| (*) Note: |
| 1. All loads applied on center point of panel via a 1 square inch indenter area. A 50 Kg preloading is default. Results above indicate center point |
| of panel permanent set after application of concentrated load shall be 2mm (0.01"). |
| 2. All loads to be applied anywhere on panel via a 1 square inch indenter area. A 50 Kg preloading is default. Permanent set after application of |
| load shall be 1 mm (0.005"). |
| 3. A concentrated load is applied at center of panel via a 1 square inch indenter area. A 50 Kg preloading is default. Result shows where |
| permanent fractures occurred. |
| 4. Local and beam top surface deformation shall not exceed 0.02mm (0.0008"), both 10 pass test and 10,000 pass test uses a 6" x 2" wide |
| alathane wheel. Loading on top of the wheel is 500Kgs. |
| 5.Drop Impact Loads: A (200 Lb) 91kg weight drops from 1ft (305 mm) hight via a 1 square inch area. Results above indicate less than 1mm |
| (0.005") deformation. |
| 6. Fatigue Test: Results above indicate 1 million cycles of loading and unloading force applied on the center of a panel via indenter. |
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