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American Airlines 587

Printed page 4. PDF page 18.

FDR, the airplane's bank angle moved from 23º to 25º left wing down at 0915:51.5, the control wheel moved to 64º right at 0915:51.5, and the rudder pedals moved to 1.7 inches right at 0915:51.9. At 0915:51.8, 0915:52.3, and 0915:52.9,
Open final at PDF page 18In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587

American Airlines 587

Printed page 5. PDF page 19.

and 1.3 inches right between 0915:52 and 0915:58.5.18 Also, the FDR showed that the control wheel moved 64º to the right at 0915:51.5, 78º (full) to the left at 0915:53.5, 64º to the right at 0915:55.5, and 78º to the
Open final at PDF page 19In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587