AFT LONGITUDINAL BELLCRANK REMOVAL/INSTALLATION continued

AFT LONGITUDINAL BELLCRANK REMOVAL/INSTALLATION continued - TM-1-1520-238-23-7-1_113

AFT LONGITUDINAL BELLCRANK REMOVAL/INSTALLATION continued - TM-1-1520-238-23-7-1_115

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 11-90 Change 4 11.12. AFT LONGITUDINAL BELLCRANK REMOVAL/INSTALLATION – continued e. Install servocylinder (1) on bellcrank (2). (1) Aline servocylinder (1) with bellcrank (2). (2) Insert alinement bolt (2.1) halfway through bellcrank (2), nylon washer (8), and servocy- linder (1) from inboard side of bellcrank. (3) Insert bushing (7) through bellcrank (2) until it seats against servocylinder (1). CAUTION Threads of bolt and nut shall be clean and compound free. Contaminated threads can cause improper torque, which may cause damage to flight control system. (4) Apply a light coat of corrosion preventive compound to shank of bolt (4). Use corrosion preventive compound (item 62A, App F). (5) Install bolt (4) through washer(s) (6) (if re- quired) and force alinement bolt (2.1) out of bellcrank (2). (6) Check fit of self-retaining bolt (4) (para 11.1). GO TO NEXT PAGE 8 2.1 1 7 2 M04-1719-11 M04-1719-12 1 6 4 2 2.1

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