M137A / M137AZ
M137A - for fixed,electrically adjustable or autonomous propellers, oil system fully compatible with aerobatics and inverted flights without restrictions, flick aerobatic manoeuvres 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, flick aerobatic manoeuvres 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 |