Aircraft Data for: Airbus A310 300

Updated: Mar. 15th 2009

Summary

The Airbus A310 is a twin engine, wide body medium/long range airliner, Derived from the A300, with shortened fuselage and new wings and flightdeck, Many have been converted to freighters or military tankers. Production ceased in 2007.

The -300 is the longer range development of the basic series 200, with extra fuel tankage in the tailplane. The -300 has winglets and is cleared for transoceanic flights to ETOPS standards .

  Country of origin: France      First flight: 1985      No. built: 170      No. in service: 150 (approx.)     Crew: 2      Passengers: 210 - 280
 
Power 2 x CFM CFM56 (18500 - 34000 lbf), General Electric CF6 (41500 - 69800 lbf), Pratt & Whitney JT9D (45800 - 56000 lbf) or Pratt & Whitney PW4000 (52000 - 99040 lbf) turbofan engines
 Typical choices would be the CFM56-80C2A8 at 59000lb thrust, or the PW4156 at 56000lb.
 
Dimensions:
Length: 153 ft. 1 in.
Wing Span: 144 ft. 0 in.
Height: 51 ft. 0 in.
Empty Weight: 179,025 lbs.
Max. Weight: 361,560 lbs.  (Max take-off weight option)
 Performance: 
Max. speed: 484 kts
Cruise speed: 430 kts
Ceiling: 40,000 ft.
Normal range: 4,310 nm
Max. range: 5,170 nm (Range for high gross weight CFM56 version)
 

Aircraft Details:
Airbus A310 300 >>>>
Kuzu Airlines Cargo
 
Location:
Tel Aviv, Israel
 
Photo by:  Yochai
Date:  2010-03-00
Image ID:  97966
 
Seen in ULS Cargo colours after arrival from Almaty, Kazakhstan.

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