____________________________________________________________________
G1000 System Maintenance Manual Page 5-83
190-00903-00 Rev. A
5.1.8.5 Engine Data Page
Figure 5-10. Engine Data Page
The Engine Data Page displays engine sensor readings in real-time. Items shown in Figure 5-x
are typically used in most aircraft. There are no configurable parameters on this page.
DATA:
a. ALT AMPS 1, 2―Alternator Amps measurement, expressed in amperes.
b. PROP D ICE CUR 1, 2―Propeller De-Ice current measurement, expressed in amperes.
c. AIRCRFT PWR 1, 2―Aircraft power input measurement, expressed in volts DC.
d. BATT VOLTS 1, 2―Battery Voltage measurement, expressed in volts DC.
e. ENGINE HOURS―Displays engine time in hours, as measured by the engine tachometer
input.
f. TACH SENSOR 1, 2―Tachometer sensor measurement, expressed in revolutions per minute
(RPM).
g. D ICE PRESS―De-Ice system pressure measurement, expressed in pounds per square inch
(PSI).
h. FUEL PRESS ENG 1, 2―Fuel Pressure measurement, expressed in pounds per square inch
(PSI).
i. FUEL QTY RIGHT, LEFT―Fuel Quantity measurement, expressed in gallons (GL).
j. FUEL FLW ENG 1, 2―Fuel Flow measurement, expressed in gallons per hour (GL/HR).
k. MAP ENG 1, 2―Manifold Air Pressure sensor reading, expressed in inches/mercury (“/Hg).
l. VAC ENG 1, 2―Vacuum measurement, expressed in inches/mercury (“/Hg).
m. OP ENG 1, 2―Oil Pressure, expressed in pounds per square inch (PSI).
n. N1, N2, N3 ENG 1, 2―Compressor spool speeds, expressed in percent RPM. (Turbine
aircraft only)
o. EGT ENG 1, 2 (1-6)—Exhaust Gas Temperature, expressed in degrees Celsius.
To Next Page
Loading...
Need help?
General
