NSN 5680-01-113-0114
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-113-0114 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: CR3185052,00 2N8.1, CR3-1-85052-,00 2N8.1, CRIII188,12, CRIII-1-8-8,1-2, 5680-01-113-0114, 01-113-0114, 5680011130114, 011130114
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | MAY 14, 1981 | 01-113-0114 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-113-0114
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CR3-1-85052-,00 2N8.1 | 04621 | HEXCEL CORP |
| CRIII-1-8-8,1-2 | 04621 | HEXCEL CORP |
Technical Data | NSN 5680-01-113-0114
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| FACE THICKNESS | 0.002 INCHES NOMINAL |
| CELL SIZE | L/8 IN. |
| CELL DEPTH | 4.000 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| RIBBON DIRECTION DIMENSION | 42.000 IN. |
| DESIGNED RIBBON DIRECTION DIMENSION | 42.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |