Garmin G2000 - Engine Parameters

Garmin G2000 Pilot’s Guide for the Cessna T240
190-01263-01 Rev. A112
engine indication SyStem
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engine parameterS
MANIFOLD PRESSURE GAUGE
The Manifold Pressure (MAP) Gauge shows engine manifold pressure from ten to forty inches of Mercury.
Figure 3-6 Manifold Pressure Gauge
TACHOMETER GAUGE
The Tachometer (RPM) Gauge measures the propeller speed from zero to 3000 revolutions per minute
(RPM).
Figure 3-7 Tachometer Gauge
CRUISE POWER DISPLAY
The Cruise Power (CRU % PWR) Display shows the percentage of available power from 51% to 91% as a
digital readout. This value is based calculations from engine RPM, manifold pressure, pressure altitude, and
outside air temperature (OAT). The system displays dashes ‘--’ instead of a readout when the percentage of
available power is outside of the range mentioned above.
Figure 3-8 Cruise Power Display
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