Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-151-6413 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: HRP143L18W24T55, HRP1-4-3L18W24T5-5, HRP143L18W24T55, HRP1-4-3L18W24T5-5, 5680-00-151-6413, 00-151-6413, 5680001516413, 001516413
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | OCT 10, 1971 | 00-151-6413 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-151-6413
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HRP1-4-3L18W24T5-5 | 04621 | HEXCEL CORP |
| HRP1-4-3L18W24T5-5 | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-00-151-6413
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS CLOTH, RESIN IMPREGNATED |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/4IN. |
| CELL DEPTH | 5.438 INCHES MINIMUM AND 5.562 INCHES MAXIMUM |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 3.0 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 3.3 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 325.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 18.500 |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 24.000 |