Aerospace Sourcing
Parts: motion

Aerospace Springs: Wire Specs, Processing and Inspection

Aerospace springs are compression, extension, torsion and wave springs made to a drawing or to SAE AS24585 and AS24586, from wire bought to an AMS spec such as AMS 5112 music wire, AMS 5688 type 302 or AMS 5678 17-7 PH. Processing, set removal and a measured load at a stated height decide acceptance.

Updated

Spring types and where they are used

A spring is defined by how it is loaded. Compression springs push, extension springs pull from hooks or loops, torsion springs return a rotating arm, and wave springs give compression force in a fraction of the height. In aerospace they show up in valves and regulators, latches and access panels, connector and switch mechanisms, deployment hinges and release devices on spacecraft, and in ground support equipment.

TypeWhat it doesKey acceptance values
Helical compressionResists push along its axisFree length, load at a test height, rate, solid height
Helical extensionResists pull through end hooks or loops; can carry initial tensionLoad at extended length, initial tension, hook orientation
TorsionResists rotation of its legsTorque at angle, leg positions, wind direction
Wave (flat wire)Compression in a short axial heightLoad at work height, free height, OD and ID clearance
Constant force and BellevilleFlat strip or disc forms for special loadsPer drawing

Smalley, a wave spring maker, states that wave springs can reduce spring height by up to 50 percent compared with an ordinary coil spring for the same job, which is why they appear in tight valve and bearing preload stacks. Bearings that springs preload are covered on aerospace bearings.

The specifications that govern springs and spring wire

Most aerospace springs are made to a drawing, with the wire bought to an AMS material spec and the processing to AMS process specs. Small standard springs can be ordered to SAE AS24585 and AS24586.

DocumentWhat it coversStatus as verified
AMS 5112Carbon steel music wire, 0.70 to 1.00 C, cold drawn, spring quality, in coils, spools or cut lengthsAMS 5112N, reaffirmed June 2024 (SAE)
ASTM A228Music wire, the commercial counterpart named by spring makersCited for uncoated music wire (Lee Spring)
AMS 5688Corrosion resistant steel wire, 18Cr 9.0Ni (type 302), spring temperAMS 5688N dated June 2026 is current (SAE)
ASTM A313Stainless spring wire, commercialCited for type 302 spring wire (Lee Spring)
AMS 5678CRES wire, 17Cr 7.1Ni 1.1Al precipitation hardenable, cold drawn, spring temperAMS 5678H dated August 2026 is current (SAE)
AMS 5699Nickel alloy wire, 72Ni 15.5Cr 0.95Cb 2.5Ti 0.70Al 7.0Fe, spring temper, to 0.625 inAMS 5699H revised May 2022 (SAE)
SAE AS24585Spring, helical, compression, for loads below 20 lbAS24585E revised March 2023; formerly MS24585
SAE AS24586Spring, helical, extension, for loads below 30 lbFormerly MS24586 (Lee Spring)
AMS 2430Shot peeningAMS 2430U, April 2018 (SAE)
AMS 2432Shot peening, computer monitoredAMS 2432E, October 2022 (SAE)

One correction to a common shorthand: AMS 5699 is not a 17-7 PH spec. It covers a heat resistant nickel alloy whose composition matches the alloy usually sold as X-750, used for springs that must hold load at temperature. 17-7 PH spring wire is AMS 5678. Mixing the two up on a PO buys the wrong alloy.

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How the part number is built

Spring part numbers are rarely self-describing, because most aerospace springs are drawing numbers. Stock catalog numbers from a spring maker do encode the geometry. Lee Spring's published part number guide decodes its extension spring example LE 014 A 01 M as follows.

ElementMeaning
LESeries: standard extension springs, inch
014Wire diameter code
AOutside diameter code; groups springs with the same OD
01Free length code, shortest to longest within the series
MMaterial: music wire (S is type 302 stainless, S316 is type 316, E is Elgiloy or an equivalent cobalt alloy)

The same guide carries a footnote buyers should notice: type 302 may be substituted with type 304 at the maker's discretion. That is normal for commercial stock, and it is exactly why a catalog spring does not meet a drawing that calls AMS 5688 type 302 wire unless the maker certifies to it. For flight hardware, put the drawing or AS sheet number on the PO, not a catalog number alone.

Materials and the trade-offs

Choose spring material by temperature, corrosion environment and magnetic or fatigue needs, then let the wire spec carry the requirement.

WireStrengthsWatch for
Music wire (AMS 5112)Cold drawn carbon steel, 0.70 to 1.00 percent carbonCorrodes unprotected; Lee Spring notes zinc or cadmium coatings protect steel sacrificially until used up, and plating brings hydrogen embrittlement risk
Type 302 CRES (AMS 5688)Corrosion resistant without plating; ASTM A313 is the commercial counterpartCatalog stock may substitute 304 unless the PO forbids it
17-7 PH (AMS 5678)Coiled in condition C, then precipitation hardened to CH900The aging cycle after coiling must be run and shown on the cert
Nickel alloy (AMS 5699)Corrosion and heat resistant nickel alloy for springs that work hotSupplied precipitation hardenable, so the aging treatment after forming must be specified
Cobalt alloy (Elgiloy or equivalent)Offered by spring makers as a standard material option (Lee Spring code E)Name the exact alloy and spec on the drawing; equivalents vary

AMS 5678 describes wire drawn to condition C that is capable of being precipitation heat treated to CH900 after the spring is formed. In practice that means the coiler or a heat treater has to run the aging cycle, and the cert should show it. For background on these alloy families see stainless and specialty steels and nickel superalloys.

Stress relief, set removal and shot peening

Processing after coiling is what turns a coil of wire into a spring that holds its load. Three steps matter on aerospace drawings.

  • Stress relief. Lee Spring defines it as a low temperature heat treatment below the point where the metallurgical structure changes, used to relieve stresses from manufacturing. It stabilizes the spring before setting and finishing. For precipitation hardening wire, the aging cycle takes this place and is specified separately. See heat treatment.
  • Set removal (presetting or scragging). The spring is compressed beyond its elastic limit in the direction it will work, so it takes its permanent set at the factory instead of in service. Lee Spring notes this can only be done in the direction of the applied force. A spring that later takes set in service has lost free length and load.
  • Shot peening. Peening induces compressive residual stress in the outer fibers of the wire, improving fatigue life. Aerospace drawings call AMS 2430, or AMS 2432 when computer monitored peening is required, with intensity and coverage.

Plating needs care. Lee Spring states that plated springs must be baked immediately after plating to drive out hydrogen. High strength spring wire is exactly where hydrogen embrittlement bites, so name the plating spec, the bake and the time limit; our surface finishing page covers relief baking.

Inspection of load and rate

A spring is accepted on measured load at a stated height or length, not on rate alone. Good drawings give one or two load points with tolerances, the free length as reference, and the solid height or maximum deflection.

  • Lee Spring publishes plus or minus 10 percent on spring rate for its stock compression and extension springs and for MS24585 and MS24586 parts, and plus 5 percent with no lower limit on solid height for stock compression springs. Drawing tolerances for flight parts are usually tighter and are set by the designer.
  • For torsion springs, load is checked at a stated radius, with load equal to torque divided by radius.
  • Wave springs may take a set if compressed below their working height, so a test that bottoms them can damage them.
  • Test on a calibrated load tester, after presetting, in the direction of use, and record actual readings on the cert for each lot sampled.

For first production lots, an AS9102 first article ties each drawing characteristic, including load points, to a measured value.

Documentation and ordering checklist

  • Drawing number and revision, or AS24585 or AS24586 dash number at its revision.
  • Wire spec and condition (AMS 5112, AMS 5688, AMS 5678 with aging to CH900, AMS 5699), with mill certs and heat or lot traceability to the coiled springs.
  • Processing: stress relief or aging, set removal, shot peening to AMS 2430 or AMS 2432 with intensity, and passivation or plating by spec with the embrittlement bake.
  • Load test points, sample size and recorded results on the cert.
  • Certificate of conformance; see certificate of conformance and material certs and traceability.
  • DFARS specialty metals for DoD items; steel and nickel and cobalt alloy wire are covered. See DFARS specialty metals.
  • Packaging that prevents tangling: extension springs and small compression springs bagged or tubed by lot.

Counterfeit and quality risks, and how to receive springs

The usual failure is substitution rather than an outright fake: 304 for 302, commercial wire for AMS wire, an unpeened spring where the drawing says peened, or a missed embrittlement bake. None of these is visible. That makes traceability from wire heat to spring lot, and a source that will certify the processing, the real control. Apply SAE AS6174 counterfeit materiel controls and our counterfeit parts avoidance process to anything not bought from the maker or its authorized channel.

At receiving, check wire diameter, OD or ID, free length and end configuration, run the drawing load points on a sample, look for peening coverage where it is required, and confirm the cert lists the wire spec, heat, processing specs and load results. Hold any lot whose cert omits the bake for plated high strength springs. Our receiving inspection guide covers sampling and MRB.

How we source springs

We do not stock springs or publish prices. We source standard AS24585 and AS24586 springs through authorized channels, and we have drawing springs made by qualified spring makers with the wire, processing and test requirements flowed down, then deliver them with the maker's certs and our certificate of conformance. Springs often ride with valves, latches, GSE mechanisms and machined housings, so we can put them on one PO with those parts or kit them by assembly. For legacy springs with no current source, we can have them made to print from your drawing, as described under obsolete aerospace parts. See also bushings, spherical bearings and rod ends, the motion category and the parts index.

Get springs made or sourced

Send the drawing or AS dash numbers, quantity, wire spec, processing and load test requirements. We return a source, lead time and the document package. Request a quote for springs.

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Questions

Is AMS 5699 the spec for 17-7 PH spring wire?

No. SAE lists AMS 5699 as a corrosion and heat resistant nickel alloy wire, 72Ni 15.5Cr 0.95Cb 2.5Ti 0.70Al 7.0Fe, in spring temper up to 0.625 in, with AMS 5699H revised in May 2022. 17-7 PH spring temper wire is AMS 5678, which SAE describes as a precipitation hardenable 17Cr 7.1Ni 1.1Al corrosion resistant steel wire.

What replaced MS24585 compression springs?

SAE AS24585, titled Spring, Helical, Compression: For Loads Below 20 Pounds. SAE lists revision E dated March 2023. Lee Spring describes its MS24585 line as now designated AS24585 and the extension spring sheet MS24586 as AS24586, for loads below 30 lb. Order to the AS sheet and revision even if your drawing still says MS.

What does set removal do to a spring?

Set removal, also called presetting or scragging, compresses the spring past its elastic limit in its working direction so it takes its permanent set during manufacture. The spring then holds its free length and load in service instead of relaxing on first use. Lee Spring notes it can only be done in the direction of the applied force, so a spring preset in compression is not preset for extension.

Do plated springs need a hydrogen embrittlement bake?

High strength plated springs normally do. Lee Spring states that springs must be baked immediately after plating to drive the hydrogen out. Put the plating specification, the bake requirement and the time limit between plating and baking on the PO, and require the bake on the cert. A missing bake cannot be seen at receiving and can cause delayed cracking.

How are spring loads inspected?

On a calibrated load tester, by compressing or extending the spring to the heights or lengths on the drawing and reading the load, after the spring has been preset. Torsion springs are checked as torque at an angle, with load read at a stated radius. Record the actual values on the cert. Rate alone is not enough, because two springs with the same rate can carry different loads at the working height.

Can a catalog stainless spring replace a drawing spring?

Only with engineering approval. Catalog stock may use a different wire spec, and Lee Spring's own part number guide says type 302 may be substituted with type 304 at its discretion. If your drawing calls AMS 5688 type 302, peening or a specific load tolerance, a catalog spring will not carry that certification unless the maker agrees to supply it.

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