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Airbus A300: Encyclopedia BETA


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Airbus A300



On 26 April 1994 China Airlines(Taiwan) A300-600 crashed at the end of runway at Nagoya, Japan, killing all 15 crews and 249 of 264 passengers on board.

On 26 September 1997 Garuda Indonesia Flight 152 crashed while landing at Medan, Indonesia killing 234 aboard.

On 16 February 1998 China Airlines(Taiwan) A300-600; crashed into residental area close to CKS international airport near Taipei, Taiwan. All 196 people onboard were killed, including Taiwan's central bank president. Six people on the ground were also killed.

On 12 November 2001 American Airlines, Flight 587 crashed into the Belle Harbor neighborhood of Queens, New York shortly after takeoff from John F. Kennedy International Airport. All 260 people on board were killed, along with 5 people on the ground. The official NTSB report of 26 October 2004 stated the cause of the crash was the overuse of the rudder to counter wake turbulence (causing the tail to eventually break off).

On 22 November 2003 a European Air Transport A300B4-203F, operating on behalf of DHL, was hit by an SA-7 'Grail' missile after take-off from Baghdad International Airport. The aeroplane rapidly lost all hydraulic pressure and thus controls. The crew found that after extending the landing gear to create more drag, they could pilot the plane using differences in engine thrust and managed to land the plane with minimal further damage. The plane was later repaired and offered for sale (incident summary and photos).

Specifications (A300-600R)

, Airliners.net
crew=2capacity=266 passengerspayload main=39,885 kgpayload alt=87,930 lbspan main=44.84 mspan alt=147 ft 1 inlength main=54.08 mlength alt=177 ft 5 inheight main=16.62 mheight alt=54 ft 6.5 inarea main=260 m²area alt=2,800 ft²airfoil=empty weight main=115,000 kgempty weight alt=200,000 lbloaded weight main= loaded weight alt=useful load main=140,000 kguseful load alt=310,000 lbmax takeoff weight main=171,700 kgengine (jet)=General Electric CF6-80C2type of jet=turbofansnumber of jets=

** 2
thrust main=61,500 lbfthrust alt=274 kN**-or-
** 2× Pratt & Whitney PW-4000 turbofans, 58,000 lbf (258 kN) each>max speed main=
max speed alt=cruise speed main=897 km/hcruise speed alt=484 knots, 557 mph range main=7,500 kmrange alt=4,000 nm, 4,700 miceiling main= ceiling alt= climb rate main= climb rate alt= loading main= loading alt= thrust/weight=

Operators

References

External links

* Official site
* Pictures
* Aircraft-Info.net - Airbus A300-600
* Airbus A300 Production List
* Airbus A300-600 rudder problems

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