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Printed page 130. PDF page 144.
pulling upward across the remaining ridges after the shearing;216 however, the Board could not determine the exact cause of the jam. 214 For more information about these studies, see section 1.16.4. 215 Because the thinnest part of the sheared threadOpen official document at PDF page 144Loss of Control and Impact with Pacific Ocean, Alaska Airlines Flight 261, McDonnell Douglas MD-83, N963AS, January 31, 2000
Printed page 135. PDF page 149.
Although the exact horizontal stabilizer angle required to produce the final pitchover could not be determined, the Safety Board's airplane performance studies determined that the airplane's pitch rate during the final dive could only have resulted from a rapid increaseOpen official document at PDF page 149Loss of Control and Impact with Pacific Ocean, Alaska Airlines Flight 261, McDonnell Douglas MD-83, N963AS, January 31, 2000