Garmin GI 275 Installation Manual page 408

NOTES
USE 47Ω, 1/4 WATT RESISTOR.
1
IF AN AP HDG DATUM SWITCH IS INSTALLED, THE SWITCH MUST BE LOCATED AS NEAR AS PRACTICAL TO
2
THE AUTOPILOT MODE CONTROL PANEL.
IF AN ENGINE ANNUNCIATOR IS REQUIRED FOR INSTALLATION IN A MULTI-ENGINE AIRCRAFT, MAKE THE
CONNECTIONS TO EIS #1 ONLY. THE LEFT-MOST ENGINE (FROM THE PILOT'S POINT-OF-VIEW) SHOULD BE
3
CONFIGURED AS EIS #1.
190-02246-10
Rev. 11
Figure B-20 External Switches and Annunciators
Sheet 2 of 2
GI 275 Part 23 AML STC Installation Manual
Page B-63