Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-149-1322 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: 6118155052H38T, 6-1-1-8-15-5052H38T, MILC7438, MIL-C-7438, 5680-00-149-1322, 00-149-1322, 5680001491322, 001491322
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | FEB 12, 1975 | 00-149-1322 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-149-1322
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6-1-1-8-15-5052H38T | 51375 | HEXCEL CORP |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-149-1322
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, MIL-C-7438 |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/8 IN |
| CELL DEPTH | 5.000 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 6.1 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 28 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96 IN. |
| NONDEFINITIVE SPEC/STD DATA | B GRADE AND 2 CLASS |