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FAA APPROVED P/N AA810-22-750
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Product Data Sheet
- Facings: .012" 7075T6 CLAD ALUMINUM PER QQ-A-250
- Core: 5052-.0020-1/4-4.3 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 |
.750 |
|
Weight |
ASTM C29 |
lbs/sq ft |
.66 |
Long Beam Flexural ('L' Direction) Bending Moment
Facing Stress
Deflection @ 100 lbs. |
AMS-STD-401
|
in-lbs/in
psi
inch |
600
73,545
0.11 |
536
65,676 |
491
60,151 |
Long Beam Flexural ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs. |
AMS-STD-401
|
in-lbs/in
psi
inch |
510
62,481
0.12 |
430
52,576 |
373
45,621 |
|
Short Beam Core Shear ('L' Dir.) |
AMS-STD-401
|
psi
|
344 |
314
|
294
|
|
Short Beam Core Shear ('W' Dir.) |
AMS-STD-401
|
psi
|
207 |
202
|
199
|
|
Climbing Drum Peel |
ASTM D1781-76 |
in-lbs/3²
width |
33 |
|
Flatwise Compression |
AMS-STD-401 |
psi |
658 |
571 |
511 |
Insert Pull-Out (Tension)
NAS-1832-3-5 (Blind)
NAS-1834-3-750 (Through)
NAS-1836-3-14 (Blind) |
TPS-SF-2000, Type II, Rev. B |
lbs lbs
lbs |
897
1,032
685 |
766
935
547 |
674
867
451 |
Insert Shear
NAS-1832-3-5 (Blind)
NAS-1834-3-750 (Through)
NAS-1836-3-14 (Blind) |
TPS-SF-2000, Type II, Rev. B |
lbs lbs
lbs |
990
1,105
913 |
872
1,021
753 |
790
962
640 |
'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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