NSN 5680-01-545-6909
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-545-6909 A light durable material having a cellular core of uniform geometric shapes. It is primarily used for, but not limited to, aircraft structure, such as fuselages, control surfaces, compartments, radomes, and the like. For items with a metallic or nonmetallic facing see PANEL, STRUCTURAL, AIRCRAFT.
Alternate Parts: 1.220X48.000X24.000, MILC7438E 22.1 18 .006N5052, MIL-C7438E 22.1 1/8 .006N5052, 5680-01-545-6909, 01-545-6909, 5680015456909, 015456909
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | NOV 21, 2006 | 01-545-6909 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-545-6909
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1.220X48.000X24.000 | 0MCC8 | TEXAS ALMET, L.P. |
| MIL-C7438E 22.1 1/8 .006N5052 | 0MCC8 | TEXAS ALMET, L.P. |
Technical Data | NSN 5680-01-545-6909
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, 5056 |
| CELL SIZE | 1/8 IN |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 22.1 POUNDS PER CUBIC FOOT |
| END ITEM IDENTIFICATION | CHINOOK CH-47D |