Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-034-7560 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: 5.7 316.0020 5056 3.5X20X36, 5.7 3/16.0020 5056 3.5X20X36, MILC7438, MIL-C-7438, 5680-01-034-7560, 01-034-7560, 5680010347560, 010347560
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 30, 1977 | 01-034-7560 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-034-7560
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5.7 3/16.0020 5056 3.5X20X36 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-034-7560
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 3.500 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 5.7 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 20 IN. |
| TRANSVERSE DIRECTION DIMENSION | 36 IN. |
| NONDEFINITIVE SPEC/STD DATA | B GRADE AND 1 CLASS |