TM 1-1520-238-23
Change 2
11-69
11.9.
LONGITUDINAL AND COLLECTIVE BELLCRANKS REMOVAL/INSTALLATION – continued
(12) Apply sealing compound around bolt heads
(5) and (11), washers (8), (14), and (15), and
nuts (6) and (12). Use sealing compound
(item 176, App F).
c. Install aft longitudinal bellcrank (para 11.12).
d. Install longitudinal links (para 11.13).
e. Install lateral bellcrank and lateral links (para
11.11).
f. Inspect (QA).
g. Install fairings T205L and T205R; install pan-
els L200 and R200 (para 2.2).
h. Perform flight control system maintenance
operational check (TM 1-1520-238-T).
END OF
M04-1727-8
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