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E-Jet Series
OverviewE-Jet SeriesBoeing 727Tecnam P2006T MKIITecnam P2006T AnalogTecnam P2012SeaRey Elite
E-Jet Series
OverviewE-Jet SeriesBoeing 727Tecnam P2006T MKIITecnam P2006T AnalogTecnam P2012SeaRey Elite
  • Introduction
    • Welcome
    • First Steps
    • FAQs
    • How To Update
  • Normal Procedures
    • Checklist
    • Limitations
    • Approach Types
    • Procedure Guide
  • 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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  • ADI LATERAL DEVIATION
  • VERTICAL DEVIATION SCALE AND POINTER
  1. Systems Guide
  2. Main Panel
  3. Primary Flight Display (PFD)

LATERAL/VERTICAL DEVIATION INDICATION

PreviousHORIZONTAL SITUATION INDICATOR (HSI)NextVERTICAL NAVIGATION (VNAV)

Last updated 1 year ago

ADI LATERAL DEVIATION

  • Magenta diamond for FMS deviation. Green trapezoid pointer used for LOC.

  • When both are displayed during PREV mode the FMS pointer overwrites the LOC pointer when both are at the same point. In PREV mode the trapezoid is displayed in cyan.

  • When a valid deviation is not available a X is depicted.

VERTICAL DEVIATION SCALE AND POINTER

  • Pointer is controlled by the selected primary navigation source (PNS).

  • Vertical deviation scale is displayed when:

    • Localizer (LOC) is selected as the PNS.

    • FMS is selected as the PNS, and the FMS commands the VNAV vertical scale in view.

  • ILS LOC deviation pointer is a green trapezoid. VNAV FMS is a magenta hollow diamond.

  • When glideslope data is invalid or when the vertical deviation scale is commanded into view by the FMS and a valid deviation is not available a X is depicted.

  • Preview vertical deviation is displayed when LOC is the PREV source.

  • LOC and FMS deviation are displayed the same way as the lateral deviation.