Cable harness test system and test method for checking cable harnesses

1. A cable harness test system, comprising:

a cable tester having a microcomputer and a multiplicity of first test point connections for connecting first ends of a multiplicity of electrical lines of a cable harness and configured to feed line test signals into the multiplicity of electrical lines of the cable harness at the first test point connections; and

a multiplicity of interface simulation devices that each have a multiplicity of second test point connections for connecting second ends of the multiplicity of electrical lines of the cable harness and are each configured to return line test signals received from the cable tester at the second test point connections to the cable tester by the multiplicity of electrical lines of the cable harness.

2. The cable harness test system according to claim 1 , wherein at least some of the multiplicity of interface simulation devices have microcomputers.

3. The cable harness test system according to claim 1 , wherein at least some of the multiplicity of interface simulation devices have only analogue circuits.

4. The cable harness test system according to claim 1 , further comprising:

a monitoring computer coupled to the cable tester and configured to evaluate line test signals returned from the multiplicity of interface simulation devices to the cable tester.

5. The cable harness test system according to claim 4 , wherein the monitoring computer is configured to take the line test signals returned from the multiplicity of interface simulation devices to the cable tester as a basis for detecting defects or faults in the lines of the cable harness and to use an output unit to output an information signal about the detected defects or faults.

6. A test method for checking a cable harness to be installed in an aircraft subassembly, comprising:

connecting a cable tester having a microcomputer and a multiplicity of first test point connections to first ends of a multiplicity of electrical lines of the cable harness;

connecting a multiplicity of interface simulation devices, each having a multiplicity of second test point connections, to second ends of the multiplicity of electrical lines of the cable harness;

feeding line test signals into the multiplicity of electrical lines of the cable harness by the cable tester; and

returning the line test signals received from the cable tester at the multiplicity of interface simulation devices to the cable tester by the multiplicity of electrical lines of the cable harness.

7. The test method according to claim 6 , wherein the cable tester and the multiplicity of interface simulation devices are connected to the multiplicity of electrical lines of the cable harness after the cable harness is installed in the aircraft subassembly.

8. The test method according to claim 6 , further comprising:

evaluating line test signals returned from the multiplicity of interface simulation devices to the cable tester by a monitoring computer coupled to the cable tester.

9. The test method according to claim 8 , wherein the evaluating of the monitoring computer comprises detecting defects or faults in the lines of the cable harness on the basis of line test signals returned from the multiplicity of interface simulation devices to the cable tester and outputting an information signal about the detected defects or faults.

10. The test method according to claim 9 , wherein the detected defects or faults comprise cable fractures, shorts, loose connections, incorrect wiring and/or open lines.