Amazing ZENAIR CH-701. Contact us for more information.
 
Aircraft Engine Specification for Zenith CH-701
 
🔧 Engine Specification
    •    Engine Model: Rotax 912 ULS
    •    Engine Type: 4-cylinder, horizontally-opposed, liquid-/air-cooled, 4-stroke piston engine
    •    Displacement: 1,352 cc (82.5 cu in)
    •    Power Output: 100 horsepower @ 5,800 RPM
    •    Maximum Continuous Power: 95 hp @ 5,500 RPM
    •    Compression Ratio: 10.5:1
    •    Fuel Type:
    •    Premium unleaded automotive fuel (minimum 95 RON)
    •    Avgas 100LL (if necessary)
    •    Fuel System: Dual carburetors
    •    Ignition System: Dual electronic ignition
    •    Cooling System: Air-cooled cylinders, liquid-cooled cylinder heads
    •    Dry Weight: 132 lbs (60 kg)
    •    Reduction Gearbox: Integrated 2.43:1 gear reduction
    •    Propeller Interface: Typically fixed-pitch or ground-adjustable
    •    Manufacturer: BRP-Rotax GmbH (Austria)
    •    Application: STOL aircraft like Zenith CH-701; ultralight and light-sport aircraft
 
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