Alloy 2219

Chemical Composition Limits Others
Weight % Si Fe Cu Mn Mg Zn Ti V Zx Each Total
Minimum - - 5.8 0.20 - - 0.02 0.05 0.10 - -
Maximum 0.20 0.30 6.8 0.40 0.02 0.10 0.10 0.15 0.25 0.05 0.15

Typical Physical Properties
Characteristic English Metric
Nominal Density (68 °F/20 °C) 0.103 lbs./in.3 2.84 Mg/m3
Melting Range 1010 °F - 1190 °F 543 °C - 643 °C
Specific Heat (212 °F/100 °C) 0.206 BTU/lb. - °F 864 J/kg - °K
Coefficient of Thermal Expansion
Linear
68 °F-212 °F
20 °C-100 °C
12.5 micro in./in.-°F 22.5 micro m/m -°K
Volumetric
68 °F/20 °C
3.62 x 10-5in.3/in.3 -°F 65 x 10-6m3/m3 -°K
Thermal Conductivity (68°F/20°C) T3,T3551 67 BTU/ft. - hr. - °F 116 W/m - °K
T8, T851, T8511 75 BTU/ft. - hr. - °F 130 W/m - °K
Electrical Conductivity (68°F/20°C) Equal Volume T3,T3551 28% IACS
T8, T851, T8511 30% IACS

Typical Mechanical Properties (Longitudinal)
  Tensile (.500" Dia. Specimen) Hardness Shear Fatigue* Modulus
Temper Yield Ultimate Elongation/4D
Brinell
500 kg
10 mm
Ultimate Shearing Strength Endurance Limit - R.R. Moore Type Modulus of Elasticity
KSI MPa KSI MPa %   KSI MPa KSI MPa KSI x 103 Gpa
0 11 76 25 172 18 45 - - - - 10.6 73.1
T3, T3511 36 248 52 359 17 95 - - - - 10.6 73.1
T8, T851, T8511 51 352 66 455 10 125 - - 15 103 10.6 73.1
*5 x 10E8 cycles of reversed stress
Comparative Characteristics
Temper Corrosion Resistance
Cold
Workability3
Machin-
ability3
Anodize
Response3
Braze-
ability4
Weldability4
General1 Stress2 Gas Arc Spot
0 - - - - - D D A B
T3, T3511 D C C B B D A A A
T8, T851, T8511 D B D B B D A A A
1 Ratings A through E are relative ratings in decreasing order of merit, based on exposures to sodium chloride solution by intermittent spraying or immersion. Alloys with A and B ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D and E ratings generally should be protected at least on faying surfaces.
2 Stress-corrosion cracking ratings are based on service experience and laboratory tests of specimens exposed to the 3.5% sodium chloride alternate immersion test.
A= No known instance of failure in service or in laboratory tests.
B= No known instance of failure in service; limited failures in laboratory tests of short transverse specimens.
C= Service failures with sustained tension stress acting in short transverse direction relative to grain structure; limited failures in laboratory tests of long transverse specimens.
D= Limited service failures with sustained longitudinal or long transverse

3 Ratings A through D for Workability (cold), A through E for Machinability and A through C for Anodize Response, are relative ratings in decreasing order of merit.
4 Ratings A through D for Weldability and Brazeability are relative ratings defined as follows:
A= Generally weldable by all commercial procedures and methods.
B= Weldable with special techniques or for specific applications that justify preliminary trails or testing to develop welding procedure and weld performance.
C= Limited weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
D= No commonly used welding methods have been developed.
Applicable Specifications  
Cold Finished Extruded
ASTM B211 ASTM B221
  AMS 4162
  AMS 4163

Alloy Description
This alloy is used in aerospace applications such as space booster and fuel tanks. The alloy is readily weldable. It is useful over a temperature range of -452º to 600 ºF. The alloy also has good fracture toughness. The T8 temper is resistant to stress corrosion craking.

 
 
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