TM 1-1520-238-T-6
9–357
9–133. CPG EDGE-LIGHTS – WIRING INTERCONNECT DIAGRAM (cont)
9–133
AF(2)
AE(2)
1
B12
B11
P465 J12
3
2
1
3
2
1
3
2
1
R25 4
W
R12 8
W
R11 4
W
CH 1 NO. 2
P
P
P
P
P
P
B
C
D
E
F
G
A
A
B
C
D
E
F
G
P
TB1 - 43
TB1 - 42
CH 1 NO. 2
A326
J14 P466
B3
B4
B5
B6
B7
B8
B9
B10
B11
B12
B13
B14
W646
W119
P/O PILOT MATRIX MODULE
P275 - 10
P275 - 1 1
P127 - 3
P127 - 1
P126 - 3
P126 - 2
P351 - 10
P351 - 1 1
P385 - Y
P385 - X
P31 - k
P31 - m
ACCELERATOR (NOTE 14)
CLOCK (NOTE 14)
VERTICAL SPEED
INDICATOR (NOTE 14)
RADIO MAGNETIC
INDICATOR (NOTE 14)
BAROMETRIC ALTIMETER
INDICATOR (NOTE 14)
CPG CAUTION / WARNING
PANEL
NOTES:
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC LINE, AND THE NUMBER IN
PARENTHESIS IDENTIFIES THE SHEET NUMBER WHERE THE SIGNAL TERMINATES.
1. AVIONICS CONFIGURATION - NAVIGATION INSTRUMENTS (TM 11-1520-238-23-2).
2. FUEL SYSTEM (TM 1-1520-238-T-7).
3. POWER PLANTS (TM 1-1520-238-T-4).
4. UTILITY SYSTEM - ANTI - ICE (TM 1-1520-238-T-8).
5. FLIGHT CONTROL SYSTEM (TM 1-1520-238-T-7).
6. FIRE CONTROL SYSTEM (TM 9-1230-476-20-2).
7. UTILITY SYSTEM - FIRE DETECTION SYSTEM (TM 1-1520-238-T-8).
8. AVIONICS CONFIGURATION - VHF AM - FM RADIO SET (TM 11-1520-238-23-2).
9. AVIONICS CONFIGURATION - INTERCOMMUNICATIONS SYSTEM (TM 11-1520-238-23-2).
10. AVIONICS CONFIGURATION - DOPPLER NAVIGATION AN / ASN - 128 (TM 11-1520-238-23-2).
11. AVIONICS CONFIGURATION - DOPPLER NAVIGATION AN / ASN - 137 (TM 11-1520-238-23-2).
12. HELLFIRE MISSILE EQUIPMENT (TM 9-1270-221-23).
13. AVIONICS CONFIGURATION - VDU (TM 11-1520-238-23-2).
14. INSTRUMENTS (TM 1-1520-238-T-5).
15. HS DESIGNATES A HARD SPLICE WHICH CANNOT BE DISCONNECTED.
M DESIGNATES A SOFT SPLICE WHICH MAY BE DISCONNETED FOR A WIRING CHECK.
W118
M69-382-7A
SHEET 7 OF 7
