NSN 5680-01-268-3405
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-268-3405 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: ALC185052.004, ALC-1/8-5052-.004, ALC185052.004, ALC-1/8-5052-.004, 5680-01-268-3405, 01-268-3405, 5680012683405, 012683405
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | NOV 27, 1987 | 01-268-3405 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-268-3405
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ALC-1/8-5052-.004 | 04621 | HEXCEL CORP |
| ALC-1/8-5052-.004 | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-01-268-3405
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/8 IN. |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 27.5 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 17.0 POUNDS PER CUBIC FOOT |
| DESIGNED RIBBON DIRECTION DIMENSION | 96.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 24.000 IN. |
| SPECIAL FEATURES | NOMINAL FOIL THICKNESS .006 IN. |