Appendix F Eis Gauge Layout - Garmin GI 275 Installation Manual

APPENDIX F EIS GAUGE LAYOUT
F.1 Main EIS Page ..................................................................................................................................F-2
F.2 AUX EIS Page ..................................................................................................................................F-7
F.3 CHT/EGT Page.................................................................................................................................F-8
F.4 Fuel Page...........................................................................................................................................F-9
F.5 Summary Page ................................................................................................................................F-10
F.6 Gauge Markings..............................................................................................................................F-11
F.6.1 Caution and Warning Alerts.....................................................................................................F-11
F.6.2 Gauge with Varying Arc Width ...............................................................................................F-12
This appendix provides guidance for configuring EIS gauge layouts for the GI 275 EIS display. Any
deviation from the requirements contained within will require the installer to obtain additional approval.
The gauge layout of the GI 275 may differ between installations due to various factors. Gauge layouts are
generated automatically by the GI 275 depending on the selected engine sensors, specific gauge
configuration and markings, and the number of EIS displays installed. Guidelines for how the EIS gauge
layout is generated are given in the following sections.
Not all aircraft and the engine indications are compatible with the GI 275 EIS due to the installed engine
gauges and the associated markings. For incompatibility cases, the original gauge must be retained. Refer
to Section 2 for limitations.
The GI 275 EIS provides up to five different pages depending on the system configuration: Main EIS
page, AUX EIS page, CHT/EGT page, Fuel page, and Summary page. Each page has three distinct
display sections: top, middle, and bottom.
NOTE
The gauge minimum and maximum limits may be adjusted to optimize pilot interpretation
of the gauge; however, all limitations in the POH/AFM or other approved aircraft data
must be displayed on the gauge.
190-02246-10
Rev. 11
GI 275 Part 23 AML STC Installation Manual
Page F-1