Amazing AIRBORNE EDGE X OUTBACK U-A44.
Aircraft Engine Specification for Airborne Edge X Outback (with Rotax 582 UL-DCDI)
π§ Engine Specification
β’ Engine Model: Rotax 582 UL-DCDI (Blue Head)
β’ Engine Type: 2-cylinder, 2-stroke, liquid-cooled piston engine with dual ignition
β’ Displacement: 580.7 cc (35.4 cu in)
β’ Power Output: 64 horsepower @ 6,500 RPM
β’ Maximum Continuous Power: 55 hp @ 6,200 RPM
β’ Fuel Type:
β’ Unleaded automotive gasoline with 2-stroke oil (50:1 mix)
β’ Avgas 100LL (only when auto fuel unavailable)
β’ Fuel System: Dual carburetors
β’ Ignition System: Dual Capacitor Discharge Ignition (CDI)
β’ Cooling System: Liquid-cooled
β’ Reduction Gearbox: Type B or E gearbox with 2.58:1 or 3.47:1 ratio
β’ Dry Weight (with gearbox and electric start): ~64 kg (141 lbs)
β’ Propeller Interface: Typically 3-blade ground-adjustable propeller
β’ Manufacturer: BRP-Rotax GmbH (Austria)
β’ Application: Microlight and ultralight aircraft such as Airborne Edge X Outback
Contact Bob for more information +660958431425
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