Eurocopter AS 350 83 Flight Manual page 156

FLIGHT MANUAL
.1.2 Instrument Panel Galvanometers (Figure 2)
The galvanometers indicate the position of the series-mounted actuators
with respect to their middle position; when the actuator is centered,
the pointer is in the middle. In pitch and roll, the actuators are
recentered automatically.
~e00
.
~
~
ABRER 1 2 3
~ NOSE UP
-~ CJ4 C:J4 CJ4
~
Figure 2
Iten Description Direction of Indication
No.
1 P (pitch) galvan<Xlleter Indicates a nose-down order given
by the autopilot
2 R (roll) galvanometer Indicates a roll-to-right order
given by the autopilot
3 Y (yaw) galvanometer Indicates a yaw-to-left order given
by the autopilot
4 Amber indicator lights When on, the associated channel(s)
is (are) not enaaaed
@n : The yaw galvanometer pointer is recentered by moving the
.
rudder pedals in the direction shown by the pointer.
1.3 Cvclic Stick GriD Controls
The autopilot controls are located on pilot's and copilot's cyclic stick
grips (if dual controls installed) :
-A four-way beep-trim button. Allows the pilot to operate the stick and
change the aircraft attitudes.
-A trim release pushbutton. Momentarily releases pitch and roll channel
artificial feel loads.
-A pushbutton. Disengages AP system.
1.4 Vertical Gyro Valid Data LiQht (If installed)
An aJltJer GYRO light on the failure monitoring panel illuminates to
indicate that the vertical gyro valid data signal is lost.
.
DGAC APproved: 350 83 SUP. 16
I A I 8 I C I F I 97-40 Page 3