Aerospace Sourcing
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Aerospace Manufacturing Processes Reference

A flight part is usually the product of a chain of processes: material, machining or forming, heat treatment, finishing, inspection and cleaning, each governed by its own specification. These pages explain each step the way a manufacturing engineer would brief a peer: the governing specs, the failure modes, what to call out and what paperwork to require.

How to use this section

Start with the process your part depends on most, then follow the links to the steps before and after it. Most quality escapes in aerospace supply chains happen at the handoff between processes, not inside one: a part plated before it was baked, a bore anodized without a pre-finish allowance, a stainless part passivated after it was precision cleaned. The pages are written to make those handoffs visible.

Every page lists its sources. Where a number comes from a supplier or a secondary source rather than the specification itself, the page says so. Specifications are revised often, so treat any revision letter here as a pointer and check the current issue before writing it on a drawing.

The process pages at a glance

ProcessUse it forGoverning documents covered
5-axis CNC machiningComplex prismatic and contoured parts in one setupISO 10791-6, ISO 230-2, ASME Y14.5
CNC turning and SwissRound parts, slender pins, fittings and valve componentsSAE AS8879 UNJ threads
EDM and precision grindingHardened features, sharp corners, small deep holes, tight size and formAMS 2649, SAE ARP4462
Sheet metal and weldingFormed parts, weldments, GSE structuresAWS D17.1, AMS 2680, AMS 2681, FAA AC 43.13-1B
Metal additiveLPBF and DED parts, consolidated assemblies, internal channelsNASA-STD-6030, NASA-STD-6033, ASTM F3301, F2924, F3055
Composites fabricationLaminates, sandwich panels, bonded structure, toolingCMH-17, ASTM D3171, D2344, D7028
Heat treatmentSetting strength and temper in aluminum, steel, nickel and titaniumAMS 2750, AMS 2770, AMS 2774, AMS 2759 family
Surface finishingCorrosion protection, wear surfaces, conductivity, paintMIL-PRF-8625, MIL-DTL-5541, AMS 2700, AMS 2404, MIL-PRF-23377, MIL-PRF-85285
Nondestructive testingFinding cracks, porosity and internal flawsASTM E1417, E1444, E1742, E2375, AMS-STD-2154, NAS 410, NASA-STD-5009
Precision and oxygen cleaningFluid system, oxygen service and contamination sensitive hardwareIEST-STD-CC1246, ASTM G93, MSFC-SPEC-164, KSC-C-123
Inspection and metrologyMeasuring, accepting and documenting partsASME Y14.5, AS9102, ISO 10360-2, ANSI/NCSL Z540.3, ASME B89.7.3.1

Special processes and why they get extra control

In aerospace quality systems, a special process is one whose result cannot be fully verified by inspecting the finished part. Heat treatment, plating, anodizing, chemical conversion coating, welding, NDT and composite cure all qualify. You cannot measure a part and confirm it was solution treated at the right temperature, or that a weld has no lack of fusion below the surface, or that a laminate saw its full cure. The only assurance is a controlled, qualified process with records.

That is why primes approve special process sources individually, and why many require accreditation through Nadcap, administered by the Performance Review Institute. Nadcap audits are organized by commodity, each with its own audit criteria. The ones engineers meet most often:

CommodityCriteria familyExamples of sub-scopes
Heat treatingAC7102Aluminum, carburizing, nitriding, hardness and conductivity testing
Chemical processingAC7108Anodizing, electroplating, electroless plating, conversion coating, painting, etching and etch inspection, solution analysis
Nondestructive testingAC7114Penetrant, magnetic particle, ultrasonic, radiography
WeldingWelding criteriaFusion and other joining processes, with procedure and welder qualification records

Two practical points. First, accreditation is granted by scope, so read the certificate rather than trusting a logo. Second, Nadcap does not replace your customer's approval. Many primes keep their own list of approved processors by specification, and a Nadcap accredited shop that is not on that list can still cause a rejection.

Typical process routes

Seeing a whole route makes the sequencing rules concrete. These are representative examples, not prescriptions. Your drawing, material spec and customer requirements decide the actual route.

PartRepresentative routeSequencing points
Machined 7075 aluminum fitting, anodizedCertified plate, rough machine, heat treat if not bought in final temper, finish machine, penetrant, anodize, final inspectionFinish dimensions must allow for anodize growth. Penetrant before anodize
17-4PH valve body, passivated, oxygen serviceCertified bar, rough machine, age to condition, finish machine, deburr, passivate, precision clean, double bagPassivation before precision cleaning. Burr control at cross holes
4340 high strength shaft, platedCertified bar, rough, harden and temper, grind, etch inspect for burn, magnetic particle, plate, embrittlement relief bake, final inspectionBake within the time limit after plating. MT before plating
718 LPBF manifoldQualified powder, build with witness coupons, stress relief, remove from plate, HIP, solution and age, machine interfaces, CT, flow test, cleanWitness testing per the qualified process. Powder removal verified
Welded stainless tube assemblyCertified tube, form, weld per qualified procedure, visual and radiograph per class, pressure test, clean, cap and bagWeld class sets inspection. Clean after all hot work

What to put on the purchase order

Drawings define the part. The purchase order defines how the supply chain must behave while making it. For aerospace work the PO quality clauses usually carry:

  • Specification revisions in effect, or a statement that the latest revision on the PO date applies
  • Approved source requirements for special processes, including Nadcap and any customer approval list
  • First article inspection to AS9102, and the triggers for a new or partial first article
  • Certificate requirements: material certs traceable to heat or lot, process certs per operation, and a certificate of conformance
  • Right of access for you and your customer to the supplier's facility and records
  • Notification of changes to process, location or sub-tier sources
  • Record retention period
  • Export control marking and handling requirements where applicable

Missing clauses are the reason many shops ship parts with incomplete paperwork. They were never asked for it. If your quality group has standard clauses, attach them to every order rather than relying on a general reference.

The certificate package

Each process leaves a record, and the set of records is how a part proves its pedigree. A complete package for a machined, heat treated and finished part might contain the material cert from the mill, the heat treat cert with furnace and cycle identification and hardness or conductivity results, the finish cert with spec, type, class and thickness, NDT reports with method, procedure, acceptance criteria and inspector certification, the dimensional report or AS9102 first article, and the supplier's certificate of conformance tying them together.

Check that every record names the same part number and revision, that heat or lot numbers carry through, and that dates are in a plausible order. A finish cert dated before the heat treat cert on a part that must be heat treated first is a finding. Receiving inspection practice is covered on the receiving inspection page.

What drives lead time across processes

Process steps add lead time mostly through queues, not processing hours. Each outside special process means a ship out, a queue at the processor, the process itself, the cert and a ship back. Batch processes such as heat treat and plating often wait to fill a load. Accredited processors for less common specs may be few, and their queues set your schedule. First article adds inspection and review time on the first lot.

Engineers can shorten lead time by allowing equivalent specifications where the program permits, avoiding exotic finishes on non critical surfaces, buying material already in the final temper when possible, and freezing the drawing before release so changes do not restart special process routing. For more on scheduling, see lead times and delivery.

Design choices that simplify the process chain

Many process headaches are designed in. A few habits at the drawing board remove whole steps or whole suppliers from the route:

  • Limit finishes to where they are needed. A hard anodize callout on the whole part when only one bore needs wear resistance adds masking or growth allowances everywhere else.
  • Choose materials that avoid a process. Buying plate or bar in the final temper can remove an outside heat treat step, as long as the machining does not depend on a softer condition.
  • Avoid mixing incompatible requirements on one part. A high strength steel part that also needs electroplating brings a mandatory bake and its timing limits. A different alloy or coating may avoid both.
  • Design for inspection. A weld or an internal channel that cannot be inspected forces either a more expensive method such as CT or a lower allowable.
  • State the intent in notes. If a feature is a sealing surface, a grounding point or a fatigue critical area, say so, because each changes how the supplier finishes and inspects it.

A short design review with a manufacturing engineer before release usually catches these. It costs less than a requalification after the first lot.

Materials and machines

Process choices are tied to material choices. Titanium raises alpha case and welding shielding questions, high strength steels raise hydrogen embrittlement and grinding burn, aluminum alloys differ widely in anodize response, and nickel alloys drive tool wear and EDM recast concerns. The materials section covers alloys, tempers and certification. The machines section covers machine classes, work envelopes and how to judge whether a shop can hold your part.

Controlled data and these processes

Many process sources handle export controlled drawings and models, and the process specifications themselves are usually public, but the part data often is not. ITAR and EAR controlled technical data must only reach authorized U.S. persons and authorized suppliers. If your part is controlled, read how we handle controlled programs before sending anything. Controlled data never goes through the website.

Get a process chain sourced

Most parts need more than one source: a machine shop, a heat treater, a finisher, an NDT lab and sometimes a cleaning house. Send the drawing and specs and we source the whole chain from qualified suppliers, flow down the requirements to each one, track the job, check every cert against the PO and deliver with the certificate package. A person replies within one business day, and we sign a mutual NDA before files.

In this section

Questions

What makes a process a special process?

A special process is one whose output cannot be fully verified by later inspection or test of the finished part, so the process itself must be controlled and qualified. Heat treatment, plating, anodizing, conversion coating, welding, NDT and composite cure are typical examples. Aerospace customers usually approve special process sources individually and often require Nadcap accreditation for the specific scope.

Is Nadcap accreditation enough to use a processor?

Not always. Nadcap accreditation shows the processor passed an industry audit for a defined scope, which you should read on the certificate. Many primes also keep their own approved processor lists by specification, and a part processed by an accredited shop that is not on the customer list can still be rejected. Check both before routing work.

In what order should heat treat, plating and inspection happen?

It depends on the part, but common rules are: finish machine after heat treatment when quench distortion matters, run penetrant or magnetic particle before plating or anodize, bake plated high strength steel within the specified time after plating, and passivate before precision cleaning. Your router should show the sequence explicitly and your process specs may impose additional rules.

What should a complete certificate package contain?

Typically a traceable material cert, a cert for each special process naming the spec, revision and results, NDT reports with inspector certification, a dimensional report or AS9102 first article for new parts, and a certificate of conformance tying them together. All records should show the same part number and revision, consistent heat or lot numbers and dates in a plausible order.

Why do specification revisions matter so much?

Because requirements change between revisions, and suppliers are audited to the revision they certify. A cert to a superseded revision can be rejected at receiving or during a customer audit. Either state revisions on the PO or state that the latest revision on the PO date applies, and make sure the supplier certs name the revision they used.

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