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Brand Name : Rotax
Model Number : 914 F2-01
Certification : EASA FORM 1
Place of Origin : Austrian
MOQ : 1 EA
Engine with propeller speed reduction gearbox i = 2.43 : 64.0 KG
Exhaust system : 4.0KG
Engine suspension frame : 2.0KG
Overload clutch : 1.7KG
External alternator : 3.0KG
PERFORMANCE : 84.8 kW 115 hp 5800 1/min
TORQUE : 144 Nm 106 ft. lb. 4900 1/min
Max RPM : 5800 1/min
BORE : 79.5 mm 3.13 in
STROKE : 61.0 mm 2.4 in
DISPLACEMENT : 1211.2 cm³ 73.91 cu in
FUEL* : min. MON 85 RON 95* min AKI 91*
Low-weight engine with excellent performance at high altitudes.
Four-stroke piston engine with four liquid and air-cooled cylinders
Turbocharger
Automatic wastegate control
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
2 carburetors
Dual electronic ignition
Electric starter
Propeller speed reduction gearbox
Engine mount assembly
Air intake system
Exhaust system
TBO 2,000 hrs
If you have requirements, we can provide a complete engine airworthiness file and engine log
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Rotax 914F2 aircraft engine,1 set in stock, the flight time does not exceed 50 hours Images |