Mechanc RF & Microwave Components
An airframe harness is routed once and then lives with the aircraft. It runs through bays that flex, past structure that vibrates and along paths that were agreed years before the wire was cut. Building it to the drawing, in a factory, is what keeps weight down and rework off the line.
Five things that decide whether a harness installs cleanly or gets reworked on the aircraft.
Programme drawings govern. These are representative conditions for airframe harness work.
| Parameter | Typical Requirement | Relevant Series | Note |
|---|---|---|---|
| Shield termination | 360° via backshell | EMI backshells | No pigtails |
| Length tolerance | Per routing drawing | Built to order | Measured, not estimated |
| Temperature | -55 °C to +125 °C | Aerospace series | Bay and bilge zones |
| Bend radius | Per cable datasheet | Low-loss, semi-rigid | Fixed vs. dynamic differs |
| Vibration | Per DO-160 Section 8 | Qualified assemblies | Category by zone |
| Marking | Per programme standard | All assemblies | Wire numbers and part marking |
Typical starting points for airframe harness work. Send us the routing drawing and we will quote the set.




Send us the routing, the zones and the shield requirements, and our engineers will come back with a harness proposal.