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C r e a t i n g a n e w C a t e g o r y i n L i g h t J e t s :
A d v A n c e d
Creating a new Category in Light Jets:
AdvAnced
E N G I N E E R E D F O R P E R F O R m a N c E
an all-composite fuselage, a natural-laminar flow airfoil and nose design,
and an over-the-wing engine configuration combine to enable the highest speed
and best fuel efficiency in its class.
D E S I G N E D F O R D E S I R E
The preferred execution of onboard comfort includes a spacious,
elegantly appointed cabin, a fully private lavatory, and generous cargo stowage.
B u I l T F O R P E R F E c T I O N
Innovative design, exacting development, and meticulous
testing result in a new class of light jet: advanced.
T h E S k y I S y O u R S
D E S I G N I N N O V a T I O N
O v e r - t h e - W i n g
e n g i n e - M O u n t D e s i g n
hondaJet’s Over-the-Wing engine-Mount (OtWeM) design
solves two challenges, beautifully:
it achieves wave-drag reduction so efficiently, it actually
out-performs clean-wing designs.
it eliminates engine-mount fuselage encroachment for a
larger, more spacious cabin and greater cargo stowage
capacity.
Jet owners no longer have to decide between performance
and comfort. HondaJet delivers both.
advanced engineering
for performance
and passenger comfort
remarkable performance
High cruise efficiency
extraordinary comfort
Expanded cabin space
D E S I G N I N N O V a T I O N
n a t u r a l - l a M i n a r F l O W
a i r F O i l a n D n O s e
the hondaJet natural-laminar Flow (nlF) airfoil and nose
design boosts fuel efficiency and improves performance,
simultaneously:
it exhibits a high maximum lift coefficient and low profile
drag coefficients at climb and cruise, resulting in high
fuel efficiency and class-leading performance.
it results in a small nosedown pitching moment coefficient
at high speeds and reduced loss in maximum lift coefficient
due to leading-edge contamination, providing responsive
and reassuring handling characteristics.
advanced engineering
for performance
and efficiency
exceptional efficiency
High maximum lift coefficient
Outstanding responsiveness
Docile stall characteristics
D E S I G N I N N O V a T I O N
g e / h O n D a h F 1 2 0
t u r b O F a n e n g i n e
ge/honda hF120 turbofan engines power hondaJet to new
levels of performance for range, payload, and dependability:
Fluid dynamics software automatically optimizes airflow
for maximized performance.
Full authority Digital electronic Control (FaDeC) system
provides superior reliability and optimal operation.
advanced engineering
for performance and
reliability
unparalleled dependability
Ultra-compact FADEC
rewarding performance
High thrust-to-weight ratio
D E S I G N I N N O V a T I O N
a l l - C O M p O s i t e F u s e l a g e
a remarkably light all-composite fuselage is one reason
hondaJet offers both exceptional fuel efficiency and
performance – and its structure allows for a more spacious
cabin, as well:
a cutting-edge combination of co-cured integral structure
and honeycomb sandwich structures produces a lighter
fuselage design that contributes to greater fuel efficiency
and increased performance.
the advanced fuselage configuration contributes to a
larger interior cabin space for greater comfort and
increased payload.
advanced engineering
in aviation fuselage
design
performance-focused structure
Fast, yet fuel efficient benefits
space-conscious design
Room to relax
s p e C i F i C a t i O n s
P E R F O R m a N c E
Maximum Cruise speed @ Fl300 420KTAS
service Ceiling FL430
rate of Climb 3990 ft/min
vFr range 1400 nm
iFr range 1180 nm
take-off Distance 3120 ft
landing Distance 2500 ft
E N G I N E S
Manufacturer / Model GE-HONDA / HF120
Output 1880 lb/each
bypass ratio 2.9
E x T E R N a l D I m E N S I O N S
height 13.21 ft [4.03 m]
length 41.70 ft [12.71 m]
span 39.87 ft [12.15 m]
P a y l O a D
passengers 2 crew + 5 passengers
baggage 66 cu.ft
H o n d a J e t
engineered for Performance | designed for desire | Built for Perfection
hondajet.com
H o n d a J e t
engineered for Performance | designed for desire | Built for Perfection
hondajet.com
