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承接2020年3月14日版本湾流G650快速检查单翻译任务

时间:2020-04-15 10:09来源:蓝天飞行翻译公司 作者:公务机翻译 点击:


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
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