FAA APPROVED P/N NE1G1-02-125 (N501E-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 .125 Weight ASTM C29 lbs/sq ft .27 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress AMS-STD-401 in-lbs/in psi   21 20,061   20 19,321   19 18,802 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress AMS-STD-401 in-lbs/in psi   20 19,254   19 17,381   17 16,065 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 186 175 163 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 113 102 95 Climbing Drum Peel ASTM D1781-76 in-lbs/3" width 30 Flatwise Compression AMS-STD-401 psi 503 450 414 '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.