Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-047-0262 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: AL145052X002P1.012X20X25X35, AL-1-4-5052X002P1.012X20X25X35, MILC7438, MIL-C-7438, 5680-01-047-0262, 01-047-0262, 5680010470262, 010470262
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | AUG 28, 1977 | 01-047-0262 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-047-0262
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AL-1-4-5052X002P1.012X20X25X35 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-047-0262
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, MIL-C-7438 |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | ANY ACCEPTABLE |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 1.012 INCHES NOMINAL |
| CELL PERFORATION | INCLUDED |
| NOMINAL DENSITY RATING | 4.3 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 20 IN. |
| DESIGNED RIBBON DIRECTION DIMENSION | 25 IN. |
| TRANSVERSE DIRECTION DIMENSION | 152 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 152 IN. |
| UNIT PACKAGE QUANTITY | 1 |
| UNIT PACKAGE TYPE | ANY ACCEPTABLE |