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The A380-800 layout with 519 seats displayed (16 First, 92 Business and 411 Economy) The Airbus A380 features two full-length decks, each measuring 49.9 metres (164 ft). The upper deck has a slightly shorter usable length of 44.93 metres (147.4 ft) due to the front fuselage curvature and the staircase.
The Airbus A380 is a very large wide-body airliner, developed and produced by Airbus. It is the world's largest passenger airliner and the only full-length double-deck jet airliner. Airbus studies started in 1988, and the project was announced in 1990 to challenge the dominance of the Boeing 747 in the long-haul market. The then-designated A3XX ...
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The change was partly prompted by the development of the Airbus A380. [17] [18] The previous three wake turbulence categories were increased to six, by splitting Medium and Heavy into pairs, and adding a Super Heavy category for the Airbus A380. [19] Capacity gains of up to 8% were achieved. [17]
The size of RMS Titanic compared with a human, car, bus, and an Airbus A380. The following is a list of the largest passenger vehicles with consumer availability in history. Overall
By comparison the LZ 18 airship, which flew the same year, was 158 metres (518 ft) long (the envelope had a capacity of 270,000 m 3 (9,500,000 cu ft)) and an empty weight of 20 tonnes. The Beardmore Inflexible of 1928 had a wingspan of 157 ft 6 in (48.01 m) and an all up weight of 37,000 lbs. However, it was underpowered for such a heavy aircraft.
Airbus A340-300 Enhanced: 0.2229 Max take-off weight, full power Airbus A380: 0.227 Max take-off weight, full power Boeing 747-8: 0.269 Max take-off weight, full power Boeing 777-200ER: 0.285 Max take-off weight, full power Boeing 737 MAX 8: 0.311 Max take-off weight, full power Airbus A320neo: 0.310 Max take-off weight, full power Boeing 757 ...
Droop flaps function with other high-lift devices on an aircraft to increase the camber of the wing and reduce the stalling speed.On the Airbus A380, the first stage of lift device selection deploys the droop flaps (called droop noses by Airbus) and leading-edge slats located further out on the wing; with the main flaps starting to extend when the second stage is selected.