TM 1-1520-238-T-7
11–114
Change 6
11–13.
FLIGHT CONTROL SYSTEM – WIRING INTERCONNECT DIAGRAM
11–13
J403
W119
L22
L23
PILOT LONGITUDINAL
(PITCH) TRIM MAGNETIC BRAKE
(ROLL) TRIM MAGNETIC BRAKE
PILOT LATERAL
W118
W118
J1047
J1049
W255
W117
J407
P407
W119
CB87
(NOTE 7)
P463
J1
5A
P/O PILOT CIRCUIT
BREAKER PANEL (CENTER)
P113
J118
J113
P118
W117
A13
W119
J1048
(PILOT)
(NOTE 4)
FORCE TRIM ON
W211
P686
P447
J2
P686
J2
W211
J447
P403
B
A
(NOTE 1)
M70-001-1B
SHEET 1 OF 3
B
A
(NOTE 1)
B
A
(NOTE 1)
L21
PILOT DIRECTIONAL
28 VDC
B9
(YAW) TRIM MAGNETIC BRAKE
BUS
Y
B8
TRIM
EMERG
6
28 VDC
7
(NOTE 6)
FORCE TRIM
REL SWITCH S3
28 VDC
IN
A400
P/O CPG CYCLIC STICK
IN
28 VDC
(NOTE 5)
4
6
5
RELEASE
7
8
9
12
11
10
ON
A401
A9
A5
P/O PILOT CYCLIC STICK
A11
116
B7
A10
P/O DASEC
A69
117
A76
(NOTE 8)
1
FORCE TRIM
REL SWITCH
S3
W605
FORCE TRIM
RELEASE ON
(PILOT OR CPG)
(NOTE 2)
A(2)
B(2)
C(2)
D(2)
E(2)
F(2)
G(2)
H(2)
J(2)
K(2)
L(2)
M(2)
N(2)
1
2
Z
ADC
