TM 1-1520-238-23
Change 3
11-917
11.212.
PILOT LATERAL CONTROL POSITION LINEAR VARIABLE DIFFERENTIAL TRANSDUCER (LVDT)
REMOVAL – continued
d. Detach connector P233 (4) from receptacle
J233 (5).
e. Remove two clamps (6) from LVDT wire har-
ness (7).
(1) Remove two screws (8) and washers (9) from
clamps (6).
(2) Remove two clamps (6) from wire harness
(7).
f. Remove connector (4) from wire harness (7), if
required (TM 55-1500-323-24).
NOTE
On BUCS-equipped aircraft, an electrical
lead will be attached to LVDT.
g. Remove electrical lead (10) from ground stud
(11).
(1) Remove nut (12) and washer (13).
(2) Remove lead (10) from stud (11).
h. Remove clamp (14) from LVDT (15).
(1) Remove nut (16) and washer (17).
(2) Remove bolt (18), washer (17), lead (10), and
washer (17).
(3) Remove clamp (14) from LVDT (15).
i. Remove LVDT (15) from bracket (20).
(1) Remove and discard cotter pin (21).
(2) Remove nut (22).
(3) Remove bolt (23) and bushing (24).
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M04-1861-3A
9
9
6
7
22
58
4
21
24
20
6
8
23
15
17
M04-1861-6
12
13
11
18
14
15
16
10
19
10
