Model



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 IT I-9347 : Alpi Aviation, AH130 prototype


1 C/N.


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