Piston Aircraft Eis - Garmin G900X Pilot's Manual

3.1 PISTON AIRCRAFT EIS

1
Engine Manifold Pressure
Gauge (MAN IN HG)
2 Tachometer (RPM)
3
Fuel Quantity Indicator
(FUEL QTY GAL)
4
Fuel Flow Indicator
(FFLOW GPH)
5
Oil Pressure Indicator
(OIL PSI)
6 Oil Temperature Indicator
(OIL °F)
7 Exhaust Gas Temperature
Indicator (EGT °F)
8
Turbo Inlet Temperature
Indicator (TIT °F)
TSIO-550-E, TIO-540-AE2A
and TEO-540 iE2 (FADEC)
only
190-00726-00 Rev. J
Displays manifold pressure in inches of Mercury (in Hg) to indicate engine power
Displays propeller speed in revolutions per minute (rpm)
Displays the amount of fuel in gallons (gal) for each side (left-L, right-R) of a
standard fuel tank. Standard fuel tank quantities are based on published
kitplane manufacturing data.
A light blue marker is displayed next to the selected fuel tank (optional)
Aircraft
IV/IV-P
ES
ES-P
Evolution
Legacy
RV-7/7A
RV-9/9A
RV-10
Seawind 300C
Velocity XL/TXL
Table 3-2 Maximum Indicated Fuel Quantities
Displays fuel flow in gallons per hour (gph)
Displays oil pressure in pounds per square inch (psi)
Displays oil temperature in degrees Fahrenheit (°F)
Displays the Exhaust Gas Temperature of the hottest cylinder (number is
shown in pointer) in °F
TSIO-550-E and TIO-540-AE2A only: Displays the temperature for the right
(R) and left (L) turbo inlets in °F; the left readout corresponds to the "L"
indication, and the right readout to the "R" indication.
TEO-540 iE2 (FADEC) only: A single turbo inlet temperature is displayed
in °F
Garmin G900X Pilot's Guide
ENGINE INDICATION SYSTEM
Maximum Standard
Fuel Quantity (gal)
Per Side
55
47.5
52.5
85
32.5
21
18
30
40
35
97