TM 1-1520-238-2311-43711.99.LATERAL F.S. 132.84 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued11.99.6. InstallationCAUTIONTo prevent damage to flight controlsystem components, do not use forceif binding or roughness occurs whilemoving controls with hydraulic power.To prevent damage to flight controlsystem components, do not use forceto aline bellcrank with bracket or toaline push-pull rod with bellcrank.a. Install rod (5) on bellcrank (14). Torque nut (16)30 to 40 INCH-POUNDS.(1) Install bolt (17) through washer (18), bushing(19), bellcrank (14), and rod (5).(2) Check fit of self-retaining bolt (17) (para11.1).(3) Install nut (16). Torque nut (16) to 30 INCH-POUNDS. Use torque wrench.(4) Increase torque to aline cotter pin hole, but donot exceed 40 INCH-POUNDS.(5) Install new cotter pin (15).GO TO NEXT PAGEM04-4377-61419171615518
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