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  2. Honda HA-420 HondaJet - Wikipedia

    en.wikipedia.org/wiki/Honda_HA-420_HondaJet

    [14] [15] The debut attracted strong interest, and convinced Honda executives to commercialize the HondaJet, which Honda publicly announced at the following year's AirVenture. [16] [17] In 2006, Honda announced the commercialization of the jet with a first delivery then planned for 2010. [18] At the time, pricing was set at $3.65 million. [19]

  3. V speeds - Wikipedia

    en.wikipedia.org/wiki/V_speeds

    Takeoff safety speed. The speed at which the aircraft may safely climb with one engine inoperative. [7] [8] [9] V 2 min: Minimum takeoff safety speed. [7] [8] [9] V 3: Flap retraction speed. [8] [9] V 4: Steady initial climb speed. The all engines operating take-off climb speed used to the point where acceleration to flap retraction speed is ...

  4. Honda Aircraft Company - Wikipedia

    en.wikipedia.org/wiki/Honda_Aircraft_Company

    Honda Aircraft Company is an aircraft manufacturer headquartered in Greensboro, North Carolina, responsible for the production of the HondaJet family of aircraft. Originally a secret research project within Honda R&D, Honda Aircraft Company was formed as a wholly owned subsidiary of Honda Motor Company in August 2006 under the leadership of HondaJet designer Michimasa Fujino. [2]

  5. GE Honda HF120 - Wikipedia

    en.wikipedia.org/wiki/GE_Honda_HF120

    An HF120 engine mounted above the wing of a Honda HA-420 HondaJet. Succeeding Honda's original HF118 prototype, the HF120 was undergoing testing in July 2008, with certification targeted for late 2009. [2] The first engines were produced at GE's factory, but in November 2014 production shifted to Burlington, North Carolina. [3]

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  7. Jet engine performance - Wikipedia

    en.wikipedia.org/wiki/Jet_engine_performance

    Air Florida Flight 90 crashed on take-off in snow and icing conditions. The required take-off thrust was 14,500 lb which would normally be set by advancing the thrust levers to give an EPR reading of 2.04. Due to EPR probe icing the value set, i.e. 2.04, was erroneous and actually equivalent to 1.70 which gave an actual thrust of only 10,750 lb.

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