avia.wikisort.org - Aeroplane

The Softex-Aero V-24 is a proposed five place twin engined aircraft from Ukrainian-based Softex-Aero.

V-24
Role	Light aircraft Type of aircraft
National origin	Ukraine
Manufacturer	Softex-Aero
First flight	2012
Introduction	2014
Status	In development

Design and development

The V-24 is a T-tailed twin engine composite construction pusher aircraft with retractable tricycle landing gear. The aircraft will be powered by either Rotax 912, or 160 hp Lycoming IO-320 engines. The aircraft has a Galaxy GRS 1200 parachute system integrated into the airframe. Turboprop engines are also under consideration.[1][2]

Variants

V-24

Rotax 912 power

V-24L

160hp Lycoming IO-320

V-24TP

PBS TJ-100 turboprop power

Specifications (V-24)

Data from AOPA[1]

General characteristics

• Crew: 1 pilot
• Capacity: 4 passengers
• Wingspan: 11.2 m (36.7 ft)
• Gross weight: 1,300 kg (2,866 lb)
• Powerplant: 2 × Rotax 912 horizontally opposed piston aircraft engine, 75 kW (100 hp) each
• Propellers: 3-bladed MT Propeller

Performance

• Maximum speed: 250 km/h (155 mph, 135 kn)
• Cruise speed: 219 km/h (136 mph, 118 kn)
• Stall speed: 98 km/h (61 mph, 53 kn)
• g limits: +4/-2

Avionics

• Dynon SkyView

References

External links

• Softex-Aero
• YouTube video
• YouTube video

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