E4340 Hot-Rolled Alloy Steel Bar Coil

Hot-rolled bars of E4340 nickel-chromium-molybdenum alloy steel in irregular coils, ideal for aircraft landing gear and high-stress components. HTS 7227.90.60.90 covers this as other hot-rolled alloy steel coils not fitting tool steel or other specific notes. Features 0.38-0.43% carbon with multiple alloying elements.

Import Duty Rates by Country of Origin

Origin CountryMFN RateCh.99 SurchargesTotal Effective Rate
🇨🇳ChinaFree+35.0%35%
🇲🇽MexicoFree+10.0%10%
🇨🇦CanadaFree+10.0%10%
🇩🇪GermanyFree+10.0%10%
🇯🇵JapanFree+10.0%10%

Alternative Classifications

This product could be classified differently depending on its characteristics or intended use.

7227.20.00Same rate: 35%

If silicon-manganese steel

Silicon-manganese alloy steels (max specified Si/Mn content) have separate heading 7227.20, not 'other alloy' 7227.90.

7228.30Lower: 10% vs 35%

If further worked like phosphatized

Chemical surface treatments (phosphatizing per Chapter note) classify as further worked in 7228, not plain hot-rolled.

7207.20.00Same rate: 35%

If semi-finished product size

If cross-section >150mm or certain thick coils, it's semi-finished under 7207, not bars/rods.

Not sure which classification is right?

Our AI classifier can analyze your specific product and recommend the correct HTS code with confidence.

Import Tips & Compliance

Include heat treatment records if normalized; over-treated may be seen as 'further worked'

Measure coil irregularity and hot-rolling temp verification to distinguish from straight lengths (7227.90.20)

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