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American Airlines 587

Printed page 5. PDF page 19.

0915:55.5, the pedal movements lagged behind the wheel movements by 0.5 second. 20 The rudder angle data detected by the rudder position sensor at the vertical stabilizer were filtered before they were recorded on the FDR. As a result, the
Open final at PDF page 19In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587

American Airlines 587

Printed page 55. PDF page 69.

parameters were recorded directly on the FDR. Even though the FDR did not directly record rudder angle data, the FDR did record a filtered rudder signal that could be used to check whether an estimate of rudder position, obtained by
Open final at PDF page 69In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587