FAA APPROVED P/N AA207-33-500 Product Data Sheet FACINGS: .020" 2024T3 CLAD ALUMINUM PER QQ-A-250 CORE: 5052-.0020-3/16-5.7 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 .500 Weight ASTM C29 lbs/sq ft .85 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 609 63,186 0.14 601 62,224 596 61,550 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 586 60,488 0.14 567 58,391 553 56,918 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 470 454 443 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 293 285 280 Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 50 Flatwise Compression AMS-STD-401 psi 916 868 834 Insert Pull-Out (Tension) NAS-1832-3-3 (Blind) NAS-1834-3-500 (Through) NAS-1836-3-12 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 788 1,044 674 694 920 614 628 833 571 Insert Shear NAS-1832-3-3 (Blind) NAS-1834-3-500 (Through) NAS-1836-3-12 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 1,235 1,444 1,076 1,027 1,119 919 881 908 808 '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.