TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date FORWARD ROTOR, CROWN, AND TUNNEL, AREA #7 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial ALL/C 7.37 Rotary-wing blade surfaces for delamination, unbonding, blisters, and cracks. Nose and erosion caps for cracks and unbonding.  Trailing edge and trim tabs for cracks, twisting, and unbonding. Electrical lead wire brackets for damage and unbonding. Tip covers for damage and security. Root end composite pads (upper and lower) for unbonding or delamination. Lightening jumper strips for damage, proper bonding, and security. Shock absorber attachment brackets, including filament windings filler material, for cracks and voids. Refer to TM 55-1520-240-23. Access 30, 72 ALL 7.38 Weather protective cover for chafing, cracks, and delamination. Attaching hardware for security. Adjacent fixed fairings for cracks and chafing. Access 30, 72 "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-52