Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-068-1688 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: 6.1180.00155052, 6.1-1/8-0.0015-5052, CRIII185052.0015N6.142X96, CRIII-1/8-5052-.0015N-6.1-42X96-, CRIII185052.0015N6.1, CRIII-1/8-5052-.0015N-6.1, CRIII185052.0015N6.1X2.5, CRIII-1/8-5052-.0015N-6.1X2.5, P1901C, P190-1C, 5680-01-068-1688, 01-068-1688, 5680010681688, 010681688
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | NOV 17, 1978 | 01-068-1688 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-068-1688
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6.1-1/8-0.0015-5052 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
| CRIII-1/8-5052-.0015N-6.1-42X96- | 04621 | HEXCEL CORP |
| CRIII-1/8-5052-.0015N-6.1 | 04621 | HEXCEL CORP |
| CRIII-1/8-5052-.0015N-6.1X2.5 | 04621 | HEXCEL CORP |
| P190-1C | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 5680-01-068-1688
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/8 IN. |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 6.1 POUNDS PER CUBIC FOOT |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY EXTRA LONG REFERENCE NUMBER |
| EXTRA LONG REFERENCE NUMBER | CRIII-1/8-5052-.0015N-6.1-42X96X2.5 |