A working guide to the metals, the standards, and the choices that change zone to zone in aerospace fastening. Written for both engineers and buyers in aviation.
Key Takeaways:
No fastener in the general industry takes the punishment an aircraft hands out. Vibration, swinging temperatures, fatigue, all arriving together. Built for exactly this, fasteners and aerospace hold their grip through every hour the airframe stays in the sky, keeping critical joints sound long after assembly is done.
Getting fasteners aerospace right pulls metallurgy, regulation, and tight manufacturing into one decision. General industrial fasteners can be chosen based on load capacity and cost alone. Aerospace components require a far wider evaluation. A bolt in a turbine casing faces conditions that a structurally identical bolt in a suspension assembly will never encounter.
Titanium as a Structural Choice: Take Grade 5 titanium, the Ti-6Al-4V alloy. It matches alloy steel on tensile strength and sheds roughly 40% of the weight doing it. Across thousands of fasteners, that adds up to real mass off the airframe. Bare titanium fights corrosion with no coating, which helps on parts nobody enjoys reaching twice.
High-Temperature Alloys for Engine Zones: Push past 700°C and Inconel 718 still holds, well after titanium and plain stainless have softened. A286 stainless steel manages here too, shrugging off oxidation and taking the cyclic fatigue turbine hardware lives with daily. Close to engine heat, both tend to get specified.
Stainless Steel in Airframe Sections: In the cooler stretches of an airframe, grades 304 and 316 earn their spot because corrosion resistance matters more than heat tolerance there. One catch. Bolt them against aluminium panels, and galvanic corrosion starts unless the right coating or isolation layer goes in first. That detail trips up assemblies more often than it should.
AS9100 and NADCAP in Practice: Think of AS9100 as the ground rules, process control, traceability, and risk spread across the supply chain. NADCAP drops a level lower, onto the steps that quietly decide a part, heat treatment, coating, non-destructive testing. Lose either accreditation and the risk hides itself. Aerospace OEMs walk from that, whatever the quoted price.
Standards Commonly Referenced in Procurement:
These show up again and again in fastener specs and supplier qualification:
Structural Joints: Catalogue tensile ratings tell you almost nothing on their own. What matters is the shear and tensile load path, and a joint in bending acts nothing like one in pure tension. Engineering review of joint geometry, material stack, and surface finish tolerance is standard before any fastener is finalised on a structural drawing.
Engine-Adjacent Areas: Heat, creep, and galling drive the choice this close to an engine. Run stainless thread against stainless under torque and it can cold-weld solid, seizing the joint for good. Dry-film lubricants or the right plating stop that, as long as both suit the base metal and the operating environment waiting in service.
Aerospace fastener procurement is a relationship, not a purchase order. A maker with decades of precision work behind it holds knowledge a newcomer simply cannot match yet. Full material traceability, live certification, and steady handling of non-conformance investigations mark the difference between a real aerospace supplier and a catalogue vendor. Talk to a specialist and lock down your specification before procurement starts.