants Storch CL Model with a longer 10.15 sq m (33.3 ft) span wing with an area of 13.6 sq m (146 sq ft) and a gross weight of 450 kg (992.1 lb), sold as the Lafayette Stork Classic in the USA. Storch HS Model with a shorter 8.70 m (28.5 ft) span wing with an area of 11.8 sq m (127 sq ft) and Junkers-style flaperons. Gross weight of 472.5 kg (1,041.7 lb) It is sold as the Lafayette Stork Super Sport in the USA. Storch S Model with separate flaps and ailerons, in place of flaperons and a gross weight of 500 kg (1,102.3 lb).
  5. The Lederlin 380L (marketed in North America as the Ladybug) is an unconventional light aircraft developed in France in the 1960s, and marketed for homebuilding. François Lederlin developed the 380L from the Mignet HM.380 "Flying Flea", and eventually created a new aircraft sharing only its choice of wing profile and general configuration. Like the Pou-du-Ciel, the 380L is a tandem wing design, with the forward wing mounted on a set of cabane struts forward of the cockpit, and designed to pivot in flight, to vary its angle of incidence. Otherwise, it is unlike the original Mignet HM.14, having side-by-side seating for two in a fully enclosed cockpit, and a neatly cowled engine. The fuselage is of steel tube construction, metal-skinned at the front and fabric-covered to the rear, and the wings have fabric-covered wooden structure. The tailwheel undercarriage is fixed.
  6. The O'Neill Model J Magnum, also called the Magnum Jake and the Magnum Pickup, is a homebuilt aircraft design for bush flying operations similar to the de Havilland Beaver. O'Neill intended to modify the Aristocraft II six-place homebuilt with a 350 hp (261 kW) radial engine. Eventually a clean sheet design was drawn up based on a bush pilot survey in Alaska. The Magnum is a single-engine, strut-braced, high-wing aircraft with an uncommon dual-main, four-wheel landing gear. The fiberglass gear legs support castoring wheels in the front, allowing for conversion to floats and providing support when the tail section is swung open for cargo loading. The fuselage is constructed from welded steel tubing, with aluminum skin. The engine cowl is sourced from a Cessna UC-78. The wings have full-span flaps, and spoilerons and are designed to fold like those of a Fairchild FB-2C. The fuel tank is mounted under the cockpit and can be released to reduce fire risk during emergency landings. Post flight-testing modifications resulted in changes to the landing gear layout, spoileron airflow control and engine cooling. The Magnum was demonstrated at the EAA Airshow in 1984. In 1996, O'Neill folded the O'Neill aircraft company due to low interest and funding for further development. The prototype was sold in 1996 for an intended turboprop conversion.
  7. https://www.msn.com/en-au/news/other/10-very-ugly-french-aircraft/ss-AA1GaKCB?ocid=winp2fptaskbar&cvid=7b05a0a7871e46c68c58562bd0c0bb34&ei=177#image=1
  8. red750

    LCA LH 212 Delta

    The LCA LH 212 Delta is a two-seat Italian piston engine ultralight helicopter first flown in 2010. Though strong similarities between the Delta and another Italian helicopter, the 1989 DF Helicopters DF334, have been noted, it is not clear if there are direct relationships between either the machines or their makers. The Delta made its first flight after eight years of development. The Delta has a standard pod and boom layout, the latter high set, slender and braced with a narrow angle V-form strut pair to its halfway point from bottom of the pod. It has a short span tailplane with small endplate fins raised above the boom on a swept, high aspect ratio fin, forming a T-tail. The tail rotor, mounted on the starboard side of the boom, has its two blades protected from ground strikes by a long, curved tubular bumper. The pod seats two side-by-side behind a full clear forward transparency. Its skin is carbon fibre over a titanium alloy tube frame. Tandem controls are fitted, with two sets of anti-torque pedals and a T-shaped cyclic control centrally mounted on a console; the single collective pitch lever is placed between the seats. A governor sets the throttle in the absence of pilot input and trim is applied electrically. Small baggage can be stored in under seat lockers. Cabin access is through forward hinged doors in each side. A 84.5 kW (113 hp) Rotax 914 turbocharged, liquid cooled, flat four piston engine with narrow rectangular cheek radiators is mounted behind the seats and partly exposed at the rear, driving a two blade main rotor. The helicopter lands on skids, transversely braced by a pair of airfoil section struts and positioned below the pod on two pairs of similar outward leaning struts, producing a skid track of 1.585 m (5 ft 2 in). The first flight was in 2010 and marketing began in September 2011 at the Blois international ultra light show. A year later eleven flyaway examples had been built. A kit build version is planned. Number built: 11 by September 2012.
  9. The Lasco Lascondor (also frequently known by the misspelling "Lasconder") was a 1930s Australian 8-seat passenger and mail carrier aircraft built by the Larkin Aircraft Supply Company (Lasco) at Coode Island, Victoria. It is claimed to be the first multi-engined aircraft designed and built in the Southern Hemisphere. Development of the Lascondor began in June 1928, concurrently with the company's Lascoter; the two aircraft had 90% commonality of structural parts. Like the Lascoter the Lascondor was a high-wing monoplane with a tubular steel structure, featuring a tailwheel undercarriage and a fully enclosed cabin for the passengers and the pilot. A major change was the Lascondor's three Armstrong Siddeley Mongoose engines instead of the Lascoter's single more powerful Siddeley Puma engine. The Lascondor also had greater fuel capacity and a slightly longer fuselage with a redesigned cabin to accommodate an extra row of seats. In addition, while the Lascoter had two sets of flying controls in the cockpit the Lascondor had only one to allow for another passenger seat, giving an overall capacity of seven passengers and one pilot. The only available photo of the Lascondor.
  10. The Laron Wizard is an American homebuilt aircraft produced by Laron Aviation Tech of Borger, Texas. When it was available the aircraft was supplied as a kit for amateur construction. The Wizard features a strut-braced high-wing, a twin-boom tail layout, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear, with a tail skid, and a single engine in pusher configuration. The aircraft is made from a combination of bolted-together aluminum tubing and fiberglass, with its flying surfaces covered doped aircraft fabric. Its 30.50 ft (9.3 m) span wing, mounts flaps and has a wing area of 140.0 sq ft (13.01 m²). The wing is supported by a single lift strut and jury strut per side. The acceptable power range is 64 to 80 hp (48 to 60 kW) and the standard engines used are the 64 hp (48 kW) Rotax 582, the 74 hp (55 kW) Rotax 618 or the 65 hp (48 kW) Hirth 2706 two stroke powerplants or the 80 hp (60 kW) Rotax 912UL four stroke engine. With the Rotax 582 engine the Wizard has a typical empty weight of 462 lb (210 kg) and a gross weight of 925 lb (420 kg), giving a useful load of 463 lb (210 kg). With full fuel of 10 U.S. gallons (38 L; 8.3 imp gal) the payload for pilot, passengers and baggage is 403 lb (183 kg). The manufacturer estimated the construction time from the supplied kit as 450 hours. By 1998 the company reported that 240 kits had been sold and 220 aircraft were completed and flying.Despite this, a search of most major aircraft photo sites, including jetphotos.com, airliners.net and airport-data.net. only one example could be found on the Russian site airwar2.ru. The image is shown below-
  11. The Lambert Mission 212 is a conventionally laid out low-wing, fixed undercarriage, single-engine, four-seat kit built aircraft designed in the UK by a Belgian college student. Kits are manufactured in Belgium. The M212 has had an unusually long gestation time. It was designed in 1992 by Filip Lambert, then a student at the College of Aeronautics, Cranfield, and was selected as one of three winners of the Royal Aeronautical Society Light Aircraft Competition in 1995. Construction of the M212-100 prototype began in 1996. This aircraft was registered in the UK in 2000 and was displayed, complete apart from some engine and fuel supply systems, at the Popular Flying Association (PFA) Rally held at Cranfield in June 2002. The first flight, delayed by another two years, took place on 13 April 2004 at Cranfield with Roger Bailey as pilot. The M212 is an all-composite aircraft with 95% of its weight in pre-pregs. The wing has two main spars plus an auxiliary one, all formed from glass and carbon fibre in epoxy resin. In plan the wing is gently straight tapered, with most sweep on the trailing edge and with turned up wingtips. It has 5° of dihedral and 2° of washout. Electrically actuated single slot flaps are fitted. Fin and rudder are swept, with a small dorsal fin; the rudder is horn-balanced. The tailplane is rectangular and set a little above the fuselage, carrying inset elevators. The fuselage is a monocoque construction, tapering strongly to the rear. The cockpit seats four in two rows with dual controls in front, covered by a forward-hinged, single-piece canopy. There are two side windows for the rear seat passengers. The M212 has a fixed tricycle undercarriage, the mainwheels mounted on forward-leaning cantilever legs in narrow chord fairings, attached to the fuselage. The mainwheels have brakes and the nosewheel is steerable. Only 2 examples were built. More details here.
  12. The 1958 Lanier Paraplane Commuter 110 or 110 Paraplane Commuter PL-8 was one of the last designs stemming from Edward H. Lanier's 1930s patents, and aircraft incorporating apertures in the upper surfaces, which claimed to give benefits in safety, lift and STOL ability. In the early 1930s Edward H. Lanier published six US patents concerned with increased aircraft lift and stability, minimising the stall, sideslip and spin. This was to be achieved through vacuum chamber ("Vacua-cells"), initially in the upper fuselage but later in the upper wing, where the reduced pressure established by airflow over a curved surface would act on the lower surface inside the cell, providing lift. The second patent suggests that the cell should contain angled spanwise slats to prevent air entering them at low speeds and that these should be adjustable so that the cells could be closed when required. The earlier patents stress stability improvements; claims of enhanced lift begin with the fourth patent. Five Lanier Vacuaplanes were built in the 1930s, followed by three Paraplanes from about 1948, before the Paraplane Commuter 110 which first flew in 1958. The Commuter 110 had a wing area of 111 sq ft (10.3 m²), large for its 20 ft 7 in (6.28 m) span, and controllable air entrance slots ("Vacua-Jets") under the lower surface near its leading edge, passing air to the upper surface for boundary layer control. Other details of the upper surface are scarce but photographs appear to show rear hinged, single-piece slats over Vacua-cells as well as narrow open channels next to the fuselage in the very long wing root fairings. Structurally, the cantilever mid wing had strongly cranked inner sections and was tapered in plan with elliptical wing tips. The outer panels carried control surfaces which operated differentially as ailerons and together as flaps. In addition there were split flaps under the trailing edges of the wing roots. More details here.
  13. Two model aero clubs in Melbourne's east that I know of, Knox Model Aero Club on Stud Road, Knoxfield, with three control line circles, and Doncaster Aeromodellers Club on Bulleen Road, Bulleen, with one control line circle and a grass runway for RC models. Both can be searched on Google Maps.
  14. The Johns Ra-Son Warrior or X-3 Warrior is a low wing bushplane with a large short coupled tail surface. The aircraft has a large tapered low wing, with a large horizontal tail surface mounted close to the trailing edge of the wing and conventional tailwheel landing gear. The fuselage has welded steel tube construction with fabric covering. The wings have fabric-covered wooden ribs and spars. A 1,000 lb (454 kg) payload can be lifted by the 185 hp (138 kW) engine. The five-seat cabin can be converted for cargo operations, and two oversized gullwing cabin doors allow loading. The prototype was built over a four-year period. The aircraft received the Experimental Aircraft Association award for achievement in 1963.
  15. An Air India plane plunged 900ft during its flight just two days after the disaster crash that killed 241 people onboard and dozens more on the ground, the airline has revealed. The plane, flying from Indira Gandhi International (IGI) Airport for Vienna, dropped 900ft in midair during a flight on June 14. It landed safely in Vienna following a nine-hour flight, but both pilots onboard have since been grounded pending an investigation by India's air watchdog, the Directorate General of Civil Aviation (DGCA), into the incident, Air India said.
  16. https://www.msn.com/en-au/news/australia/the-long-awaited-new-qantas-plane-touches-down-in-soggy-sydney/ar-AA1HNrPH?ocid=winp2fptaskbarhover&cvid=fbc70d7c517d43c391a6324c08424e44&ei=28
      • 1
      • Informative
  17. https://www.msn.com/en-au/motoring/news/china-s-first-mass-produced-flying-car-debuts/vi-AA1HMzza?ocid=winp2fptaskbarhover&cvid=6039463e2fc74a20ba8b65e00c4c5219&ei=44
  18. Typical press (or TV) ignorance. I saw a graphic on the TV about a Boeing Airbus.
  19. Reports this morning that the Airbus was parked incorrectly.
  20. https://x.com/FlightModeblog/status/1938862373424537667
  21. The Kinney HRH (Hot Rod Helicopter) is an American helicopter that was designed by Robert Kinney and produced by Vortech, Inc in the form of plans for amateur construction. The aircraft was first shown at Sun 'n Fun in 2002. The HRH was designed to comply with the US experimental – amateur-built rules. It features a single main rotor, a single-seat enclosed cockpit with a windshield, skid-type landing gear and a four-cylinder, air-cooled, four-stroke, 165 hp (123 kW) Subaru EJ25 automotive engine. It is the high power to weight ratio that gives the aircraft its name. The aircraft fuselage is made from a mix of welded 4130 steel tube and bolted-together aluminum tubing, with a composite cabin shell. Its 25 ft (7.6 m) diameter two-bladed Waitman composite rotor has a chord of 8 in (20 cm). The tail rotor has a 46 in (117 cm) diameter. The aircraft has an empty weight of 1,000 lb (454 kg) and a gross weight of 1,350 lb (612 kg), giving a useful load of 350 lb (159 kg). With full fuel of 18.5 U.S. gallons (70 L; 15.4 imp gal) the payload is 239 kg (527 lb). The HRH can hover in ground effect at 7,000 ft (2,134 m) and out of ground effect at 5,000 ft (1,524 m). By January 2013 there was one example, the 2001 prototype, registered in the United States with the Federal Aviation Administration.
  22. The Kennedy Giant was a British biplane heavy bomber designed by Kennedy Aeroplanes Ltd. during the First World War. The design was an imitation of works by Igor Sikorsky, with whom the owner of Kennedy Aeroplanes Ltd., C. J. H. Mackenzie-Kennedy, had ostensibly worked prior to setting up the company. The aeroplane was a notorious failure; its size meant that construction had to take place in an open field as none of the hangars near Hayes, Middlesex, where the prototype was assembled, were large enough to house it. For its weight, the aircraft's four engines were inadequate, and the resulting under-powered aircraft could only fly in a straight line once airborne. Following the unimpressive test flight, the design was cancelled and the prototype was left derelict at Northolt Aerodrome for a number of years.
  23. The Howland H-2 Honey Bee is an American homebuilt aircraft that was designed by Bert Howland and made available by Howland Aero Design in the form of plans for amateur construction, with kits provided by Aircraft Spruce & Specialty Co. The H-2 first flew in 1986. The H-2 is a single-seat, open cockpit biplane, with conventional landing gear and a single engine in tractor configuration. The aircraft is made from aluminium and covered in doped aircraft fabric covering. The fuselage is made from square aluminum tubing that is TIG welded and weighs 24 lb (11 kg) when completed. Its 19 ft (5.8 m) span wings are of a straight planform and both of equal span. The wings have seven foam wing ribs per wing panel and incorporate a D-cell front spar and a C-channel rear spar. The landing gear is conventional, with suspended main wheels and a steerable tailwheel. The H-2 has an open cockpit, with a small windshield. Controls are conventional three-axis, with ailerons, rudder and elevator. The standard design has two ailerons, with four optional. Since the death of the designer plans have been intermittently available and were last provided by Classic Aero Enterprises. Aircraft Spruce and Specialty continue to provide raw materials kits. The aircraft has an acceptable power range of 40 to 95 hp (30 to 71 kW) and the Hirth 2706 of 65 hp (48 kW) is the standard engine recommended. Installation of the 95 hp (71 kW) Hirth F30, or an equivalent engine, along with an inverted fuel system, allows intermediate level competition aerobatics. The plans consist of 40 engineering drawings and a booklet of construction notes. Estimated building time is 800 hours. Variants H-2 Base model with two ailerons and a 65 hp (48 kW) Hirth 2706 engine H-2A Aerobatic competition model with four ailerons, inverted fuel system and a 95 hp (71 kW) Hirth F30 engine
  24. The Hodkinson HT-1 was a U.S., eight place, three-engined sesquiplane, first flown in 1929. Despite an order for five, only one had been completed before Hodkinson Aircraft went bankrupt near the start of the Great Depression. It operated in Guatemala for several years. Hodkinson Aircraft was founded in 1929 by William Wadsworth Hodkinson, one of the pioneers of the film industry who in 1916 had organized Paramount Pictures. He later went into film distribution, founding the W.W.Hodkinson Co. and then moved into the aviation business. The HT-1 was built by Valley Manufacturing Co. a division of Hodkinson Aircraft based in Glendale, California. Its designer, Don R. Berlin, later designed the Curtiss P-40. The wings of the HT-1 were both built around spruce spars and had rectangular plans out to rounded tips. The upper wing, with three-quarters of the total wing area, provided most of the lift and mounted narrow chord, Friese ailerons that reached from wingtips to above the outer engines. The short, lower wings were braced to the upper ones with parallel interplane struts between the wing spars. The HT-1 was powered by three 170 hp (130 kW) Curtiss Challenger radial engines, one in the nose and the others on top of the lower wing, braced by vertical struts to the upper spars. Behind the central engine the fuselage was flat sided, with the wing centre-section fixed to it by inverted V cabane struts faired into the fuselage's chrome-molybdenum tube structure. These provided a clear rear view from the pilots' cabin under the leading edge of the wing. Pilot and co-pilot sat side-by-side with dual controls, though the co-pilot's controls could be removed to allow an extra passenger to be carried. Their cabin was normally accessed through doors on either side but there was also a door in the rear which led down to the passengers' windowed, six seat cabin. There was a toilet at the back and also a baggage compartment, though this was only accessible from outside. Cabin access was via doors on either side, opening just ahead of the rear seats. Its tail was conventional, The fixed surfaces, like the fuselage, had chrome-molybdenum tube structures and the tailplane was mounted on top of the fuselage. The fin was braced to the tailplane and had a cropped, roughly triangular profile. The balanced rudder had a blunted rectangular profile.
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