Aircraft Technical Data
|Country of Origin||European consortium|
|Type||Long range widebody airliner|
The A330-200 is the newest member of Airbus' widebody twinjet family and is a long range, shortened development of the standard A330, developed in part as a replacement for the A300-600R and a competitor to the 767-300ER. Airbus launched development of the A330-200 in November 1995, followed by the first customer order, for 13 from ILFC, placed in February 1996. First flight was on August 13 1997, with certification and first customer deliveries,to ILFC/Canada 3000, in April 1998. The A330-200 is based on the A330-300 and shares near identical systems, airframe, flightdeck and wings, the only major difference being the fuselage length. Compared with the 300 the A330-200 is 10 frames shorter, and so has an overall length of 59.00m (193ft 7in), compared with 63.70m (209ft 0in) for the standard length aircraft. This allows the A330-200 to seat 256 passengers in a three class configuration, or alternatively 293 in two classes. Because of its decreased length the A330-200 features enlarged horizontal and vertical tail surfaces (to compensate for the loss of moment arm with the shorter fuselage). Another important change is the addition of a centre fuel tank, which increases the A330-200's fuel capacity over the 300's, and results in the 200's 11,850km (6400nm) range. Like the A330, engine options are the GE CF6-80, Pratt & Whitney 4000 series and the RollsRoyce Trent 700. The A330-200 has sold quite strongly since its launch. Among the initial A330-200 customers are, apart from ILFC, Canada 3000, Korean Air, Austrian, Air Transat, Emirates, Swissair, Sabena, Monarch, Asiana, TAM, and Air Lanka.
|Powerplants||A330-200 - Choice of two 300.3kN (67,500lb) General Electric CF6-80E1A2s, 286.7kN (64,000lb) Pratt & Whitney PW-4164s, or PW-4168s or 302.5kN (68,000lb) RollsRoyce Trent 768 or Trent 772 turbofans.|
|Performance||Max cruising speed 880km/h (475kt) at 33,000ft, economical cruising speed 860km/h (464kt). Range with max passengers and reserves at 230t MTOW 11,850km (6400nm), at 217t MTOW 8890km (4800nm).|
|Weights||A330-200 - Operating empty 120,150kg (264,875lb) with CF6 engines, 120,750kg (266,200lb) with PW4168s, or 120,250kg (265,150lb) with Trents. Max takeoff 230,000-233,000kg (507,050-513,670lb).|
|Dimensions||Wing span 60.30m (197ft 10in), length 59.00m (193ft 7in), height 16.83m (55ft 2in). Wing area 363.1m2 (3908.4sq ft).|
|Capacity||Flightcrew of two. Passenger seating arrangements for 256 in three classes or 293 in two classes. Front and rear underbelly cargo holds can take 26 LD3 containers or six freight pallets and passenger baggage.|
|Production||Total A330-200 built stood at 108 at June 2002. Deliveries began in April 1998.|
|Related Links||Airbus A330-200|
The backbone of this section is from the The International Directory of Civil Aircraft by Gerard Frawley and used with permission. To get your own copy of the book click here.