Appears to be low-time with Mags, Harness and shipping cradle.
Internal boroscope photos are available. Buyers are encouraged to inspect the engine to ascertain its suitability for their use.
General characteristics (Details from Janes All The Worlds Aircraft)
Type: inverted V-8, air-cooled, 90° piston engine
Bore: 120 mm (4.724 in)
Stroke: 140 mm (5.512 in)
Displacement: 12.667 l (772.99 cu in)
Length: 1,105 mm (43.50 in)
Width: 880 mm (34.65 in)
Height: 936 mm (36.85 in)
Dry weight: 213 kg (470 lb) dry
Valvetrain: Two valves per cylinder.
Fuel system: Two Sun carburetors adapted for aerobatics
Fuel type: 80 octane
Oil system: Dry sump, one pressure pump and two scavenge pumps
Cooling system: Air
Power output: 240 PS (176.52 kW) at 2,000 rpm (5-min. takeoff power)
Specific power: 14.8 kW/L (0.31 hp/in³)
Compression ratio: 5.9:1
Specific fuel consumption: 235 gr/(hp*h); 0.518 lb/(hp*h)
Oil consumption: 0.010 kg/kW/hr (0.0176 lb/hp/hr)
Power-to-weight ratio: 0.835 kW/kg (0.51 hp/lb)