TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date NOSE AREA #1 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial ALL 1.10 Electrical wiring and connectors for security, visible through right and left chin bubble windshield panels or nose access door. Wires for evidence of chafing, proper support, and condition of insulation.  Terminal boards for condition and proper installation of covers.  Visible pitot-static and AFCS sideslip port tubing for proper connection and support and not kinked. Access 29 ALL/C 1.11 Dynamic absorber for security. Support structure for cracks and loose or missing hardware. Access 29 ALL/C 1.12 Entire area for structural damage, skin cracks, loose or missing rivets, dents and evidence of corrosion. Paint for chipping or peeling. Stencil and decals for condition. ALL/C 1.13 Inspect and lubricate the pedal box bearings only if they are removed from the aircraft for other maintenance. 2, 4 1.14 Inspect ducting for security of clamps, cuts, chaffing, and FOD. Access door and seal for cuts, damage, security, distortion, and wear. Access 77 "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-5