| 摘要 |
A device for bridging a cable harness between two aircraft structure elements of an aircraft includes an elongated connecting rod having a plurality of radial snap-in holes and configured to bridge a space between the two aircraft structure elements and affix to at least one of the two aircraft structure elements. The device also includes a cable guiding element having at least one receiving section for receiving the cable harness and at least one attachment section circumferentially surrounding the connecting rod, the attachment section having a resiliently held radially directed locking pin, wherein the locking pin corresponds to one of the plurality of the radial snap-in holes so as to form a clip connection and a positive locking engagement between the at least one attachment section and the connecting rod.
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