Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-957-9164 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, 5680-00-957-9164, 00-957-9164, 5680009579164, 009579164
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 01, 1962 | 00-957-9164 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-957-9164
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MILC7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-957-9164
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, QQ-A-250/2, ALLOY 3003 |
| CELL CONDITION | EXPANDED |
| FACE MATERIAL | ALUMINUM ALLOY |
| FACE THICKNESS | 0.040 INCHES NOMINAL |
| LAMINATION FEATURE | NOT LAMINATED |
| CELL SIZE | 0.250 IN. |
| CELL DEPTH | 1.046 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 7.9 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 180.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 11.500 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 11.500 IN. |
| NONDEFINITIVE SPEC/STD DATA | A CLASS |