LIMBACH L 2000 EC ..........................15 LIMBACH L 2000 DA ..........................16 Performance ..............................18 Performance Graph LIMBACH L 2000 E0 and L 2000 EC ............... 18 Performance Graph LIMBACH L 2000 EA ....................19 Performance Graph LIMBACH L 2000 EB ....................20 Performance Graph LIMBACH L 2000DA ....................
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Operating Manual L 2000 8.15 Drive Belt check, stretching and replacement ................... 35 8.16 Exhaust System Check ..........................36 8.17 Bowden Cable Check..........................36 8.18 Harness Check ............................36 8.19 Check of Bolted Connections ........................36 8.20 Engine Test Run ............................37 8.21 Engine Preservation ...........................
Operating Manual L 2000 Change Index This Edition replaces the Operating and Maintenance Manual from 07/92. This manual has 48 pages and is issued per 01.03.2016 This edition replaces: Date Description 07/92 New edition 01.03.2016 Replaces edition from 07/92 Release Relased and approved on: 01.03.2016 Dipl.-Ing.
Operating Manual L 2000 Introduction This manual is meant to instruction for proper operation and maintenance of the aircraft engine. Modifications to the engine are only permitted with the approval of our development department. Caution: The specially identifies safety notes must be observed to prevent accidents with personal injuries and to prevent damage to the engine.
Alternator • Mechanical Fuel Pump • Constant Pressure Carburetor Model Designation 2000 1. LIMBACH (Manufacturer) 2. Displacement Class in cm 3 3. (E) Single Ignition (D) Dual Ignition 4. Equipment - Basic Type of Construction Tractor Propeller Carburetor rear, bottom...
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Operating Manual L 2000 Type of Propeller Flange Flange for Variable-Pitch Propeller Flange for Fixed-Pitch Propeller 6 + 7. Installation Type Differences with regard to installation related changes Experimental Engine without Certification AA = Variant for powered glider GROB G 109 AB = Variant for powered glider VALENTIN TAIFUN AC = Variant for powered glider HOFFMANN H 36 DIMONA Page: 7/48...
Operating Manual L 2000 Cylinder Designation front = propeller side right rear = accessory mounting side left cylinder 1 cylinder 2 cylinder 3 cylinder 4 Page: 8/48 Edition: 01.03.2016...
Operating Manual L 2000 Technical Data LIMBACH L 2000 E0 Dimensions Bore 90 mm Stroke 78,4 mm Displacement per Cyl. 498,5 cm³ Total Displacement 1994 cm³ Compression Ratio 8,4 : 1 Crankshaft Rotation counterclockwise Magneto Timing 30° BTC Firing Order...
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Operating Manual L 2000 Max. Take-Off Power 59 kW / 80 shp @ 3400 RPM Max. Continuous Power 51 kW / 70 shp @ 3000 RPM Engine Rotational Speeds Max. permissible speed 3400 RPM Max. speed for cruise See flight and maintainance manual of airframe manufacturer.
Operating Manual L 2000 LIMBACH L 2000 EA Dimensions Bore 90 mm Stroke 78,4 mm Displacement per Cyl. 498,5 cm³ Total Displacement 1994 cm³ Compression Ratio 8,6 : 1 Crankshaft Rotation counterclockwise Magneto Timing 30° BTC Firing Order 1-3-2-4 Equipment...
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Operating Manual L 2000 Engine Ratings Max. Take-Off Power 59 kW / 80 shp @ 3400 RPM Max. Continuous Power 51 kW / 70 shp @ 3000 RPM Engine Rotational Speeds: Max. permissible speed 3400 RPM Max. speed for cruise See flight and maintainance manual of airframe manufacturer.
Operating Manual L 2000 LIMBACH L 2000 EB Dimensions Bore 90 mm Stroke 78,4 mm Displacement per Cyl. 498,5 cm³ Total Displacement 1994 cm³ Compression Ratio 8,4 : 1 Crankshaft Rotation counterclockwise Magneto Timing 30° BTC Firing Order 1-3-2-4 Equipment...
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Operating Manual L 2000 Engine Ratings Max. Take-Off Power 59 kW / 80 shp @ 3400 RPM Max. Continuous Power 53 kW / 72 shp @ 3000 RPM Engine Rotational Speeds Max. permissible speed 3400 RPM Max. speed for cruise See flight and maintainance manual of airframe manufacturer.
Operating Manual L 2000 LIMBACH L 2000 EC The technical data of the LIMBACH L 2000 EC model are identical to the technical data of the LIMBACH L 2000 E0 model. "C" indicates the changes concerning the axial bearing for rear engine installation (pusher propellers).
Operating Manual L 2000 LIMBACH L 2000 DA Dimensions Bore 90 mm Stroke 78,4 mm Displacement per Cyl. 498,5 cm³ Total Displacement 1994 cm³ Compression Ratio 8,5 : 1 Crankshaft Rotation counterclockwise Magneto Timing 25° BTC Firing Order 1-3-2-4 Equipment...
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Operating Manual L 2000 Engine Ratings Max. Take-Off Power 55 kW / 75 shp @ 3200 RPM Max. Continuous Power 51 kW / 70 shp @ 3000 RPM Engine Rotational Speeds Max. permissible speed 3400 RPM Max. speed for cruise See flight and maintainance manual of airframe manufacturer.
Operating Manual L 2000 Operating Instructions Strict adherence to the information contained in this operating manual is the basis for undisturbed operation of your engine. Before Starting Perform daily check (see section 7.1) Move power lever to throttle full open position. Check for interference and free movement between the idle cutoff and full open stops at the carburator.
Operating Manual L 2000 Disengage choke. Check oil pressure (must increase within 10 sec.). Runup, Performance Check Run the engine for approx. 2 min. at 1000 - 1200 RPM. Then increase speed to 1500 RPM until oil temperature is 50 °C. Due to the sluggish action of the indication, there will be sufficient effective operating temperature at 50 °C already.
As a remedy we recommend retrofitting an additional electric fuel pump. Please consult your aircraft manufacturer for additional information. In general only such fuels approved by Limbach shall be used (see section 10.2) Page: 24/48 Edition: 01.03.2016...
Operating Manual L 2000 Maintenenance Schedule Maintenance at Limbach aircraft engines is to be performed after fixed time periods or when reaching a certain interval of operating hours. In addition, a "daily check" has to be performed before each flight.
7.3.2 After the first 25 Operating hours Work as specified in Chapter 7.3.4 7.3.3 Every 25 Operating hours Grease magneto couplings. Applicable to all engines except L 2000 EA, DA. 7.3.4 Every 50 Operating hours Check fuel and lubrication system. ...
Operating Manual L 2000 7.3.5 Every 100 Operating hours Check carburetor diaphragm of the Stromberg-Zenith carburetor. Check magneto timing and adjust, if necessary. Clean fuel pump screen. Work as specified in section 7.3.4 7.3.6 Every 250 Operating hours ...
Operating Manual L 2000 Maintenence Instructions This chapter describes the performance of maintenance work. In addition, the preservation of engines as well as winter and tropical operation is covered. Repair activities during engine maintenance may only be performed by authorized persons. Caution: Disconnect spark plug connectors before performing any work on the engine.
Operating Manual L 2000 Cleaning of Air Filter Remove induction air filter. Clean air filter. Replace dry air filter (cloth filter). Wash oil-wetted air filter (wire screen) in gasoline, clean it off by using compressed air and wet with oil. Special filters are to be cleaned according to the aircraft manufacturer's instructions.
Operating Manual L 2000 Carburetor Oil level check Unscrew piston damper. Check oil level and correct as necessary. Oil level should be approx. 4 mm below the top edge of the piston guide (the piston guide has two opposite notches at the top edge).For refilling, use carburetor damper oil only (P/N: 170.210.005).
Operating Manual L 2000 8.7.2 Engines with Limbach Fuel Pump Close fuel shutoff valve. Disconnect fuel lines from pump. Disassemble top of the fuel pump (6 screws). Collect any fuel dripping from the pump. Disassemble valve assy from top of fuel pump with a suitable tool.
Operating Manual L 2000 Attach top of the fuel pump and tighten screws. Reassemble fuel hoses with new gaskets and sealing rings. Tighten hollow bolts and secure with safety wire. Open fuel valve. Perform test run and check for leaks. Fuel Filter cleaning Draining and cleaning of fuel filter.
Operating Manual L 2000 Remove valve cover. Valve clearance check. Turn propeller according to engine rotation until the valves of the second cylinder are overlapping. Now, the valve clearance of the first cylinder may be checked (see cylinder designation at page 3.2). Move thickness gauge between valve shaft and setscrew.
Operating Manual L 2000 Check valve clearance and readjust, if necessary. Mount cylinder head cover. Check gaskets and replace as necessary. 8.14 Cleaning, Check and Setting of Spark Plugs Removal of spark plugs. Disconnect spark plug connectors. Unscrew connectors on shielded spark plugs. Caution: Do not unscrew spark plugs when the engine is hot.
Operating Manual L 2000 Velvet black: Electrode gap too big Mixture too rich Lack of air (induction air filter contaminated) Engine does not reach required temperature Oillike glossy: Interrupted spark plug operation Excess oil in combustion chamber ...
Operating Manual L 2000 8.20 Engine Test Run Check of starting performance. At normal conditions (temperature, maintenance condition) the engine starts easily. If this is not the case check fuel supply and ignition system. Caution: Do not operate the starter a prolonged period of time (Risk of overheating). Warming up Run engine for approx.
Operating Manual L 2000 Removed engine: Remove spark plugs and spray engine oil into the combustion chambers so that the upper part of the cylinder barrel is wetted, too. Crank engine manually or with starter for a few turns. Spray spark plugs with engine oil and install them again.
Operating Manual L 2000 8.23 Operation in Tropical Conditions The following measures are necessary to protect the engine against heat and dust: Air induction filter If the engine is operated in areas of high dust accumulation install larger air filter (contact your aircraft manufacturer for details).
Operating Manual L 2000 Overhaul Major Overhaul Major overhaul must be performed by the manufacturer or overhaul shops, authorized by the manufacturer. Therefore, the engine has to be forwarded to the manufacturer or an authorized overhaul shop, after the operating time limit has been reached. The permissible operating time (TBO) is determined by the latest issue of Technical Bulletin No.
Operating Manual L 2000 Lubricants, Coolants, Fuels 10.1 List of Lubricants Do not use ashless dispersant or straight mineral aircraft engine oils! Use only brand name oils according to spezification API-SG, or higher. (eg. API-SH, SI, SJ, S…) as well as one of Volkswagen-specs VW 500 00, VW 501 01 or VW 502 00. As the temperature ranges of adjacent SAE classes are overlapping, there is no need to change the oil for short time temperature variations.
Operating Manual L 2000 10.2 Fuels Following fuels are factory approved: • Super Plus 98 fuel according to DIN EN 228, • AVGAS 100 LL, • or other unleaded fuels with a minimum octane rating of 98 RON and 87 MON. Notes: •...
Operating Manual L 2000 Trouble Shooting "Small", apparently neglectable causes are often responsible for a "big" effect, i.e. disturbance of engine operation. Detection of the causes is not always easy. The hints to possible trouble causes and their correction contained in this section serve as a guideline for the engine user, listing the most frequent faults.
Operating Manual L 2000 Possible Cause: Remedy: Fuel tank empty (faulty indication of fuel Refuel, replace fuel gauge. gauge). Fuel valve closed or filter locked. Open fuel valve, clean or replace filter. Fuel line defective or not connected. Replace or connect fuel line. Fuel pump defective.
Operating Manual L 2000 12.2.3 Cooling Possible Cause: Remedy: Insufficient or damaged baffling. Repair or complete baffling. Seal leakages. Carburetor shielding defective or missing Replace carburetor shielding. (2 carburetors). Cooling air inlet disturbance (missing Install spinner, increase air inlets in cowling. spinner, cross section too small).
Operating Manual L 2000 12.3 Mechanical System Possible Cause: Remedy: No valve clearance. Set valve clearance. Leaking or sticking valve. Repair cylinder head. Note: In some cases, fuel tanks made out of com- posite materials have been proven to be in- compatible with the fuel, thus causing the tank material to dissolve.
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