NOTE:
In case of the trim device failure in most forward position it is recommended to use flat, with no obstacles landing
field which is long enough for landing due to increased landing approach speed.
3.4 Instrument panel
The instrument panel consists of:
-
air speed indicator;
-
variometer;
-
altimeter;
-
oil pressure gage;
-
oil temperature gage;
-
head temperature gage;
-
engine operation time counter;
-
fuel gage;
-
tachometer;
-
compass.
The instruments arrangement is shown on the photo:
The Pitot static gage supplies ram air pressure to the air speed indicator from the nose of the cockpit.
The static pick up is at the rear of the instrument under the dash.
The power switch, ignition switches and the starter button can be found on the bottom side
of the dash.
