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AIRCRAFT FLOOR PANEL
PRODUCT DATA SHEET
- FACINGS: 0.015" EPOXY/GLASS
- CORE: 1/8" (9.0) NOMEX HONEYCOMB PER AMS-C-81986
- PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-E-GL-N-400
- PANELS MEET ALL REQUIREMENTS OF BMS 4-17, TYPE II
| PROPERTY | TEST METHOD | UNIT | VALUE |
| Thickness | ASTM C366 | inch | .39 - .41 |
| Weight, Max | ASTM C29 | lbs/sq. ft. | 0.64 |
| Warpage, Max | . | in/ft | 0.02 |
|
Long Beam Flexural 'L' Ultimate Load Deflection@100lbs. |
Boeing BMS 4-17 AMS-STD-401 Test Sect. 8.3 |
lb inch |
250 0.65 |
|
Short Beam Flexural Core Shear Stress 'L' Direction 'W' Direction |
AMS-STD-401 |
psi |
300 |
| Panel Shear, load |
Boeing BMS 4-17 test Sect. 8.4 |
lb | 610 |
| Insert Shear, load |
Boeing BMS 4-17 Test Sect. 8.7 |
lb | 910 |
| Impact Strength |
Boeing BMS 4-17 Test Sect. 8.8 |
in-lb | 45 |
| Climbing Drum Peel | ASTM D1781-76 | in-lb/3" width | 50 |
| Flatwise Compression | AMS-STD-401 | psi | 2000 |
| Roller Cart Test |
Boeing BMS 4-17 Test Sect. 8.11 |
Cycles@ 250lb/wheel plus Cycles@ 158lb/wheel |
120,000 35,000 |
|
Flammability: Panels meet all requirements of FAR 25.853, Appendix F (a)(1)(i) and Appendix F (a)(2)(iii) |
REV. NOV. '05