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American Airlines 587

Printed page 145. PDF page 159.

amount of pedal input results in the same rudder deflection at all airspeeds, but the pedal travel (and consequently, pedal force) required to hit the pedal stops decreases as airspeed increases. With a variable ratio design, a given pedal input

Open final at PDF page 159In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587