Last Updated：2022/12/24
By 2154:45, the AOA had increased to the point that both the stickshaker and the stickpusher activated. The control column moved forward rapidly in response to the activation of the stickpusher, decreasing the pitch angle to -3.5°, the AOA to 0°, and the vertical load to 0 G. The stickpusher then deactivated, and the flight crew moved the control column past neutral to about 5° ANU, which caused the pitch angle to increase to 8° and the AOA to increase to 11°.
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By
2154:45,
the
AOA
had
increased
to
the
point
that
both
the
stickshaker
and
the
stickpusher
activated.
The
control
column
moved
forward
rapidly
in
response
to
the
activation
of
the
stickpusher,
decreasing
the
pitch
angle
to
-3.5°,
the
AOA
to
0°,
and
the
vertical
load
to
0
G.
The
stickpusher
then
deactivated,
and
the
flight
crew
moved
the
control
column
past
neutral
to
about
5°
ANU,
which
caused
the
pitch
angle
to
increase
to
8°
and
the
AOA
to
increase
to
11°.
