TM 1-1520-238-23
11-527
11.120. CPG TO PILOT LONGITUDINAL F.S. 118.50 CONTROL FLIGHT BRACKET ASSEMBLY
REMOVAL/INSTALLATION – continued
11.120.6. Installation
CAUTION
To prevent damage to flight control sys-
tem components, do not use force to
aline bellcrank with bracket or to aline
push–pull rod with bellcrank.
NOTE
Install laminated spacers between the
bracket and the airframe. Adjust thick-
ness of the laminated spacer to obtain
minimum 0.010 INCH clearance from any
structure.
a. Install bracket (8) on airframe (14).
(1) Position bracket (8) on airframe (14).
(2) Install two bolts (17) and two bolts (18)
through bracket (8) and four spacers (19) into
airframe (14).
(3) Install four washers (16) and nuts (15).
(4) Verify minimum clearance of 0.010 INCH is
maintained between bracket (8) and any
structure.
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14
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16
19
18
15
16
19
8
M04-4326-6
