Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-954-5065 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, 5680-00-954-5065, 00-954-5065, 5680009545065, 009545065
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 01, 1962 | 00-954-5065 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-954-5065
| 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 5680-00-954-5065
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 0.125 IN. |
| CELL DEPTH | 8.000 INCHES NOMINAL |
| CELL PERFORATION | INCLUDED |
| NOMINAL DENSITY RATING | 8.1 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 8.9 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 72.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 24.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | 2 CLASS AND B GRADE |