Product Details, Specifications, and Technical Information

7050-T7451 plate has great stress corrosion and exfoliation resistance, strength, and fracture toughness, even more so than the more standard aerospace aluminum alloy 7075. This alloy is normally used in thicker sections because it has less quench sensitivity which allows it to keep it’s strength. Typical applications of 7050-T7451 aluminum plate are: Fuselage Frames, Bulkheads, and Wing Sections. Welding is not recommended and may result in weld cracking, porosity and a weak joint.

shape Image
Dimension Name Specification
Thickness 3.5
Max Width 48
Max Length 120
Alloy 7050
Temper T7451
MTR Availability Yes
Full Length true
Material Aluminum
Shape Sheet/Plate
Custom Cut Warehouse 1
Material Specifications

This material meets the following specs: AMS -4050, DMS -2233, AMS -4050, MMS -1420, DMS -2233, BSS -7055, AMS -STD 2154, ASTM -B594, DPS -4.713 CL A , GAMPS -9101 CL A, BAMS -516-003 REV B, BMS -7-323 Type 1 (Call for Availability), LMA -USI (Call for Availability)

Weight/Lineal Foot
51.4 pounds
Please note that this data is to be used ONLY FOR REFERENCE, NOT FOR DESIGN, and by using it,you agree that any decisions you make regarding materials for your project are at your own discretion.
Chemistry Information: 7050 Aluminum
Element Percentage
Al -
Si 0.12
Fe 0.15
Cu 2 - 2.6
Mn 0.1
Mg 1.9 - 2.6
Cr 0.04
Zn 5.7 - 6.7
Zr 0.08 - 0.15
Ti 0.06
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