TM 1-1520-238-T-6
9–206
Change 8
9–42.
BATTERY – WIRING INTERCONNECT DIAGRAM (cont)
9–42
115 VAC IN
HEATER THERMAL SWITCH
TEMPERATURE TRANSDUCER OUT
TEMPERATURE TRANSDUCER IN
GROUND OUT
TENTH CELL TAP SENSING OUT
BATTERY (+) SENSING 28 VDC OUT
2
115 VAC IN
P80 - B
P80 - T
C
P80 - C
P80 - R
CHARGER THERMAL SWITCH
P80 - S
P80 - J
P80 - G
3
10
9
11
7
6
4
P80 - F
5
2
-
A
P81
J1
P87
J3
J111 - A
APU
P430 - A4
7.5A
2
1
MAINT LT
CB8
CB148
1
X
J1
P80
X1
X2
1
SWITCH
THERMAL
BATTERY
HEATER ASSY
P80 SP2
P80 SP1
BT1
HR8
-HEATER RETURN
H
H
TRANSDUCER
TEMPERATURE
CHARGER
SWITCH
THERMAL
P80 - E
GS626
+
CELL
TAP
P/O BATTERY
HEATER
24 VDC OUT
CONTROL
TENTH
24 VDC OUT
BATTERY RELAY
BT2
P/O BATTERY CHARGER
(NOTE 1)
CR1
A1
A2
W
K6
BATTERY
RELAY
HEATER
THERMAL
SWITCH
(NOTE 2)
(NOTE 1)
CHARGER OUTPUT
W108
W108
W108
W108
W108
(NOTE 1)
A(1)
B(1)
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 - BATTERY CHARGER (TM 11-1520-238-23-2).
2. AUXILIARY POWER UNIT (TM 1-1520-238-T-8).
M69-003-BA
SHEET 2 OF 2
