The Ultimate Balance of Innovation and Inspiration
The original HondaJet introduced a number of innovations to aviation inherited by our current models. Discover what makes the HondaJet the most technologically advanced aircraft in its class.
OTWEM
Over-The-Wing Engine Mount
The Over-The-Wing Engine Mount was engineered and proven by Honda's extensive research and development. This innovative technology provides category-leading advancements such as a more spacious cabin, noise reduction, and increased fuel efficiency.
NLF
Natural Laminar Flow
Advancements in aerodynamics and NLF technology were applied to the design of the main wing airfoil and fuselage nose shape of the HondaJet to reduce aerodynamic drag. This cutting-edge engineering innovation contributes to high cruising speed and increased fuel efficiency.
Avionics
Advanced Cockpit
The HondaJet cockpit is built for optimum safety based on thoughtful ergonomic design and state-of-the-art situational awareness. Honda and Garmin developed a highly customized, next-generation all-glass avionics system that brings pilot and aircraft closer together with touch-screen technology. The cockpit is unquestionably built around the pilot to enable either single-pilot or dual-pilot operation of the HondaJet.
Composite Fuselage
Composite Fuselage
Unlike many jets that use aluminum, the HondaJet employs a lighter yet strong composite fuselage. The fuselage is created from a cutting-edge combination of co-cured integral structure and honeycomb sandwich structures. This results in increased cabin space, better performance, and greater fuel efficiency.
Ownership, by Honda.
Our global service network and 24-hour customer support ensures that Honda Aircraft is always by your side, wherever and whenever you travel.
Owner Stories
Beyond the spec sheets and technical innovations are the stories that really matter. Stories of people, using our products, to empower their lives.
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Specifications
Performance
Maximum Cruise Speed @ FL300
422 KTAS (782 km/h)
Rate of Climb
3990 ft / min (1216 m/min)
NBAA IFR Range (4 occupants)
1223 nm (2265 km)
Takeoff Distance
<4000 ft (1219 m)
Landing Distance
<3050 ft (<930 m)
Engine
Manufacturer / Model
GE Honda / HF120
Output (Uninstalled Thrust)
2050 lbf each derated from 2095 lbf each
Bypass Ratio
2.9
Exterior Dimensions
Length
42.62 ft (12.99 m)
Wing Span
39.76 ft (12.12 m)
Height
14.90 ft (4.54 m)
Interior Dimensions
Length
17.80 ft (5.43 m)
Width
5.00 ft (1.52 m)
Height
4.83 ft (1.47 m)
Baggage Space
Combined Stowage
66 cubic ft
Aft Compartment
57 cubic ft
Nose Compartment
9 cubic ft
Configuration
Typical Configuration
1 crew + 5 pax / 2 crew + 4 pax
Alternative Configuration
1 crew + 6 pax / 2 crew + 5 pax