fig7 fastening the hatrack 2 takes place by way of a detachable form locking and or force locking snap connection 35 36 which is in particular designed as a snap and click closure to provide safe and secure fastening to the structure 8 that is fixed to the aircraft for example frame elements or stringers of the aircraft fuselage 5 for individual adjustment of the hatrack 2 it is beneficial to arrange the aforesaid in rails that extend parallel to each other which rails are arranged in longitudinal direction of the aircraft in this arrangement fastening can for example take place with fastening elements integrated in the rails which fastening elements interact with the snap connections 35 36 swivelling the internal housing 9 from the loading or unloading position illustrated in fig7 to the transport position according to fig6 causes the stowed pieces of luggage to be displaced by way of the floor 17 that forms a chute to the downwards pointing trough shaped region of the internal housing 9 in the transport position the bottom 17 is seamlessly integrated in the cabin lining 6 mechanical opening of the hatrack 2 to remove items of luggage from the internal housing 9 can take place by way of the recessed grip 19 in the bottom 17 as an alternative to this.