2014

EU Gray

According to EU directives: 2000/53/EU (ELV) – 2011/65/EU (RoHS II)

This alloy has high mechanical properties, excellent resistance to fatigue, good attitude to forging and a fair machinability.

high structural resistance components for aircraft and defense.

Properties	T3,T4,T6
Machinability
Protective anodizing
Decorative anodizing
Hard anodizing
Resistance to atmospheric corrosion
Resistance to marine corrosion
MIG-TIG weldability
At resistance weldability
Brazing weldability
Plastic formability when cold
Plastic formability when hot

Excellent

Good

Acceptable

Not recommended

Density	Kg/dm^3	2,80
Modulus of elasticity	MPa	72.400
Coefficient of thermal expansion	x10^-6/C	23
Thermal conductivity at 20°C	W/mk	T4: 134 T6: 155
Electrical resistivity at 20°C	Ωmm^3/m	T4: 0,051 T6: 0,043

	Temper	Diam. mm	Rm MPa	Rp 0,2 MPa	A%	HBW
Drawn	T3	≤80	380	290	8	110
	T351	≤80	380	290	6	110
	T4	≤80	380	220	12	110
	T451	≤80	380	220	10	110
	T6	≤80	450	380	8	140
	T651	≤80	450	380	6	140
Extruded	T4, T4510, T4511	≤ 75	410	270	12	110
	T4, T4510, T4511	75 < D ≤ 150	390	250	10	110
	T4, T4510, T4511	150 < D ≤ 200	350	230	8	110
	T6, T6510, T6511	≤ 75	460	415	7	140
	T6, T6510, T6511	75 < D ≤ 150	465	420	7	140
	T6, T6510, T6511	150 < D ≤ 200	430	350	6	140
	T6, T6510, T6511	200 < D ≤ 250	420	320	5	140

DRAWN

EXTRUDED: