Document ID: chunk:federal_register_of_legislation:F2017L00081:reg:25:p6
Version: federal_register_of_legislation:F2017L00081
Segment Type: reg
Provision Reference: reg 25 (pt 6/15)
Character Range: 172733–175798

Category VIII(e) and Category XII(d));
 (e) continuous output accelerometers or gyros of any type, specified to function at acceleration levels greater than 100 g (see Category XII(d));
 (f) inertial or other equipment using accelerometers described by subitems (c) and (e) above, and systems incorporating such equipment, and specially designed integration software therefor (see Category VIII (e) and Category XII(d)).
Note 1: Subitems (a) to (f) may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft.
Note 2: In subitem (d):
(a) drift rate is defined as the time rate of output deviation from the desired output. It consists of random and systematic components and is expressed as an equivalent angular displacement per unit time with respect to inertial space.
(b) stability is defined as standard deviation (1 sigma) of the variation of a particular parameter from its calibrated value measured under stable temperature conditions. This can be expressed as a function of time.

Item 10—Category II
  Flight control systems and "technology" as follows; designed or modified for the systems in Item 1.
 (a) hydraulic, mechanical, electro‑optical, or electro‑mechanical flight control systems (including fly‑by‑wire systems), (see Category IV (h));
 (b) attitude control equipment, (see Category IV, (c) and (h));
 (c) design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces to optimize aerodynamic performance throughout the flight regime of an unmanned air vehicle, (see Category VIII (k));
 (d) design technology for integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory, (see Category IV (i)).
Note: Subitems (a) and (b) may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft.

Item 11—Category II
  Avionics equipment, "technology" and components as follows; designed or modified for use in the systems in Item 1, and specially designed software therefor:
 (a) radar and laser radar systems, including altimeters (see Category XI(a)(3));
 (b) passive sensors for determining bearings to specific electromagnetic sources (direction finding equipment) or terrain characteristics (see Category XI(b) and (d));
 (c) global Positioning System (GPS) or similar satellite receivers:
 (1) capable of providing navigation information under the following operational conditions:
 (i) at speeds in excess of 515 m/sec (1,000 nautical miles/hours); and
 (ii) at altitudes in excess of 18 km (60,000 feet), (see Category XV(d)(2); or
 (2) designed or modified for use with unmanned air vehicles covered by Item 1 (see Category XV(d)(4)).
 (d) electronic assemblies and components specifically designed for military use and operation at temperatures in excess of 125 degrees C (see Category XI(a)(7)).
 (e) design technology for protection of avionics and electrical subsystems against