Engine Turbine Shroud Segment from Japan

Single-crystal superalloy turbine shroud segment that lines the hot gas path in aircraft engine high-pressure turbine. Provides thermal and containment protection. Under 8409.10.0080 as specialized aircraft engine part.

Duty Rate — Japan → United States

10%

Rate breakdown

9903.03.0110%Except for products described in headings 9903.03.02–9903.03.11, articles the product of any country, as provided for in subdivision (aa) of U.S. note 2 to this subchapter

Import Tips

Submit single-crystal casting process certifications from approved foundries

Declare exact superalloy grade (e.g

CMSX-4) matching specific engine models

Avoid misdeclaration as general metal castings by linking to 8407 engine documentation