Airbus A330

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by 68.163.108.150 (talk) at 23:08, 30 January 2008. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Template:Infobox Aircraft The Airbus A330 is a large-capacity, wide-body, medium-to-long-range commercial passenger airliner. It was developed at the same time as the four-engined Airbus A340, and will likely be replaced by the Airbus A350.

History

Airbus intended the A330 to compete directly in the ETOPS (Extended-range Twin-engine Operation Performance Standards) market, specifically with the Boeing 767.

The A330's fuselage and wings are virtually identical to those of the smaller A340 variants, 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 flightdeck from the A320. Both the A330 and A340 are assembled on the same final assembly line at Toulouse-Blagnac, France.

By the end of December 2007, a total of 870 A330s had been ordered and 515 delivered.

Variants

There are two main variants of the A330. The A330-300 was launched in 1987 with introduction into service in 1993. The A330-200 was launched in 1995, introduced in 1998 and comes in passenger, freighter and tanker versions.

A330-200

TAM Brazilian Airlines (TAM Linhas Aéreas) A330-200
EVA Air's A330-203 Hello Kitty jet (B-16303)

The A330-200 was developed to compete with the Boeing 767-300ER. The A330-200 is similar to the A340-200 or a shortened version of the A330-300. With poor sales of the A340-200 (of which only 28 were built), Airbus decided to use the fuselage of the A340-200 with the wings and engines of the A330-300. This significantly improved the economics of the plane and made the model more popular than the four-engined variant.

Its vertical fin is taller than that of the A330-300 to restore its effectiveness due to the shorter moment arm of the shorter fuselage. It has additional fuel capacity and, like the A330-300, has a MTOW of 233 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, outselling the Boeing 767 by 23 to 9 in 2004. 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 equivalent is currently the 767-300ER and in the future will be the 787-8.

A330-200F

File:A330-200F.jpg
Artist's concept of the A330-200F derivative

Due to flagging A300-600F and A310F sales, Airbus first began marketing a freighter derivative of the A330-200 around 2000-2001, although it was not launched at this time.[1] The A330-200F re-emerged at the 2006 Farnborough Air Show and received its industrial go-ahead in January 2007. Entry into service is planned for the second half of 2009.

The A330-200F is a mid-size, long-haul all-cargo aircraft capable of carrying 64 tonnes over 4,000 NM / 7,400 km, or 69 tonnes up to 3,200 NM / 5,930 km. It introduces a new versatile main-deck cargo loading system that will be able to accommodate both pallets and containers. Several different arrangements will be possible on the main deck, taking up to 23 Side-by-Side (SBS) pallets, aimed at the high volume, high value commodities or Single Row (SR) loading of 16 pallets (96”x 96”x125” SR pallets) and/or nine AMA containers aimed at the general cargo higher density markets.

To overcome the standard A330's nose-down body angle on the ground, the A330F will make use of a revised nose landing gear layout. The same leg will be used, however it will be attached lower in the fuselage, requiring a distinctive blister fairing on the nose to accommodate the retracted nosegear.

Power is provided by two Pratt & Whitney PW4000 or Rolls-Royce Trent 700 engines.

Airbus has 66 firm orders from seven customers: Aircastle 15, Avion Aircraft Trading 8, Etihad Airways 3, Flyington Freighters 12, Guggenheim Aviation Partners 6, Intrepid Aviation Group 20 and MNG Airlines 2. Additionally ACT Airlines has signed an MOU for 2. [2] Deliveries will begin in late 2009. [3]

Other widebody freighters include the B767-300F, DC-10F, MD-11F,B777F.

A330-300

Air Canada Airbus A330-300.

The A330-300, which entered service in 1993, was developed as replacement for the A300. It is based on a stretched A300-600 fuselage but with new wings, stabilisers and fly-by-wire software.

The A330-300 carries 295 passengers in a three-class cabin layout (335 in 2 class and 440 in single class) over a range of 10,500 km (5,650 nautical miles). It has a large cargo capacity, comparable to early Boeing 747s. 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 of which are ETOPS-180 min rated. US Airways was the launch customer in the United States with nine A330-300s.

The direct Boeing equivalent is the Boeing 767-400ER.

A330 MRTT

File:RAF MRTT.JPG
A330 MRTT with two Eurofighter Typhoons

The Multi-Role Transport and Tanker version (MRTT) of the A330-200 provides aerial refueling and strategic transport. To date it has been selected by Australia, Saudi Arabia, the UAE and the UK. The KC-30, a derivative of the A330 similar to the MRTT, is in the running for the KC-X contract from the United States Air Force for 179 tankers to replace the aging KC-135 fleet. EADS is teamed with Northrop Grumman for the bid, competing against the KC-767.

Specifications

An Airbus A330-200 from TAP Portugal.
LTU Airbus A330-200 touching down RWY 23L at Düsseldorf International Airport.
Aircraft dimensions A330-200 A330-300
Overall length 58.8 m 63.6 m
Height (to top of horizontal tail) 17.40 m 16.85 m
Fuselage diameter 5.64 m
Maximum cabin width 5.28 m
Cabin length 45.0 m 50.35 m
Wingspan (geometric) 60.3 m
Wing area (reference) 361.6 m²
Wing sweep (25% chord) 30 degrees
Wheelbase 22.2 m 25.6 m
Wheel track 10.69 m
Basic operating data
Engines two CF6-80E1 or PW4000 or RR Trent 700
Engine thrust range 303-320 kN
Typical passenger seating 253 (3-class) / 293 (2-class) 295 (3-class) / 335 (2-class)
Range (w/max. passengers) 6,749 NM (12,500 km) 5,669 NM (10,500 km)
Cruising Speed Mach 0.82 (541 mph, 470 knots, 871 km/h at 35,000 ft cruise altitude)
Maximum Cruise Speed Mach 0.86 (568 mph, 493 knots, 913 km/h at 35,000 ft cruise altitude)
Takeoff run at MTOW 2,220 metres/7300ft 2,500 metres
Bulk hold volume (Standard/option) 19.7 / 13.76 m³
Design weights
Maximum ramp weight 230.9 (233.9 ) t
Maximum takeoff weight 230 (233) t
Maximum landing weight 180 (182) t 185 (187) t
Maximum zero fuel weight 168 (170) t 173 (175) t
Maximum fuel capacity 139,100 l 97,170 l
Typical operating weight empty 119.6 t 122.2 (124.5) t
Typical volumetric payload 36.4 t 45.9 t

A330 deliveries

2007 2006 2005 2004 2003 2002 2001 2000 1999 1998 1997 1996 1995 1994 1993 1992 1991
68 62 56 47 31 42 35 43 44 23 14 10 30 9 1 0 0

Incidents

Bmi A330-200 queueing for take off at London Heathrow Airport

(As of 2005)

  • Hull-loss Accidents: 2 with a total of 7 fatalities
    • On 30 June 1994, an A330 owned by Airbus on a test flight simulating an engine failure on takeoff crashed shortly after take-off from Toulouse, killing all on board [1]
    • On 15 March 2000, a 6-year-old Malaysia Airlines A330-300 aircraft was severely damaged by corrosive liquids that was being transported in the cargo hold on a passenger flight from Beijing to Kuala Lumpur. The corrosive liquid oxalyl chloride was mistakenly declared as non-toxic solid hydroxyquinoline. 18 canisters of the substance was transported via Kuala Lumpur intended to transit to Chennai. Five airport workers fell ill as they were unloading baggage from the aircraft at Kuala Lumpur after some of the canisters leaked and chemicals spilled into the aircraft's cargo hold, resulting in extensive corrosion damage to the fuselage, wing box structure and landing gear. The aircraft was subsequently declared written-off. [2] On June 12 2007, a court in Beijing ordered China National Chemical Construction Corp (the owner of the cargo) to pay US$65 million to Malaysia Airlines for the loss. [3]


External links

References

  1. ^ "Airbus aims to fill freighter void with A330 derivative." Flight International. March 14, 2006.
  2. ^ "ACT Airlines commits for two A330 freighters." Airbus. 17 August, 2006.
  3. ^ Flight International, 23-29 January 2007
  4. ^ "ASN Aircraft accident description Airbus A.330-243 4R-ALF - Colombo-Bandaranayake Internation Airport". Retrieved 2006-08-03.

See also


Related development

Aircraft of comparable role, configuration, and era

Related lists