Experimental aircraft that has been designed, built and tested in accordance with the EASA “Certification Specifications for Normal, Utility, Aerobatic and Commuter Category Airplanes CS-23 Amendment 4”. This is the first serial manufactured aircraft of the Genevation Aircraft company that was used for promotion, demo flights and competition at unlimited, advance and intermediate championship.

GENPRO is a single-seater, mid-wing aircraft with the conventional fixed tailwheel landing gear arrangement. The fuselage has a unique steel composite hybrid truss structure and an aerodynamically streamlined body cover, made of a very thin carbon-honeycomb sandwich structure.

The GENPRO has well balanced, finely tuned handling, coupled with aggressive maneuverability within an exceptionally wide speed and roll-rate range The GENPRO was designed to be a strong and agile aircraft with a +/- 10G load tolerance and over 400 degree/second roll rate. Its design and construction deliver impeccable agility and responsiveness together with a perfectly calibrated stick force. 

GENPRO main specs:

Load factor

• AEROBATIC configuration                    +10/-10 g
• NORMAL configuration                         +6/-3 g

Aircraft dimensions

• wingspan                                                  7560 mm / 7995 mm (with winglets) (25-26 ft)
• length                                                       7000 mm (23 ft)
• height                                                       2615 mm ( 8,6 ft)
• wing area                                                 10,7 m2  (11 m2 with winglet)

Weights

• Empty weight                                            636 kg (1375lbs)
• MTOW ACROBATIC                                 818 kg (1800 lbs)
• MTOW NORMAL                                      907 kg (2000 lbs)

Airspeeds

• Vno maneuvering speed                              348 km/h (188 KCAS)
• Vne never exceed speed                              423 km/h (228 KCAS)
• Vs stall speed at MTOW ACROBATIC         92 km/h (50 KCAS)
• Vs stall speed at MTOW NORMAL              100 km/h (54 KCAS)
• Vmax (tested)                                               524 km/h (283 KCAS)

Roll rate: (customizable)                              <400 °/sec 

Fuel quantity

• total capacity                                          180 litre (48 gal)
• center/aerobatic tank                             110 litre (29 gal)

In the registry of the Hungarian CAA.

Valid flight permit, radio license and noise cert.

Hybrid carbon - steel (15CDV6) welded truss. Fully conformal carbon- honeycomb streamlined body.

Widely configurable seat and pedal position.

Garmin G3X for flight data, navigation, transponder, com (8.33 kHz), engine monitoring, fuel data, compass

Mechanical speed and altimeter (metric)

Hooker Harness (5 points with double rachet straps)

Berringer breaks and wheels

Exterior Last Painted In 2018

Annual/100 FH inspection completed in June 2023.

Logs and maintenance history is available for the whole life.