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Navigation and Avionics Navigation and Avionics

Changes not yet applied. Later legislation changes this provision in ways not yet written into the text below:

Accelerometers designed for use in inertial navigation or guidance systems and having any of the following characteristics, and specially designed components thereforf1:

a.

A bias stability of less (better) than 130 micro g with respect to a fixed calibration value over a period of one year;

b.

A scale factor stability of less (better) than 130 ppm with respect to a fixed calibration value over a period of one year;

c.

Specified to function at linear acceleration levels exceeding 100 g.

  1. 7AEquipment, Assemblies and Components
  2. 7BTest, Inspection and Production Equipment
  3. 7CMaterials
  4. 7DSoftware
  5. 7ETechnology

Annotations

Footnotes

f1

See also entry 7A101.