FAA APPROVED P/N NE1G1-02-1000 (N510E-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 1.000 Weight ASTM C29 lbs/sq ft .48 Long Beam Flexural ('L' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401   in-lbs/in psi inch   307 34,391 0.190   270 30,294   245 27,418 Long Beam Flexural ('W' Direction) Bending Moment Facing Stress Deflection @ 100 lbs. AMS-STD-401   in-lbs/in psi inch   287 32,060 0.189   265 29,691   250 28,027 Short Beam Core Shear ('L' Dir.) AMS-STD-401 psi 104 88 76 Short Beam Core Shear ('W' Dir.) AMS-STD-401 psi 77 71 67 Climbing Drum Peel ASTM D1781-76 in-lbs/3" width 34 Flatwise Compression AMS-STD-401 psi 326 303 287 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 350 381 297 278 304 218 228 250 164 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 427 475 374 305 397 296 220 341 242 '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