NSN 5680-01-509-7321
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-509-7321 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: GC100N01, 5680-01-509-7321, 01-509-7321, 5680015097321, 015097321
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUL 01, 2003 | 01-509-7321 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-509-7321
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| GC100N01 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
Technical Data | NSN 5680-01-509-7321
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| NOMINAL DENSITY RATING | 55.0 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 63.2 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 82.0 DEG CELSIUS |
| SPECIAL FEATURES | ALUMINUM ALLOY 5052 PER MIL-C-81596; HONEYCOMB |