{"id":11707,"date":"2026-06-03T17:14:03","date_gmt":"2026-06-03T09:14:03","guid":{"rendered":"https:\/\/www.cncmachiningshops.com\/?p=11707"},"modified":"2026-07-16T11:28:41","modified_gmt":"2026-07-16T03:28:41","slug":"aluminum-cnc-machined-parts","status":"publish","type":"post","link":"https:\/\/www.cncmachiningshops.com\/ru\/aluminum-cnc-machined-parts\/","title":{"rendered":"\u041a\u0430\u043a\u043e\u0439 \u0430\u043b\u044e\u043c\u0438\u043d\u0438\u0435\u0432\u044b\u0439 \u0441\u043f\u043b\u0430\u0432 \u043b\u0443\u0447\u0448\u0435 \u0432\u0441\u0435\u0433\u043e \u043f\u043e\u0434\u0445\u043e\u0434\u0438\u0442 \u0434\u043b\u044f \u043e\u0431\u0440\u0430\u0431\u043e\u0442\u0430\u043d\u043d\u044b\u0445 \u0434\u0435\u0442\u0430\u043b\u0435\u0439 CNC?"},"content":{"rendered":"
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Quick Answer:<\/strong> Aluminum is the most commonly CNC machined metal because it combines excellent machinability (cutting speeds 2\u20133\u00d7 faster than steel), sufficient mechanical strength, natural corrosion resistance, and low density (~2.7 g\/cm\u00b3 versus ~7.8 g\/cm\u00b3 for steel). The correct alloy depends on the application: 6061-T6 (tensile strength 290\u2013310 MPa) is the standard choice for approximately 70\u201380% of CNC machined parts due to its balance of strength, machinability, corrosion resistance, and consistent anodizing quality. 7075-T6 (tensile strength 500\u2013570 MPa) is selected when load is high enough to justify the 20\u201340% higher machining cost. 2024-T3 (tensile strength 440\u2013470 MPa) is used for fatigue-dominated aerospace applications. 5052-H32 (tensile strength 210\u2013260 MPa) is chosen when corrosion resistance and weldability are priorities over strength.<\/p><\/blockquote>\n

\n

Why Aluminum Dominates CNC Machining<\/h2>\n

Aluminum’s prevalence in CNC machining is not because it is the strongest or cheapest material \u2014 it is because the combination of properties results in the lowest total manufacturing cost for most precision engineering components.<\/p>\n

Machinability:<\/strong> Aluminum machines at cutting speeds of 300\u2013600 m\/min with carbide tooling, compared to 80\u2013180 m\/min for stainless steel and 30\u2013100 m\/min for titanium. This 3\u20138\u00d7 speed advantage translates directly into shorter cycle times and lower cost per part. Aluminum also produces short, clean chips rather than the long stringy chips of stainless steel, reducing chip evacuation problems and simplifying automated machining.<\/p>\n

Strength-to-weight ratio:<\/strong> At 2.7 g\/cm\u00b3, aluminum weighs approximately 35% as much as steel. For moving systems (robotics, UAV structures, automotive suspension), reducing component weight reduces inertia, improves response time, and reduces the load on supporting structures. A 6061-T6 aluminum bracket replacing a mild steel equivalent at the same stress level weighs approximately 35\u201340% of the steel version while meeting the same structural requirement.<\/p>\n

Natural corrosion resistance:<\/strong> Aluminum forms a stable aluminum oxide layer (Al\u2082O\u2083) on exposure to air, which passivates the surface and prevents further oxidation. This self-protective behavior is adequate for most indoor and general outdoor applications without any surface treatment, unlike mild steel which rusts in ambient humidity without coating.<\/p>\n

Thermal conductivity:<\/strong> Aluminum 6061 has thermal conductivity of approximately 150\u2013170 W\/m\u00b7K \u2014 roughly 4\u00d7 better than steel and 10\u00d7 better than titanium. For heat sink applications, electronics housings requiring thermal management, and any component where heat dissipation is relevant, aluminum’s thermal performance is not easily matched at comparable weight.<\/p>\n

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Aluminum Alloy Selection: The Six Criteria<\/h2>\n

Alloy selection for aluminum CNC machined parts requires evaluating six factors simultaneously. Selection based on any single factor \u2014 typically strength \u2014 produces over-engineered, over-cost solutions in most cases.<\/p>\n\n\n\n\n\n\n\n\n\n\n\n
Selection Factor<\/th>\n6061<\/th>\n7075<\/th>\n2024<\/th>\n5052<\/th>\n<\/tr>\n<\/thead>\n
Tensile strength (T6\/T3\/H32)<\/td>\n290\u2013310 MPa<\/td>\n500\u2013570 MPa<\/td>\n440\u2013470 MPa<\/td>\n210\u2013260 MPa<\/td>\n<\/tr>\n
Yield strength<\/td>\n240\u2013270 MPa<\/td>\n430\u2013500 MPa<\/td>\n290\u2013345 MPa<\/td>\n160\u2013210 MPa<\/td>\n<\/tr>\n
Machinability (relative to 1212 steel)<\/td>\n~70\u201375%<\/td>\n~70\u201375%<\/td>\n~65\u201370%<\/td>\n~60\u201365%<\/td>\n<\/tr>\n
Corrosion resistance<\/td>\nGood<\/td>\nModerate (bare)<\/td>\nPoor<\/td>\nExcellent<\/td>\n<\/tr>\n
Weldability<\/td>\nGood<\/td>\nPoor<\/td>\nPoor<\/td>\nExcellent<\/td>\n<\/tr>\n
Anodizing quality<\/td>\nExcellent<\/td>\nGood<\/td>\nPoor<\/td>\nGood<\/td>\n<\/tr>\n
Relative total machining cost<\/td>\nReference<\/td>\n20\u201340% higher<\/td>\n15\u201330% higher<\/td>\n5\u201315% higher<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n
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6061-T6: The Standard Choice for Most CNC Parts<\/h2>\n

6061 is a magnesium-silicon (Mg-Si) alloy with tensile strength of approximately 290\u2013310 MPa in the T6 temper. It is the default choice for aluminum CNC machined parts because no other alloy simultaneously offers its combination of machinability, corrosion resistance, surface finish quality, and cost.<\/p>\n

Machinability:<\/strong> 6061 machines cleanly at high cutting speeds with minimal built-up edge formation. The relatively low silicon content (0.40\u20130.80%) reduces abrasive tool wear compared to higher-silicon alloys, and the alloy’s good chip formation characteristics make it compatible with automated CNC machining with minimal tool change intervention. Surface finish of Ra 0.8\u20131.6 \u00b5m is routine; Ra 0.4 \u00b5m and below is achievable with appropriate tooling and finishing passes.<\/p>\n

Anodizing:<\/strong> 6061 produces the most consistent anodizing results of any common aluminum alloy. The oxide layer grows uniformly, resulting in predictable dye uptake and consistent color across a production batch. For visible consumer products, precision instruments, and any application where anodized color consistency matters, 6061 is the engineering choice.<\/p>\n

Corrosion resistance:<\/strong> 6061 performs well in indoor environments, general outdoor use, and moderate humidity without anodizing. For outdoor industrial equipment, general aviation components, and architectural hardware, uncoated 6061 typically has adequate corrosion resistance. It is not suitable for marine immersion or continuous saltwater exposure without treatment.<\/p>\n

Strength adequacy:<\/strong> 6061-T6 yield strength of 240\u2013270 MPa means it can carry design stresses up to approximately 160\u2013180 MPa (at a 1.5 safety factor) without permanent deformation. For structural brackets, housings, frames, fixtures, and most precision machine components, this is adequate. The most common error in alloy selection is upgrading to 7075 for parts whose load analysis shows stresses well below 6061’s yield strength.<\/p>\n

When 6061 is not adequate:<\/strong> High-load rotating components (drive shafts under high torque), aerospace structure under combined flight loads, competition racing components subject to impact and fatigue, and applications where the design cannot be thickened to bring stresses within 6061’s range.<\/p>\n

\n

7075-T6: When Maximum Strength Justifies the Premium<\/h2>\n

7075 is a zinc-magnesium-copper (Zn-Mg-Cu) alloy achieving tensile strength of 500\u2013570 MPa in the T6 temper \u2014 approximately 80% of the strength of mild steel at approximately 35% of its weight. This strength-to-weight ratio is why 7075 is the standard for aerospace structural components, high-performance robotics, and load-critical precision components.<\/p>\n

When to specify 7075 instead of 6061:<\/strong><\/p>\n

    \n
  • The design stress analysis shows stresses exceeding approximately 60\u201370% of 6061’s yield strength, and geometry cannot be changed to reduce stress below this level<\/li>\n
  • Fatigue life is a concern and the design cannot accommodate the section sizes needed for 6061 at the specified fatigue life<\/li>\n
  • Weight reduction is a primary objective (7075’s higher strength allows thinner sections for the same structural capacity)<\/li>\n
  • The application is high-performance or aerospace-classified and the strength margins of 7075 are specifically required<\/li>\n<\/ul>\n

    The 7075 cost trade-off:<\/strong> 7075 is not significantly harder to machine than 6061 in the T6 temper \u2014 machinability ratings are comparable. The cost premium comes from material price (7075 costs approximately 50\u2013100% more per kilogram than 6061 in equivalent forms) and from post-machining surface treatment requirements. 7075 has significantly lower corrosion resistance than 6061 due to the high zinc and copper content \u2014 bare 7075 corrodes visibly in humid environments. Components must typically be anodized, Alodine-treated, or painted, adding process steps that 6061 often does not require.<\/p>\n

    Weldability limitation:<\/strong> 7075 has poor weldability \u2014 welding causes cracking in the heat-affected zone (HAZ) due to the precipitation-hardenable alloy’s sensitivity to the thermal cycle of welding. 7075 is essentially a machined-part alloy; welded structures using 7075 are an engineering error in most cases.<\/p>\n

    \n

    2024-T3: Fatigue-Optimized for Cyclic Loading<\/h2>\n

    2024 is a copper-manganese-magnesium (Cu-Mn-Mg) alloy developed specifically for aerospace fatigue-critical structure. Its tensile strength of 440\u2013470 MPa in the T3 temper is lower than 7075, but its fatigue resistance \u2014 resistance to crack initiation and propagation under cyclic loading \u2014 is significantly better than either 6061 or 7075.<\/p>\n

    Why fatigue resistance matters:<\/strong> Most structural failures in service are fatigue-driven, not overload-driven. An aircraft fuselage panel sees pressure cycles on every flight; a vehicle suspension component sees millions of load cycles over its life. In fatigue applications, the stress amplitude and the material’s resistance to crack initiation (related to fatigue limit\/endurance limit) determine service life, not the static tensile strength.<\/p>\n

    2024-T3’s high copper content (3.8\u20134.9% Cu) produces a microstructure with improved resistance to fatigue crack initiation. The T3 temper (solution heat treated, cold worked, naturally aged) maintains good ductility while preserving the copper precipitation strengthening. The S-N curve (stress vs number of cycles) for 2024 shows longer fatigue life than 6061 or 7075 at equal stress amplitudes.<\/p>\n

    When to specify 2024:<\/strong><\/p>\n

      \n
    • Aerospace primary structure under repeated pressurization, bending, or vibration<\/li>\n
    • Structural components with documented fatigue life requirements (typically > 10\u2077 cycles)<\/li>\n
    • Applications where crack propagation rate needs to be slow to allow for inspection-based crack detection (damage tolerant design)<\/li>\n<\/ul>\n

      2024 limitations:<\/strong> Very poor corrosion resistance \u2014 2024 must be clad (bonded aluminum alloy sheet, 2024 core + pure aluminum surface layer) or anodized and sealed for outdoor use. Poor weldability \u2014 2024 is used in riveted and mechanically fastened structures, not welded assemblies. Anodizing is possible but produces less consistent results than 6061.<\/p>\n

      \n

      5052-H32: Corrosion Resistance and Weldability<\/h2>\n

      5052 is a magnesium alloy (Mg content 2.2\u20132.8%) without copper, providing excellent corrosion resistance, particularly in saltwater and marine environments. It is the standard choice when the application combines corrosion exposure with welding.<\/p>\n

      Corrosion resistance mechanism:<\/strong> 5052’s magnesium content produces a more stable and more coherent oxide layer than the Cu-containing alloys (2024, 7075), significantly reducing pitting corrosion in chloride-rich environments (seawater, road salt, coastal air). Salt spray test performance of 5052 substantially exceeds 6061 in marine-immersion conditions.<\/p>\n

      Weldability:<\/strong> 5052 welds with minimal strength reduction in the heat-affected zone, and the welded joint maintains acceptable ductility. Compare this to 6061, which loses approximately 20\u201340% of its T6 strength in the HAZ after welding (reverting from T6 to annealed condition locally), and to 7075 and 2024, which are prone to hot cracking and should not be fusion-welded.<\/p>\n

      Applications:<\/strong> Marine hull components, fuel tanks, welded enclosures for outdoor environments, chemical-resistant housings, architectural cladding, and any application combining forming operations (bending, rolling) with welding.<\/p>\n

      5052 limitations:<\/strong> Tensile strength of 210\u2013260 MPa in the H32 condition is lower than 6061-T6. For load-bearing CNC machined components, 5052 is typically insufficient. 5052 is a fabrication alloy \u2014 it excels in sheet-form fabrication operations but is not the right choice for complex precision-machined structural components.<\/p>\n

      \n

      Application-Specific Alloy Selection<\/h2>\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n
      Application Category<\/th>\nTypical Alloy<\/th>\nPrimary Reason<\/th>\n<\/tr>\n<\/thead>\n
      General housings, brackets, frames<\/td>\n6061-T6<\/td>\nMachinability, anodizing, cost<\/td>\n<\/tr>\n
      Heat sinks and thermal management<\/td>\n6061-T6<\/td>\nMachinability + thermal conductivity ~150\u2013170 W\/m\u00b7K<\/td>\n<\/tr>\n
      Aerospace structural brackets<\/td>\n7075-T6<\/td>\nStrength-to-weight; safety margins<\/td>\n<\/tr>\n
      Aerospace fatigue structure (fuselage, skins)<\/td>\n2024-T3<\/td>\nFatigue life; crack propagation resistance<\/td>\n<\/tr>\n
      Robotics arms and UAV structures<\/td>\n7075-T6<\/td>\nHigh stiffness, minimum deflection<\/td>\n<\/tr>\n
      Marine components (boats, offshore)<\/td>\n5052-H32<\/td>\nSaltwater corrosion resistance<\/td>\n<\/tr>\n
      Welded structural assemblies<\/td>\n5052-H32 or 6061<\/td>\nWeldability; 5052 for marine, 6061 for general<\/td>\n<\/tr>\n
      Electronics enclosures (consumer)<\/td>\n6061-T6<\/td>\nAnodizing consistency; cosmetic quality<\/td>\n<\/tr>\n
      Precision optical mounts<\/td>\n6061-T6<\/td>\nDimensional stability; machining consistency<\/td>\n<\/tr>\n
      Automotive performance components<\/td>\n7075-T6 or 6061<\/td>\nDepends on load: 7075 for high load, 6061 general<\/td>\n<\/tr>\n
      Motorsport components<\/td>\n7075-T6<\/td>\nStrength + weight under race loads<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n
      \n

      Common Selection Errors and Consequences<\/h2>\n

      Over-specifying 7075 for general parts:<\/strong> 7075 machining cost is 20\u201340% higher than 6061 due to material price premium, and the corrosion resistance limitation means additional surface treatment is typically required. For brackets, enclosures, and moderate-load structural parts where stress analysis confirms 6061’s yield strength is adequate, specifying 7075 adds cost without functional benefit.<\/p>\n

      Using 2024 or 7075 for welded structures:<\/strong> Both alloys have poor to unacceptable weldability. Hot cracking in 7075 and cold cracking combined with strength loss in 2024 make welded joints in these alloys structurally unreliable. Welded aluminum structures should use 5052 (marine\/corrosion environments) or 6061 (general structures), with post-weld treatment if 6061 T6 properties are required near welds.<\/p>\n

      Ignoring corrosion environment in alloy selection:<\/strong> 2024 and 7075, without surface treatment, visibly corrode in outdoor environments. For uncoated outdoor components, 6061 or 5052 are the appropriate choices. Applying 2024 or 7075 in marine environments without cladding or coating produces service failures within months.<\/p>\n

      Specifying 2024 for its anodized appearance:<\/strong> 2024 produces non-uniform, often gray-streaked anodizing due to the high copper content. For cosmetically consistent anodized parts, 6061 is the only practical choice among the common engineering alloys.<\/p>\n

      \n

      DFM Considerations for Aluminum CNC Machined Parts<\/h2>\n

      Wall thickness:<\/strong> Minimum practical wall thickness for CNC milled aluminum features depends on the height-to-thickness ratio. For unsupported walls: below approximately 1.5 mm wall thickness in 6061, elastic deflection under cutting forces becomes visible in the machined surface. For 7075 (higher modulus-to-strength ratio effective in thin sections), minimum wall thickness can approach 1.0\u20131.2 mm. For precision tolerances on thin walls, staged machining (rough from both sides, then finish) reduces deflection-induced error.<\/p>\n

      Internal corner radii:<\/strong> Standard end mills leave a radius at internal corners equal to the tool radius. For pockets requiring specific internal corner radii, the tool diameter must match the specified radius (a 2 mm radius pocket requires a \u2264 4 mm diameter tool). Very small corner radii (below R0.5 mm) require small-diameter, short-reach tools that reduce machining speed and increase setup complexity. Specify R1.0\u20132.0 mm internal corners as the default; smaller radii only where functionally required.<\/p>\n

      Depth-to-diameter ratio:<\/strong> Pockets and bores deeper than approximately 3\u20134\u00d7 their width require longer tools with reduced stiffness, producing potential chatter and surface quality variation. For pockets requiring depth-to-width ratios above 5:1, request DFM review before finalizing drawings.<\/p>\n

      Thread considerations:<\/strong> For threaded holes in aluminum, minimum engagement length is 1.5\u20132\u00d7 the nominal thread diameter to prevent stripping (versus 1\u00d7 for steel-to-steel). M3 and smaller threads in aluminum are at risk of stripping under assembly torque \u2014 consider helicoil inserts for small threads in loaded applications or for threads that will be repeatedly assembled.<\/p>\n

      Surface finish before anodizing:<\/strong> Anodize follows the machined surface exactly \u2014 it does not fill or hide machining marks. For cosmetically anodized parts, specify final machined surface finish of Ra \u2264 0.8 \u00b5m or lighter polishing before anodizing. Visible tool marks from Ra 1.6 \u00b5m milling will remain visible through the anodized layer.<\/p>\n

      \n

      Key Takeaways<\/h2>\n
        \n
      • 6061-T6 is the correct starting point for approximately 70\u201380% of aluminum CNC machined parts<\/strong>: its balance of machinability (cycle times 20\u201340% shorter than harder alloys), good corrosion resistance, consistent anodizing quality, and lower total machining cost makes it the appropriate choice unless specific analysis identifies an inadequacy.<\/li>\n
      • 7075-T6 is a performance upgrade, not a default upgrade<\/strong>: its ~80% higher tensile strength is valuable for aerospace structure, robotics, and high-load precision components, but the 20\u201340% higher machining cost and mandatory corrosion protection requirements mean it should only be specified when stress analysis or fatigue life requirements cannot be met by 6061.<\/li>\n
      • 2024-T3 is specifically for fatigue-dominated aerospace applications<\/strong>: its lower static strength than 7075 is compensated by superior fatigue crack resistance under cyclic loading. It is the wrong choice for general structural use, marine environments (corrodes rapidly), or welded assemblies.<\/li>\n
      • 5052-H32 is the correct choice when weldability and marine corrosion resistance are both required<\/strong>: its lower strength compared to 6061 is the trade-off accepted in exchange for excellent saltwater performance and welded joint reliability.<\/li>\n
      • Anodizing quality is alloy-dependent<\/strong>: 6061 produces the most consistent, aesthetically appealing anodized finish. 7075 produces acceptable results. 2024 produces poor, non-uniform anodizing due to high copper content.<\/li>\n
      • The most common aluminum alloy selection error is choosing 7075 “for safety” on parts where stress analysis shows 6061 is adequate<\/strong>: this adds cost, extends lead time, and requires additional corrosion protection without engineering justification.<\/li>\n
      • For OEM procurement teams<\/strong>: when a supplier substitutes one aluminum alloy for another (most commonly substituting 6061 for 7075 or vice versa), request the material certificate and verify alloy designation and temper. The mechanical properties of 6061-T6 and 7075-T6 differ by a factor of approximately 1.8\u00d7 in tensile strength \u2014 not an acceptable substitution for load-bearing components.<\/li>\n<\/ul>\n
        \n

        Frequently Asked Questions<\/h2>\n

        What is the best aluminum alloy for CNC machined parts?<\/h3>\n

        There is no single best aluminum alloy \u2014 the correct choice depends on the application’s requirements. For approximately 70\u201380% of CNC machined parts (housings, brackets, frames, precision components, electronics enclosures), 6061-T6 is the optimal choice because it combines adequate strength (290\u2013310 MPa tensile), excellent machinability, good corrosion resistance, and consistent anodizing quality at the lowest total machining cost. 7075-T6 is appropriate when loads exceed what 6061 can handle at the available section sizes, particularly in aerospace structure, robotics, and competition components. 2024-T3 is used specifically for fatigue-critical aerospace applications. 5052-H32 is the standard for marine environments and welded structural assemblies.<\/p>\n

        Is 7075 aluminum significantly better than 6061 for CNC parts?<\/h3>\n

        7075-T6 has approximately 80% higher tensile strength than 6061-T6 (500\u2013570 MPa versus 290\u2013310 MPa), which makes it significantly better for high-load applications. However, this strength advantage comes with real trade-offs: 7075 material costs approximately 50\u2013100% more per kilogram, its poor corrosion resistance (due to high zinc and copper content) requires additional surface treatment for most environments, its poor weldability makes it unsuitable for fabricated assemblies, and the machining cost is 20\u201340% higher. For parts where stress analysis confirms 6061’s yield strength is adequate \u2014 which is the majority of structural brackets, housings, and precision components \u2014 specifying 7075 adds significant cost without functional benefit.<\/p>\n

        Why is 6061 aluminum so commonly used in CNC machining?<\/h3>\n

        6061’s prevalence results from its combination of properties being well-suited to the majority of CNC machining applications simultaneously: machinability is excellent (cutting speeds of 300\u2013600 m\/min, low tool wear), strength is adequate for most applications at 290\u2013310 MPa tensile, corrosion resistance is good without treatment in most environments, anodizing quality is the most consistent of common alloys, and availability is excellent (globally stocked in bar, plate, and extrusion). No other alloy simultaneously satisfies all five criteria \u2014 7075 is stronger but costs more and corrodes more easily; 5052 resists corrosion better but has lower strength; 2024 has better fatigue life but poor corrosion resistance and poor anodizing. 6061’s “good at everything” profile makes it the practical default for approximately 70\u201380% of CNC machined aluminum parts.<\/p>\n

        What aluminum alloy should be used for marine or saltwater environments?<\/h3>\n

        5052-H32 is the standard choice for components with direct marine exposure \u2014 saltwater immersion, coastal air, or spray environments. 5052’s magnesium content (2.2\u20132.8%) produces a more stable surface oxide that resists chloride-induced pitting corrosion significantly better than 6061, and far better than the copper-containing alloys (2024, 7075) which corrode rapidly in marine conditions. For applications that combine marine corrosion resistance with welding requirements \u2014 boat hardware, tank fabrication, marine enclosures \u2014 5052 is also preferred over 6061 because 5052 retains better welded joint strength and is not prone to HAZ cracking. For anodized 6061 components used in general outdoor environments (not marine immersion), the anodize layer provides adequate corrosion protection.<\/p>\n

        How does aluminum alloy selection affect anodizing quality?<\/h3>\n

        Anodizing quality varies significantly between alloys because the oxide layer forms from the base metal, and alloying elements affect the oxide layer’s uniformity, thickness, and dye uptake. 6061 produces the most consistent anodizing of the common engineering alloys \u2014 the Mg-Si precipitation phase is fine and uniformly distributed, producing a uniform oxide layer with consistent pore structure for even dye absorption. 7075 produces acceptable but somewhat less uniform anodizing \u2014 visible cosmetic variation is possible in critical appearance applications. 2024 produces poor anodizing results \u2014 the high copper content (3.8\u20134.9%) creates copper-rich particles at the surface that produce dark streaks and uneven color in the anodized layer. 5052 anodizes adequately. For any application requiring cosmetically consistent anodized finish \u2014 consumer products, instruments, control panels \u2014 6061 is the clear choice.<\/p>\n

        \n

        Written by the CMS engineering team with 15+ years of precision CNC machining experience producing aluminum components in 6061, 7075, 2024, 5052, and specialty alloys for aerospace, automotive, robotics, medical device, consumer electronics, and industrial OEM manufacturing programs. Technical references: ASM Handbook Vol. 2 (Properties and Selection: Nonferrous Alloys \u2014 Aluminum Alloys), ASTM B209 (Aluminum Alloy Sheet and Plate), Machinery’s Handbook (Properties of Aluminum Alloys), MIL-DTL-5541 (Chemical Conversion Coatings on Aluminum), AMS 2770 (Heat Treatment of Aluminum Alloys).<\/em><\/p>\n

        \n

        Sourcing Precision CNC Machined Aluminum Parts?<\/strong><\/p>\n

        At CMS, we machine 6061, 7075, 2024, 5052, and specialty aluminum alloys to tight tolerances \u2014 with DFM review at the quoting stage, material certificate verification, anodizing coordination, and CMM first-article inspection reports.<\/p>\n

        [Request an aluminum alloy selection review and CNC machining quote \u2192]<\/p>\n<\/div>\n","protected":false},"excerpt":{"rendered":"

        Best aluminum alloy for CNC machined parts: 6061 vs 7075 vs 2024 vs 5052 \u2014 strength, machinability, corrosion, weldability, anodizing & cost comparison.<\/p>","protected":false},"author":1,"featured_media":11936,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[104],"tags":[],"class_list":["post-11707","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-general-basics"],"yoast_head":"\nAluminum CNC Machined Parts: Best Alloy Selection Guide<\/title>\n<meta name=\"description\" content=\"Best aluminum alloy for CNC machined parts: 6061 vs 7075 vs 2024 vs 5052 \u2014 strength, machinability, corrosion, weldability, anodizing & cost comparison.\" \/>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" 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