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American Airlines Flight 587
Occurrence summary
Date
November 12, 2001(2001-11-12)
Type
Pilot error, design and training failures
Site
Queens, New York City, New York, United States
Passengers
251
Crew
9
Injuries
1 (ground)
Fatalities
265 (including 5 on the ground)
Survivors
0
Aircrafttype
Airbus A300-600
Operator
American Airlines
Tail number
N14053
Flight origin
John F. Kennedy International Airport
Destination
Las Amicas International Airport ,Dominican Republic
American Airlines Flight 587, an Airbus A300, crashed into the Belle Harbor neighborhood of Queens; a borough of New York City in New York, United States, shortly after takeoff from John F. Kennedy International Airport on November 12, 2001. Excluding the events of 9/11, this is the second deadliest U.S. aviation accident to date, after American Airlines Flight 191.
This accident is also the second highest death toll of any aviation accident involving an Airbus A300 after Iran Air Flight 655. It has surpassed China Airlines Flight 140 which crashed in Nagoya with 264 fatalities.
The accident took place two months after the September 11th attacks on the World Trade Center in Manhattan. Several factors, such as the date, aircraft size, airline, and location in New York, raised concerns that the crash was caused by another terrorist attack. Terrorism was officially ruled out as the cause by the National Transportation Safety Board, which instead attributed the disaster to the co-pilot's overuse of rudder controls.
Contents
1 Synopsis
2 Investigation
3 Aftermath
4 Responsibility
5 Victims
6 Memorial
7 Television documentaries
8 See also
9 References
10 External links
//
Synopsis
Flight 587, circled in white, can briefly be seen in this video still moving downward with a white streak behind the aircraft. This video, released by the NTSB, was recorded by a tollbooth camera located on the Marine Parkway-Gil Hodges Memorial Bridge.
On November 12, 2001, about 09:16 eastern standard time, American Airlines flight 587, an Airbus Industrie A300-605R, N14053, crashed into Belle Harbor, a New York City residential area, shortly after takeoff from John F. Kennedy International Airport, New York. Flight 587 was a regularly scheduled passenger flight to Las Amicas International Airport, Santo Domingo, Dominican Republic, with 2 flight crew members, seven flight attendants, and 251 passengers aboard the plane. Ed States served as the captain, and Sten Molin served as the first officer.
The plane's vertical stabilizer and rudder separated in flight and fell into Jamaica Bay, about 1 mile north of the main wreckage site. The plane's engines subsequently separated in flight and fell several blocks north and east of the main wreckage site. All 260 people aboard the plane and 5 people on the ground died, and the impact forces and a post-crash fire destroyed the plane. Flight 587 operated under the provisions of 14 Code of Federal Regulations Part 121 on an instrument flight rules flight plan. Visual meteorological conditions (VMC) prevailed at the time of the accident.
Investigation
National Transportation Safety Board (NTSB) employee Brian Murphy (second from right) updates NTSB Chairman Marion Blakey (third from right) on the investigation of the tail fin and rudder from AA flight 587 (February 11, 2002)
The A300-600, which took off minutes after a Japan Airlines Boeing 747 on the same runway, flew into the larger jet's wake, an area of turbulent air referred to as wake turbulence. The first officer attempted to keep the plane upright with aggressive rudder inputs. The strength of the air flowing against the moving rudder stressed the aircraft's vertical stabilizer and eventually snapped it off entirely, causing the aircraft to lose control and crash. The National Transportation Safety Board (NTSB) concluded that the enormous stress on the rudder was due to the first officer's "unnecessary and excessive" rudder inputs, and not the wake turbulence caused by the 747. The NTSB further stated "if the first officer had stopped making additional inputs, the aircraft would have stabilized". However, contributing to these rudder pedal inputs were characteristics of the Airbus A300-600 sensitive rudder system design and elements of the American Airlines Advanced Aircraft Maneuvering Training Program. The A300 family has the distinction of having the lightest breakout force and the highest number of degrees of rudder travel per pound of force of any other transport category aircraft. Once a pilot initiates rudder movement, he or she will be challenged with the most sensitive rudder handling qualities of any transport category airplane. This...(and so on)
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