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Last Updated: April 20, 2026

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Last Updated: April 20, 2026

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Gyros or angular rate sensors, having any of the following and specially designed components therefor: (a) Specified to function at linear acceleration levels less than or equal to 100 g and having any of the following: 1. A rate range of less than 500 degrees per second and having any of the following: a. A ‘bias’‘stability’ of less (better) than 0,5 degree per hour, when measured in a 1 g environment over a period of one month, and with respect to a fixed calibration value; or b. An ‘angle random walk’ of less (better) than or equal to 0,0035 degree per square root hour; or Note : this paragraph does not apply to ‘spinning mass gyros’. 2. A rate range greater than or equal to 500 degrees per second and having any of the following: a. A ‘bias’‘stability’ of less (better) than 4 degrees per hour, when measured in a 1 g environment over a period of three minutes, and with respect to a fixed calibration value; or b. An ‘angle random walk’ of less (better) than or equal to 0,1 degree per square root hour; or Note : this paragraph does not apply to ‘spinning mass gyros’. (b) Specified to function at linear acceleration levels exceeding 100 g.

Code

7A002

EU Code

VII.A7.002

Category

ANNEX III - CATEGORY 7 — NAVIGATION AND AVIONICS

Subcategory

7A - Systems, Equipment and Components

Prohibited Supply To
IR
Authority
EU
Document

EU Regulation No 267/2012

Notes
  • All types of gyros usable in the systems specified in 1.A., 19.A.1 or 19.A.2., with a rated ‘drift rate’‘stability’ of less than 0,5 degrees (1 sigma or rms) per hour in a 1 g environment, and specially designed components therefor. Technical Notes: 1. ‘Drift rate’ is defined as the component of gyro output that is functionally independent of input rotation and is expressed as an angular rate. (IEEE STD 528-2001 paragraph 2.56) 2. ‘Stability’ is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition. (This definition does not refer to dynamic or servo stability.) (IEEE STD 528-2001 paragraph 2.247)
  • Accelerometers or gyros of any type, designed for use in inertial navigation systems or in guidance systems of all types, specified to function at acceleration levels greater than 100 g, and specially designed components therefor.Note:9.A.5. does not include accelerometers that are designed to measure vibration or shock.
Program information
Program information

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