TAIL ROTOR PITCH LINK REMOVAL/INSTALLATION continued

TAIL ROTOR PITCH LINK REMOVAL/INSTALLATION continued - TM-1-1520-238-23-7-2_357

TAIL ROTOR DE-ICE BRUSH BLOCK REMOVAL/INSTALLATION

TM-1-1520-238-23-7-2 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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TM 1-1520-238-23 Change 3 11-1175 11.277. TAIL ROTOR PITCH LINK REMOVAL/INSTALLATION – continued b. Install pitch link (1) on pitch horn (2). Torque nut (4) 225 to 285 INCH-POUNDS. (1) Aline link (1) with horn (2). (2) Install bolt (5) through washer (6), safety washer (7), link (1), and horn (2). (3) Check fit of self-retaining bolt (5) (para 11.1). (4) Install nut (4). Torque nut (4) to 225 INCH- POUNDS. Use torque wrench. (5) Increase torque to aline cotter pin hole, but do not exceed 285 INCH-POUNDS. (6) Install new cotter pin (3). (7) Apply primer to bolt head (5) and nut (4). Use epoxy primer coating kit (item 78, App F). c. Inspect (QA). d. Install tail rotor electrical leads (para 11.276). END OF TASK M04-1764-5 1 5 6 7 4 2 3 1 2

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