TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date RIGHT FUSELAGE AREA #3 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial RIGHT FUSELAGE AREA #3 1, 3 3.1 Service forward and aft landing gear struts. Check ground contact proximity switch and target for proper rigging and gap, IAW TM 55-1520-240-23. ALL 3.2 Heater fuel solenoid valve for leaks, electrical connector, mounting bracket, and attaching hardware for security. Access 21 ALL 3.3 Hydraulic ground power service panel connections for leaks. Dust cap secure. Access 12 ALL 3.4 Fluid drain lines for damage and obstructions. ALL/C 3.5 Aft landing gear brake (disc and linings). ALL 3.6 Aft landing gear brake hoses for leaks, chafing, and damage. ALL 3.7 Swivel lock, swivel housing, and power steering, actuator assembly for leaks. "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-12