Garmin GI 275 Installation Manual page 349

NOTES
CONFIGURATION MODULE IS MOUNTED IN THE BACKSHELL OF THE P1 CONNECTOR USING 28 AWG
WIRES. CONTACTS SUPPLIED WITH THE CONFIGURATION MODULE MUST BE USED FOR CONNECTING
1
CONFIGURATION MODULE HARNESS TO P1.
OPTIONAL LIGHTING BUS CONNECTION (28 VDC, 14 VDC, 5 VDC, OR 5 VAC).
2
WIRE GAUGE SHOWN FOR POWER AND GROUND LENGTH LESS THAN 20 FEET. FOR POWER AND
GROUNDS GREATER THAN 20 FEET, REFER TO AC 43.13-1B, CHAPTER 11 TO DETERMINE THE
3
APPROPRIATE WIRE GAUGE.
AIRCRAFT POWER 2 IS USED FOR WIRING WITH INDEPENDENT POWER BUSSES AND IS NOT REQUIRED.
4
REFER TO SECTION 3.2.1 FOR BREAKER SIZING, BUSSING, AND LABELING.
REFER TO SECTION 3.2.6 FOR HSDB ARCHITECTURE.
5
P/N 325-00238-02 CABLE ASSY, USB-A RECPT TO PIGTAIL, 48" INCLUDED WITH GI 275 CONNECTOR KIT.
THE USB CONNECTOR IS FOR MAINTENANCE PURPOSES ONLY AND MUST BE CAPPED AND STOWED
PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. PROTECT THE USB CONNECTOR SUCH THAT THE
6
USB CONNECTOR OPENING IS COMPLETELY COVERED. THEN SECURE THE USB CONNECTOR FOR
FUTURE MAINTENANCE ACCESS.
A GSB 15 USB DATABASE AND CHARGING HUB CAN BE INSTALLED IN PLACE OF THE USB PIGTAIL. REFER
7
TO FIGURE B-26.
Figure B-1 GI 275 - Power, Lighting, Configuration Module, HSDB, USB Interconnect
190-02246-10
Rev. 11
Sheet 2 of 2
GI 275 Part 23 AML STC Installation Manual
Page B-4