藍(lán)天飛行翻譯公司承接AW169直升機(jī)快速檢查單翻譯任務(wù)
時(shí)間：2019-03-10 18:47來源：藍(lán)天飛行翻譯公司 作者：直升機(jī)翻譯 點(diǎn)擊：次
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Miscellaneous System Pitot Heater Off Aircraft Never Exceed Speed Weight On Wheels Switch Failure Sensor Dormant Failure Cockpit Door Open Cabin Door Open Baggage Bay Door Open External Power Socket Door Open Cockpit Vent Fan Failure Cabin Vent Fan Failure Cockpit and Cabin Vent Fan Failure ECS Fail Audio System Failure PFD and MFD Messages Loss of PFD for Pilot in Control Loss of PFD Pilot not in Control Loss of Multi Function Display EDCU Overtemperature Attitude Display Failure Heading Display Failure mag degr caption ADS Failure Double RAD ALT Failure Single Rad Alt Failure OAT Sensor Failure Display Unit Messages “REV” CAS Warning Message List Discrepancy CAS Caution Message List Discrepancy Display Unit Monitoring “DU MON” Message on PFD Only Display Unit Monitoring “DU MON” on PFD and MFD Display Unit Messages ‘CHECK PFD’ Display Unit Messages “DU OVHT” Magnetic Variation Invalid 2.5 Minute Message for OEI Conditions 5 Minute Message for AEO Conditions Engine State Indication on PFD and MFD NR Miscompare Message AHRS Miscompare ADS Miscompare AHRS Miscompare RAD ALT Miscompare Decision Height Caption Low Height Protection Height Loss Power Limit Power Loss OAT Sensor Miscompare LOC/GS Miscompare LG/vg Miscompare LOSS OF RADIONAV OR FMS LATERAL AND/OR VERTICAL DEVIATIONS Loss of VOR Data Loss of AFCS Communication to PFD FMS Messages on PFD FMS DGR + RNP + MSG RAIM MESSAGE ON PFD RAIM + GNSS RAIM UNAVAILABLE on EDCU RAIM + GNSS WILL EXCEED LIMIT on EDCU (DURING APPROACH) MSG ON PFD + GNSS RAIM ABOVE LIMIT on EDCU DR ON PFD + UNABLE GNSS RNP ON EDCU ROTOR AND TRANSMISSION Rotor Brake Fail Rotor Brake Inhibit Rotor Brake Overheat (On Ground) Main Gearbox Overtorque Main Gearbox Oil Low Transmission Chip Detector Gearbox Chip Sensor Failure Main Gearbox Input Oil Pressure Main Gearbox Input Bearing Temperature Intermediate Gearbox Oil Temperature High Tail Rotor Gearbox Oil Temperature AVSR Fail AVSR Oscillatory Malfunction Gearbox Chip Detect Unit Malfunction Single Engine Procedure Single Engine Descent Checks Single Engine Approach and Landing Single Engine Before Landing Checks Emergency Procedure for Single Engine Failure during Take-Off Single Engine Failure Recognized in Hover (6 ft (1,8 m) ATS) OEI Rejected Take-OFF PROCEDURE OEI Continued Take-Off PROCEDURE Emergency Procedures For single Engine Failure During Landing approach OEI Balked Landing PROCEDURE OEI Landing PROCEDURE |
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