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Printed page 134. PDF page 148.
to depress the rudder pedals. Therefore, the Safety Board concludes that flight 587's cyclic rudder motions after the second wake turbulence encounter were the result of the first officer's rudder pedal inputs. (Possible explanations for the first officer's rudder pedalOpen final at PDF page 148In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 159. PDF page 173.
initial release of fuel or the effects of engine compressor surges. 5. Flight 587's cyclic rudder motions after the second wake turbulence encounter were the result of the first officer's rudder pedal inputs. 6. Flight 587's vertical stabilizer performed inOpen final at PDF page 173In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587