Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-026-9874 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: 36X36X375, MILC7438, MIL-C-7438, 5680-01-026-9874, 01-026-9874, 5680010269874, 010269874
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | SEP 05, 1976 | 01-026-9874 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-026-9874
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 36X36X375 | 91610 | HEXCEL CORPORATIONDIV LIVERMORE PLANT |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-026-9874
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY, QQ-A-250/8, ALLOY 5052 |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 0.001 INCHES NOMINAL |
| CELL PERFORATION | INCLUDED |
| NOMINAL DENSITY RATING | 5.7 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 6.3 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| TRANSVERSE DIRECTION DIMENSION | 36.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 36.000 IN. |
| SPECIAL FEATURES | THICKNESS .375 |
| NONDEFINITIVE SPEC/STD DATA | B GRADE AND 1 CLASS |