Inglês/Português
<< maximum certificated takeoff weight | maximum continuous power | maximum flap extended speed >>
Back to: "M"maximum continuous power
- Definição1
- Maximum continuous power is the maximum power the engine can generate continually.
- Fonte1
- FEDERAL AVIATION ADMINISTRATION. Aircraft flying handbook. Washington, 2004. Disponível em: http://www.faa.gov/library/manuals/aircraft/media/FAA-H-8083 -5.pdf. Acesso em: 11 maio 2013.
- Fonte2
- ASSOCIAÇÃO BRASILEIRA DE NORMAS TÉCNICAS. NBR 15971-4: aeronáutica – vocabulário – parte 4: propulsão aeronáutica. Rio de Janeiro, 2011. 44 p.
- Fonte3
- INTERNATIONAL CIVIL AVIATION ORGANIATION. Annex 8 to the Convention on International Civil Aviation. Airworthiness of aircraft. 11th ed. Montreal, 2010.
- Contexto
- For aeroplanes with more than one engine that are turbine-powered or have a maximum certificated take-off mass of over 2 721 kg, after the end of the period during which the take-off power or thrust may be used, the aeroplane shall be capable of continuing to climb, with the critical engine inoperative and the remaining engine(s) operated within their maximum continuous power or thrust limitations, up to a height that it can maintain and at which it can continue safe flight and landing.
- Subárea1
- Aerodynamics
- Português
- potência máxima contínua