Garmin G3X - Page 474

190-01115-01 G3X™/G3X Touch™ Avionics Installation Manual
Rev. AV Page 27-4
Figure 27-3 GEA 24 - Lycoming IE2 Electronic Control Unit
37 PIN AIRFRAME
CAN2_HI 17
INTERFACE (AF-P1)
CAN 3 HI18
CAN2_LO
GEA 24
P244
33
CAN 3 LO17
S
CAN BUS (22 AWG TWISTED SHIELDED PAIR)
NOTES
1. WIRING GUIDANCE
A. INSTALL A 1/8 WATT, 5%, 120 OHM RESISTOR ACROSS THE CAN HI/LO PINS AT
THE GEA 24 P244 CONNECTOR TO TERMINATE THE CAN BUS AT THAT END.
2. G3X™ AVIONICS CONFIGURATION GUIDANCE
A. NO CONFIGURATION REQUIRED ON GEA 24 TO ENABLE CAN BUS
B. ON THE ENGINE CONFIGURATION PAGE
SET PROBE TYPE ON FADEC SUPPORTED ENGINE PARAMETERS
TO "LYCOMING FADEC"
LYCOMING IE2 ELECTRONIC CONTROL UNIT
120 Ω