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完成2019年6月13日版本湾流G650ER全套飞行手册翻译任务

时间:2019-08-26 11:52来源:蓝天飞行翻译公司 作者:公务机翻译 点击:


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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