Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-034-7558 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: 3.13160.0010N50568X46X49, 3.1-3/16-0.0010N5056-8X46X49, MILC7438, MIL-C-7438, 5680-01-034-7558, 01-034-7558, 5680010347558, 010347558
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 30, 1977 | 01-034-7558 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-034-7558
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3.1-3/16-0.0010N5056-8X46X49 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-034-7558
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 8.000 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 3.1 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 46 IN. |
| TRANSVERSE DIRECTION DIMENSION | 49 IN. |
| NONDEFINITIVE SPEC/STD DATA | B GRADE AND 1 CLASS |