Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-069-5306 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: 253524, 5680-00-069-5306, 00-069-5306, 5680000695306, 000695306
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 01, 1961 | 00-069-5306 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-069-5306
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 253524 | 04621 | HEXCEL CORP |
Technical Data | NSN 5680-00-069-5306
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, QQ-A-250/2, ALLOY 3003 |
| FACE MATERIAL | ALUMINUM ALLOY |
| FACE THICKNESS | 0.051 INCHES NOMINAL |
| LAMINATION FEATURE | NOT LAMINATED |
| CELL SIZE | 0.125 IN. |
| MAXIMUM DENSITY RATING | 6.588 POUNDS PER CUBIC FOOT |
| SPECIAL FEATURES | DIM. DATA 0.328 IN. THK 36.000 IN. W 36.000 IN. LG |