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LW (1)
- Usado para
- landing weight
- Fonte1
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Aircraft accident digest n.30. Montreal, 1986. (Cir. 196 AN/115).
- Fonte2
- AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL (Brasil). Regulamento Brasileiro de Aviação Civil: RBAC n. 23: requisitos de aeronavegabilidade: aviões categoria normal, utilidade, acrobática e transporte regional. Brasília, 2013. Disponível em:
- Contexto
- Based on the airplane's zero fuel weight a t Cleveland (165,681 pounds) and the fuel remaining prior to refueling a t Detroit (52,400 pounds), the airplane landing weight at Detroit was approximately 218,081 pounds with a cg of twenty-eight percent MAC.
- Seventy-five percent of maximum continuous power. However, if the power-to-weight ratio at seventy-five percent of maximum continuous power result in extreme nose-up attitudes, the test may be carried out with the power required for level flight in the landing configuration at maximum landing weight and a speed of 1.4 VSO, except that the power may not be less than fifty percent of maximum continuous power.
- Português
- peso de pouso (1)