NSN 5680-01-115-6887
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-115-6887 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: CR33162024.0015N3.5, CR3-3-16-2024-.0015N3.5, CRIII3163.53, CRIII-3-16-3.5-3, 5680-01-115-6887, 01-115-6887, 5680011156887, 011156887
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUL 12, 1981 | 01-115-6887 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-115-6887
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CR3-3-16-2024-.0015N3.5 | 04621 | HEXCEL CORP |
| CRIII-3-16-3.5-3 | 04621 | HEXCEL CORP |
Technical Data | NSN 5680-01-115-6887
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 6.500 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| RIBBON DIRECTION DIMENSION | 48.000 IN. |
| DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 I N. |
