Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-520-8376 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: CIII145052.001N2.3 78X52X1IN, CIII-1/4-5052-.001N2.3 78X52X1IN, CIII145052.001N2.3 78X52X1IN, CIII-1/4-5052-.001N2.3 78X52X1IN, 5680-01-520-8376, 01-520-8376, 5680015208376, 015208376
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | MAY 27, 2004 | 01-520-8376 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-520-8376
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CIII-1/4-5052-.001N2.3 78X52X1IN | 04621 | HEXCEL CORP |
| CIII-1/4-5052-.001N2.3 78X52X1IN | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-01-520-8376
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| FACE THICKNESS | 0.001 INCHES NOMINAL |
| CELL SIZE | 1/4 IN. |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 2.3 POUNDS PER CUBIC FOOT |
| RIBBON DIRECTION DIMENSION | 48.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |