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18-1. ENGINE INSTRUMENTS -WIRING DIAGRAM (CONT) - TM-1-1520-238-T-10_483
18-1. ENGINE INSTRUMENTS -WIRING DIAGRAM (CONT) - TM-1-1520-238-T-10_485
TM-1-1520-238-T-10 Army Model AH-64 Helicopter (NSN
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TM 1-1520-238-T-10
18–6
Change 10
18–1.
ENGINE INSTRUMENTS –
WIRING DIAGRAM
(cont)
18–1
A82
3
J1
17
P66
4
SUPPLY
LAMP
5
18
6
9
15 VDC
3
-15 VDC
4
15 VDC
NO. 2
DC GND
11
NO. 1
10
-15 VDC
B3
B17
21
B16
B14
B18
B13
B15
B1
B12
B10
B11
J
F
E
B
C
A
D
B2
B9
B7
B8
J
E
B
C
A
D
F
13
12
24
8
G
G
14
7
5 VDC
8 VDC
-8 VDC
NO. 1
P66
NO. 2
J1
J4
P401
P400
1J1
P401
46
17
1J2
46
15 VDC RTN
-15 VDC
15 VDC
8 VDC
-8 VDC
2
10
35
5 VDC
-8 VDC
-15 VDC
15 VDC
8 VDC
1J2
P409
J4
40
B4
B5
B6
42
41
29
P409
9
20
5 VDC
1
5
6
ENG 1
TORQUE
IN
DIGITAL BLANKING IN
15 VDC IN
4
3
21
15 VDC IN
-15 VDC IN
17
LAMP TEST IN
TB1-52
18
-15 VDC IN
GS255
RTN
LAMP SUPPLY
NO. 1
LAMP SUPPLY
RTN
11
9
10
7
NO. 2
8
DC GND
14
13
8 VDC
-8 VDC
5 VDC
P/O PILOT ENGINE
TORQUE
INDICATOR
1
3
DIGITAL
SHEET 5 OF 10 M50-240-5B
BLANKING IN
M2
A326
TB1-53
SUPPLY IN
LAMP DC
H
H
IN
SUPPLY
IND
1
SUPPLY OUT
LAMP DC
P/O PILOT MATRIX MODULE
SUPPLY IN
M8
IND DC
SUPPLY OUT
IND DC
P75 SP1
INDICATOR
J1
P74
12
P/O CPG ENGINE
TORQUE
P/O SIGNAL DATA CONVERTER
24
W261
15 VDC RTN
GS245
A
B
C
GS251
GS427
F
G
M
L(4)
R(4)
M(4)
A(4)
SUPPLY OUT
IND DC
C(6)
D(6)
RTN
W261
W261
W646
LAMP
TEST IN
37
38
39
ECU 1 COMMON
ECU 2 COMMON
C(1)
G(1)
NO. 1
NO. 2
ENG 2
TORQUE
IN
NO. 1
NO. 2
ENG 2
TORQUE
OUT
ENG 1
TORQUE
OUT
ENG 1
TORQUE
IN
ENG 2
TORQUE
IN
A(8)
RTN
RTN
RTN
RTN
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