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Everything posted by red750
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Like rmgwa, I am righthanded, but learnt to fly in a Musketeer (left seat, left hand on yoke, right for throttle, mixture, flaps, etc) then moved to Warrior (same), Arrow (same), Bonanza (same). It took a bit of getting used to centre stick, left hand throttle when I flew the Victa Airtourer.
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Here is a screen print of the Wiki page: As you can see, there are a number of variants, as indicated in the text above the photos. all-aero.com lists specs for 6, with different wingspan and area for most, so it depends which model you are referring to. The input form for these profiles only has provision for one set of specs.
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The importance of checklists. ✅
red750 replied to danny_galaga's topic in Aircraft Incidents and Accidents
It's more important when you switch aircraft types - retract or fixed gear, fixed pitch or constant speed, etc. -
The specs are copied from the Wikipedia entry for the Blue Yonder Merlin. aeropedia.com.au quotes the specs for the Macair Merlin as - Wingspan: 9.14 m (30 ft) Length: 6.09 m (20 ft) Height: 1.98 m (6 ft 5 in) Wing area: 15.5 m² (167 sq ft) Max speed: 193 km/h (120 mph) Cruising speed: 134 km/h (83 mph) Stalling speed: 55 km/h (34 mph) Rate of climb: 366 m/min (1,200 ft/min) Service ceiling: 5,486 m (18,000 ft) Fuel capacity: 60.5 litres (13.3 Imp gals) Range: 536 km (333 miles) Empty weight: 218 kg (480 lb) Loaded: 590 kg (1,300 lb) Power Supply: One 48 kw (65 hp) Rotax 582 two-cylinder two-stroke liquid-cooled engine Both versions are listed as designed by John Burch in Canada.
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Part of a series of incredible aircraft paint schemes.
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Cessna flips on landing Essendon 17-05-23
red750 replied to red750's topic in Aircraft Incidents and Accidents
Yeah. Zoom in on Flightradar24 and you'll see the excursion to the left of the runway. -
Cessna 172 VH-WDA flew from Bacchus Marsh to Essendon, and touched down on runway 26 whereupon it flipped onto its roof. The pilot is reported to be uninjured.
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The English Electric Wren was a 1920s British ultralight monoplane built by the English Electric Company Limited at Lytham St Annes, Lancashire. The Wren, designed by W. O. Manning, was a lightweight motor-glider. Manning was a designer of flying boats and decided to try a simpler project. The Wren was a single-engined high-wing monoplane with an empty weight of only 232 lb (105 kg). The first aircraft (Serial Number J6973) was built in 1921 for the Air Ministry. Number built:- 3.
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What's with all the Community Map Markers, did they all have to be reloaded?
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The Ball-Bartoe JW-1 Jetwing was a US research aircraft flown in the 1970s to investigate blown wing technology. The Jetwing was a small, mid-wing design powered by a turbofan and fitted with tail-wheel undercarriage. The upper surface of the swept wings incorporated a slot along 70% span, through which air from the engine's fan stage could be discharged. Mounted above this slot was a small secondary airfoil called an "augmentor", intended to direct the discharged airflow over the wing. With this arrangement, it was found that the aircraft remained controllable at airspeeds as low as 34.76 kn (64.38 km/h; 40.00 mph). Following the test program, the aircraft was donated to the University of Tennessee Space Institute in Tullahoma, which donated the Jetwing to the Wings Over the Rockies Air and Space Museum in Denver, Colorado in 2007. The aircraft was an experimental one-off with only one unit built.
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The Hiller VZ-1 Pawnee (U.S. Army designation; earlier Army designation: HO-1) was a unique direct-lift rotor aircraft, using contra-rotating ducted fans for lift inside a platform upon which the single pilot shifted body weight for directional control. The platform was developed starting in 1953 under an Office of Naval Research (ONR) contract to Hiller Aircraft, and flew successfully beginning in 1955. The original concept had been developed by Charles H. Zimmerman in the late 1940s.[2] Further development followed, both by Hiller Aircraft and the De Lackner Company. There were two main models, the ONR model 1031-A-1, and the somewhat larger VZ-1 Pawnee model produced in 1956 for the U.S. Army. Three of each model were built as prototypes. Neither of the variants was put into production. Due to aerodynamic effects in the duct within which the propellers rotated, the platform was dynamically stable, even though the pilot and center of gravity of the platform were fairly high up. In testing, the prototypes flew well, but the U.S. Army judged them to be impractical as combat vehicles as they were small, limited in speed and only barely flew out of the ground cushion effect. Number built: 6.
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The Petlyakov Pe-2 (Russian: Петляков Пе-2) was a Soviet twin-engine dive bomber used during World War II. One of the outstanding tactical attack aircraft of the war, it also proved successful as a heavy fighter, as a night fighter (Pe-3 variant) and as a reconnaissance aircraft. The Pe-2 was, numerically, the most important Soviet bomber of World War II, at their peak comprising 75% of the Soviet twin-engine bomber force.[4] The Soviets manufactured Pe-2s in greater numbers (11,430 built) during the war than any other twin-engine combat aircraft except for the German Junkers Ju 88 and the British Vickers Wellington.[3][5] Several communist air forces flew the type after the war, when it became known by the NATO reporting name Buck. In 1937, Vladimir Petlyakov was the leader of the Heavy Aircraft Brigade at the Tupolev OKB responsible for the development of the ANT-42 four-engined long-range bomber (which would eventually enter service as the TB-7/Pe-8). However, that same year saw the start of Stalin's Great Purge, and none were spared suspicion; Andrei Tupolev, the head of the OKB, was coerced into signing a "confession" in October 1937 that he had formed an anti-Soviet group that included Petlyakov, and both men along with many others were arrested. Too valuable to be simply executed, unlike many others arrested during the Great Purge, Petlyakov and other weapons designers were instead sent to sharashkas, special prisons run by the NKVD where such valuable prisoners could continue their work under close scrutiny. In 1938, Petlyakov was tasked with leading the first Special Technical Department (STO — SpetsTekhOd'yel) for aviation that also included other future well-known designers such as Vladimir Myasishchev, a colleague of Petlyakov's at the Tupolev OKB. Because the Russian word for "100" (сотка — "sotka") sounds somewhat like the pronunciation of "STO", the STO was later renamed KB-100, and there Petlyakov proposed the development of a twin-engine interceptor against high-altitude long-range bombers, particularly those being developed in Germany such as the Junkers Ju 86P and Henschel Hs 130. His proposal was accepted in March 1938, with the requirement that the first prototype be ready for its first flight before the end of 1939. The project was initially given the name Samolyot 100 (lit. "Aircraft 100") and later called VI-100 (Vysotnyi Istrebitel — "High-Altitude Fighter"). The VI-100 project was an ambitious one for its time, with advanced features such as a pressurised cabin, all-metal construction, turbo-superchargers, and many electrically actuated systems. In addition, the performance requirements were also quite demanding: it was to be capable of reaching 630 km/h at an altitude of 10,000 m, a ceiling of 12,500 m, and a range of 1,400 km. The aircraft would also need a reinforced structure in order to withstand the Mach stresses of making diving attacks from high altitude against enemy bomber formations. In order to assist with the challenging development of the "100", other OKBs such as those of Yakovlev, Mikoyan & Gurevich, and Sukhoi were also enlisted. The first full-scale VI-100 mock-up was completed in May 1939, and the first flight of the prototype occurred on 22 December 1939. For more details on the development, design, armament, operational history and 21 variants, click here. Number built 11,070 (+ 360 Pe-3 night fighter variant).
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Additional powerplant: 6 × solid-fuelled rocket engines, 500 lbf (2.2 kN) thrust each safety standby engines.
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The Bell Aerosystems Lunar Landing Research Vehicle (LLRV, nicknamed the Flying Bedstead*) was a Project Apollo era program to build a simulator for the Moon landings. The LLRVs were used by the FRC, now known as the NASA Armstrong Flight Research Center, at Edwards Air Force Base, California, to study and analyze piloting techniques needed to fly and land the Apollo Lunar Module in the Moon's low gravity environment. The research vehicles were vertical take-off vehicles that used a single jet engine mounted on a gimbal so that it always pointed vertically. It was adjusted to cancel 5/6 of the vehicle's weight, and the vehicle used hydrogen peroxide rockets which could fairly accurately simulate the behavior of a lunar lander. Success of the two LLRVs led to the building of three Lunar Landing Training Vehicles (LLTVs), an improved version of the LLRV, for use by Apollo astronauts at the Manned Spacecraft Center in Houston, Texas, predecessor of NASA's Johnson Space Center. One LLRV and two LLTVs were destroyed in crashes, but the rocket ejection seat system safely recovered the pilot in all cases. The final phase of every Apollo landing was manually piloted by the mission commander. Because of landing site selection problems, Neil Armstrong, Apollo 11 commander, said his mission would not have been successful without extensive training on the LLTVs. Selection for LLTV training was preceded by helicopter training. In a 2009 interview, astronaut Curt Michel stated, "For airborne craft, the helicopter was the closest in terms of characteristics to the lunar lander. So if you didn't get helicopter training, you knew you weren't going. That sort of gave it away." Even Tom Stafford and Gene Cernan did not get LLTV training for their Apollo 10 mission which was the first flight of the Lunar Module to the Moon, because NASA "didn't have plans to land on Apollo 10" so "there wasn't any point in ... training in the LLTV." Cernan only got this training after being assigned as backup commander for Apollo 14, and in 1972 was the last to fly the LLTV while training as commander for Apollo 17, the final landing mission. Built of aluminum alloy trusses, the LLRVs were powered by a General Electric CF700-2V turbofan engine with a thrust of 4,200 lbf (19 kN), mounted vertically in a gimbal. The engine lifted the vehicle to the test altitude and was then throttled back to support five-sixths of the vehicle's weight, simulating the reduced gravity of the Moon. Two hydrogen peroxide lift rockets with thrust that could be varied from 100 to 500 lbf (440 to 2,200 N) handled the vehicle's rate of descent and horizontal movement. Sixteen smaller hydrogen peroxide thrusters, mounted in pairs, gave the pilot control in pitch, yaw and roll. For more details on the history, and the LLTV, click here. (* Note: Another experimental machine built in the UK was also called the Flying Bedstead. It was designed for research VTOL and was the forerunner to the P.1127 and Hawker Harrier aircraft.)
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The very basic Thrust Measuring Rig or 'Flying Bedstead' was the first British VTOL aircraft and gathered useful data for the P.1127 (Harrier) project. The Bedstead's loaded weight was only about 272kg less than the combined thrust of the two engines, and some of that thrust was ducted away for the control ducts. Each control movement reduced the lifting thrust, requiring a bit more throttle and meaning that it could not be controlled at maximum thrust without a height loss. There was little margin for error - and none at all if one engine faltered. The only plus side was that the engine nozzles were arranged to give thrust (lift) on the centreline so that at least it would plunge vertically rather than flip over. Both Bedsteads did crash, one fatally, and the Harrier adopted a quite different lift system.
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CFO VANESSA HUDSON TO REPLACE JOYCE AS QANTAS CEO
red750 replied to red750's topic in AUS/NZ General Discussion
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Lockheed Have Blue (HB1001) was the code name for Lockheed's proof of concept demonstrator for a stealth bomber. Have Blue was designed by Lockheed's Skunk Works division, and tested at Groom Lake, Nevada. The Have Blue was the first fixed-wing aircraft whose external shape was defined by radar engineering rather than by aerospace engineering. The aircraft's faceted shape was designed to deflect electromagnetic waves in directions other than that of the originating radar emitter, greatly reducing its radar cross-section. The Lockheed Have Blue flight tests were proceeding smoothly until 4 May 1978, when HB1001 was making its 36th flight. The aircraft pitched up just as it made contact with the ground which forced the pilot, Bill Park, to abort the landing and make a second attempt. The impact had however been so hard that the landing gear had become jammed in a semi-retracted position. Efforts to lower the gear were unsuccessful and Bill Park was forced to climb again, and eject when his fuel ran out. Both prototypes were eventually lost.
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The Convair Kingfish reconnaissance aircraft design was the ultimate result of a series of proposals designed at Convair as a replacement for the Lockheed U-2. Kingfish competed with the Lockheed A-12 (later developed into the SR.71) for the Project Oxcart mission, and lost to that design in 1959. Never made it past the design stage, no units built.
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Armidale, NSW, light plane crash 3/5/2023
red750 replied to Carbon Canary's topic in Aircraft Incidents and Accidents
Don't know. Could see Cougar and rego on video above, searched it and got that photo. -
Armidale, NSW, light plane crash 3/5/2023
red750 replied to Carbon Canary's topic in Aircraft Incidents and Accidents
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The Blackburn B-20 was an experimental aircraft, first flying in 1940, that attempted to drastically increase the performance of flying boat designs. Blackburn Aircraft undertook an independent design study based on a patent filed by their chief designer, John Douglas Rennie for a retractable pontoon float that formed the planing hull. The B-20 was an attempt to combine the best features of both the flying boat and the floatplane. While on the water, the B-20 was essentially a floatplane, using a large float under the fuselage for buoyancy, and two smaller floats near the wingtips for stability. In flight, the main float retracted upwards towards the fuselage, fitting into a "notch" to become streamlined as a part of the fuselage. The wing floats folded outwards, somewhat like those on the American Consolidated PBY flying boat design, to become the wingtips. This configuration gave the correct wing incidence for takeoff and for flight and in the latter a much reduced drag compared to the deep hulls of flying boats. Number built: 1.
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The Consolidated Vultee XP-81 (later redesignated ZXF-81) is a development of the Consolidated Vultee Aircraft Corporation to build a single seat, long range escort fighter that combined use of both turbojet and turboprop engines. Although promising, the lack of suitable engines combined with the end of World War II doomed the project. Two prototype aircraft were ordered on 11 February 1944 that were designated XP-81. The engine selection was an attempt to couple the high-speed capability of the jet engine with the endurance offered by the propeller engine. The XP-81 was designed to use the General Electric TG-100 turboprop engine (later designated XT31 by the US military) in the nose driving a four-bladed propeller and a GE J33 turbojet in the rear fuselage. The turboprop would be used for normal flight and cruising and the turbojet added for high-speed flight.