FAA APPROVED P/N AA207-55-750 Product Data Sheet FACINGS: .032" 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 1.31 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 1,445 62,562 0.04 1,347 58,262 1,278 55,243 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 1,384 60,264 0.05 1,334 58,144 1,299 56,655 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 482 396 335 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 287 274 264 Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 32 Flatwise Compression AMS-STD-401 psi 802 745 704 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 1,132 1,405 678 963 1,233 522 844 1,113 413 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 1,780 2,065 1,612 1,578 1,862 1,462 1,437 1,719 1,357 '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