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
FLUGZEUG-FAHRWERKSANORDNUNG UND ENTSPRECHENDE ZUSAMMENBAUVERFAHREN
TRAIN D'ATERRISSAGE POUR AVION ET SON PROCÉDÉ D'ASSEMBLAGE
2020-11-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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