A high strength aerospace aluminium alloy in the fully soft condition
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SAE AMS QQ-A-250/13 Alloy QQ A 250/13 |
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|---|---|
| Chemical Element | % Present |
| Aluminium (Al) | balance |
| Other (Each) | 0.05 max |
| Others (Total) | 0.15 max |
| Titanium (Ti) | 0.2 max |
| Manganese (Mn) | 0.3 max |
| Chromium (Cr) | 0.18 - 0.35 |
| Silicon (Si) | 0.4 max |
| Iron (Fe) | 0.5 max |
| Copper (Cu) | 1.2 - 2 |
| Magnesium (Mg) | 2.1 - 2.9 |
| Zinc (Zn) | 5.1 - 6.1 |
Aluminium alloy QQ-A-250/13 has similarities to the following standard designations and specifications but may not be a direct equivalent:
AMS 4049, AMS4278, Alloy 7075, UNS A97075
Alloy QQ-A-250/13 CLAD SHEET is supplied in a range of tempers including fully soft
Alloy QQ-A-250/13 is supplied in CLAD sheet and plate
| Physical Property | Value |
|---|---|
| Density | 2.71 g/cm³ |
| Melting Point | 635 °C |
| Thermal Expansion | 23.5 x10^-6 /K |
| Modulus of Elasticity | 72 GPa |
| Thermal Conductivity | 75 W/m.K |
| Electrical Resistivity | 45.5 % IACS |
These are for sheets in the 'O' temper
| Thickness (mm) | Proof Strength (Min) | Tensile Strength (Min) | Elongation % (Min) |
| Over 0.2 up to & incl. 0.3 | 138 | 248 | 9 |
| Over 0.3 up to & incl. 1.5 | 138 | 248 | 10 |
| Over 1.6 up to & incl. 4.7 | 138 | 262 | 10 |