HondaJet Elite Specifications
General Specifications Mission Profiles
300 nm Mission
Seating 1 + 5/7 Flight Time 0:51
Range (NBAA IFR 100 nm Fuel Reserves, 1 pilot + 3 1,437 nm Fuel Used 650 lb
pax)
Takeoff Distance (Sea Level, ISA, MTOW) 3,491 ft Altitude (FL) FL390
Landing Distance (Sea Level, ISA, MLW) 2,762 ft 600 nm Mission
Aircraft Dimensions Flight Time 1:35
Length 42.6 ft Fuel Used 1,231 lb
Height 14.9 ft Altitude (FL) FL390
Span 39.8 ft 1,000 nm Mission
Interior Dimensions Flight Time 2:42
Length 12.1 ft Fuel Used 1,787 lb
Height 4.8 ft Altitude (FL) FL430
Width 5.0 ft
Baggage Volume 66 cu. Ft.
2 x GE Honda Direct Operating Costs
Engines
HF120
Thrust (Each) 2,050 lb
Fuel $430.95
TBO 5,000 hr
Maintenance (Parts & Labor) $277.29
Service Ceiling 43,000 ft
Engine Reserves $284.18
Maximum Cruise Speed 422 KTAS
Cost per Hour $992.42
Avionics Suite Garmin G3000
Certification Basis FAR Part 23
Cost per Nautical Mile $2.70/nm
Assumptions:
Mission Profiles: Direct Operating Costs:
• Standard Aircraft, ISA • Fuel Price - $4.00/ US Gallon
• 1 Pilot + 3 Passengers, NBAA IFR 100 nm Alternate Fuel • Airframe Maintenance (Parts & Labor) - FlightReady P3
Reserves. • Assumes Annual Utilization of 300 hours / 300 cycles
• Sea Level Departure and Arrival • 5 Year Average Rate
• High Speed Cruise • Engine Reserves – GE Honda EMC² Engine Program
Note: This performance is for indicative purposes and in no way constitute a guarantee or any
other contractual commitment on the part of Honda Aircraft Company. This information MUST
NOT be used for operational purposes.
© 2017 Honda Aircraft Company
Honda Aircraft Company
HA-420 AFM PERFORMANCE
FAA APPROVED HJ1-29001-003-001
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Honda Aircraft Company
HA-420 AFM PERFORMANCE
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Use of approach and landing information tables (continued):
NOTE Landing distances include a 15 % factor to account for
operational factors including crosswind and landing
technique. If required, use the Operational Factors
Required for Landing Distance section to remove or
increase the factor based on the operational rules
required.
NOTE Landing data for 10,700 lbs are provided for reference
and interpolation only in case an emergency landing is
required.
NOTE The landing field length provided in the performance
section of the flight manual is based on a dry runway.
If landing on a wet runway, it is recommended to
increase the predicted landing field length by 30 %.
NOTE Ice Protection ON assumes both ENG and WING A/I
are ON. If only ENG A/I is on, the Ice Protection ON
tables must be used.
NOTE The landing field length wind and runway slope
correction tables are valid for Ice Protection Off and On.
FAA APPROVED HJ1-29001-003-001
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HA-420 AFM PERFORMANCE
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