BEECHCRAFT
Duchess
76
SPINS
If
a
Spin
is
Entered
Inadvertently:
Section
III
Emergency Procedures
Immediately
move
the control column full forward, apply full
rudder opposite to the direction
of
the spin and reduce power
on both engines to idle. These three actions should
be
done
as nearly simultaneously
as
possible; then continue to hold
this control position until rotation stops and then neutralize all
controls and execute a smooth pullout. Ailerons should be
neutral during recovery.
NOTE
Federal Aviation Administration Regulations do
not require spin demonstration of airplanes of
this class; therefore, no spin tests have been
conducted.
The
recovery technique is based on
the
best
available information.
)
3-16
April
1979