Part Details | METAL SHEET
9535-01-407-8847 A ferrous or nonferrous product with cross-sectional dimensions limited to those established in Appendix C, FIIG A131. Includes corrugated and perforated items. For items 0.005 inch or .125mm thick and less. see FOIL, METAL. For silver items see SILVER SHEET.
Alternate Parts: 6092SICXXP.125, 6092/SIC/XXP/.125, 9535-01-407-8847, 01-407-8847, 9535014078847, 014078847
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | FEB 07, 1995 | 01-407-8847 | 37015 ( SHEET, METAL ) |
REFERENCE DRAWINGS & PICTURES
ROUND
Cross Reference | NSN 9535-01-407-8847
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6092/SIC/XXP/.125 | 1N655 | DWA COMPOSITE SPECIALTIES, INC. |
Technical Data | NSN 9535-01-407-8847
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| FABRICATION METHOD | ANY ACCEPTABLE |
| MINIMUM TENSILE STRENGTH | 66000 POUNDS PER SQUARE INCH |
| MINIMUM YIELD STRENGTH | 57000 POUNDS PER SQUARE INCH |
| LENGTH | 50.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | 0 ROUND |
| WIDTH | 30.000 INCHES NOMINAL |
| CROSS-SECTIONAL THICKNESS | 0.1250 INCHES NOMINAL |
| SPECIAL FEATURES | F-16 AIRCRAFT:METAL MATRIX COMPOSITES COMPOSED OF TITANIUM 0.15,MANGANESE,0.15,ZINC 0.25,COPPER 0.7-1.0,OXYGEN 0.05-0.50,CHROMIUM 0.15,SILICON 0.4-0.8,MAGNESIUM 0.8-1.2,IRON 0.3,IMPURIYIES 0.15,ALUMINUM REMAINING;DISCONTINUOUSLY REINFORCED ALUMINUM SHEET;AIRCRAFT VENTRAL FINS |