FAA APPROVED P/N AA207-33-750 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 .750 Weight ASTM C29 lbs/sq ft .96 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 934 63,350 0.07 875 58,625 826 55,308 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 876 59,649 0.07 851 57,911 834 56,698 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 456 424 402 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 297 287 281 Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 43 Flatwise Compression AMS-STD-401 psi 957 909 875 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 1,137 1,368 809 916 1,228 706 761 1,130 634 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 1,160 1,265 1,077 961 1,216 844 822 1,056 680 '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.