CN code 8411 91 00 Of turbojets or turbopropellers

One TARIC code carries a different end-use rate.

TARIC codes (10 digits): 3

Origin, preferential duty and next steps ›

Examples from the EU database of Binding Tariff Information (BTI). A ruling binds only its holder and many have expired — read them as guidance, not as a decision for your product.

• THE ASSEMBLY IS OF SEAMLESS COLD DRAWN CONCENTRIC HOLLOW RIGID TUBE MADE OF AMS5557 CORROSION AND HEAT RESISTANT STEEL, MEASURING 41.7 INCHES. IT IS USED AS A FUEL/LUBRICANT/AIR SUPPLY PIPELINE TO THE GAS TURBINE ENGINE. 7 BENDS FORMED TO PRECISE ANGLES AT PRECISE POSITIONS ALONG ITS LENGTH TO VERY TIGHT TOLERANCES. TO THE OUTSIDE OF THIS SHAPED TUBE 6 OFF WEAR SLEEVES MADE OF AMS5557/AMS5510…

  8411 91 00 · GB 2019 · GBBTI504430882

• TUBE ASSEMBLY, AIR LINE AMS5570 STAINLESS STEEL CORROSION AND HEAT-RESISTANT SEAMLESS TUBE. MADE TO MEASURE FOR AIRCRAFT ENGINE BR710

  8411 91 00 · GB 2018 · GBBTI503967340

• 3/4 TUBE ASSEMBLY OLIV 23 AMS5570 STAINLESS STEEL CORROSION AND HEAT RESISTANT SEAMLESS TUBE ASSEMBLY FOR OIL FOR AIRCRAFT ENGINE - MADE TO MEASUREMENT AND DESIGN FOR SPECIFIC USE IN AIRCRAFT ENGINE TRENT XWB

  8411 91 00 · GB 2018 · GBBTI503967536

• TUBE ASSEMBLY AMS5581 INCONEL 625 CORROSION AND HEAT RESISTANT NICKEL ALLOY SEAMLESS TUBE, MADE TO MEASURE FOR SPECIFIC USE IN AIRCRAFT ENGINE TRENT 700

  8411 91 00 · GB 2018 · GBBTI503967438

• TUBE ASSEMBLY FUEL 21- AMS5570 STAINLESS STEEL CORROSION AND HEAT RESISTANT SEAMLESS TUBE MADE TO MEASURE AND DESIGN SPECIFIC FOR AIRCRAFT ENGINE TRENT XWB

  8411 91 00 · GB 2018 · GBBTI503967634

• A PART DESIGNED SPECIFICALLY FOR TURBOJET AIRCRAFT. THE PRODUCT IS TUBE ASSEMBLY MADE FROM CORROSION AND HEAT RESISTANT NICKEL ALLOY SEAMLESS TUBE.

  8411 91 00 · GB 2018 · GBBTI503741180

• A PART DESIGNED SPECIFICALLY FOR TURBOJET AIRCRAFT. THE PART IS A STAINLESS STEEL STRAIGHT CONNECTOR MADE FROM CORROSION RESISTING STAINLESS STEEL. .

  8411 91 00 · GB 2018 · GBBTI503741082

• A LOWER SPLITTER CENTRE BLANKET THAT IS TO PROTECT THE LOWER SPLITTER FROM FLAMES IN A FIRE SITUATION. THE PART IS USED FOR THE HEAT SHIELD ON A TURBOFAN ENGINE USED ON AN AIRCRAFT. THE PRODUCT IS ATTACHED TO THE LOWER SPLITTER WITHIN THE ENGINE CORE AND IS POSITIONED NEAR THE FRONT OF THE ENGINE BEHIND THE FAN BLADES. THE PRODUCT IS MANUFACTURED FROM S526 CROSS CORRUGATED STAINLESS STEEL FOIL…

  8411 91 00 · GB 2016 · GB503202807