by beaky » Thu May 06, 2010 7:19 am
Even if there is a reliable GPS readout, that's only groundspeed. At the FLs, where winds can exceed 100 kts, that could have very little to do with airspeed.
As far as multiple system failures go, if I remember correctly, it was determined that there may have been a pitot blockage (did the pitot heat fail also?), in which case even "steam gauge" backups would be useless.
Perhaps this was not the case, but in the event that you have more than one electronic airspeed display, and analog backup gauges, all fed from separate pitot probes... the question is: which one do we trust? While you're trying to decide, of course, the airplane is still flying, and things can get out of hand very quickly.
It's not easy to maintain flying speed in a heavy jet by only neeedle/ball and altimeter,"feel" or slipstream noise in the best conditions, and these poor souls were, apparently, in some nasty stuff as they tried to figure out what was going on. Even if they still had at least one reliable artificial horizon or some sort of A of A indicator, in turbulence in IMC it would take a miracle to avoid getting outside the speed envelope, in either direction. In smoother air, maybe they could have just set the trim for best glide (provided they had a reliable indicator of trim tab position) and use rudder only to keep the wings level (by monitoring the ball) until they descended into VMC, at which point they might have more options.
Last edited by
beaky on Thu May 06, 2010 7:19 am, edited 1 time in total.