
When cross-referencing global supply routes or dealing with historical technical drawings, you will frequently run into the Japanese JIS H4100 / H4040 standards and the French AFNOR NF A50-411 standards for 7075 aluminum.
While they all target the exact same base $Al-Zn-Mg-Cu$ metallurgical profile, their designation systems, processing controls, and specific mechanical testing requirements have unique nuances.
The French AFNOR designation explicitly lists the critical alloying elements, whereas the Japanese JIS standard adopts the traditional 4-digit international system.
Japanese System: JIS A7075 (governed by JIS H4040 for extruded bars, rods, and wires, and JIS H4100 for extruded shapes).
French System: AFNOR 7075 / A-Z5GU (often specified in aerospace legacies as A-Z5GU-T6 or A-Z5GU-T73).
While globally unified under the Aluminum Association registry, minor tolerance windows can shift slightly between regional master standards.
| Element | JIS H4040 A7075 (%) | AFNOR A-Z5GU (%) |
| Zinc (Zn) | 5.10 â 6.10 | 5.10 â 6.10 |
| Magnesium (Mg) | 2.10 â 2.90 | 2.10 â 2.90 |
| Copper (Cu) | 1.20 â 2.00 | 1.20 â 2.00 |
| Chromium (Cr) | 0.18 â 0.28 | 0.18 â 0.28 |
| Iron (Fe) | 0.50 max | 0.40 max (Aerospace grade variants limit Fe strictly) |
| Silicon (Si) | 0.40 max | 0.30 max |
| Manganese (Mn) | 0.30 max | 0.30 max |
| Titanium (Ti) | 0.20 max | 0.20 max |
Note on Impurities: French aerospace specifications for A-Z5GU often impose tighter restrictions on Iron ($Fe \le 0.40\%$) and Silicon ($Si \le 0.30\%$) than generic global standards to maximize fracture toughness and fatigue resistance in high-stress structural components.
The mechanical properties are tested using slightly different sample geometries depending on the standard system, resulting in variations in specified minimum elongation values.
JIS A7075-T6: Typically requires a minimum Yield Strength ($R_{p0.2}$) of 470 to 480 MPa and Ultimate Tensile Strength ($R_m$) of 540 to 550 MPa depending on the diameter of the bar. Elongation values are calculated using a gauge length based on $5D$ ($5 \times \text{diameter}$).
AFNOR A-Z5GU-T6511: Controlled stretching (the "511" suffix) is strictly utilized to relieve residual quenching stresses before machining. Mechanical limits align with European EN 755-2, matching or slightly exceeding a minimum $R_m$ of 540 MPa.
Utilized when the component operates under sustained tensile stress in corrosive environments to prevent premature micro-cracking. Yield strength drops to roughly 380 - 400 MPa, but the risk of catastrophic stress corrosion failure is eliminated.
Machining Behavior: Both variants turn beautifully on a lathe or mill. Because 7075 is highly brittle compared to soft 6000-series alloys, it breaks chips cleanly, allowing for high feed rates without bird-nesting around the tooling.
Certification Cross-Over: If you are substituting a JIS A7075 bar for an older AFNOR A-Z5GU drawing requirement, you must verify if the drawing requires an aerospace-level inspection schedule (such as EN 10204 3.1 or 3.2 traceability). Commercial-grade JIS bars may lack the micro-cleanliness testing required by European aerospace engineering specifications.
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