Airbus A330

Airbus A330
Northwest Airlines A330-300
Role Wide-body jet airliner
Manufacturer Airbus
First flight 2 November 1992
Introduced January 1994 with Air Inter
Primary users Cathay Pacific
Delta Air Lines
Qatar Airways
Emirates
Number built 710 as of 31 July 2010[1]
Unit cost A330-200: US$170.9 to $200.8m (2008)[2]
A330-300: $195.9 to $205.7m (2008)[3]
A330-200F: $180.6 to $187.7m (2008)[3]
Developed from Airbus A340
Variants 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. Built at Toulouse in France by Airbus, over 700 units have been delivered.

First flown in 1992, the A330 was developed at the same time as the four-engined Airbus A340, and was designed with common fuselage and wing components. The first variant (series 300) was delivered to Air Inter in 1994 and was followed by the slightly shorter series 200.[4] This has been followed by dedicated freighter and tanker variants.

Contents

Design and development

Background

In the 1970s, Airbus was considering a larger derivative of the A300, the B9 and the smaller B10. The B9 was a stretched fuselage version of the A300B2. The B10 was a shortened fuselage version of the A300B2, and went on to become the A310. During the 1970s and into the 1980s, the availability of more powerful engines led Airbus to study even larger four and twin-engine designs.[5]

Programme launch

The A330 and A340 programs were jointly launched in November 1987.[4] Airlines purchased it to replace the McDonnell Douglas DC-10. The A330 is 38% more fuel efficient than the DC-10.[6]

Airbus intended the A330 to compete directly in the ETOPS (Extended-range Twin-engine Operation Performance Standards) market, specifically with the Boeing 767. In November 2009 the A330 became the first aircraft to receive ETOPS-240 approval, which is now offered by Airbus as an option.[7]

Air Algérie Airbus A330-200 Landing in Montréal-Trudeau

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 November 2009 a total of 1,035 A330s have been ordered and 654 delivered.[1] The 1,000 milestone was passed with orders from the 2008 Farnborough Air Show. The largest operators of the A330 are Delta Air Lines and Cathay Pacific with 32 aircraft in service each. Airbus expects the A330 to continue selling until at least 2015.[8]

Variants

There are two main variants of the A330. The A330-300 was launched in 1987 with entry into service in 1994. The A330-200 was launched in 1995, introduced in 1998 with passenger, freighter and tanker (Airbus A330 MRTT) variants available.

A330-200

The A330-200 was developed to compete with the Boeing 767-300ER. The A330-200 is similar to the A340-200 and 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 gas turbine engines. First customer deliveries, to ILFC/Canada 3000, were in April 1998.

The A330-200 is available as an ultra-long range corporate-jet by Airbus Executive and Private Aviation. The Boeing equivalent is currently the 767-300ER and in the future will be the 787-8.

First Flight: August 13, 1997 (msn 181) (General Electric CF6-80E1A2 powered aircraft).
Certification (JAA): March 31, 1998 (GE CF6-80E1A2 powered aircraft).
Certification (FAA): March 31, 1993 (GE CF6-80E1A2 powered aircraft).
First Delivery: April 29, 1998 Canada 3000 (msn 211).

A330-200HGW

In May 2009, Airbus released plans for a higher gross weight version of the A330-200 to more effectively compete against the Boeing 787-8. This new version will have a 238 t MTOW and its new range will be up to 7,200 nmi (13,300 km). The new-build A330-200HGW will have the option of an extra 3.4 tonnes of payload or an additional 330 nm range over the standard 233 tonnes A330-200s. Airbus believes the first 20 787-8s will have a 219.5 t MTOW and be limited to a 6,720 nmi (12,450 km) range, around 1,000 nmi (1,900 km) less than the figures published by Boeing.[9] Korean Air became the first customer on 27 February 2009, ordering six with deliveries starting in 2010.[10]

A330-200F

Due to flagging A300-600F and A310F sales, Airbus began marketing a freighter derivative of the A330-200 around 2000-2001, although it was not launched at that time.[11] The A330-200F re-emerged at the 2006 Farnborough Airshow and received its industrial go-ahead in January 2007. The first A330-200F has been rolled out in Toulouse on October 20, 2009. The first flight was on November 5, 2009.

Airbus A330-200F, on display at the Singapore Airshow 2010

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 70 tonnes up to 3,200 NM / 5,930 km. It introduces a new versatile main-deck cargo loading system that is able to accommodate both pallets and containers. Several different arrangements are possible on the main deck, taking up to 23 (88 in x 125 in ) Side-by-Side (SBS) pallets, aimed at the high volume, high value commodities or an optional, requiring the installation of optional secondary structure, Single Row (SR) loading of 16 pallets (96 in x 96 in x 125 in 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 uses a revised nose landing gear layout. The same A330-200 leg is used, however its attachment points are lower in the fuselage, requiring a distinctive blister fairing on the nose to accommodate the retracted nose-gear. This provides a level deck for cargo loading.[12] Power is provided by two Pratt & Whitney PW4000 or Rolls-Royce Trent 700 engines. General Electric does not plan to offer a powerplant for the A330-200F.[13]

As well as new-build freighters, Airbus has proposed passenger-to-freighter conversions of existing A330-200 airliners.[14]

As of 31 May 2010, Airbus had 64 firm orders from nine customers: Aircastle (3), BOC Aviation (5), Etihad Airways (2), Flyington Freighters (12), Intrepid Aviation Group (20), MatlinPatterson (6), Malaysia Airlines (2), MNG Airlines (4), OH, Avion LLC (8) and Turkish Airlines (2). Additionally ACT Airlines has signed an MOU for 2 aircraft.[15] The first delivery was to Etihad Crystal Cargo in August 2010.[16]

Comparable freighters include Boeing's 767-300F & 777F, Lockheed's L-1011 Tristar (after conversion) and McDonnell Douglas' DC-10F & MD-11F.

Roll-out: October 20, 2009 (A330-223F msn 1004 Pratt & Whitney 4170 powered aircraft).
First Flight: November 5, 2009 (msn 1004)
Certification (EASA): April 9, 2010 (Pratt & Whitney 4170 and Rolls Royce Trent 772B-60).
Certification (FAA): TBA.
First Delivery: August 9, 2010 to Etihad Crystal Cargo (MSN 1032). [17]

A330-300

US Airways A330-300 taking off from London Gatwick Airport.
An A330-300 in Delta Air Lines livery landing at Amsterdam.

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.

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 closest Boeing competitors are the Boeing 777-200 and, formerly, the McDonnell Douglas MD-11, which is no longer in production.

Roll-out: October 14, 1992 (GE CF6-80E1A2 powered aircraft).
First Flight: November 2, 1992 (msn 012).
Certification (JAA): October 21, 1993 (GE CF6-80E1A2 powered aircraft).
Certification (FAA): October 21, 1993 (GE CF6-80E1A2 powered aircraft).
First Delivery: December 30, 1993 Air Inter (msn 037).
Entry into service: January 17, 1994 Air Inter on Paris (Orly) and Marseille in a 412 seat configuration.

Tanker derivatives

A multi-role tanker and transport variant based on the series 200 was developed as the Airbus A330 MRTT. This was further developed as the Northrop Grumman KC-45, which won a United States Air Force order, which has since been cancelled.

Airbus A330 MRTT
The Multi-Role Transport and Tanker version (MRTT) of the A330-200 provides aerial refueling and strategic transport. To date it has been ordered by Australia, Saudi Arabia, the UAE, and the UK.
Northrop Grumman KC-45
On 29 February 2008 the United States Air Force announced that an American assembled variant of the A330 MRTT, now designated KC-45A by the USAF, had been selected to replace the Boeing KC-135 Stratotanker.[18] The replacement process has been mired in controversy, instances of corruption, and allegations of favouritism.[19][20][21][22] In July 2010 EADS submitted a tanker bid to the Air Force without Northrop Grumman as a U.S. partner.[23][24]

Operators

A330 deliveries

By the end of July 2010 a total of 1,092 aircraft of the A330 have been ordered (580 A330-200, 64 A330-200F and 448 A330-300) and 710 delivered (392 A330-200 and 318 A330-300).[1]

2010 2009 2008 2007 2006 2005 2004 2003 2002 2001 2000 1999 1998 1997 1996 1995 1994 1993
47 76 72 68 62 56 47 31 42 35 43 44 23 14 10 30 9 1

Accidents and incidents

As of 12 May 2010, the Airbus A330 has been involved in 13 incidents,[25] including three confirmed hull-loss accidents and three other losses, for a total of 338 fatalities.[26]

Notable accidents and incidents
Planform view of a Cyprus Airways A330-200 taking off. The undercarriage has fully retracted.

Specifications

A330-200 A330-200F A330-300
Cockpit crew Two
Seating capacity 293 (2-class, typical)
253 (3-class, typical)
70t cargo &

Up to 12 couriers [3]

335 (2-class, typical)
295 (3-class, typical)
Length 58.80 metres (192 ft 11 in) 63.60 metres (208 ft 8 in)
Wingspan 60.3 metres (197 ft 10 in)
Wing area 361.6 square metres (3,892 sq ft)
Wing sweepback 30°
Tail height 17.40 metres (57 ft 1 in) 16.90 metres (55 ft 5 in) 16.85 metres (55 ft 3 in)
Cabin width 5.28 metres (17 ft 4 in)
Fuselage width 5.64 metres (18 ft 6 in)
Cargo capacity 19.7 cubic metres (700 cu ft) 475 cubic metres (16,800 cu ft) 19.7 cubic metres (700 cu ft)
Operating empty weight (typical) 119,600 kilograms (264,000 lb) 109,000 kilograms (240,000 lb) 124,500 kilograms (274,000 lb)
Maximum Takeoff Weight (MTOW) 230,000 kilograms (510,000 lb)
to 238,000 kilograms (520,000 lb)
227,000 kilograms (500,000 lb)
to 233,000 kilograms (510,000 lb)
230,000 kilograms (510,000 lb)
to 233,000 kilograms (510,000 lb)
Cruising speed Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft)
Maximum speed Mach 0.86 (913 km/h/563 mph at 11,000 m/36,000 ft)
Maximum range, fully loaded 7,250 nautical miles (13,430 km; 8,340 mi) 4,000 nautical miles (7,400 km; 4,600 mi) 5,850 nautical miles (10,830 km; 6,730 mi)
Takeoff run at MTOW 2,220 metres (7,280 ft) n/a 2,500 metres (8,200 ft)
Maximum fuel capacity 139,090 litres (30,600 imp gal; 36,740 US gal) 97,530 litres (21,450 imp gal; 25,760 US gal)
Service ceiling 41,100 ft (12,527 m)
Engines (×2) CF6-80E1
PW4000
RR Trent 700
PW4000
RR Trent 700
CF6-80E1
PW4000
RR Trent 700
Thrust (×2) 303–320 kilonewtons (68,000–72,000 lbf) 303–316 kilonewtons (68,000–71,000 lbf) 303–320 kilonewtons (68,000–72,000 lbf)

Sources: Airbus [46]

LTU Airbus A330-200 touching down at Düsseldorf International Airport.

Engines

Model Date Engines
A330-201 2003 GE CF6-80E1A2
A330-202 1998 GE CF6-80E1A4 / CF6-80E1A4B
A330-203 2002 GE CF6-80E1A3
A330-221 1999 PW4164
A330-222 1999 PW4168
A330-223 1999 PW4168A / PW4168A-1D / PW4168B / PW4170
A330-223F 2010 PW4170
A330-243 2000 RR Trent 772B-60
A330-243F 2010 RR Trent 772B-60
A330-244 2007 RR Trent 775-60
A330-301 1993 GE CF6-80E1A2
A330-302 2007 GE CF6-80E1A4 / CF6-80E1A4B
A330-303 2007 GE CF6-80E1A3
A330-321 1999 PW4164
A330-322 1999 PW4168
A330-323 1999 PW4168A / PW4168A-1D / PW4168B / PW4170
A330-341 2000 RR Trent 768-60
A330-342 2000 RR Trent 772-60
A330-343 2000 RR Trent 772B-60
A330-343 2007 RR Trent 772C-60

See also

Related development

Comparable aircraft

Related lists

References

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External links