L 2400 EB
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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 2000 EB Maximum HP (5 min) Continous HP Bore Stroke Displacement Compression ratio L 2400 EB Maximum HP (5 min) Continous HP Bore Stroke Displacement Compression ratio Ignition Harness Spark plugs Firing Order Firing point Carburetor Fuel min. octane L 2400 EB shown Limbach Flugmotoren GmbH & Co.KG Air cleaner Fuel pump Starter with solenoid Generator Oil pressure Oil temperature Oil capacity Cylinder head temp. Tachometer drive Propeller drive Propeller hub Dry weight approx. 2 x LIMBACH LIMBACH 12 V - 1.1 kW 14 V - 33 A or 14 V - 55 A max. 7 bar; min. 1 bar at 2500 rpm max. 120 oC; min. 50 oC 3.5 ltrs max. 250 oC mechanical direct, anti-clockwise EB 1 for variable pitch 76,5 kg L 2000 EB 82 kg L 2400 EB Fuel consumption should be individually established during flight tests, however the average fuel consumption is approx.: 12 ltrs/hr L 2000 EB 14 ltrs/hr L 2400 EB LBA Type Certificate No. 4597 (JAR 22-H) L 2000 EB 4607 (JAR 22-H) L 2400 E

Wartung zuganglich bleiben. Carburator kids must remain Geber Oltemperatur Flachsteckverbinder 6,3 x 0,8 Sender oiltemperature flat plug 6,3 x 0,8 Space required for ignition Limbach Flugmotoren E-Mail: sales@limflug.de