Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-580-6752 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 CL1TY2, MIL-C-8073 CL1TY2, MILC8073, MIL-C-8073, AMSC8073, AMS-C-8073, 5680-00-580-6752, 00-580-6752, 5680005806752, 005806752
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 01, 1963 | 00-580-6752 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-580-6752
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-8073 CL1TY2 | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| MIL-C-8073 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| AMS-C-8073 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5680-00-580-6752
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 0.250 IN. |
| CELL DEPTH | 3.125 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 6.5 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 18.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 16.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | 1 CLASS AND 2 TYPE |