時(shí)間：2019-08-26 11:52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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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 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 Rudder Single Actuator Failure Spoiler Panel Failure 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 Anti-Skid Failure Brake System Overheat Indication Uncommanded Applied Brake Pressure - Inflight Nose Wheel Steering (NWS) Steer By Wire Failure Nose Wheel Steering (NWS) Tiller Steering Failure Nose Wheel Steering (NWS) Rudder (Pedal) Steering Failure Uncommanded Nose Wheel Steering Nose Wheel Steering (NWS) Fixed Gain Weight-On-Wheels (WOW) Fails to Shift to GROUND Mode After Touchdown Weight-On-Wheels (WOW) Fails to Shift to AIR Mode After Takeoff EH: Pneumatics / ECS ECS Synoptic Page Loss of Pressurization Emergency Descent Procedure Automatic Emergency Descent Mode (EDM) Loss of Automatic Pressurization Control Bleed Air System (BAS) Failure Bleed Air Hot Bleed Pressure High Bleed Pressure Low Abnormal Wing Anti-Ice Operation Unpressurized Flight Single Air Conditioning Pack Failure Uncontrollable Zone Temperature Cooling Turbine Hot Abnormal Cowl Anti-Ice Operation Inadvertent Passenger Oxygen Mask Activation EI: Miscellaneous Overweight Landing Ditching Emergency Escape Routes Immediate Return For Landing Rejected Takeoff Main Entrance Door Not Secure Windshield Heat or Windshield Failure Planned Airplane Evacuation Cabin Window Cracked External Baggage Door Not Secure Maximum Vertical Acceleration Reporting System S: SUPPLEMENTAL PROCEDURES / DATA Heavy Rain / Hail Encounter Turbulence Penetration / Severe Gust Encounter Lightning Strike Windshear / Microbursts Crosswind Approach and Landing |
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