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The
Airbus
A330 is a
large-capacity medium-to-long-range commercial passenger airliner manufactured
by Airbus. It was developed at the same time as the four-engined A340.
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Arpingstone
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Etihad Airways Airbus A330-200 landing at
London (Heathrow)
Airport in July 2004 |
Airbus intended the A330 to
compete directly in the ETOPS (Extended Twin-engine Operations) market, which
was effectively established by the Boeing 767. The Boeing 777 also belongs to
this class; the Boeing 757 shares a heritage with the 767 but lacks the range,
and is not wide-bodied.
The A330's fuselage and wings are virtually identical to the A340's, although
it has different engines. The A330 basic fuselage design is inherited from the
Airbus A300, as is the nose/cockpit section and the fly-by-wire system and
flight deck from the Airbus A320.
Variants
There are two variants of the A330: the long fuselage A330-300 measures 63.6
m (208 ft 1 in) in length and can fly up to 10,500 km (5,650 nautical miles).
The short fuselage A330-200 measures 59.0 m (193 ft 7 in) in length with an
operating range of 12,500 km (6,750 nautical miles).
A330-200
The A330-200 was developed in part to replace the A300-600R and to compete
with the Boeing 767-300ER.The A330-200 is a shortened version of the original
-300.
Its vertical fin is taller than that of the -300 to restore its effectiveness
due to the fuselage shrink. It has additional fuel capacity and has an MTOW of
275 tonnes. Typical range with 253 passengers in a three-class configuration is
12,500 km (6,750 nautical miles).
Power is provided by two General Electric CF6-80E, Pratt & Whitney PW4000 or
Rolls-Royce Trent 700 engines. All engines are ETOPS-180 min rated. First
customer deliveries, to ILFC/Canada 3000, were in April 1998.
The A330-200 has sold strongly since its launch and has virtually eliminated
the Boeing 767 from the marketplace. As a result, Boeing has asked both Rolls
Royce and GE to design engines that enable the 787 Dreamliner to be 15% more
economical than the A330-200.
The direct Boeing equivalents are the 767-400ER and 787.
Operators of the A330-200 include Aer Lingus, Air France (and KLM), Air
Transat, Austrian Airlines, EgyptAir, Emirates, EVA Air, Gulf Air, LTU,
Lufthansa, Malaysia Airlines, Northwest Airlines, Qantas, Qatar Airways, Swiss
International Air Lines, and TAM Linhas Aéreas.
A330-300
The A330-300 was developed as replacement for the A300. It is based on a
stretched A300-600 fuselage but with new wings, stabilizers and new fly-by-wire
software.
The A330-300 carries 295 passengers in a three-class cabin layout over a
range of 10,500 km (5,650 nautical miles). It has a large cargo capacity,
comparable to a Boeing 747. Some airlines run overnight cargo-only flights after
daytime passenger services.
It is powered by two General Electric CF6-80E, Pratt & Whitney PW4000 or
Rolls-Royce Trent 700 engines. All engines are ETOPS-180 min rated. It entered
service in 1993.
The direct Boeing equivalent is the 777-200.
Operators of the A330-300 include Aer Lingus, Air Canada, Air Transat, Asiana
Airlines, Cathay Pacific Airways, China Airlines, Dragonair, Garuda Indonesia,
Korean Air, Lufthansa, Malaysia Airlines, Northwest Airlines, Philippine
Airlines, Qantas, SAS, SN Brussels Airlines, Thai Airways International, and US
Airways.
A330 MRTT
The Multi Role Tanker Transport version of the A330-200 provides aerial
refuelling and strategic transport. In January 2004 the UK Ministry of Defence
announced that the A330 MRTT had been selected to provide air-refuelling for the
RAF for the next 30 years under the Future Strategic Tanker Aircraft programme.
In this and the Australian contest, announced April 16, 2004, the A330 beat
competition from the Boeing 767 AAR derivative. The Royal Australian Air Force
has placed an order for 5 A330 MRTT aircraft to replace its ageing fleet of
707s.
The A330 MRTT is also in the running to land a contract from the United
States Air Force for perhaps up to 200 tankers to replace aging KC-135 and KC-10
aircraft. If the contract is won, it will required EADS to invest approximately
US$600 million in an assembly plant in the United States. Boeing 767 AAR derived
tankers were originally selected by the USAF, but following the discovery of a
bribery scandal the American government cancelled the Boeing lease and reopened
the competition.
A330-200Lite
The A330-200Lite would have contained weight reduction and new engines in an
attempt to compete with the 787-9. The concept was extended and renamed as the
A350. Singapore Airlines (SIA) is one of several potential customers.
Accident summary
(As of 2005)
- Hull-loss Accidents: 1 with a total of 7 fatalities
- On 30 June 1994 an A330 on a test flight crashed shortly after take-off at
Toulouse, killing all onboard
- Other occurrences: 1 with a total of 0 fatalities
- Hijackings: 2 with a total of 1 fatalities
An A330 performed the world's longest recorded glide with a jet airliner
after suffering fuel exhaustion over the Atlantic Ocean. Human error and lack of
automated computer checks stopped the crew from realizing the cause of fuel
imbalance was leakage via a broken fuel pipe caused by poor maintenance. The
plane soared for half an hour and covered 65 nautical miles (120 km) to an
emergency landing in the Azores. No one was killed, but the aircraft suffered
some structural damage and a lot of blown tires.
Specifications
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AIRCRAFT DIMENSIONS |
A330-200 |
A330-300 |
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Overall length |
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58.8 m. |
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63.6 m. |
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Height (to top of horizontal tail) |
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17.40 m. |
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16.85 m. |
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Fuselage diameter |
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5.64 m. |
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5.64 m. |
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Maximum cabin width |
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5.28 m. |
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5.28 m. |
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Cabin length |
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45.0 m. |
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50.35 m. |
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Wingspan (geometric) |
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60.3 m. |
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60.3 m. |
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Wing area (reference) |
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361.6 m2 |
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361.6 m2 |
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Wing sweep (25% chord) |
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30 degrees |
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30 degrees |
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Wheelbase |
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22.2 m. |
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25.6 m. |
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Wheel track |
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10.69 m. |
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10.69 m. |
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BASIC OPERATING DATA |
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Engines |
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two CF6-80E1 or
PW4000
or RR Trent 700 |
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two CF6-80E1 or
PW4000
or RR Trent 700 |
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Engine thrust range |
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303-320 kN |
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303-320 kN |
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Typical passenger seating |
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253 (3-class) /
293 (2-class) |
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295 (3-class) /
335 (2-class) |
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Range (w/max. passengers) |
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12,500 km. |
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10,500 km. |
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Max. operating Mach number (Mmo) |
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0.86 Mo. |
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0.86 Mo. |
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Bulk hold volume - Standard/option |
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19.7 / 13.76 m3 |
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19.7 / 13.76 m3 |
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DESIGN WEIGHTS |
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Maximum ramp weight |
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230.9 (233.9 )
tonnes |
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230.9 (233.9)
tonnes |
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Maximum takeoff weight |
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230 (233) tonnes |
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230 (233) tonnes |
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Maximum landing weight |
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180 (182) tonnes |
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185 (187) tonnes |
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Maximum zero fuel weight |
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168 (170) tonnes |
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173 (175) tonnes |
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Maximum fuel capacity |
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139,100 Litres |
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97,170 Litres |
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Typical operating weight empty |
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119.6 tonnes |
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122.2 (124.5)
tonnes |
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Typical volumetric payload |
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36.4 tonnes |
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45.9 tonnes |
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