NSN 5680-01-288-0424
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-288-0424 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: HEXEL2211860(5052)T, HEXEL-22-1-1/8-60(5052)T, HEXEL2211860(5052)T, HEXEL-22-1-1/8-60(5052)T, 5680-01-288-0424, 01-288-0424, 5680012880424, 012880424
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
56 | NOV 01, 1988 | 01-288-0424 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-288-0424
Part Number | Cage Code | Manufacturer |
---|---|---|
HEXEL-22-1-1/8-60(5052)T | 04621 | HEXCEL CORP |
HEXEL-22-1-1/8-60(5052)T | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-01-288-0424
Characteristic | Specifications |
---|---|
BASIC MATERIAL | ALUMINUM ALLOY |
CELL CONDITION | EXPANDED |
COATING MATERIAL | PLASTIC |
SERVICE CHARACTERISTICS | WATER REPELLENT |
CELL SIZE | 1/8 IN. |
CELL DEPTH | 0.6000 INCHES NOMINAL |
CELL PERFORATION | INCLUDED |
NOMINAL DENSITY RATING | 22.1 POUNDS PER CUBIC FOOT |
MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |