Amazing AIRBORNE EDGE X CLASSIC U-P26.
Aircraft Engine Specification for Airborne Edge X Classic (with Rotax 912 ULS)
π§ Engine Specification
β’ Engine Model: Rotax 912 ULS
β’ Engine Type: 4-cylinder, 4-stroke, horizontally-opposed, air/liquid-cooled piston engine
β’ Displacement: 1,352 cc (82.5 cu in)
β’ Power Output: 100 horsepower @ 5,800 RPM
β’ Maximum Continuous Power: 95 horsepower @ 5,500 RPM
β’ Compression Ratio: 10.5:1
β’ Fuel Type:
β’ Premium unleaded gasoline (minimum 95 RON)
β’ Avgas 100LL (when auto fuel not available)
β’ Fuel System: Dual carburetors
β’ Ignition System: Dual electronic ignition
β’ Cooling System: Air-cooled cylinders and liquid-cooled cylinder heads
β’ Reduction Gearbox: Integrated gear reduction, ratio 2.43:1
β’ Dry Weight: ~132 lbs (60 kg)
β’ Propeller Interface: Ground-adjustable or constant-speed propeller
β’ Manufacturer: BRP-Rotax GmbH (Austria)
β’ Application: Airborne Edge X Classic microlight and other light-sport aircraft
Contact Bob for more information +660958431425
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