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FAA APPROVED P/N NE1G1-02-375 (N503E-1)
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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
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Flammability – 60-Second Vertical
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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.
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REV. NOV. 2005
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