Patent ID: 11927042
Assignee: AIRBUS AMERICAS, INC.
Field: Civil engineering (Other fields)
Classification: CPC E  B | IPC B  E

Claim 5:
6. The system of claim 5, wherein:
each of the plurality of hinges is configured such that, during disassembly, the key is configured to slide within the recess, such that the distal end of the key moves within the slot in a direction away from the bore hole of the second attachment plate to disengage the distal end of the key from the notch of the pin, such that the hinge is in a disassembled state; and
when each of the hinges is in the disassembled state:
the supported structure is configured to be lifted, relative to the supporting structure, in the axial direction of the pin, such that the first attachment plate and the second attachment plate are disconnected from each other; and
the supported structure is movable into a position other than the closed position so that egress from the restricted access area is not blocked by the supported structure.