NOTE
HELIPILOT indicators normally refer to SAS 1. Turning SAS 1 off.
HELIPILOT indicators will automatically switch to SAS 2.
NOTE
The attitude beep-trim on the cyclic is inoperative when flying
coupled in the relative axis or when one of the two SAS is
inoperative.
Repeated disturbances during pitch, roll, or yaw helipilot operation
Retrim the helicopter. Identify the affected axis and helipilot by observing HELIPI-
LOT indicators (API), helicopter attitudes/rates and ADIs (normal and STBY).
NOTE
SAS 2 pitch and roll actuators position may be observed by
pressing the monitor switch SAS 2 PUSH on HELIPILOT panel.
Disengage failed system and proceed as follows:
Cyclis and collective : Hands on.
Maximum Airspeed : Reduce below 120 KIAS.
Maximum ROC : 500 ft/min.
Proceed with flight.
Repair failed system before next flight.
Oscillatory malfunction during pitch, roll or yaw helipilot operation
Airspeed : Control.
Reduce below 120 KIAS.
Power : Reduce if practicable.
Rate of climb : 500 ft/min maximum.
RFM A109E
E.A.S.A. Approved 3-49
Rev. 35
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