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M132A / M132AK

M132A - for fixed or adjustable propeller, for straight flying, capable of basic aerobatics with an inverted back position time of 5 seconds, barrel-roll forbidden, G force restrictions: +6g, -3,5g
M132AK - for fixed of adjustable propeller, oil system fully compatible with aerobatic flights and inverted flights, barrel rolls 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

M132A LOM ENGINE

M132AK

M132AK LOM ENGINE