The Team

The Flying Bulls, a dedicated team of aviation enthusiasts renowned for their unparalleled passion for preserving rare historical aircraft, grace numerous European Airshows annually. Their origins trace back to the 1980s when Sigi Angerer, a pilot at Tyrolean Airways, pursued his deep-seated fondness for vintage planes alongside his modern jet responsibilities. Angerer's quest for an accessible warbird led him to acquire a North American T-28B, kickstarting the foundation of the unforgettable fleet. Over time, additions such as the Grumman G44 Widgeon and the iconic Chance Vought F4U-4 Corsair enhanced the collection's prestige, particularly after connecting with Red Bull's visionary leader, Dietrich Mateschitz, in Innsbruck, Austria.

The Corsair played a pivotal role in uniting Angerer and Dietrich Mateschitz, fueling the latter's vision of an unparalleled corporate emblem for the renowned "Red Bull gives you wings" marketing catchphrase. Consequently, the concept of the Flying Bulls took flight. As the global presence of the energizing beverage surged, the fleet's expansion mirrored its success. Facing constraints at Innsbruck airport, a strategic decision emerged in the late 1990s to erect a cutting-edge hangar adjacent to Salzburg airport.

It was around the year 1999 when the decision was made to establish a more enduring home for the dispersed group of pilots and technicians. This led to the formation of "The Flying Bulls" company. Over the years, their blend of superior technical skills and remarkable aesthetics has propelled the Flying Bulls team members to celebrity status in the aviation world.

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The Aircraft

Douglas DC-6B

The Douglas DC-6 is a piston-powered airliner and cargo aircraft built by the Douglas Aircraft Company from 1946 to 1958. Originally intended as a military transport near the end of World War II, it was reworked after the war to compete with the Lockheed Constellation in the long-range commercial transport market. More than 700 were built and many still fly today in cargo, military, and wildfire control roles.

The DC-6 was known as the C-118 Liftmaster in the United States Air Force service and as the R6D in the United States Navy service prior to 1962, after which all U.S. Navy variants were also designated as the C-118.

The United States Army Air Forces commissioned the DC-6 project as the XC-112 in 1944. The Army Air Forces wanted a lengthened, pressurized version of the DC-4-based C-54 Skymaster transport with more powerful engines. By the time the prototype XC-112A flew on 15 February 1946, the war was over, the USAAF had rescinded its requirement, and the aircraft was converted to YC-112A, being sold in 1955.

Douglas Aircraft modified the design into a civil transport 80 in (200 cm) longer than the DC-4. The civil DC-6 first flew on 29 June 1946, being retained by Douglas for testing. The first airline deliveries were to American Airlines and United Airlines on 24 November 1946. A series of inflight fires (including the fatal crash of United Airlines Flight 608) grounded the DC-6 fleet in 1947. The cause was found to be a fuel vent next to the cabin cooling turbine intake; all DC-6s were modified and the fleet was flying again after four months on the ground.

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North American B-25J Mitchell

The North American B-25 Mitchell is an American medium bomber that was introduced in 1941 and named in honour of Major General William "Billy" Mitchell, a pioneer of U.S. military aviation. Used by many Allied air forces, the B-25 served in every theatre of World War II, and after the war ended, many remained in service, operating across four decades. Produced in numerous variants, nearly 10,000 B-25s were built. These included several limited models such as the F-10 reconnaissance aircraft, the AT-24 crew trainers, and the United States Marine Corps' PBJ-1 patrol bomber.

The Air Corps issued a specification for a medium bomber in March 1939 that was capable of carrying a payload of 2,400 lb (1,100 kg) over 1,200 mi (1,900 km) at 300 mph (480 km/h) North American Aviation used its NA-40B design to develop the NA-62, which competed for the medium bomber contract. No YB-25 was available for prototype service tests. In September 1939, the Air Corps ordered the NA-62 into production as the B-25, along with the other new Air Corps medium bomber, the Martin B-26 Marauder "off the drawing board".

Early into B-25 production, NAA incorporated a significant redesign to the wing dihedral. The first nine aircraft had a constant dihedral, meaning the wing had a consistent, upward angle from the fuselage to the wingtip. This design caused stability problems. "Flattening" the outer wing panels by giving them a slight anhedral angle just outboard of the engine nacelles nullified the problem and gave the B-25 its gull-wing configuration. Less noticeable changes during this period included an increase in the size of the tail fins and a decrease in their inward tilt at their tops.

NAA continued design and development in 1940 and 1941. Both the B-25A and B-25B series entered USAAF service. The B-25B was operational in 1942. Combat requirements led to further developments. Before the year was over, NAA was producing the B-25C and B-25D series at different plants. Also in 1942, the manufacturer began design work on the cannon-armed B-25G series. The NA-100 of 1943 and 1944 was an interim armament development at the Kansas City complex known as the B-25D2. Similar armament upgrades by U.S-based commercial modification centres involved about half of the B-25G series. Further development led to the B-25H, B-25J, and B-25J2. The gunship design concept dates to late 1942 and NAA sent a field technical representative to the SWPA. The factory-produced B-25G entered production during the NA-96 order followed by the redesigned B-25H gunship. The B-25J reverted to the bomber role, but it, too, could be outfitted as a strafer.

NAA manufactured the greatest number of aircraft in World War II, the first time a company had produced trainers, bombers, and fighters simultaneously (the AT-6/SNJ Texan/Harvard, B-25 Mitchell, and the P-51 Mustang). It produced B-25s at both its Inglewood main plant and an additional 6,608 aircraft at its Kansas City, Kansas, plant at Fairfax Airport.

After the war, the USAF placed a contract for the TB-25L trainer in 1952. This was a modification program by Hayes of Birmingham, Alabama. Its primary role was reciprocating engine pilot training.

The development of the B-25 was the North American XB-28, designed as a high-altitude bomber. Two prototypes were built with the second prototype, the XB-28A, evaluated as a photo-reconnaissance platform, but the aircraft did not enter production.

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Dassault/Dornier Alpha Jet E

The Dassault/Dornier Alpha Jet is a light attack jet and advanced jet trainer co-manufactured by Dassault Aviation of France and Dornier Flugzeugwerke of Germany. It was developed specifically to perform trainer and light attack missions, as well as to perform these duties more ideally than the first generation of jet trainers that preceded it. Following a competition, a design submitted by a team comprising Breguet Aviation, Dassault Aviation, and Dornier Flugzeugwerke, initially designated as the TA501, was selected and subsequently produced as the Alpha Jet.

Both the French Air Force and German Air Force procured the Alpha Jet in large numbers, the former principally as a trainer aircraft and the latter choosing to use it as a light attack platform. As a result of post-Cold War military cutbacks, Germany elected to retire its own fleet of Alpha Jets in the 1990s and has re-sold many of these aircraft to both military and civilian operators. The Alpha Jet has been adopted by a number of air forces across the world and has also seen active combat use by some of these operators.

The Alpha Jet is a light twin-engine aircraft equipped with an intentionally simple airframe despite the performance delivered. Both the leading edges and air intakes are fixed; while the aerodynamic shape of the aircraft, which was developed with the aid of computer-aided design, conforms with the area rule. Fully powered controls are used, comprising dual-hydraulic systems and load-factor limited dynamic feel system arrangement attached to conventional flight control surfaces. The cockpit is pressurised for greater comfort during training. The Alpha Jet is designed to accommodate ten-minute turnaround times with minimal ground equipment, using features such as pressurised single-point refuelling, ladder-less entering/egress of the cockpit, and a ten-hour endurance of the liquid oxygen system.

The Alpha Jet was designed to perform a diverse range of roles. The principal users of the type, Germany and France, operated their Alpha Jets in different capacities, the former as a ground attack platform and the latter as a trainer aircraft. Beyond performing different roles, the Alpha Jet fleets of France and Germany noticeably differed in their specification and equipment; German aircraft were fitted with a more extensive weapon-aiming system, a different fuel system, a yaw damper, different brakes, nosewheel steering, an arrester hook, and Stencel ejector seats in place of Martin-Baker. According to aerospace publication Flight International, the majority of the specialised equipment used on the ground attack-orientated variant of the Alpha Jet was provided by German firms. In addition to the ground attack role, the Luftwaffe also employed the Alpha Jet in the electronic countermeasures (ECM) and aerial reconnaissance roles; for the latter purpose, a reconnaissance pod could be fitted upon the port hardpoint.

The Alpha Jet is powered by a pair of SNECMA Turbomeca Larzac turbofan engines. It is a low bypass-ratio, the twin-spool engine that uses modular construction methods. The Larzac was a new engine at the time, having only performed its first run a year prior to being selected to power the Alpha Jet. The need for greater thrust to power the aircraft than the original model of the engine could generate led to the development and adoption of the 2,970 lb Larzac 04 in February 1972; it was this version of the engine that initially powered the Alpha Jet. Germany was interested in powering the type with the General Electric J85, but France objected to the use of an American engine which would result in US export restrictions upon the overall aircraft and agreed to assume the cost of developing the French-built Larzac. During the 1980s, an upgraded model of the Larzac engine which increased the thrust by 10 per cent was developed.

The avionics of the original version of the Alpha Jet was of an austere nature, partly to make it a simple and easily exportable aircraft. The basic type lacked features such as an autopilot, inertial navigation, or radar. Later upgrade programs would typically focus on the addition of a glass cockpit and other avionics systems. The Luftwaffe's Alpha Jets were equipped with additional avionics for the attack role, such as a Doppler radar and additional hardpoints. During the 1970s, Dornier claimed that the Alpha Jet outperformed aircraft used as the McDonnell Douglas F-4 Phantom II, LTV A-7 Corsair II, and the Fairchild Republic A-10 Thunderbolt II in the close air support role; the firms specifically stated that the Alpha Jet was smaller, faster, less vulnerable, more manoeuvrable, cheaper and had higher all-round performance than the A-10.

According to aerospace publication Flight International, the Alpha Jet was more complex than competing second-generation trainer aircraft, required seven man-hours of maintenance for every flight hour. Nearly 5,000lb of munitions and equipment may be carried upon a total of five hardpoints, four of these being located upon the wings and a single one at the centerline on the lower fuselage. In an armed configuration, a gun pod containing a 30 mm DEFA cannon (as installed on French aircraft) or a 27 mm Mauser BK-27 cannon (as installed on German aircraft) would typically be installed upon the centerline hardpoint.

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Lockheed P-38 Lightning

The Lockheed P-38 Lightning is an American single-seated, piston-engined fighter aircraft that was used during World War II. Developed for the United States Army Air Corps, the P-38 had distinctive twin booms and a central nacelle containing the cockpit and armament. Allied propaganda claimed it had been nicknamed the fork-tailed devil (German: der Gabelschwanz-Teufel) by the Luftwaffe and "two planes, one pilot" by the Japanese. Along with its use as a general fighter, the P-38 was used in various aerial combat roles, including as a highly effective fighter-bomber, a night fighter, and a long-range escort fighter when equipped with drop tanks. The P-38 was also used as a bomber-pathfinder, guiding streams of medium and heavy bombers; or even other P-38s, equipped with bombs, to their targets. Used in the aerial reconnaissance role, the P-38 accounted for 90% of the aerial film captured over Europe.

The P-38 was used most successfully in the Pacific Theater of Operations and the China-Burma-India Theater of Operations as the aircraft of America's top aces, Richard Bong (40 victories), Thomas McGuire (38 victories), and Charles H. MacDonald (27 victories). In the South-West Pacific Theater, the P-38 was the primary long-range fighter of United States Army Air Forces until the introduction of large numbers of P-51D Mustangs toward the end of the war.

Unusual for a fighter of this time, the exhaust was muffled by the turbosuperchargers, making the P-38's operation relatively quiet. The two turbosuperchargers also provided the P-38 with good high-altitude performance, making it one of the earliest Allied fighters capable of performing well at high altitudes. It was extremely forgiving and could be mishandled in many ways, but the rate of roll in the early versions was too low for it to excel as a dogfighter. The P-38 was the only American fighter aircraft in large-scale production throughout American involvement in the war, from Pearl Harbor to Victory over Japan Day. At the end of the war, orders for 1,887 more were cancelled.

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Chance Vought F4U-4 Corsair

The Vought F4U Corsair is an American fighter aircraft that saw service primarily in World War II and the Korean War. Designed and initially manufactured by Chance Vought, the Corsair was soon in great demand; additional production contracts were given to Goodyear, whose Corsairs were designated FG, and Brewster, designated F3A.

The Corsair was designed and operated as a carrier-based aircraft and entered service in large numbers with the U.S. Navy in late 1944 and early 1945. It quickly became one of the most capable carrier-based fighter-bombers of World War II. Some Japanese pilots regarded it as the most formidable American fighter of World War II and its naval aviators achieved an 11:1 kill ratio. Early problems with carrier landings and logistics led to it being eclipsed as the dominant carrier-based fighter by the Grumman F6F Hellcat, powered by the same Double Wasp engine first flown on the Corsair's first prototype in 1940. Instead, Corsair's early deployment was to land-based squadrons of the U.S. Marine Corps and U.S. Navy.

The Corsair served almost exclusively as a fighter-bomber throughout the Korean War and during the French colonial wars in Indochina and Algeria. In addition to its use by the U.S. and British, the Corsair was also used by the Royal New Zealand Air Force, French Naval Aviation, and other air forces until the 1960s.

From the first prototype delivery to the U.S. Navy in 1940 to the final delivery in 1953 to the French, 12,571 F4U Corsairs were manufactured in 16 separate models. Its 1942-1953 production run was the longest of any U.S. piston-engined fighter.

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North American P-51D Mustang

The North American Aviation P-51 Mustang is an American long-range, single-seat fighter and fighter-bomber used during World War II and the Korean War, among other conflicts. The Mustang was designed in April 1940 by a design team headed by James Kindelberger of North American Aviation (NAA) in response to a requirement of the British Purchasing Commission. The Purchasing Commission approached North American Aviation to build Curtiss P-40 fighters under license for the Royal Air Force (RAF). Rather than build an old design from another company, North American Aviation proposed the design and production of a more modern fighter. The prototype NA-73X airframe was rolled out on 9 September 1940, 102 days after the contract was signed, and first flew on 26 October.

The Mustang was designed to use the Allison V-1710 engine, which had limited high-altitude performance in its earlier variants. The aircraft was first flown operationally by the RAF as a tactical-reconnaissance aircraft and fighter-bomber (Mustang Mk I). Replacing the Allison with a Rolls-Royce Merlin resulted in the P-51B/C (Mustang Mk III) model, and transformed the aircraft's performance at altitudes above 15,000 ft (4,600 m) (without sacrificing range), allowing it to compete with the Luftwaffe's fighters. The definitive version, the P-51D, was powered by the Packard V-1650-7, a license-built version of the two-speed, two-stage-supercharged Merlin 66, and was armed with six .50 calibre (12.7 mm) AN/M2 Browning machine guns.

From late 1943, P-51Bs and P-51Cs (supplemented by P-51Ds from mid-1944) were used by the USAAF's Eighth Air Force to escort bombers in raids over Germany, while the RAF's Second Tactical Air Force and the USAAF's Ninth Air Force used the Merlin-powered Mustangs as fighter-bombers, roles in which the Mustang helped ensure Allied air superiority in 1944. The P-51 was also used by Allied air forces in the North African, Mediterranean, Italian, and Pacific theatres. During World War II, Mustang pilots claimed to have destroyed 4,950 enemy aircraft.

At the start of the Korean War, the Mustang, by then redesignated F-51, was the main fighter of the United States until jet fighters, including North American's F-86, took over this role; the Mustang then became a specialized fighter-bomber. Despite the advent of jet fighters, the Mustang remained in service with some air forces until the early 1980s. After the Korean War, Mustangs became popular civilian warbirds and air racing aircraft.

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Boeing PT-17 Stearman

The Stearman (Boeing) is a biplane formerly used as a military trainer aircraft, of which at least 10,626 were built in the United States during the 1930s and 1940s. Stearman Aircraft became a subsidiary of Boeing in 1934. Widely known as the Stearman, Boeing Stearman, or Kaydet, it served as a primary trainer for the United States Army Air Forces, the United States Navy (as the NS and N2S), and with the Royal Canadian Air Force as the Kaydet throughout World War II. After the conflict was over, thousands of surplus aircraft were sold on the civilian market. In the immediate postwar years, they became popular as crop dusters and sports planes, and for aerobatic and wing walking use in air shows.

The Kaydet was a conventional biplane of rugged construction, with a large, fixed tailwheel undercarriage, and accommodation for the student and instructor in open cockpits in tandem. The radial engine was usually not cowled, although some Stearman operators choose to cowl the engine, most notably the Red Baron Stearman Squadron.

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Fairchild PT-19

The Fairchild PT-19 (company designation Fairchild M62) is an American Fairchild Aircraft monoplane primary trainer aircraft that served with the United States Army Air Forces, RAF and RCAF during World War II. It was a contemporary of the Kaydet biplane trainer and was used by the USAAF during Primary Flying Training. As with other USAAF trainers of the period, the PT-19 had multiple designation(s) based on the powerplant installed.

The PT-19 series was developed from the Fairchild M-62 when the USAAC first ordered the aircraft in 1940 as part of its expansion program. The cantilever low-wing monoplane with fixed landing gear and tailwheel design was based on a two-place, tandem-seat, open cockpit arrangement. The simple but rugged construction included a fabric-covered welded steel tube fuselage. The remainder of the aircraft used plywood construction, with a plywood-sheathed centre section, outer wing panels and tail assembly. The use of an inline engine allowed for a narrow frontal area which was ideal for visibility while the widely set-apart fixed landing gear allowed for solid and stable ground handling.

The M-62 first flew in May 1939 and won a fly-off competition later that year against 17 other designs for the new Army training airplane. Fairchild was awarded its first Army PT contract for an initial order on 22 September 1939.

The original production batch of 275 was powered by the inline 175 hp Ranger L-440-1 engine and designated the PT-19. In 1941, mass production began and 3,181 of the PT-19A model, powered by the 200 hp L-440-3, were made by Fairchild. An additional 477 were built by Aeronca and 44 by the St. Louis Aircraft Corporation. The PT-19B, of which 917 were built, was equipped for instrument flight training by attaching a collapsible hood to the front cockpit

When a shortage of engines threatened production, the PT-23 model was introduced which was identical except for the 220 hp Continental R-670 radial powerplant. A total of 869 PT-23s were built as well as 256 of the PT-23A, which was the instrument flight-equipped version. The PT-23 was manufactured in the US by Fairchild, Aeronca, St. Louis Aircraft Corporation and Howard Aircraft Corporation and in Canada by Fleet Aircraft Corporation as well as Fabrica do Galeao in Brazil (220 or 232 between 1944 and 1948).

During 1943, USAAF Training Command received a number of complaints about durability issues with the plywood wings of the PT-19 and the PT-23 when exposed to the high heat and/or humidity of training bases located in Texas and Florida. Maintenance officers at the USAAF overhaul depots had been forced to order replacement of the wooden wing sections after only two to three months' active service because of wood rot and ply separation issues. Subsequent to this incident, the USAAF incorporated a demand for all-metal wing sections on all future fixed-wing training aircraft.

The final variant was the PT-26 which used the L-440-7 engine. The Canadian-built versions of these were designated the Cornell for use by the British Commonwealth Air Training Plan which was centered in Canada.

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Cessna 208 Amphibian “Caravan”

The Cessna 208 Caravan is a utility aircraft produced by Cessna. The project was commenced on November 20, 1981, and the prototype first flew on December 9, 1982. The production model was certified by the FAA in October 1984 and its Cargomaster freighter variant was developed for FedEx. The 4 ft (1.2 m) longer 208B Super Cargomaster first flew in 1986 and was developed into the passenger 208B Grand Caravan.

The strutted, high wing 208 typically seats nine passengers in its unpressurized cabin, is powered by a single Pratt & Whitney Canada PT6A tractor turboprop and has a fixed tricycle landing gear, floats or skis. By November 2017, 2,600 have been delivered and 20 million flight hours logged. Caravans are used for flight training, commuter airlines, VIP transport, air cargo and humanitarian missions.

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Pilatus PC-6 Porter

The Pilatus PC-6 Porter is a single-engined STOL utility aircraft designed by Pilatus Aircraft of Switzerland. First flown in 1959, the PC-6 was produced at Pilatus Flugzeugwerke in Stans, Switzerland. It has been built in both piston engine- and turboprop-powered versions, and was produced under licence for a time by Fairchild Hiller in the United States. After around 600 deliveries in six decades, Pilatus produced the last one in early 2019.

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Cessna 337 Skymaster

The Cessna Skymaster is an American twin-engine civil utility aircraft built in a push-pull configuration. Its engines are mounted in the nose and rear of its pod-style fuselage. Twin booms extend aft of the wings to the vertical stabilizers, with the rear engine between them. The horizontal stabilizer is aft of the pusher propeller, mounted between and connecting the two booms. The combined tractor and pusher engines produce centerline thrust and a unique sound.

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Aviat Husky

The Aviat Husky is a tandem two-seat, high-wing, utility light aircraft built by Aviat Aircraft of Afton, Wyoming. It is the only all-new light aircraft that was designed and entered series production in the United States in the mid-to-late 1980s. The Husky features a braced high wing, tandem seating and dual controls. The structure is steel tube frames and Dacron covering over all but the rear of the fuselage, plus metal leading edges on the wings. The high wing was selected for good all-around visibility, making the Husky ideal for observation and patrol roles. Power is supplied by a relatively powerful (for the Husky's weight) 180 hp (134 kW) Textron Lycoming O-360 flat-four piston engine turning a constant speed propeller. In 2015 a reversible MT Propeller was approved under a Supplementary Type Certificate for better control during floatplane water operations. The Husky's high power-to-weight ratio and low wing loading result in good short-field performance. Options include floats, skis and banner and glider tow hooks.

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Beechcraft T-34 Mentor

The Beechcraft T-34 Mentor is an American propeller-driven, single-engined, military trainer aircraft derived from the Beechcraft Model 35 Bonanza. The earlier versions of the T-34, dating from around the late 1940s to the 1950s, were piston-engined. These were eventually succeeded by the upgraded T-34C Turbo-Mentor, powered by a turboprop engine. The T-34 remains in service more than seven decades after it was first designed.

The T-34 was the brainchild of Walter Beech, who developed it as the Beechcraft Model 45 private venture at a time when there was no defence budget for a new trainer model. Beech hoped to sell it as an economical alternative to the North American T-6/SNJ Texan, then in use by all services of the U.S. military.

Three initial design concepts were developed for the Model 45, including one with the Bonanza's signature V-tail, but the final design that emerged in 1948 incorporated conventional tail control surfaces for the benefit of the more conservative military (featuring a relatively large unswept vertical fin that would find its way onto the Travel Air twin-engine civil aircraft almost ten years later). Bonanza's fuselage with a four-passenger cabin was replaced with a narrower fuselage incorporating a two-seater tandem cockpit and bubble canopy, which provided greater visibility for the trainee pilot and flight instructor. Structurally, the Model 45 was much stronger than the Bonanza, being designed for +10g and −4.5g, while the Continental E-185 engine of 185 horsepower (hp) at takeoff (less than a third of the power of the T-6's engine) was the same as that fitted to contemporary Bonanzas

Following the prototype were three Model A45T aircraft, the first two with the same engine as the prototype and the third with a Continental E-225, which would prove to be close to the production version. Production did not begin until 1953 when Beechcraft began delivering T-34As to the United States Air Force (USAF) and similar Model B45 aircraft for export. Production of the T-34B for the United States Navy (USN) began in 1955, this version featuring a number of changes reflecting the different requirements of the two services. The T-34B had only differential braking for steering control on the ground instead of nosewheel steering, additional wing dihedral and, to cater for the different heights of pilots, adjustable rudder pedals instead of the moveable seats of the T-34A. T-34A production was completed in 1956, with T-34Bs being built until October 1957 and licensed B45 versions built in Canada (125 manufactured by Canadian Car and Foundry), Japan (173 built by Fuji Heavy Industries), and Argentina (75 by FMA) until 1958. Beechcraft delivered the last Model B45s in 1959. Total production of the Continental-engined versions in the US and abroad was 1,904 aircraft.

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Sukhoi Su-29

The Sukhoi Su-29 is a Russian two-seat aerobatic aircraft with a 268 kW (360 hp) radial engine. It was designed based on the Su-26 and inherited most of the design and technical features of its predecessor. Due to wide use of composite materials, which make up as much as 60% of the Su-29's aircraft structure, the empty weight is increased by only 50 kg (110 lb) over the single-seat Su-26's empty weight.

The Su-29 is used for initial pilot aerobatics education, flight training, and participation of pilots in aerobatics competitions and air shows, as well as for maintaining flight skills of military and civil pilots.

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Extra 300L

The Extra 300L is a Lycoming AEIO-540-powered two-seat aircraft, with a low-mounted wing and shorter fuselage. More Extra 300L ("L" is a two-seater version) aircraft have been produced than any other model. Its wing is mounted at the bottom of the fuselage, with its span reduced from 26 to 24 ft (7.9 to 7.3 m). Improved ailerons boost the 300L's roll rate to 400° per second. All 300Ls are fully certified under FAA and European Joint Aviation Authorities regulations. The design of the Extra 300 was based on the Extra 230, an early 1980s monoplane having a wing made of wood. The Extra 300 has a welded steel tube fuselage covered in aluminium and fabric. The midset wing has a carbon fibre composite spar and carbon composite skins. A symmetrical airfoil, mounted with a zero angle of incidence, provides equal performance in both upright and inverted flight. The landing gear is fixed taildragger style with composite main legs and fibreglass wheel pants. The powerplant is a fuel-injected Lycoming AEIO-540 which produces 300 horsepower (224 kW). The first two-seat Extra 300 made its maiden flight on 6 May 1988, with German type certification following on 16 May 1990. The single-seat Extra 300S flew on 4 March 1992. The Extra 300 is stressed for ±10 G with one person on board and ±8 G with two. Some Extra 300s are certified in the experimental category in the U.S., while others are certified in the aerobatic category.

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North American T-6 Texan

The North American Aviation T-6 Texan is an American single-engined advanced trainer aircraft used to train pilots of the United States Army Air Forces (USAAF), United States Navy, Royal Air Force, Royal Canadian Air Force and other air forces of the British Commonwealth during World War II and into the 1970s. Designed by North American Aviation, the T-6 is known by a variety of designations depending on the model and operating air force. The United States Army Air Corps (USAAC) and USAAF designated it as the AT-6, the United States Navy the SNJ, and British Commonwealth air forces the Harvard, the name by which it is best known outside the US. Starting in 1948, the new United States Air Force (USAF) designated it the T-6, with the USN following in 1962. It remains a popular warbird used for airshow demonstrations and static displays. It has also been used many times to simulate various historical aircraft, including the Japanese Mitsubishi A6M Zero. A total of 15,495 T-6s of all variants were built.

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Honda HA-420 HondaJet

The Honda HA-420 HondaJet is a light business jet produced by the Honda Aircraft Company of Greensboro, North Carolina, United States. Original concepts of the aircraft started in 1997 and were completed in 1999. It took its maiden flight on December 3, 2003, received its FAA type certificate in December 2015 and was first delivered that same month. By March 2020, 150 jets had been delivered.

The seven- to eight-seat aircraft has a composite fuselage and an aluminum wing, and is powered by two GE Honda HF120 turbofans unusually mounted on pylons above the wing. It can reach a 420 kn (780 km/h) speed, and has a 1,400 nmi (2,600 km) range. The HondaJet has received several aeronautic design and innovation accolades.

The HondaJet is a low-wing monoplane that uses a composite fuselage and an aluminum wing. It belongs to the very light jet category.

It uses two engines mounted on pylons above the wing, a configured called Over-The-Wing Engine Mount, or OTWEM, by Honda Aircraft. This configuration maximizes cabin space by removing the structure required to mount engines on the rear of the fuselage. A similar over-wing engine configuration was used in the 1970s on the VFW-Fokker 614, but had limited the aircraft’s speed due to interference between the engine and the wing. This, along with the overall commercial failure of the VFW-Fokker 614, made the over-wing configuration unpopular with aircraft designers. To avoid these issues, the HondaJet’s designer used computer analysis and wind tunnel testing to find the optimal position for engine placement on top of the wings, which he determined was at 75 percent of the wing chord. The HondaJet’s engines are positioned in such a way that the airflow over the wing is superimposed with the airflow around the engine to minimize wave drag at high speed. The HondaJet designer calls this “favorable interference.” This configuration not only eliminated the problems associated with earlier over-wing engine mounts, but actually reduced wave drag compared to a conventional rear-fuselage mounted configuration. OTWEM configuration is often named the most unusual feature of the HondaJet.

The nose and wing are designed for laminar flow, and the main fuselage has a constant profile, making an eventual stretch easier. The combination of engine placement, wing and fuselage was achieved using computer simulations and wind tunnels. HondaJet has a retractable tricycle landing gear with both main and nose landing gear single-wheeled.

The aircraft is powered by two GE Honda HF120 turbofans, developed with GE Aviation under the GE-Honda partnership. Honda began developing its own small turbofan engine, the HF118, in 1999, leading to the HF120. The HF120 was test-flown on a Cessna Citation CJ1. The engine features a single fan, a two-stage compressor and a two-stage turbine. The GE Honda HF120 received FAA type certification on 13 December 2013, and production certification in 2015.

Honda claims that the combination of lightweight materials, aerodynamics and efficient engines gave the HondaJet up to 20% better fuel efficiency than similar aircraft. In 2019, Business & Commercial Aviation reported that for a 1,000 nmi (1,852 km) 4-passenger mission HondaJet Elite uses 1,872 lb (849 kg) of fuel, compared to 1,919 lb (870 kg) (3% more) for the Phenom 100EV, and to 2,018 lb (915 kg) (8% more) for the Citation M2; for a 300 nmi (556 km) mission the numbers become 679 lb (308 kg), 753 lb (342 kg) (11% more), and 804 lb (365 kg) (18% more) respectively

The interior dimensions are 17.80 ft (5.43 m) long, 5.00 ft (1.52 m) wide, and 4.83 ft (1.47 m) high, while the cabin is 12.1 ft (3.7 m) long besides the enclosed lavatory. Total interior volume is 324 cu ft (9.2 m3), and luggage capacity is 66 cu ft (1.9 m3). The aircraft is equipped with a touchscreen 3-display Garmin G3000 glass cockpit system.

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Dassault Falcon 900EX

Dassault Falcon 900EX is a long-range version of the original Dassault Falcon 900 French-built corporate trijet aircraft made by Dassault Aviation, with 22.24 kN (5,000 lbf) engines. This variant features TFE731-60 engines and can store more fuel to give an increased range of 8,340 km (4,501 nm; 5,180 miles). Improved avionics (Honeywell Primus).

The Falcon 900 is a development of the Falcon 50, itself a development of the earlier Falcon 20. The Falcon 900 design incorporates composite materials and an S-duct to feed the central engine.

Improved models include the Falcon 900-B, featuring improved engines and increased range, and the Falcon 900EX featuring further improvements in engines and range and an all-glass flight deck. The Falcon 900C is a lower-cost companion to the Falcon 900EX and replaces the Falcon 900B. Later versions are the Falcon 900EX EASy and the Falcon 900DX. At EBACE 2008, Dassault announced another development of the 900 series: the Falcon 900LX, incorporating high Mach blended winglets designed by Aviation Partners Inc. The same winglets are certified for the entire Falcon 900 series as a retrofit kit.

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North American T-28B Trojan

The North American Aviation T-28 Trojan is a radial-engined military trainer aircraft used by the United States Air Force and the United States Navy beginning in the 1950s. Besides its use as a trainer, the T-28 was successfully employed as a counter-insurgency aircraft, primarily during the Vietnam War. It has continued in civilian use as an aerobatics and Warbird performer.

On September 24, 1949, the XT-28 (company designation NA-159) was flown for the first time, designed to replace the T-6 Texan. The T-28A arrived at the Air Proving Ground, Eglin Air Force Base, Florida, in mid-June 1950, for suitability tests as an advanced trainer by the 3200th Fighter Test Squadron, with consideration given to its transition, instrument, and gunnery capabilities. Found satisfactory, a contract was issued and between 1950 and 1957, a total of 1,948 were built.

Following the T-28's withdrawal from U.S. military service, a number were remanufactured by Hamilton Aircraft into two versions called the Nomair. The first refurbished machines, designated T-28R-1 were similar to the standard T-28s they were adapted from and were supplied to the Brazilian Navy. Later, a more ambitious conversion was undertaken as the T-28R-2, which transformed the two-seat tandem aircraft into a five-seat cabin monoplane for general aviation use. Other civil conversions of ex-military T-28As were undertaken by PacAero as the Nomad Mark I and Nomad Mark II

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