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Alps Aviation Syton AH130



A new helicopter ULM produced by Alps Aviation, the Syton AH130 is an ultralight helicopter built with the precision and the technology of the certified helicopters, from a kit.

The Syton AH130 has side by side seating (equipped of dual controls). The fuselage structure is of aluminium alloys and steel. The fuselage has a lattice of steel tube.

The tail boom uses aluminium sheet, with composite material. Fairings of aerodynamic form and cockpit linings are composite material. The main rotor is two blade semi-rigid. The blades are completely composite in material, with an aluminium alloy rotor head.

Engine: Turbina Turboalbero turboshaft, 130 SHP Max continuous
Max Length: 8.84 m (29.00 ft)
Max Width: 1.60 m (5.25 ft)
Max Height: 2.40 m (7.87 ft)
Fuselage Width: 1.12 m (3.67 ft)
Fuselage Height: 1.82 m (5.97 ft)
Main rotor diameter: 7.63 m (25.00 ft)
Tail rotor diameter: 1.28 m (4.20 ft)
Empty weight: 290 Kg (693.3 lb)
Normal take off weight: 450 Kg (992.0 lb)
Maximum take off weight: 580 Kg (1278.7 lb)
Max Cruise speed: 190 km/h (103.0 kts)
Normal Cruise Speed: 160 km/h (86.0 kts)
VNE: 210 km/h (113.5 kts)
Max Rate of climb: 8.5 m/s (1670 ft/min)
Hovering ceiling IGE: 2800 m (9200 ft)
Hovering ceiling OGE: 1800 m (5900 ft)
Maximum ceiling: 3800 m (12450 ft)
Max endurance: 2 hr



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