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Printed page 4. PDF page 18.
turbulence encounter, the airplane's pitch angle increased from 9º to 11.5º, decreased to about 10º, and increased again to 11º. The airplane's bank angle moved from 0º (wings level) to 17º left wing down, which was consistent with the turnOpen final at PDF page 18In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 56. PDF page 70.
vortex decay. The wake vortex from Japan Air Lines flight 47 would have had an age of about 100 seconds, and flight 587 would have encountered the wake vortex at a time before vortex linking and rapid vortex decay. TheOpen final at PDF page 70In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 77. PDF page 91.
performance would not likely display gross mistakes. An increase in fundamental frequency by about 100 to 200 percent is characteristic of stage 3 level of stress, or panic, which would likely result in the speaker's inability to think orOpen final at PDF page 91In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 83. PDF page 97.
simulator instructor pressed a touch-screen button that was programmed to roll the airplane about 10º either left or right and then roll the airplane in the opposite direction past 90º.135 The simulator inhibited the use of the ailerons, spoilers, andOpen final at PDF page 97In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 101. PDF page 115.
twice the length of the fuselage and that dark smoke from the fire turned to light smoke about 10 minutes later. The Jet Blue first officer observed an airplane in a “vertical rocking nose-down position.” The first officer also observedOpen final at PDF page 115In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 141. PDF page 155.
simulator depicted a little light chop, followed by the airplane rolling in one direction to about 10o. The similarity to flight 587 ended at this point because the simulator then depicted the airplane quickly rolling to beyond 90o in theOpen final at PDF page 155In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587