Beechcraft Baron 58 - Page 95

BEECHCRAFT Baron 58
Serial TH 773 and After
Section
III
Emergency Procedures
be done as near 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 weight; therefore, no spin tests have been
conducted. The recovery
technique is based on
the best available
information.
July 1979
3·19