TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date FORWARD ROTOR, CROWN, AND TUNNEL, AREA #7 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial ALL/C 7.19 First stage mixing bellcranks and links for damage, corrosion, security, and evidence of interference. Control stops for damage and security. Adjacent area for damage and foreign objects. ALL/C 7.20 First stage mixing complex supports and adjacent structure for buckling and cracks. ALL/C 7.21 Longitudinal cyclic trim link for security.  Longitudinal cyclic trim actuator and connector for security. Actuator, link wire bundles, and rod ends for evidence of chafing. Access 30, 72 ALL/C 7.22 Longitudinal cyclic trim yoke for damage and corrosion. Inspect forward yoke and inside diameter of the forward yoke shaft for corrosion. Yoke attaching hardware for security and evidence of looseness or wear. Access 30, 72 "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-48