result in yaw and “fish-tailing.’’ If the rudder is not centralized it would be
possible to exceed the maximum maneuver speed (V
A
) of 103 kt with the
surface fully deflected.
ENGINE
Normally the engine will continue to run during a spin, sometimes very
slowly. If the engine stops, take normal spin recovery action, during which
the propeller will probably windmill and restart the engine. If it does not,
set-up a glide at 75 kt and restart using the starter motor.
PIPER AIRCRAFT CORPORATION
SECTION 4
PA-38-112, TOMAHAWK
NORMAL PROCEDURES
ISSUED: APRIL 30, 1981
REPORT: 2126
4-27
result in yaw and “fish-tailing.’’ If the rudder is not centralized it would be
possible to exceed the maximum maneuver speed (V
A
) of 103 kt with the
surface fully deflected.
ENGINE
Normally the engine will continue to run during a spin, sometimes very
slowly. If the engine stops, take normal spin recovery action, during which
the propeller will probably windmill and restart the engine. If it does not,
set-up a glide at 75 kt and restart using the starter motor.
PIPER AIRCRAFT CORPORATION
SECTION 4
PA-38-112, TOMAHAWK
NORMAL PROCEDURES
ISSUED: APRIL 30, 1981
REPORT: 2126
4-27