TM 1-1520-238-23
Change 4
11-292.1
11.62.
PILOT CYCLIC STICK FLIGHT CONTROL ARM ASSEMBLY DISASSEMBLY/ASSEMBLY
(AVIM) – continued
g. Install arm (15) on shaft (11).
(1) Apply lubricant to faying surfaces and bore of
arm (15) that contact shaft (11). Use damping
fluid (item 69, App F).
(2) Install arm (15) on shaft (11).
h. Install collar (12) on shaft (11).
(1) Apply lubricant to faying surfaces of collar
(12) that contact shaft (11). Use damping fluid
(item 69, App F).
(2) Apply adhesive to shaft (11) Key seat. Use
adhesive (item 3A, App F).
(3) Apply adhesive to key (14). Coat all surfaces
except end to be inserted first. Use adhesive
(item 3A, App F).
(4) Install key (14). Wipe excess adhesive from
key (14).
(5) Aline and install collar (12) with key (14) and
shaft (11).
(6) Install new rivet (13) dry (TM 1-1500-204-23).
i. Allow adhesive to cure 12 HOURS at ambient
temperature or cure 1.5 HOURS at 135 F (57
C).
j. Install lever (9) on arm (1).
(1) Aline lever (9) on shaft (11).
(2) Install new rivet (10) dry (TM 1-1500-204-23).
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13
10
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M04-4295-10
