NSN 5680-00-763-0867
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-763-0867 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: MILC7438 GRBCL2, MIL-C-7438 GRBCL2, MILC7438, MIL-C-7438, 5680-00-763-0867, 00-763-0867, 5680007630867, 007630867
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | MAR 08, 1968 | 00-763-0867 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-763-0867
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-7438 GRBCL2 | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-763-0867
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, QQ-A-250/8, ALLOY 5052 |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 0.250 |
| CELL DEPTH | 0.750 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 3.4 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 180.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | B GRADE AND 2 CLASS |