Enviado por
Miguel Arana

Incidente 737 de ANA

 Fecha y hora de inicio
 
30/09/2011 04:00:54
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http://www.elmundo.es/elmundo/2011/09/30/internacional/1317335828.html

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Respondido por
José María Rebés

 Respuesta 2
 
30/09/2011 11:20:08

http://www.avherald.com/h?article=4428f2f7&opt=0

An All Nippon Airways Boeing 737-700, registration JA16AN performing flight NH-140 from Okinawa to Tokyo Haneda (Japan) with 112 passengers and 5 crew, was enroute at FL410 about 23nm south of Hamamatsu (Japan) when the aircraft violently rolled left causing injuries to two flight attendants and descended by about 6000 feet levelling off at FL350 again. The flight continued to Tokyo's Haneda Airport for a safe landing. The two injured flight attendants were delivered to a hospital with flesh wounds.

The airline reported, that the captain (64, 16,000 hours total experience) had taken a toilet break and was about to return to the cockpit requiring the first officer (38, 2400 hours total experience) to open the cockpit door. The switch to open the cockpit door is located about 10 centimeters/ 4 inches away from the rudder trim switch. By mistake the first officer operated the rudder trim switch instead of the door opening switch causing the aircraft to violently roll left and descend by about 6000 feet before the first officer was able to return the aircraft to stable level flight. The captain subsequently entered the cockpit. Two cabin crew received minor injuries (flesh wounds), no other injuries occurred. There was no turbulence in the area at the time of the occurrence.

Japan's Transportation Safety Board (JTSB) rated the occurrence a serious incident, opened an investigation and dispatched three investigators on site.

On Sep 28th the JTSB released a progress report in Japanese that the aircraft was enroute at FL410 on autopilot on a heading of 052 degrees, when the captain left the cockpit briefly. Upon returning to the cockpit the first officer had to operate the door opening switch, however, the flight data recorder at that time showed the left rudder trim button was operated. Following that button press (editorial note: there is no mention that the autopilot disconnected) the aircraft rolled left to a bank angle of 131.7 degrees, the nose dropped to 35 degrees nose down. During the resulting descent the aircraft exceeded its Mmo of 0.82 reaching 0.828 mach and experienced a vertical acceleration of +2.68G above the limit of +2.5G. The first officer was able to stabilize the aircraft again at FL347 after a loss of 6300 feet of altitude on a heading of 257 degrees. The investigation is ongoing.






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