
The designations PN AlZn6Mg2Cu, CSN 424222, and BS L95 / L96 are regional and industrial equivalents for 7075 Aluminium. These standards specify high-strength aerospace and military grade alloys, primarily used for structural components where extreme mechanical performance is required.
| Standard | Designation | Material Code |
| PN (Poland) | AlZn6Mg2Cu | - |
| CSN (Czech/Slovak) | 424222 | Al-Zn6-Mg2-Cu |
| BS (British Standard) | L95 (Plate), L96 (Sheet) | 7075 Equivalent |
| EN AW (Europe) | 7075 | EN AW-Al Zn5.5MgCu |
| WNr (Germany) | 3.4365 | AlZnMgCu1.5 |
In British aerospace standards, the specific form of the material dictates the number:
BS L95: Specifically refers to 7075 Aluminium Plate (typically in T651 temper). It is stress-relieved by stretching to prevent distortion during heavy machining.
BS L96: Specifically refers to 7075 Aluminium Sheet and Strip (typically in T6 temper). These are thinner gauges used for aircraft skins and structural panels.
These alloys contain a high percentage of Zinc, which is the primary source of their exceptional strength.
Zinc (Zn): 5.10 6.10%
Magnesium (Mg): 2.10 2.90%
Copper (Cu): 1.20 2.00%
Chromium (Cr): 0.18 0.28%
Iron (Fe): 0.50% max
Aluminium (Al): Remainder
| Property | Metric Value | Imperial Value |
| Tensile Strength ($R_m$) | 530 570 MPa | 77,000 83,000 psi |
| Yield Strength ($R_{p0.2}$) | 450 500 MPa | 65,000 73,000 psi |
| Elongation ($A_{50mm}$) | 7 11% | 7 11% |
| Hardness (Brinell) | 150 HB | 150 HB |
Fatigue Strength: These alloys have a very high fatigue limit, making them essential for parts under repeated stress (e.g., aircraft wings).
Machinability: Excellent. They are easy to machine to a fine finish, though they are harder on tools than 6000-series alloys.
Corrosion Protection: Resistance is relatively low. Parts are almost always anodized, painted, or "clad" (BS L95/L96 can be ordered as Alclad, where the high-strength core is sandwiched between layers of pure, corrosion-resistant aluminium).
Welding: Not recommended. Thermal welding (MIG/TIG) causes severe strength loss and susceptibility to cracking. Mechanical fastening (riveting/bolting) is the standard joining method.
Defense: Ordnance industries and high-stress military hardware.
Aerospace: Main structural frames, bulkheads, and wing spars.
Automotive/Machining: Precision gears, shafts, and high-performance racing components.
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