L 2000 E0/EC
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alle Datenblätter Data may change without prior notice. Four cylinder, horizontally opposed air cooled engine, with single magneto ignition, wet sump pressure lubrication L 1700 E0 / EC: Maximum HP (5 min) Continous HP Bore Stroke Displacement Compression ratio L 2000 E0 / EC: Maximum HP (5 min) Continous HP Bore Stroke Displacement Compression ratio Magneto Harness Spark plugs Electrode spacing Firing order Firing point Carburator Fuel min. octane Air cleaner Limbach Flugmotoren GmbH & Co.KG Mechanical fuel pump Starter with solenoid Generator Oil pressure Oil temperature Oil capacity Cylinder head temp. Tachometer drive Propeller drive Propeller hub APG-LIMBACH 12 V - 1.1 kW 14 V - 33 A or 14 V - 55 A max. 4 bar; min. 1 bar at 2500 rpm max. 120 oC; min. 50 oC 2.5 ltrs max. 250 oC mechanical direct, anti-clockwise E01/EC1 for variable pitch E02/EC2 for fixed pitch Dry weight approx. L 2000 E0: 74 kg L 1700 E0: 73 kg Fuel consumption should be individually established during flight tests, however the average fuel consumption is approx.: 10 ltrs/hr L 1700 E0 / EC 12 ltrs/hr L 2000 E0 / EC LBA Type Certificate No. 4582 (JAR 22-H) L 1700 E0 / EC 4597 (JAR 22-H) L 2000 E0 / EC

alle Datenblätter Limbach Flugmotoren GmbH & Co.KG Data may change without prior notice.