AIRFRAME
Carbon fiber wing assembly with integral tank
Carbon composite empennage structure
Fuselage assembly, 1.7734 steel
Steerable, lightweight tailwheel
Fiberglass landing gear spring
Single-seat bubble canopy
Carbon pushrods
Titanium firewall
POWERPLANT AND PROPELLER
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
COCKPIT
Manually adj. rudder pedals with differential toebrakes
Contour molded composite seat, adjustable
Hooker safety harness with ratchet
2 bezel-operated air vents
SYSTEMS
Smoke system, with automatic filling system
Pitot static system drain
Trickle charger socket
8 Amp alternator
12V battery
STANDARD PANEL EQUIPMENT
Airspeed indicator (kts)
Altimeter (ft, inHg/hPa)
Mechanical accelerometer
Magnetic compass
Slip and skid indicator, with holder if req'd
Aresti card holder
Digital RPM indicator
MAP/FF indicator
Fuel gauges
CHT/EGT, oil press./oil temp. gauges