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AIRCRAFT FLOOR PANEL
PRODUCT DATA SHEET
- Facings: 0.020" AND 0.030" Epoxy/Glass
- Core: 1/8"-5052-0025-8.1 Aluminum Honeycomb Per AMS-C-7438
- Mfg per: Teklam Process Specification TPS-E-GL-A-400
| PROPERTY | TEST METHOD | UNIT | VALUE |
| Thickness | ASTM C366 | inch | .39 - .41 |
| Weight | ASTM C29 | lbs/sq. ft. | 0.83 |
| Warpage, Max | . | in/ft | 0.02 |
|
Long Beam Flexural 'L' Ultimate Load Deflection@100lbs. |
AMS-STD-401 |
lb inch |
525 0.60 |
| Panel Shear, load |
Boeing BMS 4-23 test Sect. 5.4 |
lb | 1100 |
| Insert Shear, load |
Boeing BMS 4-23 Test Sect. 5.7 |
lb | 910 |
| Impact Strength |
Boeing BMS 4-23 Test Sect. 5.12 |
in-lb | 72 |
| Climbing Drum Peel | ASTM D1781-76 | in-lb/3" width | 60 |
| Flatwise Compression | AMS-STD-401 | psi | 1500 |
| Roller Cart Test |
Boeing BMS 4-23 Test Sect. 5.5 |
Cycles@ 120lb/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) |
Southwest Airlines
REV. NOV. '05