The best splice is the one you never make. NASA-STD-8739.4A puts it plainly: the simplest, most reliable wiring is one continuous, unbroken conductor from point to point.1 The FAA's advice is shorter: keep splicing to a minimum.2 But sometimes splice happens (see what I did there) harnesses get repaired, wires get extended, or a small wire has to grow to fit a large contact barrel or any other reason you may not have a choice. Some of those are among the cases where a splice is specifically allowed.3

So when you do splice, you're making two decisions. The first is which kind of splice will meet your requirements. The second is whether the conductor going into it is the right size for it, and that comes down to circular mil area (CMA). Splicing is one of the easiest design concepts to mess up.

The five kinds of splice

On aerospace and military harnesses you'll run into five main types. When dealing with purely commercial harness designs there are many more options. For the purposes of our conversation we are going to stay in the mil/aero design space:

Butt splice: crimped, then sealed

SAE AS81824 covers environment-resistant crimp splices: a metal crimp barrel inside a heat-shrink sleeve, with a hot melt adhesive sealing ring at each end (Figure 1). This hot melt is to create an environmental seal around the splice. The wires go in from opposite ends until the conductor ends meet near the center. Each half of the barrel is crimped with the tool and setting for that splice size. Then you heat the sleeve: it shrinks, and the rings melt onto the insulation and seal both ends.

The parts you'll see most are M81824/1-1, M81824/1-2 and M81824/1-3, the three sizes on the AS81824/1 sheet.4 Each size takes its own range of conductor, and that range is what you check your CMA total against.

A schematic section through a heat-shrink butt splice: two wires in a metal crimp barrel inside a sleeve with a sealing ring or hot melt adhesive at each end; then the same splice crimped on each side of the center, with the sleeve shrunk and the rings melted onto the insulation. Example parts: M81824/1-1, /1-2 and /1-3. Two small sketches show it joining one wire to one wire, and two wires to one

A self-insulated splice is the strongly preferred choice, as an environmentally sealed splice is the reliable way to join conductors in areas exposed to severe wind and moisture, the FAA's SWAMP areas.5 As well the sleeving helps to provide bend and strain releif to the joint itself.

Pluses

Minuses

Solder sleeve: solder, insulation and seal in one heat

A solder sleeve is a heat-shrink sleeve with a ring of fluxed solder in the middle and a meltable sealing ring at each end (Figure 2). One heating does everything: the solder melts and flows over the conductors, the sleeve shrinks, and the rings seal onto the insulation.

Without a lead, the sleeve joins wires. The stripped conductors lie side by side under the solder ring. Solder-style splices are mainly meant for one conductor to one conductor, but they can take more if the splice is sized for all of them.9

With a lead, the sleeve picks the ground off a cable shield. You strip a band of the jacket, slide the sleeve over the exposed braid and heat it. The lead is soldered to the braid without cutting the shield, and it runs on to a ground pin in the connector, a ground stud, or the banding porch of a backshell. That lead is the pick-off. When several shields are grounded together, keep it to no more than four conductors plus a drain wire in one splice.11 The Mill-Spec component comes with a red ink over the solder rind, when the splice is heated properly this red ink will disappear. This eleminates the need for in-process inspections of a solder joint.

The mil-spec part is SAE AS83519, and it's written as a shield termination.12 Its /1 sheet (M83519/1-1 to /1-5) has no lead, so a ground wire is laid in against the braid before heating;13 its /2 sheet (for example M83519/2-1) comes with the lead (pick off wire) already installed. This is helpful when daisy chaining shields or creating a one to two splice.

Left: a solder sleeve joining two wires, their conductors overlapping under a solder ring, before and after heating. Right: an M83519/2 type solder sleeve with a pre-installed pick-off lead over a band of exposed shield braid on a shielded cable, before and after heating; the lead runs on to a ground pin or stud while the inner wires run on to the connector contacts

Pluses

Minuses

Parallel crimp splice: one barrel, wires side by side

A parallel crimp splice is a plain metal barrel. In this authors opinion, this is the strongest mechanical connection. Because all the conductors are overlaped they create a cross section that is larger than any other conductor in the same path. If the wire gauges are large enough you can literally hang by one of these splices. The wires lie on top of one another in it, not end to end, and one crimp holds them all (Figure 3).

In the end type, or pigtail, every wire comes in from the same end and the closed end is capped. NASA's standard covers both forms as crimp ferrule splices: the barrel is sized from the maker's data, and they're usually crimped with a two-indenter tool instead of the usual four.20

For both applications, this splice type is not electrically isolated in any way. To properly use a splice like this, the designer has to include heat shrink or some other covering in the design to isolate the connection. The recomendation is to use adhesive lined heat shrink in high reliability applications.

There's no mil-spec number to quote for these. They're commercial parts, and their part number and wire range are determined by the manufacture. However these components are used widely over military and aerospace equipment.

Left: a parallel crimp splice, two wires entering one end of a barrel and one the other, their conductors lying side by side, then crimped once and covered with an insulating sleeve. Right: an end-type splice, three wires entering a closed-end barrel from the same end, crimped and capped

Pluses

Minuses

Shield splice: join the wires, then the shield

Splicing a shielded cable means splicing two things: the conductors, and the shield around them (Figure 4). These are used in applications where a conductor in a twisted shielded set need to be spliced. This is probably the least preferred of all the splice options. First, remove the jacket and cut the conductors at staggered points. Next, join each conductor with its own butt splice, such as an M81824/1, offset along the cable so the splices don't sit side by side. Then lay a jumper braid across the gap between the two cut shields and bond it to each one with a solder sleeve. Finally, an outer heat-shrink sleeve covers the whole repair, from jacket to jacket.

Not only is this a sub-par solution for maintaining shielding across a shielded set. It is also difficult to install, the shielding is sub-par, and introduces many opportunities for failure. However there are cases where this is the only option. Splices like this should only be installed in sections of a harness that have no bends and is not required to flex.

Four steps on a shielded two-wire cable: jacket removed and conductors cut staggered; each conductor joined with its own M81824/1 type butt splice, offset along the cable; a jumper braid across the gap between the two shields, bonded to each with a solder sleeve; and an outer sleeve over the whole repair

Pluses

Minuses

Hand-soldered splice: lap, lash and Western Union

A hand-soldered splice needs nothing but wire, solder and sleeving, so there's no part number to call out. This is the oldest form of a wire splice making it the most well tested and the one with the most room for improvment, NASA's standard gives three forms (Figure 5):

The sleeving has to cover the splice and run onto the insulation by at least twice the diameter of the largest wire.25 When creating this kind of splice it is strongly recommended to use adhesive lined heat shrink to make the area as rigid as possible. Bending and strain is the enemy of hand soldered splices. However a properly done solder splice can be mechanically stronger than than the conductors themselves.

Three hand-soldered splices, each shown with its tinned conductors assembled and then soldered and sleeved: the lap splice, conductors side by side; the lash splice, a lap splice bound with fine solid wire; and the Western Union splice, each conductor wrapped round the other

Pluses

Minuses

Side by side

SpliceJoined bySealedSizeToolsSpec or example parts
Butt spliceCrimpYesLargest of the sealed splicesCrimp tool and the setting for each sizeSAE AS81824 (M81824/1-1 to /1-3)
Solder sleeveSolder, one heatingYesSmallestHeat toolSAE AS83519 (/1 no lead, /2 with lead)
Parallel crimp spliceOne crimp, all wiresNoShortCrimp tool, often two-indenterCommercial: maker's data
Shield spliceCrimp, plus solder sleeves on the braidYesLongestCrimp tool and heat toolBuilt from the splices above
Hand-solderedSolderOnly with sleevingSmall (lap) to bulky (Western Union)Iron and solderNASA-STD-8739.4A forms

Circular mil area

Wire gauge is a label, and labels don't add up: two 22 AWG wires are not a 20 AWG wire. What adds up is conductor area, and wiring measures it in circular mils.

One circular mil (CM) is the area of a circle 1 mil, one thousandths of an inch (0.001 in) across. Measured that way, the area of any round conductor is simply its diameter in mils, squared:

CMA = d², with d in mils (one thousandths of an inch).

There's no π to carry around, which is the whole point of the unit. If you need ordinary units, 1 CM is 0.7854 square mil, or 0.000507 mm².

A stranded conductor isn't one circle. It's a bundle of small ones with gaps between them, so you measure the strands, not the outside of the bundle:

CMA = number of strands × (strand diameter in mils)²

Take aerospace 22 AWG wire, which is usually 19 strands of 34 AWG. A 34 AWG strand is 6.3 mil across, so each strand is 6.3² = 39.7 CM, and the wire is 19 × 39.7 = 754 CM (Figure 6). Solid 22 AWG wire is about 642 CM,27 so a stranded "22 AWG" isn't the same area as a solid one. Stranded gauges are nominal sizes.

Adding it up

  1. For each wire going into the splice, find its stranding (strand count and strand gauge) on the wire's spec sheet.
  2. Square the strand diameter in mils and multiply by the strand count. That's the wire's CMA.
  3. Add up the wires that share a barrel. In a butt splice each end is its own barrel, so total each end separately. In a parallel splice, every wire shares the one barrel.
  4. Compare the total with the barrel's range on the splice's spec sheet or the maker's data.

NASA's standard adds a margin on top. It multiplies the sum of the CMAs by 1.25 and calls the result the equivalent wire size, or EWS.8 The barrel is then sized to the EWS, or to the next larger size if the EWS falls between sizes.28

Three panels: a circle 1 mil across inside a 1-mil square, one circular mil; a 22 AWG conductor of 19 strands, each 6.3 mil across and 39.7 circular mils, 754 in all; and two 22 AWG wires going into one end of a splice, 754 plus 754 equals 1508 circular mils, compared in bars with one 20 AWG wire (1216), one 18 AWG wire (1900) and NASA's equivalent wire size, 1508 times 1.25 equals 1885

Here's the same arithmetic for the usual aerospace strandings, the 19- and 37-strand constructions the SAE AS22759 wire sheets use. The strand diameters are the nominal AWG sizes, rounded to 0.1 mil the way wire tables print them.27

Wire size
(AWG)
StrandingStrand
diameter (mil)
CMA
2619 × 38 AWG4.0304
2419 × 36 AWG5.0475
2219 × 34 AWG6.3754
2019 × 32 AWG8.01,216
1819 × 30 AWG10.01,900
1619 × 29 AWG11.32,426
1419 × 27 AWG14.23,831
1237 × 28 AWG12.65,874
1037 × 26 AWG15.99,354

Two worked examples:

Either way, the end with fewer wires has to fit the same barrel. A barrel sized for the crowded end can be too big for a single wire on the other end, so check both ends against the range.

Why the total matters: too little or too much

A crimp works by squeezing the barrel and the strands together at the indents until they cold-work into one solid mass, with no gaps for air or moisture to get into. That only happens when the amount of conductor matches the barrel (Figure 7).

Three crimps, each as a cross-section through the indents and a side view with the crimp area marked: with too little conductor the indents close on loose strands with gaps between them and the wire pulls out; with conductor in the barrel's range the strands are pressed together into one solid mass; with too much conductor the barrel cracks at an indent and strands end up outside the barrel

Too little conductor

Too much conductor

Both failures can pass a continuity check on the bench. The arithmetic takes a minute, and the failure can take years to show up.

Before you splice

Wherever the splice goes, a few rules apply:

References

  1. NASA-STD-8739.4A with Change 1 (2016), Workmanship Standard for Crimping, Interconnecting Cables, Harnesses, and Wiring, paragraph 7.2.32, p.24. ↩︎
  2. FAA Advisory Circular AC 43.13-1B with Change 1, Acceptable Methods, Techniques, and Practices: Aircraft Inspection and Repair, paragraph 11-167a, p.11-65. ↩︎
  3. AC 43.13-1B, paragraph 11-167c, p.11-65. ↩︎
  4. DLA Qualified Products Database (QPD), QPL-81824 part listing for M81824/1, checked 2026-10-25. ↩︎
  5. AC 43.13-1B, paragraph 11-167b, p.11-65. ↩︎
  6. AC 43.13-1B, paragraph 11-178, pp.11-69 and 11-70. ↩︎
  7. SAE AS81824, Splices, Electric, Permanent, Crimp Style, Copper, Insulated, Environment Resistant: scope. ↩︎
  8. NASA-STD-8739.4A, paragraph 19.12.1c, p.77. ↩︎
  9. NASA-STD-8739.4A, paragraph 19.3, p.68. ↩︎
  10. NASA-STD-8739.4A, paragraph 7.2.36, p.25. ↩︎
  11. NASA-STD-8739.4A, paragraph 11.3.2, p.46. ↩︎
  12. QPD, QPL-83519 (SAE AS83519, Shield Termination, Solder Style, Insulated, Heat-Shrinkable, Environment Resistant) part listings for M83519/1 and M83519/2, checked 2026-10-25. ↩︎
  13. NASA-STD-8739.4A, Figure 11-2, Example of Individual Shield Termination Using a Heat Shrinkable Solder Sleeve. ↩︎
  14. NASA-STD-8739.4A, paragraph 19.6.1c, pp.70-71. ↩︎
  15. NASA-STD-8739.4A, paragraph 7.2.41, p.25. ↩︎
  16. NASA-STD-8739.4A, paragraph 19.6.1b, p.70. ↩︎
  17. NASA-STD-8739.4A, paragraph 7.2.39, p.25. ↩︎
  18. NASA-STD-8739.4A, paragraph 7.2.40, p.25. ↩︎
  19. AC 43.13-1B, paragraph 11-77b(3), p.11-36. ↩︎
  20. NASA-STD-8739.4A, paragraphs 19.11 and 19.11.1b, with its note, p.75. ↩︎
  21. AC 43.13-1B, paragraph 11-167, p.11-65. ↩︎
  22. NASA-STD-8739.4A, paragraph 19.4.1, pp.68-69. ↩︎
  23. NASA-STD-8739.4A, paragraph 19.5.1, pp.69-70. ↩︎
  24. NASA-STD-8739.4A, paragraph 19.7.1, p.71. ↩︎
  25. NASA-STD-8739.4A, paragraph 19.2.6, p.67. ↩︎
  26. NASA-STD-8739.4A, paragraphs 19.2.2, 19.2.3 and 19.2.4, p.67. ↩︎
  27. ASTM B258, Standard Specification for Standard Nominal Diameters and Cross-Sectional Areas of AWG Sizes of Solid Round Wires Used as Electrical Conductors. ↩︎
  28. NASA-STD-8739.4A, paragraph 19.9.1c, p.74. ↩︎
  29. NASA-STD-8739.4A, paragraph 19.12.1a, p.76. ↩︎
  30. AC 43.13-1B, paragraph 11-167d, p.11-65; NASA-STD-8739.4A, paragraph 7.2.35, p.25. ↩︎
  31. AC 43.13-1B, paragraphs 11-167e and 11-167f, p.11-65. ↩︎
  32. NASA-STD-8739.4A, paragraph 7.2.37, p.25. ↩︎
  33. NASA-STD-8739.4A, paragraph 7.2.38, p.25. ↩︎