Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-106-9415 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: MILC7438 GRB, MIL-C-7438 GRB, SAEAMSC7438 GRB, SAE-AMS-C-7438 GRB, 22.11860N5052C, 22.1-1/8-60N5052C, MILC7438, MIL-C-7438, SAEAMSC7438, SAE-AMS-C-7438, 5680-00-106-9415, 00-106-9415, 5680001069415, 001069415
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | FEB 06, 1974 | 00-106-9415 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-106-9415
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-7438 GRB | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| SAE-AMS-C-7438 GRB | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| 22.1-1/8-60N5052C | 04621 | HEXCEL CORP |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| SAE-AMS-C-7438 | 0U583 | SAE INTERNATIONAL |
Technical Data | NSN 5680-00-106-9415
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/8 IN. |
| CELL DEPTH | 6.000 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 22.1 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 12.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 12.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | B GRADE |