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