Airbus A330 | |
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Northwest Airlines A330-300 | |
Role | Wide-body jet airliner |
Manufacturer | Airbus |
First flight | 2 November 1992 |
Introduced | January 1994 with Air Inter |
Primary users | Northwest Airlines Qatar Airways Emirates Cathay Pacific |
Number built | 572 as of 31 October 2008 [1] |
Unit cost | A330-200: US$176.3 to $185.5m (2008)[2] A330-300: $195.9 to $205.7m (2008) A330-200F: $180.6 to $187.7m (2008) |
Developed from | Airbus A300 |
Variants | Airbus A340 Airbus A330 MRTT Northrop Grumman KC-45 |
The Airbus A330 is a large-capacity, wide-body, twin-engine, medium-to-long-range commercial passenger airliner. It was developed at the same time as the four-engined Airbus 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 was launched in 1987; airlines purchased it to replace the McDonnell Douglas DC-10. The A330 is 38% more fuel efficient than the DC-10.[3]
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, and the nose/cockpit section and the fly-by-wire system and flightdeck are inherited from the A320. Both the A330 and A340 are assembled on the same final assembly line at Toulouse-Blagnac, France.
By the end of July 2008, a total of 1,006 A330s[4] had been ordered and 555 delivered. The 1,000 milestone was passed with orders from the 2008 Farnborough Air Show.
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 with passenger, freighter and tanker (Airbus A330 MRTT) variants available.
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 Maximum Take-Off Weight (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 direct Boeing equivalent is currently the 767-300ER and in the future will be the 787-8. The A330-200 has sold strongly since its launch.
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.[5] The A330-200F re-emerged at the 2006 Farnborough Airshow 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 nose-gear.
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. [6] Deliveries will begin in late 2009. [7]
Other wide-body freighters include the B767-300F, DC-10F, MD-11F,B777F.
Airbus plans to assemble the A330-200F in the USA, along with the proposed KC-45A, at a new assembly line at Brookley Field in Mobile, Alabama.
In an announcement on 9 September 2008, Airbus released plans for a higher gross weight version of the A330-200 to more effectively compete against the Boeing 787. This new version will have a 238t MTOW and a range of 6,840nmi. Airbus believes the first 20 787-8s will have a 219.5t MTOW be limited to a 6,720nmi range, around 1,000nmi less than the figures published by Boeing.[8]
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 systems.
The A330-300 carries 295 passengers in a three-class cabin layout (335 in 2 class and 440 in single class layout) 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. French domestic airline Air Inter was the launch customer for the aircraft.
The direct Boeing equivalents are the Boeing 777-200 and the Boeing 767-400ER.
By the end of October 2008 a total of 1,012 aircraft of the A330 have been ordered (554 A330-200, 74 A330-200F and 384 A330-300) and 572 delivered (322 A330-200 and 250 A330-300).[12]
2008 | 2007 | 2006 | 2005 | 2004 | 2003 | 2002 | 2001 | 2000 | 1999 | 1998 | 1997 | 1996 | 1995 | 1994 | 1993 |
63 | 68 | 62 | 56 | 47 | 31 | 42 | 35 | 43 | 44 | 23 | 14 | 10 | 30 | 9 | 1 |
(As of October 2008)
Aircraft dimensions | A330-200 | A330-300 | A330-200F |
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Overall length | 58.8 m (192 ft 11 in) | 63.6 m (208 ft 8 in) | 58.8 m (192 ft 11 in) |
Height (to top of horizontal tail) | 17.40 m (57 ft 1 in) | 16.85 m (55 ft 3 in) | 16.9 m (55 ft 5 in) |
Fuselage diameter | 5.64 m (18 ft 6 in) | ||
Maximum cabin width | 5.28 m (17 ft 4 in) | ||
Cabin length | 45.0 m (147 ft 8 in) | 50.35 m (165 ft 2 in) | 40.8 m (133 ft 10 in) |
Wingspan (geometric) | 60.3 m (197 ft 10 in) | ||
Wing area (reference) | 361.6 m² (3,892 sq ft) | ||
Wing sweep (25% chord) | 30 degrees | ||
Wheelbase | 22.2 m (72 ft 10 in) | 25.6 m (84 ft) | 22.2 m (72 ft 10 in) |
Wheel track | 10.69 m (35 ft 1 in) | ||
Basic operating data | |||
Engines | two CF6-80E1 or PW4000 or RR Trent 772B | PW4000 or Trent 700 | |
Engine thrust range | 303-320 kN | ||
Typical passenger seating | 253 (3-class) 293 (2-class) |
295 (3-class) 335 (2-class) |
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Range (w/max. passengers) | 6,749 NM (12,500 km) |
5,669 NM (10,500 km) |
4,000 NM (7,400 km) |
Cruising Speed | Mach 0.82 (871 km/h, 541 mph, 470 knots at 35,000 ft (10,7 km) cruise altitude) | ||
Maximum Cruise Speed | Mach 0.86 (913 km/h, 568 mph, 493 knots at 35,000 ft (10,7 km) cruise altitude) | ||
Takeoff run at MTOW | 2,220 metres/7300ft | 2,500 metres (8,202 ft) | - |
Bulk hold volume (Standard/option) | 19.7 / 13.76 m³ | 475 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 | 182 (187) t |
Maximum zero fuel weight | 168 (170) t | 173 (175) t | 173 (178) t |
Maximum fuel capacity | 139,100 L | 97,170 L | 139,100 L |
Typical operating weight empty | 120 t | 122 (124) t | 109 t |
Typical volumetric payload | 36.4 t | 45.9 t | 69 t |
Model | Date | Engines |
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A330-201 | 2003 | GE CF6-80E1A2 |
A330-202 | 1998 | GE CF6-80E1A4 |
A330-203 | 2002 | GE CF6-80E1A3 |
A330-223 | 1999 | PW4168A |
A330-243 | 2000 | RR Trent 772B-60 |
A330-301 | 1993 | GE CF6-80E1A2 |
A330-302 | 2007 | GE CF6-80E1A4 |
A330-303 | 2007 | GE CF6-80E1A3 |
A330-321 | 1999 | PW4164 |
A330-322 | 1999 | PW4168 |
A330-323 | 1999 | PW4168B |
A330-341 | 2000 | RR Trent 768-60 |
A330-342 | 2000 | RR Trent 772-60 |
A330-343 | 2000 | RR Trent 772B-60 |
Related development
Comparable aircraft
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