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DA42 TwinStar Standard Aircraft (with Garmin G1000 glass panel cockpit) |
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2X Thielert TAE 2.0 Centurion turbo diesel engines |
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2X MT 3-blade constant speed full-feathering propeller |
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FADEC digital engine and propeller management system |
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Garmin GDU1040, 10 inch primary flight display (PFD) |
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Garmin GDU1040, 10 inch multi function display (MFD) |
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Garmin GEA 71 Airframe/Engine Interface Unit |
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2X Garmin GIA 63 COM/NAV/GPS |
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Garmin GMA 1347 Digital Audio System |
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Garmin GTX 33 Mode S Transponder |
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Garmin GRS77 Altitude Heading Reference System |
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Garmin GDC 74 Digital Air Data Computer |
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Garmin GMU 44 Magnetometer |
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Artex ME 406 Mhz ELT |
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Honeywell KAP 140 Dual Axis Autopilot with Altitude Hold and Preselect |
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Standby instruments (Compass, Horizon, Air Speed Indicator, Altimeter) |
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Composite cabin and safety seats (up to 26g) |
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Lightning protection system |
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Fire extinguisher |
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FAILSAFETM Airframe Design |
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3 point safety belts automatic (all seats) |
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Instrument lighting |
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Overhead cabin lights |
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Standard interior (fabric seats with leather trim) |
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Hydraulic retractable landing gear |
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Heated pitot / static tube |
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Alternate static port |
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Electric operated flap system |
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High intensity discharge landing and taxi lights |
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Position and anti-collision lights |
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52 US gal fuel tank |
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4-way baggage compartment system |
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Nose baggage compartment accessible from both sides |
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Pitot cover |
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Rudder lock |
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Tow bar |
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Tool kit |