NSN 5680-01-130-7735
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-130-7735 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: 81180002N505645, 8-1-1-8-0-002N5056-4-5, MMS714125X002NG360X12X36, MMS714-125X002NG-360X12X36, 10120057, 5680-01-130-7735, 01-130-7735, 5680011307735, 011307735
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | APR 28, 1982 | 01-130-7735 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-130-7735
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8-1-1-8-0-002N5056-4-5 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
| MMS714-125X002NG-360X12X36 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 10120057 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
Technical Data | NSN 5680-01-130-7735
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| COATING MATERIAL | ALUMINUM ALLOY |
| SERVICE CHARACTERISTICS | HEAT RESISTANT |
| CELL SIZE | 1/8 IN. |
| CELL DEPTH | 0.360 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| MAXIMUM SERVICE TEMP LIMIT | 420.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 36.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 12.000 IN. |
| UNIT PACKAGE QUANTITY | 1 |
| UNIT PACKAGE TYPE | J ANY ACCEPTABLE |