Fiberply L-802 is a unique facesheet material consisting of cross-plied carbon prepreg with a fiberglass surface impregnated with flame retardant phenolic resin and comes with our proprietary thin film adhesive for bonding to core materials. Fiberply L-802 is designed as a one sheet facing for honeycomb core where high strength and stiffness are a criteria coupled with the desire to make a panel as light as possible and still meet the stringent burn requirements of today's modern commercial aircraft.

• Superior mechanical properties over fiberglass/phenolic systems used in aircraft interior construction.
• Improved stiffness by employing carbon fibers with superior flexural modulus.
• L-802 has been tested and proven superior in panel designs requiring good impact resistance and toughness.
• Preplied materials reduce the labor content of bonded sandwich panels.
• L-802 has the highest strength to weight ratio for interior materials requiring damage tolerance to normal aircraft interior abuse such as impact damage from passenger carry-on luggage storage.
• Less resin is required for unidirectional fibers than is needed for an equivalent woven product thus reducing weight.
• Lower overall cost because all of the other panel components can be down-sized due to the improved strength and stiffness in the fiberply L-802 facesheet.
• Over 10 years of service on aircraft in Commercial Airline Service.

Grade A:
• Weight: 0.080 ± 0.005 lbs/ft² (391 ± 24 g/m²)
• Thickness: 0.009” (0.229 mm)
Grade B:
• Weight: 0.095 ± 0.005 lbs/ft² (464 ± 24 g/m²)
• Thickness: 0.010” (0.254 mm)