TEKLAM - Providing the Industry with Laminated Solutions FAA APPROVED
P/N NP2G1-02-250 (N502)
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 .250
Weight ASTM C29 lbs/sq ft .52
Long Beam Flexural ('L' Direction)
Bending Moment
Facing Stress
Deflection @ 50 lbs.
AMS-STD-401
 
in-lbs/in
psi
inch
 
152
36,617
0.778
 
129
31,945
 
113
28,664
Long Beam Flexural 'L' ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 50 lbs.
AMS-STD-401
 
in-lbs/in
psi
inch
 
106
24,821
0.775
 
98
23,488
 
93
22,553
Short Beam Core Shear ('L' Dir.) AMS-STD-401
psi
165 149
138
Short Beam Core Shear ('W' Dir.) AMS-STD-401
psi
84 80
77
Climbing Drum Peel ASTM D1781-76 in-lbs/3"
width
18
Flatwise Compression AMS-STD-401 psi 357 299 258
Insert Pull-Out (Tension)
NAS-1834-3-250 (Through)
NAS-1836-3-07 (Blind)
TPS-SF-2000, Type II, Rev. B
lbs
lbs
 
201
294
 
180
259
 
166
235
Insert Shear
NAS-1834-3-250 (Through)
NAS-1836-3-07 (Blind)
TPS-SF-2000, Type II, Rev. B
lbs
lbs
 
753
520
 
626
396
 
536
309
'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