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 3.14 Lubricate aft landing gear grease fittings. ALL 3.15 Engine water wash system quick disconnect for security and condition. (With  74 ) ALL/C 3.16 Aft external cargo hook retaining bolt (access panel removed) and safety bolt for proper installation and corrosion. ALL 3.17 Aft 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, 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. 2-14