Custom Cable Assemblies & Wire Harnesses:
The Aerospace & Defense Design-to-Qualification Guide

Published: September 24, 2026 · Technical Guide

The Connector Is a Component. The Assembly Is a System.

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.

ElementWhat it decidesFailure if specified by habit
Wire & insulationCurrent, voltage, temperature, flexibility, weightInsulation cracks at a cold bend; voltage breakdown at altitude
TerminationThe contact-to-conductor jointIntermittent opens, local heating, rising contact resistance
Connector & contactsInterface, sealing, keying, mating cyclesCorrosion, water ingress, cross-mating an identical shell
Backshell & strain reliefLoad path from cable to shellConductors fatigue right behind the crimp barrel
Shield terminationEMI control and ground referenceRadiated emissions, ground loops, common-mode noise
Branching & splicesHarness topologySplice separation, abrasion at breakouts, wrong leg lengths
SealingIP rating and fluid resistanceIngress, corrosion and a short discovered after the salt fog test
Marking & documentationTraceability and build repeatabilityThe wrong harness revision installed on the aircraft

Step 1 — Choose the Wire Before the Connector

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 familyInsulationRatingWhere it belongs
AS22759 / MIL-W-22759Extruded XL-ETFE600 V, −55 °C to +200 °CThe default aerospace signal and power wire: light, tough, resistant to fuels and hydraulic fluid
MIL-W-16878/4 (Type E)PTFE600 V, −55 °C to +200 °CHigh-temperature and chemically exposed runs; stiffer, heavier, abrasion-resistant
M27500Shielded and jacketed multi-conductorSet by the component wiresEMI-controlled avionics runs where the harness itself must contain the field
MIL-DTL-3432Shielded power cable, 600 V−55 °C and upPower distribution runs where shielding and current capacity matter together
High-temperature constructionPTFE / FEP / PFA, nickel-plated copperTo +260 °C continuousEngine bays, exhaust runs and firewall passthroughs
Fire-zone constructionMineral-insulated or ceramic-beadedIntermittent excursions well above 260 °CFirewalls 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.

Step 2 — Termination: Crimp Wins, and It Is Not Close

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.

Step 3 — Backshells, Strain Relief and Shield Termination

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.

Step 4 — Routing Rules That Are Enforced After the First Failure

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:

Step 5 — Sealing and Environmental Protection

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.

Step 6 — Workmanship: Which Standard Do You Build To?

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.

StandardScopeNotes
IPC/WHMA-A-620Cable and wire harness assembly acceptanceClass 1 general, Class 2 dedicated service, Class 3 high-performance / harsh environment — the class aerospace and defense work is normally bought to
NASA-STD-8739.4Crimping, interconnecting cables, harnesses and wiringThe strictest widely referenced harness workmanship document; a useful benchmark even for non-NASA programmes
J-STD-001Soldered electrical and electronic assembliesApplies where the harness includes soldered joints rather than crimps
AS9102First article inspectionFormal FAI report on the first production unit — how a harness revision is proved before volume build
AS5553 / AS6081Counterfeit part avoidanceProducers and distributors respectively: the framework that keeps unapproved wire and contacts out of a flight harness

The Qualification Test Matrix

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.

TestWhat it provesTypical basis
Continuity / wiring verificationEvery circuit goes where the drawing says, with no opens100% of assemblies
Low-level contact resistanceContact-to-conductor joint integrity, thermally and electricallyMilliohm level, against the spec limit
Dielectric withstand (DWV / Hipot)Insulation adequacy between circuits and from circuit to shellPer the connector and wire rating
Insulation resistanceDielectric leakage does not degrade with age and humidityMegohm level at the specified test voltage
Cable pull-outThe crimp holds the wire against specification tensile loadBy wire and contact size
Contact retentionContacts stay seated under axial loadPer the connector specification
Vibration and shockNo discontinuity, no chafe, no fatigue at clamp or backshellMIL-STD-810 methods 514 / 516
Thermal cyclingSeals, boots and materials survive the full temperature rangeMIL-STD-810 method 503
Salt spray / corrosionPlating and finishes for shipboard and coastal serviceMIL-STD-810 method 509; 500 h is a common shipboard target
Fluid immersionFuel, oil, hydraulic fluid and solvent resistancePer the application fluid list

The RFQ Checklist: Ten Things to Send

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:

  1. Connector part numbers at every end, including keying variant and finish.
  2. Wire type, AWG and colour code for each circuit.
  3. A dimensional drawing with leg lengths, tolerances and branch angles — not a photograph of a hand sketch.
  4. Shield termination requirement: 360° backshell, band, or drain wire.
  5. Backshell style and exit angle, plus boot or overmold.
  6. Sealing requirement: IP class, immersion, fluid exposure.
  7. Environmental profile: temperature, vibration, altitude, salt spray.
  8. Marking and documentation: wire identification, harness label, revision, certificate of conformance.
  9. Qualification evidence required: test report, first article inspection, sample quantities.
  10. Prototype quantity and annual volume — this is what sets tooling, fixture and price.

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 Cross-Reference: Cable Assemblies and Harness Hardware

ManufacturerWhat they supplyAiroadcon equivalent
Amphenol / Amphenol AerospaceMIL-DTL-38999 and 26482 connectors, accessory hardware, built harnessesBuild-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 / DeutschDT and DTP sealed connectors, DBA, ARINC 600, Raychem wire and heat-shrink
Souriau (Eaton)851 and 8D circular connectors and European aerospace assemblies
GlenairM85049 backshells, banding systems, harness hardware and conduit
ITT CannonCircular and rectangular connectors, high-reliability contact systems
W. L. Gore / Carlisle / MarmonSpecialised high-temperature, low-loss and lightweight cable constructions
Molex / Smiths InterconnectHigh-speed and harsh-environment interconnect and cable solutions

Airoadcon Cable Assembly & Wire Harness Lines

Airoadcon builds both halves of the problem: the connectors and the finished assembly. Relevant product lines:

Frequently Asked Questions

What is the difference between a cable assembly and a wire harness?

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.

Can you build to my drawing, or do you design the harness?

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.

Which wire should I specify for an aerospace harness?

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.

What testing do you perform on a finished cable assembly?

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.

How do I cross-reference an existing cable assembly?

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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