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Last Updated: April 20, 2026

Tooling specially designed for producing gas turbine engine powder metallurgy rotor components having all of the following: (a) Designed to operate at stress levels of 60 % of ultimate tensile strength (UTS) or more measured at a temperature of 873 K (600 °C); and (b) Designed to operate at 873 K (600 °C) or more. Note : The item above does not specify tooling for the production of powder.

Code

9B008

EU Code

IX.A9.019

Category

ANNEX II - Goods and technology referred to in points (a) and (c) of Article 3(1) and in Article 7

Subcategory

IX.A9.AEROSPACE AND PROPULSION

Prohibited Supply To
KP
Authority
EU
Document

EU Regulation 2017/1509

Program information
Program information

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