• Accelerated engineering

    The pilot of the Cessna Grand Caravan EX turboprop will love its state-of-the-art command center powered by the all-glass Garmin G1000 avionics suite. With technology adapted specifically for Cessna, available synthetic vision technology (SVT) integrates all primary flight, engine, and sensor data. This intuitive, at-a-glance control panel that is featured in the Cessna Caravan, optimizes situational awareness for pilots, greatly enhancing safety.

  • Situational awareness

    The Cessna Grand Caravan EX’s uncluttered displays include two primary flight displays (PFD) and a center multifunction display (MFD) unit offering real-time, flight-critical data aggregated on three configurable, large-format high-resolution screens. Crew alerts are displayed on the PFD.

  • IFR flight plans with SVT

    Cessna Grand Caravan- Synthetic Vision Technology SVTPilots have the ability to load IFR flight plans on the G1000 to exactly match the intended route. Magenta rectangular pathways provide a visual window to help pilots follow the intended flight route. Pathways are spaced no more than 1,000 meters apart and have guidelines in each corner that point in the direction of the active flight plan leg.

    Using Synthetic Vision Technology (SVTTM), Garmin’s Towers and Obstacles database makes the existence of non-terrain structural hazards crystal clear, even in low-visibility conditions.

Standard avionics include

  • GDU 1040A Pilot and Copilot Primary Flight Display (PFD)
  • GDU 1040A Multifunction Display (MFD)
  • GDC 74A Dual Air Data Computer (ADC)
  • GEA 71 Engine/Airframe Unit
  • GRS 77 Dual Attitude and Heading Reference System (AHRS)
  • GMA 1347 Single Audio System with Integrated Marker Beacon Receiver
  • GTX 33 Mode S Transponder
  • Garmin Relative Terrain/Obstacles
  • Garmin Flight Charts Capable
  • Garmin Safe Taxi Capable
  • KN-63 DME
  • Switch, Avionics Power (Two) (On-Off)
  • Artex ME-406 2-Frequency (Non-Nav Interfaced)
  • ELT with Remote Switch and Monitor Light (Dorsal Fin Installation)
  • Avionics Cooling, (2) Cowl Deck Fans and (3) Display Fans
  • PA System with Aft Cabin Speakers

ENGINE INDICATION SYSTEM (EIS) Displayed on MFD During Normal Operations:

  • Engine and System Displays
    • Torque
    • Interstage Turbine Temperature
    • Gas Generator Speed
    • Propeller Speed
    • Oil Pressure
    • Oil Temperature
    • Fuel Quantity
    • Fuel Flow
    • Ammeter/Voltmeter
    • Standby Engine Torque Gauge
    • FAST ™ System Engine Trend Monitoring

Standard Flight Instruments:

  • Indications Displayed on Each PFD
    • Airspeed
    • Attitude with Slip/Skid Indication
    • Altitude
    • Vertical Deviation, Glideslope and Glidepath Vertical Speed
    • Horizontal Situation Indication
    • Outside Air Temperature
    • System Time
    • Generic Timer
    • Wind Data
  • Standby Flight Instruments:
    • Airspeed Indicator
    • Attitude Gyro
    • Altimeter
  • Magnetic Compass
  • Heated Pitot System, Pilot & Copilot Alternate Static Source
  • Static Source Drains
  • Instrument Static System
  • Second Independent Pitot-Static System

Standard Flight Controls:

  • Brake, Parking
  • Brakes, Hydraulic, Toe-Operated
  • Control Cables — Corrosion Resistant Steel
  • Control Lock, Ailerons and Elevator
  • Flight Control System, Pilot & Copilot (Includes All-Purpose Control Wheel, Pedals and Toe Brakes)
  • Friction Lock, Engine Controls
  • Powerplant, Quadrant Type Controls:
    • Condition Lever
    • Primary Engine Power
    • Back-Up Engine Power, (Emergency Power Lever)
  • Propeller, Speed and Feather
  • Rudder Gust Lock
  • Trim System (Aileron/Rudder [Manual], Elevator [Manual & Electric Pilot & Copilot])
  • Wing Flaps, Electric Pre-Select with Standby Motor
  • Environmental Controls:
    • Defroster, Windshield (Pilot and Copilot)
    • Heating System, Cabin (Bleed Air Type)
    • Soundproofing
    • Ventilation System, Cockpit (Ram Air)
    • Ventilator, Adjustable, Cabin Air
    • Ventilation System, Fan-Driven