The TTx’s Electronic Stability and Protection System (ESP) enhances safety like never before. This electronic monitoring and exceedance-correcting technology is integrated into the Intrinzic？ flight deck and assists in maintaining the aircraft in a safe, flight-stable condition. The ESP helps in certain situations to prevent the onset of loss-of-control conditions like stalls, spins, or steep spirals. This technology is invaluable if the worst happens — the pilot becomes compromised or incapacitated during flight.

• Equipment Details
• Intrinzic Cockpit powered by Garmin
• GMA-36 Remote Digital Audio Panel w/Marker Beacon/Intercom
• GTC-570 Touch Screen Controller
• GTX-33ES Transponder-Mode S, w-Traffic Information System capability
• GIA-63W NAV/COM/GPS/WAAS w/GS #1
• GIA-63W NAV/COM/GPS/WAAS w/GS #2
• GDU-1400 Primary Flight Display (PFD)
• GDU-1400 Multifunction Display (MFD)
• GEA-71 Engine/Airframe Computer
• GRS-77 AHRS (dual)
• GDC-74A Air Data Computer w/OAT Probe
• GMU-44 Magnetometer (dual)
• GDL-69A Flight Information System (FIS) w/XM Radio
• GCU-275 Primary Flight Display (PFD) Controller
• Terrain Awareness System (TAWS-B)
• Electronic Checklist
• GFC-700 Autopilot
• Go-Around Switch
• Electric Trim
• A/P Disconnect
• Control Wheel Steering Button
• GMC-720 Auto Flight Controller System (AFCS)
• Garmin SafeTaxi & FliteCharts (FliteCharts do not provide geosynchronous positioning)
• GTS-800 Traffic Advisory System
• ESI-1000 L-3 Trilogy (Backup Airspeed, Altimeter, and Attitude)
• Control Stick Push-To-Talk Switch-Pilot/Copilot
• Mic & Phone Jacks — Pilot/Copilot/Passengers (Bose and Standard)
• Antennas:
• Marker Beacon Antenna
• Transponder Antenna
• WAAS/COMM Antenna (1) ？ GPS/XM Antenna (1)
• COMM Antenna (1)
• NAV Antenna
• TAS Omni (1)
• TAS Directional (1)
• Artex ELT-ME406 Emergency Locator Transmitter
• Pitot System – Heated
• Alternate Static Source
• CO Detector/Pulse Oximeter
• Synthetic Vision Technology (SVT)
• Electronic Stability and Protection (ESP) Garmin - Electronic monitoring and exceedance-correcting system
• Standard flight controls:
• Dual hydraulic brakes, toe-operated
• Parking brake
• Dual flight controls — aileron/elevator/rudder speedbrake
• Speedbrakes
• Pilot and copilot control stick
• Pitch trim
• AP disconnect
• Control-stick steering button