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




    Specifications


    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
    blueprints


    List of Operators of Alpi Helicopter AH130 Syton


    From Organisation with model AH130 Syton



    Construction Numbers on database of AH130 Syton or its versions

    1ah130




    Construction Numbers

    Help Us

    C/NBuilt asYearHistory
    2008 I-9347


    1 C/N.


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