TRANSPORTATION DATASHEETS

• EHG250-44-37 Prepreg material for secondary structures in aircraft
  EHG250-44-37 consists of a E-glass fabricUS Style 120, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarnStyle 120, 105 g/m2, crowfoot 1/3, preimpregnated with 40% epoxy resin EH250 (125°C).
• EHG250-44-55 Prepreg material for secondary structures in aircraft
  EHG250-44-55 consists of a E-glass fabricUS Style 120, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarn Style 120, 105 g/m2, crowfoot 1/3, preimpregnated with 58% epoxy resin EH250 (125°C).
• EHG250-46-37 Prepreg material for secondary structures in aircraft
  EHG250-46-37 consists of a E-glass fabric Style 1543, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarnStyle 1543, 288 g/m2, crowfoot 1/3, preimpregnated with 40% epoxy resin EH250 (125°C).
• EHG250-48-50 Prepreg material for secondary structures in aircraft
  EHG250-48-50 consists of a E-glass fabric, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarn, 163 g/m², twill 2/2 preimpregnated with 53% epoxy resin EH250 (125ºC).
• EHG250-54-37 Prepreg material for secondary structures in aircraft
  EHG250-54-37 consists of a E-glass fabric, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarn, 390 g/m², twill 2/2 preimpregnated with 40% epoxy resin EH250 (125ºC).
• EHG250-54-50 Prepreg materials for secondary structures in aircraft
  EHG250-54-50 consists of a E-glass fabric, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarn, 390 g/m², twill 2/2 preimpregnated with 53% epoxy resin EH250 (125ºC).
• EHG250-68-37 Prepreg materials for secondary structures in aircraft
  EHG250-68-37 consists of a E-glass fabric US Style 7781, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% epoxy resin EH250 (125ºC).
• EHG250-68-50 Prepreg materials for secondary structures in aircraft
  EHG250-68-50 consists of a E-glass fabric US Style 7781, impregnated with the epoxy resin EH250. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 53% epoxy resin EH250 (125ºC).
• EHG275-44-37 Prepreg materials for secondary structures in aircraft
  EHG275-68-50 consists of a E-glass fabric Style 120, impregnated with the epoxy resin EH275. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 40% epoxy resin EH275 (180ºC).
• EHG275-44-55 Prepreg materials for secondary structures in aircraft
  EHG275-44-55consists of a E-glass fabric Style 120, impregnated with the epoxy resin EH275. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 58% epoxy resin EH275 (180ºC).
• EHG275-68-37 Prepreg materials for secondary structures in aircraft
  EHG275-68-37 consists of a E-glass fabric Style 7781, impregnated with the epoxy resin EH275. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% epoxy resin EH275 (180ºC).
• EHG275-68-50 Prepreg materials for secondary structures in aircraft
  EHG275-68-50 consists of a E-glass fabric Style 7781, impregnated with the epoxy resin EH275. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 53% epoxy resin EH275 (180ºC).
• EHG420C-68-40 Prepreg material used in cargo floor (v2)
  Fiber reinforced thermosetting preimpregnated material for aircraft parts (e.g. secondary structures). Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% epoxy resin EH420 (125ºC).
• EHG420CS-300-37 Prepreg materials for aircraft interiors (v2)
  Fiber reinforced thermosetting preimpregnated material for aircraft parts (e.g. secondary structures). Woven fabric of E-glass filament yarn, 300 g/m², 8H satin, preimpregnated with 37% epoxy resin EH420C (120ºC).
• EHKF420-20-48 Prepreg material used in passenger interiors (v2)
  Fiber reinforced thermosetting preimpregnated material for aircraft parts (e.g. secondary structures). Woven fabric of carbon fiber, 200 g/m², twill 2/2, preimpregnated with 48% epoxy resin EH420 (120ºC).
• EHKF420C-C20-45 Prepreg material used in passenger interiors (v2)
  Fiber reinforced thermosetting preimpregnated material for aircraft parts (e.g. secondary structures). Woven fabric of 3k HTA carbon fiber, 204 g/m², twill 2/2, preimpregnated with 40% epoxy resin EH420 (125ºC).
• EHKF420-UD24k-40 Prepreg material used in passenger interiors (v2)
  Fiber reinforced thermosetting preimpregnated material for aircraft parts (e.g. secondary structures). Unidirectional 24k carbon fiber, 210 g/m², preimpregnated with 40% epoxy resin EH420 (120ºC).
• EP121-44-50 Prepreg material used in passenger floors (v1)
  EP121-44-50 consists of a fibreglass fabric, impregnated with the epoxy resin EP121. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 50% epoxy resin EP121 (125ºC).
• EP121-44-55 Prepreg material used in passenger floors (v1)
  EP121-44-55 consists of a fibreglass fabric, impregnated with the epoxy resin EP121. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 55% epoxy resin EP121 (125ºC).
• EP121-48-50 Prepreg material used in passenger floors (v1)
  EP121-48-50 consists of a fibreglass fabric, impregnated with the epoxy resin EP121. Woven fabric of E-glass filament yarn, 163 g/m², twill 2/2, preimpregnated with 50% epoxy resin EP121 (125ºC).
• EP121-68-40 Prepreg material used in passenger floors (v1)
  EP121-68-40 consists of a fibreglass fabric Style 7781, impregnated with the epoxy resin EP121. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% epoxy resin EP121 (125ºC).
• EP121-68-50 Prepreg material used in passenger floors (v1)
  EP121-68-50 consists of a fibreglass fabric Style 7781, impregnated with the epoxy resin EP121. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 50% epoxy resin EP121 (125ºC).
• EP121-C08-45 Prepreg material used in secondary structures and passenger floors (v2)
  EP121-C08-45 consists of a carbon fibre fabric impregnated with the epoxy resin EP121. Woven fabric of 3k HTA carbon fiber, 160 g/m², plain weave, preimpregnated with 45% epoxy resin EP121 (125ºC).
• EP121-C08-53 Prepreg material used in passenger floors (v1)
  EP121-C08-53 consists of a carbon fibre fabric impregnated with the epoxy resin EP121. Woven fabric of 3k HTA carbon fiber, 160 g/m², plain weave, preimpregnated with 53% epoxy resin EP121 (125ºC).
• EP121-C15-53 Prepreg material used in passenger floors (v2)
  EP121-C15-53 consists of a 3k HTA carbon fabric, impregnated with the epoxy resin EP121. Woven fabric of 3k HTA carbon fiber, 193 g/m², plain weave, preimpregnated with 53% epoxy resin EP121 (125ºC).
• EP121-C20-45 Prepreg material used in secondary structures and passenger floors (v2)
  EP121-C20-45 consists of a 3k HTA carbon fabric, impregnated with the epoxy resin EP121. Woven fabric of 3k HTA carbon fiber, 204 g/m², twill 2/2, preimpregnated with 45% epoxy resin EP121 (125ºC).
• EP121-C25-45 Prepreg material used in secondary structures and passenger floors (v2)
  EP121-C25-45 consists of a 3k HTA carbon fabric, impregnated with the epoxy resin EP121. Woven fabric of 3k HTA carbon fiber, 285 g/m², 5H satin, preimpregnated with 45% epoxy resin EP121 (125ºC).
• EP121-C426-45 Prepreg material used in passenger floors (v1)
  EP121-C25-45 consists of a 12k HTA carbon fabric, impregnated with the epoxy resin EP121. Woven fabric of 12k carbon fiber, 400 g/m², twill 2/2, preimpregnated with 45% epoxy resin EP121 (125ºC).
• EP121-CR500_130-G138-42 Prepreg material for secondary structures in aircraft (v2)
  Fiber reinforced thermosetting preimpregnated material for aircraft parts (e.g. passenger floor, secondary structures). Woven fabric of 3k HTA carbon fiber, 204 g/m², twill 2/2, preimpregnated with 45% epoxy resin EP121 (125ºC).
• EP121-G218-50 Prepreg material used in passenger floors (v2)
  EP121-G218-50 consists of a S2-glass fabric Style 6580, impregnated with the epoxy resin EP121. Woven fabric of S2-glass filament yarn Style 6580, 190 g/m², 8shaft satin, preimpregnated with 50% epoxy resin EP121 (125ºC).
• EP121-G220-50 Prepreg material used in passenger floors (v1)
  EP121-G220-50 consists of a S2-glass fabric Style 6781, impregnated with the epoxy resin EP121. Woven fabric of S2-glass filament yarn Style 6781, 305 g/m², 8H satin, preimpregnated with 50% epoxy resin EP121 (125ºC).
• EP137-03-40 Prepreg material used in passenger floors (v2)
  EP137-03-40 consists of a E-glass fabric Style 1080, impregnated with the epoxy resin EP137. Woven fabric of E-glass filament yarn Style1080, 48 g/m², plain weave, preimpregnated with 40% epoxy resin EP137 (125ºC).
• EP137-CR527/100-35 Prepreg material used in passenger floors (v2)
  EP137-CR527/100-35 consists of unidirectional 24k IMS carbon fiber,impregnated with the epoxy resin EP137. Unidirectional 24k IMS carbon fiber, 100 g/m², preimpregnated with 35% epoxy resin EP137 (125ºC).
• EP137-CR527/100-35-G138-74 Prepreg material used in passenger floors (v1)
  EP137-CR527/100-35-G138-74 consists of unidirectional 24k IMS carbon fiber, impregnated with the epoxy resin EP137. Unidirectional 24k IMS carbon fiber, 100 g/m²,preimpregnated with 35%, Eglass scrim, 25 g/m², preimpregnated with 74% epoxy resin EP137 (125ºC).
• EP137-CR527/100-G138-50 Prepreg material used in passenger floors (v1)
  EP137-CR527/100-35-G138-74 consists of unidirectional 24k IMS carbon fiber, impregnated with the epoxy resin EP137. Unidirectional 24k IMS carbon fiber, 100 g/m²,preimpregnated with 35%, Eglass scrim, 25 g/m², preimpregnated with 74% epoxy resin EP137 (125ºC).
• EP137-CR527/120-35 Prepreg material used in passenger floors (v2)
  EP137-CR527/120-35 consists of unidirectional 24k IMS carbon fiber, impregnated with the epoxy resin EP137. Unidirectional 24k IMS carbon fiber, 120 g/m², preimpregnated with 35% epoxy resin EP137 (125ºC).
• EP137-CR527/80-35 Prepreg material used in passenger floors (v2)
  EP137-CR527/80-35 consists of unidirectional 24k IMS carbon fiber, impregnated with the epoxy resin EP137. Unidirectional 24k IMS carbon fiber, 80 g/m², preimpregnated with 35% epoxy resin EP137 (125ºC).
• EP137-G228-40 Prepreg material used in passenger floors (v2)
  EP137-G228-40 consists of a S2-glass fabric Style 6522, impregnated with the epoxy resin EP137. Woven fabric of S2-glass filament yarn Style 6522, 115 g/m², 8H satin, preimpregnated with 40% epoxy resin EP137 (125ºC).
• EP141-G218-40 Prepreg material used in cargo floor (v2)
  EP141-G218-40 consists of a S2-glass fabric Style 6580, impregnated with the epoxy resin EP141. Woven fabric of S2-glass filament yarn Style 6580, 190 g/m², 8H satin, preimpregnated with 40% epoxy resin EP141 (125ºC).
• PB1000 Modified Benzoxazine Resin (Next Generation Prepreg for Aircraft Interiors) v2
  Gurit is proud to present its next generation of aircraft interior prepregs based on PB1000. PB1000 is a modified benzoxazine resin that is without free formaldehyde and phenol and satisfies the most recent environmental standards like AIRBUS AP2091.
• PB1000-68-40 T0 Modified Benzoxazine Resin (Next Generation Prepreg for Aircraft Interiors) v21
  Fiber reinforced thermosetting preimpregnated material for transportation vehicle parts (e.g interior. Woven fabric of E-glass filament yarn, 296 g/m², Atlas 1/7, preimpregnated with 40% Poly-Benzoxazine resin PB1000.
• PF800-C15-45 Prepreg material used in passenger interiors (v2)
  PF800-C15-45 consists of a 3k HTA carbon fabric, impregnated with the phenolic resin PF800. Woven fabric of 3k HTA carbon fiber, 193 g/m², plain weave, preimpregnated with 45% phenolic resin PF800.
• PF800-G213-24 BR Prepreg material used in passenger interiors (v2)
  PF800-G213-24 BR consists of an E-glass fabric, impregnated with the phenolic resin PF800 (brown coloured). Woven fabric of E-glass roving, US Style 590, plain weave preimpregnated with 24 % phenolic resin PF 800 brown coloured
• PF800-GR101_180-G131-50 Prepreg material used in passenger interiors (v2)
  PF800-GR101/180-G131-50 is a prepreg material consisting of undirektionally 12k HTS aligned endless carbon fibres impregnated with the thermosetting phenolic resin PF800. Unidirectionally alligned, continous fibreglass filaments impregnated with the thermosetting phenolic resin PF800. The glass fibre layer is backed with a woven fibreglass scrim ply on one side.
• PF801-03-40 Prepreg material used in passenger floors (v2)
  PF801-03-40 consists of a E-glass fabric Style 0180, impregnated with the phenolic novolac resin PF801. Woven fabric of E-glass filament yarn Style 0180, 48 g/m², pain weave, preimpregnated with 40% phenolic resin PF801.
• PF801-44-53 Prepreg material used in passenger floors (v2)
  PF801-44-53 consists of a E-glass fabric Style 120, impregnated with the phenolic novolac resin PF801. Woven fabric of E-glass filament yarn Style 120, 105 g/m², plain weave, preimpregnated with 53% phenolic resin PF801.
• PF801-C08-43 Prepreg material used in passenger floors (v2)
  PF801-C08-43 consists of a 3k HTA carbon fabric, impregnated with the phenolic novolac resin PF801. Woven fabric of 3k HTA carbon fiber, 160 g/m², plain weave, preimpregnated with 43% phenolic resin PF801.
• PF801-C15-50 Prepreg material used in passenger floors (v2)
  PF801-C15-50 consists of a 3k HTA carbon fabric, impregnated with the phenolic novolac resin PF801. Woven fabric of 3k HTA carbon fiber, 193 g/m², plain weave, preimpregnated with 50% phenolic resin PF801.
• PF808-44-40 Prepreg material used in cargo lining (v2)
  PF808-44-40 consists of a E-glass fabric Style 120, impregnated with the phenolic resol resin PF808. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 40% phenolic resin PF808.
• PF808-44-53 Prepreg material used in cargo lining (v2)
  PF808-44-53 consists of a E-glass fabric Style 120, impregnated with the phenolic resol resin PF808. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 53% phenolic resin PF808.
• PF808-48-53 Prepreg material used in cargo lining (v2)
  PPF808-48-53 consists of a E-glass fabric, impregnated with the phenolic resol resin PF808. This resin is designed for high temperature stability, outstanding heat-release and smokedensity properties and excellent adhesion to honeycomb cores and metallic substrates.
• PF808-68-53 Prepreg material used in cargo lining (v2)
  PF808-68-53 consists of a E-glass fabric Style 7781, impregnated with the phenolic resol resin PF808. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 53% phenolic resin PF808.
• PF808-G218-40 Prepreg material used in cargo lining (v2)
  PF808-G218-40 consists of a S2-glass fabric Style 6580, impregnated with the phenolic resol resin PF808. Woven fabric of S2-glass filament yarn Style 6580, 190 g/m², 8H satin, preimpregnated with 40% phenolic resin PF808.
• PF808-G218-50 Prepreg material used in cargo lining (v2)
  PF808-G218-50 consists of a S2-glass fabric Style 6580, impregnated with the phenolic resol resin PF808. Woven fabric of S2-glass filament yarn Style 6580, 190 g/m², 8H satin, preimpregnated with 50% phenolic resin PF808.
• PF808-G220-40 Prepreg material used in cargo lining (v2)
  PF808-G220-40 consists of a S2-glass fabric Style 6781, impregnated with the phenolic resol resin PF808. Woven fabric of S2-glass filament yarn Style 6781, 305 g/m², 8H satin, preimpregnated with 40% phenolic resin PF808.
• PF808-G220-50 Prepreg material used in cargo lining (v2)
  PF808-G220-50 consists of a S2-glass fabric Style 6781, impregnated with the phenolic resol resin PF808. Woven fabric of S2-glass filament yarn Style 6781, 305 g/m², 8H satin, preimpregnated with 50% phenolic resin PF808.
• PF811-44-50 Prepreg material used in passenger interiors (v2)
  PF811-44-50 consists of a E-glass fabric Style 120, impregnated with the phenolic resin PF811. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 50% phenolic resin PF811.
• PF811-68-40 Prepreg material used in passenger interiors (v2)
  PF811-68-40 consists of a E-glass fabric Style 7781, impregnated with the phenolic resin PF811. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% phenolic resin PF811.
• PF811-7628-40 Prepreg material used in passenger interiors (v2)
  PF811-7628-40 consists of a E-glass fabric Style 7628, impregnated with the phenolic resin PF811. Woven fabric of E-glass filament yarn Style 7628, 203 g/m², plain weave, preimpregnated with 40% phenolic resin PF811.
• PF811-7628-43 Prepreg material used in passenger interiors (v2)
  PF811-7628-43 consists of a E-glass fabric Style 7628, impregnated with the phenolic resin PF811. Woven fabric of E-glass filament yarn Style 7628, 203 g/m², plain weave, preimpregnated with 43% phenolic resin PF811.
• PF811-C15-45 Prepreg material used in passenger interiors (v2)
  PF811-C15-45 consists of a 3k HTA carbon fabric, impregnated with the phenolic resin PF811. Woven fabric of 3k HTA carbon fiber, 193 g/m², plain weave, preimpregnated with 45% phenolic resin PF811.
• PF811-C593-43 Prepreg material used in passenger interiors (v2)
  PF811-C593-43 consists of a 3k HTA carbon fabric, impregnated with the phenolic resin PF811. Woven fabric of 3k HTA carbon fiber, 135 g/m², open weave, preimpregnated with 43% phenolic resin PF811.
• PF811-F200 Prepreg material used in passenger interiors (v2)
  PF811-F200 is a combination of Woven fabric of E-glass filament yarn Style 2037, 48 g/m², plain weave and carbon filament yarn 200 g/m2 unidirectional (90°/0°), preimpregnated with 3 8% phenolic resin PF811.
• PF811-G226-40 Prepreg material used in passenger interiors (v2)
  PF811-G226-40 consists of a S2-glass fabric Style 6580, impregnated with the phenolic resin PF811. Woven fabric of S2-glass filament yarn Style 6580, 190 g/m², 8H satin, preimpregnated with 40% phenolic resin PF811.
• PF811-G231-32 Prepreg material used in passenger interiors (v2)
  PF811-G231-32 consists of a E-glass fabric Style 93133, impregnated with the phenolic resin PF811. Woven fabric of E-glass filament yarn Style 93133, 250 g/m², open weave "leno", preimpregnated with 32% phenolic resin PF811.
• PF812-C15-45 Prepreg material used in passenger interiors (v2)
  PF812-C15-45 consists of a carbon fibre fabric, impregnated with the phenolic resol resin PF812. Woven fabric of 3k HTA carbon fiber, 193 g/m², plain weave, preimpregnated with 45% phenolic resin PF811
• PF812-G226-40 Prepreg material used in passenger interiors (v2)
  PF812-G226-40 consists of a S2-glass fabric Style 6580, impregnated with the phenolic resin PF812. Woven fabric of S2-glass filament yarn Style 6580, 190 g/m², 8H satin, preimpregnated with 40% phenolic resin PF812.
• PH840-300-42 Prepreg material for rail interior parts (v1)
  PH840-300-42 is a halogenfree modified phenolic system, designed for laminate with bright colour and good surface quality. Woven fabric of E-glass filament yarn, 300 g/m2, 8H satin, preimpregnated with 42% phenolic resin PH840
• PH840-600-40 Prepreg material for rail interior parts (v1)
  PH840-600-40 is a halogenfree modified phenolic system, designed for laminate with bright colour and good surface quality. Woven E-glass fabric, 600 g/m2, Satin HD Special, preimpregnated with 40% phenolic resin PH840
• PH840-M850-37 Prepreg material for rail interior parts (v1)
  Non-crimp-fabric reinforced thermosetting preimpregnated materials for railway parts (e.g. fairings, window-, ceiling- and floor panels). n E -Glass, 850 g/m2, Non-Crimp-Fabric, preimpregnated with 37% phenolic resin PH840
• PHG 840-7628-43 Prepreg material for rail interior parts (v1)
  PHG840-7628-43 is a halogenfree modified phenolic system,designed for laminate with bright colour and good surface quality. Woven fabric of E-glass filament yarn Style 7628, 204 g/m², plain weave, preimpregnated with 43% phenolic resin PH840
• PHG600-44-37 Prepreg material used in passenger interiors (v2)
  PHG600-44-37 consists of a E-glass fabric Style 120,impregnated with the phenolic resin PH600. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 40% phenolic resin PH600.
• PHG600-44-50 Prepreg material used in passenger interiors (v2)
  PHG600-44-50 consists of a E-glass fabric Style 120,impregnated with the phenolic resin PH600. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 53% phenolic resin PH600.
• PHG600-48-37 Prepreg material used in passenger interiors (v2)
  PHG600-48-37 consists of a E-glass fabric Style 1543,impregnated with the phenolic resin PH600. Woven fabric of E-glass filament yarn, 163 g/m², twill 2/2, preimpregnated with 40% phenolic resin PH600.
• PHG600-48-50 Prepreg material used in passenger interiors (v2)
  PHG600-48-50 consists of a E-glass fabric,impregnated with the phenolic resin PH600. Woven fabric of E-glass filament yarn, 163 g/m², twill 2/2, preimpregnated with 53% phenolic resin PH600.
• PHG600-68-37 Prepreg material used in passenger interiors (v2)
  PHG600-68-37 consists of a E-glass fabric Style 7781,impregnated with the phenolic resin PH600. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% phenolic resin PH600.
• PHG600-68-44 Prepreg material used in passenger interiors (v2)
  PHG600-68-44 consists of a E-glass fabric Style 7781,impregnated with the phenolic resin PH600. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 44% phenolic resin PH600.
• PHG600-68-50 Prepreg material used in passenger interiors (v2)
  PHG600-68-50 consists of a E-glass fabric Style 7781,impregnated with the phenolic resin PH600. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 53% phenolic resin PH600.
• PHG831-44-40 Prepreg material used in passenger interiors (v2)
  PHG831-44-40 consists of a E-glass fabric Style 120, impregnated with the phenolic resin PH831. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 40% phenolic resin PH831.
• PHG831-48-40 Prepreg materials for aircraft interiors
  PHG831-48-40 consists of a E-glass fabric, impregnated with the phenolic resin PH831. Woven fabric of E-glass filament yarn, 163 g/m², twill 2/2, preimpregnated with 40% phenolic resin PH831.
• PHG831-68-40 Prepreg materials for aircraft interiors
  PHG831-68-40 consists of a E-glass fabric Style 7781, impregnated with the phenolic resin PH831. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% phenolic resin PH831.
• PHG840-300-50 Prepreg material for rail interior parts (v1)
  PHG840-300-50 is a halogenfree modified phenolic system,designed for laminate with bright colour and good surface quality. Woven fabric of E-glass filament yarn, 300 g/m², 8H satin, preimpregnated with 50% phenolic resin PH840.
• PN900-44-43 Prepreg material used in airducts (v2)
  PN900-44-43 consists of a E-glass fabric Style 120, impregnated with the thermosetting resin PN900. Woven fabric of E-glass filament yarn Style 120, 105 g/m², crowfoot 1/3, preimpregnated with 43% cyanate ester resin PN900.
• PN900-68-40 Prepreg material used in airducts (v2)
  PN900-68-40 consists of a E-glass fabric Style 7781, impregnated with the thermosetting resin PN900. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 40% cyanate ester resin PN900.
• PN900-68-43 Prepreg material used in airducts (v2)
  PN900-68-43 consists of a E-glass fabric Style 7781, impregnated with the thermosetting resin PN900. Woven fabric of E-glass filament yarn Style 7781, 296 g/m², 8H satin, preimpregnated with 43% cyanate ester resin PN900.
• PN900-C582-43 Prepreg material used in airducts (v2)
  PN900-G205-43 consists of a 50/50 3k HTA carbon fiber and Eglass hybrid fabric, impregnated with the thermosetting resin PN900. Woven 50/50 hybrid fabric of 3k HTA carbon fiber and E-glass filament yarn, 180 g/m², twill 2/2, preimpregnated with 43% cyanate ester resin PN900.
• PN900-G205-43 Prepreg material used in airducts (v2)
  PN900-G205-43 consists of a E-glass fabric, impregnated with the thermosetting resin PN900. Woven fabric of E-glass filament yarn, 230 g/m², cross twill, preimpregnated with 43% cyanate ester resin PN900.
• PN900-G233-38 Prepreg material used in airducts (v2)
  PN900-G233-38 consists of a E-glass grid fabric, impregnated with the thermosetting resin PN900. Woven fabric of E-glass filament yarn, 240 g/m², leno, preimpregnated with 38% cyanate ester resin PN900, which is based on polymerised aromatic cyanate ester compounds.
• PN901-G219-42 Prepreg material used in airducts (v2)
  PN901-G219-42 is a prepreg material consisting of a high purity pure fused silica fabric impregnated with the thermoset resin PN901, based on Polymeric Cyanate Ester compounds. Woven fabric of Astroquartz yarn, 285 g/m², 8 shaft satin, preimpregnated with 42% thermoset resin matrix PN901, which is based on polymerised aromatic cyanate ester compounds.
• S-Core - SPRINT® Core Material (v4)
  The S-Core, or SPRINT® core, is a moulding material that consists of a single layer of a polyester non woven material, that has a pressure stable honeycomb structure, applied to a precast, precatalysed resin film.
• SF 95PF - Sandable Surfacing Film (v2)
  The SF 95PF surfacing material is a grey filled epoxy film designed to enhance the surface finish of moulded composite components. It allows a good surface finish to be obtained by vacuum-bag moulding processes.
• SPRINT® SF 80FB - Fire-Barrier Surfacing Film (v2)
  SF 80FB surfacing material is a black, filled epoxy film containing a 320g intumescent layer. Typical applications include the protection of structural components in high risk areas such as engine bays, exhaust runs, and around the fuelsystem.
• SPRINT® SF 80FR OBL - Fire Retardant Surfacing Film (v2)
  SF 80FR OBL surfacing material is a black, filled epoxy film. It provides an effective fire retarding layer capable of withstanding exposure to fire, while preventing the epoxy substrate from combustion.
• SPRINT® SF 95VH - Abrasion-Resistant Surfacing Film
  SF 95VH surfacing material is a very hard, abrasion-resistant, grey filled epoxy film. It is designed to protect vulnerable underbody components from damage caused by foreign objects.
• ST 85 - Carbon Structural SPRINT® (v2)
  The patent-approved ST 85 Structural SPRINT® is a moulding material that consists of a layer of woven carbon fabric either side of a precast, precatalysed resin film. The material therefore has the appearance of dry reinforcement which has resin concealed at its centre.
• ST 85OBL Skewered - Structural SPRINT® (v9)
  The patent-approved ST 85OBL-Skewed Carbon Structural SPRINT® is a moulding material that consists of layers of unidirectional carbon fabric skewed to ± 45º angles either side of a precast, precatalysed resin film.
• ST 86OBL - Woven Glass Structural SPRINT® (v2)
  ST86-OBL Woven Glass Structural SPRINT® is a moulding material that consists of a layer of woven glass fabric either side of a precast, precatalysed resin film.
• ST 94 - Single SPRINT® (v4)
  ST 94 Single SPRINT® is a moulding material that consists of a layer of dry reinforcement plied to a precast, precatalysed resin film. ST 94 is a toughened hot-melt, epoxy resin that offers an extremely good balance of mechanical properties.
• ST 95 - Carbon Structural SPRINT® (v4)
  The patent-approved ST 95 Structural SPRINT® is a moulding material that consists of two layers of carbon reinforcement either side of a precast, precatalysed resin film.
• ST 95 - Glass Structural SPRINT® (v2)
  The patent-approved ST 95 Structural SPRINT® is a moulding material that consists of two layers of glass reinforcement either side of a precast, precatalysed resin film.