TM 1-1520-238-T-6
9–182
9–24.
DC ELECTRICAL POWER GENERATION – WIRING INTERCONNECT DIAGRAM (cont)
9–24
T3
T3
J16
28 VDC IN
A2
35A
A1
TEMP HIGH
TRANSFORMER / RECTIFIER 1
CB7
G
AC GND
D
P6
A
GS410
A
B
PS1
J1
A
J1
P12
F
I
B
P/O GROUND SERVICE UTILITY
1
DC ELEC UTIL PWR
A
GS431
A3
P/O GROUND UTILITY RECEPTACLE
CIRCUIT BREAKER BOX
+28 VDC OUT
CONNECTOR
GS444
D
F
I
B
G
AC GND
TEMP HIGH
+28 VDC OUT
PS2
TRANSFORMER / RECTIFIER 2
115 / 200 VAC
3Ø IN
(NOTE 5)
115 / 200 VAC
3Ø IN
(NOTE 5)
ØC
ØB
ØA
ØC
ØB
ØA
W668
W668
W668
W118
L(2)
M(2)
A(1)
E(1)
F(1)
G(1)
V(2)
W(2)
H(1)
J(1)
K(1)
D(1)
AM(3)
A
GS443
NOTES:
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC
LINE, AND THE NUMBER IN PARENTHESIS IDENTIFIES THE SHEET
NUMBER WHERE THE SIGNAL TERMINATES.
1. ALL 28 VDC OUTPUTS.
2. OVER CURRENT DETECTOR CIRCUIT.
3. VOLTAGE REGULATOR.
4. INDICATOR LIGHTS WITH GND INPUT.
5. GND OUT AT FAULT.
6. BOTH INPUT FAULTS MUST BE PRESENT TO TURN ON LIGHT.
7. AVIONICS CONFIGURATION (TM 11-1520-238-23-2).
8. HELLFIRE MISSILE EQUIPMENT (TM 9-1427-475-20).
9. FUEL SYSTEM (TM 1-1520-238-T-7).
10. ARMAMENT SUBSYSTEM (TM 9-1090-208-23-2).
11. PNVS (TM 11-5855-265-20-2).
12. UTILITY SYSTEM (TM 1-1520-238-T-8).
13. FLIGHT CONTROL SYSTEM (TM 1-1520-238-T-7).
14. INSTRUMENTS (TM 1-1520-238-T-5).
15. POWER PLANTS (TM 1-1520-238-T-4).
16. HYDRAULIC SYSTEM (TM 1-1520-238-T-5).
17. TADS (TM 9-1270-476-20-2).
18. FIRE CONTROL SYSTEM (TM 9-1230-476-20-2).
ABC
AAG
_
GS400
A
B
_
M69-002-6A
SHEET 6 OF 6
