Amazing AIRBORNE EDGE X CLASSIC U-P26.
Aircraft Engine Specification for Airborne Edge X Classic (with Rotax 912 ULS)
🔧 Engine Specification
• Engine Model: Rotax 912 ULS
• Engine Type: 4-cylinder, 4-stroke, horizontally-opposed, air/liquid-cooled piston engine
• Displacement: 1,352 cc (82.5 cu in)
• Power Output: 100 horsepower @ 5,800 RPM
• Maximum Continuous Power: 95 horsepower @ 5,500 RPM
• Compression Ratio: 10.5:1
• Fuel Type:
• Premium unleaded gasoline (minimum 95 RON)
• Avgas 100LL (when auto fuel not available)
• Fuel System: Dual carburetors
• Ignition System: Dual electronic ignition
• Cooling System: Air-cooled cylinders and liquid-cooled cylinder heads
• Reduction Gearbox: Integrated gear reduction, ratio 2.43:1
• Dry Weight: ~132 lbs (60 kg)
• Propeller Interface: Ground-adjustable or constant-speed propeller
• Manufacturer: BRP-Rotax GmbH (Austria)
• Application: Airborne Edge X Classic microlight and other light-sport aircraft
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