Metal construction with aeronautical aluminum (6061T6 – 2024T3 – 7075T6), ultrasonic tested for mechanics – 15CDV6 GR3 steel tubing fuselage and engine mount frame – Folding low-middle wing – Tractive propeller – Tricycle fix /retractable landing gear with titanium legs -and manual emergency system – Nose gear steerable, independent from engine mount – Two side by side places with double controls – Safety cell – Gull-wing opening doors – Trim on three axes, ready for Autopilot (on request).
Patented Design
Non Explosion Fuel 50 lt (13 US Gal) 130 lt (34 US Gal)  tank  – Adjustable pedals – Certified braking system and wheels – Cockpit and glass air vents – Flight and maintenance manual – Warranty for 2 years.

Rotax 912 ULS 100 Hp with 3 blade propeller FG (Fixed Gear)
HS High Sport version:
Rotax 914 UL with Variable Pitch Propeller, Sport Wing and RG (Retractable Gear)

Max speed  100% power (HS): 240 (285 ) km/h – 130 (154) kts
Cruise speed 75% power (HS): 225 (255 ) km/h – 121 (138) kts
Stall full flap speed, LTF-UL certified version – (HS): 65 (75) km/h – 35 (40) kts
Max speed never exceed Vne: 305 km/h – 165 kts
Max design speed Vd: 340 km/h – 183 kts
Rapid/steep climb speed: 130/100 km/h – 70/53 kts
Take off /landing distance: 120 / 120 m – 394 /394 ft
Climb rate: 7.9 m/s – 1550 ft/min
Aerodynamic efficiency:  12 : 1 at  130 km/h – 70 kts
Operative ceiling altitude: 5000 m – 16400 ft
Fuel consumption MIN. / 75% : 13.5 / 18 lt/h  – 3.56 / 4.75 US Gal/h
Endurance min-max 50 /130 lt fuel tank:         2.7 – 3.7 max 650  km / 7.2 – 9.6 hrs  max 1700 km
Endurance min-max 13 /34 US Gal fuel tank:  2.7 – 3.7 max 351  nm / 7.2 – 9.6 hrs  max  918 nm 

AEROBATIC CATEGORY + 9 – 4.5 G (the project task is to give to pilot a safety cell without aerobatic activity intent, not recommended for the category)

Max. take off weight MTOW ULM /  LSA :  472,5 / 600 kg  – 1042 / 1323 lb
Min. EMPTY Weight: 298.5 kg – 658 lb
Max project weight: 600 kg – 1323 lb
Wing area: 10 (9.5) mq – 108 (102) sq ft
Wingspan: 7.83 m 25.7 ft  standard tip version – 7.95 m  26.1 ft winglet version
Length: 6.94 m – 22.8 ft
Cabin max width – max height (seat to cockpit roof): 1.12 m x 0,96 m – 3.7  ft x  3.1 ft
Baggage max volume (hatrack + fuselage luggage compartment) :
36 + 160 lt   – 1,3 + 5.6 cu ft  /  5+25 Kg –  11 + 55 lb

Engine: ROTAX 912 ULS2/3 – 100 HP – 5800 RPM -1352 cc (available 914 Turbo,  912 / 915 ISC SPORT)
3 blade fixed propeller (with variable pitch on request)
Consumption: 5500 rpm continuous 25 l/h (5.6 gl/h);
75% 4750 rpm continuous 18.5 l/h (4.2 gl/h)
Engine mount in special steel tubing 15 CDV 6 GR3 with pressure inspection
Double starting system with Safe Start System
Liquid – air cooling system with water and oil radiator and filter
Oil thermostat
Central Throttle control
Three fix blade propeller (with variable pitch on request)

Central non explosive fuel safety tank
Non overflowing valve
External cap with key
Fuel quick drain with filtered outlet
Protected fuel lines
Mechanical engine pump
Electrical back-up pump

Double slot flap with electronic control
Fixed / Retractable electrical /pneumatic gear with titanium GR5 main legs
( the gear legs system is the same for the fixed and retractable configuration, so that it is
possible to convert the one to the other as a simple upgrade)
Load tested wheels sand  nose gear steerable
3 Axes-Trim configuration ready for Autopilot (on request)
Nexth Color: Black Carbon Composite for fuselage skin / natural aluminum look for wings
(on request available personal painting design)

+9G -4.5G (FAR23 – CS-VLA AEROBATIC CATEGORY)

High resistance frame and safety cell in special steel tubing Cr-MO 15 CDV 6 GR3
Skin/Wing AL2024 T3 – AL6061T6 with aviation riveting – 7075 T6 CNC full machined
spars and mechanics made of ultrasonic tested material
In autoclave high pressure carbon composite elements , used only for non structural light parts

Stall warning
Gear warning system and  mechanical emergency system
NSC nose gear no steering collision system
Gull-wing doors with internal  double lock and external locking key, opening also after accidental overturning
Parachute with guaranted minimun safety opening height
Real 360° visibility and aviation sun glass
ELT (on request)
4/5 point seat belt
Wing safety sea floating tanks (on request)
Hot air glass vent (on request)
Tail strobe light – taxi light – landing light
Electrical back up pump
Firewall Shut off valve and Fuel valve with Safe Start System for 912 ULS

Engine and flight instruments in different versions: ANALOGICAL – HYBRID – DIGITAL,
available also with personal configurations including:
ENGINE: rpm, oil temp. and press., water temp., MAP, CHT/EGT, fuel pressure, fuel tank indicator, ammeter , voltmeter
FLIGHT: air/vertical speed indicator, altimeter, turn coordinator, compass,
artificial horizon (only for hybrid and digital), radio and intercom
GPS (on request)
ELT (on request)
Autopilot (on request)
Cloche main trims
Brake adjustable pedals (on request)
Carbon look Exclusive interior design
Air vents
Removable headrests
The described technical characteristics can be improved without notice by the manufacturer