Print P/N A402H-10 AIRCRAFT FLOOR PANEL PRODUCT DATA SHEET FACINGS: 0.022" EPOXY/GLASS CORE: 1/8"-5052-0025-10.0 ALUMINUM HONEYCOMB PER AMS-C-7438 PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-E-GL-A-400 THE FOLLOWING PROPERTY VALUES MEET THE REQUIREMENTS OF BMS 4-23, TYPE VI PROPERTY TEST METHOD UNIT VALUE Thickness ASTM C366 inch .39 - .41 Weight, Max ASTM C29 lbs/sq. ft. 0.90 Warpage, Max . in/ft 0.01 Long Beam Flexural 'L' Ultimate Load Deflection@100lbs. AMS-STD-401 lb inch 500 0.53 Short Beam Flexural Core Shear Stress 'L' Direction 'W' Direction AMS-STD-401 psi psi 860 490 Panel Shear, load Boeing BMS 4-23 test Sect. 5.4 lb 1400 Insert Shear, load Boeing BMS 4-23 Test Sect. 5.7 lb 1800 Impact Strength Boeing BMS 4-23 Test Sect. 5.12 in-lb 60 Climbing Drum Peel ASTM D1781-76 in-lb/3" width 60 Flatwise Compression AMS-STD-401 psi 2200 Flammability: Panels meet all requirements of FAR 25.853, Appendix F (a)(1)(i) and Appendix F (a)(2)(iii) Currently being installed on Airborne Express 767's REV. NOV '05

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