Aircraft Landing Gear Strut
A hydraulic shock-absorbing strut assembly for commercial jet aircraft landing gear systems. Falls under HTS 8807.90.90 as parts of heading 8802 airplanes, designed to withstand high-impact landings. Constructed from titanium and high-strength steel.
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More Specific Codes
This product may fall under a more specific subheading:
Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If designed for motor vehicles rather than aircraft
Vehicle suspension systems classify under Chapter 87, not aircraft parts.
If parts specifically for unmanned aerial vehicles over 250kg
UAV parts over maximum takeoff weight threshold use 8806-specific classifications.
If classified primarily as hydraulic cylinders
Generic hydraulic cylinders without aircraft specificity fall under Chapter 84 machinery.
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Import Tips & Compliance
• Include load test certificates and hydraulic specifications to prove aircraft-specific design
• Verify if components contain hazardous materials requiring special declarations
• Use temporary importation under ATA Carnet for parts intended for maintenance and return
Related Products under HTS 8807.90.90
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A lightweight aluminum-composite fuselage skin panel used in the assembly of Boeing 737 commercial aircraft. It falls under HTS 8807.90.90 as a part of goods of heading 8802 (other aircraft), specifically for fixed-wing airplanes. This component is essential for the structural integrity of the aircraft fuselage.
Airbus A320 Wing Spar
A high-strength machined aluminum spar forming the primary structural member of the Airbus A320 wing. Classified under HTS 8807.90.90 as a part of heading 8802 airplanes, this critical component bears flight loads. It requires precision engineering for fatigue resistance.
Boeing 787 Composite Rudder
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Airbus A350 Flight Control Actuator
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