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Black Eagles: South Korea: Republic of Korea Air Force: KAI T-50B Golden Eagle: 1953: Black Falcons: New Zealand: Royal New Zealand Air Force: Beechcraft T-6 Texan II: 2000: Black Knights: Singapore: Republic of Singapore Air Force: General Dynamics F-16C Fighting Falcon: 1973: Blue Angels: United States: United States Navy: Boeing F/A-18E/F ...
T4 powered by a 150 hp Lycoming O-320-E1A – fixed-pitch propeller T5 powered by a 150 hp Lycoming O-320-E1A – constant speed propeller T6 initially a small run of 4 aircraft for the RNZAF, powered by a 150 hp Lycoming O-320-E1A – constant speed propeller with gross weight increased from T-5, and with a 24 volt electrical system.
The 100th aircraft was delivered in October 2005 and the 150th in May 2008. Piaggio reported that, as of October 2010, the Avanti and Avanti II fleets had logged over 500,000 flying hours. [23] An improved Avanti II obtained European and U.S. certification in November 2005. Six months later, 70 planes had been ordered, including 36 by Avantair.
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The PC-21 is powered by a single Pratt & Whitney Canada PT6A-68B turboprop engine of 1,600 shaft horse power, which drives a five-bladed graphite scimitar propeller manufactured by Hartzell; [3] [8] it has been claimed by Pilatus that the PC-21 possesses speed and climb rates previously normally performed only by jet-powered aircraft. [15]
A pusher aircraft is a type of aircraft using propellers placed behind the engines and may be classified according to engine/propeller location and drive as well as the lifting surfaces layout (conventional or 3 surface, canard, joined wing, tailless and rotorcraft), Some aircraft have a Push-pull configuration with both tractor and pusher engines.
The Piper PA-44 Seminole is an American twin-engined light aircraft manufactured by Piper Aircraft. [2] The PA-44 is a development of the Piper Cherokee single-engined aircraft and is primarily used for multi-engined flight training. [2] [3] The Seminole has been built in three production runs; from 1979 to 1982, 1989 to 1990, and continuously ...
The Blackwing is the result of a research project commenced in the 1990s, culminating in wind tunnel tests and a 350-hour prototype flight test program. It was designed to comply with the Fédération Aéronautique Internationale microlight rules with a version at a gross weight of 472.5 kg (1,042 lb) and US light-sport aircraft rules with a version with a gross weight of 600 kg (1,323 lb).