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M332A / M332AK / M332C

M332A - with an on/off switchable supercharger,  for fixed of adjustable propeller, oil system fully compatible with aerobatic flights and inverted flights, barrel rolls forbidden, G force restrictions: +6g, -3,5g

M332AK - with an on/off switchable supercharger,  for fixed of adjustable propeller, oil system fully compatible with aerobatic flights and inverted flights, barrel rolls forbidden, G force restrictions: +6g, -3,5g

M332C- with on/off switchable supercharger, for adjustable propeller, oil system fully compatible with aerobatic flights and inverted flights, barrel rolls forbidden G force restrictions: +8g, -5g.

 

 

M332A/M332AK 

M332C 

Length (mm)

1 102

1 145 

Width (mm)

425

427 

Height (mm)

655

642 

Dry weight (kg)

113

113 

Displacement (L)

3,98

3,98 

Compression ratio (-)

6,3 : 1

7,4 : 1 

 

M332A/M332AK

The given characteristics are with the supercharger turned ON. With the supercharger OFF, the characteristics are similar to M132A/AK engine types.

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

53

 35

28

26

 

M332C

The given characteristics are with the supercharger turned ON.

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

68

 44

 27

25

  

Ground and flight characteristics 

M332A/AK

M332C

naturally aspirated

supercharged

 

naturally aspirated

 

 

 

supercharged

 

 

M332A

M332A LOM ENGINE

M332AK

M332AK LOM ENGINE

M332C

M332C LOM ENGINE