Aerospace fabrication guide
A practical guide for engineers and buyers: AS9100 discipline, traceability and documentation basics, RFQ prep, and how to align tolerances + inspection for repeatable acceptance.
What aerospace buyers are really trying to prevent
In aerospace work, the expensive failures usually happen after the part is "done": it doesn’t assemble, it can’t be verified cleanly, or the documentation package doesn’t match the acceptance expectation. The fix is rarely “machine harder.” It’s alignment: drawing intent, datum strategy, process path, and inspection method all match the same functional reality.
Table of contents
- RFQ package checklist (what to send)
- AS9100 discipline (what it changes)
- Tolerances, datums, and inspection intent
- Materials and finish notes
- Supplier selection cues (engineer-first)
RFQ package checklist (quote-ready)
If you want a quote that matches acceptance intent, don’t force the shop to guess. Send:
- PDF drawing + CAD (STEP preferred), current revision identifier
- Which file controls (drawing vs model) and any conflict resolution note
- Material and condition (if known), quantity, and must-hit date
- Critical-to-function features highlighted (fits, bores, patterns, sealing faces)
- Inspection/reporting expectations (first article, dimensional report, objective evidence)
- Finish requirements and any masking/handling/packaging constraints
For printable internal assets, use: precision machining guide (PDF), buyer checklist (PDF), and CAD prep guide (PDF).
AS9100 discipline (what it changes)
AS9100 is not “a sticker.” In practical terms, it reinforces the habits that prevent aerospace rework: controlled revisions, documentation discipline, and consistent process control. If your RFQ includes traceability, reporting, or objective evidence, it helps to state those requirements early so the quote assumptions match.
See the overview at /as9100-certified-fabrication.
Tolerances, datums, and inspection intent
In aerospace work, tolerances are only valuable if they can be verified. The fastest way to reduce risk is to align datum strategy to the functional assembly reference, then focus tight tolerances only on the interfaces that control fit and performance.
- Don’t tighten everything: tighten the few interfaces that drive function.
- Call out intent: if a dimension is critical, highlight it and include any measurement expectations.
- Qualify extreme requirements: tolerances like ± .0001 should be tied to a measurable acceptance method.
Deep dive: ultimate tolerance guide.
Materials and finish notes
Material and finish requirements frequently drive feasibility and schedule. Include the exact alloy and condition if known, and identify any surfaces that are functional (sealing faces, bearing fits, sliding interfaces).
- Specify the alloy and any acceptable alternates
- Note any heat, corrosion, or environment constraints
- Call out functional surfaces and acceptable surface finish ranges
Materials reference: materials guide.
Supplier selection cues (engineer-first)
If you want to choose a supplier faster during RFQs, look for evidence of alignment—not just capability claims.
- They ask targeted questions about datums, critical interfaces, and verification.
- Quote assumptions are explicit (material, finish, inspection/reporting, acceptance intent).
- They can explain the process path in plain, technical language.
- They can show relevant examples written as measurable outcomes.
Proof pages: case studies and gallery.
Aerospace Fabrication Guide FAQ
Do I need AS9100 for aerospace parts?
Not every aerospace-adjacent part has the same quality and documentation requirements. If your RFQ includes flow-down requirements, traceability, objective evidence, or inspection reporting, an AS9100-certified process discipline can help align expectations and reduce ambiguity. The best approach is to include your exact requirements up front so feasibility and acceptance are clear before quoting.
What should I send for an accurate aerospace fabrication / machining quote?
Send the current revision drawing (PDF) plus CAD (STEP preferred), target material and condition (if known), quantity, must-hit date, and highlight critical-to-function interfaces. Include any inspection/reporting needs (first article, dimensional report, objective evidence) and any special handling/packaging constraints.
How do I avoid tolerance-driven rework in assemblies?
Identify the few interfaces that truly drive fit and function, then align the datum strategy and inspection intent to those interfaces. Avoid tightening every dimension “just in case.” Tight tolerances should be qualified requirements with a measurable acceptance method.
Want an aerospace-ready quote review?
Send PDF + STEP, include material, quantity, must-hit date, and highlight fit-critical interfaces plus any inspection/reporting requirements. We’ll respond with clear assumptions and next steps.