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Engine displacement
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1991 cm³ |
121.5 cu.in |
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Take off power
(at 2300 rpm)
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99 kW
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135 hp
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Constant power
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available max. power at respective altitude
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Torque
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410 Nm
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302 ft.lb
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Torque at BEP
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340 Nm
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251 ft.lb
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Bore
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83 mm |
3.26 in |
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Stroke
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92 mm |
3.62 in |
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Compression ratio
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18:1
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Fuel
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Jet A1 and Diesel (EN 590) in any mixture ratio
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Consumption
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15 - 20 l/hr
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4 - 5.3 gal/hr
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Prop
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MT-Propeller with hydraulic variable pitch
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Voltage
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Alternator 14 V optional: 28 V
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Specific fuel consumption at BEP
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220 g/kWh |
0.36 lb/hphr
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Engine (complete & dry)
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134 kg
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295.4 lbs |
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* depends on aircraft type and gear configuration
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width
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depth
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height
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mm
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796
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805
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636
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in
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31.34
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31.69
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25.04
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* depends on aircraft type and gear configuration
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