Aluminum 5086

Aging Procedure

Not applicable to this alloy.

Annealing Procedure

Anneal at 650 F for long enough to insure thorough heating. Air cool.

Applications

Commonly used in the manufacture of unfired, welded pressure vessels, marine, auto aircraft cryogenics, drilling rigs, tanks, TV towers, transportation equipment, and in missile components.

Cold Workability

Excellent cold working characteristics in the O temper and somewhat less good in H36 and H38 tempers.

Forgeability

No specific data as to hot working range. However the alloy is forgeable.

Formability

Forming characteristics are best with the alloy in the O temper -- less good in the H36 or H38 tempers.

Hardening Procedure

Hardens by cold working only.

Heat Treatability

The alloy is non-heat treatable.

Hot Workability

No data in regard to hot forming. Cold forming characteristics are excellent and usually would not necessitate hot working.

Machinability

Machinability in the strain hardened tempers (H34, H36, H38) is relatively good. In the annealed (O temper) machining is difficult, but still can be accomplished. Use of lubricants is advised.

Other Mechanical Properties

Shear strength for O temper is 23 ksi, for H34 it is 27 ksi

Other Physical Properties

Electrical conductivity 30% of copper.

Principle Design Features

This is a high strength structural alloy. It is not heat treatable.

Tempering Procedure

Not applicable.

Weldability

This alloy is readily weldable by conventional methods. Use of electric arc welding in particular produces excellent results.

Known Forms

Angle

Angle

Channel

Channel

Coil

Coil

Disc

Disc

Flat Bar

Flat Bar

Foil

Foil

Hollow Bar

Hollow Bar

Pipe

Pipe

Plate

Plate

Rectangle Tube

Rectangle Tube

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Square Bar

Square Bar

Square Tube

Square Tube

Strip

Strip

Tee

Tee

Treadplate

Treadplate

Additional Data

Specifications

B209,B210,B221,B241,B313,B345,B361,B547,B548,C-26094,S-24149/2,A-200/5,A-250/7,WW-T-700/5,J454,A95086

Chemical Elements

AluminumBalance
Chromium0.05 - 0.25
Copper0.1 max
Iron0.5 max
Magnesium3.5 - 4.5
Manganese0.2 - 0.7
Remainder Each0.05 max
Remainder Total0.15 max
Silicon0.4 max
Titanium0.15 max
Zinc0.25 max

Physical Properties

Density: 0.096lb/in³Density

Melting Point: 1090°FMelting Point

Specific Gravity: 2.66Specific Gravity

Mechanical Properties

Modulus of Elasticity – Tension: 10.3MSIModulus of Elasticity – Tension

Mechanical Test Data

FormSheet
ConditionH112
Temperature68°F
Elongation14%
Tensile Strength39 KSI
Yield Strength19 KSI
FormSheet
ConditionH116
Temperature68°F
Elongation12%
Tensile Strength42 KSI
Yield Strength30 KSI
FormSheet
ConditionH32
Temperature68°F
Elongation12%
Tensile Strength42 KSI
Yield Strength30 KSI
FormSheet
ConditionH34
Temperature68°F
Elongation10%
Tensile Strength47 KSI
Yield Strength37 KSI