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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] When the runway length is equal to the balanced field length only one value for V 1 will exist.
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]
Take-off to 50 ft (15 m) Landing from 50 ft (15 m) Notes AAC Angel: US 1984 Utility Production 1,404 ft (428 m) 1,046 ft (319 m) [1] Aircraft Industries L 410 NG: Czech Republic 2015 Utility Production 1,936 ft (590 m) 1,969 ft (600 m) [2] Antonov An-14: Soviet Union 1958 Transport Production 656 ft (200 m) 985 ft (300 m) [3] Antonov An-72
The following illustration is an example of interpolating information from a takeoff distance chart: Model estimation for a wide range of atmospheric conditions, flight and engine parameters. Preparation and Validation of charts and tables from model estimation to predict the aircraft performance.
The DC-9's takeoff weight was limited to 80,000 lb (36,300 kg) for a two-person flight crew by the then-Federal Aviation Agency regulations at the time. [2] The commercial passenger aircraft have five abreast layout for economy seating that can accommodate 80 to 135 passengers, depending on version and seating arrangement.
Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch
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.
STOL is an acronym for short take-off and landing, aircraft with very short runway requirements, typically between 2,000 feet (610 m) to 3,500 feet (1,100 m). [2]