Continental IO-240-B Aircraft Engine
The Continental IO-240-B is a four-cylinder, air-cooled, fuel-injected spark-ignition reciprocating engine producing 125 horsepower (93 kW), designed specifically for civil aircraft like light sport and experimental models. It falls under HTS 8407.10.00.20 as a new aircraft engine under 373 kW for civil use, matching the hierarchy for spark-ignition piston engines.
Import Duty Rates by Country of Origin
| Origin Country | MFN Rate | Ch.99 Surcharges | Total Effective Rate |
|---|---|---|---|
| šØš³China | Free | +35.0% | 35% |
| š²š½Mexico | Free | +10.0% | 10% |
| šØš¦Canada | Free | +10.0% | 10% |
| š©šŖGermany | Free | +10.0% | 10% |
| šÆšµJapan | Free | +10.0% | 10% |
Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If designed for motor vehicles rather than aircraft
Engines principally for cars or trucks fall under automotive piston engine headings, not aircraft-specific provisions.
If power output exceeds 373 kW
Higher power aircraft engines are classified in the statistical suffix for >373 kW within the same civil aircraft category.
If imported as a complete gas turbine rather than reciprocating piston
Turbojet or turboprop aircraft engines use gas turbine technology, shifting to Chapter 84 heading 8411.
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Import Tips & Compliance
ā¢ Obtain FAA or EASA type certification documentation to verify civil aircraft use; ensure engine is certified as 'new' with manufacturer affidavit
ā¢ Common pitfall: misclassifying as rotary type, which may shift to other subheadings
Related Products under HTS 8407.10.00.20
Lycoming O-235-L2C Piston Engine
The Lycoming O-235-L2C is a carbureted, four-cylinder, air-cooled spark-ignition engine delivering 118 horsepower (88 kW), commonly used in civil trainer aircraft such as the Cessna 152. Classified under HTS 8407.10.00.20 for new spark-ignition aircraft engines under 373 kW intended for civil aviation.
Rotax 912 UL-S3 Aviation Engine
The Rotax 912 UL-S3 is a four-stroke, four-cylinder, liquid-cooled spark-ignition engine with dual ignition, rated at 100 horsepower (75 kW), popular in ultralight and light sport civil aircraft. It qualifies for HTS 8407.10.00.20 as a new reciprocating engine under 373 kW for civil aircraft applications.
UL Power UL260iS Experimental Aircraft Engine
The UL Power UL260iS is a four-cylinder, fuel-injected, air-cooled spark-ignition engine producing 97 horsepower (72 kW), tailored for experimental and light sport civil aircraft. It is classified under HTS 8407.10.00.20 due to its new condition, piston design, and power below 373 kW for civil use.
Jabiru 2200 Aircraft Piston Engine
The Jabiru 2200 is a four-cylinder, air-cooled, four-stroke spark-ignition engine rated at 85 horsepower (63 kW), used in civil kit-built and light aircraft. Falls under HTS 8407.10.00.20 as a new spark-ignition reciprocating engine under 373 kW for civil aircraft.