NSN 5680-01-181-7010
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-181-7010 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: 4.43160015N5052H381.000, 4.4-3/16-0015N5052H38-1.000, 5680-01-181-7010, 01-181-7010, 5680011817010, 011817010
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUN 13, 1984 | 01-181-7010 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-181-7010
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4.4-3/16-0015N5052H38-1.000 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
Technical Data | NSN 5680-01-181-7010
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, MIL-C-7438 |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 1.000 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 4.4 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 60.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 60.000 |