FAA APPROVED P/N NE1G1-02-750 (N507E-1) Product Data Sheet FACINGS: 1-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 .750 Weight ASTM C29 lbs/sq ft .41 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401   in-lbs/in psi inch   237 35,597 0.341   206 31,017   184 27,801 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401   in-lbs/in psi inch   213 31,797 0.343   198 29,598   187 28,054 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 108 89 75 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 77 73 71 Climbing Drum Peel ASTM D1781-76 in-lbs/3" width 42 Flatwise Compression AMS-STD-401 psi 313 277 251 '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