TM 1-1520-238-T-7
Change 7
11–205
11–27.
DASE– WIRING INTERCONNECT DIAGRAM (COLLECTIVE) (BUCS DEACTIVATED) (cont)
11–27
(NOTE 9)
P/O PILOT CIRCUIT BREAKER PANEL
(CENTER)
P371-38
S350 SP1 (M)
GS850
A
(NOTE 5)
1
1
J1
P463
S
CB29
COMM IFF
5A
A76
EMERG BUS
28 VDC
(NOTE 10)
P682 SP5 (M)
P371-39
GS601
GS601
P/O DASEC
P/O AFT AVIONICS MATRIX MODULE
A323
S350 SP2 (M)
M70-220-4C
SHEET 4 OF 14
CONTROL
CIRCUITS
SQUAT SWITCH
28
27
72
73
121
114
HI 5 VDC IN
LO (NOTE 6)
COLLECTIVE SAS RTN
28 VDC
28 VDC
GND
HARS RATE
VALID
COLLECTIVE/SAS
POWER IN
COMPUTER
POWER IN
P682 J3
28 VDC
28 VDC
RTN
112
107
108
COLLECTIVE SCAS
SOLENOID
BUCS SOLENOID
VALVE - COLLECTIVE
IN
P683 J4
21
20
0 - 10 VAC
(NOTE 1)
PILOT COLLECTIVE
SERVOCYLINDER
POSITION (LVDT)
P688 J1
58
57
33
32
29
28
38
39
A1
A2
A6
A5
P
P
P
P
A
C
B
E
G
F
P499 J5
J5 P499
W211
W211
P
P
P
P
26 VAC IN
EXCITATION
IN (PRI)
AK(3)
CPG COLLECTIVE
(VERTICAL) LVDT
P
P
P
P
P944 - 1
P944 - 3
P944 - 5
P944 - 6
AIR DATA
SUB SYSTEM
J447 P477
J234 P234
B17
B18
D
C
P
J230 P230
PILOT COLLECTIVE
(VERTICAL) LVDT
SIGNAL OUT
(SEC)
SIGNAL OUT
(SEC)
26 VAC IN
EXCITATION
IN (PRI)
P
B
A
A
B
C
D
C
P(2)
A69
MT4
MT8
S350
J459 P459
B15
B14
K(2)
0 - 5 VAC
(NOTE 4)
5 VDC
5 VDC
0 - 10 VAC
(NOTE 1)
COLLECTIVE
SERVOCYLINDER
POSITION
LVDT 2 IN
OMNIDIRECTIONAL
AIRSPEED VALID
AIR DATA VALID
CPG COLLECTIVE
STICK POSITION
(NOTE 11)
AE(3)
AG(3)
L(2)
M(2)
AH(3)
AL(3)
AF(3)
P686 J2
AC(3)
J
A3
T3
T3
T3
A(8)
TB3 - 3
W211
W211
W211
W211
W119
W119
W605
(NOTE 10)
HI
LO
LO
HI
LO
HI
LO
HI
W119
K
(NOTE 18)
W119
2
AD(3)
AJ(3)
(NOTE 17)
H
2
1
