Print P/N N402 AIRCRAFT FLOOR PANEL PRODUCT DATA SHEET FACINGS: 0.015" EPOXY/GLASS CORE: 1/8" (5.0) NOMEX HONEYCOMB PER AMS-C-81986 PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-E-GL-N-400 PANELS MEET ALL REQUIREMENTS OF BMS 4-17, TYPE I TYPICAL AVERAGE PROPERTY VALUES PROPERTY TEST METHOD UNIT VALUE Thickness ASTM C366 inch .39 - .41 Weight, Max ASTM C29 lbs/sq. ft. 0.51 Warpage, Max . in/ft 0.02 Short Beam Flexural Core Shear Stress 'L' Direction 'W' Direction AMS-STD-401 psi psi 325 175 Long Beam Flexural 'L' Ultimate Load AMS-STD-401 lb 240 Climbing Drum Peel ASTM D1781-76 in-lb/3" width 50 Flatwise Compression AMS-STD-401 psi 700 Flammability: Panels meet all requirements of FAR 25.853, Appendix F (a)(1)(i) and Appendix F (a)(2)(iii) REV. NOV '05

Home Page Aircraft Floor Panel Listing Copyright©TEKLAM 1998-2008 Site Last Updated 12/13/05