TM 1-1520-238-PM 2–72 PHASE NO. Date Aircraft Serial No. Area Name and No. MAIN ROTOR – 10 Inspect Phase Nos. Initial Action Taken Faults and/or Remarks Status Inspection Requirements ALL 12. Pitch links for cracks, distortion, and corrosion. Rod ends for bearing damage C or looseness. Check lower rod end clamp-up to floating bushings. ALL 13. Swashplate uniball for cracks, grooving, flaked or worn-through plating. C ALL 14. Rotating swashplate for cracks, corrosion, grease leakage, and security C of lower seal. Pitch link connection bosses for bending, misalinement, and worn or loose bushings. ALL 15. Stationary swashplate for cracks and corrosion. Lateral and torque link C connection bosses for bending, misalinement, and worn or loose bushings. Access T205L, T205R, T225 “FOD REMINDER” Check work area for tools and parts after completion of maintenance and inspection.