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About red750
- Currently Viewing Topic: Oddball, Experimental, or One-off
- Birthday 22/10/1944
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Former Pilot - PA-28, B23, B35
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Location
Vermont Victoria
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Australia
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The Hawker Hind is a British light bomber of the inter-war years produced by Hawker Aircraft for the Royal Air Force. It was developed from the Hawker Hart day bomber introduced in 1931. An improved Hawker Hart bomber defined by Specification G.7/34, was purchased by the RAF as an interim aircraft, while more modern monoplane bombers such as the Fairey Battle were still in development. Structural elements were a mixture of steel and duralumin with the wings being fabric covered; the main differences compared to the earlier Hart was a new powerplant, (the Rolls-Royce Kestrel V) and the inclusion of refinements from the earlier derivatives such as the cut-down rear cockpit developed for the Demon. The prototype (Serial number K2915) was constructed very rapidly due to Hawker's development work for other proposals and made its first flight on 12 September 1934. A variety of changes were subsequently incorporated ("ram's horn" exhaust manifolds, Fairey-Reed metal propeller and engine improvements) with the first production Hind (K4636) flown on 4 September 1935. The Hind went into service in November 1935 and eventually equipped 20 RAF bomber squadrons. A number were also sold to foreign customers including Afghanistan, the Republic of Ireland, Latvia, Persia (Iran), Portugal, South Africa, Switzerland, and Yugoslavia. By 1937, the Hind was being phased out of front line service, replaced by the Fairey Battle and Bristol Blenheim, with many of the Auxiliary Air Force squadrons changing their role to fighter or maritime patrol units. At the outbreak of the Second World War, 613 Squadron retained the Hind for army co-operation before re-equipping with the Hart derivative, the Hawker Hector, in November 1939. The Hind found a new career in 1938 as a training aircraft, representing the next step up from basic training on Tiger Moths. It continued in use as an intermediate trainer during the war. Hind trainers were also operated by Canada and New Zealand. In 1941, Hinds flew operations in their original role as light bombers against Axis forces. South African Hinds were employed against Italian forces in Kenya during the East African Campaign and Yugoslav Hinds were used against the Germans and Italians. Iranian Hinds were used briefly against Allied forces during the Anglo-Soviet invasion of Iran. Imperial Iranian Air Force bases were occupied by the Allies and their aircraft were destroyed or dismantled by the invading British. Hawker Hind aircraft were also used by the Afghan government to suppress the tribal revolts of 1944–1947. Variants Hind Mk I Two-seat light bomber aircraft for the RAF, powered by a 477 kW (640 hp) Rolls-Royce Kestrel piston engine. Afghan Hind Similar to the Hind Mk I, four aircraft fitted with Rolls-Royce Kestrel V engines, plus another four aircraft fitted with Kestrel UDR engines; eight built for Afghanistan. Latvian Hind Two-seat training aircraft, powered by a Bristol Mercury IX radial piston-engine; three built for Latvia. Persian Hind Modified version of the Hind Mk I, powered by a Bristol Mercury VIII radial piston-engine; 35 built for Persia. Portuguese Hind Similar to the Hind Mk I, two aircraft built as bombers, two aircraft built as trainers; four built for Portugal. Swiss Hind Two-seat unarmed communications aircraft; one built for Switzerland. Yugoslav Hind Modified version of the Hind Mk I, two aircraft fitted with Rolls-Royce Kestrel XVI piston-engines, one aircraft fitted with a Gnome-Rhone Mistral engine; three built for Yugoslavia.
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The Handley Page HP. 75 Manx was a British experimental aircraft designed by Handley Page that flew test flights in the early 1940s for possible transport, bomber and fighter aircraft projects. It was notable for its unconventional design characteristics, being a twin-engine tailless design of pusher configuration. The Manx (named after a well-known breed of stub-tailed housecat) was built to participate in a flight research program investigating problems associated with tailless aircraft. The partially-swept wings supported the vertical stabilizers of a twin tail, with elevons for pitch and roll control. Construction of the prototype was subcontracted to Dart Aircraft of Dunstable. There were serious issues encountered early in the development phase that caused a delay in the testing program. After it was delivered in 1939, redesigns had to be made because the Manx was too heavy, and there were also structural integrity issues with the main spar. An unorthodox aspect of the Manx design incorporated into the aircraft was that the main undercarriage was retractable, while the nose gear remained fixed. Taxi tests began in early 1940, but inspection revealed serious deterioration of the wing structures, which required extensive repair. These and further problems delayed the maiden flight until June 1943 (sources conflict as to whether it was 11 or 25 June.) The first flight was terminated early when the canopy was lost in mid-flight, but the pilot managed to land the plane safely. In December 1945 the Manx's regular crew were killed flying the Handley Page Hermes prototype. The Manx had accumulated only about 17 hours of flight time over approximately 30 flights when flight tests were finally terminated in April 1946. The sole example built was scrapped in 1952.
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The Bellanca 28-92 Trimotor was a racing aircraft built to compete in the Istres-Damascus-Paris Air Race of 1937, and was paid for by popular subscription in Romania. Christened Alba Iulia ("White Julia", registration YR-AHA) it was piloted by Captain Alexander Papana of the Romanian Air Force . The aircraft was a low-wing cantilever monoplane with a similar fuselage to the Bellanca 28-70 and 28-90, but was fitted with three engines, one in the nose, and one in each of two underwing nacelles. The nacelles also housed the main undercarriage units when retracted. The fuselage was of tubular steel construction and covered by aluminum back to the cockpit. Aft of the cockpit, the fuselage was covered with fabric. The wings and tail were plywood-covered, and the control surfaces were covered by fabric. The main undercarriage partially retracted into the rear of the wing engine nacelles, but the tailwheel did not retract. Installed in each wing of the aircraft was a 250-HP (186 kW) Menasco C6S4 Super Buccaneer engine. The C6S4 was a direct drive, air-cooled, inverted, straight-six aircraft engine. The C6S4 was supercharged and displaced 544 cu. in. (8.9 L). Each C6S4 engine drove a 6-ft. 6 in (0.15 m) diameter, two-blade, adjustable-pitch propeller. A 420-HP (313 kW) Ranger SGV-770 engine was in the nose of the 28–92. The SGV-770 was an air-cooled, inverted, V-12 engine. The engine was supercharged, displaced 773 cu. in. (12.7 L), and had gear reduction for the 8-ft. 3 in (0.076 m) diameter, two-blade, adjustable-pitch propeller. All of the trimotor's engines were hand cranked to start. The 28-92 had a fuel capacity of around 715 gallons (2,707 L). The aircraft had a span of 46-ft. 4 in (0.10 m), a length of 28 ft 4 in (8.64 m), and weighed 4,700 pounds (2,100 kg) empty. The 28-92 had a top speed of 285 mph (459 km/h) and a 3,000 miles (4,800 km) range at 250 mph (400 km/h) or a 4,160 miles (6,690 km) range at 200 mph (320 km/h). Landing speed was 75 mph (121 km/h). In 1938, Bellanca re-registered the aircraft in the United States as NX2433 and entered it in the Bendix Trophy cross-country race. Frank Cordova was the pilot for the race, and the trimotor flew as race number 99. Unfortunately, because of engine trouble, the aircraft did not finish the cross-country race. The aircraft competed in the 1939 Bendix Trophy race, placing second, piloted by Arthur Bussy. After being sold in South America, the 28-92 ended its days rotting in a small field in Ecuador.
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The SNCASE SE.100 was a French two-seat, twin-engined fighter that first flew in 1939. Mass production was planned to begin late in 1940 but the Fall of France prevented this. The origins of the SE.100 predate the creation of the SNCASE (Sud-Est) company in the nationalisations of 1937. It was designed by Pierre Mercier and Jacques Lecarme at Lioré et Olivier and was initially designated the LeO 50. Underpowered by two Gnome-Rhône 14M engines, the design was recast to use the more powerful Gnome-Rhône 14N-20 and -21 engines, the same used in the Lioré et Olivier LeO 451 bomber, and renamed the SE.100. The aircraft was of conventional all-metal construction, having a mid-wing layout. As with most French twin-engined aircraft of the era, the engines were handed, one airscrew rotating clockwise and the other anti-clockwise, to minimise torque. The aircraft had a twin tail. In production models it was planned to redesign the wing to use components from the LeO 451 wing to ease production. The fuselage was short in appearance, with a long nose and a very short tail, the cockpit being connected to the gunner's position aft by a windowed corridor. The undercarriage was very unconventional, a taildragger with single main wheel at the front and one rear wheel fitted under each vertical tail and retracting into them, rather than two main wheels under the wings or engine nacelles and a single tail wheel as per usual practice. The aircraft was fitted with four Hispano-Suiza HS.404 20 mm cannon in the nose and one in the gunner's post. The first prototype of the SE.100 flew on 29 March 1939 at Argenteuil, and a number of necessary changes were identified during the tests. It was destroyed in a crash on 5 April 1940.[1][2] The aircraft proved to be around 100 km/h faster than the Potez 631, the French Air Force's current twin-engined fighter, and production was authorised. While the tests were proceeding, a second prototype was being built, incorporating the changes, the most obvious of which was the removal of the windowed corridor in the fuselage and its replacement by additional fuel tanks. The armament was increased to six cannon in the nose, two in the gunner's post and one additional cannon in the floor of the gunner's post. As the second prototype was being built, the Citroën company was preparing to mass-produce the aircraft at their Paris works, deliveries planned to begin late in 1940. At least two paper variants were studied, the SE.101 powered by Pratt & Whitney R-1830 Twin Wasp engines, and the SE.102 powered by a different version of the Gnome-Rhône 14N. The SE.500 and SE.800 were to have been a 12-passenger transport and a four-engined transport, respectively, derived from the SE.100.
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The topic was about the efforts of a teenage schoolgirl and her quest for a world record in the Guinness Book of Records.
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Here we go again, led off the track of the original post. There is a Trips/Events/Seats forum. start a topic there.
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Seventeen year old year 12 student Rose Donald landed at Essendon Fields today to complete a solo round Australia flight in her Cessna 172 raising money for Little Wings, a charity providing air transport for country kids requiring medical treatment, and building hours towards her commercial pilot's licence. She has sent documentation of her trip to the Guinness Records organisation to claim the record for the youngest female to complete the trip solo.
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The Vickers Type 432 was a British high-altitude fighter aircraft developed by the Vickers group during the Second World War. Intended to enable the Royal Air Force to engage the enemy's high-altitude bomber aircraft, it was to be armed with six cannons. The origins of the Type 432 lay with a requirement set out in 1939 for twin-engined fighters with 20 mm or possibly 40 mm cannon. Vickers had set out a proposal for a Griffon-engined aircraft, equipped with a 40 mm cannon in a flexible mounting. This was subsequently encouraged by the Air Ministry. Further development was carried out for a design that could also meet F.6/39 for a fixed gun fighter with 20mm cannon. Specification F.22/39 was drawn up to cover the 40 mm project as the Vickers 414 to meet Operational Requirement (OR) 76. This was subsequently revised with aircraft redesigns to become specifications F.16/40 and then F.7/41 for OR. 108. In appearance it resembled a larger version of the de Havilland Mosquito and was known to some as the "Tin Mosquito". The pilot had a pressurised cockpit in the nose, with a bubble dome, similar to an enlarged astrodome. The pressurised cockpit took up the nose section so the cannon would have been fitted in a fairing below the fuselage, to the rear of the aircraft. The aircraft's elliptical wing was built using a unique stressed-skin structure, designed by Barnes Wallis for lightness. The top and bottom were manufactured separately, and then clamped together at the leading and trailing edges, this being named "peapod" or "lobster-claw" structure. This allowed a large internal space unobstructed by ribs, hence capable of housing large fuel tanks (similar to Wallis's geodetic designs). When the competing Westland Welkin was ordered into production, the second prototype of the Vickers fighter, the Type 446, was cancelled, before completion, on 1 May 1943. The first prototype was retained by Vickers for test purposes until the end of 1944, when the aircraft was scrapped after completing only 28 flights.
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Just checked Who's online. 8 userid's. Checked the full list. 206 users online. The rest were Guests.
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A plane has made a hard landing on a highway in Arizona, caught on a dashcam in a vehicle that was lucky to escape. Mesa family nearly hit by small plane during emergency landing near Superior WWW.AZFAMILY.COM A Valley family’s Mother’s Day drive home turned into a terrifying near miss when a small plane landed on US 60 right in front of them.
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Angel Flight - Lottery to win Cirrus G6 SR22
red750 replied to SGM's topic in AUS/NZ General Discussion
I emailed him and got a reply within 15 minutes. He is well, but has had a few system problems logging onto different sites
