www.aircraftworlddirectory.comAircraftWorldDirectory.com
Home   Civil Aircraft   Military Aircraft   World's Civil Aircraft Book  Airports
Airlines of the World  International Registrations  Art  About Us   Contact Us
Google  

 

Vortech (Adams-Wilson) Choppy     


The Vortech Choppy is an updated version of the Adams-Wilson Choppy which was first flown in 1958. Vortech Inc. of Fallston, Maryland provide plans and kits for several rotorcraft including the single seat G-1 ultralight helicopter powered by a 40hp (29kW) Rotax 447 and with a maximum take-off weight of 420lb (190kg). The Vortech Skylark single seat helicopter is powered by a 65hp (48kW) Rotax 503 and has a maximum take-off weight of 725lb (329kg).

Vortech (Adams-Wilson) Choppy

Registration unknown                         USA

Single seat helicopter first flown in 1995

Engine: 50hp(37kW) Rotax 503                                                                                                      Length: 15’0"(4.56m)                                                                                            Height: 6’0"(1.82m)Rotor diameter: 21’6"(6.54m)                                                                                         No.built: 15+ Range: 80miles(128km)                                                                    Cruising speed: 65mph(104kmh) Empty weight: 300lb(136kg)                                                     Maximum take-off weight: 600lb(272kg)

Return to Civil Aircraft V Index