TM 55-1520-240-PMPHASE NO. _____Area Name and No.Aircraft Serial No.DateNO. 1 ENGINE AREA #4InspectPhaseNo’sInspection RequirementsStatusFaults and/or RemarksAction TakenInitialALL/C4.12 No. 1 engine accessory gearboxchip detector for contamination.Remove inspect, andclean. Onhelicopters (Without 74 ), refer toTM 55-2840-254-23. On helicopters(With 74 ), refer to TM 1-2840-265-23.Access 55, 58, 60ALL4.13 Compressor housing and visibleportions of air diffuser for damage andsecurity. Access 55, 58, 60ALL4.14 Compressor bleed band andretainer spacers for wear. Actuator fordamage and security. Access 55, 58,60ALL4.15 Combustion chamber housing andfire shields for cracks, hot spots, burnedareas, and buckling. Access 55, 58, 60ALL4.16 Thermocouple bus bars fordamage and security. Access 55,58, 60ALL4.17 Fire detection system sensingelements throughout the area forchafing, damage, and security."FOD REMINDER"Check work area for tools and parts after completion of maintenance and inspection.2-22
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