TM 1-1520-238-T-7
11–233
11–28.
DASE – WIRING INTERCONNECT DIAGRAM (BUCS ACTIVATED) (cont)
11–28
M70-327-18A
SHEET 18 OF 29
2
8
2
P/O PILOT MASTER
CAUTION/WARNING PANEL
P1 J164
B4
J2 P31
t
B5
P/O CPG MASTER
CAUTION/WARNING PANEL
P1 J166
B4
B5
P31 J2
E
F
J1 P19
40
P/O CPG CAUTION/WARNING PANEL
J2 P20
P20 J2
E
F
J1 P18
P/O PILOT
CAUTION/WARNING PANEL
P18 J1
114
P908 J908
A17
J447 P447
A20
P456 J456
A12
J5 P499
A3
P/O AFT AVIONICS
MATRIX MODULE
P493 J4
B12
J402 P402
B19
J756 P756
24
W118
W118
W118
W118
W119
W211
W118
R
P
N
J
K
A4
A7
A10
B17
W170
W170
W115
(NOTE 13)
(NOTE 14)
(NOTE 14)
(NOTE 13)
W642
(NOTE 13)
TB3 - 3
TB3 - 4
(NOTE 14)
P20 SP1(HS)
J417 SP1(M)
J408 SP1(M)
(NOTE 14)
P682 SP4 (HS)
(HS)
J215
SP1
P693
SP1
(HS)
BUCS FAIL INDICATOR
(RED)
BUCS FAIL INDICATOR
(RED)
DS31
DS31
28 VDC
RTN
A157
BUCS FAIL
SIGNAL
BUCS FAIL INDICATOR
(AMBER)
BUCS FAIL
SIGNAL
BUCS ON
INDICATOR (AMBER)
t
40
HI
LO
J415 SP1(M) (NOTE 14)
A106
A323
(NOTE 14)
P402 J402
22
W211
W211
D(2)
A(19)
B(19)
C(19)
D(19)
E(19)
F(19)
G(19)
H(19)
(NOTE 14)
(NOTE 13)
(NOTE 13)
