TM 55-1520-240-PMPHASE NO. _____Area Name and No.Aircraft Serial No.DateAFT ROTOR AND PYLON, AREA #6InspectPhaseNo’sInspection RequirementsStatusFaults and/or RemarksAction TakenInitialALL/C6.6 Aft rotary-wing head droop stopsand interposer blocks (shroud removedand blades raised) for damage, wear,and security. Retorque fixed droop stopretaining bolts. Droop stop shroudsfor security and damage. Refer to TM55-1520-240-23. Access 5, 47ALL/C6.7 Rotary-wing blade surfaces fordelamination, unbonding, blisters, andcracks. Nose and erosion caps forcracks and unbending. Trailing edgeand trim tabs for cracks, twisting, andunbonding. Electrical lead bracket fordamage and unbonding. Tip coversfor damage and security. Root endcomposite pads (upper and lower) forunbonding or delamination. Lighteningjumper strips for damage, properbonding, and security. Shock absorberattachment brackets, including filamentwindings filler material, for cracks andvoids. Refer to TM 55-1520-240-23.Access 5, 47ALL6.8 Weather protective cover forchafing, cracks, and delamination.Attaching hardware for security.Adjacent fixed fairings for cracks andchafing. Access 5, 47"FOD REMINDER"Check work area for tools and parts after completion of maintenance and inspection.2-36
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