时间：2018-09-01 17:02来源：蓝天飞行翻译公司 作者：公务机翻译 点击：次
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Description EICAS Messages CTOC-CTOC10_300FCOM2 - Flight Controls - Table of Contents SFM10-01 Section 10-01 - Primary Flight Controls Introduction Description Primary Flight Controls Components and Operation Ailerons Roll Spoilers Rudder Yaw Damper Elevators Pitch Disconnect Elevator Control Schematic SFM10-02 Section 10-02 - Secondary Flight Controls Secondary Flight Controls Description Components and Operation Aileron Trim Rudder Trim Horizontal Stabilizer Trim Configuration Trim Mach Trim Aileron Trim Schematic Horizontal Stabilizer Trim Schematic Flaps Components and Operation Flap Alerting Flap Control Lever Flap Position Indication Spoiler System Components and Operation Spoiler Electronic Control Unit (SECU) Flight Spoilers Lever Roll Spoilers Roll Spoilers Disconnect Flight Spoiler Schematic Ground Spoilers Description Components and Operation Takeoff Configuration Warning System Description Components and Operation Proximity Sensing System Description Components and Operation Proximity Sensing Electronic Unit Stall Protection System Description Components and Operation Stick Pusher Disconnect Features Controls and Indications Flaps Control Lever EICAS Trim Status Display Flight Controls Synoptic Page EICAS Messages CTOC-CTOC11_300FCOM2 - Flight Instruments - Table of Contents SFM11-01 Section 11-01 - Flight Instruments Introduction EFIS Display (Typical) Flight Instruments Block Diagram Primary Flight Displays Description Components and Operations Power Supply Angle of Attack (AOA) Display Attitude Display Indicator Wall to Wall Attitude Display Indicator Flight Path Vector (FPV) Symbol Aircraft Symbol Horizon Line Sky/Ground Display Pitch Tape and Chevrons Roll Scale and Pointer ADI Slip / Skid Indicator Vertical Deviation Display Glideslope Flag De-clutter Example of De-cluttered EADI in Excessive Roll Example of De-cluttered EADI in Excessive Pitch Altitude Altitude Display Vertical Navigation Vertical Speed Field Radio Altitude Display Radio Altitude Flag Radio Altitude Comparator Flag RA MIN BARO MIN Air Data Flags Synthetic Vision System (SVS) (If installed) Description SVS Displayed on PFD Components and Operation Synthetic Vision Computer (SVC) Synthetic Vision Configuration Module (SVCM) Video Interface Unit (VIU) Power Supply FSU/SVC Data Load Switch SVS Data Bases SVS Terrain Color Bands SVS Field of View SVS Airports/Runways SVS Parked Sky/Ground SVS System and Fault Indications SVS Annunciators Air Data System Description Components and Operations Power Supply Airspeed Display References Speeds Low/Overspeed/Flap Speed Cues Low Speed Cue (LSC) Trend Vector Altimeter Barometer Knob Air Data Reversion Switch Air Data Computers Pitot Static System Total Air Temperature Probe Pitot Static Schematic Inertial Reference System (IRS) System Description Components and Operation Inertial Reference Unit (IRU) Power Supply Aircraft Personality Module (APM) IRU Strapping ATT / HDG Reversion Switch Ground Alignment In-Flight Alignment EFIS True / Magnetic Heading Operation IRS Indications EICAS Messages PFD Comparators, Flags and Annunciations |
