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E-Jet Series
E-Jet Series
  • Introduction
    • Welcome
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  • Normal Procedures
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  • Systems Guide
    • Overhead Panel
      • ELECTRICAL - AC
      • ELECTRICAL - DC
      • COCKPIT LIGHTS
      • ENGINE FIRE HANDLE
      • FUEL
      • PASSENGER SIGNS
      • FIRE EXTINGUISHER
      • APU CONTROL
      • WINDSHIELD WIPER
      • EXTERNAL LIGHTS
      • HYDRAULIC
      • PRESSURIZATION
      • ICE PROTECTION
      • AIR COND / PNEUMATIC
      • PASSENGER OXYGEN
      • GND PROX TERR INHIB AND EMERG/PRKG BRAKE
    • Main Panel
      • Primary Flight Display (PFD)
        • SPEEDS
        • FLIGHT MODE ANNUNCIATORS (FMA)
        • ALTITUDES
        • MARKER BEACONS
        • FLIGHT PATH / ATTITUDE INDICATIONS
        • HORIZONTAL SITUATION INDICATOR (HSI)
        • LATERAL/VERTICAL DEVIATION INDICATION
        • VERTICAL NAVIGATION (VNAV)
        • WIND DISPLAY / TIMER
        • FMS MODE ANNUNCIATORS
        • COM / NAV
        • DISPLAYS
      • Multifunction Display (MFD)
        • GENERAL
        • SYSTEMS/STATUS
        • SYSTEMS/ANTI ICE
        • SYSTEMS/ECS
        • SYSTEMS/ELEC
        • SYSTEMS/FLTCTRL
        • SYSTEMS/FUEL
        • SYSTEMS/HYDR
        • TCAS
        • WEATHER
      • EICAS
        • THRUST
        • FUEL / OIL
        • SLATS / FLAPS / SPEEDBRAKE
        • CREW ALERTING SYSTEM (CAS)
        • GEAR / BRAKE
        • APU
        • CABIN ALT / LFE
        • TRIM
      • Reversionary Panel
      • Integrated Electronic Standby System (IESS)
      • Autobrake
      • Gnd Prox Terr Inhib and EMERG/PRKG Brake
      • Clock
      • Landing Gear
      • ELT and GND PROX G/S INHIB
      • LG WRN INHIB and ADS Probes Heater
    • Central Pedestal
      • Multifunction Control Display Unit (MCDU)
      • FLIGHT CONTROL MODE
      • STALL WARNING
      • POWERPLANT
      • T/O CONFIG and EICAS FULL
      • Cursor Control Device (CCD)
      • SPEEDBRAKE / SPOILERS
      • THRUST LEVER QUADRANT
      • Ram Air Turbine (RAT)
      • GND PROX FLAP OVRD and SLAT/FLAP LEVER
      • AUDIO CONTROL
      • TRIM
      • COCKPIT DOOR CONTROL
      • EMERGENCY/PARKING BRAKE / PA
      • ELEVATOR / AILERON DISCONNECT
      • CONTROL WHEEL
    • Cockpit Floor
    • Cockpit Side
    • Head-Up Display
  • Autopilot Guide
    • Flight Director (FD)
    • Autopilot (AP)
    • Yaw Damper (YD)
    • AFCS Indications on PFD
    • FGCS Lateral Modes
    • FGCS Vertical Modes
    • Steep Approach Mode
    • Speed Control
  • MCDU Guide
    • TRS - Thrust Rating System
  • ⭐Special Features
    • Cabin Announcements
    • GSX Automation
  • 📂Supplements
    • GSX Profiles
    • SimBrief Profiles
    • Hardware Integration
    • PaintKit
    • Landing Distance Calculator
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On this page
  • AIRPLANE GRAPHIC
  • SURFACE POSITION STATUS
  • FLIGHT CONTROL SYSTEM STATUS ANNUNCIATIONS
  • ACTUATOR STATUS ANNUNCIATION
  • AXES MODE ANNUNCIATION
  • HYDRAULIC SYSTEM SOURCE ANNUNCIATION
  • PBIT REMAINING TIME READOUT
  1. Systems Guide
  2. Main Panel
  3. Multifunction Display (MFD)

SYSTEMS/FLTCTRL

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Last updated 1 year ago

Ein Bild, das Text, Monitor, drinnen, Screenshot enthält. Automatisch generierte Beschreibung

AIRPLANE GRAPHIC

  • Static display that shows the location of flight control surfaces and status of the flight control actuators.

SURFACE POSITION STATUS

  • Displays the surface position and status.

FLIGHT CONTROL SYSTEM STATUS ANNUNCIATIONS

  • Status annunciations are shown in a table format for three surfaces.

ACTUATOR STATUS ANNUNCIATION

  • The rudder has two actuators, upper and lower. Each left and right elevator surfaces have two actuators, inboard and outboard.

AXES MODE ANNUNCIATION

  • Axes mode annunciations are shown for the rudder, left and right elevator.

HYDRAULIC SYSTEM SOURCE ANNUNCIATION

  • Hydraulic system source annunciations are shown for the rudder, left and right elevator.

PBIT REMAINING TIME READOUT

To skip Power Build In Test you can disable the realistic startup option in the EFB options -> Aircraft page

  • Digital remaining time readout displays the hours until the electrical and hydraulic PBIT expire.

  • Electrical PBIT is automatically performed during power up after the airplane is powered by any AC source and takes approximately 3 minutes to complete.

    • Will be interrupted if any electric hydraulic pump is turned ON, if the Flight Control Mode Buttons are cycled or if AC power is interrupted while the test is running.

  • Hydraulic PBIT is performed automatically only on the ground when all 3 hydraulic systems are pressurized and takes approximately 1 minute to complete.

    • Will be interrupted if any flight control surface is moved.

    • PBIT is not performed if the temperature within the hydraulic reservoir is lower than 10 degrees Celsius.