Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-262-7347 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 CL1TY1CGRA, MIL-C-8073 CL1TY1CGRA, NP31611290, NP3-16-112-90, MILC8073, MIL-C-8073, 5680-00-262-7347, 00-262-7347, 5680002627347, 002627347
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUL 08, 1973 | 00-262-7347 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-262-7347
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-8073 CL1TY1CGRA | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| NP3-16-112-90 | 04621 | HEXCEL CORP |
| MIL-C-8073 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-262-7347
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC, PLASTIC DIPPED |
| CELL CONDITION | EXPANDED |
| SERVICE CHARACTERISTICS | WATER REPELLENT |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 0.233 INCHES MINIMUM AND 0.245 INCHES MAXIMUM |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 9.0 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 9.9 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 180.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 36.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 14.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | 1 CLASS AND 1-C TYPE AND A GRADE |