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Description
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The A330-200 was made to battle with the Boeing 767-300ER. It is similar to the A340-200 and a shorter than A330-300. Its vertical fin is taller than A330-300 to bring back its effectiveness because it has shorter moment arm of the shorter fuselage. It also has added fuel capacity and, has the same MTOW with A330-300.
The development for this aircraft has started in November 1995, and the initial order was placed in February of 1996. The initial flight took place on August 13 1997. The certification and first customer deliveries, was to ILFC/Canada 3000, in April of 1998.
Capacity
Flight crew 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
Dimension
Overall length 58.8 m (192 ft 11 in) Height 17.40 m (57 ft 1 in), Wingspan (geometric) 60.3 m (197 ft 10 in)
Weights
Maximum takeoff weight 230 (233)
Maximum landing weight 180 (182) t
Speed and Range
Cruising Speed Mach 0.82 (871 km/h, 541 mph, 470 knots at 35,000 ft (10,7 km) cruise altitude)
Takeoff run at MTOW 2,220 metres (7,300 ft)
Engines
two CF6-80E1 or PW4000 or RR Trent 772B
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