Gillfab® 4405A is a sandwich panel of fiberglass epoxy reinforced facing laminate bonded to a Gillcore® HD meta-aramid honeycomb core. Gillfab® 4405B is identical to 4405A except a sheet of aluminum foil is bonded to the bottom facing.
Flooring panel for use in passenger, cockpit and cargo compartments for Airbus Industry A300/ A300-600/A310 aircrafts. Where more stringent flammability requirement exist, 4405B is designed with the aluminum foil on the bottom facing.
|Thickness, inch (mm)||0.375 (9.5)|
|Length and Width, inch (mm)||Maximum 60 x 144 (1,524 x 3,658)|
|Facing thickness, face/back, inch (mm)||Type A 0.030/0.024 (0.762/0.610)
Type B 0.030/0.025 (0.762/0.635)
Facings Reinforcement: Fiberglass woven cloth
Facings Resin System: Epoxy
The following tests are run in accordance with A1 5360 MIM000600 specification requirements.
|TGC Part Number||4405-375|
|Weight, psf (kg/m2)||0.785 (3.83)|
|Warpage, in/ft (mm/m)||0 (0)|
|Long Beam Bending, lbs (N)||454 (2,027)|
|Drum Peel, in-lbs/3″ width (N/76 mm width)||69 (310)|
|Flammability||Meet requirements of FAR 25.853 Appendix F Part Ipara (a)(1)(i) & (a)(2)(ii)|
Figures shown reflect typical values and should not be used as design specifications.