FAA APPROVED P/N AA207-33-1000 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 1.000 Weight ASTM C29 lbs/sq ft 1.06 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 1,228 62,370 0.04 1,147 57,986 1,090 54,926 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 1,193 60,688 0.04 1,156 58,785 1,130 57,458 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 417 391 372 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 274 262 254 Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 50 Flatwise Compression AMS-STD-401 psi 841 699 598 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 1,415 1,544 729 1,243 1,414 663 1,122 1,324 618 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 1,174 1,285 1,080 1,026 1,133 957 921 1,026 871 '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. REV. NOV. 2005