NSN 5680-01-084-1018
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-084-1018 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: BMS8124,IV12.012X10X24IN., BMS8-124,IV-1-2.01/2X10X24IN., 5680-01-084-1018, 01-084-1018, 5680010841018, 010841018
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | OCT 10, 1979 | 01-084-1018 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-084-1018
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| BMS8-124,IV-1-2.01/2X10X24IN. | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 5680-01-084-1018
| Characteristic | Specifications |
|---|---|
| SERVICE CHARACTERISTICS | HEAT RESISTANT |
| CELL SIZE | 3/16 IN |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 2.0 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 250.0 DEG FAHRENHEIT |