NSN 5680-01-419-1133
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-419-1133 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: PAA2.31410N.375+.005, PAA2.3-1/4-10N-.375+/-.005, 5680-01-419-1133, 01-419-1133, 5680014191133, 014191133
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | SEP 13, 1995 | 01-419-1133 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-419-1133
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| PAA2.3-1/4-10N-.375+/-.005 | 07542 | AMERICAN CYANAMID COINDUSTRIAL CHEMICALS AND PLASTICS |
Technical Data | NSN 5680-01-419-1133
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM ALLOY |
| CELL CONDITION | EXPANDED |
| FACE THICKNESS | 0.375 INCHES NOMINAL |
| CELL SIZE | 1/4 IN. |
| CELL PERFORATION | NOT INCLUDED |
| MAXIMUM DENSITY RATING | 2.3 POUNDS PER CUBIC FOOT |
| SPECIAL FEATURES | GAUGE: 0010N(NON PERFORATED); LG-28.000 W/TOLERANCES OF +3.000 -0.000; WD 96.000 W/TOLERANCES OF +4.000 -0.000; W/TOLERANCES OF +0.005 -0.005; SPEC. MIL-C-7438-G, AMEND 1, GR B |