Airbus launched the
A380 in December 2000 to complete its product line
with this completely new very large airliner. The
A380's upper deck extends along the entire length of
the fuselage. This allows for a spacious cabin with
50% more floor space than the next largest airliner,
the Boeing 747-400, and provides seating for 555
people in standard three-class configuration or up to
853 people in full economy class configuration. It is
the largest passenger airliner in the
world.
The other launch
model, the freighter version, will be one of the
largest cargo aircraft and will have a payload
capacity exceeded only by the Antonov An-225, only
three of which were produced. They were designed to
transport the soon-to-be-abandoned Soviet space
shuttle, the Buran.
The A380 breaks the
30-year monopoly in this market held by Boeing's
original Jumbo, the 747. McDonnell Douglas pursued a
similar strategy with its ultimately unsuccessful
MD-12 design. As each manufacturer looked to build a
successor to the 747, they knew there was room for
only one new aircraft to be profitable in the 600- to
800-seat market segment. Each knew the risk of
splitting such a niche market, as had been
demonstrated by the simultaneous debut of the Lockheed
L-1011 TriStar and the McDonnell Douglas DC-10: either
aircraft met the market's needs, but the market could
profitably sustain only one model, eventually
resulting in Lockheed's departure from the civil
airliner business.
In January 1993,
Boeing and several companies in the Airbus consortium
started a joint feasibility study of an aircraft known
as the Very Large Commercial Transport (VLCT), aiming
to form a partnership to share the limited
market.
In June 1994, Airbus
began developing its own very large airliner,
designated the A3XX. Airbus considered several
designs, including a flying wing configuration, and an
odd side-by-side combination of two fuselages from the
A340, which was Airbus's largest jet at the time. The
A3XX was pitted against the VLCT study and Boeing's
own New Large Aircraft successor to the 747, which
evolved into the 747X, a stretched version of the 747
with the forebody "hump" extended rearwards to
accommodate more passengers. The joint VLCT effort
ended in July 1996, and Boeing suspended the 747X
program in January 1997, only to resurrect it several
times before finally launching the 747-8
Intercontinental in November 2005.
Possibly the reason
for Boeing's vacillation was the fact that their
market forecast, in contrast with the Europeans'
optimistic views, showed a demand for only 930
aircraft of 747-400 size and larger over the next 20
years. And within this category, more than half of the
requirement, or approximately 565 aircraft, was for
400-500-seat aircraft, leaving a projected requirement
for airplanes of 500 seats or more at only 365, most
of them during the forecast's second
decade.
From 1997 to 2000, as
the East Asian financial crisis darkened the market
outlook, Airbus refined its design, targeting a 15 to
20 percent reduction in operating costs over the
existing Boeing 747-400. The A3XX design converged on
a double-decker layout that provided higher seat
capacities than a traditional single-deck design, and
because of the significantly lighter structure
required.
Airbus Large Aircraft
Division and about 20 airlines, all of them ranked as
potential customers, jointly formed working groups to
regularly review the proposed VLTA's (Very Large
Transport Aircraft) operational requirements,
performance and technical definition. The group
included Air Canada, Air France, Air New Zealand, All
Nippon Airways, Cargolux, Emirates, Iberia, Japan
Airlines, KLM Royal Dutch Airlines, Korean Air,
Lufthansa German Airlines, Qantas, Singapore Airlines,
United Airlines, Virgin Atlantic Airways and
FedEx.
On December 19, 2000,
the supervisory board of newly restructured Airbus
voted to launch an 8.8 billion euro program to build
the A3XX, re-christened as the A380, with 55 orders
from six launch customers: Emirates (on July 24, 2000,
they became the first airline to place a firm order),
Air France, International Lease Finance Corporation
(ILFC), Singapore Airlines, Qantas and Virgin
Atlantic.
Later, the following
companies also ordered the aircraft: FedEx (the launch
customer for the A380-800F freighter), Qatar Airways,
Lufthansa, Korean Air, Malaysia Airlines, Etihad
Airways, Thai Airways and UPS.
The A380 designation
was a break from previous sequential Airbus
designations because the numeral 8 resembles the
double-deck cross section, and symbolizes good luck in
some Asian cultures. Also it emphasizes the
aircrafts huge size by distancing it from the
A340.
The aircraft's final
configuration was frozen in early 2001, and
manufacturing of the first A380 wing box component
started on January 23, 2002 at Nantes in France. In
that year more than 6,000 people were working on the
A380 development.
In the first few
months of 2000, the consortium's member companies
initiated negotiations with their four respective
European governments in preparation for multiyear loan
arrangements that could cover up to 33% of each
company's share in the program. This would comply with
the U.S.-European Union July 1992 agreement on
commercial transport funding.
Key design aims
included the ability to use existing airport
infrastructure with little modifications to the
airports, and direct operating costs per seat 15-20%
less than those for the 747-400. With 49% more floor
space and only 35% more seating than the previous
largest aircraft, Airbus was ensuring wider seats and
aisles for more passenger comfort. Using the most
advanced technologies, the A380 is also designed to
have 10-15% more range, lower fuel burn and emissions,
and less noise.
The A380 features an
advanced version of the Airbus common two-crew cockpit
with pull-out keyboards for the pilots, extensive use
of composite materials such as GLARE (an
aluminum/glass fibre composite), and four 74,000 to
84,000 lb (330 to 374kN) Rolls-Royce Trent 900
turbofans, or four 76,500lb - 81,500 lb Engine
Alliance (General Electric/Pratt & Whitney) GP7200
turbofans. The Rolls-Royce engine was certificated in
October 2004, and the GP7200 was certificated by the
European Aviation Safety Agency in December 2005 and
made its first flight in August 2006.
The A340-inspired
fly-by-wire flight controls and systems uses four
independent power systems to actuate control surfaces.
Two hydraulic systems are complemented by
electro-hydrostatic actuators and electric backup
hydraulic actuators, an electric ram air turbine, and
electric motor pumps for ground use only.
The flight deck's
design is a natural evolution of the A320/A340
concept. However, it includes new features such as
larger and interactive flight displays, takeoff
acceleration monitoring and engine thrust displays and
a vertical situation awareness system.
In an initiative set
to collect comments and preferences before freezing
the cockpit's concept, 21 airline pilots reviewed
Airbus' studies and "flew" Aérospatiale Matra's
Epopee simulator. Although Epopee is not a full-flight
simulator, it reproduces a broad range of A380 flight
configurations. Epopee, which is complemented by a
human factor interface demonstrator, was also used to
validate the cockpit of the Airbus Military Co.'s
proposed A400M military transport.
Although the A380 was
designed to comply with an 80 x 80 meters (260 x 260
ft.) apron box so that it could operate at existing
airport facilities, taxiing the aircraft requires a
CCTV system.
Several A380 models
are planned: the basic aircraft is the 555-seat
A380-800. This model has a maximum takeoff weight of
540 tonnes, and can carry an 84 tonne payload 8000 nm
(14,800 km), sufficient to fly from Chicago to Sydney
nonstop. Cruising speed is Mach 0.85 (about 900 km/h
or 560 mph at cruise altitude), similar to that of the
Boeing 747.
The A380-800F
freighter will have an increased maximum takeoff
weight of 590 tonnes to enable the aircraft to carry
up to 150 tonnes of freight over 5,725 nm (10,600 km).
The launch customer was FedEx, but they canceled their
order due to delivery delays.
Combi versions are
also planned, and potential future models include a
shortened, 480-seat A380-700, and a stretched,
656-seat A380-900. (The -700, -800, and -900
designations were chosen to reflect that the A380 will
enter service as a "fully developed aircraft" and that
the basic models will not be soon replaced by improved
variants).
Apart from the prime
contractors in France, Germany, the United Kingdom and
Spain, components for the A380 airframe are also
manufactured by industrial partners in Australia,
Austria, Belgium, Finland, Italy, Japan, South Korea,
Malaysia, Netherlands, Sweden, Switzerland and the
United States. A380 final assembly is taking place in
Toulouse, France, with interior fitment in Hamburg,
Germany. Major A380 assemblies are transported to
Toulouse by ship, barge and road.
On January 18, 2005,
the first Airbus A380 prototype, serial number 001 and
registration F-WWOW, was officially revealed in a
lavish ceremony in Toulouse, attended by 5000 invited
guests. These included the French, German, British and
Spanish heads of state or government, representing the
countries that invested heavily in the 10-year, 10
billion+ euro ($13 billion+) aircraft program, and the
CEOs of the 14 A380 customers, who had by then placed
firm orders for 149 aircraft.
The first flight took
place at 10:29 a.m. local time, April 27, 2005. The
prototype, equipped with Rolls-Royce Trent 900
engines, departed runway 32L of Toulouse Blagnac
International Airport with a flight crew of six headed
by test pilot Jacques Rosay. It was carrying 22 short
tons (20 metric tons) of flight test instrumentation
and water ballasts. The take-off weight of the
aircraft was 421 tonnes (464 short tons); although
this was only 75% of its maximum take-off weight, it
was the heaviest take-off weight of any passenger
airliner ever flown.
In mid-November 2005
the A380 embarked on a tour of Southeast Asia and
Australia for promotional and for long-haul flight
testing purposes, visiting Singapore, Brisbane,
Sydney, Melbourne and Kuala Lumpur. During this tour,
the colors of Singapore Airlines, Qantas and Malaysia
Airlines were applied in addition to the Airbus house
colors. On November 19, an A380 flew in full Emirates
colors at the Dubai Air Show.
On January 10, 2006,
the A380 made its first transatlantic flight to
Medellin in Colombia, to test engine performance at a
high altitude airport. It arrived in North America on
February 6, landing in Iqaluit, Nunavut in Canada for
cold-weather testing. The same aircraft then flew to
Singapore to participate in the Asian Aerospace 2006
exhibition, in full Singapore Airlines
livery.
On March 26, 2006, an
A380 underwent evacuation certification in Hamburg in
Germany. The test, performed to meet regulatory
requirements, involved evacuating 853 passengers and
20 crew from the aircraft within 90 seconds, with 8 of
the 16 exits blocked. The evacuation was successfully
completed in 78 seconds. Three days later, the A380
received joint European Aviation Safety Agency (EASA)
and United States Federal Aviation Administration
(FAA) approval to carry up to 853 passengers,
indicating that the evacuation trial had met their
certification standards.
Five A380s have been
built for testing and demonstration purposes. The
first A380 slated for delivery to a customer, serial
number 003 and registration F-WWSA, took to the air in
May 2006. The maiden flight of the first A380 with
GP7200 engines (F-WWEA) took place on August 25,
2006.
On September 4, 2006
the first full passenger-carrying flight test took
place. The aircraft flew from Toulouse with 474 Airbus
employees on board, in the first of a series of
flights to test passenger facilities and comfort.
From October 30, 2006
until November 13, 2006, a further series of
route-proving flights, covering 69,000 nm (128,000
km), took place to demonstrate the aircraft's
performance for 150 flight hours under typical airline
operating conditions.
During testing the
A380 visited 18 countries, Australia, Canada, China,
Colombia, Ethiopia, France, Germany, Iceland, Ireland,
Japan, Malaysia, Singapore, South Africa, South Korea,
Spain, Thailand, the United Arab Emirates and the
United Kingdom.
The manufacturer's
five test A380 aircraft, one powered by Engine
Alliance GP7200s and four by Rolls-Royce Trent 900s,
concluded their test programme in December 2006, after
having logged over 2,300 hours during more than 730
test flights.
The aircraft received
dual European Aviation Safety Agency and US Federal
Aviation Administration certification on December 12,
2006.
Initial production of
the A380 was plagued by a series of delays attributed
to the 500 kilometers (310 miles) of wiring in each
aircraft. Airbus cited as underlying causes the
complexity of the cabin wiring, its concurrent design
and production, the use of two incompatible versions
of the CATIA computer-aided design software, the high
degree of customization for each airline, and failures
of configuration management (wiring in one section
will not plug correctly into wiring in another). Over
80% of the wiring is supplied by Labinal, although
this company has not been blamed for the delays.
Deliveries will be pushed back by nearly two
years.
Airbus announced the
first delay in June 2005 and notified airlines that
delivery would slip by six months, with Singapore
Airlines receiving the first A380 in the last quarter
of 2006, Qantas getting its first delivery in April
2007 and Emirates receiving aircraft before 2008. This
reduced the number of planned deliveries by the end of
2009 from about 120 to 90-100.
On June 13, 2006
Airbus announced a second delay, with the delivery
schedule undergoing an additional shift of six to
seven months. Although the first delivery was still
slated before the end of 2006, deliveries in 2007
would drop to only 9 aircraft, and deliveries by the
end of 2009 would be cut to 70-80 aircraft. The
announcement caused a 26% drop in the share price of
Airbus's parent, EADS, and led to the departure of
EADS CEO Noël Forgeard, Airbus CEO Gustav
Humbert, and A380 program manager Charles
Champion.
In the wake of the new
delay, Malaysia Airlines and ILFC were reported to be
considering the cancellation of their orders. Launch
customers Singapore Airlines, Emirates and Qantas also
were reported to be angered by the delays and
expecting compensation. However, on July 21, 2006
Singapore Airlines ordered a further 9 A380s and
stated that Airbus had "demonstrated to our
satisfaction that the engineering design for the A380
is sound [and that] it has performed well in
flight and certification tests and the delays in its
delivery have been caused more by production, rather
than technical, issues."
On October 3, 2006,
upon completion of a review of the A380 program, the
new CEO of Airbus, Christian Streiff, announced a
third delay. The largest delay yet, it pushed the
first delivery for Singapore Airlines (a R-R
Trent-powered aircraft) to October 2007, to be
followed by 13 deliveries in 2008, 25 in 2009, and the
full production rate of 45 aircraft per year in 2010.
The delay also increased the earnings shortfall
projected by Airbus through 2010 to 4.8 billion euros.
The customer with the largest A380 order, Emirates,
saw its first delivery pushed back to August 2008 and
said as a result that it was considering scaling back
its order, potentially in favor of the rival Boeing
747-8. Virgin Atlantic deferred its deliveries by four
years, to 2013. Initial deliveries for the A380
freighter were delayed into 2010. The third delay was
followed by the first cancellation to hit the A380
program, as FedEx dropped its order for ten A380F
freighters in favor of 15 Boeing 777F
freighters.
Singapore Airlines
plans to use its first aircraft, in a 485-seat
configuration, on its London-Singapore-Sydney (the
kangaroo route) service. Subsequent routes for
Singapore Airlines may include the Singapore-San
Francisco route via Hong Kong, as well as direct
flights to Paris and Frankfurt. Qantas has announced
it will use the A380, in a 501-seat configuration, on
its Melbourne and Sydney to Los Angeles routes. Air
France's aircraft will be used on the Paris to
Montreal and New York routes.
The new Airbus is sold
in two models. The A380-800 can carry 555 passengers
in a three-class configuration or up to 853 passengers
in a single-class economy configuration. The range for
the -800 model is 15,000 km (8,000 nm). The second
model, the A380-800F freighter, will carry 150 tonnes
of cargo 10,400 km (5,600 nm). Future variants may
include an A380-900 stretch seating about 650
passengers, a shortened A380-700 seating about 455
passengers, and an extended range version with the
same passenger capacity as the A380-800. The A380's
wing is sized for a Maximum Take-Off Weight (MTOW)
over 650 metric tonnes in order to accommodate these
future versions, albeit with some strengthening
required. The stronger wing (and structure) is used on
the A380-800F freighter. This common design approach
sacrifices some fuel efficiency on the A380-800
passenger model, but the sheer size of the aircraft,
coupled with the significant advances in technology
described below, are still expected to provide lower
operating costs per passenger than all current 747
variants.
Airbus used similar
cockpit layout, procedures and handling
characteristics to those of other Airbus aircraft, to
reduce crew training costs. Accordingly, the A380
features an improved glass cockpit, and fly-by-wire
flight controls linked to side-sticks. The improved
cockpit displays feature eight 15x20 cm (6x8 in)
liquid crystal displays, all of which are physically
identical and interchangeable. These comprise two
Primary Flight Displays, two navigation displays, one
engine parameter display, one system display and two
Multi-Function Displays. These MFDs are new with the
A380, and 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 navigation
system.
Either the Rolls-Royce
Trent 900 or Engine Alliance GP7200 turbofans power
the A380. Both are derived from predecessors (Trent
800 and GE90) available on the Boeing 777. The Trent
900 is the scaled down version of the Trent 800, but
incorporating the swept-back fan and counter-rotating
spools of the stillborn Trent 8107. The GP7200 has a
GE90-derived core and PW4090-derived fan and
low-pressure turbo-machinery. Noise reduction was a
driving requirement for the A380, and particularly
affects engine design. Both engine types meet the
stringent QC/2 departure noise limits set by London's
Heathrow Airport, which is expected to become a key
destination for the A380.
Composite materials
make up 25% of the A380's airframe, by weight.
Carbon-fiber reinforced plastic, glass-fiber
reinforced plastic and quartz-fiber reinforced plastic
are used extensively in wings, fuselage sections, tail
surfaces, and doors. The A380 is the first commercial
airliner with a central wing box made of carbon fiber
reinforced plastic, and it is the first to have a wing
cross-section that is smoothly contoured. Other
commercial airliners have wings that are partitioned
in sections. The flowing, continuous cross-section
allows for maximum aerodynamic efficiency.
Thermoplastics are used in the leading edges of the
slats. The new material GLARE (GLAss-REinforced fiber
metal laminate) is used in the upper fuselage and on
the stabilizers' leading edges. This
aluminum-glass-fiber laminate is lighter and has
better corrosion and impact resistance than
conventional aluminum alloys used in aviation. Unlike
earlier composite materials, it can be repaired using
conventional aluminum repair
techniques.[25]
Newer weldable
aluminum alloys are also used. This enables the
widespread use of laser welding manufacturing
techniques - eliminating rows of rivets and resulting
in a lighter, stronger structure.
The A380 employs an
Integrated Modular Avionics (IMA) architecture, first
used in advanced military aircraft such as the F-22
Raptor and the Eurofighter Typhoon. It is based on a
commercial off-the-shelf (COTS) design. Many previous
dedicated single-purpose avionics computers are
replaced by dedicated software housed in onboard
processor modules and servers. This cuts the number of
parts, provides increased flexibility without
resorting to customized avionics, and reduces costs by
using commercially available computing
power.
Together with IMA, the
A380 avionics are very highly networked. The data
communication networks use Avionics Full-Duplex
Switched Ethernet, following the ARINC 664 standard.
The data networks are switched full-duplexed
star-topology and based on 100baseTX fast-Ethernet.
This reduces the amount of wiring required and
minimizes latency.
The Network Systems
Server (NSS) is the heart of the A380's paperless
cockpit. It eliminates the bulky manuals and charts
traditionally carried by the pilots. The NSS has
enough inbuilt robustness to do away with onboard
backup paper documents. The A380's network and server
system stores data and offers electronic
documentation, providing a required equipment list,
navigation charts, performance calculations, and an
aircraft logbook. All are accessible to the pilot from
two additional 27 cm (11 in) diagonal LCDs, each
controlled by its own keyboard and control cursor
device mounted in the foldable table in front of each
pilot.
Power-by-wire flight
control actuators are used for the first time in civil
service, backing up the primary hydraulic flight
control actuators. During certain maneuvers, they
augment the primary actuators. They have
self-contained hydraulic and electrical power
supplies. They are used as electro-hydrostatic
actuators (EHA) in the aileron and elevator, and as
electrical backup hydrostatic actuators (EBHA) for the
rudder and some spoilers.
The aircraft's 350 bar
(35 MPa or 5,000 psi) hydraulic system is an
improvement over the typical 210 bar (21 MPa or 3,000
psi) system found in other commercial aircraft since
the 1940s. First used in military aircraft, higher
pressure hydraulics reduce the size of pipelines,
actuators and other components for overall weight
reduction. The 350 bar pressure is generated by eight
de-clutchable hydraulic pumps. Pipelines are typically
made from titanium and the system features both fuel
and air-cooled heat exchangers. The hydraulics system
architecture also differs significantly from other
airliners. Self-contained electrically powered
hydraulic power packs, instead of a secondary
hydraulic system, are the backups for the primary
systems. This saves weight and reduces
maintenance.
The A380 uses four 150
kVA variable-frequency electrical generators
eliminating the constant speed drives for better
reliability. The A380 uses aluminum power cables
instead of copper for greater weight savings due to
the number of cables used for an aircraft of this size
and complexity. The electrical power system is fully
computerized and many contactors and breakers have
been replaced by solid-state devices for better
performance and increased reliability.
The A380 features a
bulbless illumination system. LEDs are employed in the
cabin, cockpit, cargo and other fuselage areas. The
cabin lighting features programmable multi-spectral
LEDs capable of creating a cabin ambience simulating
daylight, night or shades in between. On the outside
of the aircraft, HID lighting is used to give
brighter, whiter and better quality illumination.
These two bulbless technologies provide brightness and
a service life superior to traditional incandescent
light bulbs.
The A380 was initially
planned without thrust reversers, as Airbus believed
it to have ample braking capacity. The FAA disagreed,
and Airbus elected to fit only the two inboard engines
with them. The two outboard engines do not go into
reverse, to reduce the amount of debris blown up
during landing. The A380 features electrically
actuated thrust reversers, giving them better
reliability than their pneumatic or hydraulic
equivalents, in addition to saving weight.
Passenger
amenities
Initial publicity
stressed the comfort and space of the A380's cabin,
which offers room for such installations as relaxation
areas, bars, duty-free shops, and beauty salons. One
A380 customer likely to use innovative amenities is
Virgin Atlantic Airways, which has a bar in Business
Class on its aircraft, and has announced plans to
include casinos, double beds, a gymnasium and showers
on its A380s.
The A380 will expand
the improvements that the 747 made (more seats and
lower seat-distance costs) while providing wider seats
and better amenities. At 555 passengers, the A380's
seating capacity represents a 35% increase over the
747-400 in a standard three-class configuration, along
with a nearly 50% larger cabin volume, producing more
space per passenger. If, however, the plane is ordered
in an all-economy-class configuration, it can hold up
to 853 passengers, its maximum certified carrying
capacity.
Airport
compatibility
The A380 was designed
to fit within an 80 x 80 m airport gate, and can land
or take off on any runway that can take a Boeing 747.
However, airports used by the A380 in commercial
service may need infrastructure modifications. Its
large wingspan can require some taxiway and apron
reconfigurations in order to maintain safe separation
margins when two of the aircraft pass each other.
Taxiway shoulders may be required to be paved to
reduce the likelihood of foreign object damage caused
to (or by) the outboard engines, which overhang more
than 25 m (80 ft) from the center line of the
aircraft. Any taxiway or runway bridge must be capable
of supporting the A380's maximum weight. The terminal
gate must be sized such that the A380's wings do not
block adjacent gates, and may also provide multiple
jetway bridges for simultaneous boarding on both
decks. Service vehicles with lifts capable of reaching
the upper deck must be obtained, as well as tractors
capable of handling the A380's maximum ramp
weight.
The A380 test aircraft
have begun a campaign of airport compatibility
testing, to verify the modifications already made at
several large airports. To date, airports have been
visited for compatibility testing in Bangkok,
Brisbane, Frankfurt, Hong Kong, Johannesburg, Kuala
Lumpur, London, Melbourne, Seoul, Singapore, Sydney,
Tokyo, Dusseldorf and Vancouver.
Production
Major structural
sections of the A380 are built in France, Germany,
Spain, and the United Kingdom. Due to their size, they
are brought to the assembly hall in Toulouse in France
by surface transportation, rather than by the Beluga
aircraft used for other Airbus models. Components of
the A380 are provided by suppliers from around the
world; the five largest contributors, by value, are
Rolls-Royce, SAFRAN, United Technologies, General
Electric, and Goodrich.
The front and rear
sections of the fuselage are loaded on an Airbus RORO
ship, "Ville de Bordeaux," in Hamburg in northern
Germany, whence the ship sails to the United Kingdom.
The wings, which are manufactured at Filton in Bristol
and Broughton in north Wales, are transported by barge
to Mostyn docks, where the ship adds them to its
cargo. In Saint-Nazaire in western France, the ship
trades the fuselage sections from Hamburg for larger,
assembled sections, some of which include the nose.
The ship unloads in Bordeaux. Afterwards, the ship
picks up the belly and tail sections from
Construcciones Aeronauticas SA in Cadiz in southern
Spain, and delivers them to Bordeaux. From there, the
A380 parts are transported by barge to Langon, and by
oversize road convoys to the assembly hall in
Toulouse. New wider roads, canal systems and barges
were developed to deliver the A380 parts. After
assembly, the aircraft are flown to Hamburg to be
furnished and painted. Airbus sized the production
facilities and supply chain for a production rate of
four A380s per month.
Recent News
Some of the most
extensive media coverage of the A380 occurred as a
result of a promotional media flight from Toulouse in
February 2007.
In March 2007, the
A380 made its United States debut as two aircraft
landed within minutes of each other at John F. Kennedy
International Airport in New York and Los Angeles
International Airport. The New York stopover was part
of a 12-day route proving trip, while the Los Angeles
visit was used for airport compatibility and
functional checks.
With the distinctive
blue and gold logo and the name "Singapore Airlines"
across 33 meters of the aircraft fuselage, the world's
first customer A380 rolled out of the paint hangar in
Hamburg, Germany, on 2nd May 2007. About 3,600 liters
of chromate-free paint is used for three layers of
paint (primer, customer-paint, top-coat) for an A380.
Only 600 to 1,000 kg of paint stays on the aircraft.
Each layer measures only about 0.120 mm and is able to
withstand differences in temperatures of about 100
degrees Celsius.For its first visit to India, the A380
landed in New Delhi on Sunday May 6, 2007, after a
nine-hour flight from Toulouse. The aircraft stayed
for two days in New Delhi before flying to Mumbai,
headquarters of its first Indian customer, Kingfisher
Airlines. The aircraft was in India to perform
demonstration flights and to help celebrate the second
anniversary of Kingfisher, which has five A380s on
order.
The A380 will be
embarking on a visit to the Asia-Pacific region as
part of a series of demonstration tours that will take
place during 2007. The Asia-Pacific tour will take the
A380 development aircraft MSN7 to Narita (Japan) from
4th - 6th June, then to Sydney (Australia) from 6th -
8th June and finally to Taipei (Taiwan) from 8th -
10th June, after having made a series of airport
compatibility trials at Paris Charles de Gaulle (CDG)
airport from 1st - 3rd June jointly with Air France
and Aéroports de Paris.
As of April 2007,
orders for the A380 stood at 156. Airbus expects to
sell a total of 750 aircraft, and estimates break-even
at 420 units, increased from 270 due to delivery
delays and the falling exchange rate of the US dollar.
Industry analysts anticipate between 400 and 880 sales
by 2025. As of 2006, the unit cost of the A380 is US$
296 to 316 million, depending on equipment
installed.