fuselage
Overview The A380 was initially offered in two models: the
A380-800 and the
A380F. The A380-800's original configuration carried 555 passengers in a
three-class configuration or 853 passengers (538 on the main deck and 315 on the upper deck) in a single-class economy configuration. In May 2007, Airbus began marketing a configuration with 30 fewer passengers (525 total in three classes) – traded for more range – to better reflect trends in premium-class accommodation. The design range for the A380−800 model is ; capable of flying from Hong Kong to New York or from Sydney to
Istanbul non-stop. The A380 is designed for 19,000 cycles. The second model, the
A380F freighter, would have carried of cargo over a range of . Freighter development was put on hold as Airbus prioritised the passenger version, and all orders for freighters were cancelled. Other proposed variants included an
A380-900 stretchseating about 656 passengers (or up to 960 passengers in an all-economy configuration)and an extended-range version with the same passenger capacity as the A380-800. The Trent 900 is a combination of the fan and scaled compressor of the 777-200X/300X
Trent 8104 technology demonstrator derived from the Boeing 777's
Trent 800, and the Airbus A340-500/600's
Trent 500 core. Due to its modern engines and aerodynamic improvements, Lufthansa's A380s produce half the noise of the Boeing 747-200 while carrying 160 more passengers. In 2012, the A380 received an award from the
Noise Abatement Society.
London Heathrow is a key destination for the A380. Field measurements suggest the approach quota allocation for the A380 may be excessively generous compared to the older Boeing 747, but still quieter. Rolls-Royce is supporting the CAA in understanding the relatively high A380/Trent 900 monitored noise levels. Due to Heathrow's landing charges having a noise component, the A380 is cheaper to land there than a Boeing 777-200 and -300 and it saves $4,300 to $5,200 (2017 prices) per landing, or $15.3M to $18.8M (2017 prices) of
present value over 15 years.
Tokyo Narita has a similar noise charge. The A380 has
thrust reversers on the inboard engines only. The outboard engines lack them, reducing the amount of debris stirred up during landing. The combination of wheel braking and large spoilers and flaps reduces the aircraft's reliance on thrust reversal. Having reversers on only two engines also saves a great deal of maintenance expense for operators as well as avoiding unnecessary weight to the outboard engines. The optimal wingspan for such an MTOW is about but airport restrictions of force the A380 to compensate with a longer
chord for an
aspect ratio of 7.8. by about 10% and increases
operating costs several per cent, considering fuel costs constitute about 50% of the cost of long-haul aeroplane operation. The common wing design approach sacrifices fuel efficiency on the A380-800 passenger model in particular because its lower MTOW allows for a higher aspect ratio with a shorter chord or thinner wing. Still, Airbus estimated that the A380's size and advanced technology would provide lower operating costs per passenger than the 747-400. The wings incorporate
wingtip fences that extend above and below the wing surface, similar to those on the
A310 and
A320. These increase fuel efficiency and range by reducing
induced drag. The wingtip fences also reduce
wake turbulence, which endangers following aircraft. The wings of the A380 were designed in
Filton, England and
Wichita, US, with its manufacturing in Broughton in the United Kingdom. The wings were then transported to the harbour of Mostyn, where they were transported by barge to Toulouse, France, for integration and final assembly with the rest of the aircraft and its components. Singapore Airlines describes the A380's landing speed of as "impressively slow".
Materials While most of the fuselage is made of aluminium alloys,
composite materials comprise more than 20% of the A380's
airframe.
Carbon-fibre reinforced plastic,
glass-fibre reinforced plastic and
quartz-fibre reinforced plastic are used extensively in wings, fuselage sections (such as the undercarriage and rear end of fuselage), tail surfaces, and doors. The A380 is the first commercial airliner to have a central wing box made of carbon–fibre reinforced plastic. It is also the first to have a smoothly contoured wing cross–section. The wings of other commercial airliners are partitioned span-wise into sections. This flowing continuous cross section reduces aerodynamic drag.
Thermoplastics are used in the leading edges of the
slats. The hybrid fibre metal laminate material
GLARE (glass laminate aluminium reinforced epoxy) is used in the upper fuselage and on the stabilisers' leading edges. This aluminium-
glass-fibre laminate is lighter and has better corrosion and impact resistance than conventional aluminium
alloys used in aviation. Unlike earlier composite materials, GLARE can be repaired using conventional aluminium repair techniques. Newer
weldable aluminium alloys are used in the A380's airframe. This enabled the widespread use of
laser beam welding manufacturing techniques, eliminating rows of
rivets and resulting in a lighter, stronger structure. High-strength aluminium (type 7449) reinforced with carbon fibre was used in the wing brackets of the first 120 A380s to reduce weight, but cracks were discovered and newer sets of the more critical brackets are made of standard
aluminium 7010, increasing weight by 90kg (198lb). Repair costs for earlier aircraft were expected to be around €500million (US$629million). It takes of paint to cover the exterior of an A380. The paint is five layers thick and weighs about 650kg (1,433lb) when dry.
Avionics The A380 employs an
integrated modular avionics (IMA) architecture, first used in advanced military aircraft, such as the
Lockheed Martin F-22 Raptor,
Lockheed Martin F-35 Lightning II, and
Dassault Rafale. The main IMA systems on the A380 were developed by the
Thales Group. The data networks use
Avionics Full-Duplex Switched Ethernet, an implementation of ARINC 664. These are switched,
full-duplex,
star-topology and based on
100baseTX fast-Ethernet. This reduces the amount of wiring required and minimises
latency. Airbus used similar cockpit layout, procedures and handling characteristics to other Airbus aircraft, reducing crew training costs. The A380 has an improved
glass cockpit, using
fly-by-wire flight controls linked to
side-sticks. The cockpit has eight
liquid crystal displays, all physically identical and interchangeable; comprising two
primary flight displays, two navigation displays, one engine parameter display, one system display and two
multi-function displays. The MFDs were introduced on the A380 to provide an easy-to-use interface to the
flight management system – replacing three multifunction control and display units. They include
QWERTY keyboards and trackballs, interfacing with a
graphical "
point-and-click" display system. The Network Systems Server (NSS) is the heart of A380s paperless cockpit; it eliminates bulky manuals and traditional charts. The NSS has enough inbuilt robustness to eliminate onboard backup paper documents. The A380s network and server system stores data and offers electronic documentation, providing a required equipment list, navigation charts, performance calculations, and an aircraft logbook. This is accessed through the MFDs and controlled via the keyboard interface. They have self-contained hydraulic and electrical power supplies.
Electro-hydrostatic actuators (EHA) are used in the
aileron and
elevator, electric and hydraulic motors to drive the slats as well as electrical backup hydrostatic actuators (EBHA) for the rudder and some spoilers. The A380's 350bar (35MPa or 5,000psi) hydraulic system is a significant difference from the typical 210bar (21MPa or 3,000psi) hydraulics used on most commercial aircraft since the 1940s. First used in military aircraft, high-pressure hydraulics reduce the weight and size of pipelines, actuators and related components. The 350bar pressure is generated by eight de-clutchable hydraulic pumps. The hydraulic lines are typically made from
titanium; the system features both fuel- and air-cooled
heat exchangers. Self-contained electrically powered hydraulic power packs serve as backups for the primary systems, instead of a secondary hydraulic system, saving weight and reducing maintenance. The A380 uses four 150
kVA variable-frequency electrical generators, eliminating constant-speed drives and improving reliability. The A380 uses aluminium power cables instead of copper for weight reduction. The electrical power system is fully computerised and many
contactors and breakers have been replaced by solid-state devices for better performance and increased reliability. the electronic control box (ECB), and mounting hardware. The APU in use on the A380 is the PW 980A APU. The APU primarily provides air to power the Air Generation System (AGS) on the ground and to start the engines. 40% more than the next largest airliner, the
Boeing 747-8. The cabin has features to reduce traveller fatigue such as a quieter interior and higher
pressurisation than previous generations of aircraft; the A380 is pressurised to the equivalent altitude of up to . Seating options range from 3-room "residence" in first class to 11-across in economy. A380 economy seats are up to wide in a 10-abreast configuration, compared with the 10-abreast configuration on the 747-400 that typically has seats wide. On other aircraft, economy seats range from in width. The A380's upper and lower decks are connected by two stairways, one
fore and one
aft, both wide enough to accommodate two passengers side by side; this cabin arrangement allows multiple seat configurations. The maximum certified carrying capacity is 853 passengers in an all-economy-class layout, and average around 480–490 seats.
Air Austral's proposed 840 passenger layout has not come to fruition. The A380's interior illumination system uses bulbless
LEDs in the cabin, cockpit, and cargo decks. The LEDs in the cabin can be altered to create an ambience simulating daylight, night, or intermediate levels. On the outside of the aircraft,
HID lighting is used for brighter illumination. Airbus's publicity has stressed the comfort and space of the A380 cabin, and advertised onboard relaxation areas such as bars, beauty salons,
duty-free shops, and restaurants. which largely gave way to regular seats for greater passenger capacity. and that it was ultimately the airlines' decision how to configure the interior. Due to delivery delays, Singapore Airlines and Air France debuted their seat designs on different aircraft prior to the A380. Initial operators typically configured their A380s for three-class service, while adding extra features for passengers in premium cabins. Launch customer Singapore Airlines introduced partly enclosed first-class suites on its A380s in 2007, each featuring a leather seat with a separate bed; center suites could be joined to create a double bed. A year later, Qantas debuted a new first-class
seat-bed and a sofa lounge at the front of the upper deck on its A380s, and in 2009, Air France unveiled an upper deck electronic art gallery. In late 2008, Emirates introduced "shower spas" in first class on its A380s allowing each first class passenger five minutes of hot water, drawing on 2.5 tonnes of water, although only 60% of it was used. In addition to lounge areas, some A380 operators have installed amenities consistent with other aircraft in their respective fleets, including self-serve snack bars,
premium economy sections, File:Airbus A380-861, Emirates AN1721793.jpg|Ten-abreast old
economy class seating on the main deck on an Emirates A380 File:Airbus A380-861, Emirates AN1385446.jpg|Emirates A380's old
business class File:Etihad Airways aircraft interiors demo ITB 2017 (08).JPG|
Etihad Airways A380's The Residence suite File:Emirates Airbus A380-861 onboard bar Iwelumo.jpg|Emirates A380's onboard lounge and bar File:Emirates A380 Shower SPA ITB2014.jpg|Emirates A380's shower and spa
Integration with infrastructure and regulations Ground operations with separate
jetways for the main and upper decks, and
ground support equipment on a
Qatar Airways A380 In the 1990s, aircraft manufacturers were planning to introduce larger planes than the
Boeing 747. In a common effort of the
International Civil Aviation Organization (ICAO) with manufacturers, airports and its member agencies, the "80-metre box" was created, the
airport gates allowing planes up to wingspan and length to be accommodated. Airbus designed the A380 according to these guidelines, and to operate safely on Group V runways and taxiways with a loadbearing width. The US FAA initially opposed this, then in July 2007, the FAA and EASA agreed to let the A380 operate on runways without restrictions. The A380-800 is approximately 30% larger in overall size than the 747-400. Runway lighting and signage may need changes to provide clearance to the wings and avoid blast damage from the engines. Runways, runway shoulders and taxiway shoulders may be required to be stabilised to reduce the likelihood of
foreign object damage caused to (or by) the outboard engines, which are more than from the centre line of the aircraft, compared to for the
747-400, and
747-8. Airbus measured pavement loads using a 540-tonne (595short tons) ballasted test rig, designed to replicate the
landing gear of the A380. The rig was towed over a section of pavement at Airbus's facilities that had been instrumented with embedded load sensors. It was determined that the pavement of most runways will not need to be reinforced despite the higher weight, The A380 requires service vehicles with lifts capable of reaching the upper deck, as well as
tractors capable of handling the A380's maximum ramp weight. When using two jetway bridges the boarding time is 45 min, and when using an extra jetway to the upper deck it is reduced to 34 min. The A380 has an airport turnaround time of 90–110 minutes. In 2008, the A380 test aircraft were used to trial the modifications made to several airports to accommodate the type.
Takeoff and landing separation As of 2023, the A380 is the only aircraft in
wake turbulence category Super (J).
Maintenance As the A380 fleet grows older,
airworthiness authority rules require certain scheduled
inspections from approved
aircraft tool shops. The increasing fleet size (at the time projected to reach 286 aircraft in 2020) cause expected maintenance and modification to cost $6.8billion for 2015–2020, of which $2.1billion are for engines. Emirates performed its first
3C-check for 55 days in 2014. During lengthy shop stays, some airlines will use the opportunity to install new interiors. ==Operational history==