OpenLegislation

Paragraph 26 I1I2

United Kingdom

(1)

Resin-impregnated or pitch-impregnated fibres (prepregs), metal or carbon-coated fibres (preforms) or carbon fibre preforms, as follows—

(a)

made from fibrous or filamentary materials specified in paragraph 25;

(b)

epoxy resin matrix impregnated carbon fibrous or filamentary materials (prepregs), specified in Dual-Use codes 1C010.a., 1C010.b. or 1C010.c., for the repair of aircraft structures or laminates, of which the size of individual sheets does not exceed 50 cm × 90 cm;

(c)

prepregs specified in Dual-Use codes 1C010.a., 1C010.b. or 1C010.c., when impregnated with phenolic or epoxy resins having a glass transition temperature (Tg) less than 433 K (160 °C) and a cure temperature lower than the glass transition temperature.

(2)

In this paragraph the following terms have the meaning given to them in the Dual-Use Regulation—

  • “carbon fibre preforms”;

  • “fibrous or filamentary materials”;

  • “matrix”.

Annotations

Commencement

I1

Sch. 2 para. 26 not in force at made date, see reg. 1(2)

I2

Sch. 2 para. 26 in force at 31.12.2020 by S.I. 2019/627, reg. 7(2); 2020 c. 1, Sch. 5 para. 1(1)