Garmin GI 275, Руководство пилота

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Garmin GI 275 Pilot's Guide 190-02246-01 Rev. A
3
System Overview
System Overview
Flight Instruments
EIS
Navigation
Hazar
d A
voidance
Autopilot
Additional F
eatur
es
Appendices
Index
With Internal ADAHRS (Air Data and Attitude and Heading Reference System)
The MFI with internal ADAHRS can do everything the basic MFI does and additionally
contains its own air data and AHRS source, saving weight and expense.
With Internal ADAHRS and Autopilot Interface
The MFI with autopilot interface expands the MFI with internal ADAHRS capability and has
interfaces to connect to an external autopilot or AFCS, letting the MFI provide heading/course
error and attitude to compatible autopilot and AFCS devices.
UNIT CONFIGURATIONS
Primary ADI
A Primary ADI replaces the traditional attitude indicator. It may additionally show airspeed,
altitude, vertical speed, and heading. Terrain is displayed with the optional SVT enablement.
Standby ADI or MFD
Standby ADI or MFD units provide additional capability to the aircraft and display
information (e.g., maps) or external data (e.g., radar altimeter). Standby ADI units act as a
backup ADI if the Primary ADI fails.
Primary HSI
The Primary HSI displays course deviation information based on the selected NAVAID. An
HSI Map shows course deviation information overlaid on a map centered around the aircraft's
current GPS position.
Standby HSI
The Standby HSI acts as a Primary HSI under normal conditions but as a backup ADI if a
Primary ADI fails.
EIS
EIS units replace traditional mechanical engine instruments and additional information like
engine temperatures and provide features like engine lean assisting.
1.3 CONTROLS
The MFI features a 3.125" circular capacitive touchscreen and an Outer and Inner Knob
in the lower left corner. The Inner Knob can be pushed. All operations are done with the
knobs or touchscreen. The touchscreen can be operated with bare fingers or gloves made for
capacitive touchscreens.