Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-269-5986 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: AL185052001N45, AL1-8-5052-001N4-5, MILC7438, 5680-00-269-5986, 00-269-5986, 5680002695986, 002695986
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUL 20, 1973 | 00-269-5986 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-269-5986
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AL1-8-5052-001N4-5 | 04621 | HEXCEL CORP |
| MILC7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-269-5986
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/8 IN. |
| CELL DEPTH | 0.222 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 4.5 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 5.0 POUNDS PER CUBIC FOOT |
| DESIGNED RIBBON DIRECTION DIMENSION | 42.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 92.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | B GRADE AND 1 CLASS |