NSN 5680-01-295-4774
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-295-4774 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 GRB6.118150.462, MIL-C-7438 GRB6.1-1/8-15-0.462, MILC7438, MIL-C-7438, 5680-01-295-4774, 01-295-4774, 5680012954774, 012954774
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | MAR 05, 1989 | 01-295-4774 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-295-4774
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-7438 GRB6.1-1/8-15-0.462 | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-295-4774
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, 5056 |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | ANY ACCEPTABLE |
| CELL SIZE | 1/8 IN. |
| CELL DEPTH | 0.462 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 6.1 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 48.000 IN. |
| DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| UNIT PACKAGE QUANTITY | 1 |
| SPECIAL FEATURES | NOMINAL FOIL THICKNESS-0.0015 |
| NONDEFINITIVE SPEC/STD DATA | B GRADE |