Collective : As necessary to cushion the
touchdown.
NOTE
A slight rotation can be expected on touchdown.
COMPLETE LOSS OF TAIL ROTOR IN CRUISE
PROCEDURE
Collective : Lower as necessary to eliminate
yaw to the right.
Airspeed/power : As necessary in order to reach a
suitable landing site.
NOTE
Increased power will allow an extension of the flight path,
however an increase in power necessitates an increase in speed to
prevent the helicopter from turning.
Landing gear lever : DOWN.
Nose wheel lock : ON.
Parking brake : OFF.
On reaching the point of intended landing:
Collective and cyclic : As needed to control lateral-
directional stability, touch
down point, speed and attitude.
If the above procedure is not suitable to the landing site:
ENG MODE switches : OFF (full counterclockwise)
RFM A109E
3-40 R.A.I. Approved
Rev. 11
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