Flight with disabled controls: Difference between revisions

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*[[American Airlines Flight 587]], [[Airbus A300]], November 12, 2001. This was the second-deadliest aviation accident in U.S. history, with 251 passengers and 9 crew members killed, as well as five people on the ground. According to the NTSB, the aggressive use of the rudder controls by the first officer stressed the composite vertical stabilizer until it separated from the aircraft. The complete loss of the vertical stabilizer meant the loss of all rudder control. As the pilots struggled to control the aircraft, it entered a flat spin. The resultant forces caused the engines to separate from the aircraft, and it slammed into the ground 14 seconds later.
*[[Air Transat Flight 961]], an [[Airbus A310]], on 6 March 2005, catastrophic structural failure: the rudder detached from the aircraft with a loud bang and the aircraft began a [[dutch roll]]. The pilots regained enough control, albeit with difficulty on controlling the aircraft laterally, to land the aircraft safely at Varadero-Juan Gualberto Gomez Airport.<ref>[http://www.bst.gc.ca/eng/rapports-reports/aviation/2005/a05f0047/a05f0047.pdf Flight 961 – Official accident report]. www.bst.gc.ca Retrieved: 1 June 2010</ref>
*[[Air Moorea Flight 1121]], a [[de Havilland Canada DHC-6 Twin Otter]], on 9 August 2007. Deterioration of the elevator cable from frequent takeoffs and landings, and likely jet-blast from larger aircraft, caused the cable to snap one minute after takeoff. The plane then nosedived and crashed into the ocean near [[Moorea-Temae Airport]] soon afterwards, killing all 19 passengers and the sole pilot.
 
===Control system mechanical failures===