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Length |
6.65 m |
Height |
2.62 m |
Wing span |
7.50 m |
Wing area |
10.44 m² |
Engine |
Lycoming AEIO 540 - L1B5 |
Horse power |
300 HP |
Propeller |
Mühlbauer 3-blade composite |
Construction |
Steel tube fuselage.
Wings, tail & control surfaces = carbon fiber materials |
Fuel |
Gasoline 100LL (AVGAS) |
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Empty Weight |
620 kg |
Maximum aerobatic weight (A)
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820 kg |
Maximum take off weight (N)
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920 kg |
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Load Factor |
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Max. allowed speed |
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Max. cruising speed |
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Max. roll rate |
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Max. rate of climb |
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Take-off run
(brake release to lift off)
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Take - off to 15 m
(brake release to 15 m height) |
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Landing distance over 15 m
(15 m height to stop) |
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Landing roll
(touch down to stop) |
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Touchdown speed |
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© 1996-2018 Jean-Louis Monnet. All Rights Reserved
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