NSN 5680-01-309-5780
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-309-5780 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: MILC8073, MIL-C-8073, 5680-01-309-5780, 01-309-5780, 5680013095780, 013095780
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | OCT 19, 1989 | 01-309-5780 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-309-5780
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-8073 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-309-5780
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 0.250 IN. |
| CELL DEPTH | 0.880 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 3.5 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| SPECIAL FEATURES | SLICES,FULLY CURED,NOT CORROSIVE TO METAL |
| SPECIFICATION/STANDARD DATA | 81349-MIL-C-8073 GOVERNMENT SPECIFICATION |
| NONDEFINITIVE SPEC/STD DATA | 1 CLASS AND 2A TYPE |