Container for a supply unit, namely an oxygen supply unit and/or a passenger supply unit or a passenger supply device, - the container having a container well at least, wherein a container door can be pivotably joint at a container well's edge, pivotable about a hinge at the container well's edge; and - the container being adapted for respective support to another container in a panel along an aircraft's cabin, wherein the container and the another container are arranged for respective support of each other at at least one of each of the container well's edge; wherein - the container well at least consists of a sheet moulded compound material moulded from a composite of thermoset sheet material based on fiber-reinforced, polymer matrices mainly, wherein - the container has front, rear and side container walls (1.1, 1.2, 1.3, 1.4) and at least one wall region and at least one transition region (5.1, 5.2, 5.3, 5.4) there between, characterized in that - the sheet moulded compound material comprises a directed long fiber system (C-SMC) of sheet moulded material, wherein the fibers of the reinforcement are endless fibers of a directional system of fibers, or wherein dispersed long length fibers have a length greater than 2.54 cm (1 inch), - the wall region has a wall thickness of below 2 mm, and - the container well's edge has an edge material thickness and container wall's transition regions (5.1, 5.2, 5.3, 5.4) have a transition region material thickness, wherein the edge material thickness and the transition region material thickness is at least partly larger than a wall thickness, wherein at least one wall and/or transition region has reinforcing depressions and - the container well's edge is integrally moulded with the container well, wherein on the front and rear container wall (1.1, 1.2) the reinforcing depressions extend into the container well's edge, and - the reinforcing depressions have a depression material thickness wherein the depression material thickness is larger than a wall thickness. - the container having a container well at least, wherein a container door can be pivotably joint at a container well's edge, pivotable about a hinge at the container well's edge; and - the container being adapted for respective support to another container in a panel along an aircraft's cabin, wherein the container and the another container are arranged for respective support of each other at at least one of each of the container well's edge; - the container well at least consists of a sheet moulded compound material moulded from a composite of thermoset sheet material based on fiber-reinforced, polymer matrices mainly, wherein - the container has front, rear and side container walls (1.1, 1.2, 1.3, 1.4) and at least one wall region and at least one transition region (5.1, 5.2, 5.3, 5.4) there between, characterized in that - the sheet moulded compound material comprises a directed long fiber system (C-SMC) of sheet moulded material, wherein the fibers of the reinforcement are endless fibers of a directional system of fibers, or wherein dispersed long length fibers have a length greater than 2.54 cm (1 inch), - the wall region has a wall thickness of below 2 mm, and - the container well's edge has an edge material thickness and container wall's transition regions (5.1, 5.2, 5.3, 5.4) have a transition region material thickness, wherein the edge material thickness and the transition region material thickness is at least partly larger than a wall thickness, wherein at least one wall and/or transition region has reinforcing depressions and - the container well's edge is integrally moulded with the container well, wherein on the front and rear container wall (1.1, 1.2) the reinforcing depressions extend into the container well's edge, and - the reinforcing depressions have a depression material thickness wherein the depression material thickness is larger than a wall thickness.