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
| Process | Use it for | Governing documents covered |
|---|---|---|
| 5-axis CNC machining | Complex prismatic and contoured parts in one setup | ISO 10791-6, ISO 230-2, ASME Y14.5 |
| CNC turning and Swiss | Round parts, slender pins, fittings and valve components | SAE AS8879 UNJ threads |
| EDM and precision grinding | Hardened features, sharp corners, small deep holes, tight size and form | AMS 2649, SAE ARP4462 |
| Sheet metal and welding | Formed parts, weldments, GSE structures | AWS D17.1, AMS 2680, AMS 2681, FAA AC 43.13-1B |
| Metal additive | LPBF and DED parts, consolidated assemblies, internal channels | NASA-STD-6030, NASA-STD-6033, ASTM F3301, F2924, F3055 |
| Composites fabrication | Laminates, sandwich panels, bonded structure, tooling | CMH-17, ASTM D3171, D2344, D7028 |
| Heat treatment | Setting strength and temper in aluminum, steel, nickel and titanium | AMS 2750, AMS 2770, AMS 2774, AMS 2759 family |
| Surface finishing | Corrosion protection, wear surfaces, conductivity, paint | MIL-PRF-8625, MIL-DTL-5541, AMS 2700, AMS 2404, MIL-PRF-23377, MIL-PRF-85285 |
| Nondestructive testing | Finding cracks, porosity and internal flaws | ASTM E1417, E1444, E1742, E2375, AMS-STD-2154, NAS 410, NASA-STD-5009 |
| Precision and oxygen cleaning | Fluid system, oxygen service and contamination sensitive hardware | IEST-STD-CC1246, ASTM G93, MSFC-SPEC-164, KSC-C-123 |
| Inspection and metrology | Measuring, accepting and documenting parts | ASME 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:
| Commodity | Criteria family | Examples of sub-scopes |
|---|---|---|
| Heat treating | AC7102 | Aluminum, carburizing, nitriding, hardness and conductivity testing |
| Chemical processing | AC7108 | Anodizing, electroplating, electroless plating, conversion coating, painting, etching and etch inspection, solution analysis |
| Nondestructive testing | AC7114 | Penetrant, magnetic particle, ultrasonic, radiography |
| Welding | Welding criteria | Fusion 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.
| Part | Representative route | Sequencing points |
|---|---|---|
| Machined 7075 aluminum fitting, anodized | Certified plate, rough machine, heat treat if not bought in final temper, finish machine, penetrant, anodize, final inspection | Finish dimensions must allow for anodize growth. Penetrant before anodize |
| 17-4PH valve body, passivated, oxygen service | Certified bar, rough machine, age to condition, finish machine, deburr, passivate, precision clean, double bag | Passivation before precision cleaning. Burr control at cross holes |
| 4340 high strength shaft, plated | Certified bar, rough, harden and temper, grind, etch inspect for burn, magnetic particle, plate, embrittlement relief bake, final inspection | Bake within the time limit after plating. MT before plating |
| 718 LPBF manifold | Qualified powder, build with witness coupons, stress relief, remove from plate, HIP, solution and age, machine interfaces, CT, flow test, clean | Witness testing per the qualified process. Powder removal verified |
| Welded stainless tube assembly | Certified tube, form, weld per qualified procedure, visual and radiograph per class, pressure test, clean, cap and bag | Weld 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.
Related
Sources
- Performance Review Institute: Nadcap
- JAQG: Nadcap audit criteria list
- ASME: Y14.5 Dimensioning and Tolerancing
- Ideagen: AS9102 Rev C template and guide
- AWS Welding Digest: aerospace welding specifications
- NASA: NASA-STD-6030 Additive Manufacturing Requirements for Spaceflight Systems
- SAE: AMS 2759/9E hydrogen embrittlement relief baking
- NASA Technical Standards: MSFC-SPEC-164 Rev E
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