NSN 5680-01-296-3603
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-296-3603 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: ST0130GB0004 TY1, HRP143.55.500, HRP1/4-3.5-5.500, 5680-01-296-3603, 01-296-3603, 5680012963603, 012963603
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | MAR 19, 1989 | 01-296-3603 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-296-3603
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ST0130GB0004 TY1 | 43999 | BOEING COMPANY, THEDBA BOEING |
| HRP1/4-3.5-5.500 | 04621 | HEXCEL CORP |
Technical Data | NSN 5680-01-296-3603
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | PLASTIC |
| SERVICE CHARACTERISTICS | WATER REPELLENT |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 5.500 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 3.5 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 325.0 DEG FAHRENHEIT |
| UNIT PACKAGE QUANTITY | 1 |