Garmin G2000 Pilots Guide - Page 126
Engine Parameters
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SyStem oVerVieW fligHt inStrUmentS eiS & cnS aUdio panel engine indication SyStem 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 aVoidance management fligHt HaZard afcS additional featUreS appendiceS indeX 112 Garmin G2000 Pilot's Guide for the cessna T240 190-01263-01 Rev. A
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