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FAA APPROVED P/N AA209-33-500 (A505)
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Product Data Sheet
- FACINGS: .020" 2024T3 CLAD ALUMINUM PER QQ-A-250
- CORE: 5052-.0015-1/4-3.4 ALUMINUM HONEYCOMB PER AMS-C-7438
- PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-A-A-500, REV. A
PROPERTY |
TEST METHOD |
UNIT |
VALUE |
Mean |
'B' Basis |
'A' Basis |
Thickness |
ASTM C366 |
inch |
.500 |
Weight |
ASTM C29 |
lbs/sq ft |
.78 |
Long Beam Flexural ('L' Direction) Bending Moment
Facing Stress
Deflection @ 100 lbs. |
AMS-STD-401
|
in-lbs/in
psi
inch |
547
56,706
0.14 |
523
54,287 |
506
52,589 |
Long Beam Flexural ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs. |
AMS-STD-401
|
in-lbs/in
psi
inch |
503
52,425
0.15 |
492
51,212 |
484
50,360 |
Short Beam Core Shear ('L' Dir.) |
AMS-STD-401
|
psi
|
302 |
266
|
242
|
Short Beam Core Shear ('W' Dir.) |
AMS-STD-401
|
psi
|
169 |
163
|
160
|
Climbing Drum Peel |
ASTM D1781-76 |
in-lbs/3²
width |
52 |
Flatwise Compression |
AMS-STD-401 |
psi |
405 |
313 |
248 |
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 |
610
825
609 |
526
719
507 |
468
645
436 |
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 |
1,278
1,550
1,080 |
1,113
1,324
928 |
999
1,166
821 |
'A' and 'B' Basis design allowable data FAA-approved
per TEKLAM Test Plan TTP-1004 under FAA Project No. ST7145LA-T 3-22-00 |
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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