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Printed page 126. PDF page 140.
stabilizer, and its surrounding structure.205 FDR and CVR information indicated that both engines were operating normally before the final dive. Examination of the recovered thrust reversers and FDR data indicated that the thrust reversers were stowed at impact. ExaminaOpen official document at PDF page 140Loss of Control and Impact with Pacific Ocean, Alaska Airlines Flight 261, McDonnell Douglas MD-83, N963AS, January 31, 2000
Printed page 176. PDF page 190.
longitudinal trim control system, the horizontal stabilizer, and its surrounding structure. 6. Both engines were operating normally before the final dive. 7. Air traffic control personnel involved with the accident flight were properly certificated and qualified for their assigneOpen official document at PDF page 190Loss of Control and Impact with Pacific Ocean, Alaska Airlines Flight 261, McDonnell Douglas MD-83, N963AS, January 31, 2000