NSN 5680-00-887-2873
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-00-887-2873 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: MILC8073 CL2TY1B, MIL-C-8073 CL2TY1B, 40767968, 40-767968, MILC8073, MIL-C-8073, 5680-00-887-2873, 00-887-2873, 5680008872873, 008872873
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JAN 01, 1962 | 00-887-2873 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-00-887-2873
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-C-8073 CL2TY1B | 80244 | GENERAL SERVICES ADMINISTRATIONFEDERAL SUPPLY SERVICE |
| 40-767968 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| MIL-C-8073 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5680-00-887-2873
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS FABRIC |
| CELL CONDITION | EXPANDED |
| CELL SIZE | 0.188 IN. |
| CELL DEPTH | 8.000 INCHES NOMINAL |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 5.5 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 7.0 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| RIBBON DIRECTION DIMENSION | 17.500 IN. |
| DESIGNED RIBBON DIRECTION DIMENSION | 17.500 IN. TO 19.500 IN. |
| TRANSVERSE DIRECTION DIMENSION | 36.000 IN. |
| DESIGNED TRANSVERSE DIRECTION DIMENSION | 80.000 IN. TO 104.000 IN. |
| UNIT PACKAGE QUANTITY | 10 |
| NONDEFINITIVE SPEC/STD DATA | 2 CLASS AND 1B TYPE |