Spin Recovery - Beechcraft Musketeer Sport III A23-19 Pilot Operating Handbook

BEECHCRAFT Sport III
Musketeer A23-19, 19A
Section
III
Emergency Procedures
stall will assure the direction
ot
spin . The airplane nose
will drop and rotate towards the applied rudder. When the
wings are 90° to the horizon, apply fuli aileron against the
intended direction of spin . The airplane will go slightly
inverted and enter a normai spin .
lf aileron against the direction of spin is not applied or
applied too late, the airplane will enter a rapid spiral dive,
and recovery must be initiated by the second turn .
Ił the fuli back stick is not applied and held, the airplane
may spiral. Again recovery must be initiated not later than
the second turn .
lf aileron is applied too early, the airplane will not rotate
and merely remain in a straight stalled condition .
SPIN RECOVERY
From spins entered intentionally or inadvertently:
lmmediately move the eontroi column fuli forward and si-
multaneously apply fuli rudder opposite to the direction of
the spin; continue to hold this eontroi position until
rotation stops and then neutralize all controls and execute
a smooth pullout Ailerons should be neutral and throttle
in idle position at all times during recovery.
October 1979
3-11