NSN 5680-01-043-3204
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-043-3204 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: A1145052002P1260X12X48, A1-1-4-5052-002P-1-260X12X48, MMS701, MMS-701, MMS701, MMS-701, MILC7438, MIL-C-7438, 5680-01-043-3204, 01-043-3204, 5680010433204, 010433204
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUN 23, 1977 | 01-043-3204 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-043-3204
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| A1-1-4-5052-002P-1-260X12X48 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
| MMS-701 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
| MMS-701 | 76301 | BOEING COMPANY, THEDBA BOEING |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-043-3204
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, MIL-C-7438 |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | ANY ACCEPTABLE |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 1.260 INCHES NOMINAL |
| CELL PERFORATION | INCLUDED |
| NOMINAL DENSITY RATING | 4.3 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 12.000 IN. |
| DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 152.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 152.000 |
| UNIT PACKAGE QUANTITY | 1 |
| UNIT PACKAGE TYPE | ANY ACCEPTABLE |