N919ES | Cockpit

Please note: All documentation linked to on this website is being superseded by documentation and instruction provided at the FBO.

  • Highlights

    • TAA (Technically Advanced Airplane) due to available PFD/MFD/AP equipment as per FAR §61.129(j)
    • FADEC (Full-Authority Digital Engine Controls)
    • Auxiliary Fuel Tanks* for 50% more range on long XC flights
      • * Not normally in use. Use requires familiarity with corresponding limitations and procedures. Tank keys available upon specific request only. 
    • TKS Ice Protection System for FIKI (flight into known icing)
    • G1000 (Non-WAAS)
      • IFR charts (US/Canada)
      • Synthetic Vision Technology (SVT)
      • Baro Minimums altimeter bug for DA/MDA
      • Customizable Flight ID for Public Benefit Flying purposes
    • ADS-B
      • Out (1090ES) for automated WAAS GPS position transmission
      • In (Dual band: 1090ES / 978UAT) for receiving
        • TIS-B: Traffic and
        • FIS-B*: WX (Nexrad, Winds Aloft, METARs, TAFs, AIRMETs, SIGMETs, PIREPs), NOTAMs, TFRs, SUAs
        • Bluetooth streaming of TIS-B, FIS-B and AHRS to your EFB
    • KAP 140 Autopilot with Altitude Preselect
    • USB chargers (two on the pilot side, two on the co-pilot side), strong enough to charge EFBs or other devices
    • Sun visors


Synthetic Vision

Synthetic Vision example on G1000 PFD

The ADS-B In stream of FIS-B/TIS-B via Bluetooth is available after turning on the Avionics Master; look for the N919ES Bluetooth network and connect to it from your EFB.


– Use of polarized eyewear may cause glass cockpit displays to appear dim or blank – using non-polarized sunglasses is recommended

– Do not remove any of the SD cards from the devices, these cards are critical for proper operation and to be serviced by authorized personnel only!

Pilot’s Guide | Cockpit Reference Guide

AFM SupplementPilot’s Guide

  • TKS Ice Protection

AFM Supplement

  • Other
    • smartPower 250 Dual 2.7A backlit USB power supplies are available in the upper area of each of the front seat side panels:
      Pilot: USB power near the alternate static valve | Co-pilot: USB power near the two FADEC diagnostic cables


      Note: The USB ports are only active when the avionics master is on (the engines should normally be running at that point)

  • Emergency Locator Transmitter
    • The ELT in this aircraft is an ARTEX C406-1.
      It is installed in the empennage behind the back seats on the pilot side.
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