Jabiru 3300
From Wikipedia, the free encyclopedia
The Jabiru 3300 is a lightweight four-stroke, horizontally-opposed aircooled engine, used in aircraft. The engine is direct drive and is fitted with alternators, silencers, vacuum pump drives and dual ignition systems as standard.
[edit] Specifications
General characteristics
- Type: Flat-6
- Bore: 97.5 mm (3.84 in)
- Stroke: 74 mm (2.91 in)
- Displacement: 3300 cm³ (201.4 in³)
- Length: 671 mm (26.42 in)
- Width: 582 mm (22.91 in)
- Height: 445 mm (17.54 in)
- Dry weight: 81 kg (178 lbs) with exhaust, carburetors, starter motor, alternator & ignition system
Components
- Fuel system: Mechanical fuel pump
- Fuel type: AVGAS 100/130
- Oil system: Wet sump
- Cooling system: Aircooled
Performance
- Power output: 79.8 kW (107 hp) @ 2750 RPM (continuous); 89.5 kW (120 hp) @ 3300 RPM (intermittent)
- Specific power:
- Compression ratio: 8:1
- Fuel consumption: 26 liters/h @ 2750 RPM (75% power)
- Power-to-weight ratio: 1.10 kW/kg
