TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date LEFT FUSELAGE, AREA #2 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial ALL 2.27 Aft landing gear strut for leaks, cleanliness of exposed piston, normal extension (visual). ALL 2.28 Aft landing gear support structure for buckling, cracks, corrosion, and loose or missing fasteners. ALL/C 2.29 Aft landing gear drag links for security, corrosion, cracks, nicks, dents, twisting, and displacement of bearings from bores. All surfaces of lower drag link for cracks, with particular attention to area around forward trunnion anti-rotation bolt hole. Access 61 ALL/C 2.30 Lubricate aft landing gear grease fittings. ALL 2.31 Engine water wash system quick disconnect for security and damage. (With  74 ) ALL 2.32 Static ground wire for security and ground contact. "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-10