TEKLAM Corp. - A401 Aircraft Floor Panel

P/N A401
AIRCRAFT FLOOR PANEL
PRODUCT DATA SHEET

**TYPICAL AVERAGE PROPERTY VALUES**
PROPERTY	TEST METHOD	UNIT	VALUE
Thickness	ASTM C366	inch	.39 - .41
Weight, Max	ASTM C29	lbs/sq. ft.	0.53
Warpage, Max	.	in/ft	0.02
Long Beam Flexural 'L' Ultimate Load Deflection@100lbs.	AMS-STD-401	lb inch	320 0.72
Short Beam Flexural Core Shear Stress 'L' Direction 'W' Direction	AMS-STD-401	psi psi	425 225
Panel Shear, load	Boeing BMS 4-23 test Sect. 5.4	lb	800
Impact Strength	Boeing BMS 4-23 Test Sect. 5.12	in-lb	70
Climbing Drum Peel	ASTM D1781-76	in-lb/3" width	50
Flatwise Compression	AMS-STD-401	psi	670

Flammability:
Panels meet all requirements of FAR 25.853, Appendix F (a)(1)(i) and Appendix F (a)(2)(iii)

REV. NOV '05