TM 1-1520-238-T-6
9329
9114.
PILOT EDGE-LIGHTS WIRING INTERCONNECT DIAGRAM (cont)
9114
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 - RADAR JAMMER AN / ALQ - 136 (TM 11-1520-238-23-2).
2. CW - 28 VDC OUT, ARM - 0 TO 28 VDC IN, CCW - RTN.
3. AERIAL ROCKET CONTROL SYSTEM - ARMAMENT (TM 9-1090-208-23-2).
4. HS DESIGNATES A HARD SPLICE WHICH CANNOT BE DISCONNECTED.
M DESIGNATES A SOFT SPLICE WHICH MAY BE DISCONNECTED FOR A WIRING CHECK.
5. CW - 5 VDC OUT, ARM 0 TO 5 VDC IN, CCW - RTN.
6. INSTRUMENTS (TM 1-1520-238-T-5).
7. AVIONICS CONFIGURATION - VIDEO DISPLAY UNIT (TM 11-1520-238-23-2).
8. AVIONICS CONFIGURATION - VHF / UHF RADIO SETS (TM 11-1520-238-23-2).
9. FLIGHT CONTROL SYSTEM (TM 1-1520-238-T-7).
10. AVIONICS CONFIGURATION - HARS (TM 11-1520-238-23-2).
11. HYDRAULIC SYSTEM (TM 1-1520-238-T-5).
12. LANDING GEAR SYSTEM (TM 1-1520-238-T-4).
13. UTILITY SYSTEM - ROTOR BLADES DE - ICE (TM 1-1520-238-T4).
14. AVIONICS CONFIGURATION - RADAR ALTIMETER SET (TM 11-1520-238-23-2).
15. AVIONICS CONFIGURATION - RADAR WARNING (TM 11-1520-238-23-2).
16. AREA WEAPON SYSTEM - ARMAMENT (TM 9-1090-208-23-2).
17. AVIONICS CONFIGURATION - IR JAMMER AN / ALQ - 144 (TM 11-1520-238-23-2).
18. AUXILIARY POWER UNIT (TM 1-1520-238-T-8).
19. AVIONICS CONFIGURATION - ADF (TM 11-1520-238-23-2).
20. AVIONICS CONFIGURATION - IFF (TM 11-1520-238-23-2).
21. UTILITY SYSTEM - CANOPY DE - FOG AND ANTI - ICE (TM 1-1520-238-T-8).
22. FUEL SYSTEM (TM 1-1520-238-T-7).
23. ENVIRONMENTAL SYSTEM (TM 1-1520-238-T-8).
24. MISSION EQUIPMENT (TM 1-1520-238-T-8).
25. AVIONICS CONFIGURATION - KY58 SECURITY SYSTEM (TM 11-1520-238-23-2).
26. HELLFIRE MISSILE SYSTEM (TM 9-1427-475-20).
27. POWER PLANTS (TM 1-1520-238-T-4).
M69-375-10A
SHEET 10 OF 10
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