Garmin G1000:Piper, Руководство пилота

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190-00692-00 Rev. B
Garmin G1000 Pilot’s Guide for Piper PA32
3-1
ENGINE INDICATION SYSTEM
SECTION 3 ENGINE INDICATION SYSTEM
NOTE:
Refer to the Aircraft Flight Manual (AFM) for limitations.
The G1000 Engine Indication System (EIS) for the Piper PA32 displays critical engine, electrical, fuel, and other
system parameters on the left side of the MFD during normal operations. EIS information can be fully expanded
to an entire page (Engine Page) using the
ENGINE
Softkey.
In reversionary mode, the displays are re-configured to present PFD symbology together with the EIS Display
(refer to the System Overview for information about reversionary mode). Information on the engine, electrical
system, fuel, and cabin temperature is organized into three displays while the G1000 is in reversionary mode:
• Engine Display – Default display (identical to the EIS Display normally shown on the MFD); shows all critical
engine, fuel, and electrical indicators
• Lean Display – Provides engine leaning information
• System Display – Shows numeric readouts of critical engine, fuel, and electrical indicators
Figure 3-1 MFD (Normally-aspirated)
EIS Display
Instrument types include dial gauges, horizontal and vertical bar indicators, digital readouts, slide bars, and bar
graphs. Green bands indicate normal ranges of operation; yellow and red bands indicate caution and warning,
respectively. White bands indicate areas outside of normal operation not yet in the caution or warning ranges.
When unsafe operating conditions occur, the corresponding readouts flash to indicate cautions and warnings.
If sensory data to an instrument becomes invalid or unavailable, a red “X” is displayed across the instrument.