Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-149-1371 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: A1145052002P10123542, A1-1-4-5052-002P1-012-35-42, MILC7438, MIL-C-7438, 5680-00-149-1371, 00-149-1371, 5680001491371, 001491371
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
56 | FEB 12, 1975 | 00-149-1371 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-149-1371
Part Number | Cage Code | Manufacturer |
---|---|---|
A1-1-4-5052-002P1-012-35-42 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-149-1371
Characteristic | Specifications |
---|---|
BASIC MATERIAL | ALUMINUM ALLOY, MIL-C-7438 |
CELL CONDITION | EXPANDED |
CELL SIZE | 1/4 IN. |
CELL DEPTH | 1.012 INCHES NOMINAL |
CELL PERFORATION | INCLUDED |
NOMINAL DENSITY RATING | 4.3 POUNDS PER CUBIC FOOT |
RIBBON DIRECTION DIMENSION | 35.000IN. |
DESIGNED RIBBON DIRECTION DIMENSION | 35.000IN. |
TRANSVERSE DIRECTION DIMENSION | 42.000IN. |
DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000IN. |
UNIT PACKAGE QUANTITY | 1 |
NONDEFINITIVE SPEC/STD DATA | B GRADE AND 1 CLASS |