Hinge for a foldable rail section for mounting a container of an oxygen supply unit in an aircraft

A container and hinge assembly, comprising:

• a container of an oxygen supply unit for an aircraft, the container having an edge;
• a foldable rail section for mounting said container, said rail section including a plurality of spaced apart rail section parts on a longitudinal side of said rail section;
• a container door extending in parallel to a longitudinal side of said rail section, said container door being connected to said container pivotable around a pivot axis on a rear container edge;
• a first hinge part provided on said rail section, said first hinge part including a bead with a bead part formed integrally on each spaced apart rail section of said longitudinal side of said rail section, and a bead part not formed integrally with said rail section, and slots formed in said rail section, each slot being adjacent to a said bead part not made in one piece with said rail section;
• and
• a second hinge part including tongues formed in one piece with said rear container edge, said tongues having a shape corresponding to a circumferential shape of said bead, said tongues extending into said slots, said tongues of said rear container edge being raised at a tongue end with said pivot axis positioned above said tongues, whereby each said tongue end defines a stop limiting a pivoting stroke of said container door.