5052 is the highest strength alloy of the more common non heat-treatable grades. Fatigue strength is higher than most aluminum alloys. In addition, this grade has particularly good resistance to marine atmosphere and salt water corrosion. It has excellent workability. It may be drawn or formed into intricate shapes and its slightly greater strength in the annealed condition minimizes tearing that occurs in 1100 and 3003. Applications: Used in a wide variety of applications from aircraft components to home appliances, marine and transportation industry parts, heavy duty cooking utensils and equipment for bulk processing of food.

5052-H32
Mill Finish
AMS-QQ-A-250/8 AMS 4016 ASTM B209
Unit of Measure
Items
Metal and Alloy Plate & Coil

Aluminum Sheet and Coil - Series 5052-H32

Metal & Alloy Sheet & Plate

Aluminum Sheet and Coil - Series 5052-H32

Metal and Alloy Plate & Coil

Aluminum Sheet and Coil - Series 5052-H32

Metal & Alloy Sheet & Plate

Aluminum Sheet and Coil - Series 5052-H32

Metal & Alloy Sheet & Plate

Aluminum Sheet and Coil - Series 5052-H32
Material N/A Aluminum
Shapeform N/A Coil N/A Sheets N/A Coil N/A Sheets N/A Sheets
Series N/A 5052-H32
Grade N/A 5052
Temper N/A H32
Finish N/A Mill
Thickness N/A 0.02 inches0.508 mm
Size N/A 36 x Coil N/A 36 x 96 N/A 48 x Coil N/A 48 x 96 N/A 48 x 120
Width N/A 36 N/A 36 N/A 48 N/A 48 N/A 48
Length N/A N/A 96 N/A N/A 96 N/A 120
Sheet Weight per Unit Area N/A 0.279 lbs/ft²1.362 kg/m² N/A N/A N/A N/A
Weight per Sheet N/A N/A 6.70 lbs0.304 kg N/A N/A 8.94 lbs4.055 kg N/A 11.17 lbs5.067 kg
Coil Weight per Length N/A 0.838 lbs/ft1.247 kg/m N/A N/A 1.117 lbs/ft1.662 kg/m N/A N/A
ASTM Specification N/A AMS 4016 AMS-QQ-A-250/8 ASME SB-209 ASTM B209
Ultimate Strength N/A 33 ksi
Yield Strength N/A 28 ksi
Elongation percent in 2 inches N/A 12
Hardness Brinnel Number
N/A 60
Ultimate Shearing Strength N/A 20 ksi
Fatigue Endurance Limit1 N/A 17 ksi
Modulus of Elasticity2 N/A 10.2 x 102 ksi
Resistance to Corrosion - General3 N/A A
Stress Corrosion Cracking4 N/A A
Workability (Cold)5 N/A B
Mechinability N/A D
Brazeability6 N/A C
Gas Weldability7 N/A A
Arc Weldability8 N/A A
Resistance Spot and Seam Weldability9 N/A A
Applications N/A Sheet metal work, hydraulic tube, appliances
Density N/A 0.097 lbs/in³
Specific Gravity N/A 2.68
  • 1 Based on 500,000.000 cycles of completely reversed stress using the R. R. Moore-type of machine and specimen.
  • 2 Average of tension and compression moduli. Compression modulus is about 2 percent greater than tension modulus.
  • 3 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.
  • 4 Stress-corrosion cracking ratings are based on service experience and on laboratory tests of specimens exposed to the 3.5% sodium chloride alternate immersion test.
  • 5 Ratings A through D for Workability (cold), and A through E for Machinability, are relative ratings in decreasing order of merit.
  • 6 Ratings A through D for Weldability and Brazeability are relative ratings.
  • 7 A = Generally weldable by all commercial procedures and methods.
    B = Weldable with special techniques or for specific applications that justify preliminary trials 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.
  • 8 A = Generally weldable by all commercial procedures and methods.
    B = Weldable with special techniques or for specific applications that justify preliminary trials 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.
  • 9 A = Generally weldable by all commercial procedures and methods.
    B = Weldable with special techniques or for specific applications that justify preliminary trials 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.