NSN 5680-01-083-9846
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-083-9846 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: LS5898AB2, LS5898AB2, 5680-01-083-9846, 01-083-9846, 5680010839846, 010839846
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | OCT 06, 1979 | 01-083-9846 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-083-9846
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| LS5898AB2 | 72728 | GENERAL VENEER MANUFACTURING CO. |
| LS5898AB2 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 5680-01-083-9846
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, MIL-C-7438 |
| CELL CONDITION | EXPANDED |
| FACE MATERIAL | ALUMINUM ALLOY |
| FACE THICKNESS | 0.012 INCHES MINIMUM AND 0.020 INCHES MAXIMUM |
| LAMINATION FEATURE | LAMINATED |
| CELL SIZE | 1/8 IN. |
| CELL DEPTH | 0.222 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 4.5 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 180.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 42.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 92.000 IN |