M332A / M332AK / M332C
M332A – with switchable compressor, for fixed or adjustable propeller, for level flight, capable of basic aerobatics with inverted position within 5 seconds, kicking elements prohibited, operating overload limit +6g, -3.5g
M332AK – with switchable compressor, for fixed or adjustable propeller, oil system modified for full aerobatics and inverted flight, kicking elements prohibited, operating overload limit +6g, -3.5g
M332C– with switchable compressor, adjustable propeller (with blades in flagging and reverse positions), oil system modified for full aerobatics and inverted flight, kicking elements prohibited, operating overload limit +8g, -5g
M332A/M332AK | M332C | |
| Length (mm) | 1 102 | 1 145 |
| Width (mm) | 425 | 427 |
| Height (mm) | 655 | 642 |
| Dry weight (kg) | 113 | 113 |
| Stroke volume (L) | 3,98 | 3,98 |
| Compression ratio (-) | 6,3 : 1 | 7,4 : 1 |
M332A/M332AK
The characteristics listed are with the compressor switched on; the characteristics with the compressor switched off are identical to those of types M132A/AK.
| Max. take-off | Max. permanent | Max. travel | Economic travel | |
| Power (kW/k) | 103 / 140 | 84,6 / 115 | 71,3 / 97 | 66,9 / 91 |
| RPM (1/min) | 2 700 | 2 550 | 2 400 | 2 350 |
| Fuel consumption (L/hr) | 53 | 35 | 28 | 26 |
M332C
The characteristics listed are with the compressor switched on.
| Max. take-off | Max. permanent | Max. travel | Economic travel | |
| Power (kW/k) | 124 / 168,6 | 98 / 133,3 | 72 / 98 | 68 / 92,5 |
| RPM (1/min) | 3 000 | 2 700 | 2 400 | 2 300 |
| Fuel consumption (L/hr) | 68 | 44 | 27 | 25 |
Ground and altitude characteristics
M332A/AK | M332C | ||
without compressor | with compressor | without compressor | with compressor |
M332A
| M332AK
| M332C
|
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