Document ID: chunk:federal_register_of_legislation:F2016L01208:reg:10
Version: federal_register_of_legislation:F2016L01208
Segment Type: reg
Provision Reference: reg 10
Character Range: 15477–16263

10    The following resin‑impregnated or pitch‑impregnated fibres (prepregs), metal or carbon‑coated fibres (preforms) and carbon fibre preforms:
       (a) those made from fibrous or filamentary materials specified in item 9;
       (b) epoxy resin matrix impregnated carbon fibrous or filamentary materials (prepregs) meeting the following criteria:
       (i) usable for the repair of aircraft structures or laminates;
       (ii) in individual sheets of prepreg not exceeding 50 cm x 90 cm;
       (c) prepregs impregnated with phenolic or epoxy resins having:
       (i) a glass transition temperature (Tg) less than 433 K (160 °C); and
       (ii) a cure temperature lower than the glass transition temperature
      that are not specified in the Defence and Strategic Goods List