FAA APPROVED P/N AA209-33-750 (A507) 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 .750 Weight ASTM C29 lbs/sq ft .87 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 851 58,210 0.06 807 55,357 776 53,366 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 721 49,217 0.07 587 40,107 494 33,711 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 233 205 185 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 140 137 135 Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 58 Flatwise Compression AMS-STD-401 psi 391 330 288 Insert Pull-Out (Tension) NAS-1832-3-5 (Blind) NAS-1834-3-750 (Through) NAS-1836-3-14 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 796 985 631 584 826 486 435 715 384 Insert Shear NAS-1832-3-5 (Blind) NAS-1834-3-750 (Through) NAS-1836-3-14 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 1,107 1,275 1,087 943 1,031 960 829 860 871 '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.