DiNelly eXoGyro Huxly




world`s first 4 door UL gyrocopter as utility mission aircraft


with outstanding performance - ESTOL | SSTOL | STOL


The Huxly, our unique ultralight utility high tech aircraft, is deisgned to give enormous possibilities of mission operation and further enhance to reduce your operational costs. The matchless large GCSC - gyrocopter comfort space cabin - is designed to offer the pilot and operator a comfortable working place to fullfill their mission and set new standars in branch of gyrocopters. A compelling mix of distinctive styling, consistent extremly lightweight high end composite design and superios flying dynamics is what the Huxly delivers.


In the branch of gyrocopter we started as pioneer a new era with the Huxly, particularly in the field of untouched economical flight operation. A variety of innovations have been developed for the Huxly and installed in this world-wide unique aircraft for the first time.


Global matchless at the Huxly are features as 4 doors, adjustable rotormast, aerodynamic V-tail, up to 3 hatches for sensorik, double engine, 4 rotorblades in one level, 4,7m² panoramic glass, 1,6m³ cargo bay, incombustible composite fuselage, high enduranc, fuel cell as APU, in the of gyrocopter.


Up to 3 hatches at the center of gravity to support a stabile nodal point in flight, power supply including power management for your high end sensing equiment, configuration Pilot + Operator + sensing equipment safe your mision with the DiNelly eXoGyro Huxly.


The Huxly


  • ž4 doors, 5.6yd² panoramic glas (EASA certified), up to 5 seats as ultralight aircraft
  • žaerodynamic V-tail
  • ž56,5ft³ storage / cargo compartment
  • ž150l standard fuel tank
  • ž4 blade rotor – one-level, optional carbon rotor blades
  • žfuselage A1 + B1 fire resistant
  • žequipment power support 12V / 14V / 24V / 28V parallel – inkl. fuel cell support
  • žengine autonomous air conditioning system
  • žengine autonomous heating / engine pre-heating system
  • žoptionally armored: according to European standard EN1521
  • žGyro Comfort Space Cabin ( GCSC ) – full carbon monocoque in high end carbon, weight: 22,5 kg, strenght of 110Kn/mm²
  • žpropeller with 175cm diameter less than 4 kg
  • žbest aerodynamic performance (cw) for side by side gyro
  • žAPU – fuel cell
  • žcomfortable energy absorbing seats
  • žstrongest landing light (up to 700m distance)
  • ždouble engine, diesel engines, electrical engine option
  • žonboard overhead travelling crane
  • žendurance single engine standard 8 hrs, with auxiliary tank 22 hrs
  • žconstruction / assembling / production in compliance to EASA 145 / ISO:9100





energy/shock absorbing (EASA norm)

individually adjustable within seconds

integrated cooling and heating system

comfortable even on day-long operation




dirt-repellent coating

surfaces inside in textile, leather or robust coating

individual colouring of interior and outer surface




4 doors for easy access

56,5 ft³ storage space

large side and bottom windows

extravagant appearance

best aerodynamic performance




fly-by-wire system for electronic flight control

large glass displays

best overview with 5,6 yd² pane



2 and 4 blade on one level

optimized mass balance for comfortable flight feeling

minimal vibration

adjustable mast for ideal flight position

matchless high performance rotorblades



žmast system adjustable during flight for maximum flight stability

žsafety pilot system emergency autopilot system

žaviation-certified glass displays 4x redundant

žaviation-certified glass pane

žtwo separate special tanks

žAPU (auxiliary power unit)

žshock absorbing cabin

žshock absorbing wide gear

žshock absorbing seats

žaramid armored cabin

ž2 large bottom windows

žfireproof bulkheads

žCFK components ISO 9100 aviation certified

žall engine components and fuel lines out of cabin



DiNelly eXoGyro Huxly






5,7 m

18,7 ft


2,98 m

9,78 ft

Widht Cabin

1,48 m

4,86 ft

Lenght cabin inside

2,20 m

7,22 ft

Widht max. (gear)

2,03 m

6,67 ft

access height

50 cm

1,64 ft

Maximum Take-off weight (MTOM)

560 - 750 kg

1235- 1653 lb


aerodynamic V-Tail

aerodynamic V-Tail

Panorma glass


50,6 ft²

UV-transmission panorama glass

< 1%

< 1%

Max. payload

285 - 480 kg

628 lb - 1058 lb

Sinlge engine configuration (aviation certified) | R

1 x Rotax 915 is turbo charged | 1x 135 hp | injection

1 x Rotax 915 is turbo charged | 1x 135 hp | injection

Single engine configuration (aviation certified ) | R

1 x Rotax 912 is | 1x 100hp | injection

1 x Rotax 912 is | 1x 100hp | injection

Single engine configuration | DT

1 x DiNelly Tauros | 1 x 160 hp | injection

1 x DiNelly Tauros | 1 x 160 hp | injection

Double engine configuration (aviation certified) | AE

2 x Austro Engine AE 50 R | 2 x 55 hp | injection

2 x Austro Engine AE 50 R | 2 x 55 hp | injection

Engine configuration

single & double engines

single & dluble engines

Consumption at 75% - R | DT | AE

17 | 19 | 36 ltr

4,5 | 5 | 9,5 gal

Max Speed VN/E

235 km/h

127 kts

Cruise speed (VC)

187 km/h

101 kts

Minimum operation speed

37 km/h

20 kts

Climb rate (subject to ISA SL and engine)

9-17 m/s

29,5 -46 ft/s

Wind conditions - safe operation

up to 100 km/h

up to 54 kts

Service Ceiling (crew oxygen required)

7.100 m

21.100 ft

Maximum operation altidue without oxygen

4.000 m


Max. Range at 75% (6.000ft)

1.650 - 3.950 km

1.030 - 2.460 miles

Flight endurance (auxiliary tank)

8 h (21 h)

8 h ( 21 h)

Fuel consumtion at 75%

17 ltr

3,52 gal

Fuel tank standard

2x 78 ltr

2x 16,5 gal

Auxiliary tank

2x 110 ltr

2x 24,2 gal

Fuel grades



take off distance (over 15m | 49ft obstacle - ISA SL)

30 - 300 m

98 - 985 ft

landing distance (over 15m | 49ft obstacle - ISA SL)

0 - 50 m

0 - 164 ft

Crew mission operation)

single Pilot (Operator)

single Pilot (Operator)

Seats (front row + 2nd row)

2+ 3

2+ 3

Cargo bay



Rotor diameter 2 blade

8,4 | 8,6 m

27,5 | 28,2 ft

Rotor diameter 4 blade

6,2 | 6,7 m

20,34 | 22 ft

Rotor system

low vibration | composite | high performanse | NACA8H12

low vibration | composite | high performanse | NACA8H12

Propeller diameter

up to 175 cm | constant speed | automatic

up to 69 inch | constant speed | automatic




Equipment power supply

12V/ 14V / 24V / 28V

12V/ 14V / 24V / 28V

Avionik standard configuration

9x Analog + 1 x 10,4" + 1 x 5,7" EMU

9x Analog + 1 x 10,4" + 1 x 5,7" EMU

EMU Avionic Suite

EMU by Stock Flight Systems

EMU by Stock Flight Systems

APU (auxiliary power unit)

fuel cell

fuel cell


partially up to 7,62 mm

partially up to .308 Winchester

Heating system

engine-autonomous | 900 - 4.000 Watt

engine-autonomous | 900 - 4.000 Watt

Air condition system

cooling power up to 2.400 Watt

cooling power up to 2.400 Watt













DiNelly Aircraft Inc.

302A W. 12th St. # 308

New York, NY 10014



Mail: contact@dinelly-exogyro.com

Web: www.dinelly-exogyro.com


Director: Mr. Richard Waidhofer

CEO: Mr. Richard Waidhofer


Aviation design engineer: Mr. Richard Waidhofer


Richard Waidhofer Licensor of:

DiNelly - eXoGyro System

DiNelly - Emily

DiNelly - Huxly

DiNelly - UG1- Lilly

DiNelly - LPOA -Lucy

DiNelly - JLTA - Nelly

DiNelly - Molly

DiNelly - Charly

DiNelly - Rotorblades

Field of activity of DiNelly









Social Media








Perry DiClemente
Hermann Künkler - WAIDHOFER-exogyro
Peter Göllner - WAIDHOFER eXoGyro

Peter Göllner

Aerial Sensing | CASO

Geodesy engineer

Perry DiClemente

Aircraft design

Aviation engineer

Hermann Künkler

Engineering | certification

Aviation engineer

Jörn Follmer - WAIDHOFER-exogyro

Jörn Follmer

Sales executive | CSO

MBA business economist

Richard Waidhofer

Richard Waidhofer

Product Owner | CEO

Aviation design engineer



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