FAA APPROVED P/N NE2G1-02-375 (N503E) Product Data Sheet FACINGS: 2-PLY EPOXY/7781 FIBERGLASS CORE: 1/8 (3.0) NOMEX® HONEYCOMB PER AMS-C-81986 PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-CN-500 PROPERTY TEST METHOD UNIT VALUE Mean 'B' Basis 'A' Basis Thickness ASTM C366 inch .375 Weight ASTM C29 lbs/sq ft .56 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 265 42,011 0.740 248 39,743   236 38,151 Long Beam Flexural 'L' ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401 in-lbs/in psi inch 153 24,293 0.754 146 23,123 142 22,301 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 170 162 157 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 85 82 79 Climbing Drum Peel ASTM D1781-76 in-lbs/3" width 51 Flatwise Compression AMS-STD-401 psi 360 316 284 Insert Pull-Out (Tension) TYE2002-3-2 (Blind) NAS-1834-3-375 (Through) NAS-1836-3-10 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 246 380 322 220 305 289 201 252 265 Insert Shear TYE2002-3-2 (Blind) NAS-1834-3-375 (Through) NAS-1836-3-10 (Blind) TPS-SF-2000, Type II, Rev. B lbs lbs lbs 666 1,016 698 519 867 606 417 763 541 'A' and 'B' basis design allowable data FAA-approved per TEKLAM Test Plan TTP-1005 under FAA Project No. ST7145LA-T 3-22-00 Flammability – 60-Second Vertical FAR 25.853, Part I 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