TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date NO. 1 ENGINE AREA #4 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial NO. 1 ENGINE AREA #4 ALL/C 4.1 Engine inlet (screen removed) and bypass panels for cleanliness and broken or damaged wire mesh. Fiberglass for cracks or delamination. Fasteners for security and loose or missing hardware.  Lower screen inspection panel for security at hinge and latch mechanism. Access 60 ALL/C 4.2 Engine transmission for leaks, evidence of chafing, cracks, and security of components and hardware. Access 41, 59, 60 CAUTION Do not remove all bolts from the adapters at the same time during inspection. Adapters are balanced assemblies and requires replacement if all bolts are removed. "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-19