Garmin GI 275 User Manual

190-02246-10 GI 275 Part 23 AML STC Installation Manual
Rev. 11 Page F-3
Bottom Full-time AUX/Tip Fuel Quantity and Electrical Gauges
If AUX/Tip tanks are configured, AUX/Tip Fuel beaker gauges will be displayed to the left and right of the
Main Fuel Quantity beaker gauges. If AUX/Tip tanks are not configured but digital gauges (e.g.,
Alternator, Battery, Bus - Volts/AMPS) are configured, up to two digital gauges will be displayed in the
bottom left and right corners. If a single AUX gauge is configured, its fuel beaker gauge will be displayed
in the lower left corner. Additionally, if a single AUX gauge and only one digital gauge are configured, the
digital gauge will also populate next to the AUX gauge in the lower right position. Refer to Figure F-3 for
examples.
The priority for populating bottom left and bottom right full-time gauges is as follows:
(With Red or Yellow Markings)
1. AUX/Tip Fuel (left/right center) – always highest priority over any digital gauge
2. Alternator Amps
3. Battery Volts
4. Bus Volts
5. Battery Amps
(Without Red or Yellow Markings)
6. Alternator Amps
7. Battery Volts
8. Bus Volts
9. Battery Amps IAT
Figure F-3 Bottom Full-Time Gauge Examples
For twin-engine aircraft, the Fuel Quantity gauge must only be shown on one EIS unit. Toggle the Show
button in the EIS Gauges menu on one of the two EIS displays so that the Fuel Quantity gauge is only
shown on one unit.

Garmin GI 275 Specifications

General

Type	Electronic Flight Instrument
Display Type	LCD
Power Input	14 or 28 VDC
Operating Temperature Range	-20°C to +55°C
Brightness Control	Automatic and Manual
Certification	TSO-C113
Interfaces	ARINC 429, RS-232
Mounting	Panel Mount