TEKLAM - Providing the Industry with Laminated Solutions FAA APPROVED
P/N NE1G1-02-375 (N503E-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 .375
Weight ASTM C29 lbs/sq ft .32
Long Beam Flexural ('L' Direction)
Bending Moment
Facing Stress
Deflection @ 50 lbs.
AMS-STD-401
 
in-lbs/in
psi
inch
 
124
37,522
0.652
 
106
32,009
 
93
28,139
Long Beam Flexural ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 50 lbs.
AMS-STD-401
 
in-lbs/in
psi
inch
 
110
33,384
0.677
 
101
30,647
 
95
28,726
Short Beam Core Shear ('L' Dir.)
AMS-STD-401
psi
136 124 115
Short Beam Core Shear ('W' Dir.)
AMS-STD-401
psi
80 76 73
Climbing Drum Peel ASTM D1781-76 in-lbs/3"
width
43
Flatwise Compression AMS-STD-401 psi 342 307 282
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

229
310
492

198
276
441

176
252
406
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

558
622
529

513
558
476

482
513
440
'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