Cessna Cardinal RG 1974, Owner'S Manual

Page: 175 / 226

Cessna Aircraft Company
Model 177RG Supplement No.
DP-014-16
Section 9
Supplements Page 5
Revision 0
the Insight Avionics G4 engine monitor system are not aircraft
primary engine parameters indications and in case of any
discrepancy pilot should refer to the aircraft primary engine
indicators. The Insight Avionics G4 secondary engine monitor
system can monitor data of: EGT, CHT, Probe diagnostic, Fuel
flow, OAT, Buss voltage, Tachometer, Manifold pressure, Oil
Temperature, Oil Pressure, Accelerometer, Carburetor
temperature, Data logging, Probe diagnostics, Auxilliary
temperatures, RS-232 Interfaces, Vibration.
START-UP: The Insight Avionics G4 engine monitor system is
ready to operate after electrical power application. Within
seconds after starting the engine, the white EGT bar graph
columns will begin to appear on the system display. Each
white column corresponds to the Exhaust Gas Temperature
(EGT) of a cylinder. The columns are numbered with cylinder
number. In some engines, the throttle will have to be opened
to the fast idle range to get an EGT indication for all cylinders.
As the cylinder heads begin to warm up, the display will
indicate Cylinder Head Temperature (CHT) for all cylinders as
a smaller green bar in each EGT column. Digital numbers
below each bar graph column indicates the exact EGT and
CHT for each cylinder. CHT is shown in green when within
normal operating range, yellow when approaching the redline,
and red when at or exceeding the redline limit. A red horizontal
line across each column indicates the CHT limit. The top row
of supplementary annunciations (in light blue) shows RPM,
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