Print P/N A402H AIRCRAFT FLOOR PANEL PRODUCT DATA SHEET FACINGS: 0.022" EPOXY/GLASS CORE: 1/8"-5052-0025-8.1 ALUMINUM HONEYCOMB PER AMS-C-7438 PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-E-GL-A-400 PANELS MEET ALL REQUIREMENTS OF BMS 4-23, TYPE III PROPERTY TEST METHOD UNIT VALUE Thickness ASTM C366 inch .39 - .41 Weight, Max ASTM C29 lbs/sq. ft. 0.78 Warpage, Max . in/ft 0.01 Long Beam Flexural 'L' Ultimate Load Deflection@100lbs. Boeing BMS 4-23 AMS-STD-401 Test Sect. 8.3 lb inch 502 0.60 Short Beam Flexural Core Shear Stress 'L' Direction 'W' Direction AMS-STD-401 psi psi 1070 470 Panel Shear, load Boeing BMS 4-23 test Sect. 8.4 lb 1100 Insert Shear, load Boeing BMS 4-23 Test Sect. 8.7 lb 1622 Impact Strength Boeing BMS 4-23 Test Sect. 8.8 in-lb 155 Climbing Drum Peel ASTM D1781-76 in-lb/3" width 47.4 Flatwise Compression AMS-STD-401 psi 1401 Roller Cart Test Boeing BMS 4-23 Test Sect. 8.11 Cycles@ 250lb/wheel 150,000 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 SA5321-01049-1-1 Federal Express, Specification No. 91-019 UPS-AER98-5320-0004-1 REV. NOV. '05

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