M132A / M132AK
M132A - for fixed or adjustable propeller, for straight flying, capable of basic aerobatics with an inverted back position time of 5 seconds, flick aerobatic manoeuvres forbidden, G force restrictions: +6g, -3,5g
M132AK - for fixed of adjustable propeller, oil system fully compatible with aerobatic flights and inverted flights, flick aerobatic manoeuvres forbidden, G force restrictions: +6g, -3,5g
Length (mm) | 1 052 |
Width (mm) | 425 |
Height (mm) | 688 |
Dry weight (kg) | 105 |
Displacement (L) | 3,98 |
Compression ratio (-) | 6,3 : 1 |
Max. takeoff | Max. constant | Max. cruise | Economical cruise | |
Output(kW/k) | 90 / 122,4 | 80 / 108,8 | 70 / 95,2 | 58,5 / 79,6 |
RPM (1/min) | 2 700 | 2 600 | 2 500 | 2 350 |
Fuel consumption (L/hr) | 38,5 | 32 | 28,6 | 23,5 |
Ground and flight charakteristics |
M132A |
M132AK |