190-01115-01 G3X™/G3X Touch™ Avionics Installation Manual
Rev. AV Page 28-8
28.3 GSU 73 - Rotax Sensor Drawings
Figure 28-3 GSU 73 - Rotax 912/914 Sensor Wiring Examples, Page 1 of 2
GSU 73
J732
RPM 17
ROTAX TRIGGER COIL
XDCR PWR OUT LO (GND) 74
S
OUT HI
OUT LO/GROUND
300
1%
OIL TEMP LO
OIL TEMP HI
14
34
OIL TEMP SENSOR
ROTAX P/N 965531
POS 1/GP 1/TIT 1 LO
POS 1/GP 1/TIT 1 HI
67
47
CHT #1
ROTAX P/N 965531
POS 2/GP 2/TIT 2 LO
POS 2/GP 2/TIT 2 HI
8
28
CHT #2
ROTAX P/N 965531
SEE NOTE 9
S
S
S
POS 3/GP 3/FUEL FLOAT 3 HI 27
OIL PRESSURE SENSOR
+12V TRANSDUCER POWER 55
OUTPUT
+ EXCITATION
40
1%
ROTAX P/N 956413
POS 3/GP 3/FUEL FLOAT 3 LO
POS 3/GP 3/FUEL FLOAT 3 HI
7
27
GROUND
OUTPUT
OIL PRESS SENSOR
ROTAX P/N 956415
S
COMMONC
A
B
OR
MANIFOLD PRESS HI
MANIFOLD PRESS LO
65
6
FUEL PRESS LO
FUEL PRESS HI
45
26
FUEL PRESS SENSOR
S
GROUND
OUTPUT
SUPPLY VOLTAGE
MANIFOLD PRESS SENSOR
S
GROUND
OUTPUT
SUPPLY VOLTAGE
+5V TRANSDUCER POWER 75
57
GARMIN GPT15G OR
KAVLICO P4055-5020-2
GARMIN GPT 30A,
KAVLICO P4055-30A-E4A.
OR KAVLICO P500-30A-E4A
XDCR PWR OUT LO (GND)
EGT 1 HI
EGT 1 LO
EGT 2 HI
EGT 2 LO
OUT #1 LO43
23
3
OUT #2 HI
OUT #2 LO
63 OUT #1 HI
YEL
RED
YEL
RED
YEL
RED
YEL
RED
TYPE K THERMOCOUPLES
EGT SENSORS
POS 3/GP 3/FUEL FLOW 3 LO 7
S
WHT
RED
B
C
A
B
C
A
BATTERY CONTACTOR
VARIES W/ TYPE
BATTERY POSITIVE
50
70SHUNT 1 HI
SHUNT 1 LO
AMPS 1, UMA 1C4
S
1A
1A
/ ALTERNATOR B LEAD
/ POWER DISTRIBUTION BUS
SEE NOTE 8
SEE NOTE 6
SEE NOTE 10
SEE NOTE 9
SEE NOTE 7
OR ROTAX P/N 966385
OR ROTAX P/N 966385
OR ROTAX P/N 966385
SEE NOTE 13
FUEL PRESS LO
FUEL PRESS HI
45
26
FUEL PRESS SENSOR
S
GROUND
OUTPUT
SUPPLY VOLTAGE+12V TRANSDUCER POWER 55
56
UMA 1EU07D (914)
XDCR PWR OUT LO (GND)
RED
WHT
BLK
SEE NOTE 13
To Next Page
Loading...
Need help?
General
