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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.
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
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 ...
Currently the largest plane based on the number of passengers it can transport, the Airbus A380 seats well more than 500 passengers on two full decks of this megaplane. Airbus, a subsidiary of ...
Last Wednesday, Delta Air Lines announced that it had placed an order for 40 new Airbus aircraft: 10 A330 widebody aircraft, and 30 A321 narrowbody aircraft. These new planes will be used to ...
Since 2013, Delta has been working to reduce the age of its fleet by purchasing or leasing newly built aircraft or newer model used aircraft. [citation needed] Since launching the effort, Delta has preferred to purchase aircraft from Airbus, a major change for the company which had been a loyal customer of Boeing and McDonnell Douglas (which merged with Boeing in 1997).
World's largest operator of the A380. Etihad Airways: 2014 2017 7 3 Korean Air: 2011 2014 7 3 To be retired by 2026. [3] Lufthansa: 2010 2015 8 6 To be retired after 2030. [4] Qantas: 2008 2011 10 2 To be replaced with the Airbus A350-1000 from 2032. [5] Qatar Airways: 2014 2018 8 2 To be replaced with the Airbus A350-1000 from 2028. Singapore ...
As stalling is due to wing loading and maximum lift coefficient at a given altitude and speed, this limits the turning radius due to maximum load factor. At Mach 0.85 and 0.7 lift coefficient, a wing loading of 50 lb/sq ft (240 kg/m 2 ) can reach a structural limit of 7.33 g up to 15,000 feet (4,600 m) and then decreases to 2.3 g at 40,000 feet ...