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In-Flight Separation of Vertical Stabilizer American Airlines Flight 587 - Flight Path

Board Meeting Animations - In-Flight Separation of Vertical Stabilizer American Airlines Flight 587 Airbus Industrie A300-605R, N14053, Belle Harbor, New York, November 12, 2001 Presented October 26, 2004 Flight Path Simulations presented below used scene surveys, vehicle and scene testing, vehicle operating characteristics, pictures and witness statements. The depictions do not represent actual lighting and weather conditions at the time of the accident. This three-dimensional animated accident reconstruction shows most of the flight for American Airlines flight 587, which crashed shortly after takeoff from JFK International airport on November 12, 2001. The reconstruction exhibits information selected from the flight data recorder, excerpts from the cockpit voice recorder transcript, recorded radar data, and aircraft performance data. This reconstruction does not depict the weather or visibility conditions at the time of the accident. The animation shows a three-dimensional model of the airplane and its motion in the upper portion of the view. Selected comments from the cockpit voice recorder transcript or other annotations are superimposed as text in this area at the time they occurred. The lower portion of the view depicts a set of instruments and indicators, which display selected parameters from the flight data recorder. From left to right these are: •Attitude indicator showing pitch and roll attitude, control wheel/column icon depicting the control wheel (rotating right or left) and control column (moving up or down) inputs, and an indicator showing vertical acceleration. •The next box to the right depicts the data from the rudder pedal, rudder control surface, and the lateral acceleration parameters. •The last box shows a representation of the tail section as viewed from above and depicts the rudder control surface position relative to the vertical stabilizer. The red bars on the rudder pedal, rudder surface, and tail section indicators represent the relative position of the rudder limiting system. Additionally, the time of day (based on the FAA's Air Traffic Control clock), altitude in feet, and airspeed in knots are depicted as text. The animation starts with the airplane on the ground, taxiing to runway 31L. It shows the airplane's taxi, takeoff, climbout, and initial turn to the left. The rudder parameters are blanked out at the time the tail section separates from the airplane. The screen turns black at the point in time when the flight data recorder information ends (only cockpit voice recorder text or annotations are shown after this point). This animation does not include sound.