时间:2018-08-12 12:52来源:蓝天飞行翻译公司 作者:直升机翻译 点击:次
Collective Force Trim OFF or Fail Collective Force Trim Release Failure AFCS Quick Disconnect Procedure Guidance Control Panel Failure Single Collective AUTOPILOT Failure Dual Collective AUTOPILOT Failure MAU failure with FD engaged Avionic Systems (AVIONIC) primary or/and Multifunctional flight display UNIT Failure DISPLAY UNIT OVERHEATING Display Unit Degraded ADS Failure AHRS Failure Aural warning system failure AVIONIC fault Modular Avionics Unit Overheat/Fail Modular Avionics Unit Overheat/Fail (cont) Multifunction control display unit OVERHEATING System Configuration Failure Validate Configuration Flight data recorder FAILure Cockpit voice recorder failure Flight Management system FAILURE GPS FAILure FMS/GPS Miscompare FMS/GPS Miscompare Unavailable COMMUNICATION SYSTEM (AVIONIC) vhf overheat audio Panel failure MRC Overheat ELECTRICAL (ELEC) SINGLE DC GENERATOR FAILURe DC generator overheat DC generator overLOAD main battery off auxiliary battery off LOSS OF Main and/Or Auxiliary BATTERY SUPPLy BUS tie open DC MAIN BUS FAilure ENGINE MALFUNCTIONS (ENG) COMPRESSOR STALL Unusual Engine noise ENGINE limit exceedance ENGINE OIL Temperature ENGINE OIL PRESSURE HIGH ENGINE CHIP DETECTOR Engine fire detector system Engine control lever Engine Control Lever position Engine Mode select switch Engine power turbine overspeed Engine electronic control Data degradation of Engine control functions Engine Hot start Torque LImiter INTER Turbine Temperature LImiter Engine power turbine overspeed detect failure FUEL FILTER BY-PASS Fuel icing fuel heater Engine And ROTOR Parameters miscompare Engine ANALOGuE SENSOR Failure ENGINE IN FLIGHT RESTART Procedure (ENG FLT RESTART) Engine Manual Starting Engine Manual Starting on ground Procedure Manual Start Procedure Engine Manual In Flight ReStart Procedure (ENG FLT RESTART) Engine Shutdown Using ECL/Manual FUEL SYSTEM (FUEL) fuel low FUEL PRESSURE LOW Double Fuel Pump Failure FUEL Contents Gauging unit fAILURE Fuel low sensor failure Fuel probe failure Fuel contents gauging unit test system failure Abnormal Fuel Consumption HYDRAULIC System (HYD LDG GR) HYDRAULIC PRESSURE LOW NORmal landing gear PRESSURE LOW Emergency landing gear PRESSURE LOW HYDRAULIC FLUID OVERHEATING HYDRAULIC FLUID LEVEL LOW HYDRAULIC pump 1, 2 or 4 failure main VALVE SEIZURE IN MAIN OR TAIL ROTOR SERVO NOSEWHEEL unlocked (in Flight) Park brake malfunction Park brake On In Flight landing gear Retracted |