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Last Updated: April 11, 2026

Electrical power generation gas turbines, components and related equipment as follows: (a) Gas Turbines specially designed for electrical power generation, having an output exceeding 200 MW; (b) Vanes, Stators, Combustion Chambers and Fuel Injection Nozzles, specially designed for electrical power generation gas turbines specified in II.A9.003.a; (c) Equipment specially designed for the “development” and “production” of electrical power generation gas turbines specified in II. A9.003.a.

Code

9A001

EU Code

II.A9.003

Categories
  • ANNEX II - List of other goods and technology, including software, referred to in Article 3a
  • ANNEX III - CATEGORY 9 — AEROSPACE AND PROPULSION
Subcategory

A9. Aerospace and Propulsion

Prohibited Supply To
IR
Authority
EU
Document

EU Regulation No 267/2012

Note

Turbojet and turbofan engines, as follows: a. Engines having both of the following characteristics: 1. ‘Maximum thrust value’ greater than 400 N (achieved un-installed) excluding civil certified engines with a ‘maximum thrust value’ greater than 8,89 kN (achieved un-installed); and 2. Specific fuel consumption of 0,15 kg N –1 h –1 or less (at maximum continuous power at sea level static conditions using the ICAO standard atmosphere); Technical Note: In 3.A.1.a.1., ‘maximum thrust value’ is the manufacturer's demonstrated maximum thrust for the engine type un-installed. The civil type certified thrust value will be equal to or less than the manufacturer's demonstrated maximum thrust for the engine type. b. Engines designed or modified for systems specified in 1.A. or 19.A.2., regardless of thrust or specific fuel consumption. Note: Engines specified in 3.A.1. may be exported as part of a manned aircraft or in quantities appropriate for replacement parts for a manned aircraft.

Program information
Program information

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