| Airbus A330 | |
|---|---|
| TAP Portugal A330-200 | |
| Type | Airliner |
| Manufacturer | EADS (Airbus S.A.S.) |
| Maiden flight | 1992-11-02 |
| Introduced | January 1994 with Air Inter |
| Primary users | Emirates Airline (29) Cathay Pacific (27) Qatar Airways (24) Northwest Airlines (23) |
| Number built | 464 (as of March 2007) |
| Unit cost | US$139.6 to $145.5 million in 2003 |
| Developed from | Airbus A300 |
| Variants | Airbus A330 MRTT Airbus A340 |
The Airbus A330 is a large-capacity, wide-body, medium-to-long-range commercial passenger airliner manufactured by EADS (Airbus S.A.S.). It was developed at the same time as the four-engined A340.
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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 February 2007 a total of 680 A330 had been ordered and 459 delivered.
There are two variants of the A330. The A330-300 was launched in 1987 with introduction into service in 1993. The A330-200 was launched in 1995 with introduction into service in 1998.
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 fuselage shrink. 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 was originally the 767-400ER and in the future will be the 787-9.
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 4,000nm / 7,400 km, or 69 tonnes up to 3,200nm / 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.
Airbus has so far secured commitments for 40 aircraft from five customers: Intrepid Aviation Group, Guggenheim Aviation Partners, Flyington Freighters, Avion Aircraft Trading and MNG Airlines. Deliveries will begin in late 2009[2].
Other widebody freighters include the B767-300F, DC-10F, MD-11F, and the larger B777F.
The Airbus A330 MRTT version of the A330-200 provides aerial refueling and strategic transport. To date it has been selected by Australia and the UK.
The KC-30, a derivative of the A330 similar to the MRTT, is in the running to land 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. If the contract is won, it will require EADS to invest approximately US$600 million in an assembly plant in the United States. The competing KC-767 won the original competition in 2002. However, this contract was cancelled, due to a corruption scandal, in December 2003. In the new competition Airbus will again face competition from the KC-767.
In early 2006, the United States Congress passed a bill which reversed an earlier amendment barring Airbus from bidding for the contract.[3]
To support the possible USAF contract, Airbus has announced that it will create an engineering and manufacturing site at Mobile, Alabama.
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 new 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 777-200.
| 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) | 12,500 km | 10,500 km |
| Max. operating Mach number | 0.86 M | |
| Takeoff run at MTOW | 2,220 metres | 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 |
| 2007 | 2006 | 2005 | 2004 | 2003 | 2002 | 2001 | 2000 | 1999 | 1998 | 1997 | 1996 | 1995 | 1994 | 1993 | 1992 | 1991 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 17 | 62 | 56 | 47 | 31 | 42 | 35 | 43 | 44 | 23 | 14 | 10 | 30 | 9 | 1 | 0 | 0 |
(As of 2005)
Civil: A300 (-600ST Beluga) · A310 · A320 family · A330 · A340 · A380
Military: A310 MRTT · A330 MRTT
In development/proposed: A350 · A400M · NSR
Other supported types: Sud Aviation Caravelle · Aérospatiale-BAC Concorde
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