TM 1-1520-238-23
11-911
11.210.
PILOT DIRECTIONAL CONTROL POSITION LINEAR VARIABLE DIFFERENTIAL TRANSDUCER
(LVDT) REMOVAL – continued
NOTE
On BUCS-equipped aircraft, an electrical
lead will be attached to LVDT.
c. Detach connector P231 (1) from receptacle
J231 (2).
d. Remove connector (1) from LVDT wire har-
ness (3), if required (TM 55-1500-323-24).
e. Remove electrical lead (4) from ground stud
(5).
(1) Remove nut (6) and washer (7).
(2) Remove lead (4) from stud (5).
f. Remove clamp (8) from LVDT (9).
(1) Remove nut (10) and washer (11).
(2) Remove bolt (12), washer (13), lead (4), and
washer (14).
(3) Remove clamp (8) from LVDT (9).
GO TO NEXT PAGE
3
M04-1859-2
VIEW
LOOKING UP AND AFT
1
2
7
M04-1859-3
9
8
12
10
11
14
4
13
6
5
