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Good

Last Updated: May 31, 2026

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Last Updated: May 31, 2026

Good

b. Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in ‘missiles’;

Code

7A103

EU Code

M9A1

Categories

  • ANNEX III - CATEGORY 7 — NAVIGATION AND AVIONICS
  • ANNEX II - Goods and technology referred to in Articles 2(1), 2(2) and 2(4), 3(3), 5(1), 8(4), 17(2), 31(1) and 45

Subcategory

A7. Navigation and Avionics

Prohibited Supply To

IR

Authority

EU

Document

EU Regulation No 267/2012

Date of Delisting

2026-04-12

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.
  • ‘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.
  • 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.
Program information

Program information

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