TM 55-1520-240-PMPHASE NO. _____Area Name and No.Aircraft Serial No.DateFORWARD ROTOR, CROWN, ANDTUNNEL, AREA #7InspectPhaseNo’sInspection RequirementsStatusFaults and/or RemarksAction TakenInitialALL/C7.23 Forward transmission upper cover,mount lugs, mounting hardware, andadjacent structure for security, buckling,cracks, and corrosion. Transmissiontorque box structure for twisting,buckling, cracks, damage, and loose ormissing rivets. Access 30, 72ALL/C7.24 Upper boost servocylindersfor leaks and security, chafing orinterference with adjacent structurecomponents. Support fittings forwear, damage, and cracks. Adjacentstructure for cracks, buckling, andloose or missing rivets. Bearings andbushings for condition, radial and axialplay.ALL/C7.25 Drive arms and collar for excessivewear at hinge points. Bearings forfrayed or unbonded liners. Access 30,72ALL7.26 Forward transmission oil coolermount flanges for cracks. Hardware forsecurity. Access 30, 72"FOD REMINDER"Check work area for tools and parts after completion of maintenance and inspection.2-49
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