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The $10–12 million jet would be the longest-range single-pilot business aircraft, it would keep the HondaJet configuration, stretched from 42.6 to 57.8 ft (13.0 to 17.6 m), and has a 56.7 ft (17.3 m) wingspan, 16 ft (4.9 m) larger, for a maximum takeoff weight of 17,500 lb (7,900 kg) and a 3,300 ft (1,000 m) takeoff distance, while its ...
Maximum structural cruising speed or maximum speed for normal operations. Speed at which exceeding the limit load factor may cause permanent deformation of the aircraft structure. [7] [8] [9] [24] V O: Maximum operating maneuvering speed. [25] V R: Rotation speed. The speed at which the pilot begins to apply control inputs to cause the aircraft ...
As of 2020, more Learjet 35s have been sold than any other Learjet aircraft. [4] As a private jet the Learjet 35 was popular because of its good range (it can fly 2,056 miles nonstop), takeoff and landing performance (its Honeywell engines provide 3,500 pounds of thrust and can land on short runways at regional airports), fast cruise ...
Powered aircraft range is limited by the aviation fuel energy storage capacity (chemical or electrical) considering both weight and volume limits. [1] Unpowered aircraft range depends on factors such as cross-country speed and environmental conditions. The range can be seen as the cross-country ground speed multiplied by the maximum time in the ...
Piper estimated that this engine would get the Altaire up to a 35,000 feet (11,000 m) maximum cruise altitude and a 320 knot cruise speed. Maximum cruise speed was projected to be 360 knots. The aircraft was expected to have a 1,200-to-1,300-nautical-mile (2,200 to 2,400 km) non-stop range.
More than private jets. The Boeing Business Jet (BBJ) range was developed in the late 1990s to produce dedicated corporate jets based on the Boeing 737, explains Gary Crichlow, an aviation analyst ...
The G700 is considered the premier long-range business jet, able to hit Mach 0.925, around 710 miles per hour. It sports a length of nearly 110 feet and a wingspan of 103 feet.
The minimum control speed is the airspeed below which the force the rudder or ailerons can apply to the aircraft is not large enough to counteract the asymmetrical thrust at a maximum power setting. Above this speed it should be possible to maintain control of the aircraft and maintain straight flight with asymmetrical thrust. [4]