Abstract: A method for leakage detection in an aeronautical band for a high split HFC network includes: providing a vehicle borne leak detector configured to perform substantially simultaneous upstream and downstream leakage detection; and while traversing a hub containing any quantity of high split nodes, performing a substantially simultaneous upstream leakage detection and a downstream leakage detection at about a same frequency. A system for leakage detection in an aeronautical band for a high split HFC network is also described.

Abstract: A time stamp method of location leakage in an aeronautical band of a high split HFC includes: scheduling at a cable modem termination system (CMTS), a generation of a plurality of OUDP bursts by at least one cable modem (CM) within a node in a fixed sequence; measuring a field leakage detector time stamp of a plurality of detected OUDP bursts relative to a half second GPS synch pulse, and sending a report to a leakage data server with a set of current GPS coordinates of a leakage detector, a time stamp, a detected leak level, and a measured OUDP time stamp; and calculating at the leakage data server, a CM ID based on the measured OUDP time stamp and a duration of an OUDP burst combined with a query to the CMTS and a CM database, to define a physical address of a CM corresponding to the CM ID.