Engine size: 993CC
Diameter and stroke: 90x78
Compression ratio: 10:1
Max Power: 135 HP at 6800 Rpm
Belt reduction: 1:4 Poly-V belt
BN46-42-8002 double-diaphragm carburetor
Electronic ignition with variable advance
Electric starter
Fixed point thrust: 370kg
Two-blade propeller AS25/2, diameter: 2550 mm
Ultralight type – 3-axis and taildragger
Manoeuvring speed: from 40 to 100 km/h
Roll rate: 250 degrees/sec
Take-off / Landing run: 10/20 metres
Load factor: 300kg (+ 6 – 4)
Thrust to weight ratio: 250 kg (1:0.7)
Ballistic parachute