Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-126-6280 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: CIII1820240039.5, CIII-1/8-2024-003-9.5, CIII1820240039.5, CIII-1/8-2024-003-9.5, 5680-01-126-6280, 01-126-6280, 5680011266280, 011266280
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | FEB 15, 1982 | 01-126-6280 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-126-6280
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CIII-1/8-2024-003-9.5 | 04621 | HEXCEL CORP |
| CIII-1/8-2024-003-9.5 | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-01-126-6280
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| FACE THICKNESS | 0.003 INCHES NOMINAL |
| CELL SIZE | 1/8 IN. |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 9.5 POUNDS PER CUBIC FOOT |
| RIBBON DIRECTION DIMENSION | 30.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |