Hola Woqr te pongo el enlace para que leas el informe final si tienes interes.
Fijate en los siguientes minutos, donde creo que esta la clave
2 h 10 min y 47 seg y 2 h 10 min y 51 seg (te adjunto text extraido en Ingles)
At 2 h 10 min 47, the thrust controls were pulled back slightly to 2/3 of the IDLE/
CLB notch (85% of N1). Two seconds later, the pitch attitude came back to a little
above 6°, the roll was controlled and the angle of attack was slightly less than 5°.
From 2 h 10 min 50, the PNF called the Captain several times.
At 2 h 10 min 51, the stall warning triggered again, in a continuous manner. The
thrust levers were positioned in the TO/GA detent and the PF made nose-up
http://www.bea.aero/en/enquetes/flig...t.final.en.php
Otro debate interesante es el sistema "joystick" de Airbus, ya que el Piloto mas experimentado (el que sustituia al Capitan) no tenia forma de saber lo que estaba haciendo el copiloto. En otro tipo de avion con "cuernos" esto no hubiera pasado.
Un saludo. Coronadobx