Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-562-4541 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: HRH103162.0, HRH-10-3/16-2.0, 5680-01-562-4541, 01-562-4541, 5680015624541, 015624541
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | APR 09, 2008 | 01-562-4541 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-562-4541
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HRH-10-3/16-2.0 | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-01-562-4541
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | NYLON |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | PLASTIC |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 4.650 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 2.0 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 250.0 DEG FAHRENHEIT |
| SPECIAL FEATURES | 36 IN. LENGTH AND 16 IN. WIDE |
| END ITEM IDENTIFICATION | HELICOPTER ROTOR BLADE |