Nozzle Guide Vane for LEAP-1A Engine
Single-crystal superalloy nozzle guide vane (NGV) for the hot-section transition in CFM LEAP-1A turbofan powering Airbus A320neo. Features advanced cooling passages for turbine inlet temperatures. HTS 8411.99.90.90 as stationary aircraft gas turbine hardware.
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Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If certain cast iron aircraft turbine parts
Specific material-based provisions exist.
If superalloy ingot form before forging/casting
Ferrous scrap and waste materials classify under Chapter 72.
If incorporates integrated temperature measuring devices
Measuring instruments in parts shift to Chapter 90.
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Import Tips & Compliance
• Include thermal barrier coating specifications and EASA Form 1 airworthiness tag
• Declare as 'OEM replacement part' with serial number traceability
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