Aircraft Engine 1700 E0/EC, 2000 E0/EC Four cylinder, horizontally opposed air cooled engine, with single magneto ignition, wet sump pressure lubrication

L1700 E0/EC:
Maximum HP (5 min) 68hp / 50kW / 3600rpm
Con ti nous HP 60 hp / 44 kW / 3200 rpm
Bore 88 mm / 3.46 inch
Stroke 69 mm / 2.71 inch
Displacement 1680 cm3 / 102.52 cub. in.
Compression ratio 8:1
L2000 E0/EC:
Maximum HP (5 min) 80hp / 59kW / 3400rpm
Continous HP 70 hp / 51 kW / 3000 rpm
Bore 90 mm / 3.54 inch
Stroke 78.4 mm / 3.09 inch
Displacement 1994 cm³ / 121.68 cub. in.
Com pres si on ra tio 8.4 : 1
Magneto Slick 4330
Harness LIMBACH
Spark plugs LIMBACH LB-N41.0
Electro despacing 0.5 mm
Firing order 1 – 3 – 2 – 4
Firing point 30° BTDC
Carburator Zenith 150 CD-3
Fuel min. octane 98 RON (Un lea ded) or AV GAS 100LL
Air cleaner LIMBACH
Mechanical fuel pump APG-LIMBACH
Starter with solenoid 12 V – 1.1 kW
Generator 14 V – 33 A or 14 V – 55 A
Oil pressure max. 4 bar; min. 1 bar at 2500 rpm
Oil temperature max. 120 oC; min. 50 oC
Oil capacity 2.5 ltrs
Cylinder head temp. max. 250 oC
Tachometer drive mechanical
Propeller drive direct, anti-clockwise
Propeller hub E01/EC1 for variable pitch
E02/EC2 for fixed pitch
Dry weight approx. L2000 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 Cer ti fi ca te No. 4582 (JAR 22-H) L 1700 E0 / EC
4597 (JAR 22-H) L 2000 E0 / EC