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Engine indication system – Garmin G1000 Piper PA32 User Manual

Page 90

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Garmin G1000 Pilot’s Guide for Piper PA32

190-00692-00 Rev. B

3-10

ENGINE INDICATION SYSTEM

1

Engine Manifold Pressure

Gauge (MAN IN HG)

Displays manifold pressure in inches of Mercury (in Hg) to indicate engine power

Turbocharged Aircraft – Maximum manifold pressure range displayed in red

2

Tachometer

(RPM)

Displays propeller speed in revolutions per minute (rpm); the red range

indicates propeller overspeed

3

Fuel Quantity Indicator

(FUEL QTY GAL)

Displays the amount of fuel in gallons (gal) for each tank, labeled ‘L’ (left)

and ‘R’ (right)

4

Fuel Flow Indicator

(FFLOW GPH)

Displays fuel flow in gallons per hour (gph)

5

Turbine Inlet Temperature

Indicator (TIT °F)
Turbocharged aircraft

Displays the temperature at the turbine inlet in degrees Fahrenheit (°F)

6

Exhaust Gas Temperature

Bar Graph (EGT °F)
Normally-aspirated aircraft

Displays exhaust gas temperatures (EGT) for all cylinders in °F; the readout

is for the hottest cylinder

7

Cylinder Head

Temperature Bar Graph
(CHT °F)

Displays head temperatures for all cylinders with a readout for the hottest

cylinder in °F