TM 1-1520-238-23
11-961
11.224.
STABILATOR ACTUATOR REMOVAL/INSTALLATION – continued
e. Lock stabilator (5) in up position.
(1) Move stabilator (5) up until rig pin holes (13)
and (14) are alined.
(2) Install -9 rig pin (15) in alined holes (13) and
(14).
f. Remove actuator (6) from airframe (16).
(1) Remove and discard cotter pin (17).
(2) Remove nut (18).
(3) Remove bolt (19), washer (20), and bushing
(21).
11.224.4. Cleaning
a. Wipe removed and attaching parts with a
clean rag.
11.224.5. Inspection
a. Check all removed and attaching parts for
damage (para 11.190).
b. Check removed and attaching parts for corro-
sion (para 1.49).
c. Check all installed bushing(s) and/or bear-
ing(s) for wear (para 11.190).
d. Check all removed bushing(s) and/or bear-
ing(s) for wear (para 11.4).
GO TO NEXT PAGE
M04-2111-4
5
15
14
13
M04-2111-7
16
18
17
6
21
20
19
