NSN 5680-01-152-2315
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-152-2315 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: CRIII182024T81.002N6.7X1.5, CRIII-1/8-2024-T81-.002N-6.7X1.5, CRIII182024T81.002N6.742, CRIII-1/8-2024-T81-.002N-6.7-42-, CRIII182024002N6.7, CRIII-1/8-2024-002N-6.7, 5680-01-152-2315, 01-152-2315, 5680011522315, 011522315
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | APR 29, 1983 | 01-152-2315 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-152-2315
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CRIII-1/8-2024-T81-.002N-6.7X1.5 | 04621 | HEXCEL CORP |
| CRIII-1/8-2024-T81-.002N-6.7-42- | 04621 | HEXCEL CORP |
| CRIII-1/8-2024-002N-6.7 | 04621 | HEXCEL CORP |
Technical Data | NSN 5680-01-152-2315
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | PLASTIC |
| CELL SIZE | 1/8 IN. |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 6.7 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY EXTRA LONG REFERENCE NUMBER |
| EXTRA LONG REFERENCE NUMBER | CRIII-1/8-2024-T81-.002N-6.7-42X96X1.5 |