A landing gear assembly for use with an aircraft includes a housing including a trunnion brace, a drag brace, and an aft brace that together define an opening through the housing. The landing gear assembly also includes a shrink link assembly coupled to the housing such that the shrink link assembly is accessible through the opening.
Aircraft landing gear assembly and method of assembling the same
26.11.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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