Pedals : They tend to move to tail rotor
traction zero position (right
pedal about three centimeters
more forward than left pedal).
NOTE
The pedal movement is plus or minus evident depending from
flight condition. It increases the quicker the pressure drops and
more left pedal movement is required.
Control force on pedals increases
to approximately 35 kg in hover-
ing and less in forward flight.
Cyclic and collective : No change in control force.
PROCEDURE
Airspeed : Reduce gradually avoiding pull
up manoeuvers; recommanded
maximum 90 Kts and 25° bank
angle in order to maintain ac-
ceptable control loads.
Flight controls : Avoid rapid movements.
Failed servo hydraulic system : OFF.
NOTE
The hydraulic system is designed in order to prevent the deacti-
vation of the operative system when one of SERVO caution
messages is activated.
Land as soon as practical.
RFM A109E
3-42 R.A.I. Approved
Rev. 11
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