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FAA APPROVED P/N A402H |
- FACINGS: 0.022" EPOXY / GLASS
- CORE: 1/8"-5052-0025-8.1 ALUMINUM HONEYCOMB PER AMS-C-7438
- PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-E-GL-A-400
- PANEL MEETS THE REQUIREMENTS OF BMS 4-23 TYPE III
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| Thickness | ASTM C366 | inch |
.39
- .41
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| Weight, Max. | ASTM C29 | lbs/sq ft |
.78
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| Warpage, Max. | Boeing BMS 4-23 Test Section 8.10 | in/ft |
.01
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| Long Beam Flexural 'L' Ultimate Load Facing Stress Bending Moment Deflection @ 100lbs |
Boeing BMS 4-23 Test Sect. 8.3.1 AMS-STD-401 AMS-STD-401 Test Sect. 8.3.2 |
lbs, x - ks psi, x - ks per inch, x - ks in, x + ks |
502 49,489 423 0.50 |
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| Long Beam Flexural 'L' after Humidity Exposure Ultimate Load |
Boeing
BMS 4-23 Test Sect. 8.3.1 |
lb, x - ks |
426 |
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| Panel Shear, load | Boeing BMS 4-23 Test Sec. 8.4 | lb, x - ks |
1070
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| In-Plane Shear | Boeing BMS 4-23 Test Sect. 8.6 | lb/in, x - ks |
634
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| Insert Shear, load | Boeing BMS 4-23 Test Sect. 8.7 | lbs, x - ks |
1622
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| Impact Strength | Boeing BMS 4-23 Test Sect. 8.8 | in-lb |
155
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| Climbing Drum Peel | Boeing BMS 4-23 Test Sect. 8.5 | in-lb/3" width, x - ks |
47.4
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| Drum Peel after Humidity Exposure | Boeing BMS 4-23 Test Sect. 8.5 | in-lb/3" width, x - ks |
47.6
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| Stabilized Core Compression | Boeing BMS 4-23 Test Sect. 8.9 | psi, x - ks |
1401
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| Flammability: Panels meet all requirements of FAR 25.853, Appendix F (a)(1)(i) and Appendix F (a)(2)(iii) |
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| TEKLAM Corporation makes no warranty, whether expressed or implied, including warranties of merchantability or of fitness for a particular purpose. Under no circumstances shall TEKLAM Corporation be liable for incidental, consequential, or other damages arising out of a claim from alleged negligence, breach of warranty, strict liability or any other theory, through the use or handling of this product or the inability to use the product. The sole liability of TEKLAM Corporation for any claims arising out of the manufacture, use or sale of its products shall be for the replacement of the quantity of this product which has proven to not substantially comply with this spec sheet. Users should make their own assessment of the suitability of any product for the purposes required. The above supersedes any provision in your company's forms, letters, or other documents. |