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American Airlines 587

Printed page 5. PDF page 19.

attachment fitting fractured), the rudder was deflected between 10º and 11º to the right, the sideslip angle was between 11º and 12º to the right,22 and the airplane experienced a 0.2 G shift to the right in lateral load factor.

Open final at PDF page 19In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587