7075 T6 Aluminum Alloy Sheet for Aircraft from United States
7075 T6 aluminum alloy sheet, rectangular, thickness exceeding 0.2 mm, non-clad, with zinc as the primary alloying element. This high-strength material is precision-rolled for aircraft skin panels and structural components, and it meets the aluminum alloy definition under Chapter 76 subheading note 1.
Duty Rate — United States → Canada
Rate breakdown
PGA flags (1)Show detailsHide detailsGACAluminumMay be required
- GAC
Aluminum · May be required · on some HTS numbers under this code
May require GAC Aluminum (Aluminum Products) depending on the full 10-digit classification number (only some numbers under this code are listed). Matching criteria: Equal To 7606120020; Equal To 7606120011; Equal To 7606120012. Logic: MATCH IF (Valid HS Code).
CBSA Single Window matching criteria, unknown
Import Tips
• Verify the T6 temper and alloy composition with a certificate of analysis
• Ensure the sheet is non-clad and rectangular
• Keep documentation of the aerospace application for customs