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Airbus A310
Airbus A310 is a medium- to long-range widebody airliner developed from the Airbus A300 and manufactured by Airbus. Perhaps the greatest attribute of the A310 is that of range. The A310-300's range exceeds all A300 models. The A300 and A310 commonality which has become one of the Airbus family's greatest marketing points: A300-600 and A310 pilots can qualify for the other aircraft with only short time of training.        The fuselage of A310 was shortened by 13 frames compared to the A300B, reducing seating to around 200 to 230 passengers and a new higher aspect ratio wing of smaller span and area was developed. New and smaller horizontal tail surfaces, fly-by-wire outboard spoilers and a two crew EFIS flight deck were incorporated. The A310 (along with the A300) will cease production in July of 2007.        The program was launched in July 1978 and the first flight of the A310 occurred on April 3, 1982. Service entry was with Lufthansa in April 1983. Early production A310s did not have the small winglets that became a feature of later build A310-200s and the A310-300. The A310-300 is a longer range, this version can carry a further 7000kg (15,430lb) of fuel in the tailplane.
SPECIFICATIONS A310
	A310-200	A310-300
Passengers (2 classes config.)	207	218
Passengers (single classes config.)	265	282
Cargo loading standard	69 cu.m	79.9 cu.m
Range	4815 km.	8519 km.
Number of engine	2	2
Engine types	GE-CF6-80A	GE-CF6-80C2 & PW 4152
Engine Thrust	21,772 lbs	24,267-26,503 lbs.
Wing dimensions
wing span	43.90 m.	43.90 m.
wing area	219 sqm.	219 sqm.
wing sweep	28 degrees	28 degrees.
Max.operating speed	0.84 mach	0.84 mach
Max.take off weight	141,974 kgs.	150,004 kgs.
Max.landing weight	117,934 kgs.	123,015 kgs.
Operating weight empty	76,884 kgs.	80,830 kgs.
Max.fuel capacity	55,200 lit	61,260 lit
Cockpit A310
1 nm.(nautical mile) = 1.15155 miles, 1 kt (knot) = 1.15155 mile / hr. 1 mach = 761 mph.(SL,ISA)
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