Turboprop Aircraft Eis - Garmin G900X Pilot's Manual

3.2 TURBOPROP AIRCRAFT EIS

1
Torque Gauge
(TRQ FT-LB)
2 Interstage Turbine
Temperature Gauge
(ITT °C)
3
Propeller Speed Gauge
(NP RPM)
4
Gas Generator Speed
Gauge (NG %)
5 Fuel Flow
(FFLOW GPH)
6
Oil Pressure Indicator
(OIL PSI)
7
Oil Temperature Indicator
(OIL °C)
8 Ammeter
(AMPS)
9
Voltmeter
(VOLTS)
10
Fuel Quantity Indicator
(FUEL QTY)
11
Aileron and Rudder Trim
Bars (AIL, RUD)
Elevator Trim Bar
(ELEV)
Flap Position Indicator
(FLAPS)
190-00726-00 Rev. J
Displays engine torque in foot-pounds (ft-lb)
Displays Interstage Turbine Temperature (ITT) in degrees Celsius (°C)
When the engine is not running, 'OFF' is annunciated above the ITT readout;
this changes to 'STRT' upon engine start. No annunciation is shown when
the engine is running normally (see Figure 3-30).
Displays propeller speed in revolutions per minute (rpm)
Displays gas generator speed as a percentage
Displays current fuel flow in gallons per hour (gph)
Displays engine oil pressure in pounds per square inch (psi)
Displays engine oil temperature in °C
Displays DC current in amperes (amps) for the generator (G) and the
alternator (A)
Displays DC bus voltages
Displays quantities of fuel in gallons in the left (L) and right (R) tanks
Aircraft
Evolution
Epic LT
Table 3-3 Maximum Indicated Fuel Quantities
Aileron and rudder trim are indicated with pointers along slide bars; the
white bars indicate takeoff trim positions
Elevator trim is indicated with a pointer along a slide bar; takeoff trim position
is indicated with a white bar and T/O label
Flap deflection is indicated with a pointer along a slide bar
Garmin G900X Pilot's Guide
ENGINE INDICATION SYSTEM
Maximum Standard Fuel
Quantity (gal) Per Side
85
144
123