I was waiting to board NW1672 AUS-MSP on Monday, and saw that one side of the elevator goes up a little farther than the other. I was just wondering why it does that. I've seen it on a few of AA's MD-80s that I've paid attention to.
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Seeing control surfaces at a gate really isn't going to give you a good idea. You'd need a pic of it like that during taxi to see really.
EG on an Airbus with Hydraulic systems depowered, the ailerons will both flop down... very disconcerting to a Boeing pilot!
On the tail on a 744, you can see half of the rudder pointing one way, and the other half pointing the other!
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Originally posted by MCMSeeing control surfaces at a gate really isn't going to give you a good idea. You'd need a pic of it like that during taxi to see really.
EG on an Airbus with Hydraulic systems depowered, the ailerons will both flop down... very disconcerting to a Boeing pilot!
On the tail on a 744, you can see half of the rudder pointing one way, and the other half pointing the other!
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Split elevator that uses tabs to move it(can't remember whether they're servo or anti-servo tabs). I believe the elevator itself is free floating.
The way it works is that the yoke is connected to the tabs rather than the elevator itself. Those tabs use aerodynamic force to move the elevator.Bite me Airways.....
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