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FAA APPROVED P/N AA805-11-500
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Product Data Sheet
- FACINGS: .010" 7075T6 CLAD ALUMINUM PER QQ-A-250
- CORE: 5052-.0010-3/16-3.1 ALUMINUM HONEYCOMB PER AMS-C-7438
- PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-A-A-500, REV. A
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PROPERTY |
TEST METHOD |
UNIT |
VALUE |
Mean |
'B' Basis |
'A' Basis |
|
Thickness |
ASTM C366 |
inch |
.500 |
|
Weight |
ASTM C29 |
lbs/sq ft |
.53 |
Long Beam Flexural ('L' Direction) Bending Moment
Facing Stress
Deflection @ 100 lbs. |
AMS-STD-401
|
in-lbs/in
psi
inch |
413
75,997
0.24 |
372
68,546 |
344
63,315 |
Long Beam Flexural ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs. |
AMS-STD-401
|
in-lbs/in
psi
inch |
388
71,118
0.24 |
367
67,093 |
352
64,275 |
|
Short Beam Core Shear ('L' Dir.) |
AMS-STD-401
|
psi
|
285 |
259
|
240
|
|
Short Beam Core Shear ('W' Dir.) |
AMS-STD-401
|
psi
|
170 |
154
|
143
|
|
Climbing Drum Peel |
ASTM D1781-76 |
in-lbs/3²
width |
43 |
|
Flatwise Compression |
AMS-STD-401 |
psi |
393 |
341 |
305 |
Insert Pull-Out (Tension)
NAS-1832-3-3 (Blind)
NAS-1834-3-500 (Through)
NAS-1836-3-12 (Blind) |
TPS-SF-2000, Type II, Rev. B |
lbs lbs
lbs |
533
593
529 |
469
467
470 |
424
378
429 |
Insert Shear
NAS-1832-3-3 (Blind)
NAS-1834-3-500 (Through)
NAS-1836-3-12 (Blind) |
TPS-SF-2000, Type II, Rev. B |
lbs lbs
lbs |
904
1,129
828 |
767
973
699 |
670
864
608 |
'A' and 'B' Basis design allowable data FAA-approved
per TEKLAM Test Plan TTP-1004 under FAA Project No. ST7145LA-T 3-22-00 |
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Flammability – 60-Second Vertical |
FAR 25.853, Part I |
Pass
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OSU Heat Release |
FAR 25.853, Part IV |
Pass
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NBS Smoke Emission
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FAR 25.853, Part V |
Pass
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- 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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