LIMBACH L 2400 DF/EF - liquid cooled Data may change without prior notice. Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual (DF only) ignition system, automatic altitude compensation, wet sump pressure lubrication Maximum Power Bore Stroke Displacement Compression ratio Ignition Spark plugs Electrode spacing Firing Order Firing point Injectors Fuel min. octane Air cleaner Fuel pump Starter with solenoid Generator Oil pressure 74 kW (100 HP) / 3000 rpm 97 mm / 3.82 inch 82 mm / 3.23 inch 2424 cm3 / 147.91 cub. in. 9.5 : 1 Electronic engine management NGK DCPR 7 E 0.7 mm 1-3-2-4 variable, memory mapped 4 x Weber 98 RON (Unleaded) / AVGAS 100 LL LIMBACH 2 x electric 2.5 bar 12 V - 1.0 kW 14 V - 55 A max. 7 bar; min. 1 bar at 2500 rpm Limbach Flugmotoren Kotthausener Straße 5 GmbH & Co. KG D-53639 Königswinter-Sassenberg Tel. ++49-22 44/92 01- 0 Fax ++49-22 44/92 01- 30 E-Mail: [email protected] www.limflug.de Oil temperature Oil capacity Coolant temperature Coolant capacity Tachometer drive Propeller drive Propeller hub Dry weight approx. Fuel consumption LBA Type Certificate max. 120 °C; min. 50 °C 3.5 Itrs max. 110 °C approx. 3 ltrs Electric signal direct anti-clockwise for variable pitch propeller 76 kg, plus accessories 265 g/kWh at WOT 245 g/kWh at part throttle EASA.E.084 (CS 22-

Gaszughülle hier befestigen Fasten guide tube for throttle cable here Hebel in Leerlaufstellung Lever in idle position Raumbedarf für Anschlußstecker Space required for connector Kraftstoffrücklauf zum Druckregler Fuelreturn to pressure regulator Position des Ölfilters bei optionalem Ölkühleradapter Position of oil filter with optional oil cooler adapter Limbach Flugmotoren GmbH & Co.KG Data may change without prior notice.