TM 1-1520-238-23
11-86
Change 3
11.12.
AFT LONGITUDINAL BELLCRANK REMOVAL/INSTALLATION – continued
c. Remove left side of bellcrank (9) from bell-
crank (2).
(1) Remove sealant from attaching hardware
(para 1.47).
(2) Remove and discard cotter pin (14).
(3) Hold bolt (15). Use socket.
(4) Remove nut (16) and washer (17). Use open
end wrench.
WARNING
FLIGHT SAFETY PART
Heat-treated condition of aft longitudi-
nal bellcrank and bolts is critical to
their service ability. Any indication of
heat oxidizing (discoloration), where
visually detectable, requires replace-
ment of the part. These parts must be
protected from unscheduled heating
and external impact during inspection
and other handling procedures.
NOTE
Do not remove bolt until bellcrank is to be
removed.
d. Remove bellcrank (9) from bellcrank (2).
(1) Remove sealant from attaching hardware
(para 1.47).
(2) Position and support bellcrank (2) to allow
removal of bolt (11).
(3) Remove bolt (11), washer (18) (if installed),
bushing (19), and spacer (20).
(4) Position and support bellcrank (2) to allow
removal of bolt (15).
(5) Remove bolt (15), washer (21) (if installed),
bushing (22), and spacer (23).
11.12.4. Cleaning
a. Wipe removed and attaching parts with a
clean rag.
GO TO NEXT PAGE
M04-1719-10A
2
17
14
15
9
16
M04-1719-4
19
11
18
9
20
22
21
15
2
23
