Garmin G3X - 27.2 GEA 24 Engine Interface Module - Lycoming;Continental Sensor Drawings

190-01115-01 G3X™/G3X Touch™ Avionics Installation Manual
Rev. AV Page 27-2
27.2 GEA™ 24 Engine Interface Module - Lycoming/Continental Sensor Drawings
Figure 27-2 GEA 24 - 4/6 Cylinder Lycoming/Continental Sensor Wiring Examples,
Page 1 of 2
GEA 24
J243
OIL TEMP LO
OIL TEMP HI
32
33
OIL TEMP SENSOR
OUT HI
S
OUT LO
MANIFOLD PRESS
MANIFOLD PRESS GND
13
12
FUEL PRESS GND
FUEL PRESS
1
2
FUEL PRESS SENSOR
S
GROUND (PIN A)
OUTPUT (PIN C)
VOLTAGE IN (PIN B)
MANIFOLD PRESS SENSOR
GARMIN GPT 30A, OR
KAVLICO P4055-30A-E4A
S
FUEL PRESS XCDR +5V 4
GARMIN GPT 15G (CARB),
GARMIN GPT 30G (INJ),
P4055-5020-2 (CARB),
OR P4055-5020-3 (INJ)
RED
GRN
BLK
OIL PRESS
OIL PRESS GND
17
16
OIL PRESS SENSOR
S
GARMIN GPT 15G OR
KAVLICO P4055-150G-E4A
FUEL FLOW
22
23
FUEL FLOW TRANSDUCER
OUT LO/GND
OUT HI
FUEL FLOW XCDR +12V 24 EXCITATION INPUT
S
EI FT-60 (RED CUBE)
RED
WHT
BLK
UMA 1B3-2.5R
.0005 OHM
36
37SHUNT 1 HI
SHUNT 1 LO
S
1A
1A
BATTERY CONTACTOR
BATTERY POSITIVE
/ ALTERNATOR B LEAD
/ POWER DISTRIBUTION BUS
AMPS 1, UMA 1C4
FUEL FLOW XCDR GND
SEE NOTE 9
SEE NOTE 10
RPM XCDR GND 7
8
OUT LO/GROUND
OUT HI
TACH SENSOR
RPM XCDR +12V 9 EXCITATION INPUT
S
UMA T1A9-1 (SLICK)
OR T1A9-2 (BENDIX)
OR 1A3C-2 (MECHANICAL)
RPM 1 8 OUT HI
ELECTRONIC IGNITION #1
OR
4 OR 6 CYLINDER
SEE NOTE 8
WHT
SEE NOTE 7
SEE NOTES 6 AND 12
S
8
LIGHT SPEED
ELECTRONIC IGNITION
WHT
SEE NOTE 15
S
RPM 2 6 OUT HI
ELECTRONIC IGNITION #2
4 OR 6 CYLINDER
WHT
S
8
E MAG P MODEL
ELECTRONIC IGNITION
WHT
S
OR
OUT HI
OUT HI6
MAN PRESS XCDR +5V 15
OIL PRESS XCDR +5V
19
RPM XCDR GND 7
GROUND (PIN A)
OUTPUT (PIN C)
VOLTAGE IN (PIN B)RED
GRN
BLK
GROUND (PIN A)
OUTPUT (PIN C)
VOLTAGE IN (PIN B)RED
GRN
BLK
4 OR 6 CYLINDER
4 OR 6 CYLINDER
OR
8
SUREFLY TACH2
S
0-5v (TACH OUTPUT)
RPM 1
RPM 1
RPM 1
RPM 1
SHIELD GROUND