BOMBARDIER Johnson 90 Service Manual page 65

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ENGINE CONTROL SYSTEM
COMPONENTS FOR SYSTEM CONTROL
ECM CONNECTOR / TERMINAL$ LAYOUT
1
r7
1
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
• •
• • • • • • • • • • • • • •
• • • • •
• • • • • • • •
• • •
• •
• • • • •
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
ECM CIRCUITS
TERMI-
WIRE
NAL
COLOR
CIRCUIT
1
-
-
2
8I/R
Emergency stop switch
3
o
Buzzer cancel
4
Y/8
Tachometer
5
Br
Neutral switch
6
B
Ground
7
V/W
Ex-manifold temp. sensor
8
-
-
9
Lg/W
Cylinder temp. sensor
10
B
Ground far ECM
11
8/W
Ground far sensors
12
81/8
Oillamp
13
P/8
Ground for ECM main relay
14
-
-
15
R/8
CKP sensor
16
O/Y
PC communication
17
G/Y
TEMP lamp
18
B/R
IAC valve solenoid (-)
19
-
-
20
B
Ground far ignition coil
21
-
-
22
Lg
No.4 Fuel injector (-)
TERMI-
WIRE
NAL
COLOR
CIRCUIT
23
81
Oil pressure switch
24
Lg/R
CTP switch
25
-
-
26
G/W
CHECK ENGINE lamp
27
8I/W
Buzzer
28
-
-
29
w
MAP sensor
30
Gr
ECM power source
31
Lg/8
IATsensor
32
B
Ground far ECM
33
O/G
CMP sensor
34
8/G
0
2
feedback / PC
communication
35
R
Power source for MAP sensor
36
y
PC communication
37
B/W
Fuel pump (-)
38
R/W
No.3 Fuel injector (-)
39
B/Y
No.2 Fuel injector (-)
40
O/B
No.1 Fuel injector (-)
41
-
-
42
B
Ground far ignition coil
43
81
No.2 lgnition coil (-)
44
o
No.1 lgnition coil (-)
3-5

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