Published: September 24, 2026 · Technical Guide
A cable assembly is where the electrical design stops being an abstraction and becomes a physical part that has to survive a temperature swing, a vibration profile, a salt fog chamber and a technician installing it in the dark. Buyers who specify the connector carefully and leave the assembly to chance are the ones who find intermittent opens at the crimp, chafed insulation at the clamp, and a shield that terminates through a drain wire long enough to be an antenna.
Every cable assembly is the same eight decisions in a different order. Get them wrong and the failure shows up somewhere else entirely — which is why the troubleshooting starts at the connector and the root cause is usually in the harness.
| Element | What it decides | Failure if specified by habit |
|---|---|---|
| Wire & insulation | Current, voltage, temperature, flexibility, weight | Insulation cracks at a cold bend; voltage breakdown at altitude |
| Termination | The contact-to-conductor joint | Intermittent opens, local heating, rising contact resistance |
| Connector & contacts | Interface, sealing, keying, mating cycles | Corrosion, water ingress, cross-mating an identical shell |
| Backshell & strain relief | Load path from cable to shell | Conductors fatigue right behind the crimp barrel |
| Shield termination | EMI control and ground reference | Radiated emissions, ground loops, common-mode noise |
| Branching & splices | Harness topology | Splice separation, abrasion at breakouts, wrong leg lengths |
| Sealing | IP rating and fluid resistance | Ingress, corrosion and a short discovered after the salt fog test |
| Marking & documentation | Traceability and build repeatability | The wrong harness revision installed on the aircraft |
Wire specification drives the contact size, the backshell, the bend radius and the price. In aerospace and defense work the choice is almost always a member of a small, well-defined family.
| Wire family | Insulation | Rating | Where it belongs |
|---|---|---|---|
| AS22759 / MIL-W-22759 | Extruded XL-ETFE | 600 V, −55 °C to +200 °C | The default aerospace signal and power wire: light, tough, resistant to fuels and hydraulic fluid |
| MIL-W-16878/4 (Type E) | PTFE | 600 V, −55 °C to +200 °C | High-temperature and chemically exposed runs; stiffer, heavier, abrasion-resistant |
| M27500 | Shielded and jacketed multi-conductor | Set by the component wires | EMI-controlled avionics runs where the harness itself must contain the field |
| MIL-DTL-3432 | Shielded power cable, 600 V | −55 °C and up | Power distribution runs where shielding and current capacity matter together |
| High-temperature construction | PTFE / FEP / PFA, nickel-plated copper | To +260 °C continuous | Engine bays, exhaust runs and firewall passthroughs |
| Fire-zone construction | Mineral-insulated or ceramic-beaded | Intermittent excursions well above 260 °C | Firewalls and fire zones where the circuit must keep working during an event |
Two rules survive every programme. First, the wire temperature rating must exceed the hottest steady-state ambient at the harness, not the ambient of the compartment it starts in. Second, size the conductor for the current at the worst-case bundled condition and altitude — a wire that is comfortable alone in free air is not comfortable in a 40-conductor bundle at 55,000 ft. Bundle derating, altitude derating and connector contact rating are three separate limits, and the lowest one governs.
Crimp termination dominates aerospace harness work because it is the only method that is simultaneously repeatable, inspectable and heat-free. A calibrated crimp tool with the correct positioner produces a defined deformation of the barrel into the conductor strands — a cold weld at the strand level — and the result can be verified by a pull test and by micro-section on a sample.
The two workmanship defects that end up in the field are a crimp made with the wrong positioner (looks correct, tests intermittently) and a stripped length that puts the insulation either inside the barrel or too far from it. Both are caught by inspection — which means the inspection criteria must be written into the drawing, not left to the operator's judgement.
The backshell is what makes the difference between a harness that lasts the life of the platform and one that fails at the connector. It does three jobs: it anchors the cable so no tensile load reaches the crimps, it provides the environmental seal at the rear of the connector, and it is the ground path that terminates the shield.
Bend radius is a specification, not a preference. General practice for a bundled harness is a minimum bend radius of roughly six times the bundle outside diameter, and shielded or coaxial cable typically sits at the higher end of the six-to-ten-times range because a tight bend distorts the dielectric and changes the impedance. Always confirm against the cable's own specification — and remember the bend starts at the backshell, so the accessory and the clamp spacing set the real limit.
Wiring in an aerospace vehicle is governed by a vehicle wiring standard — in the civil world, SAE AS50881, formerly MIL-W-5088. The parts of it that cause real harness problems are the boring ones:
Sealing happens at three levels and all three have to work: the contact and interfacial seal inside the connector, the rear seal at the backshell or boot, and the jacket or overmold that keeps the bundle dry along its length. A sealed connector on an unsealed bundle simply moves the ingress point 200 mm down the harness.
For off-highway, marine and engine-compartment work, an IP67/IP68 sealed harness combines grommeted connectors, adhesive-lined boots and a jacket that resists fuel, oil, hydraulic fluid and salt water. Where the harness enters a pressurised or potted assembly, the transition is potted rather than taped — a taped transition is a wicking path.
Harness quality is defined by a workmanship standard, and the class you build to is a commercial decision that should appear on the purchase order.
| Standard | Scope | Notes |
|---|---|---|
| IPC/WHMA-A-620 | Cable and wire harness assembly acceptance | Class 1 general, Class 2 dedicated service, Class 3 high-performance / harsh environment — the class aerospace and defense work is normally bought to |
| NASA-STD-8739.4 | Crimping, interconnecting cables, harnesses and wiring | The strictest widely referenced harness workmanship document; a useful benchmark even for non-NASA programmes |
| J-STD-001 | Soldered electrical and electronic assemblies | Applies where the harness includes soldered joints rather than crimps |
| AS9102 | First article inspection | Formal FAI report on the first production unit — how a harness revision is proved before volume build |
| AS5553 / AS6081 | Counterfeit part avoidance | Producers and distributors respectively: the framework that keeps unapproved wire and contacts out of a flight harness |
A cable assembly is qualified before it is shipped, and the tests map directly onto the failure modes above. Not every programme needs every row — but the first four are the ones that should never be waived.
| Test | What it proves | Typical basis |
|---|---|---|
| Continuity / wiring verification | Every circuit goes where the drawing says, with no opens | 100% of assemblies |
| Low-level contact resistance | Contact-to-conductor joint integrity, thermally and electrically | Milliohm level, against the spec limit |
| Dielectric withstand (DWV / Hipot) | Insulation adequacy between circuits and from circuit to shell | Per the connector and wire rating |
| Insulation resistance | Dielectric leakage does not degrade with age and humidity | Megohm level at the specified test voltage |
| Cable pull-out | The crimp holds the wire against specification tensile load | By wire and contact size |
| Contact retention | Contacts stay seated under axial load | Per the connector specification |
| Vibration and shock | No discontinuity, no chafe, no fatigue at clamp or backshell | MIL-STD-810 methods 514 / 516 |
| Thermal cycling | Seals, boots and materials survive the full temperature range | MIL-STD-810 method 503 |
| Salt spray / corrosion | Plating and finishes for shipboard and coastal service | MIL-STD-810 method 509; 500 h is a common shipboard target |
| Fluid immersion | Fuel, oil, hydraulic fluid and solvent resistance | Per the application fluid list |
An RFQ for a custom cable assembly is answered in a day or turns into three weeks of questions. These ten inputs make the difference:
An experienced harness house will run a design-for-manufacture review on that package and come back with the three or four places where the drawing will make the part expensive or unreliable: a bend radius that is not achievable at the backshell, a shield termination that cannot be banded at that diameter, a splice buried where it cannot be inspected.
| Manufacturer | What they supply | Airoadcon equivalent |
|---|---|---|
| Amphenol / Amphenol Aerospace | MIL-DTL-38999 and 26482 connectors, accessory hardware, built harnesses | Build-to-print cable assemblies on Airoadcon J599 circular connectors, ZH83723 bayonet, marine and subsea connectors, plus M85049 backshells and full harness assembly (engine, high-temperature, sealed IP67/IP68, 400 Hz ground power, bomb-borne, RF and measurement). Send the drawing or the incumbent part numbers for a cross-reference and quote. |
| TE Connectivity / Deutsch | DT and DTP sealed connectors, DBA, ARINC 600, Raychem wire and heat-shrink | |
| Souriau (Eaton) | 851 and 8D circular connectors and European aerospace assemblies | |
| Glenair | M85049 backshells, banding systems, harness hardware and conduit | |
| ITT Cannon | Circular and rectangular connectors, high-reliability contact systems | |
| W. L. Gore / Carlisle / Marmon | Specialised high-temperature, low-loss and lightweight cable constructions | |
| Molex / Smiths Interconnect | High-speed and harsh-environment interconnect and cable solutions |
Airoadcon builds both halves of the problem: the connectors and the finished assembly. Relevant product lines:
A cable assembly is a length of cable terminated with connectors at one or both ends to a defined electrical performance; a wire harness is a branched bundle with multiple legs, breakouts and often several different connector types. In practice the two overlap — a harness is a cable assembly with a topology. The distinction matters commercially because a branched harness with breakouts and splices is a more complex build than a single-leg assembly, and it needs a dimensional drawing rather than just a length and two part numbers.
Both. Build-to-print is the normal route: send the connector part numbers, wire schedule, dimensional drawing and qualification requirements and the assembly is built and tested to that package. Where the harness is not yet designed, the same inputs plus the routing envelope and environmental profile are enough to produce a drawing for approval, including a design-for-manufacture review that flags the bend radii, shield terminations and splice locations that would make the part unreliable.
Start with an AS22759 / MIL-W-22759 XL-ETFE wire — 600 V, rated to +200 °C, lightweight and resistant to fuels and hydraulic fluid. Move to PTFE (MIL-W-16878/4) where temperature or chemical exposure is more severe, to M27500 shielded and jacketed multi-conductor cable where the harness itself has to contain EMI, and to mineral-insulated or ceramic-beaded construction inside a fire zone. Then check the connector contact rating and derate the bundle for current, altitude and ambient temperature.
100 % continuity and wiring verification, low-level contact resistance, dielectric withstand (DWV / Hipot) and insulation resistance on every assembly. Sample-based or type testing then covers cable pull-out, contact retention, vibration and shock, thermal cycling, salt spray and fluid immersion, with first article inspection to AS9102 on the first production unit where the programme requires it.
Send the incumbent assembly or connector part numbers, the wire schedule, the drawing (or the routing envelope if there is no drawing) and the qualification requirements. Airoadcon maps Amphenol, TE / Deutsch, Souriau, Glenair, ITT Cannon, Gore and Carlisle hardware onto the equivalent J599 circular, ZH83723 bayonet, marine or subsea connector and the matching M85049 accessory, then quotes the assembly with its test report.
Need a custom cable assembly or wire harness built to your drawing?
Airoadcon assembles J599 circular, ZH83723 bayonet, marine and subsea connectors into qualified harnesses — engine and firewall cable, high-temperature construction to +260 °C, sealed IP67/IP68 harnesses, 400 Hz ground power, RF assemblies and bomb-borne leads. Send the drawing, the wire schedule and the qualification requirements — we return a cross-reference, a design-for-manufacture review and a quote with the test plan.
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