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：次
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Engine Cranking Cycle APU Inflight Operation High Elevation Airport Operations QFE Operations TCAS II Flight Procedures Use Of The Rudder In Flight "Vectors" Approach Transition to Final Use of the Standby Flight Displays High Latitude Navigation Use of Electronic Charts Approved Use of Video Function Use of COMM / NAV 3 Datalink (DLK) Operation ADS-B Out Operation Use of the Preview Mode Engine Start - Battery Power Only Vertical Situation Display (VSD) Recommended Use of Video and Charts Automatic Sensor Reversion Uplink Weather Advanced Graphics Module - AGM Reversion Windshield Surface Seal Protection System Runway Awareness and Advisory System (RAAS) Synthetic Vision-Primary Flight Display (SV-PFD) Fuel Balancing In Flight Polar Navigation Operation at Airports Not In FMS Navigation Database High Altitude Ice Crystal Icing Visual Guidance Procedures Enhanced Vision System (EVS) to 100 Feet Above The Touchdown Zone Elevation Operational Procedures Head-Up Display (HUD) Operational Procedures Enhanced Flight Vision System (EFVS) Landing System to Touchdown and Rollout Operational Procedures Chapter 04 - Messages and Annunciations Procedures List Of Effective Pages Messages and Annunciations Procedures Introduction Methods of Notification Visual Notification Aural Notification Warning Messages and Annunciations Crew Alerting System (CAS) Warning Messages and Procedures Other Warning Annunciations and Procedures Amber Caution Messages and Annunciations Crew Alerting System (CAS) Caution Messages and Procedures Other Caution Annunciations and Procedures Blue Advisory Messages and Annunciations Crew Alerting System (CAS) Advisory Messages and Procedures Other Advisory Annunciations and Procedures Chapter 05 - Expanded Abnormal / Emergency Procedures List Of Effective Pages Expanded Abnormal / Emergency Procedures General Guidance Air Conditioning System Single Air Conditioning Pack Failure Uncontrollable Zone Temperature Cooling Turbine Hot Auto Flight System Autopilot Malfunction Autothrottle Malfunction Autopilot (AP) Failure Auxiliary Power System APU Inflight Operation - Alternate Electrical Power Source APU Operating Envelope APU Generator Failure APU Shutdown - Essential Mode Electrical Power System Dual Generator Failure (Above Altitude FL300) Single Generator / Main AC Bus Power Failure L (or R) ESS DC Bus Failure Operation On Airplane Batteries, EBHA and UPS Batteries Only (RAT Unavailable) Generator Overload Electrical Power System Bus Faults 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 Systems, Circuit Breakers and Locations By Bus Dual Generator Failure (Altitude FL300 or Below) Engine Control System FADEC Alternate Control Mode FADEC Hot Engine Failure 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 Operating Parameters High Oil Temperature Low Oil Pressure Low Fuel Pressure Fuel Tank Temperature Engine Exceedance Engine Vibration Engine Ice Shedding Procedure Abnormal Cowl Anti-Ice Operation Abnormal Wing Anti-Ice Operation Engine Shutdown / Airstart / Single Engine Procedures Engine Shutdown in Flight Normal Airstart - Automatic Manual Airstart - Starter Assist Manual Airstart - Windmilling One (1) Engine Inoperative Landing Procedure One (1) Engine Inoperative Go-Around Procedure Engine Starting System 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 Fire: Engine / APU / Electrical / Aircraft Interior Engine Fire In Flight Engine Fire On Ground Tailpipe Fire APU Fire Airplane Interior Fire / Smoke / Fumes Fire Detection System Engine Fire Warning System Malfunction Flaps System Flaps Failure Zero Flaps Or Partial Flaps Landings Flap Electronic Control Unit (FECU) Failure Flight Controls System Landing Controllability Check Uncommanded Aircraft Motion 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 Left or Right Aileron Failure |
