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Printed page 20. PDF page 36.
and establish a climb rate of at least 2,000 ft per minute. During the next 6 seconds, automated flight commands advanced the thrust levers to about 80� to 82�, resulting in increased thrust and longitudinal acceleration, and moved the controlOpen official document at PDF page 36Rapid Descent and Crash into Water, Atlas Air Inc. Flight 3591, Boeing 767-375BCF, N1217A, Trinity Bay, Texas, February 23, 2019
Printed page 2. PDF page 18.
from IAH at an altitude about 6,300 ft msl. During the next 6 seconds, the airplane's automated flight functions commanded nose-up pitch and an increase in engine thrust, consistent with go-around mode-driven commands. Neither crewmember made any callout to indicateOpen official document at PDF page 18Rapid Descent and Crash into Water, Atlas Air Inc. Flight 3591, Boeing 767-375BCF, N1217A, Trinity Bay, Texas, February 23, 2019
Printed page 10. PDF page 26.
pitch limit indicator, flight director commands, localizer and glideslope deviations, automated flight mode annunciations, airspeed (using an airspeed tape), radio altitude, and decision height (see figure 3).14 Figure 3. Exemplar ADI with select features labeled. 14 TheOpen official document at PDF page 26Rapid Descent and Crash into Water, Atlas Air Inc. Flight 3591, Boeing 767-375BCF, N1217A, Trinity Bay, Texas, February 23, 2019