TM 1-1520-238-T-7
11–242
Change 3
11–28.
DASE – WIRING INTERCONNECT DIAGRAM (BUCS ACTIVATED) (cont)
11–28
M70-327-27B
SHEET 27 OF 29
12
P/O AIR DATA
PROCESSOR
J3 P944
P499 J5
J1 P463
B14
P
P
P
P
P
P912 J912
W211
S
R
P
W
T
Z
P/O AFT AVIONICS MATRIX MODULE
(NOTE 13)
J2 - B10
C
A
TB1 - 5
J2 - B1 1 (NOTE 25)
A323
W642
G(28)
1
3
5
6
39
20
P
(NOTE 25)
A636
A(28)
J2 P371
39
B(28)
C(28)
D(28)
E(28)
F(28)
H(28)
38
46
47
J(28)
K(28)
L(28)
M(28)
A310
P/O HARS
(NOTE 26)
(NOTE 26)
J1 P19
46
P/O CPG CAUTION/
WARNING PANEL
ASE
INDICATOR
(AMBER)
(NOTE 13)
J2 P31
g
J1 P750
L
A320
P/O VIDEO DISPLAY UNIT
M
+
-
(NOTE 21)
J459 P459
A323
P18 J1
116
h
A
B
J1 P18
46
ASE
INDICATOR
(AMBER)
P/O PILOT CAUTION/
WARNING PANEL
(NOTE 13)
P908 J908
A16
J2 P20
9
A106
N(28)
K
B18
B19
A15
A16
R(28)
P(28)
P
B13
B12
P
P
P
P
W211
W118
W118
W119
W118
W119
W211
GS240
GS406
38
19
P
TB1 - 5
B15
W211
OAS
FAIL
ADP
FAIL
VxT OUT
RTN
RATE OF TURN
