1A002"Composite" structures or laminates, as follows:

N.B. SEE ALSO 1A202, 9A010 and 9A110.
a. Made from any of the following:
1. An organic "matrix" and "fibrous or filamentary materials" specified in 1C010.c. or 1C010.d.: or
2. Prepregs or preforms specified in 1C010.e.;
b. Made from a metal or carbon "matrix", and any of the following:
1. Carbon "fibrous or filamentary materials" having all of the following:
a. A "specific modulus" exceeding 10,15 × 106 m; and
b. A "specific tensile strength" exceeding 17,7 × 104 m; or
2. Materials specified in 1C010.c.
Note 1:
1A002 does not control "composite" structures or laminates made from epoxy resin impregnated carbon "fibrous or filamentary materials" for the repair of "civil aircraft" structures or laminates, having all of the following:
a. An area not exceeding 1 m2;
b. A length not exceeding 2,5 m;
and
c. A width exceeding 15 mm.
Note 2:
1A002 does not control semi-finished items specially designed for purely civilian applications as follows:
a. Sporting goods;
b. Automotive industry;
c. Machine tool industry;
d. Medical applications.
Note 3:
1A002.b.1. does not control semi-finished items containing a maximum of two dimensions of interwoven filaments and specially designed for applications as follows:
a. Metal heat-treatment furnaces for tempering metals;
b. Silicon boule production equipment.
Note 4:
1A002 does not control finished items specially designed for a specific application.
Note 5:
1A002.b.1. does not control mechanically chopped, milled, or cut carbon "fibrous or filamentary materials" 25,0 mm or less in length.