L 2000 EA datasheet
2Pages

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 EA: Maximum HP (5 min) Continous HP Bore Stroke Displacement Compression ratio L 2000 EA: 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 1 60 hp / 44 kW / 3600 rpm 56 hp / 41 kW / 3300 rpm 88 mm / 3.46 inch 69 mm / 2.71 inch 1680 cm / 102.52 cub. in. 8:1 80 hp / 59 kW / 3400 rpm 70 hp / 51 kW / 3000 rpm 90 mm / 3.54 inch 78.4 mm / 3.09 inch 1994 cm / 121.68 cub. in. 8.6 : 1 Slick 4330 LIMBACH LIMBACH LB-N41.0 0.5 mm 1-3-2-4 30o BTDC Zenith 150 CD-3 98 RON (Unleaded) or AVGAS 100LL Air cleaner Mechanical fuel pump Starter Generator Oil pressure Oil temperature Oil capacity Cylinder head temp. Tachometer drive Propeller drive Propeller hub LIMBACH APG-LIMBACH 12 V - 1,1 kW 14 V - 28 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 EA 1 for variable pitch EA 2 for fixed pitch Dry weight approx. L 2000 EA: 69 kg L 1700 EA: 73 kg1 Fuel consumption should be individually established during flight tests, however the average fuel consumption is approx.: 10 ltrs/hr L 1700 EA 12 ltrs/hr L 2000 EA LBA Type Certificate No. 4582 (JAR 22-H) L 1700 EA 4597 (JAR 22-H) L 2000 EA Optionally available in “light” version with aluminium cylinders: dry weight approx.: 69 kg. Limbach Flugmotoren GmbH & Co.KG

this space required 60 Space required for ignition harness and magneto removal. Limbach Flugmotoren E-Mail: sales@limflug.de