NSN 5680-01-134-6516
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-134-6516 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: 5353200015N5056X25, 5-3-5-32-0-0015N5056X2-5, 5680-01-134-6516, 01-134-6516, 5680011346516, 011346516
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
56 | JUL 07, 1982 | 01-134-6516 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-134-6516
Part Number | Cage Code | Manufacturer |
---|---|---|
5-3-5-32-0-0015N5056X2-5 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
Technical Data | NSN 5680-01-134-6516
Characteristic | Specifications |
---|---|
BASIC MATERIAL | ALUMINUM ALLOY |
CELL CONDITION | EXPANDED |
COATING MATERIAL | ALUMINUM ALLOY |
SERVICE CHARACTERISTICS | HEAT RESISTANT |
CELL SIZE | 5/32 IN. |
CELL DEPTH | 2.500 INCHES NOMINAL |
CELL PERFORATION | NOT INCLUDED |
MAXIMUM SERVICE TEMP LIMIT | 420.0 DEG FAHRENHEIT |
RIBBON DIRECTION DIMENSION | 26.000 IN. |
TRANSVERSE DIRECTION DIMENSION | 20.000 IN. |
UNIT PACKAGE QUANTITY | 1 |
UNIT PACKAGE TYPE | J ANY ACCEPTABLE |