EasyManua.ls Logo

Piper TOMAHAWK - Page 88

Piper TOMAHAWK
213 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
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

Table of Contents

Related product manuals