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Aldinga Airfield, Colville Rd, Aldinga, SA 5173, Australia. Gates open 8:30am Aldinga Airshow 2024 WWW.TICKETEBO.COM.AU Aldinga Aviation is proud to bring you the 2024 Aldinga Airshow.

The Fieseler Fi 167 was a 1930s German biplane torpedo and reconnaissance bomber designed for use from the Graf Zeppelin class aircraft carriers under construction from 1936 to 1942. In early 1937, the Reichsluftfahrtministerium (German Ministry of Aviation) issued a specification for a carrier-based torpedo bomber to operate from Germany's first aircraft carrier, the Graf Zeppelin construction of which had started at the end of 1936. The specification was issued to two aircraft producers, Fieseler and Arado, and demanded an all-metal biplane with a maximum speed of at least 300 km/h (186 mph), a range of at least 1,000 km (631 mi) and capable both of torpedo and dive-bombing. By mid-1938 the Fiesler design proved to be superior to the Arado design, the Ar 195. The aircraft exceeded by far all requirements, had excellent handling capabilities and could carry about twice the required weapons payload. Like the company's better known Fieseler Fi 156 Storch, the Fi 167 had surprising slow-speed capabilities; under the right conditions, the plane would be able to land almost vertically on a moving aircraft carrier. During a test flight, Gerhard Fieseler himself let the plane drop from 3,050 to 30 metres (10,000 to 100 ft) while staying above the same ground point. For emergency landings at sea the Fi 167 could jettison its landing gear, and airtight compartments in the lower wing would help the aircraft stay afloat at least long enough for the two-man crew to evacuate. Two prototypes (Fi 167 V1 and V2) were built, followed by twelve pre-production models (Fi 167 A-0) which had only slight modifications from the prototypes.

The Curtiss A-8 was a low-wing monoplane ground-attack aircraft built by the United States company Curtiss Aeroplane and Motor Company, designed in response to a 1929 United States Army Air Corps requirement for an attack aircraft to replace the A-3 Falcon. The Model 59 "Shrike" was designated XA-8. The XA-8 won a competition against the General Aviation/Fokker XA-7, after which 13 service test aircraft were ordered (five as YA-8s and eight as Y1A-8s). After the completion of testing, 11 of these aircraft were redesignated A-8. The A-8 was the first Curtiss machine of all-metal low-wing monoplane configuration with advanced features such as automatic leading edge slats and trailing-edge flaps. Four forward-firing .30 in (7.62 mm) machine guns were mounted in the wheel fairings, and an additional weapon of the same calibre was fitted in the observer's cockpit for rear defense. The standard bomb load was four 100 lb (45 kg) bombs. One YA-8 was fitted with a radial engine and designated YA-10, while another was used for testing of the Curtiss V-1570 Conqueror engine as the Y1A-8A. This aircraft was redesignated A-8 upon the completion of testing. 46 aircraft were ordered as A-8Bs, however the order was changed to the Model 60 A-12s before production began. The A-8 created a sensation in US aviation circles when it went into service with the 3rd Attack Group at Fort Crockett, Texas in April 1932. All other standard aircraft were of biplane configuration, and the first monoplane fighter (the Boeing P-26A) did not become operational until eight months later. Variants XA-8 Model 59, one prototype, (30-387), length 32 ft 6 in (9.91 m), wingspan 44 ft (13 m), gross weight 5,413 lb (2,455 kg) Curtiss V-1570-23 direct drive engine YA-8 Model 59A, service test aircraft, 5 built, (32-344 to 32-348), gross weight 5,706 lb (2,588 kg), one was reworked as the YA-10 prototype with the 625 hp (466 kW) Pratt & Whitney Hornet radial engine Y1A-8 service test aircraft, 8 built, (32-349 to 32-356) gross weight 5,710 lb (2,590 kg) A-8 12 redesignated YA-8 and Y1A-8 aircraft Y1A-8A last Y1A-8 with Curtiss V-1570-57 geared engine, length 3 ft 7 in (1.09 m), gross weight 6,287 lb (2,852 kg) A-8A redesignated Y1A-8A aircraft A-8B cancelled, replaced by A-12 Shrike

The Junkers Ju 86 was a German monoplane bomber and civilian airliner designed in the early 1930s, and employed by various air forces on both sides during World War II. The civilian model Ju 86B could carry ten passengers. Two were delivered to Swissair and five to Deutsche Luft Hansa. In addition a single civilian Ju 86Z was delivered to Sweden's AB Aerotransport. In 1934, a specification for a modern twin-engined aircraft, capable of operating both as a high-speed airliner for the German airline Luft Hansa and as a medium bomber for the nascent Luftwaffe, was issued to both Junkers and Heinkel. Five prototypes were ordered from each company; the Junkers Ju 86 and Heinkel He 111. Junkers' design was a low-winged twin-engined monoplane, of all-metal stressed skin construction. Unlike most of Junkers' previous designs, it discarded the typical corrugated skinning in favour of smooth metal skinning which helped to reduce drag. The craft was fitted with a narrow track retractable-main gear conventional undercarriage with a fixed tailwheel, and twin fins and rudders. It was intended to be powered by Junkers Jumo 205 diesel engines, which although heavy, gave better fuel consumption than conventional petrol engines. The design featured the distinctive Junkers doppelflügel control surfaces on the wing, similar to those on the Junkers Ju 52. These were hinged below the wing's trailing edge, with the outboard section on each side functioning as an aileron, and the inner section functioning as a wing flap. The bomber aircraft had a crew of four; a pilot, navigator, radio operator/bombardier and gunner. Defensive armament consisted of three machine guns, situated at the nose; at a dorsal position; and within a retractable ventral position. Bombs were carried vertically in four fuselage cells behind the cockpit. The airliner version replaced the bomb cells with seating for ten passengers, with fuel tanks being moved from the fuselage to the wings. Jumo 205s were unavailable when the first prototype airframe was completed. Instead, the bomber-configured Ju 86ab1 was fitted with Siemens SAM 22 radial engines and flew for the first time on 4 November 1934. The second prototype, also a bomber, flew in January 1935. The third Ju 86, the first civil prototype, flew on 4 April 1935. Production of pre-series military and civil aircraft started in late 1935, with full production of the Ju 86A-1 bomber commencing in April 1936. Production quickly switched to the improved Ju 86D with a modified tail cone to improve stability. Early use of the Jumo-powered Ju 86 bomber in the Spanish Civil War showed that it was inferior to the He 111, with the diesel engines being unsuitable for rough treatment during combat; and production plans were cut back. One Ju 86 had already been converted to use radial engines as a testbed for possible export versions, and this showed improved reliability. Production switched to a version powered by the BMW 132 engine, the Ju 86E, with production continuing until 1938. The sudden end to production without advance warning meant that there were still enough component parts to construct a further 1,000 aircraft.[10] After the war started, the Luftflotte (Air Fleet) commanders raided their training schools for Ju 52s as transport aircraft, together with their experienced aircrew instructors. This depletion continued with the formation of special bomber crews for the invasions of Norway, the Low Countries, and Crete. This was to a severe blow to the pilot training programme, and Oberstleutnant Lt-Colonel Paul Deichmann, Chief of Staff to the Luftwaffe's Chief of Training Helmuth Wilberg suggested that Ju-86s with dual controls and instruments could be easily produced to replace the appropriated Ju 52s. However, his contention that "the need for air transport services would soon reach tremendous proportions" was simply brushed aside by Göring. Export variants Civil variants, introduced in 1936, were designated Ju 86Z in three different models differing in their engines. The Jumo-engined Ju 86Z-1 (corresponding to the former B-0 or C-1) was sold to Swissair (one), Airlines of Australia (one), and LAN-Chile (three). The BMW 132H-powered Ju 86Z-2 was sold to DLH (two) and the para-military Manchukuo Air Transport (five or more). The Pratt & Whitney R-1690 Hornet-engined Ju 86Z-7 was delivered to AB Aerotransport (ABA) of Sweden (one, for use as a mail carrier), Lloyd Aéreo Boliviano (three), and South African Airways - SAA - (17). The ABA aircraft was later transferred to the Swedish Air Force, with which it served, under the designation Tp 9, until 1958. South African Airways' original intention was to have its Ju 86s powered by 745 hp Rolls-Royce Kestrels. Six aircraft for SAA, flown with these engines, were refitted with Hornets before delivery, and the remainder were also Hornet-powered. The Ju 86K was an export model, also built under license in Sweden by Saab as the B 3 with (905 hp) Bristol Mercury XIX radial engines. Several aircraft remained in service with the Swedish Air Force until 1958. A few were converted for radio interception activities. For details of operational history and 29 variants, click here. Picture above courtesy Geoff Goodall Collection.

The Mooney M10 Cadet is a light airplane manufactured by the Mooney Aircraft Company in 1969 and 1970. The M10 is derived from the ERCO Ercoupe, the type certificates for which Mooney purchased from the Alon Corporation in 1967. The M10 is similar to the Alon A2-A, and indeed a handful of "Mooney A2-As" were built in Kerrville in 1968 before changeover of Mooney's production line was completed. According to the FAA Type Certificate Data Sheet, the "Model 10 is similar to Model A2-A except for new design empennage, ailerons and fuel tank vent." The most obvious difference is that the M10 replaces the iconic Ercoupe-style dual vertical stabilizer with a tail designed to allow the airplane to spin. Changes to the ailerons, along with replacement of the A2-A's tail, were motivated by Mooney's intent to market the M10 as a trainer: student pilots receiving training in a non-spinnable airplane, as the Ercoupe was, were issued FAA pilot certificates carrying the restriction that they could only fly airplanes which were "characteristically incapable of spinning"; thus the spinnable tail was necessary to turn the A2-A into a general-purpose trainer. Given that they were replacing the tail, Mooney's engineers opted to give it the "backward" profile characteristic of the M20 series. Although the M10's empennage has the same silhouette as the "big Mooneys", it does not swivel the way the M20's does; the Cadet's tail is a conventional design with fixed horizontal stabilizer, hinged elevator, and trim tabs. The two type certificates that cover all Ercoupe variants, including the Mooney M10, are currently owned by Univair Aircraft Corporation, in Aurora, Colorado, USA.

The Mooney M22 Mustang is the first attempt at a pressurized single engine aircraft by the Mooney Aircraft Company of the United States. The Mustang was developed to be a top-of-the-line model to supplement Mooney's successful Mooney M20 high-performance light aircraft. It is a five-seat pressurized single-engined aircraft with a wider and longer fuselage than the M20E Super 21 and a taller fin and leading edge fillet. It is a low-winged monoplane with a retractable nosewheel undercarriage, with a similar wing to that used on Mooney's earlier M20 Ranger. The first prototype flew on September 24, 1964, with the type being certified on September 26, 1966. First deliveries commenced in 1965, continuing until 1970. 36 aircraft were completed before the line was closed. It was produced and sold at a loss, which contributed to the bankruptcy of Mooney. The "Mark 22" name had previously been applied to a 1957 Mooney M20 experimental aircraft built with twin engines, a nose cone, and an enlarged tail surface. That aircraft did not go into production. The Model 22, although produced in fairly small numbers, has been operated by private and commercial owners in several countries including the United States and Australia. Its Garrett AiResearch cabin pressurization system gives the equivalent of 11,000 feet (3,400 m) at the aircraft's operational ceiling of 24,000 feet (7,300 m). As a demonstration of its high performance, the second production aircraft was flown non-stop from New York to the Paris Air Show in June 1967, the flight taking 13 hours 10 minutes. The achievement is recorded on the display board in the accompanying photograph. The aircraft had been fitted with an extra fuel tank for the flight. A total of 36 were built. In 2001, 24 aircraft remained in service.