An aircraft landing gear fairing door 300 to releasably cover at least part of an aircraft landing gear bay aperture. The door comprises a base portion 320 having a hinge portion 321, 322, 323 to receive at least one hinge pin along a hinge axis, a body portion 360 to cover at least part of the aperture, and a coupling portion 345 to couple the door with a coupling device 230 coupled to the landing gear such that movement of a leg of the landing gear causes movement of the door about the hinge axis, wherein at least the base and body portions are formed as one integral component. A door assembly to releasably cover an aircraft external aperture comprises a door having a base and body portions, and a connector member connected with the base portion for relative rotation therebetween about a common axis, the connector member fixedly connectable to the aircraft adjacent the aperture to support the door for movement relative to the aircraft about the axis, wherein the door assembly is pre-assembled for subsequent fixing to the aircraft.


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    Title :

    Landing gear doors and installation processes therefor


    Publication date :

    2023-05-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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