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Printed page 5. PDF page 19.
time, the airplane's airspeed was about 100 knots. FDR data also showed that the roll angle reached 105� right wing down before the airplane began to roll back to the left and the stick pusher activated a second time (aboutOpen final report at PDF page 19NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407