🪶 MAGNESIUM

Inspecting Magnesium Parts and Castings Safely

Magnesium inspection carries a complication no other common metal does: the fines and chips are flammable, so even the inspection process (grinding samples, deburring) has safety controls baked in. Beyond that, magnesium is bought purely for lightness, which means corrosion protection and casting soundness dominate the quality plan, AZ91D die castings hide porosity, AZ31B sheet parts need their protective treatment verified, and WE43 aerospace parts demand full metallurgical scrutiny. ManufacturingBase buyers searching magnesium inspection are usually verifying corrosion protection and internal soundness on a reactive, safety-sensitive metal.

AS9100ISO 9001NADCAP

Corrosion protection verification: the make-or-break check

Magnesium is the most chemically active structural metal, and bare magnesium corrodes fast, so nearly every magnesium part depends on a protective surface treatment, and verifying that treatment is the central quality activity. The common systems are chromate conversion coatings (per older MIL specs), chrome-free conversion coatings, and anodize-type treatments. Inspection confirms coating presence, coverage, and often a salt-spray performance test per ASTM B117, since a magnesium part with a missed or thin conversion coating will corrode in weeks rather than years. Galvanic corrosion is the design-level trap that inspection has to flag. Magnesium is anodic to nearly everything, so a magnesium part bolted to steel or aluminum with the wrong fasteners or no isolation corrodes at the joint. Inspection of magnesium assemblies should verify isolation provisions (coatings, isolating washers, compatible fasteners) are present, because a perfectly coated magnesium part still fails galvanically if assembled wrong. The coating-thickness and adhesion checks mirror other coated metals but with higher stakes. For aerospace WE43 and AZ91 parts, the conversion coating spec and its verification are called out explicitly, and a NADCAP chemical-processing accreditation backs the treatment. A supplier that machines magnesium but treats corrosion protection as an afterthought is the most common path to field corrosion failures on these parts.

Casting porosity and the inspection of die-cast and sand-cast magnesium

Most magnesium parts are castings (AZ91D dominates high-pressure die casting; sand and investment casting cover larger aerospace parts), and casting porosity is the primary internal-defect concern. High-pressure die casting traps gas, producing subsurface porosity that a dimensional check never sees but that becomes a leak path or fatigue initiator when machining cuts into it. X-ray (radiographic) inspection per ASTM E155 reference radiographs is the standard for grading magnesium casting porosity against a defined acceptance class on critical parts. The machining-exposes-porosity problem hits magnesium castings hard. A die-cast AZ91D housing can gauge perfectly until a machined boss or sealing face cuts into a gas pocket, creating a leak path on a pressurized part. Inspection of machined casting features includes a visual and sometimes penetrant check (using approved, non-reactive penetrant systems) for exposed porosity on sealing and bearing surfaces. For aerospace sand and investment magnesium castings, the inspection escalates to full radiography, fluorescent penetrant for surface cracks, and sometimes dimensional layout of the casting envelope. Porosity acceptance classes are called out by zone, with critical zones (around bolt holes and high-stress regions) held tighter than non-critical areas. This zoned inspection is specialized work, and the qualified supplier base is narrower than for aluminum castings.

Alloy verification, microstructure, and the WE43 aerospace tier

The reference grades span a wide range. AZ31B is a wrought magnesium-aluminum-zinc alloy for sheet and extrusion; AZ91D is the workhorse die-casting alloy; WE43 is a magnesium-yttrium-rare-earth alloy developed for elevated-temperature aerospace and high-performance applications, with much better high-temperature strength and creep resistance. Inspection rigor tracks the grade: AZ31B and AZ91D get standard alloy and coating verification, while WE43 aerospace parts get full metallurgical scrutiny including microstructure and mechanical verification. WE43's properties depend on a solution-and-aging heat treatment that precipitates the rare-earth strengthening phases, so for aerospace WE43, hardness and microstructure verification confirm the heat treatment took, similar in spirit to aluminum and superalloy aging checks. A WE43 part machined from un-aged stock gauges fine and underperforms in strength and temperature capability. Alloy verification by spectrometry confirms the grade, important because the rare-earth content of WE43 makes it expensive and a substitution with cheaper AZ91 would be a serious escape on a part chosen for high-temperature service. Mill and foundry certs anchor the chemistry, and on aerospace work incoming verification plus full traceability to the heat is standard. WE43 is also used in bioabsorbable medical applications, where purity and microstructure control are even tighter, a specialized inspection tier that few suppliers can certify.

Frequently Asked Questions

Because magnesium is the most chemically active structural metal, and bare magnesium corrodes rapidly, so nearly every magnesium part depends on a protective surface treatment to survive. A part with a missed, thin, or damaged conversion coating can corrode visibly within weeks, regardless of how perfect its dimensions are. The common protection systems are chromate or chrome-free conversion coatings and anodize-type treatments, and inspection verifies coating presence, coverage, and performance, typically with a salt-spray test per ASTM B117 run for a specified duration against an acceptance criterion. Coating thickness and adhesion are also checked. Beyond the coating itself, inspection of magnesium assemblies must flag galvanic isolation, because magnesium is anodic to nearly every other metal and a magnesium part bolted to steel or aluminum without isolating washers, compatible fasteners, or barrier coatings corrodes aggressively at the joint even if its own surface is well coated. For aerospace AZ91 and WE43 parts, the conversion-coating spec and its verification are called out explicitly and backed by NADCAP chemical-processing accreditation. Specify the coating system, the salt-spray requirement, and the galvanic isolation provisions on the print, because corrosion is how magnesium parts most commonly fail in service.
It requires specific controls because magnesium fines, dust, and fine chips are flammable and, once ignited, burn extremely hot and are difficult to extinguish with water, which can make a magnesium fire worse. This affects the inspection process itself: grinding metallographic samples, deburring, and any operation that generates fine magnesium particles must use the right controls. These include keeping tools sharp to produce chips rather than fines, using flood coolant or wet grinding where appropriate, avoiding accumulation of dust, having Class D fire extinguishing media on hand rather than water, and proper housekeeping to prevent dust buildup. Dry machining and grinding of magnesium are done deliberately and with controls, since some coolants react with magnesium, so the choice of wet versus dry is application-specific and managed by experienced shops. For inspection labs preparing magnesium metallographic specimens, the grinding and polishing steps follow magnesium-specific procedures. The practical takeaway for buyers is to use suppliers and labs that routinely handle magnesium and have these safety procedures established, rather than a shop that occasionally machines it. On ManufacturingBase you can find suppliers experienced with magnesium specifically, which matters more for this metal than for inert materials because the safety discipline is real.
High-pressure die casting, which produces most AZ91D parts, traps gas and creates subsurface porosity that dimensional inspection never reveals but that becomes a leak path or fatigue-initiation site when machining cuts into it. The standard method is radiographic (X-ray) inspection, grading porosity against ASTM E155 reference radiographs to a defined acceptance class called out on the print, often zoned so high-stress regions like bolt-hole areas are held tighter than non-critical zones. The machining-exposes-porosity problem is acute on magnesium castings: a housing can gauge perfectly until a machined sealing face or boss cuts into a gas pocket, creating a leak on a pressurized part, so inspection of machined sealing and bearing surfaces includes a visual and sometimes penetrant check using approved non-reactive penetrant systems for exposed porosity. For aerospace sand and investment magnesium castings, inspection escalates to full radiography plus fluorescent penetrant for surface cracks and dimensional layout of the casting envelope. Specify the porosity acceptance class, the critical zones, and any sealing-surface porosity requirement on the print. Pressure parts should also get a leak or pressure test after machining to confirm no porosity path was opened. This zoned casting inspection is specialized, so use suppliers qualified for it.
WE43 is a magnesium-yttrium-rare-earth alloy developed for elevated-temperature aerospace and high-performance use, with far better high-temperature strength and creep resistance than AZ alloys, and it is expensive because of the rare-earth content. Its properties depend on a solution-and-aging heat treatment that precipitates the rare-earth strengthening phases, so inspection includes hardness and microstructure verification to confirm the heat treatment took, much like aging verification on aluminum or superalloys, because a WE43 part machined from un-aged stock gauges dimensionally fine while underperforming in strength and temperature capability. Alloy verification by spectrometry is important to confirm you actually received WE43 and not a substituted cheaper AZ alloy, which would be a serious escape on a part chosen for high-temperature service. Full traceability to the heat, mechanical-property verification via witness samples on critical parts, fluorescent penetrant for surface cracks, and the standard magnesium corrosion-protection verification all apply, backed by AS9100 and NADCAP accreditation. WE43 also appears in bioabsorbable medical implants, where purity and microstructure control are even tighter, a specialized inspection tier. For aerospace WE43, expect a full metallurgical inspection package, not just dimensional and coating checks, and confirm the supplier can certify the heat-treat condition.
Galvanic corrosion is the most common in-service magnesium assembly failure, and it is a design-and-inspection issue more than a material one. Magnesium sits at the anodic end of the galvanic series, more active than steel, aluminum, and nearly every other engineering metal, so when magnesium contacts a more noble metal in the presence of moisture, the magnesium corrodes preferentially and rapidly at the joint. Prevention requires isolating the magnesium from dissimilar metals: barrier coatings on mating surfaces, isolating washers and sleeves at fasteners, compatible fastener materials such as coated or aluminum fasteners rather than bare steel, sealants at interfaces, and drainage to prevent moisture traps. Inspection of magnesium assemblies must verify these isolation provisions are present and correct, because a perfectly conversion-coated magnesium part still fails galvanically if it is bolted directly to steel with bare steel fasteners. The print and assembly drawing should call out the fastener materials, isolation hardware, and sealants explicitly, and the inspection should confirm them as installed. For aerospace magnesium, the galvanic isolation scheme is part of the controlled configuration. Treat galvanic isolation verification as a required inspection step on any magnesium assembly that joins dissimilar metals, not an optional one.

Last updated: July 2026

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