Aluminum Sheet - 7075-0 Alclad

7075 is one of the highest strength aluminum alloys available Its strength-to weight ratio is excellent and it is ideally used for highly stressed parts. It may be formed in the annealed condition and subsequently heat treated. Spot or flash welding can be used, although arc and gas welding are not recommended. It is available in the clad ('Alclad") form to improve the corrosion resistance with the over-all high strength being only moderately affected. Applications: Used where highest strength is needed.

7075-0 Alclad
Heat Treatable, Interleaved and Stenciled
AMS-QQ-A-250/13 AMS 4048

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Items	7075-0A-040-48-144 Aluminum Sheet - 7075-0 Alclad	7075-0A-050-48-144 Aluminum Sheet - 7075-0 Alclad	7075-0A-063-48-144 Aluminum Sheet - 7075-0 Alclad	7075-0A-071-48-144 Aluminum Sheet - 7075-0 Alclad	7075-0A-080-48-144 Aluminum Sheet - 7075-0 Alclad
Material	N/A Aluminum
Shapeform	N/A Sheets
Series	N/A 7075-0 Alclad
Grade	N/A 7075
Preparation	N/A Interleaved and Stenciled
Condition	N/A Heat Treatable
Temper	N/A Soft Alclad
Thickness	N/A 0.040 inches1.016 mm	N/A 0.063 inches1.6002 mm	N/A 0.0710 inches1.8034 mm	N/A 0.080 inches2.032 mm	N/A 0.090 inches2.286 mm
Size	N/A 48 x 144
Width	N/A 48
Length	N/A 144
Sheet Weight per Unit Area	N/A 0.582 lbs/ft²2.841324 kg/m²	N/A 0.916 lbs/ft²4.471912 kg/m²	N/A 1.033 lbs/ft²5.043106 kg/m²	N/A 1.164 lbs/ft²5.682648 kg/m²	N/A 1.309 lbs/ft²6.390538 kg/m²
Weight per Sheet	N/A 27.92 lbs12.64776 kg	N/A 43.98 lbs19.92294 kg	N/A 49.57 lbs22.45521 kg	N/A 55.85 lbs25.30005 kg	N/A 62.83 lbs28.46199 kg
ASTM Specification	N/A AMS 4044 AMS 4045 AMS 4048 AMS 4078 AMS-QQ-A-250/12 AMS-QQ-A-250/13 AMS-QQ-A-250/24
Ultimate Strength	N/A 32 ksi	N/A 33 ksi	N/A 33 ksi	N/A 33 ksi	N/A 33 ksi
Yield Strength	N/A 14 ksi	N/A 15 ksi	N/A 15 ksi	N/A 15 ksi	N/A 15 ksi
Elongation percent in 2 inches	N/A 17
Hardness Brinnel Number	N/A	N/A 60	N/A 60	N/A 60	N/A 60
Ultimate Shearing Strength	N/A 22 ksi
Modulus of Elasticity¹	N/A 10.4 x 10² ksi
Mechinability	N/A D
Brazeability²	N/A D
Gas Weldability³	N/A D
Arc Weldability⁴	N/A D
Resistance Spot and Seam Weldability⁵	N/A B
Applications	N/A Aircraft and other structures
Density	N/A 0.101 lbs/in³
Specific Gravity	N/A 2.81
¹ Average of tension and compression moduli. Compression modulus is about 2 percent greater than tension modulus. ² Ratings A through D for Weldability and Brazeability are relative ratings. ³ 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. ⁴ 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. ⁵ 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.

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