TM 1-1520-238-T-6
Change 5
9–509
9–234. CIRCUIT PROTECTION SYSTEM (DC ESSENTIAL BUS 3 – PILOT STATION) –
9–234
WIRING INTERCONNECT DIAGRAM (cont)
P/O ELECTRICAL POWER DISTRIBUTION BOXJ10 P454
V
A402
1
W668
J2
P2
J30
P432
A10
H
E
J25
P437
X
J26
P483
A2
J24
P441
B1
B2
J22
P457
A11
(NOTE 1)
(NOTE 4)
(NOTE 5)
(NOTE 6)
(NOTE 5)
TB2 - 9
K
M
TB2 - 4
B
TB2 - 28
J1
P1
TB2 - 3
J1
P1
47
14
A
F
TB2 - 22
53
W605
k
W
A
GS8
P
51
46
J1
P1
(NOTE 2)
J5
P442
A9
(NOTE 3)
J2
P2
J
17
J12
P425
A11
(NOTE 5)
27
33
34
A
C
TB2 - 7
D
G
B
A
J27
P431
B1
A10
(NOTE 6)
J20
P433
A12
(NOTE 7)
J27
P431
B9
B11
(NOTE 6)
J28
P427
D
C
(NOTE 6)
E
D
C
XK3 - H
(NOTE 7)
J2
P2
f
A3
A
D
F
29
A(1)
D(1)
C(1)
E(1)
F(1)
B(1)
G(1)
H(1)
J(1)
K(1)
L(1)
M(1)
N(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. PILOT NIGHT VISION SENSOR (PNVS)
(TM 1-5855-265-T).
2. AVIONICS CONFIGURATION -
DOPPLER NAVIGATION AN / ASN - 128
(TM 11-1520-238-23-2).
3. AVIONICS CONFIGURATION - HARS
(TM 11-1520-238-23-2).
4. AVIONICS CONFIGURATION - AIR
DATA SUBSYSTEM
(TM 11-1520-238-23-2).
5. ARMAMENT - AERIAL ROCKET
CONTROL SYSTEM
(TM 9-1090-208-23-2).
6. FLIGHT CONTROL SYSTEM
(TM 1-1520-238-T-7).
7. UTILITY SYSTEM - ROTOR BLADE
DE - ICE (TM 1-1520-238-T-8).
8. AVIONICS CONFIGURATION - EGI
(TM 11-1520-238-23-2) (ADD)
9. AVIONICS CONFIGURATION - DTU
(TM 11-1520-238-23-2) (ADD)
W605
W605
W605
W605
W605
W116
W266
W102
W119
W119
W119
W119
W117
W117
W211
W211
W211
M69-390-2B
SHEET 2 OF 2
