Crew: one pilot
Capacity: two
Length: 6.95 m (22 ft 9½ in)
Wingspan: 7.39 m (24 ft 3 in)
Height: 2.62 m (8 ft 7¼ in)
Wing area: 10.44 m² (112.4 ft²)
Airfoil: symmetrical (no camber), zero incidence, zero dihedral/anhedral
Empty weight: 682 kg (approx.) (1,500 lb (approx.))
Useful load: 270 kg (595 lb)
Loaded weight: 952 kg (2095 lb)
Max. takeoff weight: 952 kg (2095 lb)
Fuel capacity: 199.5 l (52.7 U.S. gal)
Powerplant: 1 × Lycoming AEIO-540-L1B5 MT Propeller composite propeller (3- or 4-blade), 224 kW (300 hp)
Performance
Never exceed speed: 408 km/h (220 knot, 253 mph)
Cruise speed: 317 km/h (170 knot, 196 mph)
Stall speed: 102 km/h (55 knot, 63 mph)
Range: 944 km with auxiliary fuel (510 nmi, 586 statute mi)
Service ceiling: 4875 m (16,000 ft)
Rate of climb: 16 meters/s (3200 ft/min)
Roll Rate : 400 degrees per second
(Wiki- GA all the way!)
@Adrien… Pls note Source for both photo and data are shown in parentheses at conclusion of characteristics paragraph. I always include appropriate attribution when source material is utilized as required by appropriate copyright statues., This material is in the “Public Domain”
(Info: @BavariaAVIATION …@anon31652286)