An aircraft landing gear support 1 is provided comprising a support member (such as a landing gear rib 2) and a plurality of pintle supports typically in the form of lugs 5, 7, 8, which form a pintle support arrangement 17 for holding a pintle on which a landing gear assembly may be rotatably supported. The lugs 5, 7, 8 are removably attached to the gear rib 2.
Landing gear support
30.12.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |