Description of the engines:
Lycoming AEIO-580-B1A, 315 hp, 6 cylinder engine
Muehlbauer, MTV 9-B-C/C198-25, 3-blade propeller
Two fuel pumps (1 engine-driven, 1 electric)
Gomolzig, 6-in-1 exhaust system
Single oil cooler system
Electric starter
Avionics:
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)
Equipment:
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)
Exterior:
Fuselage assembly, 1.7734 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
Interior:
Fixed composite front seat, contour molded
Adjustable composite rear seat, contour molded
Forward rudder pedals with differential toebrakes
Front and rear seat Hooker safety harness with ratchet
2 front and 2 rear bezel-operated air vents
Moulded control stick handle
