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M137A / M137AZ

M137A – for fixed or electrically adjustable or autonomous propeller, oil system modified for full aerobatic operation and unlimited inverted flight, kicked aerobatic maneuvers permitted, specially modified crankshaft, air intake to the engine from the front of the propeller, operating overload +6g, -3.5g

M137AZ – for fixed or electrically adjustable or autonomous propeller, oil system modified for full aerobatic operation and unlimited inverted flight, kicked aerobatic elements permitted, specially modified crankshaft, air intake into the engine from the rear of the engine with the option of connecting to an air filter, operating overload +6g, -3.5g

Length (mm)1 344
Width (mm)

468/450

Height (mm)

688

Dry weight (kg)

146,5

Stroke volume (L)

5,97

Compression ratio (-)

6,3 : 1

 Max. take-offMax. permanentMax. travelEconomic travel
Power (kW/k)

132,4 / 180

117,6 / 160

103 / 140

86 / 117

RPM (1/min)

2 750

2 680

2 580

2 400

Fuel consumption (L/hr)

62

52

43

37

Ground and altitude characteristics

M137AZ

M137AZ LOM ENGINE

Technical description and user manual 

en_GBEnglish (UK)