Table 2-1 Aml Stc Installed Sensors; Mfd Functionality; Eis Functionality - Garmin GI 275 Maintenance Manual

2.1.5

MFD Functionality

The Multi-Function Display provides, at a minimum, a moving map display. The display can optionally
provide traffic, terrain, and weather functions depending on installed equipment. The required MFD
system installation consists of:
• GI 275 display
2.1.6

EIS Functionality

The Engine Indicating System is an optional feature for single- and twin-engine reciprocating engine
equipped aircraft listed on the STC AML. The EIS will display 4 and 6 cylinder engine data and select
airframe parameters. The EIS can display engine and airframe operating parameters on the GI 275.
Configurable EIS gauges include optional gauges and those required by the aircraft POH and
manufacturer.
This manual only provides information for the EIS sensors installed per the GI 275 AML STC. Table 2-1
lists the sensors that are maintained in this manual. Refer to the applicable maintenance data and/or TSO
manual for other sensors that are interfaced to the EIS.
Function
Oil Press
Oil Temp
Manifold Press
Fuel Press
Fuel Flow
RPM
Carb Air Temp
190-02246-11
Rev. 1

Table 2-1 AML STC Installed Sensors

Manufacturer P/N
Garmin 150 PSIG pressure, (Brass)
Kulite APT-20GX-1000-150G (Stainless)
UMA T3B3-2.5G
Garmin 30 PSIA Press, (Brass)
Kulite APT-20GX-1000-25A (Stainless)
Garmin 75 PSIG Press, (Brass)
Garmin 15 PSIG Press, (Brass)
Kulite APT-20GX-1000-50G (Stainless)
Kulite APT-20GX-1000-15G (Stainless)
EI FT-60 (Red)
EI FT-90 (Gold)
N/A (Magneto P-lead)
UMA T3B10-SG
GI 275 Part 23 AML STC Maintenance Manual
Garmin P/N
011-04202-30
494-30032-00
494-70009-00
011-04202-00
494-30030-00
011-04202-20
011-04202-10
494-30031-00
494-30029-00
494-10001-00
494-10001-01
N/A
494-70010-00
Page 2-3