NSN 5680-00-618-8078
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-618-8078 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, N0NUMBER52, 5680-00-618-8078, 00-618-8078, 5680006188078, 006188078
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 01, 1963 | 00-618-8078 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-618-8078
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MILC8073 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| N0NUMBER52 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 5680-00-618-8078
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 0.188 IN. |
| CELL DEPTH | 0.750 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| MAXIMUM DENSITY RATING | 9.9 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 70.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 40.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | II CLASS AND 1-C TYPE AND B GRADE |