TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date RIGHT FUSELAGE AREA #3 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial ALL/C 3.26 Remove, clean, inspect, and repack forward landing gear wheel bearings. ALL/C 3.27 Forward landing gear support structure for buckling, cracks, corrosion, and loose or missing hardware. Access 24 ALL 3.28 Forward landing gear strut for leakage, cleanliness of exposed piston, and normal extension (visual). ALL 3.29 Forward external cargo hook for freedom of motion, cleanliness, damage, bumpers and corrosion. Attachment fitting on structure for cleanliness. Hook latch mechanism for locked position. Manual release cable for sufficient clearance between ball fitting and lever (through inspection window).  Electrical harness and release cable for proper installation and cuts, kinking or fraying. Latch roller for freedom of operation. "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-16