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The Limbach L2000 is a series of German piston aero-engines designed and built by Limbach Flugmotoren. They are four-cylinder, four-stroke, air-cooled horizontally opposed, piston engines with a power output of 75 to 80 hp (56 to 60 kW).[1][2]

Limbach L2000
Type	Piston aircraft engine
National origin	Germany
Manufacturer	Limbach Flugmotoren
First run	c.1980
Major applications	Scheibe SF 36

Variants

L2000 DA

Certified in 1989 as a double-ignition tractor engine with carburettor in the back, top location,^{[clarification needed]} alternator in the front, starter in the front. 75 hp (56 kW)[1][3]

L2000 EO

Certified in 1980 as a single-ignition tractor engine with carburettor in the back, bottom location,^{[clarification needed]} alternator in the back, starter in the back. 80 hp (60 kW)[1][3]

L2000 EA

Certified in 1980 as a single-ignition tractor engine with carburettor in the back, top location,^{[clarification needed]} alternator in the front, starter in the front. 80 hp (60 kW)[1][3]

L2000 EB

Certified in 1980 as a single-ignition tractor engine with two carburettors in the back, bottom location,^{[clarification needed]} alternator in the back, starter in the back. 80 hp (60 kW)[1][3]

L2000 EC

Certified in 1980 as a single-ignition pusher engine with carburettor in the back, bottom location,^{[clarification needed]} alternator in the back, starter in the back. 80 hp (60 kW)[1][3]

Applications

Specifications (L 2000 E0)

Data from L 2000 series data sheet[3]

General characteristics

• Type: Four-cylinder, four-stroke air-cooled flat piston engine
• Bore: 90 mm
• Stroke: 78.4 mm
• Displacement: 1.994 cm³
• Length: 627 mm
• Width: 775 mm
• Height: 415 mm
• Dry weight: 70 kg

Components

• Fuel type: Mogas and 100LL Octane petrol
• Cooling system: Air-cooled

Performance

• Power output: 53 kW at 3,000 rpm (max continuous)
• Compression ratio: 8:5 - 8:9:1

See also

Related lists

• Limbach Flugmotoren
• List of aircraft engines

References

Notes

Bibliography

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