時(shí)間：2020-04-15 10:09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
|
Dual Generator Failure (Above Altitude FL300) Dual Generator Failure (Altitude FL300 or Below) Operation On Airplane Batteries, EBHA and UPS Batteries Only (RAT Unavailable) Single Generator / Main AC Bus Power Failure L (or R) ESS DC Bus Failure Generator Overload Left Main AC Bus Fault Right Main AC Bus Fault Emergency AC Bus Fault Electrical Power System RESET Messages Displayed Battery or Battery Charger Failure Essential DC Bus on Battery Power APU Inflight Operation - Alternate Electrical Power Source APU Generator Failure APU Shutdown - Essential Mode APU Operating Envelope EB: Engines Engine Failure Considerations Engine Failure Below V1 Engine Failure Above V1 Dual Engine Flameout Inadvertent Engine (One Or Both) Shut Down Dual Engine Failure - Mid Altitude Dual Engine Out Landing Procedure Engine Shutdown in Flight Engine Out Driftdown Charts Normal Airstart - Automatic Manual Airstart - Starter Assist Manual Airstart - Windmilling One (1) Engine Inoperative Landing Procedure One (1) Engine Inoperative Go-Around Procedure Engine Exceedance High Oil Temperature Low Oil Pressure Low Fuel Pressure Thrust Reverser Unlock or Deploy During Takeoff Thrust Reverser Unlock or Deploy During Flight Thrust Reverser Failure Thrust Reverser Manual Stow Procedure Engine Failure to Start Engine Vibration Engine Ice Shedding Procedure Volcanic Ash Encounter 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 FADEC Hot 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 Control Mode Comparison Jammed Aileron Jammed Elevator Jammed Rudder Jammed Spoiler(s) Ground Spoiler Failure in Flight Ground Spoiler Failure On Landing Landing Controllability Check Uncommanded Aircraft Motion Roll Trim Motor Failure Runaway Pitch Trim Runaway Roll Trim Runaway Rudder Trim Flight Control System (FCS) Normal Mode Transition Failure Flight Control Surface Electric Backup Hydraulic Actuator (EBHA) in Electrical Backup (EB) Mode Flight Control Computer (FCC) Multiple (Two or Three) Channels Fail Left or Right Aileron Failure (Airplanes Not Equipped with ASC 135) Left or Right Aileron Failure (Airplanes Equipped with ASC 135) Aileron Single Actuator Failure Backup Flight Control Unit (BFCU) Active Left or Right Elevator Failure Elevator Single Actuator Failure Flight Control Computer (FCC) Alternate Mode Flight Control Computer (FCC) Direct Mode Jammed Flight Control Column Jammed Flight Control Wheel Jammed Flight Control Pedals Rudder Failure (Airplanes Not Equipped with ASC 134) Rudder Failure (Airplanes Equipped with Both ASC 134 and ASC 135) Rudder Failure (Airplanes Equipped with ASC 134, but Not Equipped with ASC 135) Rudder Single Actuator Failure Spoiler Panel Failure (Airplanes Not Equipped with ASC 135) Spoiler Panel Failure (Airplanes Equipped with ASC 135) Stabilizer Failure Flaps Failure Zero Flaps Or Partial Flaps Landings Flap Electronic Control Unit (FECU) Failure Autopilot Malfunction Autothrottle Malfunction Autopilot (AP) Failure EE: Fuel / Hydraulics Hydraulic Synoptic Page Fuel System Diagram Dual Hydraulic System (L SYS and R SYS) Failure Left Hydraulic System (L SYS) Failure - Loss of Pressure and Fluid Right Hydraulic System (R SYS) Failure - Loss of Pressure and/or Fluid Left Hydraulic System (L SYS) Failure - Loss of Pressure Only 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 One or More Air Data System(s) (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 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 SATCOM / AIRCELL Inoperative Following Electrical Power Application Triple FMS Failure / Reset EG: Landing Gear / Brakes / Steering Landing Gear / Brakes / Steering System Diagram Landing Gear Failure to Retract Unsafe Landing Gear Indication Landing Gear Failure to Extend Attempted Landing Gear Retraction with Safety Pins Installed Nose Gear Retracted, Both Main Gear Down and Locked One Main Gear and Nose Gear Down and Locked, Opposite Main Gear Retracted One Main Gear Only Down and Locked Both Main Gear Retracted, Nose Gear Down and Locked All Gear Up Landing Procedure Landing Gear Retraction Following Alternate Extension Braking Using the PARKING BRAKE Inboard / Outboard Wheel Brake Failure Due to Hydraulic System Failure |
