Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-258-7110 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: NP14214, NP1-4-21-4, MILC8073, 5680-00-258-7110, 00-258-7110, 5680002587110, 002587110
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUN 29, 1973 | 00-258-7110 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-258-7110
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| NP1-4-21-4 | 04621 | HEXCEL CORP |
| MILC8073 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-258-7110
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC, PLASTIC DIPPED |
| CELL CONDITION | EXPANDED |
| SERVICE CHARACTERISTICS | WATER REPELLENT |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 0.274 INCHES MINIMUM AND 0.286 INCHES MAXIMUM |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 4.0 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 4.5 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 180.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 18.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 36.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | 1 CLASS AND 2-A TYPE AND A GRADE |