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Federal Register / Vol. 86, No. 58 / Monday, March 29, 2021 / Rules and Regulations
GBS: Yes for 1C006.d List of Items Controlled Related Controls: See also 1C996.
Related Definitions: N/A
Items:
a. Reserved b. Lubricating materials containing, as their principal ingredients, any of the following:
b.1. Phenylene or alkylphenylene ethers or thio-ethers, or their mixtures, containing more than two ether or thio-ether functions or mixtures thereof; or b.2. Fluorinated silicone fluids with a kinematic viscosity of less than 5,000 mm2/
s 5,000 centistokes measured at 298 K 25
C;
c. Damping or flotation fluids having all of the following:
c.1. Purity exceeding 99.8%;
c.2. Containing less than 25 particles of 200
mm or larger in size per 100 ml; and c.3. Made from at least 85% of any of the following:
c.3.a.Dibromotetrafluoroethane CAS
25497307, 124732, 27336238;
c.3.b.Polychlorotrifluoroethylene oily and waxy modifications only; or c.3.c.Polybromotrifluoroethylene;
d. Fluorocarbon fluids designed for electronic cooling and having all of the following:
d.1. Containing 85% by weight or more of any of the following, or mixtures thereof:
d.1.a. Monomeric forms of perfluoropolyalkylether-triazines or perfluoroaliphatic-ethers;
d.1.b. Perfluoroalkylamines;
d.1.c. Perfluorocycloalkanes; or d.1.d. Perfluoroalkanes;
d.2. Density at 298 K 25 C of 1.5 g/ml or more;
d.3. In a liquid state at 273 K 0 C; and d.4. Containing 60% or more by weight of fluorine.
Note: 1C006.d does not apply to materials specified and packaged as medical products.

24. In supplement no. 1 to part 774
the CCL, Category 1, ECCN 1C010 is revised to read as follow:

1C010 Fibrous or filamentary materials as follows see List of Items Controlled.
License Requirements Reason for Control: NS, NP, AT
Controls NS applies to entire entry.
NP applies to 1C010.a aramid fibrous or filamentary materials, b carbon fibrous and filamentary materials, and e.1
for fibrous and filamentary materials that meet or exceed the control criteria of ECCN
1C210.

VerDate Sep<11>2014

Country Chart See Supp. No. 1 to part 738
NS Column 2
NP Column 1

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Country Chart See Supp. No. 1 to part 738

Controls AT applies to entire entry.

AT Column 1

Reporting Requirements See 743.1 of the EAR for reporting requirements for exports under License Exceptions, and Validated End-User authorizations.
List Based License Exceptions See Part 740
for a Description of All License Exceptions LVS: $1500, N/A for NP
GBS: N/A
Special Conditions for STA
STA: License Exception STA may not be used to ship any item in 1C010.c to any of the destinations listed in Country Group A:6 See Supplement No.1 to part 740 of the EAR.
List of Items Controlled Related Controls: 1 See ECCNs 1E001
development and production and 1E201 use for technology for items controlled by this entry. 2 Also see ECCNs 1C210 and 1C990. 3 See also 9C110 for material not controlled by 1C010.e, as defined by notes 1 or 2.
Related Definitions: 1. Specific modulus:
Youngs modulus in pascals, equivalent to N/m2 divided by specific weight in N/m3, measured at a temperature of 2962 K
232C and a relative humidity of 505%. 2. Specific tensile strength:
Ultimate tensile strength in pascals, equivalent to N/m2 divided by specific weight in N/m3, measured at a temperature of 2962 K 232C and a relative humidity of 505%.
Items:
Technical Notes:
1. For the purpose of calculating specific tensile strength, specific modulus or specific weight of fibrous or filamentary materials in 1C010.a, 1C010.b or 1C010.c, the tensile strength and modulus should be determined by using Method A described in ISO 10618 2004 or national equivalents.
2. Assessing the specific tensile strength, specific modulus or specific weight of nonunidirectional fibrous or filamentary materials e.g., fabrics, random mats or braids in 1C010 is to be based on the mechanical properties of the constituent unidirectional monofilaments e.g., monofilaments, yarns, rovings or tows prior to processing into the non-unidirectional fibrous or filamentary materials.
a. Organic fibrous or filamentary materials, having all of the following:
a.1. Specific modulus exceeding 12.7 x 106 m; and a.2. Specific tensile strength exceeding 23.5 x 104 m;
Note: 1C010.a does not control polyethylene.
b. Carbon fibrous or filamentary materials, having all of the following:
b.1. Specific modulus exceeding 14.65 x 106 m; and
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b.2. Specific tensile strength exceeding 26.82 x 104 m;
Note: 1C010.b does not control:
a. Fibrous or filamentary materials, for the repair of civil aircraft structures or laminates, having all of the following:
1. An area not exceeding 1 m2;
2. A length not exceeding 2.5 m; and 3. A width exceeding 15 mm.
b. Mechanically chopped, milled or cut carbon fibrous or filamentary materials 25.0 mm or less in length.
c. Inorganic fibrous or filamentary materials, having all of the following:
c.1. Having any of the following:
c.1.a. Composed of 50% or more by weight silicon dioxide SiO2 and having a specific modulus exceeding 2.54 x 106 m; or c.1.b. Not specified in 1C010.c.1.a and having a specific modulus exceeding 5.6 x 106 m; and c.2. Melting, softening, decomposition or sublimation point exceeding 1,922 K 1,649
C in an inert environment;
Note: 1C010.c does not control:
a. Discontinuous, multiphase, polycrystalline alumina fibers in chopped fiber or random mat form, containing 3% by weight or more silica, with a specific modulus of less than 10 x 106 m;
b. Molybdenum and molybdenum alloy fibers;
c. Boron fibers;
d. Discontinuous ceramic fibers with a melting, softening, decomposition or sublimation point lower than 2,043 K 1,770
C in an inert environment.
d. Fibrous or filamentary materials, having any of the following:
d.1. Composed of any of the following:
d.1.a. Polyetherimides controlled by 1C008.a; or d.1.b. Materials controlled by 1C008.b to 1C008.f; or d.2. Composed of materials controlled by 1C010.d.1.a or 1C010.d.1.b and commingled with other fibers controlled by 1C010.a, 1C010.b or 1C010.c;
Technical Note: Commingled is filament to filament blending of thermoplastic fibers and reinforcement fibers in order to produce a fiber reinforcement matrix mix in total fiber form.
e. Fully or partially resin impregnated or pitch impregnated fibrous or filamentary materials prepregs, metal or carbon coated fibrous or filamentary materials preforms or carbon fiber preforms, having all of the following:
e.1. Having any of the following:
e.1.a. Inorganic fibrous or filamentary materials controlled by 1C010.c; or e.1.b. Organic or carbon fibrous or filamentary materials, having all of the following:
e.1.b.1. Specific modulus exceeding 10.15 x 106 m; and e.1.b.2 Specific tensile strength exceeding 17.7 x 104 m; and e.2. Having any of the following:
e.2.a. Resin or pitch, controlled by 1C008
or 1C009.b;
e.2.b. Dynamic Mechanical Analysis glass transition temperature DMA Tg equal to or exceeding 453 K 180 C and having a phenolic resin; or
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