NSN 5680-01-283-0092
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-283-0092 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: CR III145052.0015N3.428X9, CR III-1/4-5052-.0015N-3.4-28X9-, 3.41415N(15052H39), 3.4-1/4-15N(15052H39), MILC7438, MIL-C-7438, 114S250515, 114S2505-15, 5680-01-283-0092, 01-283-0092, 5680012830092, 012830092
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUL 27, 1988 | 01-283-0092 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-283-0092
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CR III-1/4-5052-.0015N-3.4-28X9- | 04621 | HEXCEL CORP |
| 3.4-1/4-15N(15052H39) | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| MIL-C-7438 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 114S2505-15 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 5680-01-283-0092
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | ALUMINUM |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 1/4 IN. |
| CELL DEPTH | 1.750 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 3.4 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 26.000 IN. |
| DESIGNED RIBBON DIRECTION DIMENSION | 28.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 96.000 IN. |
| SPECIAL FEATURES | USED IN C141 AIRCRAFT |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | DIFFERENTIATED BY LENGTH |