時(shí)間：2020-06-04 06:06來(lái)源：藍(lán)天飛行翻譯公司 作者：公務(wù)機(jī)翻譯 點(diǎn)擊：次
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Essential DC Bus on Battery Power Engine Control System FADEC Alternate Control Mode Engine Operating Parameters Engine Vibration Ice Shedding Procedure Abnormal Cowl Anti-Ice Operation Abnormal Wing Anti-Ice Operation Engine Starting System Engine Failure to Start Start Valve Failure to Open or Indicate Open on Engine Start Start Valve Failure to Close After Engine Start SAV (Starter Air Valve) Maintenance Message Displayed In Flight Hot Start Flaps System Failure of Flap / Stabilizer Synchronization Flaps Operation With Loss of Normal Hydraulics Zero Flaps Or Partial Flaps Landings Uncommanded Stabilizer Movement Uncommanded Flap Movement Flap Control Unit (FCU) Failure Simultaneous Display of "Uncommanded Flaps" and "Uncommanded Stabilizer" CAS Messages Flight Controls System Flight Controls Considerations Flight Control Runaway To Hardover Position Aileron HOPS Activation Elevator HOPS Activation Rudder HOPS Activation Runaway Pitch Trim Frozen Pitch Trim Frozen Aileron Trim Fuel System Fuel Boost Pump Failure Failure of Two Boost Pumps on One Side Low Fuel State Fuel Return Fail Hydraulic System Left Hydraulic System (L SYS) Failure - Loss of Pressure Only Right Hydraulic System (R SYS) Failure - Loss of Pressure and / or Fluid Landing With The Standby Electrical Power System (HMG) On With Both Hydraulic Systems Operating Landing With The Standby Electrical Power System (HMG) Operating On Single Hydraulic System Indicating / Recording System Display Unit (DU) Failure Operation With An Air Data System (ADS) Failed Traffic and Collision Avoidance System (TCAS) Failure Enhanced Ground Proximity Warning System (EGPWS) Failure Blocked Total Air Temperature (TAT) Probe Modular Avionics Unit (MAU) Failure MAU 1A Failure MAU 1B Failure MAU 2A Failure MAU 2B Failure MAU 3A Failure MAU 3B Failure Enhanced Vision System (EVS) Malfunctions Head-Up Display (HUD) Malfunctions Equipment Loss While In RVSM Airspace Radio Failure / Mistune During A Dual Coupled ILS Approach IRS Align In Motion FMS Powers Up In Single or Independent Mode Loss of All Display Units (DUs) Video Malfunctions Charts Function Failure Charts Function - DU 2 and 3 Inoperative Display Units (DUs) Blanking / Intermittent Synthetic Vision-Primary Flight Display Failure GPS / SBAS Reception Loss During A RNAV (GPS) Approach To LPV Minima Landing Gear Alternate Operation Landing Gear Failure to Retract Unsafe Landing Gear Indication Landing Gear Failure to Extend Landing Gear Retraction Following Alternate Extension Attempted Landing Gear Retraction with Safety Pins Installed Landing Gear System Wheel Brake Failure Due to Hydraulic System Failure Anti-Skid Failure Anti-Skid Off Braking Brake System Overheat Indication Nose Wheel Steering (NWS) Failure Uncommanded Nose Wheel Steering Weight-On-Wheels (WOW) Fails to Shift to GROUND Mode After Touchdown Weight-On-Wheels (WOW) Fails to Shift to AIR Mode After Takeoff Nose Weight-On-Wheels (WOW) Fails to Shift to AIR Mode After Takeoff Landing, Stopping and Evacuation Planned Airplane Evacuation Overheat / Hot Conditions Forward Floor Hot and / or TRU Hot EER Hot / PDB Overheat MAU / MRC Overheat Pressurization Control System Loss of Automatic Pressurization Control Bleed Air System (BAS) Failure Bleed Air Hot Bleed Pressure High Bleed Pressure Low Unpressurized Flight Inadvertent Passenger Oxygen Mask Activation Thrust Reverser System Thrust Reverser Manual Stow Procedure Dispatch With Inoperative Thrust Reverser(s) On Wet Runways Windshield / Door System Windshield Heat Failure Windshield Cracked |
