AIRCRAFT SPECIFICATIONS

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1 . G e n e r a l D e s c r i p t i o n. 1.1. Number of Crew Places. the basic aircraft shall have accommodation for a pilot. and copilot. …

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A I R C R A F T S P E C I F I C A T I O N S
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A I R C R A F T S P E C I F I C A T I O N S
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1 . G e n e r a l D e s c r i p t i o n 1.1. Number of Crew Places the basic aircraft shall have accommodation for a pilot and copilot. 1.2. Number of Passengers the aircraft shall be designed to accommodate a maximum of five passengers and two crew members in the standard interior configuration; and six passengers and two crew members in the air taxi configuration. 1.3. Number and Type of Engines two Ge Honda HF120 turbofan engines 1.4. Certification the aircraft will be certified to the requirements of U.s. Far part 23, including: Day, night, VFr, iFr, single pilot operation, flight into known icing conditions, and rVsM certification. 1.5. Approximate Dimensions overall Height ………………………………………13.21 ft (4.03 m) overall length……………………………………..41.70 ft (12.71 m) Wing span (overall)……………………………………….39.87 ft (12.15 m) cabin Height (overall) ………………………………………..4.94 ft (1.51 m) length— Fwd. pressure Bulkhead to aft pressure Bulkhead ………………………….. 17.80 ft (5.43 m) Width…………………………………………………….5.00 ft (1.52 m) 1.6. Approximate Weights Useful load………………………………………..3,378 lb (1,532 kg) Maximum payload……………………………….. 1,400 lb (635 kg) figure 1 HondaJet Exterior Dimensions 41.70 ft 13.21 ft 39.87 ft H o n D a J e t aircraft Description september 2007 I N T R O D u C T I O N HondaJet employs numerous advancements in aircraft technology and design to achieve far better fuel efficiency, more available cabin space, and higher cruise speed than conven- tional aircraft in its class. This document is published for the purpose of providing general information for the evaluation of the design, performance and equipment of the Aircraft. HondaJet carries with it Honda’s legendary commitment to world-class quality in design and manufacture. Key HondaJet innovations include a unique over- the-wing engine-mount (OTWEM) configuration, a natural-laminar flow (NLF) wing and fuselage nose, and an all-composite fuselage. H o n D a a i r c r a F t c o M pa n y, i n c . 6423-B Bryan Blvd. Greensboro, North Carolina 27409 hondajet.com

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