TM 1-1520-238-T-6
9–661
9–334. PILOT CAUTION AND WARNING SYSTEM – WIRING INTERCONNECT
9–334
DIAGRAM (cont)
NOTES:
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC LINE, AND THE NUMBER IN
PARENTHESIS IDENTIFIES THE SHEET NUMBER WHERE THE SIGNAL TERMINATES.
1. GROUND AT FAULT INPUT.
2. AUXILIARY POWER UNIT (TM 1-1520-238-T-8).
3. UTILITY SYSTEM (TM 1-1520-238-T-8).
4. POWER PLANTS (TM 1-1520-238-T-4).
5. HYDRAULIC SYSTEM (TM 1-1520-238-T-5).
6. AREA WEAPON AND ROCKETS (TM 9-1090-238-23-2).
7. AVIONICS CONFIGURATION - INTERCOMMUNICATION SYSTEM (TM 11-1520-238-23-2).
8. FIRE CONTROL SYSTEM (TM 9-1230-476-20-2).
9. DRIVE SYSTEM (TM 1-1520-238-T-4).
10. FLIGHT CONTROL SYSTEM (TM 1-1520-238-T-7).
11. HS DESIGNATES A HARD SPLICE WHICH CANNOT BE DISCONNECTED.
M DESIGNATES A SOFT SPLICE WHICH MAY BE DISCONNECTED FOR A WIRING CHECK.
12. LANDING GEAR SYSTEM (TM 1-1520-238-T-4).
13. AVIONICS CONFIGURATION - RADAR WARNING SYSTEM (TM 11-1520-238-23-2).
M69-013-8
SHEET 8 OF 8
