The Airbus A330 is a
large-capacity, wide-body, medium-to-long-range
commercial passenger airliner. Airbus intended the
A330 to compete directly in the ETOPS (Extended-range
Twin-engine Operation Performance Standards) market,
specifically with the Boeing 767.
After studying a
number of possible stretched versions and other
derivatives of the basic A300 wide-body twinjet,
Airbus Industrie had by the mid-1980s narrowed the
choice to two. At the project stage, these were
identified as the TA9, a medium-range large-capacity
twin, and the TA11, a four-engine long-range variant
of the same design. As the TA designations indicated,
these were twin-aisle designs, based on use of the
basic A300 fuselage cross-section.
By early 1986, Airbus
had reached the conclusions that it needed to add both
of these types to its product range to maintain its
competitive position against the major US aircraft
companies, and that the developing market would
justify production of both for entry into service in
the early 1990s.
The TA9 would thus
become Airbus largest twinjet, and the TA11
would be the company's first four-engine
aircraft.
The move from project
definition to the preliminary marketing phase (though
still short of a formal launch decision) was marked by
designating them A330 and A340 respectively. By late
1986 the two types had been closely integrated at
design and engineering levels, while launch orders
were being sought and the necessary financial backing
of the Airbus partner companies was being
arranged.
The Airbus proposal
for the A330 and A340 was unusual, if not unique, in
that it planned to use a single airframe, with
basically the same fuselage, wing and tail unit, in
both two- and four-engine versions. The fuselage would
use the same cross-section as the A300 and A310, with
a new and longer center section to mate with a new
wing and provide about 17 ft. (5.2 m.) of extra length
to increase the seating capacity.
The wing is all-new
for the A330 and A340 but is practically the same for
both versions. Of advanced design, it has a very high
aspect ratio (= length divided by width), and is
notable also for its use of variable camber, using an
on-board computer to tailor the camber, through small
movements of the trailing edge flaps, to suit the
weight, speed and altitude at which the aircraft is
flying. Only small aerodynamic differences are
necessary to allow for the variation in number of
engines, and the structure is also identical except
for some differences in skin thickness and the engine
attachments.
Although the A340
operates at slightly higher weights than the A330,
wing bending moments are similar because of the extra
relief provided by the weight of the outside engines.
Additionally, the lighter, shorter-range A330 needs as
much strength as the A340 because it makes more
fatigue-inducing flights in a given number of
hours.
Both types use the
same carbon-fiber reinforced plastic (CFRP) fins as
the A310, and a CFRP tailplane trim-tank as in the
A310-300. Cockpit and systems are based on those of
the A320, with a computerized fIy-by-wire flight
control system, and an advanced EFIS (Electronic
Flight Instrument System) flightdeck with side stick
controllers.
In 1986/87, Airbus had
considered using the 28,600 lb thrust CFM56-5C2 and
the 30,000 lb IAE SuperFan derivative of the V2500.
However, the company announced on April 8, 1987, that
it had selected the CFM56-5C3 (32,597 lb thrust) to
power the A340, and a development of the General
Electric CF6-80C2 for the A330.
The A330 (a -300)
first flew on November 2, 1992, and although the A330
and A340 had been launched simultaneously in June
1987, and developed in parallel, the first flight of
the A340 had occurred more than a year earlier, on
October 25, 1991.
Final assembly of both
aircraft is undertaken by EADS Aérospatiale in
Toulouse, France.
On October 21, 1993,
the A330-300 was given simultaneous JAA/FAA
certification, the first time this had happened to an
airplane.
Air Inter was launch
customer for the General Electric engined version and
received its first delivery in 1993. US Airways was
the launch customer in the United States with nine
A330s. Thai International received its first two
A330-300s with PW 4183 turbofans in December 1994,
delayed slightly by the impact on the test program of
the crash of an A330 during flight testing by
Airbus.
The Rolls-Royce Trent
700 was certificated at 72,000 lb in December 1994,
and Cathay took delivery of the first of its ten
Trent-powered A300s at the end of February 1995,
putting it in service on March 3, 1995.
In a two-class cabin
layout, the A330-300 can carry 335 passengers over
4,610 nm (8540 km) and, with the addition of 16.7
tonnes of freight in its large cargo space, its range
is still better than 2,800 nm (5,190 km).
In a three-class cabin
layout, the A330-300 can carry 295 passengers 5,660 nm
(10,500 km), and in a single-class layout, it can
carry 440 passengers.
The aircraft's large
cargo capacity is such that it is comparable to early
Boeing 747s, and some airlines run overnight
cargo-only flights after their daytime passenger
services.
While the standard
A330-300 shares the same fuselage length as the
A340-300, Airbus studied various stretched (A330-400)
and shortened (A330-100 and -200) versions. One
stretched, high capacity concept looked at for a time
featured lower-deck seating in place of the forward
freight hold.
The shortened A330-200
version was formally launched in November 1995 as a
long range 767-300ER competitor, and is described
separately. It has a range of up to 6,400 nm (11,860
km), has a typical seating capacity of 253 passengers
in three classes. First flight was on August 13 1997,
with certification and first customer delivery, to
ILFC, in April 1998. (See separate entry)
Current powerplant
options for the A330 are either two GE CF6-80E1A1s or
-80E1A2s producing 65,500 lb or 67,443 lb thrust, two
Pratt & Whitney PW4164s or PW4183s rated at 64,070
lb and 68,000 lb respectively, or two Rolls-Royce
Trent 700s rated at 72,000 lb thrust. All of these
engines are ETOPS-rated for 180 minutes.
The direct Boeing
equivalent of the A330-300 is the 777-200.
Airbus will replace
the A330-300 with the future A350-900 XWB, currently
predicted to fly in 2013.
As of November 2006,
total deliveries of the A330-300 stood at 202. Of
these, 201 were still in service.