A fairing door assembly for use with an aircraft includes a first door pivotable between a first door open position and a first door closed position. The first door open position is associated with a first flap position of a flap of the aircraft, and the first door closed position is associated with a second flap position of the flap. The fairing door assembly also includes a second door pivotally coupled to the first door. The second door is pivotable between a second door open position and a second door closed position. The second door open position is associated with the first flap position and the second door closed position is associated with a third flap position that is different than the first flap position.
FAIRING DOOR ASSEMBLY AND METHODS OF OPERATING THE SAME
2019-03-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2018
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