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GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL
GERMAN LTF-UL

AERO&TECH NEXTH

advanced aerodynamic development
Technology and Design Made in Italy
V Max
285 km/h
Cruise Speed
255 km/h
Tested Load Factors
+9 - 4.5 G
Endurance
1700 km Endurance
CERTIFICATION
GERMAN LTF-UL



TECHNICAL DESCRIPTION

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.

 

PERFORMANCE

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

 

ULTIMATE LOAD FACTORS

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)

 

WEIGHT AND DIMENSIONS

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-PROPELLER

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)

 

FUEL SYSTEM

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

 

EXTERNAL

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)

 

STRUCTURE

+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

 

SAFETY

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

 

INSTRUMENTS AND INTERNAL ERGONOMICS

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