TEKLAM - Providing the Industry with Laminated Solutions FAA APPROVED
P/N NP2G1-02-375 (N503)
Product Data Sheet
  • FACINGS: 2-PLY PHENOLIC/7781 FIBERGLASS PER FAR 25.853, AMS-C-9084
  • 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 .54
Long Beam Flexural ('L' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs.
AMS-STD-401
 
in-lbs/in
psi
inch
 
218
34,463
0.674
 
203
32,359
 
192
30,882
Long Beam Flexural ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs.
AMS-STD-401
 
in-lbs/in
psi
inch
 
144
22,766
0.696
 
137
21,432
 
133
20,766
Short Beam Core Shear ('L' Dir.)
AMS-STD-401
psi
146 136
130
Short Beam Core Shear ('W' Dir.)
AMS-STD-401
psi
80 77
75
Climbing Drum Peel ASTM D1781-76 in-lbs/3"
width
23
Flatwise Compression AMS-STD-401 psi 336 289 256
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

264
404
285

235
357
256

214
325
235
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

575
780
588

420
617
430

312
503
319
'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
OSU Heat Release FAR 25.853, Part IV
Pass
NBS Smoke Emission
FAR 25.853, Part V
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