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Length |
6.44 m |
Height |
2.30 m |
Wing span |
7.50 m |
Wing area |
11.25 m² |
Engine |
Lycoming AEIO 580 L1B5, Takeoff performance 220 kW
6 cylinder – four stroke - reciprocating |
Propeller |
MTV-9-C-C/C203-20d, three blade, 203 cm diameter |
Construction |
Fuselage shells, wing, all control surfaces and stabilizer are made of high-tech carbon / honeycomb sandwich, manufactured in a wet layup method |
Fuel |
Gasoline 100LL (AVGAS) |
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Empty Weight |
570 kg |
Maximum aerobatic weight (A)
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650 kg |
Maximum take off weight (N)
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750 kg |
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Load Factor |
+10g / -10g |
Max. level speed IAS @ 900m |
407 km/h |
Design Speeds: |
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VA |
305 km/h |
VC |
333 km/h |
VD |
445 km/h |
Max. roll rate |
380°/sec |
Max. rate of climb |
18 m/sec. |
Take - off to 15 m
(brake release to 15 m height) |
270 m |
Landing distance over 15 m
(15 m height to stop) |
360 m |
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© 1996-2018 Jean-Louis Monnet. All Rights Reserved
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