Code

EU Code

Categories

• ANNEX II - List of other goods and technology, including software, referred to in Article 3a
• ANNEX III - CATEGORY 7 — NAVIGATION AND AVIONICS

Subcategory

Prohibited Supply To

Authority

Document

Notes

• Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in the systems specified in 1.A., or 19.A.1. or 19.A.2. and specially designed components therefor.
• Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:a. Internal tilt compensation in pitch (+/– 90 degrees) and having roll (+/– 180 degrees) axes.b. Capable of providing azimuthal accuracy better (less) than 0,5 degrees rms at latitudes of +/– 80 degrees, referenced to local magnetic field; andc. Designed or modified to be integrated with flight control and navigation systems.Note:Flight control and navigation systems in Item 9.A.8. include gyrostabilisers, automatic pilots and inertial navigation systems.
• Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor.
• ‘Integrated navigation systems’, designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2. and capable of providing a navigational accuracy of 200 m CEP or less.Technical Note:An ‘integrated navigation system’ typically incorporates all of the following components:a.An inertial measurement device (e.g. an attitude and heading reference system, inertial reference unit, or inertial navigation system);b.One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight (e.g. satellite navigation receiver, radar altimeter, and/or Doppler radar); andc.Integration hardware and software.N.B. For integration “software”, see Item 9.D.4.