TM 1-1520-238-2311-58611.132. CPG TO PILOT CONTROL COLLECTIVE F.S. 118.50 SUPPORT BRACKETREMOVAL/INSTALLATION – continuedCAUTIONTo prevent damage to flight control sys-tem components, do not use force toaline bellcrank with bracket or to alinepush-pull rod with bellcrank.b. Install bellcrank (2) on bracket (8). Torque nut(10) 30 to 40 INCH-POUNDS.(1) Aline bellcrank (2) with bracket (8).(2) Install bolt (11) through washer (12), bushing(13), bracket (14), and bellcrank (2).(3) Check fit of self-retaining bolt (11) (para 11.1).(4) Install nut (10). Torque nut (10) to 30 INCH-POUNDS. Use torque wrench.(5) Increase torque to aline cotter pin hole, but donot exceed 40 INCH-POUNDS.(6) Install new cotter pin (9).c. Install rod (1) on bellcrank (2). Torque nut (4) 30to 40 INCH-POUNDS.(1) Aline rod (1) with bellcrank (2).(2) Install bolt (5) through washer (6), bushing(7), bellcrank (2), and rod (1).(3) Check fit of self-retaining bolt (5) (para 11.1).(4) Install nut (4). Torque nut (4) to 30 INCH-POUNDS. Use torque wrench.(5) Increase torque to aline cotter pin hole, but donot exceed 40 INCH-POUNDS.(6) Install new cotter pin (3).GO TO NEXT PAGE1110M04-4334-72913128571326M04-4334-84
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