<< maximum landing gear operating speed | maximum landing weight | maximum performance takeoff >>
Back to: "M"
maximum landing weight
- Definição1
- The greatest weight an aircraft is allowed to have for landing. It is often less than the maximum takeoff weight, and the pilot may have to dump fuel or jettison some stores before executing a landing shortly after takeoff. A landing with a higher than maximum weight may require a check of the aircraft structure, especially the undercarriages.
- Fonte1
- KUMAR, Bharat (ed.). An illustrated dictionary of aviation. New York: McGraw-Hill, c2005. 752 p.
- Fonte2
- EMBRAER. Technical dictionary english-portuguese. [São José dos Campos], 2001.
- Fonte3
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Manual of aircraft accident and incident investigation. Part III: investigation. 1st ed. Montreal, 2011. (Doc. 9756)
- Fonte4
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. New larger aeroplanes: infringement of the obstacle free zone: operational measures and aeronautical study. Montreal, 2005. (Cir. 301 AN/174).
- Contexto
- Aircraft wheels are designed with the aircraft maximum operating weight, maximum landing weight, expected landing conditions and maximum performance stopping limitations in mind. In their normal operating environment, aircraft wheels are not expected to last the life of the aircraft and may be time or cycle limited.
- In addition, the maximum landing weight was exceeded, pre-flight planning was incorrect, weather minima were ignored, and the DH procedure was not followed (28 November 1986).
- Subárea
- Aerodynamics
- Français
- masse maximale à l'atterrissage