TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date COCKPIT AREA #10 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial ALL 10.38 Pilot’s and copilot’s brake cylinders for leaks and security. Brake hose for leaks and proper routing. ALL 10.39 Left power distribution panel (opened) for security of components and loose or missing hardware. Wiring and connections for damage, security, chafing, and proper support. Wiring insulation for cuts, cracks, and fraying. Inspect all left PDP circuit breakers for evidence of water/moisture, arcing/burning, and circuit breaker terminal studs/hardware for evidence of corrosion/salt. ALL 10.40 Instrument range marks for accuracy and legibility. Refer to TM 1-1520-240-10. Instruments lenses for cracks, cleanliness, looseness, and slippage marks (if required). Instruments for security and proper position.  Knobs for security and damage. ALL 10.41 Perform inspection of pitot-static system. "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-76