TM 55-1520-240-23-9
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INSTALL COCKPIT CONTROL TRANSFER CONNECTING LINKS
(Continued)
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26.
Working through left access (20), torque three
nuts (21, 26, and 58) to 30 to 60 inch-pounds.
Install cotter pins (61, 62, and 63).
27.
Check three bolts (24, 29, and 59). Bolts shall
not rotate with torque less than 10 inch-pounds.
There shall be no axial looseness. If bolt rotates
or is loose, add washer under nut, and repeat
step 26.
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