Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-438-8066 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: 231410N5052H39T, 2-3-1-4-10N5052H39T, MILC7438, 5680-00-438-8066, 00-438-8066, 5680004388066, 004388066
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | MAY 20, 1974 | 00-438-8066 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-438-8066
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-3-1-4-10N5052H39T | 51375 | HEXCEL CORP |
| MILC7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-438-8066
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 0.667 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 2.3 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 28.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| NONDEFINITIVE SPEC/STD DATA | B GRADE AND 1 CLASS |