So, what does the 'Unreliable airspeed' procedure include, and would it have helped?
It's a simple enough procedure. Basically it tells you to turn off autopilot, autothrust, and flight director, and asks for the selection of 5 degrees of pitch, and CLB power. Cruising along at F350 that will simply destabilise the aircraft. In this instance, the pilot has selected in excess of 10 degrees of pitch...there is no circumstance in which an A3(anything) would have sufficient performance to use that attitude at any sort of altitude. Even 5 degrees (as per the procedure) and full power, will soon have the aircraft decelerating, and entering the same sort of scenario...albeit with a slower rate of entry.
The real hint is in the lead in line to the procedure, where it states 'if safe conduct of the flight impacted'.... Realistically, it isn't. You'll need to get rid of the automatics (and they are more than likely to disengage of their own accord anyway)...but, at that point, the next thing to do is NOTHING. If you leave the power exactly where it was set, and leave the attitude at 2.5 degrees nose up...pretty much nothing will happen. Goes back to a very old aviation rule....power+attitude=performance.
From the flight recorder data, it has been established that the combination of multiple improbable factors led to the disaster in less than four minutes: the icing of the Pitot probes was the initial event that led to the disconnection of the autopilot, the loss of associated piloting control protections and considerable roll movements. After the manoeuvres carried out by the crew in deteriorated and destabilizing piloting conditions, the aircraft stalled at high altitude, could not be recovered and struck the surface of the Atlantic Ocean at high speed. It should be noted that the misleading stopping and starting of the stall warning alarm, contradicting the actual state of the aircraft, greatly contributed to the crew’s difficulty in analyzing the situation.
Misleading airspeed and angle of attack warnings happen surprisingly often. Most of us get to see simultaneous stall and overspeed warnings at some stage in our careers (it's a fault in the warning system). Use the equation above, and all is well.
I simply cannot understand the ongoing nose up inputs, especially once they called that they were in alternate law..in which case the normal angle of attack protections no longer work. Perhaps this is the sort of performance we'll all be able to look forward to as 200 hour cadets start to become the aviation 'norm'.