Crossky
A Gentleman and a bother
- Joined
- Sep 23, 2004
- Posts
- 406
In reading the Q drivers explanation of how the AOA/Stall system is rescheduled in icing, the wing may not have actually aerodynamically stalled until it reached it's critical AOA during the abrupt pull-up maneuver.
There may not have actually been an aerodynamic stall when the pusher activated, since the pusher is biased by 20 knots as a function of being in icing conditions.
Put another way, with the 'icing switch' off, stall speed was shown to be computed at 90 kts or so.
. . .
Likely, as is typically the case, a combination. But it is clear the speed was allowed to decay to a very low value. After this, the abrupt pull-up sealed their fate at such a low altitude.
I agree with this scenario.
We'll know perhaps whether the crew was concerned about a tail stall from the CVR. They seemingly reacted to a perceived tail stall: extend flaps, the AP disconnects and they get shaker, then pusher. In a tail stall the nose drops, the remedy is to retract flaps and increase back pressure. Only thing is, they could've misinterpreted it. Stick shaker and pusher means WING STALL.
Fly the plane first, if the plane is still flying, don't mess with it. I got AP disconnect, shaker and pusher once with the boards out when new in the RJ on a visual. I had focused on descending after ALTS CAP to catch the GS, only a lower ALT hadn't been selected. I had increased thrust, but not enough to compensate for the drag from the flight spoilers. It took the jumpseater behind us to say 'spoilers' (yes this was humbling for me) before I clued in. But in that momemt before I got SA back I had increased thrust some, and done nothing to the pitch attitude.
Pilot error is sad, tragic, and unfortunately often a fact of life in aviation accidents. NBC didn't do regional pilots any favors tonight, explaining how long (short really) each had been employed by Colgan.