Rudder; Rudder Trim - Daher-Socata TBM 900 Pilot's Information Manual

SECTION 7
PILOT'S OPERATING HANDBOOK
DESCRIPTION

RUDDER

(Figure 7.4.5)
The rudder is hinged on three fittings attached to the vertical stabilizer rear spar.
The rudder pedals / rudder linkage is ensured through cables and a rod.
Pilot and R.H. station rudder pedal positions are adjustable at each station. The rudder pedal adjustment
mechanism (for piloting comfort purposes) includes a manual control located against the external bulkhead
beneath the instrument panel and a locking device on the rudder pedals. This ball locking device allows selecting
six different positions.
When landing gear is down, rudder pedals are linked to nose gear steering system.
Spring system of rudder / roll combination induces aileron deflection at the time of pedal displacement and vice
versa.

RUDDER TRIM

(Figure 7.4.6)
A trim tab hinged at two points located at rudder trailing edge provides rudder trim.
Trim tab is linked by two rods to an electric actuator attached to rudder. It is controlled by rudder trim
switch (Y L / Y R) located on pilot control wheel.
Electrical circuit of rudder trim tab is protected by "RUD TRIM" circuit breaker.
Edition 0 -- October 31, 2013 Page 7.4.11
Rev. 1