Print P/N N404H AIRCRAFT FLOOR PANEL PRODUCT DATA SHEET FACINGS: 0.022" EPOXY/GLASS CORE: 1/8" (9.0) 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 III TYPICAL AVERAGE PROPERTY VALUES PROPERTY TEST METHOD UNIT VALUE Thickness ASTM C366 inch .39 - .41 Weight, Max ASTM C29 lbs/sq. ft. 0.84 Warpage, Max . in/ft 0.02 Long Beam Flexural 'L' Ultimate Load Deflection@100lbs. AMS-STD-401 lb inch 500 0.55 Short Beam Flexural Core Shear Stress 'L' Direction 'W' Direction AMS-STD-401 psi psi 515 300 Panel Shear, load Boeing BMS 4-23 test Sect. 5.4 lb 675 Insert Shear, load Boeing BMS 4-23 Test Sect. 5.7 lb 910 Impact Strength Boeing BMS 4-23 Test Sect. 5.12 in-lb 50 Climbing Drum Peel ASTM D1781-76 in-lb/3" width 50 Flatwise Compression AMS-STD-401 psi 2000 Roller Cart Test Boeing BMS 4-23 Test Sect. 5.5 Cycles@ 250lb/wheel plus Cycles@ 158lb/wheel 120,000 35,000 Flammability: Panels meet all requirements of FAR 25.853, Appendix F (a)(1)(i) and Appendix F (a)(2)(iii) Currently being used by: Northwest Airlines, P/N SA5321-01049-1-2 REV. NOV '05

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