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| AIRFRAME |
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- Fuselage assembly, 1.7734,4 steel
- carbon fiber wing assembly with integral tank
- carbon / glass hybrid composite empennage structure
- fiberglass landing gear spring
- choice of steerable, lightweight tailwheel or soft tailwheel
- two-seat bubble canopy
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| POWERPLANT AND PROPELLER |
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- Lycoming AEIO-580-B1A, 315 hp 6 cylinders engine
- Gomolzig, 6-in-1 exhaust system
- single oil cooler system
- Muehlbauer, MTV 9-B-C/C198-25, 3-blade propeller
- electric starter
- two fuel pumps (1 engine-driven, 1 electric)
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| COCKPIT |
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- Fixed composite front seat, contour molded
- adjustable composite rear seat, contour molded
- forward rudder pedals with differential toe brakes
- electrically adj. rear rudder pedals with differential toe brakes
- front and rear seat hooker safety harness with ratchet
- 2 front and 2 rear bezel-operated air vent
- moulded control stick handle
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| SYSTEMS |
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- Electric stall warning system
- pitot static system drain
- 65 amp alternator
- 12V battery
- LED nav lights
- cowling light, strobe lights
- electric trim system
- smoke system (optional)
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| AVIONICS |
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| STANDARD PANEL EQUIPMENT |
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- Airspeed indicator (kts)
- altimeter (ft, inHg/hPa)
- mechanical accelerometer
- magnetic compass
- ASPEN PFD
- ASPEN MFD
- GARMIN GNS 430W
- XPDR GARMIN GTX 328 mode S
- EI MVP-50P engine monitor
- intercom syst. NAT AA83
- ARTEX 406MHz ELT (optional)
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