Horizontal Stabilizer (Tail) Stall Warning
#31
Bracing for Fallacies
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Joined APC: Jul 2007
Position: In favor of good things, not in favor of bad things
Posts: 3,543
To this end I do seek more experienced pilots' advice.
#32
Gets Weekends Off
Joined APC: Jun 2009
Posts: 317
If, say a 777, had a larger quantity of bleed air per square foot distributed to the tail surfaces than it would confirm, to me, that engineers recognize the tendency for smaller surfaces to acquire ice more readily and compensate for that. Systems with boots are not complex enough to allow for such adjustments, such as, heated surfaces, weeping wings, or bleed air surfaces can through quantity, whether it be electricity, liquid, or air, distribution.
Hope that helps. If not, sorry I give up.
#33
Gets Weekends Off
Joined APC: Jun 2007
Posts: 348
Because the systems on larger aircraft are more complex and have the capability to handle various ranges of heating/bleed air to each different surface. I would suspect if the tail will gain ice that much easier/faster than the wings this would be somehow accounted for with the larger more complex systems. It appears as you and KC-10 have explained other systems that they keep the tail on and or activate it multiple times in a cycle, nobody seems to know why.
If, say a 777, had a larger quantity of bleed air per square foot distributed to the tail surfaces than it would confirm, to me, that engineers recognize the tendency for smaller surfaces to acquire ice more readily and compensate for that. Systems with boots are not complex enough to allow for such adjustments, such as, heated surfaces, weeping wings, or bleed air surfaces can through quantity, whether it be electricity, liquid, or air, distribution.
Hope that helps. If not, sorry I give up.
If, say a 777, had a larger quantity of bleed air per square foot distributed to the tail surfaces than it would confirm, to me, that engineers recognize the tendency for smaller surfaces to acquire ice more readily and compensate for that. Systems with boots are not complex enough to allow for such adjustments, such as, heated surfaces, weeping wings, or bleed air surfaces can through quantity, whether it be electricity, liquid, or air, distribution.
Hope that helps. If not, sorry I give up.
But I see what you're getting at now. In a way, I guess, our boot system does adjust the amount of de-icey-ness power by increasing the frequency of the boot inflations on the tail. Since it can't really blow the boots any harder, it just does it twice.
#34
Gets Weekends Off
Joined APC: Jan 2008
Position: 319/320/321...whatever it takes.
Posts: 492
I do know that the CRJ and the A320 series don't even have tail deice. Suppoosedly the engineers say that it just can't happen. Don't know if I believe them, but I don't know of any accident caused by tail plane icing.
#35
I always wondered about that. The reason I got for the Boeings was that at low speeds, the engine exhaust keeps the stabs warm, but at high speeds, friction (TAT) takes care of it. But that doesn't explain the CRJ, or the most interesting to me, the Piaggio Avanti (No tail anti-ice at all, and a much slower airplane than the jets). Maybe we should ask NASA for clarification.
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