Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-106-1312 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: P0221A4896, P022-1A48-96, 5680-01-106-1312, 01-106-1312, 5680011061312, 011061312
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 13, 1981 | 01-106-1312 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-106-1312
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P022-1A48-96 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 5680-01-106-1312
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/8 IN. |
| CELL PERFORATION | NOT INCLUDED |
| MAXIMUM DENSITY RATING | 3.1 POUNDS PER CUBIC FOOT |
| DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |