Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-293-8429 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: LB0130136, LB0130-136, HFT3164.01.289, HFT3/16-4.0-1.289, HFT3164.01.289, HFT3/16-4.0-1.289, 5680-01-293-8429, 01-293-8429, 5680012938429, 012938429
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | FEB 07, 1989 | 01-293-8429 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-293-8429
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| LB0130-136 | 43999 | BOEING COMPANY, THEDBA BOEING |
| HFT3/16-4.0-1.289 | 04621 | HEXCEL CORP |
| HFT3/16-4.0-1.289 | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-01-293-8429
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | PLASTIC |
| SERVICE CHARACTERISTICS | WATER REPELLENT |
| CELL SIZE | 3/16 IN. |
| CELL DEPTH | 1.289 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 4.0 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 325.0 DEG FAHRENHEIT |
| UNIT PACKAGE QUANTITY | 1 |