LIMBACH L 2400 DT/ET - turbocharged Data may change without prior notice. Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual (DT 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 Limbach Flugmotoren GmbH & Co. KG 96 kW / 130 HP at 3000 rpm 97 mm / 3.82 inch 82 mm / 3.23 inch 2424 cm3 / 147.91 cub. in. 8:1 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 Oil temperature Oil capacity Coolant temperature Coolant capacity Tachometer drive Propeller drive Propeller hub Dry weight 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 86 kg, plus accessories 255 g/kWh at WOT 240 g/kWh at part throttle EASA.E.084 (CS 22-

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