Cargo tie down system

The lashing point fixture (1) for a cargo loading system of especially an aircraft has a lashing element (2) mounted in a housing (5) and rotatable around a pivot axis. The housing furthermore has a fastening holder (8) which has a rail profile system (13) which when the lashing component is not in use can accommodate at least one connecting element for additional components. The lashing element is pivotable into an approximately horizontal position, and the fastening holder is located in a plane above the pivot axis.