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Printed page 7. PDF page 21.
block [altitude] between uh, twenty and twenty five?”24 FDR data indicated that, by 1611:13, the airplane's airspeed had decreased to 262 KIAS, and the airplane was maintaining an altitude of approximately 24,400 feet with a pitch angle of 4.4°. AtOpen official document at PDF page 21Loss of Control and Impact with Pacific Ocean, Alaska Airlines Flight 261, McDonnell Douglas MD-83, N963AS, January 31, 2000
Printed page 64. PDF page 78.
-5° airplane nose down, and the elevators had moved to about a -11° position. About 1611:13, the speed brakes were stowed. By this time, the airplane's airspeed had decreased to 262 KIAS, and the airplane was maintaining an altitudeOpen official document at PDF page 78Loss of Control and Impact with Pacific Ocean, Alaska Airlines Flight 261, McDonnell Douglas MD-83, N963AS, January 31, 2000