NSN 5680-01-084-3900

Part Details | STRUCTURAL CELLULAR CORE MATERIAL

5680-01-084-3900 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: MILC81986, MIL-C-81986, HRH 103162.0 (2), HRH 10-3/16-2.0 (2), AMSC81986, AMS-C-81986, BMS8124 CLASS 4 TYPE 1 GRADE 2, BMS8-124 CLASS 4 TYPE 1 GRADE 2, 5680-01-084-3900, 01-084-3900, 5680010843900, 010843900

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
56OCT 18, 197901-084-390020324 ( CORE MATERIAL, CELLULAR, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-084-3900
Part Number Cage Code Manufacturer
MIL-C-8198681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
HRH 10-3/16-2.0 (2)51344NORTHROP GRUMMAN CORPMILITARY AIRCRAFT SYSTEMS DIV
AMS-C-8198681343SOCIETY OF AUTOMOTIVE ENGINEERS INC
BMS8-124 CLASS 4 TYPE 1 GRADE 277272THE BOEING COMPANYDBA BOEING
Technical Data | NSN 5680-01-084-3900
Characteristic Specifications
BASIC MATERIAL NYLON
CELL CONDITION EXPANDED
COATING MATERIAL PLASTIC
SERVICE CHARACTERISTICS HEAT RESISTANT AND WATER REPELLENT
CELL SIZE3/16 IN.
CELL DEPTH2.000 INCHES NOMINAL
CELL PERFORATION NOT INCLUDED
NOMINAL DENSITY RATING2.0 POUNDS PER CUBIC FOOT
MAXIMUM DENSITY RATING2.2 POUNDS PER CUBIC FOOT
MAXIMUM SERVICE TEMP LIMIT250.0 DEG FAHRENHEIT
RIBBON DIRECTION DIMENSION48.000 IN.
TRANSVERSE DIRECTION DIMENSION96.000 IN.