NSN 5680-01-127-0770
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-127-0770 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: BMS44,315P526, BMS4-4,3-15P526, 5680-01-127-0770, 01-127-0770, 5680011270770, 011270770
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | FEB 22, 1982 | 01-127-0770 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-127-0770
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| BMS4-4,3-15P526 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
Technical Data | NSN 5680-01-127-0770
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, MIL-C-7438 |
| FACE THICKNESS | 0.005 INCHES NOMINAL |
| CELL SIZE | 3/16 IN. |
| CELL PERFORATION | INCLUDED |
| RIBBON DIRECTION DIMENSION | 60.000 |
| TRANSVERSE DIRECTION DIMENSION | 96.000 |
| SPECIAL FEATURES | FOIL THICKNESS .0015 |