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The Cessna 172 Skyhawk is an American four-seat, single-engine, high wing, fixed-wing aircraft made by the Cessna Aircraft Company. [2] First flown in 1955, [2] more 172s have been built than any other aircraft. [3] It was developed from the 1948 Cessna 170 but with tricycle landing gear rather than conventional landing gear.
Most general aviation aircraft retain this short-field performance; the Cessna 172, the most produced aircraft in history, will take off in as little as 805 feet (245 m) at Standard Temperature when fully loaded. [5]
Max take-off weight, full power Boeing 747-8: 0.269 Max take-off weight, full power Boeing 777: 0.285 Max take-off weight, full power (777-200ER) Boeing 737 MAX 8: 0.311 Max take-off weight, full power Airbus A320neo: 0.310 Max take-off weight, full power Boeing 757-200: 0.341 Max take-off weight, full power (w/Rolls-Royce RB211) Tupolev 154B ...
Data from Global Security [better source needed] General characteristics Crew: one Capacity: three passengers Length: 26 ft 11 in (8.20 m) Wingspan: 35 ft 10 in (10.92 m) Height: 8 ft 10 in (2.69 m) Wing area: 159 sq ft (14.8 m 2) Empty weight: 1,363 lb (618 kg) Gross weight: 2,500 lb (1,134 kg) Powerplant: 1 × Continental IO-360-D 6-cylinder air-cooled horizontally-opposed piston engine, 210 ...
Lift and drag are the two components of the total aerodynamic force acting on an aerofoil or aircraft.. In aerodynamics, the lift-to-drag ratio (or L/D ratio) is the lift generated by an aerodynamic body such as an aerofoil or aircraft, divided by the aerodynamic drag caused by moving through air.
An overweight take-off typically requires an exceptionally long runway. Overweight operations are not permitted with passengers aboard. Many smaller aircraft have a maximum landing weight that is the same as the maximum take-off weight, in which case issues of overweight landing due to excess fuel being on board cannot arise.
Converted Cessna Skymaster. [11] De Havilland Canada DHC-2 Beaver Mk 1: Canada 1947 Transport Production 1,015 ft (309 m) 1,000 ft (305 m) [12] De Havilland Canada DHC-2 Beaver Mk III: Canada 1947 Transport Production 920 ft (280 m) 870 ft (265 m) [12] De Havilland Canada DHC-3 Otter: Canada 1951 Transport Production 1,155 ft (352 m)
In discussions of the takeoff performance of military aircraft, the term V ref stands for refusal speed. Refusal speed is the maximum speed during takeoff from which the air vehicle can stop within the available remaining runway length for a specified altitude, weight, and configuration. [ 19 ]
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