Print P/N A402MD AIRCRAFT FLOOR PANEL PRODUCT DATA SHEET FACINGS: EPOXY/GLASS 0.022" and 0.044" CORE: 1/8"-5052-0025-8.1 ALUMINUM HONEYCOMB PER AMS-C-7438 PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-E-GL-A-400 TYPICAL AVERAGE PROPERTY VALUES PROPERTY TEST METHOD UNIT VALUE Thickness ASTM C366 inch .39 - .41 Weight, Max ASTM C29 lbs/sq. ft. 1.00 Warpage, Max . in/ft 0.02 Long Beam Flexural 'L' Ultimate Load Deflection@100lbs. AMS-STD-401 lb inch 700 0.40 Short Beam Flexural Core Shear Stress 'L' Direction 'W' Direction AMS-STD-401 psi psi 800 470 Panel Shear, load Boeing BMS 4-23 test Sect. 5.4 lb 1100 In-plane Shear, load Boeing BMS 4-23 test Sect. 5.6 lb/in 585* Insert Shear, load Boeing BMS 4-23 Test Sect. 5.7 lb 1900** Impact Strength Boeing BMS 4-23 Test Sect. 5.12 in-lb 130 Climbing Drum Peel ASTM D1781-76 in-lb/3" width 60 Flatwise Compression AMS-STD-401 psi 1500 Flammability: Panels meet all requirements of FAR 25.853, Appendix F (a)(1)(i) and Appendix F (a)(2)(iii) * Maximum recorded due to 10,000 lb load limit of test equipment **Accomplished using AEP Torlon floor panel inserts, P/N GAA5888B Currently being used on: NWA DC9 cargo hold UPS-AER98-5320-0004-1 REV. NOV '05

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