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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]
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.
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 ]
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)
The Cessna 172 is a four-seat aircraft. At maximum weight it has a V Y of 75 kn (139 km/h) indicated airspeed [ 4 ] providing a rate of climb of 721 ft/min (3.66 m/s). Rate of climb at maximum power for a small aircraft is typically specified in its normal operating procedures but for large jet airliners it is usually mentioned in emergency ...
A headwind will reduce the ground speed needed for takeoff, as there is a greater flow of air over the wings. Typical takeoff air speeds for jetliners are in the range of 240–285 km/h (130–154 kn; 149–177 mph). Light aircraft, such as a Cessna 150, take off at around 100 km/h (54 kn; 62 mph). Ultralights have even lower takeoff speeds.
Tens of thousands of Social Security Administration staffers can continue teleworking into 2029 under a recent deal signed between their union and the agency.
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 ...
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