Document ID: chunk:federal_register_of_legislation:F2017L00081:reg:25:p13
Version: federal_register_of_legislation:F2017L00081
Segment Type: reg
Provision Reference: reg 25 (pt 13/15)
Character Range: 193315–196467

actuated by remote control or automatically after a lapse of time.
Note 11: Subparagraph (24)—the cluster munitions that are subject to this exclusion are set forth below:
 The Convention on Cluster Munitions, signed December 3, 2008, and entered into force on August 1, 2010, defines a "cluster munition" as:
 A conventional munition that is designed to disperse or release explosive submunitions each weighing less than 20 kilograms, and includes those explosive submunitions. Under the Convention, a "cluster munition" does not include the following munitions:
(a) a munition or submunition designed to dispense flares, smoke, pyrotechnics or chaff; or a munition designed exclusively for an air defence role;
(b) a munition or submunition designed to produce electrical or electronic effects;
(c) a munition that, in order to avoid indiscriminate area effects and the risks posed by unexploded submunitions, has all of the following characteristics:
 1) each munition contains fewer than ten explosive submunitions;
 2) each explosive submunition weighs more than four kilograms;
 3) each explosive submunition is equipped with an electronic self‑destruction mechanism; and
 4) each explosive submunition is equipped with an electronic self‑deactivating feature.
            No military assistance shall be furnished for cluster munitions, no defence export licence for cluster munitions may be issued, and no cluster munitions or cluster munitions technology shall be sold or transferred.
Note 12: Subparagraph (25)—a complete gas turbine engine with embedded hot section components or digital engine controls is eligible for export or transfer under the Treaty. Technical data, other than required for routine external maintenance and operation, related to the hot section or digital engine controls, as well as individual hot section parts or components are not eligible for the Treaty exemption whether shipped separately or accompanying a complete engine. Gas turbine hot section exempted Defence Article components and technology are combustion chambers and liners; high pressure turbine blades, vanes, disks and related cooled structure; cooled low pressure turbine blades, vanes, disks and related cooled structure; cooled augmenters; and cooled nozzles. Examples of gas turbine engine hot section developmental technologies are Integrated High Performance Turbine Engine Technology (IHPTET), Versatile, Affordable Advanced Turbine Engine (VAATE), and Ultra‑Efficient Technology (UEET), which are also excluded from export under the exemptions.
Note 13: Subparagraph (26)—a complete gas turbine engine with embedded hot section components or digital engine controls is eligible for export or transfer under the Treaty. Technical data, other than required for routine external maintenance and operation, related to the hot section or digital engine controls, as well as individual hot section parts or components are not eligible for the Treaty exemption whether shipped separately or accompanying a complete engine. Gas turbine hot section exempted Defence Article components and technology are combustion chambers and liners; high pressure