FAA APPROVED P/N AA209-33-1000 (A510) Product Data Sheet FACINGS: .020" 2024T3 CLAD ALUMINUM PER QQ-A-250 CORE: 5052-.0015-1/4-3.4 ALUMINUM HONEYCOMB PER AMS-C-7438 PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-A-A-500, REV. A PROPERTY TEST METHOD UNIT VALUE Mean 'B' Basis 'A' Basis Thickness ASTM C366 inch 1.000 Weight ASTM C29 lbs/sq ft .93 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 1,157 58,720 0.04 1,103 56,064 1,066 54,199 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 938 47,777 0.04 897 45,654 868 44,164 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 246 231 221 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 154 148 143 Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 42 Flatwise Compression AMS-STD-401 psi 417 362 324 Insert Pull-Out (Tension) NAS-1832-3-7 (Blind) NAS-1834-3-1000 (Through) NAS-1836-3-16 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 1,113 1,167 701 996 1,041 578 914 951 492 Insert Shear NAS-1832-3-7 (Blind) NAS-1834-3-1000 (Through) NAS-1836-3-16 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 1,242 1,146 1,140 1,115 1,015 875 1,027 923 689 'A' and 'B' Basis design allowable data FAA-approved per TEKLAM Test Plan TTP-1004 under FAA Project No. ST7145LA-T 3-22-00 Flammability – 60-Second Vertical FAR 25.853, Part I Pass OSU Heat Release FAR 25.853, Part IV Pass NBS Smoke Emission FAR 25.853, Part V Pass STANDARD PANEL SIZES: 48" X 96", 48" X 144", OTHER SIZES AVAILABLE. STANDARD DIMENSIONAL TOLERANCES: WIDTH AND LENGTH: +/- 1/2"; THICKNESS: +/- 0.010". FLATNESS: MAX. DEVIATION, DELTA, INS.= (LxL) x .004/T, WHERE L=LENGTH IN FT, T=THICKNESS IN INS.