Document ID: chunk:federal_register_of_legislation:F2016L01208:reg:7
Version: federal_register_of_legislation:F2016L01208
Segment Type: reg
Provision Reference: reg 7
Character Range: 34153–35398

7     Inertial or other equipment using:
       (a) linear accelerometers designed for use in inertial navigation systems or guidance systems and having either:
              (i) a bias stability of less than 130 micro g in relation to a fixed calibration value over a period of one year; or
              (ii) a scale factor stability of less than 130 ppm in relation to a fixed calibration value over a period of one year; and
       (b) linear accelerometers specified to function at linear acceleration levels greater than 100 g; and
       (c) linear accelerometers (other than a linear accelerometer that is specially designed and developed as an MWD sensor for use in downhole well services operations), designed for use in inertial navigation systems or in guidance systems of all types, and usable in missiles, having both of the following characteristics:
              (i) a bias repeatability of less than 1 250 micro g, with one sigma standard deviation in relation to a fixed calibration over a period of one year;
              (ii) a scale factor repeatability of less than 1 250 ppm, with one sigma standard deviation in relation to a fixed calibration over a period of one year; and
       (d) continuous output accelerometers