NSN 5680-01-200-1611
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-200-1611 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: SAEAMSC7438 GRB, SAE-AMS-C-7438 GRB, MILC7438 GRB, MIL-C-7438 GRB, CRIII3165052.0013.1, CRIII-3/16-5052-.001-3.1, MILC7438, MIL-C-7438, SAEAMSC7438, SAE-AMS-C-7438, 5680-01-200-1611, 01-200-1611, 5680012001611, 012001611
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 31, 1985 | 01-200-1611 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-200-1611
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| SAE-AMS-C-7438 GRB | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| MIL-C-7438 GRB | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| CRIII-3/16-5052-.001-3.1 | 04621 | HEXCEL CORP |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| SAE-AMS-C-7438 | 0U583 | SAE INTERNATIONAL |
Technical Data | NSN 5680-01-200-1611
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 1.000 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 3.1 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| SPECIAL FEATURES | NOMINAL FOIL THK 0.001 IN. |