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 2.33 Fluid drain lines for damage and obstructions. ALL/C 2.34 Access doors, work platforms, and panels for damage.  Latching mechanism for security and proper operation. Seals for cuts, tears, cracks, and security. Engine work platform support struts for security, twisting, and proper operation of pins. Access 57, 60, 61, 62, 63, 66, 68, 69, 70 ALL/C 2.35 Entire area for structural damage, skin cracks, dents or buckling, loose or missing rivets, evidence of corrosion. Paint for chipping or peeling. Stencils and decals for condition. ALL 2.36 Static port for obstruction and damage. "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-11