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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.
V 1 also means the minimum speed in the takeoff, following a failure of the critical engine at V EF, at which the pilot can continue the takeoff and achieve the required height above the takeoff surface within the takeoff distance." [7] V 1 thus includes reaction time. [26]
The speed will ensure the aircraft achieves the required height above the takeoff surface within the takeoff distance. [citation needed] To achieve a balanced field takeoff, V 1 is selected so the take-off distance with one engine inoperative, and the accelerate-stop distance, are equal. [1]
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 ...
Data from Jane's All The World's Aircraft 1982-83 General characteristics Crew: 1 Capacity: 3 pax Length: 7.24 m (23 ft 9 in) Wingspan: 9.986 m (32 ft 9 in) Height: 2.77 m (9 ft 1 in) Wing area: 13.4 m 2 (144 sq ft) Aspect ratio: 7.45 Airfoil: NACA 63A515 Empty weight: 600 kg (1,323 lb) Max takeoff weight: 990 kg (2,183 lb) Fuel capacity: 162 L (43 US gal; 36 imp gal) fuel ; 7.5 L (2 US gal; 2 ...
However, typical daytime VFR minimums for most airspace is 3 statute miles of flight visibility and a distance from clouds of 500 feet below, 1,000 feet above, and 2,000 feet horizontally. [4] Flight conditions reported as equal to or greater than these VFR minimums are referred to as visual meteorological conditions (VMC).
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