The JIN-250SA engine is a two-stroke horizontally opposed twin-cylinder, water-cooled aircraft engine. The engine displacement is 248cc and the maximum power is 21hp.

Features:

1.Water cooling;

2.Integral cylinder crankcase;

3.Cylinder and cylinder block ceramic plating technology, forged crankshaft, high-strength piston

4.DC automatic timing CDI ignition system;

5.Built-in electric starter, one-button starting.

6.The JIN-250SA engine can be adapted to different types of propellers from 32 to 36 inches.

Parameter:

Engine type: two-stroke twin cylinder

Speed range: 1500-7000rpm

Cooling type: natural air cooling

Rotation direction: clockwise facing the propeller

Weight: 12.5kg

Generator: 14V 300W

Size: 210mm * 330mm * 160mm(L*W*H)

Maximum power: 15.5kw/7500rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 29*20, 30*18, 32*16