NSN 5680-01-296-5994
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-296-5994 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: MILC7438GRB 2.31410,1.25, MIL-C-7438GRB 2.3-1/4-10,1.25, MILC7438, MIL-C-7438, 5680-01-296-5994, 01-296-5994, 5680012965994, 012965994
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | MAR 23, 1989 | 01-296-5994 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-296-5994
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-7438GRB 2.3-1/4-10,1.25 | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-296-5994
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, 5056 |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 1.250 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 2.3 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 0.0010 |
| NONDEFINITIVE SPEC/STD DATA | B GRADE |