Ultralight helicopter with gas turbine produced by Alpi Aviation in Pordenone, Italy


Engine: 1 x Solar T61-A 130 shp
Capacity: 1 + 1
Length: (m) 8.84
Height: (m) 2.4
Blades: 2
Rotor diam.: (m) 7.63
Disc area: (m2) 45.7
Weight: (kgs) Empty: 290     Max: 500
Speed: (km/h) Cruise: 160     Max: 200
Range: (km)
Ceiling: (m) 3800
Rate/Climb: (m/min) 510

List of Operators of Alpi Helicopter AH130 Syton

From Organisation with model AH130 Syton

Construction Numbers on database of AH130 Syton or its versions


Construction Numbers

Help Us

C/NBuilt asYearHistory
2008 IT I-9347 : Alpi Aviation, AH130 prototype

1 C/N.

share     facebook     twitter     linkedin