DIRECTIONAL F.S. 159.98 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION continued

DIRECTIONAL F.S. 159.98 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION continued - TM-1-1520-238-23-7-1_769

DIRECTIONAL F.S. 159.98 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION continued - TM-1-1520-238-23-7-1_771

TM-1-1520-238-23-7-1 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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TM 1-1520-238-23 11-743 11.168. DIRECTIONAL F.S. 159.98 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued 11.168.6. Installation CAUTION To prevent damage to flight control sys- tem components, do not use force if bind- ing or roughness occurs while moving controls with hydraulic power. a. Install rod (1) on bellcrank (8). Torque nut (10) 30 to 40 INCH-POUNDS. (1) Aline rod (1) with bellcrank (8). (2) Install bolt (11) through washer (12), bushing (13), bellcrank (8), and rod (1). (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 do not exceed 40 INCH-POUNDS. (6) Install new cotter pin (9). GO TO NEXT PAGE M04-4371-5 1 8 11 12 9 13 10

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