TM 1-1520-238-PM 2–23 PHASE NO. Date Aircraft Serial No. Area Name and No. LEFT FORWARD AVIONICS BAY AND MLG – 3 Inspect Phase Nos. Initial Action Taken Faults and/or Remarks Status Inspection Requirements 2,4 8. MLG trailing arm for cracks, distortion, or corrosion. Cross tube end pivot boss C for security, damaged or worn bearing, loose or missing hardware. Hydraulic brake line for leakage, dents, corrosion, and clamping security. Access L115 ALL 9. MLG end cap for cracks, distortion, fractured weld, and elongated bolt holes. C ALL 10. MLG SHOCK STRUT UPPER AND LOWER ROD ENDS FOR BEARING C DAMAGE. 2,4 11. MLG wheel for cracks, distortion, or corrosion. Hub for grease leakage. Tire C for tread damage or uneven wear. “FOD REMINDER” Check work area for tools and parts after completion of maintenance and inspection.