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M137A / M137AZ

M137A - for fixed,electrically adjustable or autonomous propellers, oil system fully compatible with aerobatics and inverted flights without restrictions, barrel rolls allowed, specially bulit crankshaft, frontal engine air intake, G force restrictions: +6g, -3,5g

M137AZ - for fixed,electrically adjustable or autonomous propellers, oil system fully compatible with aerobatics and inverted flights without restrictions, barrel rolls allowed, specially bulit crankshaft, rear engine air intake with a possibility of mounting an air filter, G force restrictions: +6g, -3,5g

 

Length (mm) 1 344
Width(mm)

468/450

Height (mm)

688

Dry weight (kg)

146,5

Displacement (L)

5,97

Compression ratio (-)

6,3 : 1

Max. takeoff Max. constant Max. cruise Economical cruise
Output (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/hod)

62

52

43

37

 

Ground and flight characteristics

 

M137AZ

M137AZ LOM ENGINE