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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Thrust Reverser Failure Thrust Reverser Manual Stow Procedure Dispatch With Inoperative Thrust Reverser(s) On Wet Runways Engine Vibration Ice Shedding Procedure Volcanic Ash Encounter 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 FADEC Alternate Control Mode EC: Fire / Overheat / Smoke Fire Extinguishing System Diagram Engine Fire In Flight Engine Fire On Ground Tailpipe Fire APU Fire Airplane Interior Fire / Smoke / Fumes Engine Fire Warning System Malfunction Engine Hot Pylon Hot Aft Equipment Hot Aft Floor Hot Forward Floor Hot and / or TRU Hot EER Hot / PDB Overheat MAU / MRC Overheat ED: Flight Controls / Autoflight Flight Controls System Diagram Jammed Ailerons Jammed Elevator Jammed Rudder Jammed Stabilizer Jammed Spoilers Inadvertent Powered Disconnect Lever Activation (SN 5001 thru 5389 without ASC 099) Stall Barrier Malfunction Ground Spoiler Failure Inflight Ground Spoiler Failure On Landing Runaway Pitch Trim Frozen Pitch Trim Frozen Aileron Trim Flight Control Runaway To Hardover Position Aileron HOPS Activation Elevator HOPS Activation Rudder HOPS Activation 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 Autopilot Malfunction Autothrottle Malfunction Autopilot (AP) Failure Mach Trim Failure Yaw Damper Failure EE: Fuel / Hydraulics Hydraulic System Diagram Fuel System Diagram Dual Hydraulic System (L SYS and R SYS) Failure - AUX Pump Available Dual Hydraulic System (L SYS and R SYS) Failure - AUX Pump Unavailable Left Hydraulic System (L SYS) Failure - Loss of Pressure and Fluid 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 Master Table of Hydraulic Component Availability Fuel Tank Temperature Fuel Leak In Flight Fuel Boost Pump Failure Failure of Two Boost Pumps on One Side Low Fuel State Fuel Return Fail Maximum Fuel Imbalance EF: Instruments / Avionics Primary Flight Display (PFD) Malfunction Suspected Erroneous / Unreliable Airspeed Indications Display Units (DUs) Blanking / Intermittent Display Unit (DU) Failure Loss of All Display Units (DUs) 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 Modular Avionics Unit (MAU) Function / Failure Matrix 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 Video Malfunctions Charts Function Failure Charts Function - DU 2 and 3 Inoperative Synthetic Vision-Primary Flight Display Failure GPS / SBAS Reception Loss During A RNAV (GPS) Approach To LPV Minima EG: Landing Gear / Brakes / Steering Landing Gear / Brakes / Steering System Diagram |
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