ECCN 7A003

NSMTAT

'Inertial measurement equipment or systems', having any of the following.

Category: 7 - NavigationProduct Group: A - EquipmentLast Updated: 2026-04-10

What This ECCN Covers

ECCN 7A003 controls inertial measurement equipment and systems (IMUs/INS) — including units that integrate satellite navigation or "Data-Based Referenced Navigation" — that meet specified accuracy thresholds for aircraft, land vehicles, vessels, or missiles. These systems provide self-contained position, velocity, and attitude data, which is why navigation-grade units are tightly controlled for National Security, Missile Technology, and Anti-Terrorism.

Who needs to check this?

Manufacturers of inertial navigation systems, GPS/INS units, and guidance packages for aerospace, marine, and autonomous platforms.

Compliance tip

As a Missile Technology entry, 7A003 generally does not permit license exceptions, and missile or UAV end use raises end-user controls under EAR Part 744. Classification hinges on stated position and velocity accuracy — review the entry's parameters and the associated Technical Notes for the conditions under which accuracy is measured.

Reviewed by Jack Tan · Last reviewed: Jun 4, 2026

Items Covered

  • a."Satellite navigation system";
  • b."Data-Based Referenced Navigation" ("DBRN").
  • a.Designed for "aircraft", land vehicles or vessels, providing position without the use of 'positional aiding references', and having any of the following "accuracies" subsequent to normal alignment:
  • 1. 0.8 nautical miles per hour (nm/hr) "Circular Error Probable" ("CEP") rate or less (better);
  • 2. 0.5% distanced travelled "CEP" or less (better); or
  • 3. Total drift of 1 nautical mile "CEP" or less (better) in a 24 hr period;
  • b.Designed for "aircraft", land vehicles or vessels, with an embedded 'positional aiding reference' and providing position after loss of all 'positional aiding references' for a period of up to 4 minutes, having an "accuracy" of less (better) than 10 meters "CEP";
  • c.Designed for "aircraft", land vehicles or vessels, providing heading or True North determination and having any of the following:
  • 1. A maximum operating angular rate less (lower) than 500 deg/s and a heading "accuracy" without the use of 'positional aiding references' equal to or less (better) than 0.07 deg sec (Lat) (equivalent to 6 arc minutes rms at 45 degrees latitude); or
  • 2. A maximum operating angular rate equal to or greater (higher) than 500 deg/s and a heading "accuracy" without the use of 'positional aiding references' equal to or less (better) than 0.2 deg sec (Lat) (equivalent to 17 arc minutes rms at 45 degrees latitude);
  • d.Providing acceleration measurements or angular rate measurements, in more than one dimension, and having any of the following:
  • 1. Performance specified by 7A001 or 7A002 along any axis, without the use of any aiding references; or
  • 2. Being "space-qualified" and providing angular rate measurements having an "angle random walk" along any axis of less (better) than or equal to 0.1 degree per square root hour.

Control Reasons

NSNational Security

Items controlled for national security reasons under multilateral export control regimes.

Column 1: YesColumn 2: No
MTMissile Technology

Items controlled under the Missile Technology Control Regime (MTCR).

Column 1: YesColumn 2: No
ATAnti-Terrorism

Items controlled for anti-terrorism reasons. Most items on the CCL have AT controls.

Column 1: YesColumn 2: No

Disclaimer

This information is for reference only. For official classifications, consult BIS or a qualified export control professional.

Official Reference