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Thread 426/54
Aluminium specification code for L110 and L165
Can somebody please explain what L110 & L165 aluminium is ?
Dino Cecalaaerospace - Australia
publicly reply to Dino Cecala
2006
These specifications are British Standard Aerospace series aluminium alloys.
L110 should be quoted as BS L110, this is Aluminium-coated sheet and strip of Aluminium-Copper-Magnesium-Manganese alloy (Cu 4.4, Mg 1.5, Mn 0.6). Commonly called clad 2024 T42.
L165 should be quoted as BS L165, this is Sheet and strip of Aluminium-Copper-Magnesium-Silicon-Manganese alloy (Solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8). Commonly called 2014 T42.
Aerospace - Yeovil, Somerset, UK
publicly reply to Brian Terry
2006
'L' indicates a British Standard aerospace aluminium alloy:
L110 is 2024-T42 Clad Sheet and Strip (cladding may be 1230, as in AMSQQ250F)
L165 is 2014A-T6 Clad Sheet and Strip (cladding is 1050A).
Vendors should have more info.
Standards available from ILS http://aero-defense.ihs.com
- Goleta, California

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publicly reply to Ken Vlach
2006
"L110 should be quoted as BS L110, this is Aluminium-coated sheet and strip of Aluminium-Copper-Magnesium-Manganese alloy (Cu
4.4, Mg 1.5, Mn 0.6). Commonly called clad 2024 T42.
L165 should be quoted as BS L165, this is Sheet and strip of Aluminium-Copper-Magnesium-Silicon-Manganese alloy (Solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8). Commonly called 2014 T42"
Are these sheets of aluminium off the shelf at T42, or are they heat treated to T42 after forming ?
Aerostaff - Australia
publicly reply to Dino Cecala
T42 is the "as supplied" temper state. You then heat treat the material to obtain the temper state you require.
Brian TerryAerospace - Yeovil, Somerset, UK
2006
publicly reply to Brian Terry
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