4A-8 Developed for Training Purposes Leerjet 35/36
February 2007
CAE SimuFlite
Ram Air Temperature Gage
The ram air temperature system consists of a temperature indi-
cator and a resistance-type temperature bulb.
The RAM AIRTEMP indicator on the center instrument panel
displays existing outside temperature in degrees Celsius.
Magnetic Compass
A standard liquid-filled magnetic compass is on the windshield
center post.
Flight Hour Meter
The optional flight hour meter, located on the lower right instru-
ment panel, displays total flight time on the aircraft in hours and
tenths of hours.
Optional True Airspeed Indicator
The optional true airspeed (TAS) indicator displays true air-
speed in knots and static air temperature (SAT) in degrees Cel-
sius. The indicator receives data from the air data sensor/unit,
a heated temperature sensor probe, and an SAT/TAS com-
puter.
Emergency Attitude Gyro
The emergency attitude gyro on the left instrument panel indi-
cates visual pitch and roll attitude information. The No.1 emer-
gency battery powers the emergency attitude gyro in the event
of DC failure. The gyro is powered when the emergency EMER
PWR BAT 1 switch is in standby or on. A red OFF warning flag
appears if one or more phases of power is interrupted or the
caging/pitch knob is pulled out.
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