NSN 5680-01-297-7919
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-297-7919 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: MILC7438GRB 316.00154.4, MIL-C-7438GRB 3/16-.0015-4.4, MILC7438, MIL-C-7438, 5680-01-297-7919, 01-297-7919, 5680012977919, 012977919
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
56 | APR 07, 1989 | 01-297-7919 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-297-7919
Part Number | Cage Code | Manufacturer |
---|---|---|
MIL-C-7438GRB 3/16-.0015-4.4 | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-01-297-7919
Characteristic | Specifications |
---|---|
BASIC MATERIAL | ALUMINUM ALLOY, 5056 |
CELL CONDITION | EXPANDED |
CELL SIZE | 3/16 IN. |
CELL PERFORATION | NOT INCLUDED |
NOMINAL DENSITY RATING | 4.4 POUNDS PER CUBIC FOOT |
MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
RIBBON DIRECTION DIMENSION | 48.000 IN. |
DESIGNED RIBBON DIRECTION DIMENSION | 48.000 IN. |
TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
UNIT PACKAGE QUANTITY | 1 |
SPECIAL FEATURES | NOMINAL FOIL THICKNESS 0.0015 |
NONDEFINITIVE SPEC/STD DATA | B GRADE |