An aircraft door latch apparatus includes a stowage bin assembly having a door that is rotatably moveable between open and closed positions, and a frame structure. The aircraft apparatus includes a latch apparatus that is configured to couple and uncouple the door to the frame structure, the latch apparatus includes a floating strike assembly that pivotably adjusts to a deflection of the stowage bin assembly. Related methods are also provided.
AIRCRAFT LATCH APPARATUS HAVING FLOATING STRIKE ASSEMBLY
26.11.2020
Patent
Elektronische Ressource
Englisch
AIRCRAFT LATCH APPARATUS HAVING FLOATING STRIKE ASSEMBLY
Europäisches Patentamt | 2020
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